- mffd_typewpSpecifies the finite differencing type for Jacobian-free solve types. Note that the default is wp (for Walker and Pernice).
Default:wp
C++ Type:MooseEnum
Controllable:No
Description:Specifies the finite differencing type for Jacobian-free solve types. Note that the default is wp (for Walker and Pernice).
- n_max_nonlinear_pingpong100The maximum number of times the non linear residual can ping pong before requesting halting the current evaluation and requesting timestep cut
Default:100
C++ Type:unsigned int
Controllable:No
Description:The maximum number of times the non linear residual can ping pong before requesting halting the current evaluation and requesting timestep cut
- nl_forced_its0The Number of Forced Nonlinear Iterations
Default:0
C++ Type:unsigned int
Controllable:No
Description:The Number of Forced Nonlinear Iterations
- petsc_optionsSingleton PETSc options
C++ Type:MultiMooseEnum
Controllable:No
Description:Singleton PETSc options
- petsc_options_inameNames of PETSc name/value pairs
C++ Type:MultiMooseEnum
Controllable:No
Description:Names of PETSc name/value pairs
- petsc_options_valueValues of PETSc name/value pairs (must correspond with "petsc_options_iname"
C++ Type:std::vector<std::string>
Controllable:No
Description:Values of PETSc name/value pairs (must correspond with "petsc_options_iname"
- skip_exception_checkFalseSpecifies whether or not to skip exception check
Default:False
C++ Type:bool
Controllable:No
Description:Specifies whether or not to skip exception check
- solve_typePJFNK: Preconditioned Jacobian-Free Newton Krylov JFNK: Jacobian-Free Newton Krylov NEWTON: Full Newton Solve FD: Use finite differences to compute Jacobian LINEAR: Solving a linear problem
C++ Type:MooseEnum
Controllable:No
Description:PJFNK: Preconditioned Jacobian-Free Newton Krylov JFNK: Jacobian-Free Newton Krylov NEWTON: Full Newton Solve FD: Use finite differences to compute Jacobian LINEAR: Solving a linear problem
- splittingTop-level splitting defining a hierarchical decomposition into subsystems to help the solver.
C++ Type:std::vector<std::string>
Controllable:No
Description:Top-level splitting defining a hierarchical decomposition into subsystems to help the solver.
- time0System time
Default:0
C++ Type:double
Controllable:No
Description:System time
- verboseFalseSet to true to print additional information
Default:False
C++ Type:bool
Controllable:No
Description:Set to true to print additional information
Steady
Executioner for steady-state simulations.
Overview
Steady is a general solver for discrete steady-state nonlinear or linear problem:
(1)By default the line-search Newton in PETSc is used with the PJFNK (preconditioned Jacobian-free Newton Krylov) method. At each Newton iteration the executioner solves
(2)where
is the Jacobian matrix evaluated at . Jacobian matrix depends on for general nonlinear problems while it is constant for linear problems. The right hand side is also typically referred to as the residual at of Eq. (1). The Krylov methods are employed for solving the above linear equation, which requires only the evaluation of the matrix-vector product . Within the MOOSE framework, the Jacobian-Free Newton Krylov method is used that approximates matrix vector products by the Finite-Difference like approximation:
(3)where the scalar value is chosen by PETSc automatically to approximate accurately for the linear solve. It is noted that for a linear problem of which can be expressed as , where matrix is the Jacobian independent on and is the right-hand-side vector, the right hand side of Eq. (3) is independent on . Section 5.5 of PETSc user's manual on matrix-free methods details the algorithm for choosing the value of . It is actually the PETSc option -mat_mffd_err controls the but not -snes_mf_err unless we set -snes_mf_version to 2 other than the default 1. This could be changed in future PETSc updates.
The Krylov methods typically also require an approximation of the actual Jacobian for pre-conditioning the Krylov solution at each linear iteration. Note, the preconditioning matrix is seldom the exact Jacobian because it would require too much computational time and memory to compute, and in some cases is simply impossible to compute. By default the type of Krylov method in use is GMRES because it does not have assumptions on the underlying Jacobian. The initial guess for each linear solve is always set to zero, which implies that the initial linear residual is the same of the nonlinear residual. The residual norm at each linear iteration is evaluated by PETSc, for instance, during updating the Hessenberg matrix if GMRES method is used. At the conclusion of the nonlinear iteration, the solution is updated as follows
(4)where is determined by the line-search algorithm. We can see that at each nonlinear or Newton iteration, we will need to update the preconditioning matrix and evaluate the residual with the updated solution. At each linear iteration, we simply need a residual evaluation and the operation of the preconditioner built from the preconditioning matrix. In PETSc the preconditioner type refers to the method to obtain an approximation of the inverse of and not a means to compute the elements of . It is noted that the default preconditioner type depends on the number of processors and also depends on the assembled preconditioning matrix . Typically incomplete LU (PCILU) is the default type with one processor and block Jacobi (PCBJACOBI) is the type with multiple processors. Consequently, you will not see the same convergence with the different number of processors. Note, there are two approximations in play here: (1) the Jacobian is approximated by a matrix that is easier to compute, and (2) the matrix is inverted approximately. The preconditioning matrix can be viewed with the PETSc option -ksp_view_pmat.
Solve Type
The general method in which the nonlinear system is solved is controled by the "solve_type" parameter. Below is a description of each of the options:
PJFNKis the default solve type. It makes the executioner perform Jacobian-free linear solves at each Newton iteration with the preconditioner built from the preconditioning matrix . By default, the preconditioning matrix is block-diagonal with each block corresponding to a single MOOSE variable without custom preconditioning, refer to Preconditioning. Off-diagonal Jacobian terms are ignored. It essentially activates the matrix-free Jacobian-vector products, and the preconditioning matrix.JFNKmeans there is no preconditioning during the Krylov solve. No Jacobian will be assembled. It essentially activates the matrix-free Jacobian-vector products and no preconditioning matrix.LINEARwill use PETSc control parameter-ksp_onlyto set the type of SNES for solving the linear system. Note that it only works when you have an exact Jacobian because it is not activating matrix-free calculations.NEWTONmeans PETSc will use the Jacobian provided by kernels (typically not exact) to do the Krylov solve. If the Jacobian is not exact, Newton update in Eq. (4) will not reduce the residual effectively and typically results into an unconverged Newton iteration.FDmeans the Jacobian is assembled via a finite differencing method. This is costly and should used only for testing purpose.
Preconditioning
Krylov methods need preconditioning to be efficient (or even effective!).
Even though the Jacobian is never formed, JFNK methods still require preconditioning.
MOOSE's automatic (without user intervention) preconditioning is fairly minimal.
Many options exist for implementing improved preconditioning in MOOSE.
Preconditioned JFNK
Using right preconditioning, solve
symbolically represents the preconditioning matrix or process
Inside GMRES, we only apply the action of on a vector
Right preconditioned matrix free version
PETSc Options
PETSc parameters can either be set on the command line or by using the "petsc_options", "petsc_options_iname", and "petsc_options_value" parameters. Several PETSc parameters that users could frequently use are listed below:
Common stand-alone petsc options
petsc_options | Description |
|---|---|
-snes_ksp_ew | Variable linear solve tolerance – useful for transient solves |
-help | Show PETSc options during the solve |
Common petsc options and values
petsc_options_iname | petsc_options_value | Description |
|---|---|---|
-pc_type | ilu | Default for serial |
bjacobi | Default for parallel with -sub_pc_type ilu | |
asm | Additive Schwartz with -sub_pc_type ilu | |
lu | Full LU, serial only! | |
gamg | PETSc Geometric AMG Preconditioner | |
hypre | Hypre, usually used with boomeramg | |
-sub_pc_type | ilu, lu, hypre | Can be used with bjacobi or asm |
-pc_hypre_type | boomeramg | Algebraic multigrid |
-pc_hypre_boomeramg (cont.) | "Information Threshold" for AMG process | |
_strong_threshold | 0.0 - 1.0 | (0.7 is auto set for 3D) |
-ksp_gmres_restart | # | Number of Krylov vectors to store |
Input Parameters
- accept_on_max_fixed_point_iterationFalseTrue to treat reaching the maximum number of fixed point iterations as converged.
Default:False
C++ Type:bool
Controllable:No
Description:True to treat reaching the maximum number of fixed point iterations as converged.
- auto_advanceFalseWhether to automatically advance sub-applications regardless of whether their solve converges, for transient executioners only.
Default:False
C++ Type:bool
Controllable:No
Description:Whether to automatically advance sub-applications regardless of whether their solve converges, for transient executioners only.
- custom_abs_tol1e-50The absolute nonlinear residual to shoot for during fixed point iterations. This check is performed based on postprocessor defined by the custom_pp residual.
Default:1e-50
C++ Type:double
Controllable:No
Description:The absolute nonlinear residual to shoot for during fixed point iterations. This check is performed based on postprocessor defined by the custom_pp residual.
- custom_ppPostprocessor for custom fixed point convergence check.
C++ Type:PostprocessorName
Controllable:No
Description:Postprocessor for custom fixed point convergence check.
- custom_rel_tol1e-08The relative nonlinear residual drop to shoot for during fixed point iterations. This check is performed based on the postprocessor defined by custom_pp residual.
Default:1e-08
C++ Type:double
Controllable:No
Description:The relative nonlinear residual drop to shoot for during fixed point iterations. This check is performed based on the postprocessor defined by custom_pp residual.
- direct_pp_valueFalseTrue to use direct postprocessor value (scaled by value on first iteration). False (default) to use difference in postprocessor value between fixed point iterations.
Default:False
C++ Type:bool
Controllable:No
Description:True to use direct postprocessor value (scaled by value on first iteration). False (default) to use difference in postprocessor value between fixed point iterations.
- disable_fixed_point_residual_norm_checkFalseDisable the residual norm evaluation thus the three parameters fixed_point_rel_tol, fixed_point_abs_tol and fixed_point_force_norms.
Default:False
C++ Type:bool
Controllable:No
Description:Disable the residual norm evaluation thus the three parameters fixed_point_rel_tol, fixed_point_abs_tol and fixed_point_force_norms.
- fixed_point_abs_tol1e-50The absolute nonlinear residual to shoot for during fixed point iterations. This check is performed based on the main app's nonlinear residual.
Default:1e-50
C++ Type:double
Controllable:No
Description:The absolute nonlinear residual to shoot for during fixed point iterations. This check is performed based on the main app's nonlinear residual.
- fixed_point_algorithmpicardThe fixed point algorithm to converge the sequence of problems.
Default:picard
C++ Type:MooseEnum
Options:picard, secant, steffensen
Controllable:No
Description:The fixed point algorithm to converge the sequence of problems.
- fixed_point_force_normsFalseForce the evaluation of both the TIMESTEP_BEGIN and TIMESTEP_END norms regardless of the existence of active MultiApps with those execute_on flags, default: false.
Default:False
C++ Type:bool
Controllable:No
Description:Force the evaluation of both the TIMESTEP_BEGIN and TIMESTEP_END norms regardless of the existence of active MultiApps with those execute_on flags, default: false.
- fixed_point_max_its1Specifies the maximum number of fixed point iterations.
Default:1
C++ Type:unsigned int
Controllable:No
Description:Specifies the maximum number of fixed point iterations.
- fixed_point_min_its1Specifies the minimum number of fixed point iterations.
Default:1
C++ Type:unsigned int
Controllable:No
Description:Specifies the minimum number of fixed point iterations.
- fixed_point_rel_tol1e-08The relative nonlinear residual drop to shoot for during fixed point iterations. This check is performed based on the main app's nonlinear residual.
Default:1e-08
C++ Type:double
Controllable:No
Description:The relative nonlinear residual drop to shoot for during fixed point iterations. This check is performed based on the main app's nonlinear residual.
- relaxation_factor1Fraction of newly computed value to keep.Set between 0 and 2.
Default:1
C++ Type:double
Controllable:No
Description:Fraction of newly computed value to keep.Set between 0 and 2.
- transformed_postprocessorsList of main app postprocessors to transform during fixed point iterations
C++ Type:std::vector<PostprocessorName>
Controllable:No
Description:List of main app postprocessors to transform during fixed point iterations
- transformed_variablesList of main app variables to transform during fixed point iterations
C++ Type:std::vector<std::string>
Controllable:No
Description:List of main app variables to transform during fixed point iterations
Fixed Point Iterations Parameters
- automatic_scalingFalseWhether to use automatic scaling for the variables.
Default:False
C++ Type:bool
Controllable:No
Description:Whether to use automatic scaling for the variables.
- compute_scaling_onceTrueWhether the scaling factors should only be computed once at the beginning of the simulation through an extra Jacobian evaluation. If this is set to false, then the scaling factors will be computed during an extra Jacobian evaluation at the beginning of every time step.
Default:True
C++ Type:bool
Controllable:No
Description:Whether the scaling factors should only be computed once at the beginning of the simulation through an extra Jacobian evaluation. If this is set to false, then the scaling factors will be computed during an extra Jacobian evaluation at the beginning of every time step.
- ignore_variables_for_autoscalingList of variables that do not participate in autoscaling.
C++ Type:std::vector<std::string>
Controllable:No
Description:List of variables that do not participate in autoscaling.
- off_diagonals_in_auto_scalingFalseWhether to consider off-diagonals when determining automatic scaling factors.
Default:False
C++ Type:bool
Controllable:No
Description:Whether to consider off-diagonals when determining automatic scaling factors.
- resid_vs_jac_scaling_param0A parameter that indicates the weighting of the residual vs the Jacobian in determining variable scaling parameters. A value of 1 indicates pure residual-based scaling. A value of 0 indicates pure Jacobian-based scaling
Default:0
C++ Type:double
Controllable:No
Description:A parameter that indicates the weighting of the residual vs the Jacobian in determining variable scaling parameters. A value of 1 indicates pure residual-based scaling. A value of 0 indicates pure Jacobian-based scaling
- scaling_group_variablesName of variables that are grouped together for determining scale factors. (Multiple groups can be provided, separated by semicolon)
C++ Type:std::vector<std::vector<std::string>>
Controllable:No
Description:Name of variables that are grouped together for determining scale factors. (Multiple groups can be provided, separated by semicolon)
Solver Variable Scaling Parameters Parameters
- compute_initial_residual_before_preset_bcsFalseUse the residual norm computed *before* preset BCs are imposed in relative convergence check
Default:False
C++ Type:bool
Controllable:No
Description:Use the residual norm computed *before* preset BCs are imposed in relative convergence check
- l_abs_tol1e-50Linear Absolute Tolerance
Default:1e-50
C++ Type:double
Controllable:No
Description:Linear Absolute Tolerance
- l_max_its10000Max Linear Iterations
Default:10000
C++ Type:unsigned int
Controllable:No
Description:Max Linear Iterations
- l_tol1e-05Linear Tolerance
Default:1e-05
C++ Type:double
Controllable:No
Description:Linear Tolerance
- nl_abs_div_tol1e+50Nonlinear Absolute Divergence Tolerance. A negative value disables this check.
Default:1e+50
C++ Type:double
Controllable:No
Description:Nonlinear Absolute Divergence Tolerance. A negative value disables this check.
- nl_abs_step_tol0Nonlinear Absolute step Tolerance
Default:0
C++ Type:double
Controllable:No
Description:Nonlinear Absolute step Tolerance
- nl_abs_tol1e-50Nonlinear Absolute Tolerance
Default:1e-50
C++ Type:double
Controllable:No
Description:Nonlinear Absolute Tolerance
- nl_div_tol1e+10Nonlinear Relative Divergence Tolerance. A negative value disables this check.
Default:1e+10
C++ Type:double
Controllable:No
Description:Nonlinear Relative Divergence Tolerance. A negative value disables this check.
- nl_max_funcs10000Max Nonlinear solver function evaluations
Default:10000
C++ Type:unsigned int
Controllable:No
Description:Max Nonlinear solver function evaluations
- nl_max_its50Max Nonlinear Iterations
Default:50
C++ Type:unsigned int
Controllable:No
Description:Max Nonlinear Iterations
- nl_rel_step_tol0Nonlinear Relative step Tolerance
Default:0
C++ Type:double
Controllable:No
Description:Nonlinear Relative step Tolerance
- nl_rel_tol1e-08Nonlinear Relative Tolerance
Default:1e-08
C++ Type:double
Controllable:No
Description:Nonlinear Relative Tolerance
- num_grids1The number of grids to use for a grid sequencing algorithm. This includes the final grid, so num_grids = 1 indicates just one solve in a time-step
Default:1
C++ Type:unsigned int
Controllable:No
Description:The number of grids to use for a grid sequencing algorithm. This includes the final grid, so num_grids = 1 indicates just one solve in a time-step
- snesmf_reuse_baseTrueSpecifies whether or not to reuse the base vector for matrix-free calculation
Default:True
C++ Type:bool
Controllable:No
Description:Specifies whether or not to reuse the base vector for matrix-free calculation
Solver Parameters
- contact_line_search_allowed_lambda_cuts2The number of times lambda is allowed to be cut in half in the contact line search. We recommend this number be roughly bounded by 0 <= allowed_lambda_cuts <= 3
Default:2
C++ Type:unsigned int
Controllable:No
Description:The number of times lambda is allowed to be cut in half in the contact line search. We recommend this number be roughly bounded by 0 <= allowed_lambda_cuts <= 3
- contact_line_search_ltolThe linear relative tolerance to be used while the contact state is changing between non-linear iterations. We recommend that this tolerance be looser than the standard linear tolerance
C++ Type:double
Controllable:No
Description:The linear relative tolerance to be used while the contact state is changing between non-linear iterations. We recommend that this tolerance be looser than the standard linear tolerance
- line_searchdefaultSpecifies the line search type (Note: none = basic)
Default:default
C++ Type:MooseEnum
Options:basic, bt, contact, cp, default, l2, none, project, shell
Controllable:No
Description:Specifies the line search type (Note: none = basic)
- line_search_packagepetscThe solver package to use to conduct the line-search
Default:petsc
C++ Type:MooseEnum
Options:petsc, moose
Controllable:No
Description:The solver package to use to conduct the line-search
Solver Line Search Parameters Parameters
- control_tagsAdds user-defined labels for accessing object parameters via control logic.
C++ Type:std::vector<std::string>
Controllable:No
Description:Adds user-defined labels for accessing object parameters via control logic.
- enableTrueSet the enabled status of the MooseObject.
Default:True
C++ Type:bool
Controllable:No
Description:Set the enabled status of the MooseObject.
- outputsVector of output names were you would like to restrict the output of variables(s) associated with this object
C++ Type:std::vector<OutputName>
Controllable:No
Description:Vector of output names were you would like to restrict the output of variables(s) associated with this object
Advanced Parameters
- max_xfem_update4294967295Maximum number of times to update XFEM crack topology in a step due to evolving cracks
Default:4294967295
C++ Type:unsigned int
Controllable:No
Description:Maximum number of times to update XFEM crack topology in a step due to evolving cracks
- update_xfem_at_timestep_beginFalseShould XFEM update the mesh at the beginning of the timestep
Default:False
C++ Type:bool
Controllable:No
Description:Should XFEM update the mesh at the beginning of the timestep
Xfem Fixed Point Iterations Parameters
Restart Parameters
Input Files
- (test/tests/multiapps/steffensen_postprocessor/steady_main.i)
- (test/tests/mesh/splitting/grid_from_generated.i)
- (test/tests/misc/check_error/function_conflict.i)
- (test/tests/kernels/array_kernels/standard_save_in.i)
- (test/tests/materials/derivative_material_interface/execution_order.i)
- (test/tests/kernels/scalar_constraint/scalar_constraint_bc.i)
- (modules/heat_conduction/test/tests/gap_heat_transfer_mortar/gap_heat_transfer_mortar.i)
- (test/tests/materials/derivative_material_interface/ad_derivative_parsed_material_zero.i)
- (test/tests/executioners/nl_forced_its/2d_diffusion_test.i)
- (test/tests/outputs/misc/default_names.i)
- (modules/porous_flow/test/tests/fluids/co2.i)
- (test/tests/relationship_managers/evaluable/edge_neighbors.i)
- (examples/ex13_functions/ex13.i)
- (test/tests/misc/check_error/bad_bc_test.i)
- (modules/heat_conduction/test/tests/gap_heat_transfer_mortar/modular_gap_heat_transfer_mortar_displaced_conduction.i)
- (test/tests/auxkernels/parsed_aux/parsed_aux_test.i)
- (modules/thermal_hydraulics/test/tests/jacobians/bcs/radiation_heat_flux_rz_bc/radiation_heat_flux_rz_bc.i)
- (modules/navier_stokes/test/tests/finite_volume/pins/mms/1d-rc-no-diffusion-strong-bc.i)
- (test/tests/vectorpostprocessors/extra_id_integral/extra_id_vpp.i)
- (test/tests/postprocessors/element_l2_norm/element_l2_norm.i)
- (test/tests/controls/time_periods/aux_kernels/enable_disable.i)
- (test/tests/materials/discrete/reset_warning.i)
- (test/tests/kernels/materialpropertyvalue/materialpropertyvalue.i)
- (test/tests/ics/check_error/two_ics_on_same_boundary.i)
- (test/tests/meshgenerators/gmsh_bcs/gmsh_bcs.i)
- (test/tests/transfers/multiapp_conservative_transfer/master_nearest_point.i)
- (test/tests/materials/derivative_material_interface/ad_execution_order.i)
- (test/tests/fvkernels/mms/mass-mom-mat-advection-diffusion/input.i)
- (test/tests/materials/has_material/has_boundary_prop.i)
- (test/tests/vectorpostprocessors/csv_reader/read_preic.i)
- (test/tests/functions/parsed/combined.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/mms/cylindrical/2d-rc.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/cylindrical/cartesian-version/2d-rc-no-slip-walls.i)
- (test/tests/misc/check_error/interface_kernel_with_aux_var.i)
- (test/tests/parser/multiple_inputs/diffusion1a.i)
- (test/tests/ics/check_error/two_ics_on_same_block.i)
- (modules/heat_conduction/test/tests/fvbcs/fv_thermal_resistance/test_functor.i)
- (modules/navier_stokes/test/tests/auxkernels/peclet-number-functor-aux/fe-thermal.i)
- (modules/geochemistry/test/tests/time_dependent_reactions/except3.i)
- (test/tests/bcs/ad_bc_preset_nodal/bc_preset_nodal.i)
- (test/tests/vectorpostprocessors/elements_along_plane/1d.i)
- (test/tests/bcs/ad_penalty_dirichlet_bc/function_penalty_dirichlet_bc_test.i)
- (modules/navier_stokes/test/tests/finite_element/ins/lid_driven/ad_lid_driven_action_stabilized_steady.i)
- (modules/porous_flow/test/tests/fluids/ideal_gas.i)
- (modules/porous_flow/test/tests/thermal_conductivity/ThermalCondPorosity01.i)
- (modules/heat_conduction/test/tests/verify_against_analytical/2d_steady_state.i)
- (modules/heat_conduction/test/tests/radiation_transfer_action/radiative_transfer_action_external_boundary.i)
- (test/tests/outputs/format/output_test_nemesis.i)
- (test/tests/materials/has_material/has_block_prop.i)
- (modules/navier_stokes/test/tests/auxkernels/reynolds-number-functor-aux/fe.i)
- (modules/heat_conduction/test/tests/gap_heat_transfer_mortar_action/modular_gap_heat_transfer_mortar_displaced_radiation_conduction_action.i)
- (test/tests/controls/time_periods/dampers/enable_disable.i)
- (test/tests/markers/combo_marker/combo_marker_test.i)
- (modules/navier_stokes/test/tests/finite_element/ins/mms/supg/supg_mms_test.i)
- (modules/fluid_properties/test/tests/calorically_imperfect_gas/test.i)
- (python/peacock/tests/input_tab/InputTreeWriter/gold/simple_diffusion_inactive.i)
- (test/tests/materials/functor_properties/functor-vector-mat-props.i)
- (test/tests/executioners/steady_time/steady_time.i)
- (modules/heat_conduction/test/tests/heat_conduction/2d_quadrature_gap_heat_transfer/nonmatching.i)
- (modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/rz_cone_by_parts_steady_stabilized.i)
- (modules/heat_conduction/test/tests/view_factors_symmetry/cavity_with_pillars_symmetry_bc.i)
- (modules/navier_stokes/examples/pipe_mixing_length/pipe_mixing_length.i)
- (test/tests/kernels/ad_value/generic_value.i)
- (modules/heat_conduction/test/tests/gap_heat_transfer_mortar/bc_gap_heat_transfer_displaced_conduction.i)
- (tutorials/tutorial01_app_development/step05_kernel_object/problems/pressure_diffusion.i)
- (test/tests/geomsearch/2d_penetration_locator/2d_penetration_locator_test.i)
- (modules/thermal_hydraulics/test/tests/functions/smooth_transition/space.i)
- (test/tests/postprocessors/area_pp/area_pp.i)
- (modules/ray_tracing/test/tests/raybcs/errors/raybc_errors.i)
- (test/tests/dirackernels/constant_point_source/2d_point_source.i)
- (test/tests/meshgenerators/sidesets_bounding_box_generator/overlapping_sidesets.i)
- (modules/porous_flow/test/tests/poroperm/PermFromPoro04.i)
- (test/tests/controls/error/non_existing_dependency.i)
- (test/tests/transfers/multiapp_conservative_transfer/sub_conservative_transfer.i)
- (test/tests/restart/pointer_restart_errors/pointer_store_error.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/action/errors/2d-rc-error-action.i)
- (modules/navier_stokes/test/tests/finite_volume/fvkernels/flow_diode/friction.i)
- (test/tests/variables/fe_hier/hier-3-1d.i)
- (modules/reactor/test/tests/meshgenerators/extra_element_id_copy_generator/copy_elem_id_test.i)
- (modules/heat_conduction/test/tests/heat_conduction_patch/heat_conduction_patch_hex20.i)
- (test/tests/kernels/forcing_function/forcing_function_error_check.i)
- (test/tests/materials/material/qp_material.i)
- (test/tests/mesh_modifiers/add_extra_nodeset/extra_nodeset_coord_test.i)
- (modules/geochemistry/test/tests/geochemistry_quantity_aux/except5.i)
- (test/tests/materials/piecewise_by_block_material/test_functor.i)
- (test/tests/reporters/declare_initial_setup/declare_initial_setup_with_get.i)
- (modules/misc/test/tests/kernels/thermo_diffusion/ad_thermo_diffusion.i)
- (modules/porous_flow/test/tests/gravity/fully_saturated_grav01a.i)
- (test/tests/postprocessors/nodal_extreme_value/block_nodal_pps_test.i)
- (test/tests/userobjects/element_quality_check/bypass_warning.i)
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- (test/tests/bcs/penalty_dirichlet_bc/function_penalty_dirichlet_bc_test.i)
- (modules/heat_conduction/test/tests/view_factors/view_factor_3d.i)
- (test/tests/materials/types/test.i)
- (test/tests/vectorpostprocessors/line_material_sampler/line_material_real_sampler.i)
- (modules/heat_conduction/test/tests/gap_heat_transfer_mortar/modular_gap_heat_transfer_mortar_displaced_conduction_function.i)
- (modules/porous_flow/test/tests/gravity/fully_saturated_upwinded_grav01c_action.i)
- (modules/heat_conduction/test/tests/fvbcs/fv_thermal_resistance/test.i)
- (test/tests/transfers/multiapp_nearest_node_transfer/source_boundary_sub.i)
- (modules/thermal_hydraulics/test/tests/materials/ad_material_function_product/ad_material_function_product.i)
- (test/tests/mesh/custom_partitioner/custom_linear_partitioner_test.i)
- (test/tests/dirackernels/point_caching/point_caching.i)
- (test/tests/misc/check_error/bad_kernel_action.i)
- (test/tests/kernels/tag_errors/no_tags/no_tags.i)
- (test/tests/outputs/debug/show_var_residual_norms.i)
- (test/tests/misc/check_error/incomplete_kernel_block_coverage_test.i)
- (test/tests/mesh/concentric_circle_mesh/concentric_circle_mesh.i)
- (modules/porous_flow/test/tests/fluids/simple_fluid_hr.i)
- (test/tests/meshgenerators/patterned_mesh_generator/patterned_mesh_generator.i)
- (test/tests/userobjects/layered_integral/average_sample.i)
- (test/tests/scaling/residual-based/residual-based-two-var.i)
- (test/tests/partitioners/hierarchical_grid_partitioner/hierarchical_grid_partitioner.i)
- (python/peacock/tests/input_tab/InputTree/gold/simple_diffusion_vp.i)
- (test/tests/materials/get_material_property_names/get_material_property_any_block_id.i)
- (test/tests/misc/block_boundary_material_check/bc_check.i)
- (test/tests/kernels/ad_value/ad_value.i)
- (test/tests/relationship_managers/check_coupling_functor/check_no_mallocs.i)
- (test/tests/misc/block_boundary_material_check/dgkernel_check_block.i)
- (test/tests/restart/pointer_restart_errors/pointer_load_error2.i)
- (test/tests/mortar/continuity-3d-non-conforming/continuity_mixed.i)
- (test/tests/usability/bad.i)
- (test/tests/outputs/perf_graph/perf_graph.i)
- (modules/geochemistry/test/tests/time_dependent_reactions/except2.i)
- (test/tests/restrictable/undefined_ids/undefined_block_kernel.i)
- (modules/fluid_properties/test/tests/methane/methane.i)
- (test/tests/controls/dependency/test.i)
- (modules/tensor_mechanics/tutorials/basics/part_1.2.i)
- (modules/navier_stokes/test/tests/finite_element/ins/hydrostatic/gravity.i)
- (test/tests/postprocessors/element_average_material_property/element_average_material_property.i)
- (test/tests/meshgenerators/rename_boundary_generator/rename_boundary.i)
- (test/tests/problems/no_kernel_coverage_check/no_coverage_check.i)
- (modules/stochastic_tools/examples/parameter_study/nonlin_diff_react/nonlin_diff_react_sub.i)
- (test/tests/indicators/gradient_jump_indicator/gradient_jump_indicator_test.i)
- (test/tests/auxkernels/gap_value/gap_value_subdomain_restricted.i)
- (test/tests/transfers/multiapp_copy_transfer/errors/sub.i)
- (test/tests/preconditioners/hmg/diffusion_hmg.i)
- (test/tests/ics/random_ic_test/random_ic_test.i)
- (test/tests/multiapps/picard/pseudo_transient_picard_master.i)
- (test/tests/auxkernels/vector_magnitude/vector_magnitude.i)
- (test/tests/outputs/exodus/exodus.i)
- (test/tests/auxkernels/vectorpostprocessor/vectorpostprocessor.i)
- (python/peacock/tests/common/simple_diffusion2.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/cylindrical/2d-rc-slip.i)
- (test/tests/mesh/named_entities/named_entities_test.i)
- (modules/tensor_mechanics/examples/cframe_iga/cframe_iga.i)
- (modules/navier_stokes/test/tests/finite_volume/cns/straight_channel_porosity_step/hllc.i)
- (test/tests/bcs/1d_neumann/1d_neumann.i)
- (test/tests/variables/fe_hier/hier-2-3d.i)
- (modules/tensor_mechanics/test/tests/ad_linear_elasticity/linear_elastic_material.i)
- (test/tests/markers/uniform_marker/uniform_marker.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/advection-schemes/test.i)
- (modules/geochemistry/test/tests/equilibrium_models/HCl_no_action.i)
- (modules/heat_conduction/test/tests/code_verification/cartesian_test_no4.i)
- (test/tests/fvkernels/mms/skewness-correction/diffusion/skewed.i)
- (test/tests/preconditioners/fdp/fdp_test.i)
- (tutorials/tutorial01_app_development/step06_input_params/test/tests/kernels/simple_diffusion/simple_diffusion.i)
- (test/tests/userobjects/layered_side_integral/layered_side_average.i)
- (modules/tensor_mechanics/test/tests/gravity/material_vector_body_force.i)
- (modules/tensor_mechanics/test/tests/lagrangian/total/stabilization/cook_large.i)
- (modules/navier_stokes/test/tests/finite_element/ins/lid_driven/ad_lid_driven_stabilized_action.i)
- (test/tests/postprocessors/difference_pps/difference_depend_check.i)
- (modules/ray_tracing/test/tests/traceray/internal_sidesets/internal_sidesets_2d.i)
- (test/tests/bcs/ad_1d_neumann/from_cubit.i)
- (test/tests/mesh_modifiers/assign_element_subdomain_id/quad_with_subdomainid_test.i)
- (test/tests/kernels/ad_reaction/ad_reaction.i)
- (test/tests/dgkernels/ad_dg_diffusion/2d_diffusion_ad_dg_test.i)
- (test/tests/functions/image_function/moose_logo_test_2D.i)
- (test/tests/materials/discrete/recompute2.i)
- (test/tests/materials/functor_properties/wrong-type.i)
- (modules/ray_tracing/test/tests/actions/add_raykernel_action/add_raykernel_action.i)
- (test/tests/parser/param_substitution/unit_conversion.i)
- (test/tests/misc/check_error/function_file_test11.i)
- (modules/thermal_hydraulics/test/tests/jacobians/bcs/convection_heat_transfer_bc/convection_heat_transfer_bc.i)
- (test/tests/mesh/high_order_elems/high_order_elems.i)
- (modules/navier_stokes/test/tests/finite_element/ins/scalar_adr/supg/tauOpt.i)
- (test/tests/outputs/json/distributed/distributed.i)
- (test/tests/outputs/debug/show_var_residual_norms_debug.i)
- (test/tests/misc/check_error/checked_pointer_param_test.i)
- (modules/fluid_properties/test/tests/auxkernels/stagnation_pressure_aux.i)
- (test/tests/outputs/csv/csv_sort.i)
- (test/tests/misc/save_in/save_in_test.i)
- (test/tests/indicators/value_jump_indicator/value_jump_indicator_test.i)
- (modules/tensor_mechanics/test/tests/ad_action/two_block.i)
- (test/tests/interfacekernels/1d_interface/reaction_1D_steady.i)
- (test/tests/materials/interface_material/interface_value_material.i)
- (tutorials/darcy_thermo_mech/step03_darcy_material/tests/materials/packed_column/packed_column.i)
- (modules/fluid_properties/test/tests/auxkernels/specific_enthalpy_aux.i)
- (test/tests/userobjects/layered_average/layered_average_bounds.i)
- (test/tests/functions/parsed/vals_error.i)
- (test/tests/tag/tag_interface_kernels.i)
- (test/tests/materials/material/bnd_material_test.i)
Child Objects
solve_type
C++ Type:MooseEnum
Options:PJFNK, JFNK, NEWTON, FD, LINEAR
Controllable:No
Description:PJFNK: Preconditioned Jacobian-Free Newton Krylov JFNK: Jacobian-Free Newton Krylov NEWTON: Full Newton Solve FD: Use finite differences to compute Jacobian LINEAR: Solving a linear problem
petsc_options
C++ Type:MultiMooseEnum
Options:-dm_moose_print_embedding, -dm_view, -ksp_converged_reason, -ksp_gmres_modifiedgramschmidt, -ksp_monitor, -ksp_monitor_snes_lg-snes_ksp_ew, -ksp_snes_ew, -snes_converged_reason, -snes_ksp, -snes_ksp_ew, -snes_linesearch_monitor, -snes_mf, -snes_mf_operator, -snes_monitor, -snes_test_display, -snes_view
Controllable:No
Description:Singleton PETSc options
petsc_options_iname
C++ Type:MultiMooseEnum
Options:-ksp_atol, -ksp_gmres_restart, -ksp_max_it, -ksp_pc_side, -ksp_rtol, -ksp_type, -mat_fd_coloring_err, -mat_fd_type, -mat_mffd_type, -pc_asm_overlap, -pc_factor_levels, -pc_factor_mat_ordering_type, -pc_hypre_boomeramg_grid_sweeps_all, -pc_hypre_boomeramg_max_iter, -pc_hypre_boomeramg_strong_threshold, -pc_hypre_type, -pc_type, -snes_atol, -snes_linesearch_type, -snes_ls, -snes_max_it, -snes_rtol, -snes_divergence_tolerance, -snes_type, -sub_ksp_type, -sub_pc_type
Controllable:No
Description:Names of PETSc name/value pairs
petsc_options_value
C++ Type:std::vector<std::string>
Controllable:No
Description:Values of PETSc name/value pairs (must correspond with "petsc_options_iname"
(test/tests/multiapps/steffensen_postprocessor/steady_main.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
parallel_type = replicated
uniform_refine = 1
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[source]
type = BodyForce
variable = u
value = 1
[]
[]
[BCs]
[left]
type = PostprocessorDirichletBC
variable = u
boundary = left
postprocessor = 'from_sub'
[]
[]
[Postprocessors]
[from_sub]
type = Receiver
default = 0
[]
[to_sub]
type = SideAverageValue
variable = u
boundary = right
[]
[average]
type = ElementAverageValue
variable = u
[]
[]
[Executioner]
type = Steady
# Solve parameters
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
nl_abs_tol = 1e-14
# App coupling parameters
fixed_point_algorithm = 'steffensen'
fixed_point_max_its = 100
transformed_postprocessors = 'from_sub'
[]
[Outputs]
csv = true
exodus = false
[]
[MultiApps]
[sub]
type = FullSolveMultiApp
app_type = MooseTestApp
positions = '0 0 0'
input_files = steady_sub.i
clone_master_mesh = true
execute_on = 'timestep_begin'
transformed_postprocessors = 'from_main'
[]
[]
[Transfers]
[left_from_sub]
type = MultiAppPostprocessorTransfer
from_multi_app = sub
from_postprocessor = 'to_main'
to_postprocessor = 'from_sub'
reduction_type = 'average'
[]
[right_to_sub]
type = MultiAppPostprocessorTransfer
to_multi_app = sub
from_postprocessor = 'to_sub'
to_postprocessor = 'from_main'
[]
[]
(test/tests/mesh/splitting/grid_from_generated.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[Partitioner]
type = GridPartitioner
nx = 2
ny = 2
nz = 1
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
[AuxVariables]
[pid]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[pid_aux]
type = ProcessorIDAux
variable = pid
execute_on = 'INITIAL'
[]
[]
(test/tests/misc/check_error/function_conflict.i)
# A function name that could be interpreted as a ParsedFunction
[Mesh]
type = GeneratedMesh
dim = 2
[]
[Functions]
[./x]
type = ConstantFunction
[../]
[]
[Variables]
[./var]
[../]
[]
[ICs]
[./dummy]
type = FunctionIC
variable = var
function = x
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = var
[../]
[]
[Executioner]
type = Steady
[]
(test/tests/kernels/array_kernels/standard_save_in.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 4
ny = 4
[]
[subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '0.5 0.5 0'
top_right = '1 1 0'
block_id = 1
[]
[]
[Variables]
[u_0]
order = FIRST
family = L2_LAGRANGE
[]
[u_1]
order = FIRST
family = L2_LAGRANGE
[]
[]
[AuxVariables]
[u_diff_save_in_0]
order = FIRST
family = L2_LAGRANGE
[]
[u_diff_save_in_1]
order = FIRST
family = L2_LAGRANGE
[]
[u_vacuum_save_in_0]
order = FIRST
family = L2_LAGRANGE
[]
[u_vacuum_save_in_1]
order = FIRST
family = L2_LAGRANGE
[]
[u_dg_save_in_0]
order = FIRST
family = L2_LAGRANGE
[]
[u_dg_save_in_1]
order = FIRST
family = L2_LAGRANGE
[]
[u_diff_diag_save_in_0]
order = FIRST
family = L2_LAGRANGE
[]
[u_diff_diag_save_in_1]
order = FIRST
family = L2_LAGRANGE
[]
[u_vacuum_diag_save_in_0]
order = FIRST
family = L2_LAGRANGE
[]
[u_vacuum_diag_save_in_1]
order = FIRST
family = L2_LAGRANGE
[]
[u_dg_diag_save_in_0]
order = FIRST
family = L2_LAGRANGE
[]
[u_dg_diag_save_in_1]
order = FIRST
family = L2_LAGRANGE
[]
[]
[Kernels]
[diff0]
type = MatCoefDiffusion
variable = u_0
conductivity = dc
save_in = u_diff_save_in_0
diag_save_in = u_diff_diag_save_in_0
[]
[diff1]
type = Diffusion
variable = u_1
save_in = u_diff_save_in_1
diag_save_in = u_diff_diag_save_in_1
[]
[reaction0]
type = CoefReaction
variable = u_0
[]
[reaction1]
type = CoefReaction
variable = u_1
[]
[reaction01]
type = CoupledForce
variable = u_1
v = u_0
coef = 0.1
[]
[]
[DGKernels]
[dgdiff0]
type = DGDiffusion
variable = u_0
diff = dc
sigma = 4
epsilon = 1
save_in = u_dg_save_in_0
diag_save_in = u_dg_diag_save_in_0
[]
[dgdiff1]
type = DGDiffusion
variable = u_1
sigma = 4
epsilon = 1
save_in = u_dg_save_in_1
diag_save_in = u_dg_diag_save_in_1
[]
[]
[BCs]
[left0]
type = VacuumBC
variable = u_0
boundary = 1
save_in = u_vacuum_save_in_0
diag_save_in = u_vacuum_diag_save_in_0
[]
[left1]
type = VacuumBC
variable = u_1
boundary = 1
save_in = u_vacuum_save_in_1
diag_save_in = u_vacuum_diag_save_in_1
[]
[right0]
type = PenaltyDirichletBC
variable = u_0
boundary = 2
value = 1
penalty = 4
[]
[right1]
type = PenaltyDirichletBC
variable = u_1
boundary = 2
value = 2
penalty = 4
[]
[]
[Materials]
[dc0]
type = GenericConstantMaterial
block = 0
prop_names = dc
prop_values = 1
[]
[dc1]
type = GenericConstantMaterial
block = 1
prop_names = dc
prop_values = 2
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Postprocessors]
[intu0]
type = ElementIntegralVariablePostprocessor
variable = u_0
[]
[intu1]
type = ElementIntegralVariablePostprocessor
variable = u_1
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
file_base = array_save_in_out
exodus = true
[]
(test/tests/materials/derivative_material_interface/execution_order.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Materials]
# fetch the properties first...
[./client]
type = DerivativeMaterialInterfaceTestClient
block = 0
[../]
# ...then declare them!
[./provider]
type = DerivativeMaterialInterfaceTestProvider
block = 0
outputs = exodus
output_properties = 'dprop/db dprop/da d^2prop/dadb d^2prop/dadc d^3prop/dadbdc'
[../]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Debug]
show_material_props = true
[]
[Outputs]
exodus = true
[]
(test/tests/kernels/scalar_constraint/scalar_constraint_bc.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 3
ny = 3
elem_type = QUAD4
[]
# NL
[Variables]
[./u]
family = LAGRANGE
order = FIRST
[../]
[./alpha]
family = SCALAR
order = FIRST
initial_condition = 1
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[ScalarKernels]
[./alpha_ced]
type = AlphaCED
variable = alpha
value = 10
[../]
[]
[BCs]
[./left]
type = ScalarVarBC
variable = u
boundary = '3'
alpha = alpha
[../]
[./right]
type = DirichletBC
variable = u
boundary = '1'
value = 0
[../]
[]
[Preconditioning]
active = 'pc'
[./pc]
type = SMP
full = true
solve_type = 'PJFNK'
[../]
[./FDP_PJFNK]
type = FDP
full = true
solve_type = 'PJFNK'
# These options **together** cause a zero pivot in this problem, even without SUPG terms.
# But using either option alone appears to be OK.
# petsc_options_iname = '-mat_fd_coloring_err -mat_fd_type'
# petsc_options_value = '1.e-10 ds'
petsc_options_iname = '-mat_fd_coloring_err'
petsc_options_value = '1.e-10'
# petsc_options_iname = '-mat_fd_type'
# petsc_options_value = 'ds'
[../]
[] # End preconditioning block
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
hide = alpha
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_mortar/gap_heat_transfer_mortar.i)
[Mesh]
[file]
type = FileMeshGenerator
file = 2blk-gap.e
[]
[secondary]
type = LowerDBlockFromSidesetGenerator
sidesets = '101'
new_block_id = '10001'
new_block_name = 'secondary_lower'
input = file
[]
[primary]
type = LowerDBlockFromSidesetGenerator
sidesets = '100'
new_block_id = '10000'
new_block_name = 'primary_lower'
input = secondary
[]
[]
[Problem]
kernel_coverage_check = false
material_coverage_check = false
[]
[Variables]
[./temp]
order = FIRST
family = LAGRANGE
block = '1 2'
[../]
[./lm]
order = FIRST
family = LAGRANGE
block = 'secondary_lower'
[../]
[]
[Materials]
[./left]
type = HeatConductionMaterial
block = 1
thermal_conductivity = 1000
specific_heat = 1
[../]
[./right]
type = HeatConductionMaterial
block = 2
thermal_conductivity = 500
specific_heat = 1
[../]
[]
[Kernels]
[./hc]
type = HeatConduction
variable = temp
use_displaced_mesh = false
block = '1 2'
[../]
[]
[Constraints]
[./ced]
type = GapConductanceConstraint
variable = lm
secondary_variable = temp
k = 100
primary_boundary = 100
primary_subdomain = 10000
secondary_boundary = 101
secondary_subdomain = 10001
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = temp
boundary = 'left'
value = 1
[../]
[./right]
type = DirichletBC
variable = temp
boundary = 'right'
value = 0
[../]
[]
[Preconditioning]
[./fmp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
nl_rel_tol = 1e-11
[]
[Outputs]
exodus = true
[]
(test/tests/materials/derivative_material_interface/ad_derivative_parsed_material_zero.i)
[Problem]
solve = false
[]
[Mesh]
type = GeneratedMesh
dim = 2
[]
[Variables]
[eta]
[]
[]
[Materials]
[F]
type = ADDerivativeParsedMaterial
args = 'eta'
function = 'eta+5'
derivative_order = 3
outputs = exodus
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/executioners/nl_forced_its/2d_diffusion_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
# BCs cannot be preset due to Jacobian test
active = 'left right'
[./left]
type = DirichletBC
variable = u
preset = false
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
preset = false
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
nl_forced_its = 2
nl_abs_tol = 1e-10
nl_rel_tol = 1e-50
solve_type = 'NEWTON'
[]
(test/tests/outputs/misc/default_names.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[./oversample]
type = Exodus
refinements = 1
[../]
[]
(modules/porous_flow/test/tests/fluids/co2.i)
# Test the density and viscosity calculated by the simple CO2 Material
# Pressure 5 MPa
# Temperature 50C
# These conditions correspond to the gas phase
# CO2 density should equal 104 kg/m^3 (NIST webbook)
# CO2 viscosity should equal 0.000017345 Pa.s (NIST webbook)
# Results are within expected accuracy
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[]
[Variables]
[pp]
initial_condition = 5e6
[]
[]
[Kernels]
[dummy]
type = Diffusion
variable = pp
[]
[]
[AuxVariables]
[temp]
initial_condition = 50
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
temperature = temp
[]
[ppss]
type = PorousFlow1PhaseFullySaturated
porepressure = pp
[]
[co2]
type = PorousFlowSingleComponentFluid
temperature_unit = Celsius
fp = co2
phase = 0
[]
[]
[Modules]
[FluidProperties]
[co2]
type = CO2FluidProperties
[]
[]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Postprocessors]
[pressure]
type = ElementIntegralVariablePostprocessor
variable = pp
[]
[temperature]
type = ElementIntegralVariablePostprocessor
variable = temp
[]
[density]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_fluid_phase_density_qp0'
[]
[viscosity]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_viscosity_qp0'
[]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = co2
csv = true
[]
(test/tests/relationship_managers/evaluable/edge_neighbors.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 8
ny = 8
# We are testing geometric ghosted functors
# so we have to use distributed mesh
parallel_type = distributed
[]
[GlobalParams]
order = CONSTANT
family = MONOMIAL
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[ghosting0]
[]
[ghosting1]
[]
[ghosting2]
[]
[proc]
[]
[]
[AuxKernels]
[ghosting0]
type = ElementUOAux
variable = ghosting0
element_user_object = ghosting_uo0
field_name = "ghosted"
execute_on = initial
[]
[ghosting1]
type = ElementUOAux
variable = ghosting1
element_user_object = ghosting_uo1
field_name = "ghosted"
execute_on = initial
[]
[ghosting2]
type = ElementUOAux
variable = ghosting2
element_user_object = ghosting_uo2
field_name = "ghosted"
execute_on = initial
[]
[proc]
type = ProcessorIDAux
variable = proc
execute_on = initial
[]
[]
[UserObjects]
[ghosting_uo0]
type = ElemSideNeighborLayersTester
execute_on = initial
element_side_neighbor_layers = 2
rank = 0
[]
[ghosting_uo1]
type = ElemSideNeighborLayersTester
execute_on = initial
element_side_neighbor_layers = 2
rank = 1
[]
[ghosting_uo2]
type = ElemSideNeighborLayersTester
execute_on = initial
element_side_neighbor_layers = 2
rank = 2
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
[Problem]
solve = false
kernel_coverage_check = false
[]
(examples/ex13_functions/ex13.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 100
ny = 100
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
[]
[Variables]
[./forced]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
# A ParsedFunction allows us to supply analytic expressions
# directly in the input file
[./bc_func]
type = ParsedFunction
value = sin(alpha*pi*x)
vars = 'alpha'
vals = '16'
[../]
# This function is an actual compiled function
# We could have used ParsedFunction for this as well
[./forcing_func]
type = ExampleFunction
alpha = 16
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = forced
[../]
# This Kernel can take a function name to use
[./forcing]
type = BodyForce
variable = forced
function = forcing_func
[../]
[]
[BCs]
# The BC can take a function name to use
[./all]
type = FunctionDirichletBC
variable = forced
boundary = 'bottom right top left'
function = bc_func
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(test/tests/misc/check_error/bad_bc_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
# Test for bad BC
[./left]
type = Foo
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_mortar/modular_gap_heat_transfer_mortar_displaced_conduction.i)
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
[file]
type = FileMeshGenerator
file = 2blk-gap.e
[]
[secondary]
type = LowerDBlockFromSidesetGenerator
sidesets = '101'
new_block_id = 10001
new_block_name = 'secondary_lower'
input = file
[]
[primary]
type = LowerDBlockFromSidesetGenerator
sidesets = '100'
new_block_id = 10000
new_block_name = 'primary_lower'
input = secondary
[]
allow_renumbering = false
[]
[Problem]
kernel_coverage_check = false
material_coverage_check = false
[]
[Variables]
[temp]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[disp_x]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[disp_y]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[lm]
order = FIRST
family = LAGRANGE
block = 'secondary_lower'
[]
[]
[Materials]
[left]
type = ADHeatConductionMaterial
block = 1
thermal_conductivity = 0.01
specific_heat = 1
[]
[right]
type = ADHeatConductionMaterial
block = 2
thermal_conductivity = 0.005
specific_heat = 1
[]
[]
[Kernels]
[hc_displaced_block]
type = ADHeatConduction
variable = temp
use_displaced_mesh = true
block = '1'
[]
[hc_undisplaced_block]
type = ADHeatConduction
variable = temp
use_displaced_mesh = false
block = '2'
[]
[disp_x]
type = Diffusion
variable = disp_x
block = '1 2'
[]
[disp_y]
type = Diffusion
variable = disp_y
block = '1 2'
[]
[]
[UserObjects]
[conduction]
type = GapFluxModelConduction
temperature = temp
boundary = 100
gap_conductivity = 10.0
[]
[]
[Constraints]
[ced]
type = ModularGapConductanceConstraint
variable = lm
secondary_variable = temp
use_displaced_mesh = true
primary_boundary = 100
primary_subdomain = 10000
secondary_boundary = 101
secondary_subdomain = 10001
gap_flux_models = conduction
[]
[]
[BCs]
[left]
type = DirichletBC
variable = temp
boundary = 'left'
value = 100
[]
[right]
type = DirichletBC
variable = temp
boundary = 'right'
value = 0
[]
[left_disp_x]
type = DirichletBC
preset = false
variable = disp_x
boundary = 'left'
value = .1
[]
[right_disp_x]
type = DirichletBC
preset = false
variable = disp_x
boundary = 'right'
value = 0
[]
[bottom_disp_y]
type = DirichletBC
preset = false
variable = disp_y
boundary = 'bottom'
value = 0
[]
[]
[Preconditioning]
[fmp]
type = SMP
full = true
solve_type = 'NEWTON'
[]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-11
nl_abs_tol = 1.0e-10
[]
[VectorPostprocessors]
[NodalTemperature]
type = NodalValueSampler
sort_by = id
boundary = '100 101'
variable = 'temp'
[]
[]
[Outputs]
exodus = false
csv = true
[]
(test/tests/auxkernels/parsed_aux/parsed_aux_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 10
ny = 10
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
[]
[v]
order = FIRST
family = LAGRANGE
[]
[]
[AuxVariables]
[parsed]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
[diff_u]
type = Diffusion
variable = u
[]
[diff_v]
type = Diffusion
variable = v
[]
[]
[BCs]
[left_u]
type = DirichletBC
variable = u
boundary = 2
value = 0
[]
[right_u]
type = DirichletBC
variable = u
boundary = 0
value = 1
[]
[left_v]
type = DirichletBC
variable = v
boundary = 3
value = 0
[]
[right_v]
type = DirichletBC
variable = v
boundary = 1
value = 1
[]
[]
[Bounds]
[u_bounds]
type = ParsedAux
variable = parsed
args = 'u v'
function = '(u-0.5)^3*v'
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/thermal_hydraulics/test/tests/jacobians/bcs/radiation_heat_flux_rz_bc/radiation_heat_flux_rz_bc.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
[]
[Variables]
[T]
initial_condition = 1000
[]
[]
[BCs]
[bc]
type = RadiativeHeatFluxRZBC
variable = T
boundary = 2
Tinfinity = 1500
boundary_emissivity = 0.3
view_factor = 0.5
axis_point = '0 0 0'
axis_dir = '1 0 0'
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Problem]
kernel_coverage_check = false
[]
[Executioner]
type = Steady
petsc_options = '-snes_test_jacobian'
petsc_options_iname = '-snes_test_error'
petsc_options_value = '1e-8'
[]
(modules/navier_stokes/test/tests/finite_volume/pins/mms/1d-rc-no-diffusion-strong-bc.i)
mu=1e-15
rho=1.1
advected_interp_method='upwind'
velocity_interp_method='rc'
[Mesh]
[mesh]
type = GeneratedMeshGenerator
dim = 1
nx = 2
xmax = 0.5
[]
[]
[GlobalParams]
two_term_boundary_expansion = true
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = PINSFVRhieChowInterpolator
u = u
pressure = pressure
porosity = porosity
[]
[]
[Problem]
fv_bcs_integrity_check = false
[]
[Variables]
[u]
type = PINSFVSuperficialVelocityVariable
initial_condition = .1
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[AuxVariables]
[porosity]
family = MONOMIAL
order = CONSTANT
fv = true
initial_condition = 0.8
[]
[]
[Problem]
error_on_jacobian_nonzero_reallocation = true
[]
[Functions]
[exact_u]
type = ParsedFunction
value = 'cos((1/2)*x*pi)'
[]
[forcing_u]
type = ADParsedFunction
value = '-1.25*pi*rho*sin((1/2)*x*pi)*cos((1/2)*x*pi) + 0.8*cos(x)'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_p]
type = ParsedFunction
value = 'sin(x)'
[]
[forcing_p]
type = ParsedFunction
value = '-1/2*pi*rho*sin((1/2)*x*pi)'
vars = 'rho'
vals = '${rho}'
[]
[]
[FVKernels]
[mass]
type = PINSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[u_advection]
type = PINSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
porosity = porosity
momentum_component = 'x'
[]
[u_pressure]
type = PINSFVMomentumPressureFlux
variable = u
pressure = pressure
porosity = porosity
momentum_component = 'x'
force_boundary_execution = false
[]
[u_forcing]
type = INSFVBodyForce
variable = u
functor = forcing_u
momentum_component = 'x'
[]
[]
[FVBCs]
[mass]
variable = pressure
type = PINSFVFunctorBC
boundary = 'left right'
superficial_vel_x = u
pressure = pressure
eqn = 'mass'
porosity = porosity
[]
[momentum]
variable = u
type = PINSFVFunctorBC
boundary = 'left right'
superficial_vel_x = u
pressure = pressure
eqn = 'momentum'
momentum_component = 'x'
porosity = porosity
[]
[inlet-u]
type = FVFunctionDirichletBC
boundary = 'left'
variable = u
function = 'exact_u'
[]
[outlet_p]
type = FVFunctionDirichletBC
boundary = 'right'
variable = pressure
function = 'exact_p'
[]
[]
[Materials]
[const]
type = ADGenericFunctorMaterial
prop_names = 'rho'
prop_values = '${rho}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'bt'
[]
[Postprocessors]
[inlet_p]
type = SideAverageValue
variable = 'pressure'
boundary = 'left'
[]
[outlet-u]
type = SideIntegralVariablePostprocessor
variable = u
boundary = 'right'
[]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2p]
variable = pressure
function = exact_p
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
[Outputs]
exodus = true
csv = true
[]
(test/tests/vectorpostprocessors/extra_id_integral/extra_id_vpp.i)
[Mesh]
[fmg]
type = FileMeshGenerator
file = 'extra_id_vpp.e'
use_for_exodus_restart = true
exodus_extra_element_integers = 'pin_id assembly_id'
[]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[AuxVariables]
[value1]
order = FIRST
initial_from_file_var = value1
[]
[value2]
order = FIRST
initial_from_file_var = value2
[]
[]
[VectorPostprocessors]
[integral]
type = ExtraIDIntegralVectorPostprocessor
variable = 'value1'
id_name = 'assembly_id'
[]
[]
[Outputs]
exodus = false
csv = true
execute_on = timestep_end
[]
(test/tests/postprocessors/element_l2_norm/element_l2_norm.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 3
ny = 3
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Postprocessors]
[./L2_norm]
type = ElementL2Norm
variable = u
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
csv = true
[]
(test/tests/controls/time_periods/aux_kernels/enable_disable.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Dampers]
[./const_damp]
type = ConstantDamper
damping = 0.9
[../]
[]
[Outputs]
exodus = true
[]
(test/tests/materials/discrete/reset_warning.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = MatDiffusionTest
variable = u
prop_name = 'prop'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Materials]
[./mat]
type = GenericConstantMaterial
prop_names = 'prop'
prop_values = 1
compute = false # testing that this produces warning because resetQpProperties is not re-defined
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/kernels/materialpropertyvalue/materialpropertyvalue.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 15
ny = 15
nz = 0
xmin = 0
xmax = 1
ymin = 0
ymax = 1
elem_type = QUAD4
[]
[Variables]
[./c]
order = FIRST
family = LAGRANGE
[../]
[]
[Materials]
#
[./funcmat]
type = GenericFunctionMaterial
block = 0
prop_names = 'C'
prop_values = 'x^2-y^2'
outputs = exodus
[../]
[]
[Kernels]
[./value]
type = MaterialPropertyValue
prop_name = C
variable = c
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/ics/check_error/two_ics_on_same_boundary.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[ICs]
[./left]
type = ConstantIC
variable = u
boundary = left
value = 0.5
[../]
[./left2]
type = ConstantIC
variable = u
boundary = left
value = 2
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
[]
(test/tests/meshgenerators/gmsh_bcs/gmsh_bcs.i)
[Mesh]
[./fmg]
type = FileMeshGenerator
file = plate_hole.msh
[]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 12
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 10
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(test/tests/transfers/multiapp_conservative_transfer/master_nearest_point.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmax = 1
ymax = 1
nx = 10
ny = 10
[]
[block1]
input = gen
type = SubdomainBoundingBoxGenerator
block_id = 1
bottom_left = '0.5 0 0'
top_right = '1 1 0'
[]
[]
[Variables]
[power_density]
[]
[]
[Functions]
[pwr_func]
type = ParsedFunction
value = '1e3*x*(1-x)+5e2'
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = power_density
[]
[coupledforce]
type = BodyForce
variable = power_density
function = pwr_func
[]
[]
[BCs]
[left]
type = DirichletBC
variable = power_density
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = power_density
boundary = right
value = 1e3
[]
[]
[AuxVariables]
[from_sub]
[]
[]
[VectorPostprocessors]
[from_nearest_point]
type = NearestPointIntegralVariablePostprocessor
variable = power_density
points = '0 0.5 0 1 0.5 0'
[]
[to_nearest_point]
type = NearestPointIntegralVariablePostprocessor
variable = from_sub
points = '0 0.5 0 1 0.5 0'
execute_on = 'transfer'
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[MultiApps]
[sub]
type = FullSolveMultiApp
input_files = sub_nearest_point.i
positions = '0 0 0 0.5 0 0'
execute_on = timestep_end
[]
[]
[Transfers]
[to_sub]
type = MultiAppMeshFunctionTransfer
source_variable = power_density
variable = from_master
to_multi_app = sub
execute_on = timestep_end
# The following inputs specify what postprocessors should be conserved
# 1 NearestPointIntegralVariablePostprocessor is specified on the master
# side with N points, where N is the number of subapps
# 1 pp is specified on the subapp side
from_postprocessors_to_be_preserved = 'from_nearest_point'
to_postprocessors_to_be_preserved = 'from_master_pp'
[]
[from_sub]
type = MultiAppMeshFunctionTransfer
source_variable = sink
variable = from_sub
from_multi_app = sub
execute_on = timestep_end
# The following inputs specify what postprocessors should be conserved
# 1 NearestPointIntegralVariablePostprocessor is specified on the master
# with N points, where N is the number of subapps
# 1 pp is specified on the subapp side
to_postprocessors_to_be_preserved = 'to_nearest_point'
from_postprocessors_to_be_preserved = 'sink'
[]
[]
[Outputs]
csv = true
exodus = true
[]
(test/tests/materials/derivative_material_interface/ad_execution_order.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Materials]
# fetch the properties first...
[./client]
type = ADDerivativeMaterialInterfaceTestClient
block = 0
[../]
# ...then declare them!
[./provider]
type = ADDerivativeMaterialInterfaceTestProvider
block = 0
outputs = exodus
output_properties = 'dprop/db dprop/da d^2prop/dadb d^2prop/dadc d^3prop/dadbdc'
[../]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Debug]
show_material_props = true
[]
[Outputs]
exodus = true
[]
(test/tests/fvkernels/mms/mass-mom-mat-advection-diffusion/input.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 2
xmin = -.6
xmax = .6
[]
[]
[GlobalParams]
advected_interp_method = 'average'
[]
[Variables]
[fv_rho]
order = CONSTANT
family = MONOMIAL
fv = true
initial_condition = 2
[]
[fv_vel]
order = CONSTANT
family = MONOMIAL
fv = true
initial_condition = 2
[]
[]
[FVKernels]
[adv_rho]
type = FVMatAdvection
variable = fv_rho
vel = 'fv_velocity'
[]
[diff_rho]
type = FVDiffusion
variable = fv_rho
coeff = coeff
[]
[forcing_rho]
type = FVBodyForce
variable = fv_rho
function = 'forcing_rho'
[]
[adv_rho_u]
type = FVMatAdvection
variable = fv_vel
vel = 'fv_velocity'
advected_quantity = 'rho_u'
[]
[diff_vel]
type = FVDiffusion
variable = fv_vel
coeff = coeff
[]
[forcing_vel]
type = FVBodyForce
variable = fv_vel
function = 'forcing_vel'
[]
[]
[FVBCs]
[boundary_rho]
type = FVFunctionDirichletBC
boundary = 'left right'
function = 'exact_rho'
variable = fv_rho
[]
[boundary_vel]
type = FVFunctionDirichletBC
boundary = 'left right'
function = 'exact_vel'
variable = fv_vel
[]
[]
[Materials]
[euler_material]
type = ADCoupledVelocityMaterial
vel_x = fv_vel
rho = fv_rho
velocity = 'fv_velocity'
[]
[diff]
type = ADGenericFunctorMaterial
prop_names = 'coeff'
prop_values = '1'
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
line_search = 'none'
[]
[Outputs]
csv = true
exodus = true
[]
[Functions]
[forcing_rho]
type = ParsedFunction
value = '-1.331*sin(1.1*x)^2 + 1.331*sin(1.1*x) + 1.331*cos(1.1*x)^2'
[]
[exact_rho]
type = ParsedFunction
value = '1.1*sin(1.1*x)'
[]
[forcing_vel]
type = ParsedFunction
value = '-2.9282*sin(1.1*x)^2*cos(1.1*x) + 1.4641*cos(1.1*x)^3 + 1.331*cos(1.1*x)'
[]
[exact_vel]
type = ParsedFunction
value = '1.1*cos(1.1*x)'
[]
[]
[Postprocessors]
[./l2_rho]
type = ElementL2Error
variable = fv_rho
function = exact_rho
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./l2_vel]
type = ElementL2Error
variable = fv_vel
function = exact_vel
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(test/tests/materials/has_material/has_boundary_prop.i)
[Mesh]
type = FileMesh
file = rectangle.e
[]
[Variables]
[./u]
[../]
[]
[Kernels]
active = 'u_diff'
[./u_diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[./right]
type = MatTestNeumannBC
variable = u
boundary = 2
mat_prop = 'right_bc'
has_check = true
[../]
[]
[Materials]
[./right_bc]
type = GenericConstantMaterial
boundary = 2
prop_names = 'right_bc'
prop_values = '2.0'
[../]
[./other]
type = GenericConstantMaterial
boundary = 1
prop_names = 'other_value'
prop_values = '1.0'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(test/tests/vectorpostprocessors/csv_reader/read_preic.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[VectorPostprocessors]
[./reader]
type = CSVReader
csv_file = 'example.csv'
force_preic = true
[../]
[]
[Outputs]
csv = true
execute_on = INITIAL
[]
(test/tests/functions/parsed/combined.i)
[Mesh]
type = GeneratedMesh
dim = 1
xmin = -1
xmax = 1
nx = 20
[]
[AuxVariables]
[./f]
[../]
[./sv]
family = SCALAR
order = FIRST
initial_condition = 100
[../]
[]
[AuxKernels]
[./function_aux]
type = FunctionAux
variable = f
function = fn
[../]
[]
[Functions]
[./pp_fn]
type = ParsedFunction
value = '2*(t+1)'
[../]
[./cos_fn]
type = ParsedFunction
value = 'cos(pi*x)'
[../]
[./fn]
type = ParsedFunction
value = 'scalar_value * func / pp'
vars = 'scalar_value func pp'
vals = 'sv cos_fn pp'
[../]
[]
[Postprocessors]
[./pp]
type = FunctionValuePostprocessor
function = pp_fn
execute_on = initial
[../]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
show = f
exodus = true
execute_on = final
[]
(modules/navier_stokes/test/tests/finite_volume/ins/mms/cylindrical/2d-rc.i)
mu=1.1
rho=1.1
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 1
xmax = 3
ymin = -1
ymax = 1
nx = 2
ny = 2
[]
[]
[Problem]
coord_type = 'RZ'
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[lambda]
family = SCALAR
order = FIRST
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = 'average'
velocity_interp_method = 'rc'
rho = ${rho}
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[mean_zero_pressure]
type = FVScalarLagrangeMultiplier
variable = pressure
lambda = lambda
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_interp_method = 'average'
velocity_interp_method = 'rc'
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[u_forcing]
type = INSFVBodyForce
variable = u
functor = forcing_u
momentum_component = 'x'
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_interp_method = 'average'
velocity_interp_method = 'rc'
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[v_forcing]
type = INSFVBodyForce
variable = v
functor = forcing_v
momentum_component = 'y'
[]
[]
[FVBCs]
[no-slip-wall-u]
type = INSFVNoSlipWallBC
boundary = 'left right top bottom'
variable = u
function = 'exact_u'
[]
[no-slip-wall-v]
type = INSFVNoSlipWallBC
boundary = 'left right top bottom'
variable = v
function = 'exact_v'
[]
[]
[Functions]
[exact_u]
type = ParsedFunction
value = 'sin(y)*sin(x*pi)'
[]
[exact_rhou]
type = ParsedFunction
value = 'rho*sin(y)*sin(x*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_u]
type = ADParsedFunction
value = 'mu*sin(y)*sin(x*pi) - (-x*pi^2*mu*sin(y)*sin(x*pi) + pi*mu*sin(y)*cos(x*pi))/x + (2*x*pi*rho*sin(y)^2*sin(x*pi)*cos(x*pi) + rho*sin(y)^2*sin(x*pi)^2)/x + (-1/2*x*pi*rho*sin(x)*sin(y)*sin(x*pi)*sin((1/2)*y*pi) + x*rho*sin(x)*sin(x*pi)*cos(y)*cos((1/2)*y*pi))/x'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_v]
type = ParsedFunction
value = 'sin(x)*cos((1/2)*y*pi)'
[]
[exact_rhov]
type = ParsedFunction
value = 'rho*sin(x)*cos((1/2)*y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_v]
type = ADParsedFunction
value = '(1/4)*pi^2*mu*sin(x)*cos((1/2)*y*pi) - pi*rho*sin(x)^2*sin((1/2)*y*pi)*cos((1/2)*y*pi) + cos(y) - (-x*mu*sin(x)*cos((1/2)*y*pi) + mu*cos(x)*cos((1/2)*y*pi))/x + (x*pi*rho*sin(x)*sin(y)*cos(x*pi)*cos((1/2)*y*pi) + x*rho*sin(y)*sin(x*pi)*cos(x)*cos((1/2)*y*pi) + rho*sin(x)*sin(y)*sin(x*pi)*cos((1/2)*y*pi))/x'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_p]
type = ParsedFunction
value = 'sin(y)'
[]
[forcing_p]
type = ParsedFunction
value = '-1/2*pi*rho*sin(x)*sin((1/2)*y*pi) + (x*pi*rho*sin(y)*cos(x*pi) + rho*sin(y)*sin(x*pi))/x'
vars = 'rho'
vals = '${rho}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 30 lu NONZERO'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[./L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2v]
type = ElementL2Error
variable = v
function = exact_v
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2p]
variable = pressure
function = exact_p
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/cylindrical/cartesian-version/2d-rc-no-slip-walls.i)
mu=1.1
rho=1.1
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 2
ny = 2
[]
[]
[Problem]
fv_bcs_integrity_check = false
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
two_term_boundary_expansion = true
advected_interp_method = 'average'
velocity_interp_method = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
[]
[v]
type = INSFVVelocityVariable
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[ICs]
[u]
type = FunctionIC
function = 'exact_u'
variable = u
[]
[v]
type = FunctionIC
function = 'exact_v'
variable = v
[]
[pressure]
type = FunctionIC
function = 'exact_p'
variable = pressure
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
rho = ${rho}
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[u_forcing]
type = INSFVBodyForce
variable = u
functor = forcing_u
momentum_component = 'x'
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[v_forcing]
type = INSFVBodyForce
variable = v
functor = forcing_v
momentum_component = 'y'
[]
[]
[FVBCs]
[u_walls]
type = INSFVNoSlipWallBC
variable = u
boundary = 'left right'
function = 'exact_u'
[]
[v_walls]
type = INSFVNoSlipWallBC
variable = v
boundary = 'left right'
function = 'exact_v'
[]
[p]
type = INSFVOutletPressureBC
variable = pressure
function = 'exact_p'
boundary = 'top'
[]
[inlet_u]
type = INSFVInletVelocityBC
variable = u
function = 'exact_u'
boundary = 'bottom'
[]
[inlet_v]
type = INSFVInletVelocityBC
variable = v
function = 'exact_v'
boundary = 'bottom'
[]
[]
[Functions]
[exact_u]
type = ParsedFunction
value = 'sin(x*pi)*cos(y*pi)'
[]
[forcing_u]
type = ADParsedFunction
value = '2*pi^2*mu*sin(x*pi)*cos(y*pi) - 2*pi*rho*sin(x*pi)*sin(y*pi)*cos(1.3*x)*cos(y*pi) + 2*pi*rho*sin(x*pi)*cos(x*pi)*cos(y*pi)^2 + 1.5*cos(1.5*x)*cos(1.6*y)'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_v]
type = ParsedFunction
value = 'cos(1.3*x)*cos(y*pi)'
[]
[forcing_v]
type = ADParsedFunction
value = '1.69*mu*cos(1.3*x)*cos(y*pi) + pi^2*mu*cos(1.3*x)*cos(y*pi) - 1.3*rho*sin(1.3*x)*sin(x*pi)*cos(y*pi)^2 - 2*pi*rho*sin(y*pi)*cos(1.3*x)^2*cos(y*pi) + pi*rho*cos(1.3*x)*cos(x*pi)*cos(y*pi)^2 - 1.6*sin(1.5*x)*sin(1.6*y)'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_p]
type = ParsedFunction
value = 'sin(1.5*x)*cos(1.6*y)'
[]
[forcing_p]
type = ParsedFunction
value = '-pi*rho*sin(y*pi)*cos(1.3*x) + pi*rho*cos(x*pi)*cos(y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_shift_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu NONZERO superlu_dist'
line_search = 'none'
nl_rel_tol = 1e-12
nl_abs_tol = 1e-12
[]
[Outputs]
csv = true
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[./L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2v]
type = ElementL2Error
variable = v
function = exact_v
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2p]
variable = pressure
function = exact_p
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[p_avg]
type = ElementAverageValue
variable = pressure
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(test/tests/misc/check_error/interface_kernel_with_aux_var.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./v]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./rea]
type = Reaction
variable = u
[../]
[]
[InterfaceKernels]
[./nope]
type = InterfaceDiffusion
variable = v
neighbor_var = u
boundary = 'left'
D = 4
D_neighbor = 2
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/parser/multiple_inputs/diffusion1a.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/ics/check_error/two_ics_on_same_block.i)
[Mesh]
type = FileMesh
file = 'rectangle.e'
[]
[Variables]
[./u]
[../]
[]
[ICs]
[./block]
type = ConstantIC
variable = u
block = 1
value = 0.5
[../]
[./block2]
type = ConstantIC
variable = u
block = 1
value = 2
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
[]
(modules/heat_conduction/test/tests/fvbcs/fv_thermal_resistance/test_functor.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 5
ny = 5
xmax = 2
[]
[]
[Variables]
[u]
type = MooseVariableFVReal
initial_condition = 0.5
[]
[]
[FVKernels]
[diff_left]
type = FVDiffusion
variable = u
coeff = 4
[]
[gradient_creating]
type = FVBodyForce
variable = u
[]
[]
[FVBCs]
[left]
type = FunctorThermalResistanceBC
geometry = 'cartesian'
variable = u
T_ambient = 10
htc = 'htc'
emissivity = 0.2
thermal_conductivities = '0.1 0.2 0.3'
conduction_thicknesses = '1 0.7 0.2'
boundary = 'left'
# Test setting iteration parameters
step_size = 0.02
max_iterations = 120
tolerance = 1e-4
[]
[top]
type = FunctorThermalResistanceBC
geometry = 'cartesian'
variable = u
# Test setting the temperature separately from the variable
temperature = 'u'
T_ambient = 14
htc = 'htc'
emissivity = 0
thermal_conductivities = '0.1 0.2 0.3'
conduction_thicknesses = '1 0.7 0.4'
boundary = 'top'
[]
[other]
type = FVDirichletBC
variable = u
boundary = 'right bottom'
value = 0
[]
[]
[Materials]
[cht]
type = ADGenericFunctorMaterial
prop_names = 'htc'
prop_values = '1'
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/auxkernels/peclet-number-functor-aux/fe-thermal.i)
rho = 1
mu = 1
k = 1
cp = 1
[GlobalParams]
gravity = '0 0 0'
pspg = true
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[corner_node]
type = ExtraNodesetGenerator
new_boundary = 'pinned_node'
nodes = '0'
input = gen
[]
[]
[AuxVariables]
[Pe]
family = MONOMIAL
order = FIRST
[]
[]
[AuxKernels]
[Pe]
type = PecletNumberFunctorAux
variable = Pe
speed = speed
thermal_diffusivity = 'thermal_diffusivity'
[]
[]
[Variables]
[vel_x][]
[vel_y][]
[p][]
[T][]
[]
[Kernels]
# mass
[mass]
type = INSMass
variable = p
u = vel_x
v = vel_y
pressure = p
[]
# x-momentum, space
[x_momentum_space]
type = INSMomentumLaplaceForm
variable = vel_x
u = vel_x
v = vel_y
pressure = p
component = 0
[]
# y-momentum, space
[y_momentum_space]
type = INSMomentumLaplaceForm
variable = vel_y
u = vel_x
v = vel_y
pressure = p
component = 1
[]
[temperature_space]
type = INSTemperature
variable = T
u = vel_x
v = vel_y
[]
[]
[BCs]
[x_no_slip]
type = DirichletBC
variable = vel_x
boundary = 'bottom right left'
value = 0.0
[]
[lid]
type = FunctionDirichletBC
variable = vel_x
boundary = 'top'
function = 'lid_function'
[]
[y_no_slip]
type = DirichletBC
variable = vel_y
boundary = 'bottom right top left'
value = 0.0
[]
[pressure_pin]
type = DirichletBC
variable = p
boundary = 'pinned_node'
value = 0
[]
[T_hot]
type = DirichletBC
variable = T
boundary = 'bottom'
value = 1
[]
[T_cold]
type = DirichletBC
variable = T
boundary = 'top'
value = 0
[]
[]
[Materials]
[const]
type = GenericConstantMaterial
block = 0
prop_names = 'rho mu k cp'
prop_values = '${rho} ${mu} ${k} ${cp}'
[]
[speed]
type = ADVectorMagnitudeFunctorMaterial
x_functor = vel_x
y_functor = vel_y
vector_magnitude_name = speed
[]
[thermal_diffusivity]
type = ThermalDiffusivityFunctorMaterial
k = ${k}
rho = ${rho}
cp = ${cp}
[]
[]
[Functions]
[lid_function]
# We pick a function that is exactly represented in the velocity
# space so that the Dirichlet conditions are the same regardless
# of the mesh spacing.
type = ParsedFunction
value = '4*x*(1-x)'
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
solve_type = 'NEWTON'
[]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_asm_overlap -sub_pc_type'
petsc_options_value = 'asm 2 lu'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(modules/geochemistry/test/tests/time_dependent_reactions/except3.i)
#Exception: bad fixed-activity name
[TimeDependentReactionSolver]
model_definition = definition
geochemistry_reactor_name = reactor
charge_balance_species = "Cl-"
constraint_species = "H2O H+ Na+ K+ Ca++ Mg++ Al+++ SiO2(aq) Cl- SO4-- HCO3-"
constraint_value = " 1.0 1E-5 1E-5 1E-5 1E-5 1E-5 1E-5 1E-5 1E-5 1E-5 1E-5"
constraint_meaning = "kg_solvent_water activity bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition"
constraint_unit = "kg dimensionless moles moles moles moles moles moles moles moles moles"
remove_fixed_activity_name = "NaCl"
remove_fixed_activity_time = "0"
[]
[Executioner]
type = Steady
[]
[UserObjects]
[definition]
type = GeochemicalModelDefinition
database_file = "../../../database/moose_geochemdb.json"
basis_species = "H2O H+ Na+ K+ Ca++ Mg++ Al+++ SiO2(aq) Cl- SO4-- HCO3-"
[]
[]
(test/tests/bcs/ad_bc_preset_nodal/bc_preset_nodal.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
nz = 0
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = ADDiffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
# We will use preset BCs
[./left]
type = ADDirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = ADDirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = bc_preset_out
exodus = true
[]
(test/tests/vectorpostprocessors/elements_along_plane/1d.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 10
# Our CSV diffs here depend on a fixed element id numbering
allow_renumbering = false
parallel_type = replicated
[]
[Problem]
solve = false
[]
[VectorPostprocessors]
[./elems]
type = ElementsAlongPlane
point = '0.55 0.0 0.0'
normal = '1.0 0.0 0.0'
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
[]
(test/tests/bcs/ad_penalty_dirichlet_bc/function_penalty_dirichlet_bc_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 10
ny = 10
elem_type = QUAD9
[]
[Functions]
[./forcing_fn]
type = ParsedFunction
value = -4+x*x+y*y
[../]
[./solution]
type = ParsedGradFunction
value = x*x+y*y
grad_x = 2*x
grad_y = 2*y
[../]
[]
[Variables]
[./u]
order = SECOND
family = HIERARCHIC
[../]
[]
[Kernels]
active = 'diff forcing reaction'
[./diff]
type = ADDiffusion
variable = u
[../]
[./reaction]
type = Reaction
variable = u
[../]
[./forcing]
type = ADBodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
active = 'bc_all'
[./bc_all]
type = ADFunctionPenaltyDirichletBC
variable = u
function = solution
boundary = 'top left right bottom'
penalty = 1e6
[../]
[]
[Postprocessors]
[./dofs]
type = NumDOFs
[../]
[./h]
type = AverageElementSize
[../]
[./L2error]
type = ElementL2Error
variable = u
function = solution
[../]
[./H1error]
type = ElementH1Error
variable = u
function = solution
[../]
[./H1Semierror]
type = ElementH1SemiError
variable = u
function = solution
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
nl_rel_tol = 1e-14
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
csv = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/lid_driven/ad_lid_driven_action_stabilized_steady.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
nx = 16
ny = 16
[]
[]
[Modules]
[IncompressibleNavierStokes]
equation_type = steady-state
velocity_boundary = 'bottom right top left'
velocity_function = '0 0 0 0 lid_function 0 0 0'
initial_velocity = '1e-15 1e-15 0'
add_standard_velocity_variables_for_ad = false
pressure_pinned_node = 0
density_name = rho
dynamic_viscosity_name = mu
use_ad = true
laplace = true
family = LAGRANGE
order = FIRST
add_temperature_equation = true
fixed_temperature_boundary = 'bottom top'
temperature_function = '1 0'
supg = true
pspg = true
[]
[]
[Materials]
[const]
type = ADGenericConstantMaterial
prop_names = 'rho mu cp k'
prop_values = '1 1 1 .01'
[]
[]
[Functions]
[lid_function]
# We pick a function that is exactly represented in the velocity
# space so that the Dirichlet conditions are the same regardless
# of the mesh spacing.
type = ParsedFunction
value = '4*x*(1-x)'
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_levels -ksp_gmres_restart'
petsc_options_value = 'asm 6 200'
line_search = 'none'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
exodus = true
[]
(modules/porous_flow/test/tests/fluids/ideal_gas.i)
# Example of using the IdealGasFluidProperties userobject to provide fluid
# properties for an ideal gas. Use values for hydrogen (H2) at 1 MPa and 50 C.
#
# Input values:
# M = 2.01588e-3 kg/mol
# gamma = 1.4
# viscosity = 9.4393e-6 Pa.s
#
# Expected output:
# density = 750.2854 kg/m^3
# internal energy = 3.33 MJ/kg
# enthalpy = 4.66 MJ/kg
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[]
[Variables]
[pp]
initial_condition = 1e6
[]
[]
[Kernels]
[dummy]
type = Diffusion
variable = pp
[]
[]
[AuxVariables]
[temp]
initial_condition = 50.0
[]
[]
[Modules]
[FluidProperties]
[idealgas]
type = IdealGasFluidProperties
molar_mass = 2.01588e-3
gamma = 1.4
mu = 9.4393e-6
[]
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
temperature = temp
[]
[ppss]
type = PorousFlow1PhaseFullySaturated
porepressure = pp
[]
[idealgass]
type = PorousFlowSingleComponentFluid
temperature_unit = Celsius
fp = idealgas
phase = 0
[]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Postprocessors]
[pressure]
type = ElementIntegralVariablePostprocessor
variable = pp
[]
[temperature]
type = ElementIntegralVariablePostprocessor
variable = temp
[]
[density]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_fluid_phase_density_qp0'
[]
[viscosity]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_viscosity_qp0'
[]
[internal_energy]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_fluid_phase_internal_energy_qp0'
[]
[enthalpy]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_fluid_phase_enthalpy_qp0'
[]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = ideal_gas
csv = true
[]
(modules/porous_flow/test/tests/thermal_conductivity/ThermalCondPorosity01.i)
# Trivial test of PorousFlowThermalConductivityFromPorosity
# Porosity = 0.1
# Solid thermal conductivity = 3
# Fluid thermal conductivity = 2
# Expected porous medium thermal conductivity = 3 * (1 - 0.1) + 2 * 0.1 = 2.9
[Mesh]
type = GeneratedMesh
dim = 3
xmin = 0
xmax = 1
ymin = 0
ymax = 1
zmin = -1
zmax = 0
nx = 1
ny = 1
nz = 1
# This test uses ElementalVariableValue postprocessors on specific
# elements, so element numbering needs to stay unchanged
allow_renumbering = false
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
[]
[]
[]
[Variables]
[temp]
initial_condition = 1
[]
[pp]
initial_condition = 0
[]
[]
[Kernels]
[heat_conduction]
type = PorousFlowHeatConduction
variable = temp
[]
[dummy]
type = Diffusion
variable = pp
[]
[]
[BCs]
[temp]
type = DirichletBC
variable = temp
boundary = 'front back'
value = 1
[]
[pp]
type = DirichletBC
variable = pp
boundary = 'front back'
value = 0
[]
[]
[AuxVariables]
[lambda_x]
order = CONSTANT
family = MONOMIAL
[]
[lambda_y]
order = CONSTANT
family = MONOMIAL
[]
[lambda_z]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[lambda_x]
type = MaterialRealTensorValueAux
property = PorousFlow_thermal_conductivity_qp
row = 0
column = 0
variable = lambda_x
[]
[lambda_y]
type = MaterialRealTensorValueAux
property = PorousFlow_thermal_conductivity_qp
row = 1
column = 1
variable = lambda_y
[]
[lambda_z]
type = MaterialRealTensorValueAux
property = PorousFlow_thermal_conductivity_qp
row = 2
column = 2
variable = lambda_z
[]
[]
[Postprocessors]
[lambda_x]
type = ElementalVariableValue
elementid = 0
variable = lambda_x
execute_on = 'timestep_end'
[]
[lambda_y]
type = ElementalVariableValue
elementid = 0
variable = lambda_y
execute_on = 'timestep_end'
[]
[lambda_z]
type = ElementalVariableValue
elementid = 0
variable = lambda_z
execute_on = 'timestep_end'
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp temp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
temperature = temp
[]
[ppss_qp]
type = PorousFlow1PhaseFullySaturated
porepressure = pp
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[porosity_qp]
type = PorousFlowPorosityConst
porosity = 0.1
[]
[lambda]
type = PorousFlowThermalConductivityFromPorosity
lambda_s = '3 0 0 0 3 0 0 0 3'
lambda_f = '2 0 0 0 2 0 0 0 2'
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
[]
[]
[Executioner]
solve_type = Newton
type = Steady
[]
[Outputs]
file_base = ThermalCondPorosity01
csv = true
execute_on = 'timestep_end'
[]
(modules/heat_conduction/test/tests/verify_against_analytical/2d_steady_state.i)
# This test solves a 2D steady state heat equation
# The error is found by comparing to the analytical solution
# Note that the thermal conductivity, specific heat, and density in this problem
# Are set to 1, and need to be changed to the constants of the material being
# Analyzed
[Mesh]
type = GeneratedMesh
dim = 2
nx = 30
ny = 30
xmax = 2
ymax = 2
[]
[Variables]
[./T]
[../]
[]
[Kernels]
[./HeatDiff]
type = HeatConduction
variable = T
[../]
[]
[BCs]
[./zero]
type = DirichletBC
variable = T
boundary = 'left right bottom'
value = 0
[../]
[./top]
type = FunctionDirichletBC
variable = T
boundary = top
function = '10*sin(pi*x*0.5)'
[../]
[]
[Materials]
[./properties]
type = GenericConstantMaterial
prop_names = 'thermal_conductivity specific_heat density'
prop_values = '1 1 1'
[../]
[]
[Postprocessors]
[./nodal_error]
type = NodalL2Error
function = '10/(sinh(pi))*sin(pi*x*0.5)*sinh(pi*y*0.5)'
variable = T
[../]
[./elemental_error]
type = ElementL2Error
function = '10/(sinh(pi))*sin(pi*x*0.5)*sinh(pi*y*0.5)'
variable = T
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/radiation_transfer_action/radiative_transfer_action_external_boundary.i)
[Problem]
kernel_coverage_check = false
[]
[Mesh]
[./cmg]
type = CartesianMeshGenerator
dim = 2
dx = '1 1.3 1.9'
ix = '3 3 3'
dy = '6'
iy = '9'
subdomain_id = '0 1 2'
[../]
[./inner_left]
type = SideSetsBetweenSubdomainsGenerator
input = cmg
primary_block = 0
paired_block = 1
new_boundary = 'inner_left'
[../]
[./inner_right]
type = SideSetsBetweenSubdomainsGenerator
input = inner_left
primary_block = 2
paired_block = 1
new_boundary = 'inner_right'
[../]
[./inner_top]
type = ParsedGenerateSideset
combinatorial_geometry = 'abs(y - 6) < 1e-10'
normal = '0 1 0'
included_subdomain_ids = 1
new_sideset_name = 'inner_top'
input = 'inner_right'
[../]
[./inner_bottom]
type = ParsedGenerateSideset
combinatorial_geometry = 'abs(y) < 1e-10'
normal = '0 -1 0'
included_subdomain_ids = 1
new_sideset_name = 'inner_bottom'
input = 'inner_top'
[../]
[./rename]
type = RenameBlockGenerator
old_block = '2'
new_block = '0'
input = inner_bottom
[../]
[]
[Variables]
[./temperature]
block = 0
[../]
[]
[Kernels]
[./heat_conduction]
type = HeatConduction
variable = temperature
block = 0
diffusion_coefficient = 5
[../]
[]
[GrayDiffuseRadiation]
[./cavity]
boundary = '4 5 6 7'
emissivity = '0.9 0.8 0.4 1'
n_patches = '2 2 2 3'
partitioners = 'centroid centroid centroid centroid'
centroid_partitioner_directions = 'x y y x'
temperature = temperature
adiabatic_boundary = '7'
fixed_temperature_boundary = '6'
fixed_boundary_temperatures = '800'
view_factor_calculator = analytical
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = temperature
boundary = left
value = 1000
[../]
[./right]
type = DirichletBC
variable = temperature
boundary = right
value = 300
[../]
[]
[Postprocessors]
[./average_T_inner_right]
type = SideAverageValue
variable = temperature
boundary = inner_right
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/format/output_test_nemesis.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
nz = 0
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[]
[Postprocessors]
[./avg_block]
type = ElementAverageValue
variable = u
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
nemesis = 1
[]
(test/tests/materials/has_material/has_block_prop.i)
[Mesh]
type = FileMesh
file = rectangle.e
[]
[Variables]
[./u]
[../]
[]
[Kernels]
active = 'u_diff'
[./u_diff]
type = MatCoefDiffusion
variable = u
block = '1 2'
conductivity = k
[../]
[]
[BCs]
[./left]
type = NeumannBC
variable = u
boundary = 1
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 0
[../]
[]
[Materials]
[./right]
type = GenericConstantMaterial
block = 2
prop_names = 'k k_right'
prop_values = '1 2'
[../]
[./left]
type = GenericConstantMaterial
block = 1
prop_names = 'k'
prop_values = '0.1'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(modules/navier_stokes/test/tests/auxkernels/reynolds-number-functor-aux/fe.i)
rho=1
mu=1
[GlobalParams]
gravity = '0 0 0'
pspg = true
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[corner_node]
type = ExtraNodesetGenerator
new_boundary = 'pinned_node'
nodes = '0'
input = gen
[]
[]
[AuxVariables]
[Reynolds]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[Reynolds]
type = ReynoldsNumberFunctorAux
variable = Reynolds
speed = speed
rho = ${rho}
mu = ${mu}
[]
[]
[Variables]
[vel_x]
[]
[vel_y]
[]
[p]
[]
[]
[Kernels]
# mass
[mass]
type = INSMass
variable = p
u = vel_x
v = vel_y
pressure = p
[]
# x-momentum, space
[x_momentum_space]
type = INSMomentumLaplaceForm
variable = vel_x
u = vel_x
v = vel_y
pressure = p
component = 0
[]
# y-momentum, space
[y_momentum_space]
type = INSMomentumLaplaceForm
variable = vel_y
u = vel_x
v = vel_y
pressure = p
component = 1
[]
[]
[BCs]
[x_no_slip]
type = DirichletBC
variable = vel_x
boundary = 'bottom right left'
value = 0.0
[]
[lid]
type = FunctionDirichletBC
variable = vel_x
boundary = 'top'
function = 'lid_function'
[]
[y_no_slip]
type = DirichletBC
variable = vel_y
boundary = 'bottom right top left'
value = 0.0
[]
[pressure_pin]
type = DirichletBC
variable = p
boundary = 'pinned_node'
value = 0
[]
[]
[Materials]
[const]
type = GenericConstantMaterial
block = 0
prop_names = 'rho mu'
prop_values = '${rho} ${mu}'
[]
[speed]
type = ADVectorMagnitudeFunctorMaterial
x_functor = vel_x
y_functor = vel_y
vector_magnitude_name = speed
[]
[]
[Functions]
[lid_function]
# We pick a function that is exactly represented in the velocity
# space so that the Dirichlet conditions are the same regardless
# of the mesh spacing.
type = ParsedFunction
value = '4*x*(1-x)'
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
solve_type = 'NEWTON'
[]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_asm_overlap -sub_pc_type'
petsc_options_value = 'asm 2 lu'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_mortar_action/modular_gap_heat_transfer_mortar_displaced_radiation_conduction_action.i)
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
[file]
type = FileMeshGenerator
file = 2blk-gap.e
[]
allow_renumbering = false
[]
[Problem]
kernel_coverage_check = false
material_coverage_check = false
[]
[Variables]
[temp]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[disp_x]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[disp_y]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[]
[Materials]
[left]
type = ADHeatConductionMaterial
block = 1
thermal_conductivity = 0.01
specific_heat = 1
[]
[right]
type = ADHeatConductionMaterial
block = 2
thermal_conductivity = 0.005
specific_heat = 1
[]
[]
[Kernels]
[hc_displaced_block]
type = ADHeatConduction
variable = temp
use_displaced_mesh = true
block = '1'
[]
[hc_undisplaced_block]
type = ADHeatConduction
variable = temp
use_displaced_mesh = false
block = '2'
[]
[disp_x]
type = Diffusion
variable = disp_x
block = '1 2'
[]
[disp_y]
type = Diffusion
variable = disp_y
block = '1 2'
[]
[]
[MortarGapHeatTransfer]
[mortar_heat_transfer]
temperature = temp
primary_emissivity = 1.0
secondary_emissivity = 1.0
boundary = 100
use_displaced_mesh = true
gap_conductivity = 0.02
primary_boundary = 100
secondary_boundary = 101
gap_flux_options = 'CONDUCTION RADIATION'
[]
[]
[BCs]
[left]
type = DirichletBC
variable = temp
boundary = 'left'
value = 100
[]
[right]
type = DirichletBC
variable = temp
boundary = 'right'
value = 0
[]
[left_disp_x]
type = DirichletBC
preset = false
variable = disp_x
boundary = 'left'
value = .1
[]
[right_disp_x]
type = DirichletBC
preset = false
variable = disp_x
boundary = 'right'
value = 0
[]
[bottom_disp_y]
type = DirichletBC
preset = false
variable = disp_y
boundary = 'bottom'
value = 0
[]
[]
[Preconditioning]
[fmp]
type = SMP
full = true
solve_type = 'NEWTON'
[]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-11
nl_abs_tol = 1.0e-10
[]
[VectorPostprocessors]
[NodalTemperature]
type = NodalValueSampler
sort_by = id
boundary = '100 101'
variable = 'temp'
[]
[]
[Outputs]
csv = true
[exodus]
type = Exodus
show = 'temp'
[]
[]
(test/tests/controls/time_periods/dampers/enable_disable.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Dampers]
[./const_damp]
type = ConstantDamper
damping = 0.9
[../]
[]
[Outputs]
exodus = true
[]
(test/tests/markers/combo_marker/combo_marker_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
nz = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Adaptivity]
[./Markers]
[./box]
type = BoxMarker
bottom_left = '0.3 0.3 0'
top_right = '0.6 0.6 0'
inside = refine
outside = do_nothing
[../]
[./combo]
type = ComboMarker
markers = 'box box2'
[../]
[./box2]
type = BoxMarker
bottom_left = '0.5 0.5 0'
top_right = '0.8 0.8 0'
inside = refine
outside = coarsen
[../]
[../]
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/mms/supg/supg_mms_test.i)
mu=1.5
rho=2.5
[GlobalParams]
gravity = '0 0 0'
supg = true
convective_term = true
integrate_p_by_parts = false
laplace = true
u = vel_x
v = vel_y
pressure = p
alpha = 1
order = SECOND
family = LAGRANGE
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
elem_type = QUAD9
nx = 4
ny = 4
[]
[./corner_node]
type = ExtraNodesetGenerator
new_boundary = 'pinned_node'
nodes = '0'
input = gen
[../]
[]
[Variables]
[./vel_x]
[../]
[./vel_y]
[../]
[./p]
order = FIRST
[../]
[]
[Kernels]
# mass
[./mass]
type = INSMass
variable = p
[../]
# x-momentum, space
[./x_momentum_space]
type = INSMomentumLaplaceForm
variable = vel_x
component = 0
forcing_func = vel_x_source_func
[../]
# y-momentum, space
[./y_momentum_space]
type = INSMomentumLaplaceForm
variable = vel_y
component = 1
forcing_func = vel_y_source_func
[../]
[./p_source]
type = BodyForce
function = p_source_func
variable = p
[../]
[]
[BCs]
[./vel_x]
type = FunctionDirichletBC
preset = false
boundary = 'left right top bottom'
function = vel_x_func
variable = vel_x
[../]
[./vel_y]
type = FunctionDirichletBC
preset = false
boundary = 'left right top bottom'
function = vel_y_func
variable = vel_y
[../]
[./p]
type = FunctionDirichletBC
preset = false
boundary = 'left right top bottom'
function = p_func
variable = p
[../]
[]
[Functions]
[./vel_x_source_func]
type = ParsedFunction
value = '-${mu}*(-0.028*pi^2*x^2*sin(0.2*pi*x*y) - 0.028*pi^2*y^2*sin(0.2*pi*x*y) - 0.1*pi^2*sin(0.5*pi*x) - 0.4*pi^2*sin(pi*y)) + ${rho}*(0.14*pi*x*cos(0.2*pi*x*y) + 0.4*pi*cos(pi*y))*(0.6*sin(0.8*pi*x) + 0.3*sin(0.3*pi*y) + 0.2*sin(0.3*pi*x*y) + 0.3) + ${rho}*(0.14*pi*y*cos(0.2*pi*x*y) + 0.2*pi*cos(0.5*pi*x))*(0.4*sin(0.5*pi*x) + 0.4*sin(pi*y) + 0.7*sin(0.2*pi*x*y) + 0.5) + 0.1*pi*y*cos(0.2*pi*x*y) + 0.25*pi*cos(0.5*pi*x)'
[../]
[./vel_y_source_func]
type = ParsedFunction
value = '-${mu}*(-0.018*pi^2*x^2*sin(0.3*pi*x*y) - 0.018*pi^2*y^2*sin(0.3*pi*x*y) - 0.384*pi^2*sin(0.8*pi*x) - 0.027*pi^2*sin(0.3*pi*y)) + ${rho}*(0.06*pi*x*cos(0.3*pi*x*y) + 0.09*pi*cos(0.3*pi*y))*(0.6*sin(0.8*pi*x) + 0.3*sin(0.3*pi*y) + 0.2*sin(0.3*pi*x*y) + 0.3) + ${rho}*(0.06*pi*y*cos(0.3*pi*x*y) + 0.48*pi*cos(0.8*pi*x))*(0.4*sin(0.5*pi*x) + 0.4*sin(pi*y) + 0.7*sin(0.2*pi*x*y) + 0.5) + 0.1*pi*x*cos(0.2*pi*x*y) + 0.3*pi*cos(0.3*pi*y)'
[../]
[./p_source_func]
type = ParsedFunction
value = '-0.06*pi*x*cos(0.3*pi*x*y) - 0.14*pi*y*cos(0.2*pi*x*y) - 0.2*pi*cos(0.5*pi*x) - 0.09*pi*cos(0.3*pi*y)'
[../]
[./vel_x_func]
type = ParsedFunction
value = '0.4*sin(0.5*pi*x) + 0.4*sin(pi*y) + 0.7*sin(0.2*pi*x*y) + 0.5'
[../]
[./vel_y_func]
type = ParsedFunction
value = '0.6*sin(0.8*pi*x) + 0.3*sin(0.3*pi*y) + 0.2*sin(0.3*pi*x*y) + 0.3'
[../]
[./p_func]
type = ParsedFunction
value = '0.5*sin(0.5*pi*x) + 1.0*sin(0.3*pi*y) + 0.5*sin(0.2*pi*x*y) + 0.5'
[../]
[./vxx_func]
type = ParsedFunction
value = '0.14*pi*y*cos(0.2*pi*x*y) + 0.2*pi*cos(0.5*pi*x)'
[../]
[]
[Materials]
[./const]
type = GenericConstantMaterial
block = 0
prop_names = 'rho mu'
prop_values = '${rho} ${mu}'
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
petsc_options = '-snes_converged_reason -ksp_converged_reason'
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
nl_abs_tol = 1e-13
nl_max_its = 6
l_tol = 1e-6
l_max_its = 500
[]
[Outputs]
[./exodus]
type = Exodus
[../]
[./csv]
type = CSV
[../]
[]
[Postprocessors]
[./L2vel_x]
type = ElementL2Error
variable = vel_x
function = vel_x_func
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2vel_y]
variable = vel_y
function = vel_y_func
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2p]
variable = p
function = p_func
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2vxx]
variable = vxx
function = vxx_func
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[]
[AuxVariables]
[./vxx]
family = MONOMIAL
order = FIRST
[../]
[]
[AuxKernels]
[./vxx]
type = VariableGradientComponent
component = x
variable = vxx
gradient_variable = vel_x
[../]
[]
(modules/fluid_properties/test/tests/calorically_imperfect_gas/test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
elem_type = QUAD4
[]
[Functions]
[f_fn]
type = ParsedFunction
value = -4
[]
[bc_fn]
type = ParsedFunction
value = 'x*x+y*y'
[]
[e_fn]
type = PiecewiseLinear
x = '100 280 300 350 400 450 500 550 600 700 800 900 1000 1200 1400 1600 1800 2000 2200 2400 2600 2800 3000 5000'
y = '783.9 2742.3 2958.6 3489.2 4012.7 4533.3 5053.8 5574 6095.1 7140.2 8192.9 9256.3 10333.6 12543.9 14836.6 17216.3 19688.4 22273.7 25018.3 28042.3 31544.2 35818.1 41256.5 100756.5'
scale_factor = 1e3
[]
[mu_fn]
type = PiecewiseLinear
x = '100 280 300 350 400 450 500 550 600 700 800 900 1000 1200 1400 1600 1800 2000 2200 2400 2600 2800 3000 5000'
y = '85.42 85.42 89.53 99.44 108.9 117.98 126.73 135.2 143.43 159.25 174.36 188.9 202.96 229.88 255.5 280.05 303.67 326.45 344.97 366.49 387.87 409.48 431.86 431.86'
scale_factor = 1e-7
[]
[k_fn]
type = PiecewiseLinear
x = '100 280 300 350 400 450 500 550 600 700 800 900 1000 1200 1400 1600 1800 2000 2200 2400 2600 2800 3000 5000'
y = '186.82 186.82 194.11 212.69 231.55 250.38 268.95 287.19 305.11 340.24 374.92 409.66 444.75 511.13 583.42 656.44 733.32 826.53 961.15 1180.38 1546.31 2135.49 3028.08 3028.08'
scale_factor = 1e-3
[]
[]
[Variables]
[u]
[]
[]
[AuxVariables]
[e]
initial_condition = 4012.7e3
[]
[v]
initial_condition = 0.0007354064593540647
[]
[p]
family = MONOMIAL
order = CONSTANT
[]
[T]
family = MONOMIAL
order = CONSTANT
[]
[cp]
family = MONOMIAL
order = CONSTANT
[]
[cv]
family = MONOMIAL
order = CONSTANT
[]
[c]
family = MONOMIAL
order = CONSTANT
[]
[mu]
family = MONOMIAL
order = CONSTANT
[]
[k]
family = MONOMIAL
order = CONSTANT
[]
[g]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[p]
type = MaterialRealAux
variable = p
property = pressure
[]
[T]
type = MaterialRealAux
variable = T
property = temperature
[]
[cp]
type = MaterialRealAux
variable = cp
property = cp
[]
[cv]
type = MaterialRealAux
variable = cv
property = cv
[]
[c]
type = MaterialRealAux
variable = c
property = c
[]
[mu]
type = MaterialRealAux
variable = mu
property = mu
[]
[k]
type = MaterialRealAux
variable = k
property = k
[]
[g]
type = MaterialRealAux
variable = g
property = g
[]
[]
[Modules]
[FluidProperties]
[h2]
type = CaloricallyImperfectGas
molar_mass = 0.002
e = e_fn
k = k_fn
mu = mu_fn
min_temperature = 100
max_temperature = 5000
[]
[]
[]
[Materials]
[fp_mat]
type = FluidPropertiesMaterial
e = e
v = v
fp = h2
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[ffn]
type = BodyForce
variable = u
function = f_fn
[]
[]
[BCs]
[all]
type = FunctionDirichletBC
variable = u
boundary = 'left right top bottom'
function = bc_fn
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(python/peacock/tests/input_tab/InputTreeWriter/gold/simple_diffusion_inactive.i)
inactive = 'Kernels BCs Executioner'
[Mesh]
[generate]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
inactive = 'diff'
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[]
[]
[Executioner]
# Preconditioned JFNK (default)
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/materials/functor_properties/functor-vector-mat-props.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 4
ny = 4
xmax = 2
ymax = 1
[]
[subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '1.0 0 0'
block_id = 1
top_right = '2.0 1.0 0'
[]
[]
[AuxVariables]
# cant use nodal variables because of the two blocks, which material to use
# there is undefined
[mat_x]
family = MONOMIAL
order = CONSTANT
[]
[mat_y]
family = MONOMIAL
order = CONSTANT
[]
[mat_z]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[matprop_to_aux_x]
type = FunctorVectorElementalAux
variable = mat_x
functor = 'matprop'
component = '0'
[]
[matprop_to_aux_y]
type = FunctorVectorElementalAux
variable = mat_y
functor = 'matprop'
component = '1'
[]
[matprop_to_aux_z]
type = FunctorVectorElementalAux
variable = mat_z
functor = 'matprop'
component = '2'
[]
[]
[Materials]
[block0]
type = GenericVectorFunctorMaterial
block = '0'
prop_names = 'matprop'
prop_values = '4 2 1'
[]
[block1]
type = GenericVectorFunctorMaterial
block = '1'
prop_names = 'matprop'
prop_values = 'f_x f_x f_z'
[]
[]
[Functions]
[f_x]
type = ParsedFunction
value = 'x + 2 * y'
[]
[f_z]
type = ParsedFunction
value = 'x * y - 2'
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/executioners/steady_time/steady_time.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
elem_type = QUAD4
nx = 4
ny = 4
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./force]
type = BodyForce
variable = u
function = time_function
[../]
[]
[Functions]
[./time_function]
type = ParsedFunction
value = 't+1'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 'left right bottom top'
value = 0
[../]
[]
[Postprocessors]
[./norm]
type = ElementL2Norm
variable = u
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/heat_conduction/2d_quadrature_gap_heat_transfer/nonmatching.i)
[Mesh]
file = nonmatching.e
[]
[Variables]
[./temp]
[../]
[]
[Kernels]
[./hc]
type = HeatConduction
variable = temp
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = temp
boundary = leftleft
value = 1000
[../]
[./right]
type = DirichletBC
variable = temp
boundary = rightright
value = 400
[../]
[]
[ThermalContact]
[./left_to_right]
emissivity_primary = 0
emissivity_secondary = 0
secondary = leftright
quadrature = true
primary = rightleft
variable = temp
type = GapHeatTransfer
[../]
[]
[Materials]
[./hcm]
type = HeatConductionMaterial
block = 'left right'
specific_heat = 1
thermal_conductivity = 1
[../]
[./gap_conductance]
type = GenericConstantMaterial
prop_names = 'gap_conductance gap_conductance_dT'
boundary = 'leftright rightleft'
prop_values = '1 0'
[../]
[]
[Postprocessors]
[./left]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = leftright
diffusivity = thermal_conductivity
[../]
[./right]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = rightleft
diffusivity = thermal_conductivity
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/rz_cone_by_parts_steady_stabilized.i)
# This input file tests several different things:
# .) The axisymmetric (RZ) form of the governing equations.
# .) An open boundary.
# .) Not integrating the pressure by parts, thereby requiring a pressure pin.
# .) Natural boundary condition at the outlet.
[GlobalParams]
integrate_p_by_parts = true
laplace = true
gravity = '0 0 0'
supg = true
pspg = true
order = FIRST
[]
[Mesh]
file = '2d_cone.msh'
[]
[Problem]
coord_type = RZ
[]
[Preconditioning]
[./SMP_PJFNK]
type = SMP
full = true
solve_type = Newton
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = 'bjacobi ilu 4'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
csv = true
console = true
[./out]
type = Exodus
[../]
[]
[Variables]
[./vel_x]
# Velocity in radial (r) direction
[../]
[./vel_y]
# Velocity in axial (z) direction
[../]
[./p]
[../]
[]
[BCs]
[./u_in]
type = DirichletBC
boundary = bottom
variable = vel_x
value = 0
[../]
[./v_in]
type = FunctionDirichletBC
boundary = bottom
variable = vel_y
function = 'inlet_func'
[../]
[./u_axis_and_walls]
type = DirichletBC
boundary = 'left right'
variable = vel_x
value = 0
[../]
[./v_no_slip]
type = DirichletBC
boundary = 'right'
variable = vel_y
value = 0
[../]
[]
[Kernels]
[./mass]
type = INSMassRZ
variable = p
u = vel_x
v = vel_y
pressure = p
[../]
[./x_momentum_space]
type = INSMomentumLaplaceFormRZ
variable = vel_x
u = vel_x
v = vel_y
pressure = p
component = 0
[../]
[./y_momentum_space]
type = INSMomentumLaplaceFormRZ
variable = vel_y
u = vel_x
v = vel_y
pressure = p
component = 1
[../]
[]
[Materials]
[./const]
type = GenericConstantMaterial
block = 'volume'
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[]
[Functions]
[./inlet_func]
type = ParsedFunction
value = '-4 * x^2 + 1'
[../]
[]
[Postprocessors]
[./flow_in]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'bottom'
execute_on = 'timestep_end'
[../]
[./flow_out]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'top'
execute_on = 'timestep_end'
[../]
[]
(modules/heat_conduction/test/tests/view_factors_symmetry/cavity_with_pillars_symmetry_bc.i)
[Mesh]
[cartesian]
type = CartesianMeshGenerator
dim = 3
dx = '0.5 0.5 0.5'
dy = '0.5 0.75 0.5'
dz = '1.5 0.5'
subdomain_id = '1 1 1
1 2 1
1 1 1
1 1 1
1 1 1
1 1 1'
[]
[add_obstruction]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 2
paired_block = 1
new_boundary = obstruction
input = cartesian
[]
[add_new_back]
type = ParsedGenerateSideset
combinatorial_geometry = 'abs(z) < 1e-10'
included_subdomain_ids = '1'
normal = '0 0 -1'
new_sideset_name = back_2
input = add_obstruction
[]
[]
[UserObjects]
[view_factor_study]
type = ViewFactorRayStudy
execute_on = initial
boundary = 'left top bottom front back_2 obstruction'
face_order = FOURTH
[]
[view_factor]
type = RayTracingViewFactor
boundary = 'left top bottom front back_2 obstruction'
execute_on = INITIAL
normalize_view_factor = false
ray_study_name = view_factor_study
[]
[]
[RayBCs]
[vf_bc]
type = ViewFactorRayBC
boundary = 'left top bottom front back_2 obstruction'
[]
[symmetry]
type = ReflectRayBC
boundary = 'right'
[]
[]
[Postprocessors]
[left_left]
type = ViewFactorPP
from_boundary = left
to_boundary = left
view_factor_object_name = view_factor
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
[]
(modules/navier_stokes/examples/pipe_mixing_length/pipe_mixing_length.i)
# This example demonstrates how the mixing length model can be tuned to match an
# established correlation for pressure drop in a smooth circular pipe.
# The primary input parameters for this example are the system Reynolds number
# and the von Karman constant for the mixing length model. These two parameters
# can be changed here:
Re = 1e5
von_karman_const = 0.22
# Note that for this model (using the wall-distance mixing length for the entire
# pipe) different von Karman constants are optimal for different Reynolds
# numbers.
# This model has been non-dimensionalized. The diameter (D), density (rho), and
# bulk velocity (bulk_u) are all considered unity.
D = 1
total_len = ${fparse 40 * D}
rho = 1
bulk_u = 1
# With those parameters set, the viscosity is then computed in order to reach
# the desired Reynolds number.
mu = ${fparse rho * bulk_u * D / Re}
# Here the DeltaP will be evaluted by using a postprocessor to find the pressure
# at a point that is 10 diameters away from the outlet. (The outlet pressure is
# set to zero.)
L = ${fparse 10 * D}
# We will use the McAdams correlation to find the Darcy friction factor. Note
# that this correlation is valid for fully developed flow in smooth circular
# tubes at 3e4 < Re < 1e6.
f = ${fparse 0.316 * Re^(-0.25)}
# The DeltaP can then be computed using this friction factor as,
ref_delta_P = ${fparse f * L / D * rho * bulk_u^2 / 2}
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${total_len}
ymin = 0
ymax = ${fparse 0.5 * D}
nx = 200
ny = 40
bias_y = ${fparse 1 / 1.2}
[]
[rename1]
type = RenameBoundaryGenerator
input = gen
old_boundary = 'left'
new_boundary = 'inlet'
[]
[rename2]
type = RenameBoundaryGenerator
input = rename1
old_boundary = 'right'
new_boundary = 'outlet'
[]
[rename3]
type = RenameBoundaryGenerator
input = rename2
old_boundary = 'bottom'
new_boundary = 'symmetry'
[]
[rename4]
type = RenameBoundaryGenerator
input = rename3
old_boundary = 'top'
new_boundary = 'wall'
[]
[]
[Outputs]
exodus = true
[]
[Problem]
kernel_coverage_check = false
fv_bcs_integrity_check = true
coord_type = 'RZ'
rz_coord_axis = 'X'
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
# The upwind and Rhie-Chow interpolation schemes are used here.
advected_interp_method='upwind'
velocity_interp_method='rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1e-6
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1e-6
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[AuxVariables]
[mixing_len]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_viscosity_rans]
type = INSFVMixingLengthReynoldsStress
variable = u
rho = ${rho}
mixing_length = mixing_len
momentum_component = 'x'
u = u
v = v
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
momentum_component = 'y'
[]
[v_viscosity_rans]
type = INSFVMixingLengthReynoldsStress
variable = v
rho = ${rho}
mixing_length = mixing_len
momentum_component = 'y'
u = u
v = v
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[]
[AuxKernels]
[mixing_len]
type = WallDistanceMixingLengthAux
walls = 'wall'
variable = mixing_len
execute_on = 'initial'
von_karman_const = ${von_karman_const}
[]
[]
[FVBCs]
[inlet_u]
type = INSFVInletVelocityBC
boundary = 'inlet'
variable = u
function = ${bulk_u}
[]
[inlet_v]
type = INSFVInletVelocityBC
boundary = 'inlet'
variable = v
function = '0'
[]
[walls_u]
type = INSFVNoSlipWallBC
boundary = 'wall'
variable = u
function = 0
[]
[walls_v]
type = INSFVNoSlipWallBC
boundary = 'wall'
variable = v
function = 0
[]
[sym_u]
type = INSFVSymmetryVelocityBC
boundary = 'symmetry'
variable = u
u = u
v = v
mu = ${mu}
momentum_component = x
[]
[sym_v]
type = INSFVSymmetryVelocityBC
boundary = 'symmetry'
variable = v
u = u
v = v
mu = ${mu}
momentum_component = y
[]
[sym_p]
type = INSFVSymmetryPressureBC
boundary = 'symmetry'
variable = pressure
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'outlet'
variable = pressure
function = '0'
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
line_search = 'none'
nl_rel_tol = 1e-12
nl_abs_tol = 1e-12
[]
[Postprocessors]
[delta_P]
type = PointValue
variable = 'pressure'
point = '${fparse total_len - L} 0 0'
[]
[reference_delta_P]
type = Receiver
default = ${ref_delta_P}
[]
[]
(test/tests/kernels/ad_value/generic_value.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[AuxVariables]
[./u_jac]
[../]
[./v_jac]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[./value_test_v]
type = GenericValueTest
variable = v
diag_save_in = v_jac
[../]
[./ad_value_test]
type = ADGenericValueTest
variable = u
diag_save_in = u_jac
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = left
value = 0
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'Newton'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_mortar/bc_gap_heat_transfer_displaced_conduction.i)
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
[file]
type = FileMeshGenerator
file = 2blk-gap.e
[]
allow_renumbering = false
[]
[Problem]
kernel_coverage_check = false
material_coverage_check = false
[]
[Variables]
[temp]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[disp_x]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[disp_y]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[]
[Materials]
[left]
type = ADHeatConductionMaterial
block = 1
thermal_conductivity = 0.01
specific_heat = 1
[]
[right]
type = ADHeatConductionMaterial
block = 2
thermal_conductivity = 0.005
specific_heat = 1
[]
[]
[Kernels]
[hc_displaced_block]
type = ADHeatConduction
variable = temp
use_displaced_mesh = true
block = '1'
[]
[hc_undisplaced_block]
type = ADHeatConduction
variable = temp
use_displaced_mesh = false
block = '2'
[]
[disp_x]
type = Diffusion
variable = disp_x
block = '1 2'
[]
[disp_y]
type = Diffusion
variable = disp_y
block = '1 2'
[]
[]
[ThermalContact]
[thermal_contact]
type = GapHeatTransfer
variable = temp
primary = 100
secondary = 101
emissivity_primary = 0.0
emissivity_secondary = 0.0
gap_conductivity = 100.0
quadrature = true
[]
[]
[BCs]
[left]
type = DirichletBC
variable = temp
boundary = 'left'
value = 100
[]
[right]
type = DirichletBC
variable = temp
boundary = 'right'
value = 0
[]
[left_disp_x]
type = DirichletBC
preset = false
variable = disp_x
boundary = 'left'
value = .1
[]
[right_disp_x]
type = DirichletBC
preset = false
variable = disp_x
boundary = 'right'
value = 0
[]
[bottom_disp_y]
type = DirichletBC
preset = false
variable = disp_y
boundary = 'bottom'
value = 0
[]
[]
[Preconditioning]
[fmp]
type = SMP
full = true
solve_type = 'NEWTON'
[]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-11
nl_abs_tol = 1.0e-10
[]
[VectorPostprocessors]
[NodalTemperature]
type = NodalValueSampler
sort_by = id
boundary = '100 101'
variable = 'temp'
[]
[]
[Outputs]
exodus = false
csv = true
[]
(tutorials/tutorial01_app_development/step05_kernel_object/problems/pressure_diffusion.i)
[Mesh]
type = GeneratedMesh # Can generate simple lines, rectangles and rectangular prisms
dim = 2 # Dimension of the mesh
nx = 100 # Number of elements in the x direction
ny = 10 # Number of elements in the y direction
xmax = 0.304 # Length of test chamber
ymax = 0.0257 # Test chamber radius
[]
[Problem]
type = FEProblem # This is the "normal" type of Finite Element Problem in MOOSE
coord_type = RZ # Axisymmetric RZ
rz_coord_axis = X # Which axis the symmetry is around
[]
[Variables]
[pressure]
# Adds a Linear Lagrange variable by default
[]
[]
[Kernels]
[diffusion]
type = DarcyPressure # Zero-gravity, divergence-free form of Darcy's law
variable = pressure # Operate on the "pressure" variable from above
[]
[]
[BCs]
[inlet]
type = ADDirichletBC # Simple u=value BC
variable = pressure # Variable to be set
boundary = left # Name of a sideset in the mesh
value = 4000 # (Pa) From Figure 2 from paper. First data point for 1mm spheres.
[]
[outlet]
type = ADDirichletBC
variable = pressure
boundary = right
value = 0 # (Pa) Gives the correct pressure drop from Figure 2 for 1mm spheres
[]
[]
[Executioner]
type = Steady # Steady state problem
solve_type = NEWTON # Perform a Newton solve
# Set PETSc parameters to optimize solver efficiency
petsc_options_iname = '-pc_type -pc_hypre_type' # PETSc option pairs with values below
petsc_options_value = ' hypre boomeramg'
[]
[Outputs]
exodus = true # Output Exodus format
[]
(test/tests/geomsearch/2d_penetration_locator/2d_penetration_locator_test.i)
[Mesh]
file = 2d_contact_test.e
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./penetration]
order = FIRST
family = LAGRANGE
[../]
[./tangential_distance]
order = FIRST
family = LAGRANGE
[../]
[./normal_x]
order = FIRST
family = LAGRANGE
[../]
[./normal_y]
order = FIRST
family = LAGRANGE
[../]
[./closest_point_x]
order = FIRST
family = LAGRANGE
[../]
[./closest_point_y]
order = FIRST
family = LAGRANGE
[../]
[./element_id]
order = FIRST
family = LAGRANGE
[../]
[./side]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = penetration
boundary = 2
paired_boundary = 3
[../]
[./penetrate2]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 2
paired_boundary = 3
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 3
paired_boundary = 2
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 2
paired_boundary = 3
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 3
paired_boundary = 2
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 2
paired_boundary = 3
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 3
paired_boundary = 2
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = closest_point_x
boundary = 2
paired_boundary = 3
quantity = closest_point_x
[../]
[./penetrate10]
type = PenetrationAux
variable = closest_point_x
boundary = 3
paired_boundary = 2
quantity = closest_point_x
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_y
boundary = 2
paired_boundary = 3
quantity = closest_point_y
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_y
boundary = 3
paired_boundary = 2
quantity = closest_point_y
[../]
[./penetrate13]
type = PenetrationAux
variable = element_id
boundary = 2
paired_boundary = 3
quantity = element_id
[../]
[./penetrate14]
type = PenetrationAux
variable = element_id
boundary = 3
paired_boundary = 2
quantity = element_id
[../]
[./penetrate15]
type = PenetrationAux
variable = side
boundary = 2
paired_boundary = 3
quantity = side
[../]
[./penetrate16]
type = PenetrationAux
variable = side
boundary = 3
paired_boundary = 2
quantity = side
[../]
[]
[BCs]
active = 'block1_left block1_right block2_left block2_right'
[./block1_left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./block1_right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[./block2_left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./block2_right]
type = DirichletBC
variable = u
boundary = 4
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/thermal_hydraulics/test/tests/functions/smooth_transition/space.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 100
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Functions]
[transition_fn]
type = CosineTransitionFunction
axis = y
transition_center = 0.3
transition_width = 0.4
function1 = 0
function2 = 100
[]
[]
[AuxVariables]
[transition]
order = FIRST
family = LAGRANGE
[]
[]
[AuxKernels]
[transition_kernel]
type = FunctionAux
variable = transition
function = transition_fn
execute_on = initial
[]
[]
[Outputs]
exodus = true
show = transition
file_base = space_weighted
execute_on = initial
[]
(test/tests/postprocessors/area_pp/area_pp.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 4
xmax = 1.2
ymax = 2.3
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Postprocessors]
[./right]
type = AreaPostprocessor
boundary = 'right'
execute_on = 'initial timestep_end'
[../]
[./bottom]
type = AreaPostprocessor
boundary = 'bottom'
execute_on = 'initial timestep_end'
[../]
[./all]
type = AreaPostprocessor
boundary = 'left right bottom top'
execute_on = 'initial timestep_end'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
csv = true
[]
(modules/ray_tracing/test/tests/raybcs/errors/raybc_errors.i)
[Mesh]
active = 'gmg'
[gmg]
type = CartesianMeshGenerator
dim = 1
dx = '0.5 0.5'
ix = '1 1'
subdomain_id = '0 1'
[]
[internal]
type = SideSetsBetweenSubdomainsGenerator
input = gmg
primary_block = 1
paired_block = 0
new_boundary = internal
[]
[]
[UserObjects]
active = 'study'
[study]
type = RepeatableRayStudy
start_points = '0 0 0'
directions = '1 0 0'
names = 'ray'
execute_on = INITIAL
ray_kernel_coverage_check = false
[]
[set_end_study]
type = RepeatableRayStudy
start_points = '0 0 0'
end_points = '1 0 0'
names = 'ray'
execute_on = INITIAL
ray_kernel_coverage_check = false
use_internal_sidesets = true
[]
[start_internal_study]
type = RepeatableRayStudy
start_points = '0.5 0 0'
directions = '1 0 0'
names = 'ray'
execute_on = INITIAL
ray_kernel_coverage_check = false
use_internal_sidesets = true
[]
[]
[RayBCs]
active = ''
[kill]
type = KillRayBC
boundary = right
[]
[change]
type = ChangeRayRayBCTest
boundary = right
change_direction = true
[]
[change_again]
type = ChangeRayRayBCTest
boundary = right
change_direction = true
[]
[change_internal]
type = ChangeRayRayBCTest
boundary = internal
change_direction = true
[]
[change_zero]
type = ChangeRayRayBCTest
boundary = right
change_direction_zero = true
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
(test/tests/dirackernels/constant_point_source/2d_point_source.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
uniform_refine = 4
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[./v]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[DiracKernels]
active = 'point_source1 point_source2'
[./point_source1]
type = ConstantPointSource
variable = u
value = 1.0
point = '0.2 0.3'
[../]
[./point_source2]
type = ConstantPointSource
variable = u
value = -0.5
point = '0.2 0.8'
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = 2d_out
exodus = true
[]
(test/tests/meshgenerators/sidesets_bounding_box_generator/overlapping_sidesets.i)
[Mesh]
#active = 'gmg'
[./gmg]
type = GeneratedMeshGenerator
dim = 3
nx = 10
ny = 10
nz = 10
[]
[./createNewSidesetOne]
type = SideSetsFromBoundingBoxGenerator
input = gmg
boundary_id_old = 'bottom back left'
boundary_id_new = 10
bottom_left = '-1.1 -1.1 -1.1'
top_right = '1.1 1.1 1.1'
block_id = 0
boundary_id_overlap = true
[]
[./createNewSidesetTwo]
type = SideSetsFromBoundingBoxGenerator
input = createNewSidesetOne
boundary_id_old = 'right bottom'
boundary_id_new = 11
bottom_left = '-1.1 -1.1 -1.1'
top_right = '1.1 1.1 1.1'
block_id = 0
boundary_id_overlap = true
[]
[./createNewSidesetThree]
type = SideSetsFromBoundingBoxGenerator
input = createNewSidesetTwo
boundary_id_old = 'top front'
boundary_id_new = 12
bottom_left = '-1.1 -1.1 -1.1'
top_right = '1.1 1.1 1.1'
block_id = 0
boundary_id_overlap = true
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./BCone]
type = DirichletBC
variable = u
boundary = 10
value = 1
[../]
[./BCtwo]
type = DirichletBC
variable = u
boundary = 11
value = 1
[../]
[./BCthree]
type = DirichletBC
variable = u
boundary = 12
value = 0
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/porous_flow/test/tests/poroperm/PermFromPoro04.i)
# Testing permeability from porosity
# Trivial test, checking calculated permeability is correct
# k = k_anisotropic * k
# with log k = A * phi + B
[Mesh]
type = GeneratedMesh
dim = 1
nx = 3
xmin = 0
xmax = 3
[]
[GlobalParams]
block = 0
PorousFlowDictator = dictator
[]
[Variables]
[pp]
[InitialCondition]
type = ConstantIC
value = 0
[]
[]
[]
[Kernels]
[flux]
type = PorousFlowAdvectiveFlux
gravity = '0 0 0'
variable = pp
[]
[]
[BCs]
[ptop]
type = DirichletBC
variable = pp
boundary = right
value = 0
[]
[pbase]
type = DirichletBC
variable = pp
boundary = left
value = 1
[]
[]
[AuxVariables]
[poro]
order = CONSTANT
family = MONOMIAL
[]
[perm_x]
order = CONSTANT
family = MONOMIAL
[]
[perm_y]
order = CONSTANT
family = MONOMIAL
[]
[perm_z]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[poro]
type = PorousFlowPropertyAux
property = porosity
variable = poro
[]
[perm_x]
type = PorousFlowPropertyAux
property = permeability
variable = perm_x
row = 0
column = 0
[]
[perm_y]
type = PorousFlowPropertyAux
property = permeability
variable = perm_y
row = 1
column = 1
[]
[perm_z]
type = PorousFlowPropertyAux
property = permeability
variable = perm_z
row = 2
column = 2
[]
[]
[Postprocessors]
[perm_x_bottom]
type = PointValue
variable = perm_x
point = '0 0 0'
[]
[perm_y_bottom]
type = PointValue
variable = perm_y
point = '0 0 0'
[]
[perm_z_bottom]
type = PointValue
variable = perm_z
point = '0 0 0'
[]
[perm_x_top]
type = PointValue
variable = perm_x
point = '3 0 0'
[]
[perm_y_top]
type = PointValue
variable = perm_y
point = '3 0 0'
[]
[perm_z_top]
type = PointValue
variable = perm_z
point = '3 0 0'
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureVG
# unimportant in this fully-saturated test
m = 0.8
alpha = 1e-4
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 2.2e9
viscosity = 1e-3
density0 = 1000
thermal_expansion = 0
[]
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[massfrac]
type = PorousFlowMassFraction
[]
[eff_fluid_pressure]
type = PorousFlowEffectiveFluidPressure
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pp
capillary_pressure = pc
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[porosity]
type = PorousFlowPorosity
porosity_zero = 0.1
[]
[relperm]
type = PorousFlowRelativePermeabilityCorey
n = 0 # unimportant in this fully-saturated situation
phase = 0
[]
[permeability]
type = PorousFlowPermeabilityExponential
k_anisotropy = '1 0 0 0 2 0 0 0 0.1'
poroperm_function = log_k
A = 4.342945
B = -8
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
[]
[]
[Executioner]
solve_type = Newton
type = Steady
l_tol = 1E-5
nl_abs_tol = 1E-3
nl_rel_tol = 1E-8
l_max_its = 200
nl_max_its = 400
petsc_options_iname = '-pc_type -pc_asm_overlap -sub_pc_type -ksp_type -ksp_gmres_restart'
petsc_options_value = ' asm 2 lu gmres 200'
[]
[Outputs]
csv = true
execute_on = 'timestep_end'
[]
(test/tests/controls/error/non_existing_dependency.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = CoefDiffusion
variable = u
coef = 0.1
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Controls]
[./ctrl]
type = TestControl
test_type = 'real'
parameter = 'BCs/left/value'
execute_on = 'initial timestep_begin'
depends_on = 'no-control'
[../]
[]
(test/tests/transfers/multiapp_conservative_transfer/sub_conservative_transfer.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
xmin = 0.05
xmax = 1.2
ymin = 0.05
ymax = 1.1
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./coupledforce]
type = CoupledForce
variable = u
v = aux_u
[../]
[]
[AuxVariables]
[./aux_u]
family = LAGRANGE
order = FIRST
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Postprocessors]
[./to_postprocessor]
type = ElementIntegralVariablePostprocessor
variable = aux_u
execute_on = 'transfer'
[../]
[]
[Problem]
type = FEProblem
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
nl_abs_tol = 1e-12
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/restart/pointer_restart_errors/pointer_store_error.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[UserObjects]
[./restartable_types]
type = PointerStoreError
[../]
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[./checkpoint]
type = Checkpoint
num_files = 1
[../]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/action/errors/2d-rc-error-action.i)
mu=1
rho=1
k=1e-3
cp=1
alpha=1
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 5
ymin = -1
ymax = 1
nx = 10
ny = 4
[]
[]
[Variables]
inactive = 'vel_x vel_y pressure T_fluid scalar'
[vel_x]
type = 'INSFVVelocityVariable'
initial_condition = 1
block=0
[]
[vel_y]
type = 'INSFVVelocityVariable'
initial_condition = 1
block=0
[]
[pressure]
type = 'INSFVPressureVariable'
initial_condition = 0
block=0
[]
[T_fluid]
type = 'INSFVEnergyVariable'
initial_condition = 0
[]
[scalar]
type = MooseVariableFVReal
initial_condition = 0
[]
[]
[Modules]
[NavierStokesFV]
compressibility = 'incompressible'
porous_medium_treatment = false
add_energy_equation = true
passive_scalar_names = 'scalar'
density = 'rho'
dynamic_viscosity = 'mu'
thermal_conductivity = 'k'
specific_heat = 'cp'
passive_scalar_diffusivity = 1e-3
passive_scalar_source = 0.1
initial_velocity = '1 1 0'
initial_pressure = 0.0
initial_temperature = 0.0
inlet_boundaries = 'left'
momentum_inlet_types = 'fixed-velocity'
momentum_inlet_function = '1 0'
energy_inlet_types = 'fixed-temperature'
energy_inlet_function = '1'
passive_scalar_inlet_types = 'fixed-value'
passive_scalar_inlet_function = '1'
wall_boundaries = 'top bottom'
momentum_wall_types = 'noslip noslip'
energy_wall_types = 'heatflux heatflux'
energy_wall_function = '0 0'
outlet_boundaries = 'right'
momentum_outlet_types = 'fixed-pressure'
pressure_function = '0'
ambient_convection_alpha = 'alpha'
ambient_temperature = '100'
[]
[]
[Materials]
[const_functor]
type = ADGenericFunctorMaterial
prop_names = 'cp k rho mu alpha'
prop_values = '${cp} ${k} ${rho} ${mu} ${alpha}'
[]
[]
[Postprocessors]
[temp]
type = ElementAverageValue
variable = T_fluid
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[]
(modules/navier_stokes/test/tests/finite_volume/fvkernels/flow_diode/friction.i)
mu = 1
rho = 1
[Mesh]
[cmg]
type = CartesianMeshGenerator
dim = 2
dx = '1 0.5 1'
dy = '0.5 0.5'
ix = '8 5 8'
iy = '8 8'
subdomain_id = '0 1 2
1 2 1'
[]
[top_outlet]
type = ParsedGenerateSideset
input = cmg
combinatorial_geometry = 'x>2.499 & y>0.4999'
new_sideset_name = top_right
[]
[bottom_outlet]
type = ParsedGenerateSideset
input = top_outlet
combinatorial_geometry = 'x>2.499 & y<0.50001'
new_sideset_name = bottom_right
[]
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
advected_interp_method = 'upwind'
velocity_interp_method = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = 1e-6
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 1e-6
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
[]
[diodes_against_flow]
type = INSFVFrictionFlowDiode
resistance = 100
variable = vel_x
direction = '-1 0 0'
block = 1
momentum_component = 'x'
[]
[diode_free_flow]
type = INSFVFrictionFlowDiode
resistance = 100
variable = vel_x
direction = '1 0 0'
block = 2
momentum_component = 'y'
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
[]
[]
[FVBCs]
[walls_u]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'top bottom'
function = 0
[]
[walls_v]
type = INSFVNoSlipWallBC
variable = vel_y
boundary = 'top bottom'
function = 0
[]
[inlet_u]
type = INSFVInletVelocityBC
variable = vel_x
boundary = 'left'
function = 1
[]
[inlet_v]
type = INSFVInletVelocityBC
variable = vel_y
boundary = 'left'
function = 0
[]
[outlet]
type = INSFVOutletPressureBC
variable = pressure
boundary = 'right'
function = 1
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_shift_type -ksp_gmres_restart'
petsc_options_value = 'asm lu NONZERO 200'
line_search = 'none'
nl_abs_tol = 1e-14
[]
[Postprocessors]
[mdot_top]
type = VolumetricFlowRate
boundary = 'top_right'
vel_x = vel_x
vel_y = vel_y
advected_quantity = ${rho}
[]
[mdot_bottom]
type = VolumetricFlowRate
boundary = 'bottom_right'
vel_x = vel_x
vel_y = vel_y
advected_quantity = ${rho}
[]
[]
[Outputs]
exodus = true
[]
(test/tests/variables/fe_hier/hier-3-1d.i)
[Mesh]
type = GeneratedMesh
dim = 1
xmin = -1
xmax = 1
nx = 5
elem_type = EDGE3
[]
[Functions]
[./bc_fnl]
type = ParsedFunction
value = -3*x*x
[../]
[./bc_fnr]
type = ParsedFunction
value = 3*x*x
[../]
[./forcing_fn]
type = ParsedFunction
value = -6*x+(x*x*x)
[../]
[./solution]
type = ParsedGradFunction
value = x*x*x
grad_x = 3*x*x
[../]
[]
[Variables]
[./u]
order = THIRD
family = HIERARCHIC
[../]
[]
[Kernels]
active = 'diff forcing reaction'
[./diff]
type = Diffusion
variable = u
[../]
[./reaction]
type = Reaction
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
[./bc_left]
type = FunctionNeumannBC
variable = u
boundary = 'left'
function = bc_fnl
[../]
[./bc_right]
type = FunctionNeumannBC
variable = u
boundary = 'right'
function = bc_fnr
[../]
[]
[Postprocessors]
[./dofs]
type = NumDOFs
[../]
[./h]
type = AverageElementSize
[../]
[./L2error]
type = ElementL2Error
variable = u
function = solution
[../]
[./H1error]
type = ElementH1Error
variable = u
function = solution
[../]
[./H1Semierror]
type = ElementH1SemiError
variable = u
function = solution
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
csv = true
[]
(modules/reactor/test/tests/meshgenerators/extra_element_id_copy_generator/copy_elem_id_test.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
xmax = 1
ymax = 1
extra_element_integers = test_id
subdomain_ids = '0 0 0 0 0 0 0 0 0 0
0 1 0 0 0 0 0 0 0 0
0 0 2 0 0 0 0 0 0 0
0 0 0 3 0 0 0 0 0 0
0 0 0 0 4 0 0 0 0 0
0 0 0 0 0 5 0 0 0 0
0 0 0 0 0 0 6 0 0 0
0 0 0 0 0 0 0 7 0 0
0 0 0 0 0 0 0 0 8 0
0 0 0 0 0 0 0 0 0 9'
[]
[subdomains]
type = SubdomainBoundingBoxGenerator
input = gmg
bottom_left = '0 0 0'
block_id = 1
top_right = '0.9 0.9 0'
integer_name = test_id
[]
[another_subdomains]
type = SubdomainBoundingBoxGenerator
input = subdomains
bottom_left = '0 0 0'
block_id = 2
top_right = '0.9 0.9 0'
location = OUTSIDE
integer_name = test_id
[]
[copy_test_id]
type = ExtraElementIDCopyGenerator
input = another_subdomains
source_extra_element_id = test_id
target_extra_element_ids = 'test_id1 test_id2'
[]
[copy_test_id1]
type = ExtraElementIDCopyGenerator
input = copy_test_id
source_extra_element_id = subdomain_id
target_extra_element_ids = 'test_id3'
[]
[copy_test_id2]
type = ExtraElementIDCopyGenerator
input = copy_test_id1
source_extra_element_id = element_id
target_extra_element_ids = 'test_id4'
[]
# element id could be renumbered with distributed mesh
# causing exodiff on test_id4 variable, thus we turn off
# this flag, normal calculations are fine with element IDs
# being renumbered.
allow_renumbering = false
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[AuxVariables]
[test_id]
family = MONOMIAL
order = CONSTANT
[]
[test_id1]
family = MONOMIAL
order = CONSTANT
[]
[test_id2]
family = MONOMIAL
order = CONSTANT
[]
[test_id3]
family = MONOMIAL
order = CONSTANT
[]
[test_id4]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[test_id]
type = ExtraElementIDAux
variable = test_id
extra_id_name = test_id
[]
[test_id1]
type = ExtraElementIDAux
variable = test_id1
extra_id_name = test_id1
[]
[test_id2]
type = ExtraElementIDAux
variable = test_id2
extra_id_name = test_id2
[]
[test_id3]
type = ExtraElementIDAux
variable = test_id3
extra_id_name = test_id3
[]
[test_id4]
type = ExtraElementIDAux
variable = test_id4
extra_id_name = test_id4
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/heat_conduction_patch/heat_conduction_patch_hex20.i)
#
# This problem is taken from the Abaqus verification manual:
# "1.5.8 Patch test for heat transfer elements"
#
# The temperature on the exterior nodes is 200x+100y+200z.
#
# This gives a constant flux at all Gauss points.
#
# In addition, the temperature at all nodes follows the same formula.
#
# Node x y z Temperature
# 1 1.000E+00 0.000E+00 1.000E+00 4.0000E+02
# 2 6.770E-01 3.050E-01 6.830E-01 3.0250E+02
# 3 3.200E-01 1.860E-01 6.430E-01 2.1120E+02
# 4 0.000E+00 0.000E+00 1.000E+00 2.0000E+02
# 5 1.000E+00 1.000E+00 1.000E+00 5.0000E+02
# 6 7.880E-01 6.930E-01 6.440E-01 3.5570E+02
# 7 1.650E-01 7.450E-01 7.020E-01 2.4790E+02
# 8 0.000E+00 1.000E+00 1.000E+00 3.0000E+02
# 9 8.385E-01 1.525E-01 8.415E-01 3.5125E+02
# 10 4.985E-01 2.455E-01 6.630E-01 2.5685E+02
# 11 1.600E-01 9.300E-02 8.215E-01 2.0560E+02
# 12 5.000E-01 0.000E+00 1.000E+00 3.0000E+02
# 13 1.000E+00 5.000E-01 1.000E+00 4.5000E+02
# 14 7.325E-01 4.990E-01 6.635E-01 3.2910E+02
# 15 2.425E-01 4.655E-01 6.725E-01 2.2955E+02
# 16 0.000E+00 5.000E-01 1.000E+00 2.5000E+02
# 17 8.940E-01 8.465E-01 8.220E-01 4.2785E+02
# 18 4.765E-01 7.190E-01 6.730E-01 3.0180E+02
# 19 8.250E-02 8.725E-01 8.510E-01 2.7395E+02
# 20 5.000E-01 1.000E+00 1.000E+00 4.0000E+02
# 21 1.000E+00 0.000E+00 0.000E+00 2.0000E+02
# 22 0.000E+00 0.000E+00 0.000E+00 0.0000E+00
# 23 8.260E-01 2.880E-01 2.880E-01 2.5160E+02
# 24 2.490E-01 3.420E-01 1.920E-01 1.2240E+02
# 25 1.000E+00 0.000E+00 5.000E-01 3.0000E+02
# 26 5.000E-01 0.000E+00 0.000E+00 1.0000E+02
# 27 0.000E+00 0.000E+00 5.000E-01 1.0000E+02
# 28 9.130E-01 1.440E-01 1.440E-01 2.2580E+02
# 29 1.245E-01 1.710E-01 9.600E-02 6.1200E+01
# 30 7.515E-01 2.965E-01 4.855E-01 2.7705E+02
# 31 5.375E-01 3.150E-01 2.400E-01 1.8700E+02
# 32 2.845E-01 2.640E-01 4.175E-01 1.6680E+02
# 33 2.730E-01 7.500E-01 2.300E-01 1.7560E+02
# 34 0.000E+00 1.000E+00 0.000E+00 1.0000E+02
# 35 2.610E-01 5.460E-01 2.110E-01 1.4900E+02
# 36 0.000E+00 5.000E-01 0.000E+00 5.0000E+01
# 37 2.190E-01 7.475E-01 4.660E-01 2.1175E+02
# 38 1.365E-01 8.750E-01 1.150E-01 1.3780E+02
# 39 0.000E+00 1.000E+00 5.000E-01 2.0000E+02
# 40 8.500E-01 6.490E-01 2.630E-01 2.8750E+02
# 41 8.380E-01 4.685E-01 2.755E-01 2.6955E+02
# 42 8.190E-01 6.710E-01 4.535E-01 3.2160E+02
# 43 5.615E-01 6.995E-01 2.465E-01 2.3155E+02
# 44 1.000E+00 1.000E+00 0.000E+00 3.0000E+02
# 45 1.000E+00 5.000E-01 0.000E+00 2.5000E+02
# 46 1.000E+00 1.000E+00 5.000E-01 4.0000E+02
# 47 9.250E-01 8.245E-01 1.315E-01 2.9375E+02
# 48 5.000E-01 1.000E+00 0.000E+00 2.0000E+02
[Mesh]#Comment
file = heat_conduction_patch_hex20.e
[] # Mesh
[Functions]
[./temps]
type = ParsedFunction
value='200*x+100*y+200*z'
[../]
[] # Functions
[Variables]
[./temp]
order = SECOND
family = LAGRANGE
[../]
[] # Variables
[Kernels]
[./heat_r]
type = HeatConduction
variable = temp
[../]
[] # Kernels
[BCs]
[./temps]
type = FunctionDirichletBC
variable = temp
boundary = 10
function = temps
[../]
[] # BCs
[Materials]
[./heat]
type = HeatConductionMaterial
block = 1
specific_heat = 0.116
thermal_conductivity = 4.85e-4
[../]
[] # Materials
[Executioner]
type = Steady
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -ksp_gmres_restart'
petsc_options_value = 'lu 101'
line_search = 'none'
nl_abs_tol = 1e-11
nl_rel_tol = 1e-10
l_max_its = 20
[./Quadrature]
order = THIRD
[../]
[] # Executioner
[Outputs]
exodus = true
[] # Output
(test/tests/kernels/forcing_function/forcing_function_error_check.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
uniform_refine = 4
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
active = 'forcing_func'
[./forcing_func]
type = ParsedFunction
value = '"alpha*alpha*pi*pi*sin(alpha*pi*x)"'
vars = 'alpha'
vals = '16'
[../]
[]
[Kernels]
active = 'diff forcing'
[./diff]
type = Diffusion
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_func
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-12
[]
[Outputs]
execute_on = 'timestep_end'
file_base = out
exodus = true
[]
(test/tests/materials/material/qp_material.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 3
ny = 3
elem_type = QUAD4
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left_u]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Materials]
[./mat1]
type = QpMaterial
block = 0
outputs = all
constant_on = ELEMENT
property_name = 'zero_prop'
[../]
# The second copy of QpMaterial is not constant_on_elem.
[./mat2]
type = QpMaterial
block = 0
outputs = all
property_name = 'nonzero_prop'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/mesh_modifiers/add_extra_nodeset/extra_nodeset_coord_test.i)
[Mesh]
[file]
type = FileMeshGenerator
file = square.e
[]
[middle_node]
type = ExtraNodesetGenerator
input = file
new_boundary = 'middle_node'
coord = '0.5 0.5'
[]
[]
[Variables]
active = 'u'
[u]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
active = 'diff'
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
active = 'left right middle'
[left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[]
[middle]
type = DirichletBC
variable = u
boundary = 'middle_node'
value = -1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/geochemistry/test/tests/geochemistry_quantity_aux/except5.i)
#Exception test: inappropriate quantity
[TimeDependentReactionSolver]
model_definition = definition
charge_balance_species = "Cl-"
constraint_species = "H2O H+ Cl- Fe+++ >(s)FeOH >(w)FeOH"
constraint_value = " 1.0 1.0 1.0 1.0 1.0 1.0"
constraint_meaning = "kg_solvent_water bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition"
constraint_unit = "kg moles moles moles moles moles"
kinetic_species_name = "Fe(OH)3(ppd)"
kinetic_species_initial_value = "1.0"
kinetic_species_unit = "moles"
[]
[UserObjects]
[definition]
type = GeochemicalModelDefinition
database_file = "../../database/ferric_hydroxide_sorption.json"
basis_species = "H2O H+ Cl- Fe+++ >(s)FeOH >(w)FeOH"
kinetic_minerals = "Fe(OH)3(ppd)"
[]
[]
[Executioner]
type = Steady
[]
[AuxVariables]
[error]
[]
[]
[AuxKernels]
[error]
type = GeochemistryQuantityAux
species = "Fe(OH)3(ppd)"
reactor = geochemistry_reactor
variable = error
quantity = kinetic_moles
[]
[]
(test/tests/materials/piecewise_by_block_material/test_functor.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 10
xmax = 2
[]
[subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '1.0 0 0'
block_id = 1
top_right = '2.0 1.0 0'
[]
[]
[Variables]
[u]
type = MooseVariableFVReal
[]
[]
[FVKernels]
[diff]
type = FVDiffusion
variable = u
coeff = 'coeff'
[]
[]
[FVBCs]
[left]
type = FVDirichletBC
variable = u
boundary = 'left'
value = 1
[]
[right]
type = FVDirichletBC
variable = u
boundary = 'right'
value = 0
[]
[]
[Materials]
[coeff_mat]
type = ADPiecewiseByBlockFunctorMaterial
prop_name = 'coeff'
subdomain_to_prop_value = '0 4
1 2'
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(test/tests/reporters/declare_initial_setup/declare_initial_setup_with_get.i)
[Mesh]
[generate]
type = GeneratedMeshGenerator
dim = 1
[]
[]
[Variables/u]
[]
[Executioner]
type = Steady
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[Reporters]
[initialSetup]
type = TestDeclareInitialSetupReporter
value = 1980
[]
[get]
type = TestGetReporterDeclaredInInitialSetupReporter
other_reporter = initialSetup/value
[]
[]
[Outputs]
[out]
type = JSON
execute_on = FINAL
execute_system_information_on = NONE
[]
[]
(modules/misc/test/tests/kernels/thermo_diffusion/ad_thermo_diffusion.i)
# Steady-state test for the ThermoDiffusion kernel.
#
# This test applies a constant temperature gradient to drive thermo-diffusion
# in the variable u. At steady state, the thermo-diffusion is balanced by
# diffusion due to Fick's Law, so the total flux is
#
# J = -D ( grad(u) - ( Qstar u / R ) grad(1/T) )
#
# If there are no fluxes at the boundaries, then there is no background flux and
# these two terms must balance each other everywhere:
#
# grad(u) = ( Qstar u / R ) grad(1/T)
#
# The dx can be eliminated to give
#
# d(ln u) / d(1/T) = Qstar / R
#
# This can be solved to give the profile for u as a function of temperature:
#
# u = A exp( Qstar / R T )
#
# Here, we are using simple heat conduction with Dirichlet boundaries on 0 <= x <= 1
# to give a linear profile for temperature: T = x + 1. We also need to apply one
# boundary condition on u, which is u(x=0) = 1. These conditions give:
#
# u = exp( -(Qstar/R) (x/(x+1)) )
#
# This analytical result is tracked by the aux variable "correct_u".
[Mesh]
type = GeneratedMesh
dim = 1
nx = 100
[]
[Variables]
[./u]
initial_condition = 1
[../]
[./temp]
initial_condition = 1
[../]
[]
[Kernels]
[./soret]
type = ADThermoDiffusion
variable = u
temperature = temp
[../]
[./diffC]
type = ADDiffusion
variable = u
[../]
# Heat diffusion gives a linear temperature profile to drive the Soret diffusion.
[./diffT]
type = ADDiffusion
variable = temp
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
preset = false
boundary = left
value = 1
[../]
[./leftt]
type = DirichletBC
variable = temp
preset = false
boundary = left
value = 1
[../]
[./rightt]
type = DirichletBC
variable = temp
preset = false
boundary = right
value = 2
[../]
[]
[Materials]
[./ad_soret_coefficient]
type = ADSoretCoeffTest
temperature = temp
coupled_var = u
[../]
[]
[Preconditioning]
[./full]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[./error]
type = NodalL2Error
variable = u
function = 'exp(-x/(x+1))'
[../]
[]
[Outputs]
execute_on = FINAL
exodus = true
[]
(modules/porous_flow/test/tests/gravity/fully_saturated_grav01a.i)
# Checking that gravity head is established
# 1phase, constant fluid-bulk, constant viscosity, constant permeability
# fully saturated
# For better agreement with the analytical solution (ana_pp), just increase nx
[Mesh]
type = GeneratedMesh
dim = 1
nx = 100
xmin = -1
xmax = 0
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Variables]
[pp]
[InitialCondition]
type = RandomIC
min = 0
max = 1
[]
[]
[]
[Kernels]
[flux0]
type = PorousFlowFullySaturatedDarcyBase
variable = pp
gravity = '-1 0 0'
[]
[]
[Functions]
[ana_pp]
type = ParsedFunction
vars = 'g B p0 rho0'
vals = '1 1.2 0 1'
value = '-B*log(exp(-p0/B)+g*rho0*x/B)' # expected pp at base
[]
[]
[BCs]
[z]
type = DirichletBC
variable = pp
boundary = right
value = 0
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 1.2
density0 = 1
viscosity = 1
thermal_expansion = 0
[]
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow1PhaseFullySaturated
porepressure = pp
[]
[massfrac]
type = PorousFlowMassFraction
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1 0 0 0 2 0 0 0 3'
[]
[]
[Postprocessors]
[pp_base]
type = PointValue
variable = pp
point = '-1 0 0'
[]
[pp_analytical]
type = FunctionValuePostprocessor
function = ana_pp
point = '-1 0 0'
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = fully_saturated_grav01a
[csv]
type = CSV
[]
[]
(test/tests/postprocessors/nodal_extreme_value/block_nodal_pps_test.i)
[Mesh]
file = rect-2blk.e
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
block = 1
[../]
[./v]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[BCs]
[./left_u]
type = DirichletBC
variable = u
boundary = 6
value = 0
[../]
[./right_u]
type = NeumannBC
variable = u
boundary = 8
value = 4
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = 6
value = 1
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = 3
value = 6
[../]
[]
[Postprocessors]
# This test demonstrates that you can have a block restricted NodalPostprocessor
[./restricted_max]
type = NodalMaxValue
variable = v
block = 1 # Block restricted
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/userobjects/element_quality_check/bypass_warning.i)
[Mesh]
file = Quad.e
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./top]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[UserObjects]
[./elem_quality_check]
type = ElementQualityChecker
metric_type = DIAGONAL
failure_type = WARNING
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/partitioners/petsc_partitioner/petsc_partitioner.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[Partitioner]
type = PetscExternalPartitioner
part_package = parmetis
[]
parallel_type = distributed
# Need a fine enough mesh to have good partition
uniform_refine = 1
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[AuxVariables]
[pid]
family = MONOMIAL
order = CONSTANT
[]
[npid]
family = Lagrange
order = first
[]
[]
[AuxKernels]
[pid_aux]
type = ProcessorIDAux
variable = pid
execute_on = 'INITIAL'
[]
[npid_aux]
type = ProcessorIDAux
variable = npid
execute_on = 'INITIAL'
[]
[]
[Postprocessors]
[sum_sides]
type = StatVector
stat = sum
object = nl_wb_element
vector = num_partition_sides
[]
[min_elems]
type = StatVector
stat = min
object = nl_wb_element
vector = num_elems
[]
[max_elems]
type = StatVector
stat = max
object = nl_wb_element
vector = num_elems
[]
[]
[VectorPostprocessors]
[nl_wb_element]
type = WorkBalance
execute_on = initial
system = nl
balances = 'num_elems num_partition_sides'
outputs = none
[]
[]
[Outputs]
exodus = true
[out]
type = CSV
execute_on = FINAL
[]
[]
(test/tests/quadrature/qweights/positive_qweights.i)
[Mesh]
[./square]
type = FileMeshGenerator
file = cube.e
[../]
[]
[Variables]
[u][]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[heat_source_fuel]
type = CoupledForce
variable = u
v = power_density
[]
[]
[BCs]
[robin]
type = RobinBC
variable = u
boundary = '1 2 3 4 5 6'
[]
[]
[AuxVariables]
[power_density]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[source]
type = ParsedAux
variable = power_density
use_xyzt = true
function = 'if(x>0.1,100,1)'
[]
[]
[Executioner]
type = Steady
[./Quadrature]
allow_negative_qweights = false
[../]
solve_type = 'NEWTON'
petsc_options_iname = "-pc_type"
petsc_options_value = "hypre"
[]
[Outputs]
exodus = true
[]
(test/tests/dirackernels/constant_point_source/3d_point_source.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 10
ny = 10
nz = 10
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[./v]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[DiracKernels]
[./point_source1]
type = ConstantPointSource
variable = u
value = 0.1
point = '0.2 0.3 0.0'
[../]
[./point_source2]
type = ConstantPointSource
variable = u
value = -0.1
point = '0.2 0.8 0.0'
[../]
[./point_source3]
type = ConstantPointSource
variable = u
value = -1.0
point = '0.8 0.5 0.8'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = 3d_out
exodus = true
[]
(modules/heat_conduction/test/tests/heat_conduction/2d_quadrature_gap_heat_transfer/perfectQ8.i)
[GlobalParams]
order = SECOND
[]
[Mesh]
file = perfectQ8.e
[]
[Variables]
[./temp]
[../]
[]
[Kernels]
[./hc]
type = HeatConduction
variable = temp
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = temp
boundary = leftleft
value = 300
[../]
[./right]
type = DirichletBC
variable = temp
boundary = rightright
value = 400
[../]
[]
[ThermalContact]
[./left_to_right]
secondary = leftright
quadrature = true
primary = rightleft
emissivity_primary = 0
emissivity_secondary = 0
variable = temp
type = GapHeatTransfer
[../]
[]
[Materials]
[./hcm]
type = HeatConductionMaterial
block = 'left right'
specific_heat = 1
thermal_conductivity = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[./Quadrature]
order = THIRD
[../]
[]
[Outputs]
exodus = true
[]
(test/tests/postprocessors/interface_value/interface_fe_variable_value_postprocessor.i)
postprocessor_type = InterfaceAverageVariableValuePostprocessor
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 6
xmax = 3
ny = 9
ymax = 3
elem_type = QUAD4
[]
[./subdomain_id]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '0 0 0'
top_right = '2 1 0'
block_id = 1
[../]
[./interface]
input = subdomain_id
type = SideSetsBetweenSubdomainsGenerator
primary_block = '0'
paired_block = '1'
new_boundary = 'interface'
[../]
[]
[Functions]
[./fn_exact]
type = ParsedFunction
value = 'x*x+y*y'
[../]
[./ffn]
type = ParsedFunction
value = -4
[../]
[]
[Variables]
[./u]
family = LAGRANGE
order = FIRST
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = ffn
[../]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
boundary = '0 1 2 3'
function = fn_exact
[../]
[]
[Materials]
[./stateful1]
type = StatefulMaterial
block = 0
initial_diffusivity = 5
[../]
[./stateful2]
type = StatefulMaterial
block = 1
initial_diffusivity = 2
[../]
[]
[AuxKernels]
[./diffusivity_1]
type = MaterialRealAux
property = diffusivity
variable = diffusivity_1
[]
[./diffusivity_2]
type = MaterialRealAux
property = diffusivity
variable = diffusivity_2
[]
[]
[AuxVariables]
[./diffusivity_1]
family = MONOMIAL
order = CONSTANT
[]
[./diffusivity_2]
family = MONOMIAL
order = CONSTANT
[]
[]
[Postprocessors]
[./diffusivity_average]
type = ${postprocessor_type}
interface_value_type = average
variable = diffusivity_1
neighbor_variable = diffusivity_2
execute_on = TIMESTEP_END
boundary = 'interface'
[../]
[./diffusivity_jump_primary_secondary]
type = ${postprocessor_type}
interface_value_type = jump_primary_minus_secondary
variable = diffusivity_1
neighbor_variable = diffusivity_2
execute_on = TIMESTEP_END
boundary = 'interface'
[../]
[./diffusivity_jump_secondary_primary]
type = ${postprocessor_type}
interface_value_type = jump_secondary_minus_primary
variable = diffusivity_1
neighbor_variable = diffusivity_2
execute_on = TIMESTEP_END
boundary = 'interface'
[../]
[./diffusivity_jump_abs]
type = ${postprocessor_type}
interface_value_type = jump_abs
variable = diffusivity_1
neighbor_variable = diffusivity_2
execute_on = TIMESTEP_END
boundary = 'interface'
[../]
[./diffusivity_primary]
type = ${postprocessor_type}
interface_value_type = primary
variable = diffusivity_1
neighbor_variable = diffusivity_2
execute_on = TIMESTEP_END
boundary = 'interface'
[../]
[./diffusivity_secondary]
type = ${postprocessor_type}
interface_value_type = secondary
variable = diffusivity_1
neighbor_variable = diffusivity_2
execute_on = TIMESTEP_END
boundary = 'interface'
[../]
[./diffusivity_single_variable]
type = ${postprocessor_type}
interface_value_type = primary
variable = diffusivity_1
execute_on = TIMESTEP_END
boundary = 'interface'
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
file_base = ${raw ${postprocessor_type} _fe}
exodus = true
[]
(test/tests/materials/derivative_material_interface/ad_material_chaining.i)
#
# This test validates the correct application of the chain rule to coupled
# material properties within DerivativeParsedMaterials
#
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
xmin = 0
xmax = 1
ymin = 0
ymax = 1
[]
[Variables]
[./eta1]
[../]
[./eta2]
[../]
[]
[BCs]
[./left]
variable = eta1
boundary = left
type = DirichletBC
value = 0
[../]
[./right]
variable = eta1
boundary = right
type = DirichletBC
value = 1
[../]
[./top]
variable = eta2
boundary = top
type = DirichletBC
value = 0
[../]
[./bottom]
variable = eta2
boundary = bottom
type = DirichletBC
value = 1
[../]
[]
[Materials]
# T1 := (eta1+1)^4
[./term]
type = ADDerivativeParsedMaterial
f_name= T1
args = 'eta1'
function = '(eta1+1)^4'
derivative_order = 4
[../]
# in this material we substitute T1 explicitly
[./full]
type = ADDerivativeParsedMaterial
args = 'eta1 eta2'
f_name = F1
function = '(1-eta2)^4+(eta1+1)^4'
[../]
# in this material we utilize the T1 derivative material property
[./subs]
type = ADDerivativeParsedMaterial
args = 'eta1 eta2'
f_name = F2
function = '(1-eta2)^4+T1'
material_property_names = 'T1(eta1)'
[../]
# calculate differences between the explicit and indirect substitution version
# the use if the T1 property should include dT1/deta1 contributions!
# This also demonstrated the explicit use of material property derivatives using
# the D[...] syntax.
[./diff0]
type = ADParsedMaterial
f_name = D0
function = '(F1-F2)^2'
material_property_names = 'F1 F2'
[../]
[./diff1]
type = ADParsedMaterial
f_name = D1
function = '(dF1-dF2)^2'
material_property_names = 'dF1:=D[F1,eta1] dF2:=D[F2,eta1]'
[../]
[./diff2]
type = ADParsedMaterial
f_name = D2
function = '(d2F1-d2F2)^2'
material_property_names = 'd2F1:=D[F1,eta1,eta1] d2F2:=D[F2,eta1,eta1]'
[../]
# check that explicitly pulling a derivative yields the correct result by
# taking the difference of the manually calculated 1st derivative of T1 and the
# automatic derivative dT1 pulled in through dT1:=D[T1,eta1]
[./diff3]
type = ADParsedMaterial
f_name = E0
function = '(dTd1-(4*(eta1+1)^3))^2'
args = eta1
material_property_names = 'dTd1:=D[T1,eta1]'
[../]
[]
[Kernels]
[./eta1diff]
type = Diffusion
variable = eta1
[../]
[./eta2diff]
type = Diffusion
variable = eta2
[../]
[]
[Postprocessors]
[./D0]
type = ADElementIntegralMaterialProperty
mat_prop = D0
[../]
[./D1]
type = ADElementIntegralMaterialProperty
mat_prop = D1
[../]
[./D2]
type = ADElementIntegralMaterialProperty
mat_prop = D2
[../]
[./E0]
type = ADElementIntegralMaterialProperty
mat_prop = E0
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
l_tol = 1e-03
[]
[Outputs]
execute_on = 'TIMESTEP_END'
csv = true
print_linear_residuals = false
[]
(test/tests/reporters/iteration_info/iteration_info_steady.i)
[Mesh]
[generate]
type = GeneratedMeshGenerator
dim = 1
nx = 10
[]
[]
[Variables/u][]
[Kernels]
[diff]
type = ADDiffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 10
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Reporters/iteration_info]
type = IterationInfo
[]
[Outputs]
[out]
type = JSON
execute_system_information_on = NONE
[]
[]
(test/tests/misc/save_in/save_in_soln_var_err_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./saved]
[../]
[./bc_saved]
[../]
[./accumulated]
[../]
[./diag_saved]
[../]
[./bc_diag_saved]
[../]
[./saved_dirichlet]
[../]
[./diag_saved_dirichlet]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
save_in = 'u saved accumulated saved_dirichlet'
diag_save_in = 'diag_saved diag_saved_dirichlet'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
save_in = saved_dirichlet
diag_save_in = diag_saved_dirichlet
[../]
[./nbc]
type = NeumannBC
variable = u
boundary = right
value = 1
save_in = 'bc_saved accumulated'
diag_save_in = bc_diag_saved
[../]
[]
[Postprocessors]
[./left_flux]
type = NodalSum
variable = saved
boundary = 1
[../]
[./saved_norm]
type = NodalL2Norm
variable = saved
execute_on = timestep_end
block = 0
[../]
[./saved_dirichlet_norm]
type = NodalL2Norm
variable = saved_dirichlet
execute_on = timestep_end
block = 0
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/outputs/format/output_test_tecplot_binary.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
nz = 0
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
[./out]
type = Tecplot
binary = true
[../]
[]
(test/tests/mesh/named_entities/named_entities_test_xda.i)
[Mesh]
file = named_entities.xda
uniform_refine = 1
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
block = '1 center_block 3'
[./InitialCondition]
type = ConstantIC
value = 20
block = 'center_block 3'
[../]
[../]
[]
[AuxVariables]
[./reporter]
order = CONSTANT
family = MONOMIAL
block = 'left_block 3'
[../]
[]
[ICs]
[./reporter_ic]
type = ConstantIC
variable = reporter
value = 10
[../]
[]
[Kernels]
active = 'diff body_force'
[./diff]
type = Diffusion
variable = u
# Note we are using both names and numbers here
block = 'left_block 2 right_block'
[../]
[./body_force]
type = BodyForce
variable = u
block = 'center_block'
value = 10
[../]
[]
[AuxKernels]
[./hardness]
type = MaterialRealAux
variable = reporter
property = 'hardness'
block = 'left_block 3'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 'left_side'
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = 'right_side'
value = 1
[../]
[]
[Postprocessors]
[./elem_average]
type = ElementAverageValue
variable = u
block = 'center_block'
execute_on = 'initial timestep_end'
[../]
[./side_average]
type = SideAverageValue
variable = u
boundary = 'right_side'
execute_on = 'initial timestep_end'
[../]
[]
[Materials]
[./constant]
type = GenericConstantMaterial
prop_names = 'hardness'
prop_values = 10
block = '1 right_block'
[../]
[./empty]
type = MTMaterial
block = 'center_block'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(modules/stochastic_tools/test/tests/surrogates/polynomial_regression/sub_vector.i)
L = 1
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
nx = 100
xmax = ${L}
elem_type = EDGE3
[]
[]
[Variables]
[T]
order = SECOND
family = LAGRANGE
[]
[]
[Kernels]
[diff]
type = MatDiffusion
variable = T
diffusivity = k
[]
[source]
type = BodyForce
variable = T
value = 10000
[]
[]
[Materials]
[conductivity]
type = GenericConstantMaterial
prop_names = k
prop_values = 2.0
[]
[]
[BCs]
[right]
type = DirichletBC
variable = T
boundary = right
value = 300
[]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[VectorPostprocessors]
[T_vec]
type = LineValueSampler
variable = T
start_point = '0 0 0'
end_point = '${L} 0 0'
num_points = 10
sort_by = x
[]
[]
[Outputs]
[]
(test/tests/misc/check_error/incomplete_fvkernel_block_coverage_test.i)
[Mesh]
file = rectangle.e
[]
[Variables]
active = 'u'
[./u]
order = CONSTANT
family = MONOMIAL
fv = true
[../]
[]
[FVKernels]
active = 'diff body_force'
[./diff]
type = FVDiffusion
variable = u
block = 1
coeff = 1
[../]
[./body_force]
type = FVBodyForce
variable = u
block = 1
value = 10
[../]
[]
[FVBCs]
active = 'right'
[./left]
type = FVDirichletBC
variable = u
boundary = 1
value = 1
[../]
[./right]
type = FVDirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
[]
(test/tests/variables/fe_hier/hier-3-2d.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 5
ny = 5
elem_type = QUAD9
[]
[Functions]
[./bc_fnt]
type = ParsedFunction
value = 3*y*y
[../]
[./bc_fnb]
type = ParsedFunction
value = -3*y*y
[../]
[./bc_fnl]
type = ParsedFunction
value = -3*x*x
[../]
[./bc_fnr]
type = ParsedFunction
value = 3*x*x
[../]
[./forcing_fn]
type = ParsedFunction
value = -6*x-6*y+(x*x*x)+(y*y*y)
[../]
[./solution]
type = ParsedGradFunction
value = (x*x*x)+(y*y*y)
grad_x = 3*x*x
grad_y = 3*y*y
[../]
[]
[Variables]
[./u]
order = THIRD
family = HIERARCHIC
[../]
[]
[Kernels]
active = 'diff forcing reaction'
[./diff]
type = Diffusion
variable = u
[../]
[./reaction]
type = Reaction
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
[./bc_top]
type = FunctionNeumannBC
variable = u
boundary = 'top'
function = bc_fnt
[../]
[./bc_bottom]
type = FunctionNeumannBC
variable = u
boundary = 'bottom'
function = bc_fnb
[../]
[./bc_left]
type = FunctionNeumannBC
variable = u
boundary = 'left'
function = bc_fnl
[../]
[./bc_right]
type = FunctionNeumannBC
variable = u
boundary = 'right'
function = bc_fnr
[../]
[]
[Postprocessors]
[./dofs]
type = NumDOFs
[../]
[./h]
type = AverageElementSize
[../]
[./L2error]
type = ElementL2Error
variable = u
function = solution
[../]
[./H1error]
type = ElementH1Error
variable = u
function = solution
[../]
[./H1Semierror]
type = ElementH1SemiError
variable = u
function = solution
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
csv = true
[]
(test/tests/dampers/constant_damper/constant_damper_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Dampers]
[./const_damp]
type = ConstantDamper
damping = 0.9
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/interfacekernels/3d_interface/coupled_value_coupled_flux_with_jump_material.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
nx = 2
xmax = 2
ny = 2
ymax = 2
nz = 2
zmax = 2
[]
[./subdomain1]
type = SubdomainBoundingBoxGenerator
bottom_left = '0 0 0'
top_right = '1 1 1'
block_id = 1
input = gen
[../]
[./break_boundary]
input = subdomain1
type = BreakBoundaryOnSubdomainGenerator
[../]
[./interface]
type = SideSetsBetweenSubdomainsGenerator
input = break_boundary
primary_block = '0'
paired_block = '1'
new_boundary = 'primary0_interface'
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
block = 0
[../]
[./v]
order = FIRST
family = LAGRANGE
block = 1
[../]
[]
[Kernels]
[./diff_u]
type = CoeffParamDiffusion
variable = u
D = 4
block = 0
[../]
[./diff_v]
type = CoeffParamDiffusion
variable = v
D = 2
block = 1
[../]
[./source_u]
type = BodyForce
variable = u
value = 1
[../]
[]
[AuxVariables]
[./jump_var]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[jump_aux]
type = MaterialRealAux
boundary = primary0_interface
property = jump
variable = jump_var
[]
[]
[InterfaceKernels]
[./interface]
type = PenaltyInterfaceDiffusion
variable = u
neighbor_var = v
boundary = primary0_interface
penalty = 1e6
jump_prop_name = jump
[../]
[]
[Materials]
[./jump]
type = JumpInterfaceMaterial
var = u
neighbor_var = v
boundary = primary0_interface
[../]
[]
[BCs]
[./u]
type = VacuumBC
variable = u
boundary = 'left_to_0 bottom_to_0 back_to_0 right top front'
[../]
[./v]
type = VacuumBC
variable = v
boundary = 'left_to_1 bottom_to_1 back_to_1'
[../]
[]
[Postprocessors]
[./u_int]
type = ElementIntegralVariablePostprocessor
variable = u
block = 0
[../]
[./v_int]
type = ElementIntegralVariablePostprocessor
variable = v
block = 1
[../]
[interface_var_jump]
type = InterfaceAverageVariableValuePostprocessor
interface_value_type = jump_abs
variable = u
neighbor_variable = v
execute_on = TIMESTEP_END
boundary = primary0_interface
[]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
print_linear_residuals = true
[]
(modules/heat_conduction/test/tests/code_verification/cylindrical_test_no5.i)
# Problem II.5
#
# The volumetric heat generation in an infinitely long solid cylinder
# varies with spatial location. It has a constant thermal conductivity.
#
# REFERENCE:
# A. Toptan, et al. (Mar.2020). Tech. rep. CASL-U-2020-1939-000, SAND2020-3887 R. DOI:10.2172/1614683.
[Mesh]
[./geom]
type = GeneratedMeshGenerator
dim = 1
elem_type = EDGE2
nx = 1
[../]
[]
[Variables]
[./u]
order = FIRST
[../]
[]
[Problem]
coord_type = RZ
[]
[Functions]
[./volumetric_heat]
type = ParsedFunction
vars = 'q ro beta'
vals = '1200 1 0.1'
value = 'q * (1-beta*x/ro)'
[../]
[./exact]
type = ParsedFunction
vars = 'uo q k ro beta'
vals = '300 1200 1 1 0.1'
value = 'uo + (0.25*q*ro^2/k) * ( (1-(x/ro)^2) - (1-(x/ro)^3) * beta * 4/9 )'
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = u
[../]
[./heatsource]
type = HeatSource
function = volumetric_heat
variable = u
[../]
[]
[BCs]
[./uo]
type = DirichletBC
boundary = right
variable = u
value = 300
[../]
[]
[Materials]
[./property]
type = GenericConstantMaterial
prop_names = 'density specific_heat thermal_conductivity'
prop_values = '1.0 1.0 1.0'
[../]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[./error]
type = ElementL2Error
function = exact
variable = u
[../]
[./h]
type = AverageElementSize
[]
[]
[Outputs]
csv = true
[]
(test/tests/quadrature/order/code-order-bump.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 1
ny = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 2
[]
[left]
type = SubdomainBoundingBoxGenerator
input = gmg
block_id = 1
bottom_left = '0 0 0'
top_right = '1 1 0'
[]
[right]
type = SubdomainBoundingBoxGenerator
input = left
block_id = 2
bottom_left = '0 1 0'
top_right = '1 2 0'
[]
[]
[Materials]
[mat2]
type = QuadratureOrderBumper
order = third
block = '1'
[]
[mat]
type = QuadratureOrderBumper
order = tenth
block = '2'
[]
[]
[Postprocessors]
[block1_qps]
type = NumElemQPs
block = 1
[]
[block2_qps]
type = NumElemQPs
block = 2
[]
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
execute_on = 'timestep_end'
exodus = false
csv = true
[]
(test/tests/kernels/ad_coupled_force/aux_test.i)
[Mesh]
[square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[]
[]
[Variables]
[u]
[]
[]
[AuxVariables]
[a]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
[diff]
type = ADDiffusion
variable = u
[]
[force]
type = ADCoupledForce
variable = u
v = a
[]
[]
[AuxKernels]
[a]
variable = a
type = ConstantAux
value = 10
[]
[]
[BCs]
[left]
type = ADDirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = ADDirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
(test/tests/postprocessors/scale_pps/scale_pps.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
[]
[Variables]
[./u]
[../]
[]
[ICs]
[./u_ic]
type = ConstantIC
variable = u
value = 2
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Postprocessors]
[./u_avg]
type = ElementAverageValue
variable = u
execute_on = 'initial timestep_end'
[../]
[./scaled_u]
type = ScalePostprocessor
value = u_avg
scaling_factor = 2
execute_on = 'initial timestep_end'
[../]
[./scaled_scaled_u]
type = ScalePostprocessor
value = scaled_u
scaling_factor = 2
execute_on = 'initial timestep_end'
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/partitioners/file_mesh_skip_partition/file_mesh_skip_partitioning.i)
[Mesh]
[generate_2d]
type = FileMeshGenerator
file = 2d_base.e
skip_partitioning = true
[]
[extrude]
type = MeshExtruderGenerator
input = generate_2d
extrusion_vector = '0 0 1'
num_layers = 5
[]
[Partitioner]
type = HierarchicalGridPartitioner
nx_nodes = 2
ny_nodes = 1
nz_nodes = 1
nx_procs = 1
ny_procs = 1
nz_procs = 2
[]
[]
[Variables]
[u]
[]
[]
[AuxVariables]
[pid]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[pid]
type = ProcessorIDAux
variable = pid
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/pp_as_reporter/pp_as_reporter.i)
[Mesh/gen]
type = GeneratedMeshGenerator
dim = 1
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Postprocessors/data]
type = FunctionValuePostprocessor
function = 1980
[]
[Outputs]
[out]
type = JSON
postprocessors_as_reporters = true
execute_system_information_on = none
[]
[]
(tutorials/darcy_thermo_mech/step01_diffusion/problems/step1.i)
[Mesh]
type = GeneratedMesh # Can generate simple lines, rectangles and rectangular prisms
dim = 2 # Dimension of the mesh
nx = 100 # Number of elements in the x direction
ny = 10 # Number of elements in the y direction
xmax = 0.304 # Length of test chamber
ymax = 0.0257 # Test chamber radius
[]
[Variables]
[pressure]
# Adds a Linear Lagrange variable by default
[]
[]
[Kernels]
[diffusion]
type = ADDiffusion # Laplacian operator using automatic differentiation
variable = pressure # Operate on the "pressure" variable from above
[]
[]
[BCs]
[inlet]
type = DirichletBC # Simple u=value BC
variable = pressure # Variable to be set
boundary = left # Name of a sideset in the mesh
value = 4000 # (Pa) From Figure 2 from paper. First data point for 1mm spheres.
[]
[outlet]
type = DirichletBC
variable = pressure
boundary = right
value = 0 # (Pa) Gives the correct pressure drop from Figure 2 for 1mm spheres
[]
[]
[Problem]
type = FEProblem # This is the "normal" type of Finite Element Problem in MOOSE
coord_type = RZ # Axisymmetric RZ
rz_coord_axis = X # Which axis the symmetry is around
[]
[Executioner]
type = Steady # Steady state problem
solve_type = NEWTON # Perform a Newton solve, uses AD to compute Jacobian terms
petsc_options_iname = '-pc_type -pc_hypre_type' # PETSc option pairs with values below
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true # Output Exodus format
[]
(test/tests/misc/check_error/coupling_scalar_into_field.i)
[Mesh]
type = GeneratedMesh
dim = 2
[]
[Variables]
[./u]
[../]
[./a]
family = SCALAR
order = FIRST
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./coupled]
type = CoupledForce
variable = u
# this should trigger an error message, 'v' should a field variable
v = a
[../]
[]
[ScalarKernels]
[./alpha]
type = AlphaCED
variable = a
value = 1
[../]
[]
[BCs]
[./all]
type = DirichletBC
boundary = 'left right top bottom'
variable = u
value = 0
[../]
[]
[Executioner]
type = Steady
[]
(test/tests/misc/check_error/constraint_with_aux_var.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./v]
[../]
[]
[Constraints]
[./nope]
type = CoupledTiedValueConstraint
variable = v
secondary = 2
primary = 3
primary_variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/porous_flow/test/tests/poroperm/PermFromPoro05.i)
# Testing permeability from porosity
# Trivial test, checking calculated permeability is correct
# k = k_anisotropic * k
# with ln k = A * phi + B
[Mesh]
type = GeneratedMesh
dim = 1
nx = 3
xmin = 0
xmax = 3
[]
[GlobalParams]
block = 0
PorousFlowDictator = dictator
[]
[Variables]
[pp]
[InitialCondition]
type = ConstantIC
value = 0
[]
[]
[]
[Kernels]
[flux]
type = PorousFlowAdvectiveFlux
gravity = '0 0 0'
variable = pp
[]
[]
[BCs]
[ptop]
type = DirichletBC
variable = pp
boundary = right
value = 0
[]
[pbase]
type = DirichletBC
variable = pp
boundary = left
value = 1
[]
[]
[AuxVariables]
[poro]
order = CONSTANT
family = MONOMIAL
[]
[perm_x]
order = CONSTANT
family = MONOMIAL
[]
[perm_y]
order = CONSTANT
family = MONOMIAL
[]
[perm_z]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[poro]
type = PorousFlowPropertyAux
property = porosity
variable = poro
[]
[perm_x]
type = PorousFlowPropertyAux
property = permeability
variable = perm_x
row = 0
column = 0
[]
[perm_y]
type = PorousFlowPropertyAux
property = permeability
variable = perm_y
row = 1
column = 1
[]
[perm_z]
type = PorousFlowPropertyAux
property = permeability
variable = perm_z
row = 2
column = 2
[]
[]
[Postprocessors]
[perm_x_bottom]
type = PointValue
variable = perm_x
point = '0 0 0'
[]
[perm_y_bottom]
type = PointValue
variable = perm_y
point = '0 0 0'
[]
[perm_z_bottom]
type = PointValue
variable = perm_z
point = '0 0 0'
[]
[perm_x_top]
type = PointValue
variable = perm_x
point = '3 0 0'
[]
[perm_y_top]
type = PointValue
variable = perm_y
point = '3 0 0'
[]
[perm_z_top]
type = PointValue
variable = perm_z
point = '3 0 0'
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureVG
# unimportant in this fully-saturated test
m = 0.8
alpha = 1e-4
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 2.2e9
viscosity = 1e-3
density0 = 1000
thermal_expansion = 0
[]
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[massfrac]
type = PorousFlowMassFraction
[]
[eff_fluid_pressure]
type = PorousFlowEffectiveFluidPressure
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pp
capillary_pressure = pc
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[porosity]
type = PorousFlowPorosity
porosity_zero = 0.1
[]
[permeability]
type = PorousFlowPermeabilityExponential
k_anisotropy = '1 0 0 0 2 0 0 0 0.1'
poroperm_function = ln_k
A = 10.0
B = -18.420681
[]
[relperm]
type = PorousFlowRelativePermeabilityCorey
n = 0 # unimportant in this fully-saturated situation
phase = 0
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
[]
[]
[Executioner]
solve_type = Newton
type = Steady
l_tol = 1E-5
nl_abs_tol = 1E-3
nl_rel_tol = 1E-8
l_max_its = 200
nl_max_its = 400
petsc_options_iname = '-pc_type -pc_asm_overlap -sub_pc_type -ksp_type -ksp_gmres_restart'
petsc_options_value = ' asm 2 lu gmres 200'
[]
[Outputs]
csv = true
execute_on = 'timestep_end'
[]
(test/tests/ics/depend_on_uo/geometric_neighbors_ic.i)
# This test verifies that if an Initial Condition depends on a UO and is
# set to "initial" that it will be executed _BEFORE_ the initial condition
[Mesh]
type = GeneratedMesh
dim = 2
nx = 8
ny = 8
# We are testing geometric ghosted functors
# so we have to use distributed mesh
parallel_type = distributed
[]
[Variables]
[./ghost]
order = CONSTANT
family = MONOMIAL
[../]
[]
[ICs]
[./ghost_ic]
type = ElementUOIC
variable = ghost
element_user_object = ghost_uo
field_name = "ghosted"
field_type = long
[../]
[]
[UserObjects]
[./ghost_uo]
type = ElemSideNeighborLayersTester
execute_on = initial
element_side_neighbor_layers = 1
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
[Problem]
solve = false
kernel_coverage_check = false
[]
(modules/ray_tracing/test/tests/traceray/backface_culling/backface_culling.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
nx = 5
ny = 5
nz = 5
xmax = 5
ymax = 5
zmax = 5
[]
[]
[RayBCs]
active = ''
[kill_1d]
type = KillRayBC
boundary = 'left right'
[]
[kill_2d]
type = KillRayBC
boundary = 'top right bottom left'
[]
[kill_3d]
type = KillRayBC
boundary = 'top right bottom left front back'
[]
[]
[UserObjects/study]
type = BackfaceCullingStudyTest
ray_kernel_coverage_check = false
vertex_to_vertex = true
centroid_to_vertex = true
centroid_to_centroid = true
side_aq = true
centroid_aq = true
edge_to_edge = false
compute_expected_distance = true
execute_on = initial
[]
[Postprocessors]
[total_distance]
type = RayTracingStudyResult
study = study
result = total_distance
[]
[expected_distance]
type = LotsOfRaysExpectedDistance
lots_of_rays_study = study
[]
[distance_difference]
type = DifferencePostprocessor
value1 = total_distance
value2 = expected_distance
[]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Outputs]
exodus = false
csv = true
[]
(test/tests/meshgenerators/distributed_rectilinear/partition/squarish_partition.i)
[Mesh]
[gmg]
type = DistributedRectilinearMeshGenerator
dim = 2
nx = 20
ny = 30
partition = square
[]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[pid]
family = MONOMIAL
order = CONSTANT
[]
[npid]
family = Lagrange
order = first
[]
[]
[AuxKernels]
[pid_aux]
type = ProcessorIDAux
variable = pid
execute_on = 'INITIAL'
[]
[npid_aux]
type = ProcessorIDAux
variable = npid
execute_on = 'INITIAL'
[]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
preset = false
boundary = 'left'
value = 0
[../]
[./right]
type = DirichletBC
variable = u
preset = false
boundary = 'right'
value = 1
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type'
petsc_options_value = 'hypre'
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(test/tests/userobjects/layered_side_integral/layered_side_diffusive_flux_average.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 6
ny = 6
nz = 6
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./layered_side_flux_average]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = u
boundary = bottom
value = 0
[../]
[./top]
type = DirichletBC
variable = u
boundary = top
value = 1
[../]
[]
[AuxKernels]
[./lsfa]
type = SpatialUserObjectAux
variable = layered_side_flux_average
boundary = top
user_object = layered_side_flux_average
[../]
[]
[Materials]
[./gcm]
type = GenericConstantMaterial
prop_values = 2
prop_names = diffusivity
boundary = 'right top'
[../]
[]
[UserObjects]
[./layered_side_flux_average]
type = LayeredSideDiffusiveFluxAverage
direction = y
diffusivity = diffusivity
num_layers = 1
variable = u
execute_on = linear
boundary = top
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
[Debug]
show_material_props = true
[]
(modules/porous_flow/test/tests/capillary_pressure/brooks_corey2.i)
# Test Brooks-Corey capillary pressure curve by varying saturation over the mesh
# lambda = 2, sat_lr = 0.1, log_extension = true
[Mesh]
type = GeneratedMesh
dim = 1
nx = 500
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Variables]
[p0]
initial_condition = 1e6
[]
[s1]
[]
[]
[AuxVariables]
[s0aux]
family = MONOMIAL
order = CONSTANT
[]
[s1aux]
family = MONOMIAL
order = CONSTANT
[]
[p0aux]
family = MONOMIAL
order = CONSTANT
[]
[p1aux]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[s0]
type = PorousFlowPropertyAux
property = saturation
phase = 0
variable = s0aux
[]
[s1]
type = PorousFlowPropertyAux
property = saturation
phase = 1
variable = s1aux
[]
[p0]
type = PorousFlowPropertyAux
property = pressure
phase = 0
variable = p0aux
[]
[p1]
type = PorousFlowPropertyAux
property = pressure
phase = 1
variable = p1aux
[]
[]
[Functions]
[s1]
type = ParsedFunction
value = x
[]
[]
[ICs]
[s1]
type = FunctionIC
variable = s1
function = s1
[]
[]
[Kernels]
[p0]
type = Diffusion
variable = p0
[]
[s1]
type = Diffusion
variable = s1
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'p0 s1'
number_fluid_phases = 2
number_fluid_components = 2
[]
[pc]
type = PorousFlowCapillaryPressureBC
lambda = 2
log_extension = true
pe = 1e5
sat_lr = 0.1
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow2PhasePS
phase0_porepressure = p0
phase1_saturation = s1
capillary_pressure = pc
[]
[kr0]
type = PorousFlowRelativePermeabilityVG
phase = 0
m = 0.5
[]
[kr1]
type = PorousFlowRelativePermeabilityCorey
phase = 1
n = 2
[]
[]
[VectorPostprocessors]
[vpp]
type = LineValueSampler
variable = 's0aux s1aux p0aux p1aux'
start_point = '0 0 0'
end_point = '1 0 0'
num_points = 500
sort_by = id
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
nl_abs_tol = 1e-6
[]
[BCs]
[sleft]
type = DirichletBC
variable = s1
value = 0
boundary = left
[]
[sright]
type = DirichletBC
variable = s1
value = 1
boundary = right
[]
[]
[Outputs]
csv = true
execute_on = timestep_end
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_mortar/modular_gap_heat_transfer_mortar_displaced_radiation.i)
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
[file]
type = FileMeshGenerator
file = 2blk-gap.e
[]
[secondary]
type = LowerDBlockFromSidesetGenerator
sidesets = '101'
new_block_id = 10001
new_block_name = 'secondary_lower'
input = file
[]
[primary]
type = LowerDBlockFromSidesetGenerator
sidesets = '100'
new_block_id = 10000
new_block_name = 'primary_lower'
input = secondary
[]
allow_renumbering = false
[]
[Problem]
kernel_coverage_check = false
material_coverage_check = false
[]
[Variables]
[temp]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[disp_x]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[disp_y]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[lm]
order = FIRST
family = LAGRANGE
block = 'secondary_lower'
[]
[]
[Materials]
[left]
type = ADHeatConductionMaterial
block = 1
thermal_conductivity = 0.01
specific_heat = 1
[]
[right]
type = ADHeatConductionMaterial
block = 2
thermal_conductivity = 0.005
specific_heat = 1
[]
[]
[Kernels]
[hc_displaced_block]
type = ADHeatConduction
variable = temp
use_displaced_mesh = true
block = '1'
[]
[hc_undisplaced_block]
type = ADHeatConduction
variable = temp
use_displaced_mesh = false
block = '2'
[]
[disp_x]
type = Diffusion
variable = disp_x
block = '1 2'
[]
[disp_y]
type = Diffusion
variable = disp_y
block = '1 2'
[]
[]
[UserObjects]
[radiation]
type = GapFluxModelRadiation
temperature = temp
boundary = 100
primary_emissivity = 1.0
secondary_emissivity = 1.0
use_displaced_mesh = true
[]
[]
[Constraints]
[ced]
type = ModularGapConductanceConstraint
variable = lm
secondary_variable = temp
use_displaced_mesh = true
primary_boundary = 100
primary_subdomain = 10000
secondary_boundary = 101
secondary_subdomain = 10001
gap_flux_models = radiation
[]
[]
[BCs]
[left]
type = DirichletBC
variable = temp
boundary = 'left'
value = 100
[]
[right]
type = DirichletBC
variable = temp
boundary = 'right'
value = 0
[]
[left_disp_x]
type = DirichletBC
preset = false
variable = disp_x
boundary = 'left'
value = .1
[]
[right_disp_x]
type = DirichletBC
preset = false
variable = disp_x
boundary = 'right'
value = 0
[]
[bottom_disp_y]
type = DirichletBC
preset = false
variable = disp_y
boundary = 'bottom'
value = 0
[]
[]
[Preconditioning]
[fmp]
type = SMP
full = true
solve_type = 'NEWTON'
[]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-11
nl_abs_tol = 1.0e-10
[]
[VectorPostprocessors]
[NodalTemperature]
type = NodalValueSampler
sort_by = id
boundary = '100 101'
variable = 'temp'
[]
[]
[Outputs]
exodus = false
csv = true
[]
(examples/ex07_ics/steady.i)
[Mesh]
file = half-cone.e
[]
[Variables]
[./diffused]
order = FIRST
family = LAGRANGE
# Use the initial Condition block underneath the variable
# for which we want to apply this initial condition
[./InitialCondition]
type = ExampleIC
coefficient = 2.0
[../]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = diffused
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = diffused
boundary = 'top'
value = 2
[../]
[./right]
type = DirichletBC
variable = diffused
boundary = 'bottom'
value = 8
[../]
[]
[Executioner]
type = Steady
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
[]
[Outputs]
# Request that we output the initial condition so we can inspect
# the values with our visualization tool
exodus = true
[]
(test/tests/variables/optionally_coupled/optionally_coupled_system.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
elem_type = QUAD4
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[./v]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./coupled]
type = OptionallyCoupledForce
variable = u
v = v
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[BCs]
[./left_u]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = left
value = 2
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = right
value = 3
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(modules/phase_field/test/tests/MultiPhase/orderparameterfunctionmaterial.i)
#
# This test validates the helper materials that generate material properties for
# the h(eta) switching function and the g(eta) double well function
#
[Mesh]
type = GeneratedMesh
dim = 2
nx = 40
ny = 5
nz = 0
xmin = 0
xmax = 1
ymin = 0
ymax = 1
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[BCs]
[./left1]
type = DirichletBC
variable = eta1
boundary = 'left'
value = 0
[../]
[./right1]
type = DirichletBC
variable = eta1
boundary = 'right'
value = 1
[../]
[./left2]
type = DirichletBC
variable = eta2
boundary = 'left'
value = 0
[../]
[./right2]
type = DirichletBC
variable = eta2
boundary = 'right'
value = 1
[../]
[]
[Variables]
# order parameter 1
[./eta1]
order = FIRST
family = LAGRANGE
[../]
# order parameter 2
[./eta2]
order = FIRST
family = LAGRANGE
[../]
[]
[Materials]
[./h_eta1]
type = SwitchingFunctionMaterial
h_order = SIMPLE
eta = eta1
function_name = h1
outputs = exodus
[../]
[./h_eta2]
type = SwitchingFunctionMaterial
h_order = HIGH
eta = eta2
function_name = h2
outputs = exodus
[../]
[./g_eta1]
type = BarrierFunctionMaterial
g_order = SIMPLE
eta = eta1
function_name = g1
outputs = exodus
[../]
[./g_eta2]
type = BarrierFunctionMaterial
g_order = LOW
eta = eta2
function_name = g2
outputs = exodus
[../]
[]
[Kernels]
[./eta1diff]
type = Diffusion
variable = eta1
[../]
[./eta2diff]
type = Diffusion
variable = eta2
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(test/tests/auxkernels/solution_aux/solution_aux_exodus_elem_map.i)
[Mesh]
file = elem_map.e
# The SolutionUserObject uses the copy_nodal_solution() capability
# of the Exodus reader, and therefore won't work if the initial mesh
# has been renumbered (it will be reunumbered if you are running with
# DistributedMesh in parallel). Hence, we restrict this test to run with
# ReplicatedMesh only.
parallel_type = replicated
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
initial_condition = 0.0
[../]
[]
[AuxVariables]
[./matid]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./matid]
type = SolutionAux
solution = soln
variable = matid
scale_factor = 1.0
[../]
[]
[UserObjects]
[./soln]
type = SolutionUserObject
mesh = elem_map.e
system_variables = MatID
timestep = LATEST
[../]
[]
[BCs]
[./stuff]
type = DirichletBC
variable = u
boundary = '1'
value = 1.0
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(test/tests/relationship_managers/evaluable/evaluable.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 8
ny = 8
[]
[GlobalParams]
order = CONSTANT
family = MONOMIAL
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
[]
[]
[AuxVariables]
[evaluable0]
[]
[evaluable1]
[]
[evaluable2]
[]
[proc]
[]
[]
[AuxKernels]
[evaluable0]
type = ElementUOAux
variable = evaluable0
element_user_object = evaluable_uo0
field_name = "evaluable"
execute_on = initial
[]
[evaluable1]
type = ElementUOAux
variable = evaluable1
element_user_object = evaluable_uo1
field_name = "evaluable"
execute_on = initial
[]
[evaluable2]
type = ElementUOAux
variable = evaluable2
element_user_object = evaluable_uo2
field_name = "evaluable"
execute_on = initial
[]
[proc]
type = ProcessorIDAux
variable = proc
execute_on = initial
[]
[]
[UserObjects]
[evaluable_uo0]
type = ElemSideNeighborLayersTester
execute_on = initial
element_side_neighbor_layers = 2
rank = 0
[]
[evaluable_uo1]
type = ElemSideNeighborLayersTester
execute_on = initial
element_side_neighbor_layers = 2
rank = 1
[]
[evaluable_uo2]
type = ElemSideNeighborLayersTester
execute_on = initial
element_side_neighbor_layers = 2
rank = 2
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
[Problem]
solve = false
kernel_coverage_check = false
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_mortar_action/modular_gap_heat_transfer_mortar_displaced_conduction_UOs_function.i)
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
[file]
type = FileMeshGenerator
file = 2blk-gap.e
[]
allow_renumbering = false
[]
[Problem]
kernel_coverage_check = false
material_coverage_check = false
[]
[Variables]
[temp]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[disp_x]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[disp_y]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[]
[Functions]
[gc_function]
type = PiecewiseLinear
x = '-10000 10000'
y = '0.02 0.02'
[]
[]
[Materials]
[left]
type = ADHeatConductionMaterial
block = 1
thermal_conductivity = 0.01
specific_heat = 1
[]
[right]
type = ADHeatConductionMaterial
block = 2
thermal_conductivity = 0.005
specific_heat = 1
[]
[]
[Kernels]
[hc_displaced_block]
type = ADHeatConduction
variable = temp
use_displaced_mesh = true
block = '1'
[]
[hc_undisplaced_block]
type = ADHeatConduction
variable = temp
use_displaced_mesh = false
block = '2'
[]
[disp_x]
type = Diffusion
variable = disp_x
block = '1 2'
[]
[disp_y]
type = Diffusion
variable = disp_y
block = '1 2'
[]
[]
[MortarGapHeatTransfer]
[mortar_heat_transfer]
temperature = temp
boundary = 100
use_displaced_mesh = true
primary_boundary = 100
secondary_boundary = 101
user_created_gap_flux_models = 'radiation_uo conduction_uo'
[]
[]
[UserObjects]
[radiation_uo]
type = GapFluxModelRadiation
temperature = temp
boundary = 100
primary_emissivity = 1.0
secondary_emissivity = 1.0
use_displaced_mesh = true
[]
[conduction_uo]
type = GapFluxModelConduction
temperature = temp
boundary = 100
gap_conductivity_function = gc_function
gap_conductivity_function_variable = temp
gap_conductivity = 1.0
use_displaced_mesh = true
[]
[]
[BCs]
[left]
type = DirichletBC
variable = temp
boundary = 'left'
value = 100
[]
[right]
type = DirichletBC
variable = temp
boundary = 'right'
value = 0
[]
[left_disp_x]
type = DirichletBC
preset = false
variable = disp_x
boundary = 'left'
value = .1
[]
[right_disp_x]
type = DirichletBC
preset = false
variable = disp_x
boundary = 'right'
value = 0
[]
[bottom_disp_y]
type = DirichletBC
preset = false
variable = disp_y
boundary = 'bottom'
value = 0
[]
[]
[Preconditioning]
[fmp]
type = SMP
full = true
solve_type = 'NEWTON'
[]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-11
nl_abs_tol = 1.0e-10
[]
[VectorPostprocessors]
[NodalTemperature]
type = NodalValueSampler
sort_by = id
boundary = '100 101'
variable = 'temp'
[]
[]
[Outputs]
csv = true
[exodus]
type = Exodus
show = 'temp'
[]
[]
(test/tests/userobjects/layered_integral/cumulative_layered_integral.i)
# ##########################################################
# This is a test of the UserObject System. The
# LayeredIntegral UserObject executes independently during
# the solve to compute a user-defined value. In this case
# an integral value in discrete layers along a vector
# in the domain. (Type: ElementalUserObject)
#
# @Requirement F6.40
# ##########################################################
[Mesh]
type = GeneratedMesh
dim = 2
nx = 6
ny = 6
nz = 6
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./layered_integral]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./liaux]
type = SpatialUserObjectAux
variable = layered_integral
execute_on = timestep_end
user_object = layered_integral
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = u
boundary = bottom
value = 0
[../]
[./top]
type = DirichletBC
variable = u
boundary = top
value = 1
[../]
[]
[UserObjects]
[./layered_integral]
type = LayeredIntegral
direction = y
num_layers = 3
variable = u
execute_on = linear
cumulative = true
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/mesh_modifiers/assign_subdomain_id/assign_subdomain_id.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[assign_id]
type = SubdomainIDGenerator
input = gen
subdomain_id = 3
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/variables/previous_newton_iteration/test.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 2
ny = 2
elem_type = QUAD9
[]
[Problem]
previous_nl_solution_required = true
[]
[Functions]
[./v_fn]
type = ParsedFunction
value = -4+(x*x+y*y)+1
[../]
[./left_u_bc_fn]
type = ParsedFunction
value = -2*x
[../]
[./top_u_bc_fn]
type = ParsedFunction
value = 2*y
[../]
[./right_u_bc_fn]
type = ParsedFunction
value = 2*x
[../]
[./bottom_u_bc_fn]
type = ParsedFunction
value = -2*y
[../]
[]
[AuxVariables]
[./a]
order = SECOND
[../]
[./v]
order = SECOND
[../]
[]
[AuxKernels]
[./ak_a]
type = QuotientAux
variable = a
numerator = v
denominator = u
[../]
[./ak_v]
type = FunctionAux
variable = v
function = v_fn
[../]
[]
[Variables]
[./u]
order = SECOND
[../]
[]
[ICs]
[./u_ic]
type = ConstantIC
variable = u
value = 1
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./react]
type = Reaction
variable = u
[../]
[./cv_u]
type = CoupledForceLagged
variable = u
v = v
[../]
[]
[BCs]
[./u_bc_left]
type = FunctionNeumannBC
variable = u
boundary = 'left'
function = left_u_bc_fn
[../]
[./u_bc_top]
type = FunctionNeumannBC
variable = u
boundary = 'top'
function = top_u_bc_fn
[../]
[./u_bc_right]
type = FunctionNeumannBC
variable = u
boundary = 'right'
function = right_u_bc_fn
[../]
[./u_bc_bottom]
type = FunctionNeumannBC
variable = u
boundary = 'bottom'
function = bottom_u_bc_fn
[../]
[]
[Preconditioning]
[./pc]
type = SMP
full = true
solve_type = PJFNK
[../]
[]
[Executioner]
type = Steady
# to get multiple NL iterations
l_tol = 1e-3
nl_rel_tol = 1e-10
[]
[Outputs]
[./out]
type = Exodus
execute_on = 'nonlinear'
[../]
[]
(test/tests/dgkernels/2d_diffusion_dg/2d_diffusion_dg_test.i)
###########################################################
# This is a test of the Discontinuous Galerkin System.
# Discontinous basis functions are used (Monomials) and
# a Laplacian DGKernel contributes to the
# internal edges around each element. Jumps are allowed
# but penalized by this method.
#
# @Requirement F3.60
###########################################################
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
# xmin = -1
# xmax = 1
# ymin = -1
# ymax = 1
xmin = 0
xmax = 1
ymin = 0
ymax = 1
elem_type = QUAD4
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = MONOMIAL
[./InitialCondition]
type = ConstantIC
value = 1
[../]
[../]
[]
[Functions]
active = 'forcing_fn exact_fn'
[./forcing_fn]
type = ParsedFunction
# function = -4.0+(x*x)+(y*y)
# function = x
# function = (x*x)-2.0
value = 2*pow(e,-x-(y*y))*(1-2*y*y)
# function = (x*x*x)-6.0*x
[../]
[./exact_fn]
type = ParsedGradFunction
# function = x
# grad_x = 1
# grad_y = 0
# function = (x*x)+(y*y)
# grad_x = 2*x
# grad_y = 2*y
# function = (x*x)
# grad_x = 2*x
# grad_y = 0
value = pow(e,-x-(y*y))
grad_x = -pow(e,-x-(y*y))
grad_y = -2*y*pow(e,-x-(y*y))
# function = (x*x*x)
# grad_x = 3*x*x
# grad_y = 0
[../]
[]
[Kernels]
active = 'diff abs forcing'
[./diff]
type = Diffusion
variable = u
[../]
[./abs] # u * v
type = Reaction
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[DGKernels]
active = 'dg_diff'
[./dg_diff]
type = DGDiffusion
variable = u
epsilon = -1
sigma = 6
[../]
[]
[BCs]
active = 'all'
[./all]
type = DGFunctionDiffusionDirichletBC
variable = u
boundary = '0 1 2 3'
function = exact_fn
epsilon = -1
sigma = 6
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
# petsc_options = '-snes_mf'
# petsc_options_iname = '-pc_type -pc_hypre_type'
# petsc_options_value = 'hypre boomeramg'
# petsc_options = '-snes_mf'
# max_r_steps = 2
[./Adaptivity]
steps = 2
refine_fraction = 1.0
coarsen_fraction = 0
max_h_level = 8
[../]
nl_rel_tol = 1e-10
# nl_rel_tol = 1e-12
[]
[Postprocessors]
active = 'h dofs l2_err'
[./h]
type = AverageElementSize
[../]
[./dofs]
type = NumDOFs
[../]
[./l2_err]
type = ElementL2Error
variable = u
function = exact_fn
[../]
[]
[Outputs]
file_base = out
exodus = true
csv = true
[]
(test/tests/misc/check_error/function_file_test1.i)
# Test for usage of missing function
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = ic_function
[../]
[../]
[]
[Functions]
[./ic_function]
type = PiecewiseLinear
data_file = piecewise_linear_columns.csv #Will generate error because data is expected in rows
scale_factor = 1.0
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/pins/mms/porosity_change/2d-rc-continuous.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 2
ymin = -1
ymax = 1
nx = 8
ny = 8
[]
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = PINSFVRhieChowInterpolator
u = u
v = v
porosity = porosity
pressure = pressure
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[Variables]
[u]
type = PINSFVSuperficialVelocityVariable
initial_condition = 1
[]
[v]
type = PINSFVSuperficialVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[AuxVariables]
[porosity]
family = MONOMIAL
order = CONSTANT
fv = true
[]
[]
[ICs]
[porosity_continuous]
type = FunctionIC
variable = porosity
function = smooth_jump
[]
[]
[GlobalParams]
porosity = porosity
[]
[FVKernels]
[mass]
type = PINSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[u_advection]
type = PINSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = PINSFVMomentumDiffusion
variable = u
mu = ${mu}
porosity = porosity
momentum_component = 'x'
[]
[u_pressure]
type = PINSFVMomentumPressure
variable = u
pressure = pressure
porosity = porosity
momentum_component = 'x'
[]
[u_forcing]
type = INSFVBodyForce
variable = u
functor = forcing_u
momentum_component = 'x'
[]
[v_advection]
type = PINSFVMomentumAdvection
variable = v
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = PINSFVMomentumDiffusion
variable = v
mu = ${mu}
porosity = porosity
momentum_component = 'y'
[]
[v_pressure]
type = PINSFVMomentumPressure
variable = v
pressure = pressure
porosity = porosity
momentum_component = 'y'
[]
[v_forcing]
type = INSFVBodyForce
variable = v
functor = forcing_v
momentum_component = 'y'
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = 'exact_u'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = 'exact_v'
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = u
function = 'exact_u'
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = v
function = 'exact_v'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 'exact_p'
[]
[]
[Functions]
[smooth_jump]
type = ParsedFunction
value = '1 - 0.5 * 1 / (1 + exp(-30*(x-1))) - 0.01 * y'
[]
# Output from compute-functions-2d.py
[exact_u]
type = ParsedFunction
value = 'sin((1/2)*y*pi)*cos((1/2)*x*pi)'
[]
[forcing_u]
type = ADParsedFunction
value = '15.0*mu*(-1/2*pi*sin((1/2)*x*pi)*sin((1/2)*y*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1)) + 15.0*exp(30 - 30*x)*sin((1/2)*y*pi)*cos((1/2)*x*pi)/((exp(30 - 30*x) + 1)^2*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2))*exp(30 - 30*x)/(exp(30 - 30*x) + 1)^2 + 0.01*mu*((1/2)*pi*cos((1/2)*x*pi)*cos((1/2)*y*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1)) + 0.01*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2) - mu*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))*(-1/4*pi^2*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1)) + 0.01*pi*cos((1/2)*x*pi)*cos((1/2)*y*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2 + 0.0002*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^3) - mu*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))*(-1/4*pi^2*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1)) - 15.0*pi*exp(30 - 30*x)*sin((1/2)*x*pi)*sin((1/2)*y*pi)/((exp(30 - 30*x) + 1)^2*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2) - 450.0*exp(30 - 30*x)*sin((1/2)*y*pi)*cos((1/2)*x*pi)/((exp(30 - 30*x) + 1)^2*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2) + 900.0*exp(60 - 60*x)*sin((1/2)*y*pi)*cos((1/2)*x*pi)/((exp(30 - 30*x) + 1)^3*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2) + 450.0*exp(60 - 60*x)*sin((1/2)*y*pi)*cos((1/2)*x*pi)/((exp(30 - 30*x) + 1)^4*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^3)) - 1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1)) + (1/2)*pi*rho*sin((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)^2/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1)) - pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1)) + 0.01*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2 + 15.0*rho*exp(30 - 30*x)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi)^2/((exp(30 - 30*x) + 1)^2*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2) - 1/4*pi*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))*sin((1/4)*x*pi)*sin((3/2)*y*pi)'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_v]
type = ParsedFunction
value = 'sin((1/4)*x*pi)*cos((1/2)*y*pi)'
[]
[forcing_v]
type = ADParsedFunction
value = '0.01*mu*(-1/2*pi*sin((1/4)*x*pi)*sin((1/2)*y*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1)) + 0.01*sin((1/4)*x*pi)*cos((1/2)*y*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2) + 15.0*mu*((1/4)*pi*cos((1/4)*x*pi)*cos((1/2)*y*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1)) + 15.0*exp(30 - 30*x)*sin((1/4)*x*pi)*cos((1/2)*y*pi)/((exp(30 - 30*x) + 1)^2*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2))*exp(30 - 30*x)/(exp(30 - 30*x) + 1)^2 - mu*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))*(-1/4*pi^2*sin((1/4)*x*pi)*cos((1/2)*y*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1)) - 0.01*pi*sin((1/4)*x*pi)*sin((1/2)*y*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2 + 0.0002*sin((1/4)*x*pi)*cos((1/2)*y*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^3) - mu*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))*(-1/16*pi^2*sin((1/4)*x*pi)*cos((1/2)*y*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1)) - 450.0*exp(30 - 30*x)*sin((1/4)*x*pi)*cos((1/2)*y*pi)/((exp(30 - 30*x) + 1)^2*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2) + 7.5*pi*exp(30 - 30*x)*cos((1/4)*x*pi)*cos((1/2)*y*pi)/((exp(30 - 30*x) + 1)^2*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2) + 900.0*exp(60 - 60*x)*sin((1/4)*x*pi)*cos((1/2)*y*pi)/((exp(30 - 30*x) + 1)^3*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2) + 450.0*exp(60 - 60*x)*sin((1/4)*x*pi)*cos((1/2)*y*pi)/((exp(30 - 30*x) + 1)^4*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^3)) - pi*rho*sin((1/4)*x*pi)^2*sin((1/2)*y*pi)*cos((1/2)*y*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1)) - 1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*y*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1)) + (1/4)*pi*rho*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1)) + 0.01*rho*sin((1/4)*x*pi)^2*cos((1/2)*y*pi)^2/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2 + 15.0*rho*exp(30 - 30*x)*sin((1/4)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)/((exp(30 - 30*x) + 1)^2*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2) + (3/2)*pi*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))*cos((1/4)*x*pi)*cos((3/2)*y*pi)'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_p]
type = ParsedFunction
value = 'sin((3/2)*y*pi)*cos((1/4)*x*pi)'
[]
[forcing_p]
type = ParsedFunction
value = '-1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi) - 1/2*pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2v]
type = ElementL2Error
variable = v
function = exact_v
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2p]
type = ElementL2Error
variable = pressure
function = exact_p
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(test/tests/transfers/multiapp_high_order_variable_transfer/master_L2_Lagrange_conservative.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
[]
[Variables]
[power_density]
family = L2_LAGRANGE
order = FIRST
[]
[]
[Functions]
[pwr_func]
type = ParsedFunction
value = '1e3*x*(1-x)+5e2'
[]
[]
[Kernels]
[diff]
type = Reaction
variable = power_density
[]
[coupledforce]
type = BodyForce
variable = power_density
function = pwr_func
[]
[]
[Postprocessors]
[pwr_avg]
type = ElementAverageValue
block = '0'
variable = power_density
execute_on = 'initial timestep_end'
[]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart '
petsc_options_value = 'hypre boomeramg 100'
nl_abs_tol = 1e-8
nl_rel_tol = 1e-12
[]
[Postprocessors]
[./from_postprocessor]
type = ElementIntegralVariablePostprocessor
variable = power_density
[../]
[]
[MultiApps]
[sub]
type = FullSolveMultiApp
app_type = MooseTestApp
positions = '0 0 0'
input_files = sub_L2_Lagrange_conservative.i
execute_on = 'timestep_end'
[]
[]
[Transfers]
[p_to_sub]
type = MultiAppMeshFunctionTransfer
source_variable = power_density
variable = power_density
to_multi_app = sub
execute_on = 'timestep_end'
from_postprocessors_to_be_preserved = 'from_postprocessor'
to_postprocessors_to_be_preserved = 'pwr_density'
[]
[]
[Outputs]
exodus = true
perf_graph = true
[]
(test/tests/misc/check_error/missing_active_section.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
# Check for missing referenced section
active = 'left right top'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/tag/tag_ad_kernels.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = ADDiffusion
variable = u
extra_matrix_tags = 'mat_tag1 mat_tag2'
extra_vector_tags = 'vec_tag1 vec_tag2'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
extra_matrix_tags = 'mat_tag1 mat_tag2'
extra_vector_tags = 'vec_tag1'
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
extra_matrix_tags = 'mat_tag1 mat_tag2'
extra_vector_tags = 'vec_tag1'
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Problem]
type = TagTestProblem
test_tag_vectors = 'nontime residual vec_tag1 vec_tag2'
test_tag_matrices = 'mat_tag1 mat_tag2'
extra_tag_matrices = 'mat_tag1 mat_tag2'
extra_tag_vectors = 'vec_tag1 vec_tag2'
[]
[Executioner]
type = Steady
solve_type = 'Newton'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
l_tol = 1e-10
nl_rel_tol = 1e-9
nl_max_its = 1
[]
[Outputs]
exodus = true
[]
(test/tests/meshgenerators/sidesets_bounding_box_generator/error_no_nodes_found.i)
[Mesh]
[./gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
#parallel_type = replicated
[]
[./createNewSidesetOne]
type = SideSetsFromBoundingBoxGenerator
input = gmg
boundary_id_old = 'right'
boundary_id_new = 11
bottom_left = '0.5 0.5 0'
top_right = '1.9 1.9 0'
block_id = 0
[]
[./createNewSidesetTwo]
type = SideSetsFromBoundingBoxGenerator
input = createNewSidesetOne
boundary_id_old = 'top right'
boundary_id_new = 10
bottom_left = '-0.1 -0.1 0'
top_right = '0.7 0.3 0'
block_id = 0
boundary_id_overlap = true
[]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./leftBC]
type = DirichletBC
variable = u
boundary = 10
value = 1
[../]
[./rightBC]
type = DirichletBC
variable = u
boundary = 11
value = 0
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/pins/materials/2d-rc.i)
mu=0.01
rho=2000
u_inlet = 1
advected_interp_method='upwind'
velocity_interp_method='rc'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 10
ymin = 0
ymax = 1
nx = 10
ny = 6
[]
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = PINSFVRhieChowInterpolator
u = superficial_vel_x
v = superficial_vel_y
pressure = pressure
porosity = porosity
[]
[]
[Variables]
[superficial_vel_x]
type = PINSFVSuperficialVelocityVariable
initial_condition = ${u_inlet}
[]
[superficial_vel_y]
type = PINSFVSuperficialVelocityVariable
initial_condition = 1e-6
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[AuxVariables]
[porosity]
family = MONOMIAL
order = CONSTANT
fv = true
initial_condition = 0.5
[]
[speed_output]
type = MooseVariableFVReal
[]
[vel_x_output]
type = MooseVariableFVReal
[]
[vel_y_output]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[speed]
type = ADFunctorElementalAux
variable = 'speed_output'
functor = 'speed'
[]
[vel_x]
type = ADFunctorVectorElementalAux
variable = 'vel_x_output'
functor = 'velocity'
component = 0
[]
[vel_y]
type = ADFunctorVectorElementalAux
variable = 'vel_y_output'
functor = 'velocity'
component = 1
[]
[]
[FVKernels]
[mass]
type = PINSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = PINSFVMomentumAdvection
variable = superficial_vel_x
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
porosity = porosity
momentum_component = 'x'
[]
[u_viscosity]
type = PINSFVMomentumDiffusion
variable = superficial_vel_x
mu = ${mu}
porosity = porosity
momentum_component = 'x'
[]
[u_pressure]
type = PINSFVMomentumPressure
variable = superficial_vel_x
momentum_component = 'x'
pressure = pressure
porosity = porosity
[]
[v_advection]
type = PINSFVMomentumAdvection
variable = superficial_vel_y
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
porosity = porosity
momentum_component = 'y'
[]
[v_viscosity]
type = PINSFVMomentumDiffusion
variable = superficial_vel_y
mu = ${mu}
porosity = porosity
momentum_component = 'y'
[]
[v_pressure]
type = PINSFVMomentumPressure
variable = superficial_vel_y
momentum_component = 'y'
pressure = pressure
porosity = porosity
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = superficial_vel_x
function = ${u_inlet}
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = superficial_vel_y
function = 0
[]
[no-slip-u]
type = INSFVNoSlipWallBC
boundary = 'top'
variable = superficial_vel_x
function = 0
[]
[no-slip-v]
type = INSFVNoSlipWallBC
boundary = 'top'
variable = superficial_vel_y
function = 0
[]
[symmetry-u]
type = PINSFVSymmetryVelocityBC
boundary = 'bottom'
variable = superficial_vel_x
u = superficial_vel_x
v = superficial_vel_y
mu = ${mu}
momentum_component = 'x'
[]
[symmetry-v]
type = PINSFVSymmetryVelocityBC
boundary = 'bottom'
variable = superficial_vel_y
u = superficial_vel_x
v = superficial_vel_y
mu = ${mu}
momentum_component = 'y'
[]
[symmetry-p]
type = INSFVSymmetryPressureBC
boundary = 'bottom'
variable = pressure
[]
[outlet-p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 0.1
[]
[]
[Materials]
# Testing this object
[var_mat]
type = PINSFVSpeedFunctorMaterial
superficial_vel_x = 'superficial_vel_x'
superficial_vel_y = 'superficial_vel_y'
porosity = porosity
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
nl_abs_tol = 1e-11
[]
# Some basic Postprocessors to examine the solution
[Postprocessors]
[inlet-p]
type = SideAverageValue
variable = pressure
boundary = 'left'
[]
[outlet-u]
type = SideAverageValue
variable = superficial_vel_x
boundary = 'right'
[]
[]
[Outputs]
exodus = true
csv = false
[]
(modules/heat_conduction/test/tests/heat_conduction/2d_quadrature_gap_heat_transfer/gap_conductivity_property.i)
[Mesh]
file = perfect.e
[]
[Variables]
[./temp]
[../]
[]
[AuxVariables]
[./gap_conductivity]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./hc]
type = HeatConduction
variable = temp
[../]
[]
[AuxKernels]
[./gap_conductivity]
type = MaterialRealAux
boundary = leftright
property = gap_conductivity
variable = gap_conductivity
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = temp
boundary = leftleft
value = 300
[../]
[./right]
type = DirichletBC
variable = temp
boundary = rightright
value = 400
[../]
[]
[ThermalContact]
[./left_to_right]
secondary = leftright
quadrature = true
primary = rightleft
emissivity_primary = 0
emissivity_secondary = 0
variable = temp
type = GapHeatTransfer
gap_conductivity = 3.0
[../]
[]
[Materials]
[./hcm]
type = HeatConductionMaterial
block = 'left right'
specific_heat = 1
thermal_conductivity = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/kernels/hfem/robin.i)
[Mesh]
[square]
type = GeneratedMeshGenerator
nx = 3
ny = 3
dim = 2
[]
build_all_side_lowerd_mesh = true
[]
[Variables]
[u]
order = THIRD
family = MONOMIAL
block = 0
[]
[lambda]
order = CONSTANT
family = MONOMIAL
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
[]
[]
[Kernels]
[diff]
type = MatDiffusion
variable = u
diffusivity = '1'
block = 0
[]
[source]
type = BodyForce
variable = u
value = '1'
block = 0
[]
[]
[DGKernels]
[surface]
type = HFEMDiffusion
variable = u
lowerd_variable = lambda
[]
[]
[BCs]
[all]
type = VacuumBC
boundary = 'left right top bottom'
variable = u
[]
[]
[Postprocessors]
[intu]
type = ElementIntegralVariablePostprocessor
variable = u
block = 0
[]
[lambdanorm]
type = ElementL2Norm
variable = lambda
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu basic mumps'
[]
[Outputs]
[out]
# we hide lambda because it may flip sign due to element
# renumbering with distributed mesh
type = Exodus
hide = lambda
[]
csv = true
[]
(test/tests/mortar/convergence-studies/solution-continuity/continuity.i)
[Mesh]
second_order = true
[./left_block]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
elem_type = QUAD4
[../]
[./left_block_sidesets]
type = RenameBoundaryGenerator
input = left_block
old_boundary_id = '0 1 2 3'
new_boundary_name = 'lb_bottom lb_right lb_top lb_left'
[../]
[./left_block_id]
type = SubdomainIDGenerator
input = left_block_sidesets
subdomain_id = 1
[../]
[./right_block]
type = GeneratedMeshGenerator
dim = 2
xmin = 1
xmax = 2
ymin = 0
ymax = 1
nx = 2
ny = 2
elem_type = QUAD4
[../]
[./right_block_id]
type = SubdomainIDGenerator
input = right_block
subdomain_id = 2
[../]
[right_block_change_boundary_id]
type = RenameBoundaryGenerator
input = right_block_id
old_boundary_id = '0 1 2 3'
new_boundary_id = '100 101 102 103'
[]
[./combined]
type = MeshCollectionGenerator
inputs = 'left_block_id right_block_change_boundary_id'
[../]
[./block_rename]
type = RenameBlockGenerator
input = combined
old_block = '1 2'
new_block = 'left_block right_block'
[../]
[right_right_sideset]
type = SideSetsAroundSubdomainGenerator
input = block_rename
new_boundary = rb_right
block = right_block
normal = '1 0 0'
[]
[right_left_sideset]
type = SideSetsAroundSubdomainGenerator
input = right_right_sideset
new_boundary = rb_left
block = right_block
normal = '-1 0 0'
[]
[right_top_sideset]
type = SideSetsAroundSubdomainGenerator
input = right_left_sideset
new_boundary = rb_top
block = right_block
normal = '0 1 0'
[]
[right_bottom_sideset]
type = SideSetsAroundSubdomainGenerator
input = right_top_sideset
new_boundary = rb_bottom
block = right_block
normal = '0 -1 0'
[]
[secondary]
input = right_bottom_sideset
type = LowerDBlockFromSidesetGenerator
sidesets = 'lb_right'
new_block_id = '10001'
new_block_name = 'secondary_lower'
[]
[primary]
input = secondary
type = LowerDBlockFromSidesetGenerator
sidesets = 'rb_left'
new_block_id = '10000'
new_block_name = 'primary_lower'
[]
[]
[Variables]
[./T]
block = 'left_block right_block'
order = SECOND
[../]
[./lambda]
block = 'secondary_lower'
[../]
[]
[BCs]
[./neumann]
type = FunctionGradientNeumannBC
exact_solution = exact_soln_primal
variable = T
boundary = 'lb_bottom lb_top lb_left rb_bottom rb_right rb_top'
[../]
[]
[Kernels]
[./conduction]
type = Diffusion
variable = T
block = 'left_block right_block'
[../]
[./sink]
type = Reaction
variable = T
block = 'left_block right_block'
[../]
[./forcing_function]
type = BodyForce
variable = T
function = forcing_function
block = 'left_block right_block'
[../]
[]
[Functions]
[./forcing_function]
type = ParsedFunction
value = ''
[../]
[./exact_soln_primal]
type = ParsedFunction
value = ''
[../]
[exact_soln_lambda]
type = ParsedFunction
value = ''
[]
[]
[Debug]
show_var_residual_norms = 1
[]
[Constraints]
[./mortar]
type = EqualValueConstraint
primary_boundary = rb_left
secondary_boundary = lb_right
primary_subdomain = primary_lower
secondary_subdomain = secondary_lower
secondary_variable = T
variable = lambda
delta = 0.4
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
solve_type = NEWTON
type = Steady
petsc_options = '-snes_converged_reason -ksp_converged_reason'
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu basic mumps'
[]
[Outputs]
exodus = true
csv = true
[dofmap]
type = DOFMap
execute_on = 'initial'
[]
[]
[Postprocessors]
[L2lambda]
type = ElementL2Error
variable = lambda
function = exact_soln_lambda
execute_on = 'timestep_end'
block = 'secondary_lower'
[]
[L2u]
type = ElementL2Error
variable = T
function = exact_soln_primal
execute_on = 'timestep_end'
block = 'left_block right_block'
[]
[h]
type = AverageElementSize
block = 'left_block right_block'
[]
[]
(test/tests/auxkernels/linear_combination/test.i)
# All tested logic is in the aux system
# The non-linear problem is unrelated
[Mesh]
type = GeneratedMesh
dim = 1
xmin = -1
xmax = 1
nx = 10
[]
[Functions]
[./v1_func]
type = ParsedFunction
value = (1-x)/2
[../]
[./v2_func]
type = ParsedFunction
value = (1+x)/2
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./lc]
[../]
[./v1]
[../]
[./v2]
[../]
[./w1]
[../]
[./w2]
[../]
[]
[ICs]
[./v1_ic]
type = FunctionIC
variable = v1
function = v1_func
[../]
[./v2_ic]
type = FunctionIC
variable = v2
function = v2_func
[../]
[./w1_ic]
type = ConstantIC
variable = w1
value = 0.3
[../]
[./w2_ic]
type = ConstantIC
variable = w2
value = 0.5
[../]
[]
[AuxKernels]
[./lc-aux]
type = ParsedAux
variable = lc
function = 'v1*w1+v2*w2'
args = 'v1 w1 v2 w2'
execute_on = 'timestep_end'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 2
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
[./out]
type = Exodus
[../]
[]
(test/tests/tag/2d_diffusion_tag_vector.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./tag_variable1]
order = FIRST
family = LAGRANGE
[../]
[./tag_variable2]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
extra_vector_tags = 'vec_tag1 vec_tag2'
[../]
[]
[AuxKernels]
[./TagVectorAux1]
type = TagVectorAux
variable = tag_variable1
v = u
vector_tag = vec_tag1
[../]
[./TagVectorAux2]
type = TagVectorAux
variable = tag_variable2
v = u
vector_tag = vec_tag2
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
preset = false
extra_vector_tags = vec_tag1
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
preset = false
extra_vector_tags = vec_tag2
[../]
[]
[Problem]
type = FEProblem
extra_tag_vectors = 'vec_tag1 vec_tag2'
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
file_base = tag_vector_out
exodus = true
[]
(test/tests/misc/check_error/coupled_grad_without_declare.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 10
ny = 10
elem_type = QUAD9
[]
[Functions]
[./forcing_fnu]
type = ParsedFunction
value = -5.8*(x+y)+x*x*x-x+y*y*y-y
[../]
[./forcing_fnv]
type = ParsedFunction
value = -4
[../]
[./slnu]
type = ParsedGradFunction
value = x*x*x-x+y*y*y-y
grad_x = 3*x*x-1
grad_y = 3*y*y-1
[../]
[./slnv]
type = ParsedGradFunction
value = x*x+y*y
grad_x = 2*x
grad_y = 2*y
[../]
#NeumannBC functions
[./bc_fnut]
type = ParsedFunction
value = 3*y*y-1
[../]
[./bc_fnub]
type = ParsedFunction
value = -3*y*y+1
[../]
[./bc_fnul]
type = ParsedFunction
value = -3*x*x+1
[../]
[./bc_fnur]
type = ParsedFunction
value = 3*x*x-1
[../]
[]
[Variables]
[./u]
order = THIRD
family = HIERARCHIC
[../]
[./v]
order = SECOND
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff1 diff2 test1 forceu forcev react'
[./diff1]
type = Diffusion
variable = u
[../]
[./test1]
type = CoupledConvection
variable = u
velocity_vector = v
# Trigger the error in this class
test_coupling_declaration_error = true
[../]
[./diff2]
type = Diffusion
variable = v
[../]
[./react]
type = Reaction
variable = u
[../]
[./forceu]
type = BodyForce
variable = u
function = forcing_fnu
[../]
[./forcev]
type = BodyForce
variable = v
function = forcing_fnv
[../]
[]
[BCs]
active = 'bc_u_tb bc_v bc_ul bc_ur bc_ut bc_ub'
[./bc_u]
type = FunctionPenaltyDirichletBC
variable = u
function = slnu
boundary = 'left right top bottom'
penalty = 1e6
[../]
[./bc_v]
type = FunctionDirichletBC
variable = v
function = slnv
boundary = 'left right top bottom'
[../]
[./bc_u_lr]
type = FunctionPenaltyDirichletBC
variable = u
function = slnu
boundary = 'left right top bottom'
penalty = 1e6
[../]
[./bc_u_tb]
type = CoupledKernelGradBC
variable = u
var2 = v
vel = '0.1 0.1'
boundary = 'top bottom left right'
[../]
[./bc_ul]
type = FunctionNeumannBC
variable = u
function = bc_fnul
boundary = 'left'
[../]
[./bc_ur]
type = FunctionNeumannBC
variable = u
function = bc_fnur
boundary = 'right'
[../]
[./bc_ut]
type = FunctionNeumannBC
variable = u
function = bc_fnut
boundary = 'top'
[../]
[./bc_ub]
type = FunctionNeumannBC
variable = u
function = bc_fnub
boundary = 'bottom'
[../]
[]
[Preconditioning]
active = ' '
[./prec]
type = SMP
full = true
[../]
[]
[Postprocessors]
active='L2u L2v'
[./dofs]
type = NumDOFs
[../]
[./h]
type = AverageElementSize
[../]
[./L2u]
type = ElementL2Error
variable = u
function = slnu
[../]
[./L2v]
type = ElementL2Error
variable = v
function = slnv
[../]
[./H1error]
type = ElementH1Error
variable = u
function = solution
[../]
[./H1Semierror]
type = ElementH1SemiError
variable = u
function = solution
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
# petsc_options = '-snes'
nl_rel_tol = 1e-15
nl_abs_tol = 1e-13
[]
[Outputs]
execute_on = 'timestep_end'
[]
[Debug]
show_var_residual_norms = true
[]
(test/tests/fvbcs/fv_pp_dirichlet/fv_pp_dirichlet.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 2
[]
[Variables]
[u]
family = MONOMIAL
order = CONSTANT
fv = true
[]
[]
[FVKernels]
[diff]
type = FVDiffusion
variable = u
coeff = 1
[]
[]
[FVBCs]
[left]
type = FVPostprocessorDirichletBC
variable = u
boundary = left
postprocessor = bc_val
[]
[right]
type = FVDirichletBC
variable = u
boundary = right
value = 0
[]
[]
[Postprocessors]
[bc_val]
type = Receiver
default = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'Newton'
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_mortar/modular_gap_heat_transfer_mortar.i)
[Mesh]
[file]
type = FileMeshGenerator
file = 2blk-gap.e
[]
[secondary]
type = LowerDBlockFromSidesetGenerator
sidesets = '101'
new_block_id = '10001'
new_block_name = 'secondary_lower'
input = file
[]
[primary]
type = LowerDBlockFromSidesetGenerator
sidesets = '100'
new_block_id = '10000'
new_block_name = 'primary_lower'
input = secondary
[]
[]
[Problem]
kernel_coverage_check = false
material_coverage_check = false
[]
[Variables]
[temp]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[lm]
order = FIRST
family = LAGRANGE
block = 'secondary_lower'
[]
[]
[Materials]
[left]
type = HeatConductionMaterial
block = 1
thermal_conductivity = 1000
specific_heat = 1
[]
[right]
type = HeatConductionMaterial
block = 2
thermal_conductivity = 500
specific_heat = 1
[]
[]
[Kernels]
[hc]
type = HeatConduction
variable = temp
use_displaced_mesh = false
block = '1 2'
[]
[]
[UserObjects]
[simple]
type = GapFluxModelSimple
k = 100
temperature = temp
boundary = 100
[]
[]
[Constraints]
[ced]
type = ModularGapConductanceConstraint
variable = lm
secondary_variable = temp
primary_boundary = 100
primary_subdomain = 10000
secondary_boundary = 101
secondary_subdomain = 10001
gap_flux_models = simple
[]
[]
[BCs]
[left]
type = DirichletBC
variable = temp
boundary = 'left'
value = 1
[]
[right]
type = DirichletBC
variable = temp
boundary = 'right'
value = 0
[]
[]
[Preconditioning]
[fmp]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
nl_rel_tol = 1e-11
[]
[Outputs]
exodus = true
[]
(test/tests/restrictable/block_api_test/block_restrictable.i)
[Mesh]
type = FileMesh
file = rectangle.e
dim = 2
[]
[Variables]
[./u]
block = '1 2'
[../]
[]
[Kernels]
[./diff]
type = BlkResTestDiffusion
variable = u
block = '1 2'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Materials]
[./mat0]
type = GenericConstantMaterial
block = '1'
prop_names = 'a b'
prop_values = '1 2'
[../]
[./mat1]
type = GenericConstantMaterial
block = '2'
prop_names = 'a'
prop_values = '10'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/userobjects/side_user_object_no_boundary_error/side_no_boundary.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Postprocessors]
[./avg]
type = SideAverageValue
variable = u
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/mortar/continuity-2d-non-conforming/dual-soln-continuity-vcp.i)
[Mesh]
second_order = false
[file]
type = FileMeshGenerator
file = nodal_normals_test_offset_nonmatching_gap.e
[]
[primary]
input = file
type = LowerDBlockFromSidesetGenerator
sidesets = '2'
new_block_id = '20'
[]
[secondary]
input = primary
type = LowerDBlockFromSidesetGenerator
sidesets = '1'
new_block_id = '10'
[]
[]
[Problem]
kernel_coverage_check = false
[]
[Variables]
[T]
block = '1 2'
order = FIRST
[]
[lambda]
block = '10'
order = FIRST
use_dual = true
[]
[]
[BCs]
[neumann]
type = FunctionGradientNeumannBC
exact_solution = exact_soln
variable = T
boundary = '3 4 5 6 7 8'
[]
[]
[Kernels]
[conduction]
type = Diffusion
variable = T
block = '1 2'
[]
[sink]
type = Reaction
variable = T
block = '1 2'
[]
[forcing_function]
type = BodyForce
variable = T
function = forcing_function
block = '1 2'
[]
[]
[Functions]
[forcing_function]
type = ParsedFunction
value = '-4 + x^2 + y^2'
[]
[exact_soln]
type = ParsedFunction
value = 'x^2 + y^2'
[]
[]
[Debug]
show_var_residual_norms = 1
[]
[Constraints]
[mortar]
type = EqualValueConstraint
primary_boundary = 2
secondary_boundary = 1
primary_subdomain = 20
secondary_subdomain = 10
variable = lambda
secondary_variable = T
[]
[]
[Preconditioning]
[vcp]
type = VCP
full = true
lm_variable = 'lambda'
primary_variable = 'T'
preconditioner = 'AMG'
is_lm_coupling_diagonal = true
[]
[]
[Executioner]
solve_type = NEWTON
type = Steady
petsc_options_iname = ' -pc_factor_shift_type -pc_factor_shift_amount'
petsc_options_value = ' NONZERO 1e-15'
[]
[Outputs]
file_base = 'dual-soln-continuity_out'
exodus = true
[]
(test/tests/ics/hermite_ic/hermite_ic.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
order = THIRD
family = HERMITE
[../]
[]
[Functions]
[./afunc]
type = ParsedFunction
value = x^2
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
[ICs]
[./func_ic]
function = afunc
variable = u
type = FunctionIC
[../]
[]
(test/tests/auxkernels/solution_aux/thread_xda.i)
[Mesh]
# This test uses SolutionUserObject which doesn't work with ParallelMesh.
type = GeneratedMesh
parallel_type = REPLICATED
dim = 2
nx = 2
ny = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
[./u_xda_func]
type = SolutionFunction
solution = xda_u
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 2
[../]
[]
[UserObjects]
[./xda_u]
type = SolutionUserObject
system = nl0
mesh = aux_nonlinear_solution_out_0001_mesh.xda
es = aux_nonlinear_solution_out_0001.xda
system_variables = u
execute_on = initial
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
nl_rel_tol = 1e-10
[]
[Postprocessors]
[./unorm]
type = ElementL2Norm
variable = u
[../]
[./uerror]
type = ElementL2Error
variable = u
function = u_xda_func
[../]
[]
[Outputs]
csv = true
[]
(test/tests/materials/ad_material/ad_global_index_mapping.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
second_order = true
[]
[Variables]
[u]
initial_condition = 1
[]
[v]
initial_condition = 1
order = SECOND
[]
[]
[Kernels]
[u_diff]
type = ADMatDiffusion
variable = u
diffusivity = diffusivity
[]
[v_diff]
type = ADMatDiffusion
variable = v
diffusivity = diffusivity
[]
[]
[BCs]
[left_u]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right_u]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[left_v]
type = DirichletBC
variable = v
boundary = left
value = 1
[]
[right_v]
type = DirichletBC
variable = v
boundary = right
value = 0
[]
[]
[Materials]
[ad_coupled_mat]
type = ADCheckGlobalToDerivativeMap
u = u
v = v
mat_prop = diffusivity
[]
[]
[Executioner]
type = Steady
solve_type = 'Newton'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/check_syntax_error.i)
[Mesh]
file = 2-lines.e
construct_side_list_from_node_list = true
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
block = '1 2'
[../]
[./lm]
order = FIRST
family = SCALAR
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[ScalarKernels]
[./ced]
type = NodalEqualValueConstraint
variable = lm
var = u
boundary = '100 101 1'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = '1'
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = '2'
value = 3
[../]
[./evc1]
type = OneDEqualValueConstraintBC
variable = u
boundary = '100'
lambda = lm
component = 0
vg = 1
[../]
[./evc2]
type = OneDEqualValueConstraintBC
variable = u
boundary = '101'
lambda = lm
component = 0
vg = -1
[../]
[]
[Preconditioning]
[./fmp]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
execute_on = 'timestep_end'
[]
(test/tests/outputs/exodus/hide_variables.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[AuxVariables]
[./aux0]
order = SECOND
family = SCALAR
[../]
[./aux1]
family = SCALAR
initial_condition = 5
[../]
[./aux2]
family = SCALAR
initial_condition = 10
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./diff_v]
type = CoefDiffusion
variable = v
coef = 2
[../]
[]
[BCs]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[./left_u]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = right
value = 3
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = left
value = 2
[../]
[]
[Postprocessors]
[./num_vars]
type = NumVars
system = 'NL'
[../]
[./num_aux]
type = NumVars
system = 'AUX'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
[./out]
type = Exodus
hide = 'aux2 v num_aux'
[../]
[]
[ICs]
[./aux0_IC]
variable = aux0
values = '12 13'
type = ScalarComponentIC
[../]
[]
(test/tests/userobjects/mat_prop_user_object/mat_prop_user_object.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./uo_e]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./uo_reporter]
type = MatPropUserObjectAux
variable = uo_e
material_user_object = uo
execute_on = timestep_end
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 'left'
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = 'right'
value = 2
[../]
[]
[Materials]
[./material]
block = 0
type = GenericConstantMaterial
prop_names = 'e'
prop_values = 2.718281828459
[../]
[]
[UserObjects]
[./uo]
type = MaterialPropertyUserObject
mat_prop = 'e'
execute_on = timestep_end
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = uo_material
exodus = true
[]
(tutorials/tutorial01_app_development/step10_auxkernels/problems/pressure_diffusion.i)
[Mesh]
type = GeneratedMesh # Can generate simple lines, rectangles and rectangular prisms
dim = 2 # Dimension of the mesh
nx = 100 # Number of elements in the x direction
ny = 10 # Number of elements in the y direction
xmax = 0.304 # Length of test chamber
ymax = 0.0257 # Test chamber radius
[]
[Problem]
type = FEProblem # This is the "normal" type of Finite Element Problem in MOOSE
coord_type = RZ # Axisymmetric RZ
rz_coord_axis = X # Which axis the symmetry is around
[]
[Variables]
[pressure]
# Adds a Linear Lagrange variable by default
[]
[]
[AuxVariables]
[velocity]
order = CONSTANT # Since "pressure" is approximated linearly, its gradient must be constant
family = MONOMIAL_VEC # A monomial interpolation means this is an elemental AuxVariable
[]
[]
[Kernels]
[diffusion]
type = DarcyPressure # Zero-gravity, divergence-free form of Darcy's law
variable = pressure # Operate on the "pressure" variable from above
[]
[]
[AuxKernels]
[velocity]
type = DarcyVelocity
variable = velocity # Store volumetric flux vector in "velocity" variable from above
pressure = pressure # Couple to the "pressure" variable from above
execute_on = TIMESTEP_END # Perform calculation at the end of the solve step - after Kernels run
[]
[]
[Materials]
[filter]
type = PackedColumn # Provides permeability and viscosity of water through packed 1mm spheres
[]
[]
[BCs]
[inlet]
type = ADDirichletBC # Simple u=value BC
variable = pressure # Variable to be set
boundary = left # Name of a sideset in the mesh
value = 4000 # (Pa) From Figure 2 from paper. First data point for 1mm spheres.
[]
[outlet]
type = ADDirichletBC
variable = pressure
boundary = right
value = 0 # (Pa) Gives the correct pressure drop from Figure 2 for 1mm spheres
[]
[]
[Executioner]
type = Steady # Steady state problem
solve_type = NEWTON # Perform a Newton solve
# Set PETSc parameters to optimize solver efficiency
petsc_options_iname = '-pc_type -pc_hypre_type' # PETSc option pairs with values below
petsc_options_value = ' hypre boomeramg'
[]
[Outputs]
exodus = true # Output Exodus format
[]
(test/tests/userobjects/layered_average/layered_average_interpolate.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./layered_average]
order = CONSTANT
family = MONOMIAL
[../]
[./nodal_layered_average]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./layered_average]
type = SpatialUserObjectAux
variable = layered_average
execute_on = timestep_end
user_object = average
[../]
[./nodal_layered_average]
type = SpatialUserObjectAux
variable = nodal_layered_average
execute_on = timestep_end
user_object = average
[../]
[]
[BCs]
[./top]
type = DirichletBC
variable = u
boundary = top
value = 1
[../]
[./bottom]
type = DirichletBC
variable = u
boundary = bottom
value = 0
[../]
[]
[UserObjects]
[./average]
type = LayeredAverage
variable = u
direction = y
num_layers = 19
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(tutorials/darcy_thermo_mech/step04_velocity_aux/tests/auxkernels/velocity_aux/velocity_aux.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
[pressure]
[]
[]
[AuxVariables]
[velocity]
order = CONSTANT
family = MONOMIAL_VEC
[]
[]
[AuxKernels]
[velocity]
type = DarcyVelocity
variable = velocity
execute_on = timestep_end
pressure = pressure
[]
[]
[Functions]
[pressure_ic_func]
type = ParsedFunction
value = 2000*x*y*x*y
[]
[]
[ICs]
[pressure_ic]
type = FunctionIC
variable = pressure
function = pressure_ic_func
[]
[]
[Problem]
type = FEProblem
coord_type = RZ
rz_coord_axis = X
solve = false
[]
[Materials]
[pressure]
type = ADGenericConstantMaterial
prop_values = '0.8451e-9 7.98e-4'
prop_names = 'permeability viscosity'
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/userobjects/nearest_point_layered_average/points_from_uo.i)
[Mesh]
type = GeneratedMesh
dim = 3
xmax = 1.5
ymax = 1.5
zmax = 1.2
nx = 10
ny = 10
nz = 10
[]
[Variables]
[u]
[]
[]
[AuxVariables]
[np_layered_average]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[AuxKernels]
[np_layered_average]
type = SpatialUserObjectAux
variable = np_layered_average
execute_on = timestep_end
user_object = npla
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[one]
type = DirichletBC
variable = u
boundary = 'right back top'
value = 1
[]
[]
[UserObjects]
[npla]
type = NearestPointLayeredAverage
direction = y
num_layers = 3
variable = u
points = '0.375 0.0 0.3
1.125 0.0 0.3
0.375 0.0 0.9
1.125 0.0 0.9'
[]
[]
[VectorPostprocessors]
# getting the points from the user object itself is here exactly equivalent to the points
# provided in the 'spatial_manually_provided' vector postprocessor
[spatial_from_uo]
type = SpatialUserObjectVectorPostprocessor
userobject = npla
[]
[spatial_manually_provided]
type = SpatialUserObjectVectorPostprocessor
userobject = npla
points = '0.375 0.25 0.3
0.375 0.75 0.3
0.375 1.25 0.3
1.125 0.25 0.3
1.125 0.75 0.3
1.125 1.25 0.3
0.375 0.25 0.9
0.375 0.75 0.9
0.375 1.25 0.9
1.125 0.25 0.9
1.125 0.75 0.9
1.125 1.25 0.9'
[]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
csv = true
execute_on = 'final'
[]
(test/tests/userobjects/layered_side_integral/layered_side_integral.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 6
ny = 6
nz = 6
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./layered_integral]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = u
boundary = bottom
value = 0
[../]
[./top]
type = DirichletBC
variable = u
boundary = top
value = 1
[../]
[]
[AuxKernels]
[./liaux]
type = SpatialUserObjectAux
variable = layered_integral
boundary = right
user_object = layered_integral
[../]
[]
[UserObjects]
[./layered_integral]
type = LayeredSideIntegral
direction = y
num_layers = 3
variable = u
execute_on = linear
boundary = right
[../]
[]
[VectorPostprocessors]
[int]
type = SpatialUserObjectVectorPostprocessor
userobject = layered_integral
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
csv = true
[]
(test/tests/auxkernels/extra_element_id_aux/extra_element_integer_aux.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
xmax = 1
ymax = 1
extra_element_integers = test_id
[]
[subdomains]
type = SubdomainBoundingBoxGenerator
input = gmg
bottom_left = '0.1 0.1 0'
block_id = 1
top_right = '0.9 0.9 0'
integer_name = test_id
[]
[another_subdomains]
type = SubdomainBoundingBoxGenerator
input = subdomains
bottom_left = '0.9 0.9 0'
block_id = 2
top_right = '1 1 0'
integer_name = test_id
[]
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[AuxVariables]
[test_id]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[test_id]
type = ExtraElementIDAux
variable = test_id
extra_id_name = test_id
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/heat_conduction_patch/heat_conduction_patch.i)
#
# This problem is taken from the Abaqus verification manual:
# "1.5.8 Patch test for heat transfer elements"
#
# The temperature on the exterior nodes is 200x+100y+200z.
#
# This gives a constant flux at all Gauss points.
#
# In addition, the temperature at all nodes follows the same formula.
#
# Node x y z Temperature
# 1 1.00E+00 0.00E+00 1.00E+00 400
# 2 6.77E-01 3.05E-01 6.83E-01 302.5
# 3 3.20E-01 1.86E-01 6.43E-01 211.2
# 4 0.00E+00 0.00E+00 1.00E+00 200
# 5 1.00E+00 1.00E+00 1.00E+00 500
# 6 7.88E-01 6.93E-01 6.44E-01 355.7
# 7 1.65E-01 7.45E-01 7.02E-01 247.9
# 8 0.00E+00 1.00E+00 1.00E+00 300
# 9 1.00E+00 0.00E+00 0.00E+00 200
# 10 0.00E+00 0.00E+00 0.00E+00 0
# 11 8.26E-01 2.88E-01 2.88E-01 251.6
# 12 2.49E-01 3.42E-01 1.92E-01 122.4
# 13 2.73E-01 7.50E-01 2.30E-01 175.6
# 14 0.00E+00 1.00E+00 0.00E+00 100
# 15 8.50E-01 6.49E-01 2.63E-01 287.5
# 16 1.00E+00 1.00E+00 0.00E+00 300
[Mesh]#Comment
file = heat_conduction_patch.e
[] # Mesh
[Functions]
[./temps]
type = ParsedFunction
value='200*x+100*y+200*z'
[../]
[] # Functions
[Variables]
[./temp]
order = FIRST
family = LAGRANGE
[../]
[] # Variables
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[] # Kernels
[BCs]
[./temps]
type = FunctionDirichletBC
variable = temp
boundary = 10
function = temps
[../]
[] # BCs
[Materials]
[./heat]
type = HeatConductionMaterial
block = 1
specific_heat = 0.116
thermal_conductivity = 4.85e-4
[../]
[] # Materials
[Executioner]
type = Steady
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -ksp_gmres_restart'
petsc_options_value = 'lu 101'
line_search = 'none'
nl_abs_tol = 1e-11
nl_rel_tol = 1e-10
l_max_its = 20
[] # Executioner
[Outputs]
exodus = true
[] # Output
(test/tests/vectorpostprocessors/vector_of_postprocessors/vector_of_postprocessors.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Postprocessors]
[./max]
type = ElementExtremeValue
variable = u
[../]
[./min]
type = ElementExtremeValue
variable = u
value_type = min
[../]
[]
[VectorPostprocessors]
[./min_max]
type = VectorOfPostprocessors
postprocessors = 'min max'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = false
csv = true
[]
(test/tests/materials/material/mat_cyclic_coupling.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 10
ny = 10
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = MatDiffusionTest
variable = u
prop_name = some_prop
[../]
[./conv]
type = MatConvection
variable = u
x = 1
y = 0
mat_prop = some_other_prop
[../]
[]
[BCs]
[./right]
type = NeumannBC
variable = u
boundary = 1
value = 1
[../]
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[]
[Materials]
# order is switched intentionally, so we won't get lucky and dep-resolver has to do its job
[./mat2]
type = CoupledMaterial
block = 0
mat_prop = 'some_prop'
coupled_mat_prop = 'some_other_prop'
[../]
[./mat1]
type = CoupledMaterial
block = 0
mat_prop = 'some_other_prop'
coupled_mat_prop = 'some_prop'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out_coupled
exodus = true
[]
(test/tests/materials/material/coupled_material_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 10
ny = 10
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = MatDiffusionTest
variable = u
prop_name = mp1
[../]
[./conv]
type = MatConvection
variable = u
x = 1
y = 0
mat_prop = some_prop
[../]
[]
[BCs]
[./right]
type = NeumannBC
variable = u
boundary = 1
value = 1
[../]
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[]
[Materials]
# order is switched intentionally, so we won't get luck and dep-resolver has to do its job
[./mat2]
type = CoupledMaterial
block = 0
mat_prop = 'some_prop'
coupled_mat_prop = 'mp1'
[../]
[./mat1]
type = GenericConstantMaterial
block = 0
prop_names = 'mp1'
prop_values = '2'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out_coupled
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/energy_source/steady-action.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
nx = 16
ny = 16
[]
[]
[Modules]
[IncompressibleNavierStokes]
equation_type = steady-state
velocity_boundary = 'bottom right top left'
velocity_function = '0 0 0 0 lid_function 0 0 0'
initial_velocity = '1e-15 1e-15 0'
add_standard_velocity_variables_for_ad = false
pressure_pinned_node = 0
density_name = rho
dynamic_viscosity_name = mu
use_ad = true
laplace = true
family = LAGRANGE
order = FIRST
add_temperature_equation = true
fixed_temperature_boundary = 'bottom top'
temperature_function = '1 0'
has_heat_source = true
heat_source_function = 1
supg = true
pspg = true
[]
[]
[Materials]
[const]
type = ADGenericConstantMaterial
prop_names = 'rho mu cp k'
prop_values = '1 1 1 .01'
[]
[]
[Functions]
[lid_function]
# We pick a function that is exactly represented in the velocity
# space so that the Dirichlet conditions are the same regardless
# of the mesh spacing.
type = ParsedFunction
value = '4*x*(1-x)'
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_levels -ksp_gmres_restart'
petsc_options_value = 'asm 6 200'
line_search = 'none'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
exodus = true
[]
(modules/combined/test/tests/linear_elasticity/thermal_expansion.i)
# This input file is designed to test the RankTwoAux and RankFourAux
# auxkernels, which report values out of the Tensors used in materials
# properties.
# Materials properties into AuxVariables - these are elemental variables, not nodal variables.
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
nz = 0
xmin = 0
xmax = 2
ymin = 0
ymax = 2
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Modules/TensorMechanics/Master/All]
strain = SMALL
eigenstrain_names = eigenstrain
add_variables = true
generate_output = 'stress_xx stress_yy stress_xy'
[]
[Materials]
[./elasticity_tensor]
type = ComputeElasticityTensor
fill_method = symmetric9
C_ijkl = '1e6 0 0 1e6 0 1e6 .5e6 .5e6 .5e6'
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[./eigenstrain]
type = ComputeEigenstrain
eigen_base = '1e-4'
eigenstrain_name = eigenstrain
[../]
[]
[BCs]
[./bottom_y]
type = DirichletBC
variable = disp_y
boundary = 'bottom'
value = 0
[../]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = 'left'
value = 0
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
nl_rel_tol = 1e-14
[]
[Outputs]
exodus = true
[]
(test/tests/materials/ad_piecewise_linear_interpolation_material/piecewise_linear_interpolation_material.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 3
ny = 3
nz = 0
elem_type = QUAD4
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff1]
type = ADDiffusion
variable = u
[../]
[]
[BCs]
[./left_u]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Materials]
[./m1]
type = ADPiecewiseLinearInterpolationMaterial
property = m1
variable = u
xy_data = '0 0
1 1'
block = 0
outputs = all
[../]
[./m2]
type = ADPiecewiseLinearInterpolationMaterial
property = m2
variable = u
x = '0 1'
y = '0 1'
block = 0
outputs = all
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/postprocessor/output_pps_hidden_shown_check.i)
# Computing two postprocessors and specifying one of them both in the
# show list and the hide list, which should throw an error message.
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 10
ny = 10
elem_type = QUAD4
# This test uses ElementalVariableValue postprocessors on specific
# elements, so element numbering needs to stay unchanged
allow_renumbering = false
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./lr_u]
type = DirichletBC
variable = u
boundary = '1 3'
value = 1
[../]
[]
[Postprocessors]
[./elem_56]
type = ElementalVariableValue
variable = u
elementid = 56
[../]
[./elem_12]
type = ElementalVariableValue
variable = u
elementid = 12
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
[./console]
type = Console
show = 'elem_56'
hide = 'elem_56'
[../]
[]
(modules/navier_stokes/test/tests/finite_element/ins/bcs/advection_bc/advection_bc.i)
[Mesh]
type = GeneratedMesh
dim = 1
xmin = 0
xmax = 10.0
nx = 100
[]
[Variables]
[./phi]
[../]
[]
[AuxVariables]
[./vx]
[../]
[./force]
[../]
[]
[ICs]
[./vx]
type = FunctionIC
variable = vx
function = vx_function
[../]
[./force]
type = FunctionIC
variable = force
function = forcing
[../]
[]
[Kernels]
[./advection]
type = MassConvectiveFlux
variable = phi
vel_x = vx
[../]
[./rhs]
type = CoupledForce
variable = phi
v = force
[../]
[]
[BCs]
[./inflow_enthalpy]
type = DirichletBC
variable = phi
boundary = 'left'
value = 1
[../]
[./outflow_term]
type = AdvectionBC
variable = phi
velocity_vector = 'vx'
boundary = 'right'
[../]
[]
[Functions]
[./vx_function]
type = ParsedFunction
value = '1 + x * x'
[../]
[./forcing]
type = ParsedFunction
value = 'x'
[../]
[./analytical]
type = ParsedFunction
value = '(1 + 0.5 * x * x) / (1 + x * x)'
[../]
[]
[Postprocessors]
[./error]
type = ElementL2Error
variable = phi
function = analytical
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
perf_graph = true
[]
(test/tests/geomsearch/quadrature_penetration_locator/quadrature_penetration_locator.i)
[Mesh]
file = 2dcontact_collide.e
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./penetration]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 2
paired_boundary = 3
[../]
[]
[BCs]
[./block1_left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./block1_right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[./block2_left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./block2_right]
type = DirichletBC
variable = u
boundary = 4
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/bcs/advection_bc/2d_advection_bc.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 10.0
ymax = 10
nx = 10
ny = 10
[]
[Variables]
[./phi]
[../]
[]
[AuxVariables]
[./vx]
[../]
[./force]
[../]
[]
[ICs]
[./vx]
type = FunctionIC
variable = vx
function = vx_function
[../]
[./force]
type = FunctionIC
variable = force
function = forcing
[../]
[]
[Kernels]
[./advection]
type = MassConvectiveFlux
variable = phi
vel_x = vx
[../]
[./rhs]
type = CoupledForce
variable = phi
v = force
[../]
[]
[BCs]
[./inflow_enthalpy]
type = DirichletBC
variable = phi
boundary = 'left'
value = 1
[../]
[./outflow_term]
type = AdvectionBC
variable = phi
velocity_vector = 'vx'
boundary = 'right'
[../]
[]
[Functions]
[./vx_function]
type = ParsedFunction
value = '1 + x * x'
[../]
[./forcing]
type = ParsedFunction
value = 'x'
[../]
[./analytical]
type = ParsedFunction
value = '(1 + 0.5 * x * x) / (1 + x * x)'
[../]
[]
[Postprocessors]
[./error]
type = ElementL2Error
variable = phi
function = analytical
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
perf_graph = true
[]
(test/tests/vectorpostprocessors/point_value_sampler/point_value_sampler.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = left
value = 1
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = right
value = 0
[../]
[]
[VectorPostprocessors]
[./point_sample]
type = PointValueSampler
variable = 'u v'
points = '0.1 0.1 0 0.23 0.4 0 0.78 0.2 0'
sort_by = x
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
csv = true
[]
(modules/heat_conduction/test/tests/sideset_heat_transfer/gap_thermal_1D.i)
[Mesh]
[mesh]
type = GeneratedMeshGenerator
dim = 1
nx = 2
xmax = 2
[]
[split]
type = SubdomainBoundingBoxGenerator
input = mesh
block_id = 1
bottom_left = '1 0 0'
top_right = '2 0 0'
[]
[interface]
type = SideSetsBetweenSubdomainsGenerator
input = split
primary_block = 1
paired_block = 0
new_boundary = 'interface0'
[]
uniform_refine = 4
[]
[Variables]
# Defining a DFEM variable to handle gap discontinuity
[T]
order = FIRST
family = MONOMIAL
[]
[]
[AuxVariables]
# Auxvariable containing bulk temperature of gap
[Tbulk]
order = FIRST
family = LAGRANGE
initial_condition = 300 # K
[]
[]
[Kernels]
[diff]
type = MatDiffusion
variable = T
diffusivity = conductivity
[]
[source]
type = BodyForce
variable = T
value = 1.0
[]
[]
[DGKernels]
# DG kernel to represent diffusion accross element faces
[./dg_diff]
type = DGDiffusion
variable = T
epsilon = -1
sigma = 6
diff = conductivity
# Ignoring gap side set because no diffusion accross there
exclude_boundary = 'interface0'
[../]
[]
[InterfaceKernels]
active = 'gap'
# Heat transfer kernel using Tbulk as material
[gap]
type = SideSetHeatTransferKernel
variable = T
neighbor_var = T
boundary = 'interface0'
[]
# Heat transfer kernel using Tbulk as auxvariable
[gap_var]
type = SideSetHeatTransferKernel
variable = T
neighbor_var = T
boundary = 'interface0'
Tbulk_var = Tbulk
[]
[]
[Functions]
[bc_func]
type = ConstantFunction
value = 300
[]
[exact]
type = ParsedFunction
value = '
A := if(x < 1, -0.5, -0.25);
B := if(x < 1, -0.293209850655001, 0.0545267662299068);
C := if(x < 1, 300.206790149345, 300.19547323377);
d := -1;
A * (x+d) * (x+d) + B * (x+d) + C'
[]
[]
[BCs]
[bc_left]
type = DGFunctionDiffusionDirichletBC
boundary = 'left'
variable = T
diff = 'conductivity'
epsilon = -1
sigma = 6
function = bc_func
[]
[bc_right]
type = DGFunctionDiffusionDirichletBC
boundary = 'right'
variable = T
diff = 'conductivity'
epsilon = -1
sigma = 6
function = bc_func
[]
[]
[Materials]
[k0]
type = GenericConstantMaterial
prop_names = 'conductivity'
prop_values = 1.0
block = 0
[]
[k1]
type = GenericConstantMaterial
prop_names = 'conductivity'
prop_values = 2.0
block = 1
[]
[gap_mat]
type = SideSetHeatTransferMaterial
boundary = 'interface0'
conductivity = 1.5
gap_length = 1.0
h_primary = 1
h_neighbor = 1
Tbulk = 300
emissivity_primary = 1
emissivity_neighbor = 1
[]
[]
[Postprocessors]
[error]
type = ElementL2Error
variable = T
function = exact
[]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(test/tests/mortar/continuity-3d-non-conforming/continuity_sphere_hex20.i)
[Mesh]
second_order = true
[file]
type = FileMeshGenerator
file = spheres_hex20.e
[]
[secondary]
input = file
type = LowerDBlockFromSidesetGenerator
new_block_id = 11
new_block_name = "secondary"
sidesets = '101'
[]
[primary]
input = secondary
type = LowerDBlockFromSidesetGenerator
new_block_id = 12
new_block_name = "primary"
sidesets = '102'
[]
[]
[Problem]
kernel_coverage_check = false
[]
[Variables]
[T]
block = '1 2'
family = LAGRANGE
order = SECOND
[]
[lambda]
block = 'secondary'
family = LAGRANGE
order = FIRST
[]
[]
[BCs]
[neumann]
type = FunctionGradientNeumannBC
exact_solution = exact_soln_primal
variable = T
boundary = '1 2'
[]
[]
[Kernels]
[conduction]
type = Diffusion
variable = T
block = '1 2'
[]
[sink]
type = Reaction
variable = T
block = '1 2'
[]
[forcing_function]
type = BodyForce
variable = T
function = forcing_function
block = '1 2'
[]
[]
[Functions]
[forcing_function]
type = ParsedFunction
value = 'x^2 + y^2 + z^2 - 6'
[]
[exact_soln_primal]
type = ParsedFunction
value = 'x^2 + y^2 + z^2'
[]
[exact_soln_lambda]
type = ParsedFunction
value = '4'
[]
[]
[Debug]
show_var_residual_norms = 1
[]
[Constraints]
[mortar]
type = EqualValueConstraint
primary_boundary = 2
secondary_boundary = 1
primary_subdomain = '12'
secondary_subdomain = '11'
variable = lambda
secondary_variable = T
correct_edge_dropping = true
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
solve_type = NEWTON
type = Steady
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_shift_type '
'-pc_factor_shift_amount'
petsc_options_value = 'lu basic NONZERO 1e-15'
[]
[Outputs]
exodus = true
[]
[Postprocessors]
[L2lambda]
type = ElementL2Error
variable = lambda
function = exact_soln_lambda
execute_on = 'timestep_end'
block = 'secondary'
[]
[L2u]
type = ElementL2Error
variable = T
function = exact_soln_primal
execute_on = 'timestep_end'
block = '1 2'
[]
[h]
type = AverageElementSize
block = '1 2'
[]
[]
(modules/phase_field/examples/fourier_noise.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 100
ny = 100
[]
[Variables]
[./c]
[../]
[]
[Functions]
[./fn]
type = FourierNoise
lambda = 0.1
[../]
[]
[ICs]
[./c]
type = FunctionIC
variable = c
function = fn
[../]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/porous_flow/test/tests/fluids/simple_fluid_dy.i)
# Test the properties calculated by the simple fluid Material
# Time unit is chosen to be days
# Pressure 10 MPa
# Temperature = 300 K (temperature unit = K)
# Density should equal 1500*exp(1E7/1E9-2E-4*300)=1426.844 kg/m^3
# Viscosity should equal 1.27E-8 Pa.dy
# Energy density should equal 4000 * 300 = 1.2E6 J/kg
# Specific enthalpy should equal 4000 * 300 + 10e6 / 1426.844 = 1.207008E6 J/kg
[Modules]
[FluidProperties]
[the_simple_fluid]
type = SimpleFluidProperties
thermal_expansion = 2.0E-4
cv = 4000.0
cp = 5000.0
bulk_modulus = 1.0E9
thermal_conductivity = 1.0
viscosity = 1.1E-3
density0 = 1500.0
[]
[]
[]
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp T'
number_fluid_phases = 1
number_fluid_components = 1
[]
[]
[Variables]
[pp]
initial_condition = 10E6
[]
[T]
initial_condition = 300.0
[]
[]
[Kernels]
[dummy_p]
type = Diffusion
variable = pp
[]
[dummy_T]
type = Diffusion
variable = T
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
temperature = T
[]
[ppss]
type = PorousFlow1PhaseFullySaturated
porepressure = pp
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
temperature_unit = Kelvin
time_unit = days
fp = the_simple_fluid
phase = 0
[]
[]
[Postprocessors]
[pressure]
type = ElementIntegralVariablePostprocessor
variable = pp
[]
[temperature]
type = ElementIntegralVariablePostprocessor
variable = T
[]
[density]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_fluid_phase_density_qp0'
[]
[viscosity]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_viscosity_qp0'
[]
[internal_energy]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_fluid_phase_internal_energy_qp0'
[]
[enthalpy]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_fluid_phase_enthalpy_qp0'
[]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
csv = true
[]
(test/tests/misc/check_error/invalid_steady_exec_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
# Time kernel in a steady state simulation
[./ie]
type = TimeDerivative
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/postprocessors/geometry/2d_geometry.i)
radius = 0.5
inner_box_length = 2.2
outer_box_length = 3
sides = 16
alpha = ${fparse 2 * pi / ${sides}}
perimeter_correction = ${fparse alpha / 2 / sin(alpha / 2)}
area_correction = ${fparse alpha / sin(alpha)}
[Mesh]
file = 2d.e
construct_side_list_from_node_list = true
[]
[Variables]
[./u]
initial_condition = 1
block = circle
[../]
[./v]
initial_condition = 2
block = 'inside outside'
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[BCs]
[./circle]
type = DirichletBC
variable = u
boundary = circle_side_wrt_inside
value = 2
[../]
[./inner]
type = DirichletBC
variable = v
boundary = circle_side_wrt_circle
value = 4
[../]
[./outer]
type = DirichletBC
variable = v
boundary = outside_side
value = 6
[../]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[./u_avg]
type = ElementAverageValue
variable = u
block = circle
[../]
[./v_avg]
type = ElementAverageValue
variable = v
block = 'inside outside'
[../]
[./circle_perimeter_wrt_circle]
type = AreaPostprocessor
boundary = circle_side_wrt_circle
[../]
[./circle_perimeter_wrt_inside]
type = AreaPostprocessor
boundary = circle_side_wrt_inside
[../]
[./inside_perimeter_wrt_inside]
type = AreaPostprocessor
boundary = inside_side_wrt_inside
[../]
[./inside_perimeter_wrt_outside]
type = AreaPostprocessor
boundary = inside_side_wrt_outside
[../]
[./outside_perimeter]
type = AreaPostprocessor
boundary = outside_side
[../]
[./circle_area]
type = VolumePostprocessor
block = circle
[../]
[./inside_area]
type = VolumePostprocessor
block = inside
[../]
[./outside_area]
type = VolumePostprocessor
block = outside
[../]
[./total_area]
type = VolumePostprocessor
block = 'circle inside outside'
[../]
[./circle_perimeter_exact]
type = FunctionValuePostprocessor
function = 'circle_perimeter_exact'
[../]
[./inside_perimeter_exact]
type = FunctionValuePostprocessor
function = 'inside_perimeter_exact'
[../]
[./outside_perimeter_exact]
type = FunctionValuePostprocessor
function = 'outside_perimeter_exact'
[../]
[./circle_area_exact]
type = FunctionValuePostprocessor
function = 'circle_area_exact'
[../]
[./inside_area_exact]
type = FunctionValuePostprocessor
function = 'inside_area_exact'
[../]
[./outside_area_exact]
type = FunctionValuePostprocessor
function = 'outside_area_exact'
[../]
[./total_area_exact]
type = FunctionValuePostprocessor
function = 'total_area_exact'
[../]
[]
[Functions]
[./circle_perimeter_exact]
type = ParsedFunction
value = '2 * pi * ${radius} / ${perimeter_correction}'
[../]
[./inside_perimeter_exact]
type = ParsedFunction
value = '${inner_box_length} * 4'
[../]
[./outside_perimeter_exact]
type = ParsedFunction
value = '${outer_box_length} * 4'
[../]
[./circle_area_exact]
type = ParsedFunction
value = 'pi * ${radius}^2 / ${area_correction}'
[../]
[./inside_area_exact]
type = ParsedFunction
value = '${inner_box_length}^2 - pi * ${radius}^2 / ${area_correction}'
[../]
[./outside_area_exact]
type = ParsedFunction
value = '${outer_box_length}^2 - ${inner_box_length}^2'
[../]
[./total_area_exact]
type = ParsedFunction
value = '${outer_box_length}^2'
[../]
[]
[Outputs]
csv = true
[]
(test/tests/variables/fe_hier/hier-3-3d.i)
[Mesh]
type = GeneratedMesh
dim = 3
xmin = -1
xmax = 1
ymin = -1
ymax = 1
zmin = -1
zmax = 1
nx = 1
ny = 1
nz = 1
elem_type = HEX27
# This problem only has 1 element, so using DistributedMesh in parallel
# isn't really an option, and we don't care that much about DistributedMesh
# in serial.
parallel_type = replicated
[]
[Functions]
[./bc_fnt]
type = ParsedFunction
value = 3*y*y
[../]
[./bc_fnb]
type = ParsedFunction
value = -3*y*y
[../]
[./bc_fnl]
type = ParsedFunction
value = -3*x*x
[../]
[./bc_fnr]
type = ParsedFunction
value = 3*x*x
[../]
[./bc_fnk]
type = ParsedFunction
value = -3*z*z
[../]
[./bc_fnf]
type = ParsedFunction
value = 3*z*z
[../]
[./forcing_fn]
type = ParsedFunction
value = -6*x-6*y-6*z+(x*x*x)+(y*y*y)+(z*z*z)
[../]
[./solution]
type = ParsedGradFunction
value = (x*x*x)+(y*y*y)+(z*z*z)
grad_x = 3*x*x
grad_y = 3*y*y
grad_z = 3*z*z
[../]
[]
[Variables]
[./u]
order = THIRD
family = HIERARCHIC
[../]
[]
[Kernels]
active = 'diff forcing reaction'
[./diff]
type = Diffusion
variable = u
[../]
[./reaction]
type = Reaction
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
[./bc_top]
type = FunctionNeumannBC
variable = u
boundary = 'top'
function = bc_fnt
[../]
[./bc_bottom]
type = FunctionNeumannBC
variable = u
boundary = 'bottom'
function = bc_fnb
[../]
[./bc_left]
type = FunctionNeumannBC
variable = u
boundary = 'left'
function = bc_fnl
[../]
[./bc_right]
type = FunctionNeumannBC
variable = u
boundary = 'right'
function = bc_fnr
[../]
[./bc_front]
type = FunctionNeumannBC
variable = u
boundary = 'front'
function = bc_fnf
[../]
[./bc_back]
type = FunctionNeumannBC
variable = u
boundary = 'back'
function = bc_fnk
[../]
[]
[Postprocessors]
[./dofs]
type = NumDOFs
[../]
[./h]
type = AverageElementSize
[../]
[./L2error]
type = ElementL2Error
variable = u
function = solution
[../]
[./H1error]
type = ElementH1Error
variable = u
function = solution
[../]
[./H1Semierror]
type = ElementH1SemiError
variable = u
function = solution
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
csv = true
[]
(test/tests/interfacekernels/1d_interface/sorted-interface-materials.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 10
xmax = 2
[]
[subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '1.0 0 0'
block_id = 1
top_right = '2.0 1.0 0'
[]
[interface]
input = subdomain1
type = SideSetsBetweenSubdomainsGenerator
primary_block = '0'
paired_block = '1'
new_boundary = 'primary0_interface'
[]
[]
[Variables]
[u]
block = '0'
initial_condition = 1
[]
[v]
block = '1'
initial_condition = 0
[]
[]
[Kernels]
[diff_u]
type = Diffusion
variable = u
block = 0
[]
[diff_v]
type = Diffusion
variable = v
block = 1
[]
[]
[InterfaceKernels]
[interface]
type = ADMaterialPropertySource
variable = u
neighbor_var = v
boundary = primary0_interface
source = couple
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 1
[]
[right]
type = DirichletBC
variable = v
boundary = 'right'
value = 0
[]
[]
[Materials]
[consumer]
type = ConsumerInterfaceMaterial
prop_consumed = ad_jump
prop_produced = couple
boundary = primary0_interface
[]
[jump]
type = JumpInterfaceMaterial
var = u
neighbor_var = v
boundary = primary0_interface
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(test/tests/variables/fe_hermite/hermite-3-3d.i)
[Mesh]
type = GeneratedMesh
dim = 3
xmin = -1
xmax = 1
ymin = -1
ymax = 1
zmin = -1
zmax = 1
nx = 1
ny = 1
nz = 1
elem_type = HEX27
# This problem only has 1 element, so using DistributedMesh in parallel
# isn't really an option, and we don't care that much about DistributedMesh
# in serial.
parallel_type = replicated
[]
[Functions]
[./bc_fnt]
type = ParsedFunction
value = 3*y*y
[../]
[./bc_fnb]
type = ParsedFunction
value = -3*y*y
[../]
[./bc_fnl]
type = ParsedFunction
value = -3*x*x
[../]
[./bc_fnr]
type = ParsedFunction
value = 3*x*x
[../]
[./bc_fnk]
type = ParsedFunction
value = -3*z*z
[../]
[./bc_fnf]
type = ParsedFunction
value = 3*z*z
[../]
[./forcing_fn]
type = ParsedFunction
value = -6*x-6*y-6*z+(x*x*x)+(y*y*y)+(z*z*z)
[../]
[./solution]
type = ParsedGradFunction
value = (x*x*x)+(y*y*y)+(z*z*z)
grad_x = 3*x*x
grad_y = 3*y*y
grad_z = 3*z*z
[../]
[]
[Variables]
[./u]
order = THIRD
family = HERMITE
[../]
[]
[Kernels]
active = 'diff forcing reaction'
[./diff]
type = Diffusion
variable = u
[../]
[./reaction]
type = Reaction
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
[./bc_top]
type = FunctionNeumannBC
variable = u
boundary = 'top'
function = bc_fnt
[../]
[./bc_bottom]
type = FunctionNeumannBC
variable = u
boundary = 'bottom'
function = bc_fnb
[../]
[./bc_left]
type = FunctionNeumannBC
variable = u
boundary = 'left'
function = bc_fnl
[../]
[./bc_right]
type = FunctionNeumannBC
variable = u
boundary = 'right'
function = bc_fnr
[../]
[./bc_front]
type = FunctionNeumannBC
variable = u
boundary = 'front'
function = bc_fnf
[../]
[./bc_back]
type = FunctionNeumannBC
variable = u
boundary = 'back'
function = bc_fnk
[../]
[]
[Postprocessors]
[./dofs]
type = NumDOFs
[../]
[./h]
type = AverageElementSize
[../]
[./L2error]
type = ElementL2Error
variable = u
function = solution
[../]
[./H1error]
type = ElementH1Error
variable = u
function = solution
[../]
[./H1Semierror]
type = ElementH1SemiError
variable = u
function = solution
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
csv = true
[]
(test/tests/userobjects/element_quality_check/failure_error.i)
[Mesh]
file = Quad.e
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./top]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[UserObjects]
[./elem_quality_check]
type = ElementQualityChecker
metric_type = STRETCH
failure_type = ERROR
upper_bound = 1.0
lower_bound = 0.5
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/phase_field/test/tests/initial_conditions/ClosePackIC_3D.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 5
ny = 5
nz = 5
xmax = 0.5
ymax = .5
zmax = 0.5
uniform_refine = 3
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./phi]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
[ICs]
[./close_pack]
radius = 0.1
outvalue = 0
variable = phi
invalue = 1
type = ClosePackIC
[../]
[]
(test/tests/kernels/simple_diffusion/simple_diffusion.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/usability/input.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/phase_field/test/tests/MultiSmoothCircleIC/test_problem.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
xmin = 0
xmax = 50
ymin = 0
ymax = 50
elem_type = QUAD4
[]
[Variables]
[./c]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./features]
order = CONSTANT
family = MONOMIAL
[../]
[./ghosts]
order = CONSTANT
family = MONOMIAL
[../]
[./halos]
order = CONSTANT
family = MONOMIAL
[../]
[./proc_id]
order = CONSTANT
family = MONOMIAL
[../]
[]
[ICs]
[./c]
type = LatticeSmoothCircleIC
variable = c
invalue = 1.0
outvalue = 0.0001
circles_per_side = '2 2'
pos_variation = 10.0
radius = 8.0
int_width = 5.0
radius_variation_type = uniform
avoid_bounds = false
[../]
[]
[BCs]
[./Periodic]
[./c]
variable = c
auto_direction = 'x y'
[../]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = c
[../]
[]
[AuxKernels]
[./features]
type = FeatureFloodCountAux
variable = features
execute_on = 'initial timestep_end'
flood_counter = features
[../]
[./ghosts]
type = FeatureFloodCountAux
variable = ghosts
field_display = GHOSTED_ENTITIES
execute_on = 'initial timestep_end'
flood_counter = features
[../]
[./halos]
type = FeatureFloodCountAux
variable = halos
field_display = HALOS
execute_on = 'initial timestep_end'
flood_counter = features
[../]
[./proc_id]
type = ProcessorIDAux
variable = proc_id
execute_on = 'initial timestep_end'
[../]
[]
[Postprocessors]
[./features]
type = FeatureFloodCount
variable = c
flood_entity_type = ELEMENTAL
execute_on = 'initial timestep_end'
[../]
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/mesh/splitting/grid_from_file.i)
[Mesh]
type = FileMesh
file = grid_from_file.e
[Partitioner]
type = GridPartitioner
nx = 2
ny = 2
nz = 1
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
[AuxVariables]
[pid]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[pid_aux]
type = ProcessorIDAux
variable = pid
execute_on = 'INITIAL'
[]
[]
(test/tests/utils/spline_interpolation/bicubic_spline_interpolation.i)
[Mesh]
type = GeneratedMesh
dim = 3
nz = 1
nx = 4
ny = 4
xmax = 4
ymax = 4
[]
[Functions]
[./yx1]
type = ParsedFunction
value = '3*x^2'
[../]
[./yx2]
type = ParsedFunction
value = '6*y^2'
[../]
[./spline_fn]
type = BicubicSplineFunction
x1 = '0 2 4'
x2 = '0 2 4 6'
y = '0 16 128 432 8 24 136 440 64 80 192 496'
yx11 = '0 0 0 0'
yx1n = '48 48 48 48'
yx21 = '0 0 0'
yx2n = '216 216 216'
yx1 = 'yx1'
yx2 = 'yx2'
[../]
[./u_func]
type = ParsedFunction
value = 'x^3 + 2*y^3'
[../]
[./u2_forcing_func]
type = ParsedFunction
value = '-6*x - 12*y'
[../]
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./bi_func_value]
order = FIRST
family = LAGRANGE
[../]
[./x_deriv]
order = FIRST
family = LAGRANGE
[../]
[./y_deriv]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./bi_func_value]
type = FunctionAux
variable = bi_func_value
function = spline_fn
[../]
[./deriv_1]
type = FunctionDerivativeAux
function = spline_fn
variable = x_deriv
component = x
[../]
[./deriv_2]
type = FunctionDerivativeAux
function = spline_fn
variable = y_deriv
component = y
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./body_force]
type = BodyForce
variable = u
function = u2_forcing_func
[../]
[]
[BCs]
[./sides]
type = FunctionDirichletBC
variable = u
boundary = '0 1 2 3'
function = u_func
[../]
[]
[Postprocessors]
[./nodal_l2_err_spline]
type = NodalL2Error
variable = u
function = spline_fn
execute_on = 'initial timestep_end'
[../]
[./nodal_l2_err_analytic]
type = NodalL2Error
variable = u
function = u_func
execute_on = 'initial timestep_end'
[../]
[./x_deriv_err_analytic]
type = NodalL2Error
variable = x_deriv
function = yx1
execute_on = 'initial timestep_end'
[../]
[./y_deriv_err_analytic]
type = NodalL2Error
variable = y_deriv
function = yx2
execute_on = 'initial timestep_end'
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(test/tests/misc/block_user_object_check/block_check.i)
[Mesh]
[./generator]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 5
[../]
[./left_block]
type = SubdomainBoundingBoxGenerator
input = generator
block_id = 1
bottom_left = '0 0 0'
top_right = '0.5 1 0'
[../]
[./right_block]
type = SubdomainBoundingBoxGenerator
input = left_block
block_id = 2
bottom_left = '0.5 0 0'
top_right = '1 1 0'
[../]
[]
[Variables]
[./var_1]
block = 1
initial_condition = 100
[../]
[./var_2]
block = 2
initial_condition = 200
[../]
[]
[Problem]
type = FEProblem
kernel_coverage_check = true
solve = false
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[./obj]
type = NodalExtremeValue
variable = var_1
#block = 1 # this is what being tested, see the test spec
execute_on = 'initial'
[../]
[]
(modules/stochastic_tools/test/tests/multiapps/transient_with_full_solve/sub.i)
[Mesh/gen]
type = GeneratedMeshGenerator
dim = 1
nx = 10
[]
[Variables/u]
[]
[Kernels/diff]
type = ADDiffusion
variable = u
[]
[BCs]
[left]
type = ADDirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = ADDirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
[]
[Postprocessors/center]
type = PointValue
point = '0.5 0 0'
variable = u
[]
[Controls/stochastic]
type = SamplerReceiver
[]
[Outputs]
[]
(modules/heat_conduction/test/tests/code_verification/spherical_test_no3.i)
# Problem III.3
#
# The thermal conductivity of a spherical shell varies linearly with
# temperature: k = k0(1+beta* u). The inside radius is ri and the outside radius
# is ro. It has a constant internal heat generation q and is exposed to
# the same constant temperature on both surfaces: u(ri) = u(ro) = uo.
#
# REFERENCE:
# A. Toptan, et al. (Mar.2020). Tech. rep. CASL-U-2020-1939-000, SAND2020-3887 R. DOI:10.2172/1614683.
[Mesh]
[./geom]
type = GeneratedMeshGenerator
dim = 1
elem_type = EDGE2
nx = 4
xmin = 0.2
[../]
[]
[Variables]
[./u]
order = FIRST
[../]
[]
[Problem]
coord_type = RSPHERICAL
[]
[Functions]
[./exact]
type = ParsedFunction
vars = 'q k0 ri ro beta u0'
vals = '1200 1 0.2 1.0 1e-3 0'
value = 'u0+(1/beta)*( ( 1 + (1/3)*beta*((ro^2-x^2)-(ro^2-ri^2) * (1/x-1/ro)/(1/ri-1/ro))*q/k0 )^0.5 - 1)'
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = u
[../]
[./heatsource]
type = HeatSource
function = 1200
variable = u
[../]
[]
[BCs]
[./uo]
type = DirichletBC
boundary = 'left right'
variable = u
value = 0
[../]
[]
[Materials]
[./property]
type = GenericConstantMaterial
prop_names = 'density specific_heat'
prop_values = '1.0 1.0'
[../]
[./thermal_conductivity]
type = ParsedMaterial
f_name = 'thermal_conductivity'
args = u
function = '1 * (1 + 1e-3*u)'
[../]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[./error]
type = ElementL2Error
function = exact
variable = u
[../]
[./h]
type = AverageElementSize
[]
[]
[Outputs]
csv = true
[]
(modules/thermal_hydraulics/test/tests/auxkernels/sum/sum.i)
# Tests the sum aux, which sums an arbitrary number of aux variables
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
allow_renumbering = false
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[AuxVariables]
[sum]
family = MONOMIAL
order = CONSTANT
[]
[value1]
family = MONOMIAL
order = CONSTANT
[]
[value2]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[sum_auxkernel]
type = SumAux
variable = sum
values = 'value1 value2'
[]
[value1_kernel]
type = ConstantAux
variable = value1
value = 2
[]
[value2_kernel]
type = ConstantAux
variable = value2
value = 3
[]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[sum_pp]
type = ElementalVariableValue
elementid = 0
variable = sum
[]
[]
[Outputs]
csv = true
execute_on = timestep_end
[]
(test/tests/relationship_managers/evaluable/all-systems-evaluable.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
[]
[Variables]
[u]
[]
[]
[UserObjects]
[all_sys]
type = AllSystemsEvaluable
execute_on = 'initial'
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
[Problem]
type = MooseTestProblem
solve = false
kernel_coverage_check = false
[]
(test/tests/meshgenerators/mesh_extruder_generator/extrude_remap_layer2.i)
[Mesh]
[./fmg]
type = FileMeshGenerator
file = multiblock.e
[]
[./extrude]
type = MeshExtruderGenerator
input = fmg
num_layers = 6
extrusion_vector = '0 0 2'
bottom_sideset = 'new_bottom'
top_sideset = 'new_top'
# Remap layers
existing_subdomains = '1 2 5'
layers = '1 3 5'
new_ids = '10 12 15' # Repeat this remapping for each layer
[]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = u
boundary = 'new_bottom'
value = 0
[../]
[./top]
type = DirichletBC
variable = u
boundary = 'new_top'
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/samplers/base/errors.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
ny = 1
[]
[Variables]
[./u]
[../]
[]
[Samplers]
[sample]
type = TestSampler
execute_on = 'INITIAL TIMESTEP_END'
[]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[test]
type = SamplerTester
sampler = sample
test_type = 'getGlobalSamples'
[]
[]
[Problem]
solve = false
kernel_coverage_check = false
[]
[Outputs]
[]
(test/tests/outputs/error/all_reserved.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[./all]
type = Exodus
[../]
[]
(test/tests/bcs/ad_matched_value_bc/test.i)
[Mesh]
[square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[]
[]
# Solves a pair of coupled diffusion equations where u=v on the boundary
[Variables]
[u]
order = FIRST
family = LAGRANGE
initial_condition = 3
[]
[v]
order = FIRST
family = LAGRANGE
initial_condition = 2
[]
[]
[Kernels]
[diff_u]
type = ADDiffusion
variable = u
[]
[diff_v]
type = ADDiffusion
variable = v
[]
[]
[BCs]
[right_v]
type = ADDirichletBC
variable = v
boundary = 1
value = 3
[]
[left_u]
type = ADMatchedValueBC
variable = u
boundary = 3
v = v
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
nl_rel_tol = 1e-10
l_tol = 1e-12
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/porous_flow/test/tests/relperm/corey1.i)
# Test Corey relative permeability curve by varying saturation over the mesh
# Corey exponent n = 1 for both phases (linear residual saturation)
# No residual saturation in either phase
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Variables]
[p0]
initial_condition = 1e6
[]
[s1]
[]
[]
[AuxVariables]
[s0aux]
family = MONOMIAL
order = CONSTANT
[]
[s1aux]
family = MONOMIAL
order = CONSTANT
[]
[kr0aux]
family = MONOMIAL
order = CONSTANT
[]
[kr1aux]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[s0]
type = PorousFlowPropertyAux
property = saturation
phase = 0
variable = s0aux
[]
[s1]
type = PorousFlowPropertyAux
property = saturation
phase = 1
variable = s1aux
[]
[kr0]
type = PorousFlowPropertyAux
property = relperm
phase = 0
variable = kr0aux
[]
[kr1]
type = PorousFlowPropertyAux
property = relperm
phase = 1
variable = kr1aux
[]
[]
[Functions]
[s1]
type = ParsedFunction
value = x
[]
[]
[ICs]
[s1]
type = FunctionIC
variable = s1
function = s1
[]
[]
[Kernels]
[p0]
type = Diffusion
variable = p0
[]
[s1]
type = Diffusion
variable = s1
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'p0 s1'
number_fluid_phases = 2
number_fluid_components = 2
[]
[pc]
type = PorousFlowCapillaryPressureConst
pc = 0
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow2PhasePS
phase0_porepressure = p0
phase1_saturation = s1
capillary_pressure = pc
[]
[kr0]
type = PorousFlowRelativePermeabilityCorey
phase = 0
n = 1
[]
[kr1]
type = PorousFlowRelativePermeabilityCorey
phase = 1
n = 1
[]
[]
[VectorPostprocessors]
[vpp]
type = LineValueSampler
warn_discontinuous_face_values = false
variable = 's0aux s1aux kr0aux kr1aux'
start_point = '0 0 0'
end_point = '1 0 0'
num_points = 20
sort_by = id
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
nl_abs_tol = 1e-8
[]
[BCs]
[sleft]
type = DirichletBC
variable = s1
value = 0
boundary = left
[]
[sright]
type = DirichletBC
variable = s1
value = 1
boundary = right
[]
[]
[Outputs]
csv = true
execute_on = timestep_end
[]
(test/tests/kernels/hfem/array_neumann.i)
[Mesh]
[square]
type = GeneratedMeshGenerator
nx = 3
ny = 3
dim = 2
[]
build_all_side_lowerd_mesh = true
[]
[Variables]
[u]
order = THIRD
family = MONOMIAL
block = 0
components = 2
[]
[lambda]
order = CONSTANT
family = MONOMIAL
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
components = 2
[]
[]
[AuxVariables]
[v]
order = CONSTANT
family = MONOMIAL
block = 0
initial_condition = '1'
[]
[]
[Kernels]
[diff]
type = ArrayDiffusion
variable = u
block = 0
diffusion_coefficient = dc
[]
[reaction]
type = ArrayReaction
variable = u
block = 0
reaction_coefficient = rc
[]
[source]
type = ArrayCoupledForce
variable = u
v = v
coef = '1 2'
block = 0
[]
[]
[DGKernels]
[surface]
type = ArrayHFEMDiffusion
variable = u
lowerd_variable = lambda
[]
[]
[BCs]
[all]
type = ArrayNeumannBC
boundary = 'left right top bottom'
variable = u
[]
[]
[Materials]
[dc]
type = GenericConstantArray
prop_name = dc
prop_value = '1 1'
[]
[rc]
type = GenericConstantArray
prop_name = rc
prop_value = '1 1'
[]
[]
[Postprocessors]
[intu]
type = ElementIntegralArrayVariablePostprocessor
variable = u
block = 0
[]
[lambdanorm]
type = ElementArrayL2Norm
variable = lambda
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu basic mumps'
[]
[Outputs]
[out]
# we hide lambda because it may flip sign due to element
# renumbering with distributed mesh
type = Exodus
hide = lambda
[]
csv = true
[]
(tutorials/tutorial01_app_development/step06_input_params/problems/pressure_diffusion.i)
[Mesh]
type = GeneratedMesh # Can generate simple lines, rectangles and rectangular prisms
dim = 2 # Dimension of the mesh
nx = 100 # Number of elements in the x direction
ny = 10 # Number of elements in the y direction
xmax = 0.304 # Length of test chamber
ymax = 0.0257 # Test chamber radius
[]
[Problem]
type = FEProblem # This is the "normal" type of Finite Element Problem in MOOSE
coord_type = RZ # Axisymmetric RZ
rz_coord_axis = X # Which axis the symmetry is around
[]
[Variables]
[pressure]
# Adds a Linear Lagrange variable by default
[]
[]
[Kernels]
[diffusion]
type = DarcyPressure # Zero-gravity, divergence-free form of Darcy's law
variable = pressure # Operate on the "pressure" variable from above
permeability = 0.8451e-09 # (m^2) assumed permeability of the porous medium
[]
[]
[BCs]
[inlet]
type = ADDirichletBC # Simple u=value BC
variable = pressure # Variable to be set
boundary = left # Name of a sideset in the mesh
value = 4000 # (Pa) From Figure 2 from paper. First data point for 1mm spheres.
[]
[outlet]
type = ADDirichletBC
variable = pressure
boundary = right
value = 0 # (Pa) Gives the correct pressure drop from Figure 2 for 1mm spheres
[]
[]
[Executioner]
type = Steady # Steady state problem
solve_type = NEWTON # Perform a Newton solve
# Set PETSc parameters to optimize solver efficiency
petsc_options_iname = '-pc_type -pc_hypre_type' # PETSc option pairs with values below
petsc_options_value = ' hypre boomeramg'
[]
[Outputs]
exodus = true # Output Exodus format
[]
(test/tests/misc/check_error/missing_coupled_mat_prop_test.i)
[Mesh]
file = rectangle.e
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff body_force'
[./diff]
type = Diffusion
variable = u
[../]
[./body_force]
type = BodyForce
variable = u
block = 1
value = 10
[../]
[]
[BCs]
active = 'right'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Materials]
# This material is global and uses a coupled property
[./mat_global]
type = CoupledMaterial
mat_prop = 'some_prop'
coupled_mat_prop = 'mp1'
block = '1 2'
[../]
# This material supplies a value for block 1 ONLY
[./mat_0]
type = GenericConstantMaterial
block = 1
prop_names = 'mp1'
prop_values = 2
[../]
[]
[Executioner]
type = Steady
# solve_type = 'PJFNK'
# preconditioner = 'ILU'
solve_type = 'PJFNK'
# petsc_options_iname = '-pc_type -pc_hypre_type'
# petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
file_base = missing_mat_prop_test
exodus = true
[]
(modules/ray_tracing/test/tests/traceray/raybc_check/raybc_check.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 1
ny = 1
xmax = 1
ymax = 1
[]
[]
[UserObjects/study]
type = RepeatableRayStudy
start_points = '0 0 0'
directions = '1 1 0'
names = ray
[]
[RayKernels/null]
type = NullRayKernel
[]
[RayBCs]
active = ''
[top]
type = NullRayBC
boundary = top
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
(modules/heat_conduction/test/tests/code_verification/cartesian_test_no5.i)
# Problem I.5
#
# The volumetric heat generation in an infinite plate varies linearly
# with spatial location. It has constant thermal conductivity.
# It is insulated on the left boundary and exposed to a
# constant temperature on the right.
#
# REFERENCE:
# A. Toptan, et al. (Mar.2020). Tech. rep. CASL-U-2020-1939-000, SAND2020-3887 R. DOI:10.2172/1614683.
[Mesh]
[./geom]
type = GeneratedMeshGenerator
dim = 1
elem_type = EDGE2
nx = 1
[../]
[]
[Variables]
[./u]
order = FIRST
[../]
[]
[Functions]
[./volumetric_heat]
type = ParsedFunction
vars = 'q L beta'
vals = '1200 1 0.1'
value = 'q * (1-beta*x/L)'
[../]
[./exact]
type = ParsedFunction
vars = 'uo q k L beta'
vals = '300 1200 1 1 0.1'
value = 'uo + (0.5*q*L^2/k) * ( (1-(x/L)^2) - (1-(x/L)^3) * beta/3 )'
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = u
[../]
[./heatsource]
type = HeatSource
function = volumetric_heat
variable = u
[../]
[]
[BCs]
[./uo]
type = DirichletBC
boundary = right
variable = u
value = 300
[../]
[]
[Materials]
[./property]
type = GenericConstantMaterial
prop_names = 'density specific_heat thermal_conductivity'
prop_values = '1.0 1.0 1.0'
[../]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[./error]
type = ElementL2Error
function = exact
variable = u
[../]
[./h]
type = AverageElementSize
[]
[]
[Outputs]
csv = true
[]
(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/heated/2d-rc-heated-action.i)
mu=1
rho=1
k=1e-3
cp=1
u_inlet=1
T_inlet=200
h_cv = 1.0
[Mesh]
[mesh]
type = CartesianMeshGenerator
dim = 2
dx = '5 5'
dy = '1.0'
ix = '50 50'
iy = '20'
subdomain_id = '1 2'
[]
[]
[Variables]
[T_solid]
type = MooseVariableFVReal
[]
[]
[AuxVariables]
[porosity]
type = MooseVariableFVReal
initial_condition = 0.5
[]
[]
[Modules]
[NavierStokesFV]
compressibility = 'incompressible'
porous_medium_treatment = true
add_energy_equation = true
density = ${rho}
dynamic_viscosity = ${mu}
thermal_conductivity = ${k}
specific_heat = ${cp}
porosity = 'porosity'
initial_velocity = '${u_inlet} 1e-6 0'
initial_pressure = 0.0
initial_temperature = 0.0
inlet_boundaries = 'left'
momentum_inlet_types = 'fixed-velocity'
momentum_inlet_function = '${u_inlet} 0'
energy_inlet_types = 'heatflux'
energy_inlet_function = '${fparse u_inlet * rho * cp * T_inlet}'
wall_boundaries = 'top bottom'
momentum_wall_types = 'noslip symmetry'
energy_wall_types = 'heatflux heatflux'
energy_wall_function = '0 0'
outlet_boundaries = 'right'
momentum_outlet_types = 'fixed-pressure'
pressure_function = '0.1'
ambient_convection_alpha = ${h_cv}
ambient_temperature = 'T_solid'
[]
[]
[FVKernels]
[solid_energy_diffusion]
type = FVDiffusion
coeff = ${k}
variable = T_solid
[]
[solid_energy_convection]
type = PINSFVEnergyAmbientConvection
variable = 'T_solid'
is_solid = true
T_fluid = 'T_fluid'
T_solid = 'T_solid'
h_solid_fluid = ${h_cv}
[]
[]
[FVBCs]
[heated-side]
type = FVDirichletBC
boundary = 'top'
variable = 'T_solid'
value = 150
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-14
[]
# Some basic Postprocessors to examine the solution
[Postprocessors]
[inlet-p]
type = SideAverageValue
variable = pressure
boundary = 'left'
[]
[outlet-u]
type = SideAverageValue
variable = superficial_vel_x
boundary = 'right'
[]
[outlet-temp]
type = SideAverageValue
variable = T_fluid
boundary = 'right'
[]
[solid-temp]
type = ElementAverageValue
variable = T_solid
[]
[]
[Outputs]
exodus = true
csv = false
[]
(test/tests/misc/check_error/scalar_aux_kernel_with_var.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./v]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./rea]
type = Reaction
variable = u
[../]
[]
[AuxScalarKernels]
[./nope]
type = ConstantScalarAux
variable = u
value = 11
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/tensor_mechanics/test/tests/action/material_output_first_lagrange_manual.i)
# This input file is designed to test adding extra stress to ADComputeLinearElasticStress
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmax = 50
ymax = 50
[]
[AuxVariables]
[vonmises_stress]
order = FIRST
family = LAGRANGE
[]
[]
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Modules/TensorMechanics/Master/All]
strain = SMALL
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx hydrostatic_stress'
material_output_order = 'CONSTANT CONSTANT CONSTANT CONSTANT CONSTANT CONSTANT CONSTANT'
material_output_family = 'MONOMIAL MONOMIAL MONOMIAL MONOMIAL MONOMIAL MONOMIAL MONOMIAL'
use_automatic_differentiation = true
[]
[AuxKernels]
[vonmises_stress]
type = ADRankTwoScalarAux
variable = vonmises_stress
rank_two_tensor = stress
scalar_type = VonMisesStress
[]
[]
[Materials]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0
[]
[stress]
type = ADComputeLinearElasticStress
extra_stress_names = 'stress_one stress_two'
[]
[stress_one]
type = GenericConstantRankTwoTensor
tensor_name = stress_one
tensor_values = '0 1e3 1e3 1e3 0 1e3 1e3 1e3 0'
[]
[stress_two]
type = GenericConstantRankTwoTensor
tensor_name = stress_two
tensor_values = '1e3 0 0 0 1e3 0 0 0 1e3'
[]
[]
[BCs]
[disp_x_BC]
type = ADDirichletBC
variable = disp_x
boundary = 'bottom top'
value = 0.5
[]
[disp_x_BC2]
type = ADDirichletBC
variable = disp_x
boundary = 'left right'
value = 0.01
[]
[disp_y_BC]
type = ADDirichletBC
variable = disp_y
boundary = 'bottom top'
value = 0.8
[]
[disp_y_BC2]
type = ADDirichletBC
variable = disp_y
boundary = 'left right'
value = 0.02
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Postprocessors]
[hydrostatic]
type = ElementAverageValue
variable = hydrostatic_stress
[]
[von_mises]
type = ElementAverageValue
variable = vonmises_stress
[]
[]
[Outputs]
exodus = true
[]
(test/tests/bcs/penalty_dirichlet_bc/penalty_dirichlet_bc_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 10
ny = 10
elem_type = QUAD9
[]
[Functions]
[./forcing_fn]
type = ParsedFunction
value = -2*(x*x+y*y-2)+(1-x*x)*(1-y*y)
[../]
[./solution]
type = ParsedGradFunction
value = (1-x*x)*(1-y*y)
grad_x = 2*(x*y*y-x)
grad_y = 2*(x*x*y-y)
[../]
[]
[Variables]
[./u]
order = SECOND
family = HIERARCHIC
[../]
[]
[Kernels]
active = 'diff forcing reaction'
[./diff]
type = Diffusion
variable = u
[../]
[./reaction]
type = Reaction
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
active = 'bc_all'
[./bc_all]
type = PenaltyDirichletBC
variable = u
value = 0
boundary = 'top left right bottom'
penalty = 1e5
[../]
[]
[Postprocessors]
[./dofs]
type = NumDOFs
[../]
[./h]
type = AverageElementSize
[../]
[./L2error]
type = ElementL2Error
variable = u
function = solution
[../]
[./H1error]
type = ElementH1Error
variable = u
function = solution
[../]
[./H1Semierror]
type = ElementH1SemiError
variable = u
function = solution
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
nl_rel_tol = 1e-14
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
csv = true
[]
(test/tests/bcs/sideset_from_nodeset/sideset_from_nodeset_test2.i)
[Mesh]
file = cube_no_sidesets2.e
construct_side_list_from_node_list = true
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = NeumannBC
variable = u
boundary = 3
value = 3
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
file_base = cube_tet_out
exodus = true
[]
(python/mms/test/mms_spatial.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 8
ny = 8
[]
[Variables]
[u][]
[]
[Kernels]
[diff]
type = ADDiffusion
variable = u
[]
[force]
type = BodyForce
variable = u
function = force
[]
[]
[Functions]
[exact]
type = ParsedFunction
value = 'sin(2*pi*x)*sin(2*pi*y)'
[]
[force]
type = ParsedFunction
value = '8*pi^2*sin(2*x*pi)*sin(2*y*pi)'
[]
[]
[BCs]
[all]
type = FunctionDirichletBC
variable = u
function = exact
boundary = 'left right top bottom'
[]
[]
[Postprocessors]
[error]
type = ElementL2Error
function = exact
variable = u
[]
[h]
type = AverageElementSize
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
csv = true
[]
(test/tests/auxkernels/array_var_component/array_var_component.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 4
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
components = 2
[]
[]
[Kernels]
[diff]
type = ArrayDiffusion
variable = u
diffusion_coefficient = dc
[]
[]
[BCs]
[left]
type = ArrayDirichletBC
variable = u
boundary = 1
values = '0 0'
[]
[right]
type = ArrayDirichletBC
variable = u
boundary = 2
values = '1 2'
[]
[]
[Materials]
[dc]
type = GenericConstantArray
prop_name = dc
prop_value = '1 1'
[]
[]
[AuxVariables]
[u0][]
[]
[AuxKernels]
[u0]
type = ArrayVariableComponent
variable = u0
array_variable = u
component = 0
[]
[]
[Postprocessors]
[intu0]
type = ElementIntegralVariablePostprocessor
variable = u0
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(test/tests/meshgenerators/unique_extra_id_mesh_generator/unique_id.i)
[Mesh]
[fmg]
type = FileMeshGenerator
file = unique_id.e
exodus_extra_element_integers = 'id1 id0'
[]
[parse_id]
type = UniqueExtraIDMeshGenerator
input = fmg
id_name = 'id1 id0'
new_id_name = 'parsed_id'
[]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[AuxVariables]
[parsed_id]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[aux_parsed_id]
type = ExtraElementIDAux
variable = parsed_id
extra_id_name = parsed_id
[]
[]
[Outputs]
exodus = true
execute_on = timestep_end
[]
(test/tests/fvkernels/block-restriction/just-mat-blk-restriction.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 50
xmax = 4
[]
[./subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '2.0 0 0'
block_id = 1
top_right = '4.0 1.0 0'
[../]
[./left_right]
input = subdomain1
type = SideSetsBetweenSubdomainsGenerator
primary_block = '0'
paired_block = '1'
new_boundary = 'left_right'
[../]
[./right_left]
input = left_right
type = SideSetsBetweenSubdomainsGenerator
primary_block = '1'
paired_block = '0'
new_boundary = 'right_left'
[../]
[]
[Variables]
[fv]
family = MONOMIAL
order = CONSTANT
fv = true
initial_condition = 1
[]
[]
[FVKernels]
[diff]
type = FVDiffusion
variable = fv
coeff = diff
[]
[]
[FVBCs]
[left]
type = FVDirichletBC
variable = fv
boundary = left
value = 0
[]
[right]
type = FVDirichletBC
variable = fv
boundary = right
value = 1
[]
[]
[Materials]
[left]
type = ADGenericFunctorMaterial
prop_names = 'diff'
prop_values = '1'
block = 0
[]
[right]
type = ADGenericFunctorMaterial
prop_names = 'diff'
prop_values = '2'
block = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
[]
[Outputs]
exodus = true
[dof]
type = DOFMap
execute_on = 'initial'
[]
[]
(test/tests/controls/control_connection/alias_connection.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = CoefDiffusion
variable = u
coef = 0.1
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Controls]
[./control]
type = TestControl
execute_on = INITIAL
test_type = 'alias'
[../]
[]
[Outputs]
exodus = true
[]
(test/tests/mesh/node_list_from_side_list/node_list_from_side_list.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[rename]
type = RenameBoundaryGenerator
input = gen
old_boundary = 'left'
new_boundary = 'renamed_left'
[]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/ic_bnd_for_non_nodal.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
[]
[Variables]
[./u]
order = CONSTANT
family = MONOMIAL
[../]
[]
[ICs]
[./u_ic]
type = ConstantIC
value = 1
variable = u
boundary = top
[../]
[../]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/cns/mms/1d-with-bcs/straight-channel-hllc.i)
[GlobalParams]
fp = fp
[]
[Mesh]
[./gen_mesh]
type = CartesianMeshGenerator
dim = 1
dx = '.1 .1 .1 .1 .1 .5 .1 .1 .1 .1 .1'
# dx = '.1 .1 .1 .1 .1 .1 .1 .1 .1 .1 .1 .1 .1 .1 .1'
[../]
[]
[Modules]
[FluidProperties]
[fp]
type = IdealGasFluidProperties
[]
[]
[]
[Variables]
[rho]
type = MooseVariableFVReal
initial_condition = 1.28969
scaling = 1e3
[]
[rho_u]
type = MooseVariableFVReal
initial_condition = 1.28969
[]
[rho_et]
type = MooseVariableFVReal
initial_condition = 2.525e5
scaling = 1e-2
[]
[]
[FVKernels]
[mass_advection]
type = CNSFVMassHLLC
variable = rho
fp = fp
[]
[momentum_x_advection]
type = CNSFVMomentumHLLC
variable = rho_u
momentum_component = x
fp = fp
[]
[drag]
type = FVReaction
variable = rho_u
rate = 1000
[]
[fluid_energy_advection]
type = CNSFVFluidEnergyHLLC
variable = rho_et
fp = fp
[]
[]
[FVBCs]
[mass_in]
variable = rho
type = CNSFVHLLCSpecifiedMassFluxAndTemperatureMassBC
boundary = left
temperature = 273.15
rhou = 1.28969
[]
[momentum_in]
variable = rho_u
type = CNSFVHLLCSpecifiedMassFluxAndTemperatureMomentumBC
boundary = left
temperature = 273.15
rhou = 1.28969
momentum_component = 'x'
[]
[energy_in]
variable = rho_et
type = CNSFVHLLCSpecifiedMassFluxAndTemperatureFluidEnergyBC
boundary = left
temperature = 273.15
rhou = 1.28969
[]
[mass_out]
variable = rho
type = CNSFVHLLCSpecifiedPressureMassBC
boundary = right
pressure = 1.01e5
[]
[momentum_out]
variable = rho_u
type = CNSFVHLLCSpecifiedPressureMomentumBC
boundary = right
pressure = 1.01e5
momentum_component = 'x'
[]
[energy_out]
variable = rho_et
type = CNSFVHLLCSpecifiedPressureFluidEnergyBC
boundary = right
pressure = 1.01e5
[]
[]
[Materials]
[var_mat]
type = ConservedVarValuesMaterial
rho = rho
rhou = rho_u
rho_et = rho_et
[]
[]
[Executioner]
solve_type = NEWTON
type = Steady
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
nl_max_its = 50
line_search = none
[]
[Outputs]
exodus = true
csv = true
[]
[Debug]
show_var_residual_norms = true
[]
(test/tests/fvbcs/fv_neumannbc/fv_neumannbc.i)
[Mesh]
[mesh]
type = CartesianMeshGenerator
dim = 2
dx = '1 1'
dy = '1'
ix = '5 5'
iy = '5'
subdomain_id = '1 1'
[]
[internal_sideset]
type = ParsedGenerateSideset
combinatorial_geometry = 'x<1.01 & x>0.99'
included_subdomain_ids = 1
new_sideset_name = 'center'
input = 'mesh'
[]
[]
[Variables]
[u]
family = MONOMIAL
order = CONSTANT
fv = true
block = 1
[]
[]
[FVKernels]
[diff]
type = FVDiffusion
variable = u
coeff = 1
[]
[]
[FVBCs]
inactive = 'center'
[left]
type = FVDirichletBC
variable = u
boundary = left
value = 1
[]
[right]
type = FVNeumannBC
variable = u
boundary = right
value = 4
[]
# Internal center sideset, should cause erroring out
[center]
type = FVNeumannBC
variable = u
boundary = center
value = 0
[]
[]
[Executioner]
type = Steady
solve_type = 'Newton'
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
[]
[Outputs]
exodus = true
[]
(test/tests/materials/derivative_material_interface/material_chaining.i)
#
# This test validates the correct application of the chain rule to coupled
# material properties within DerivativeParsedMaterials
#
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
xmin = 0
xmax = 1
ymin = 0
ymax = 1
[]
[Variables]
[./eta1]
[../]
[./eta2]
[../]
[]
[BCs]
[./left]
variable = eta1
boundary = left
type = DirichletBC
value = 0
[../]
[./right]
variable = eta1
boundary = right
type = DirichletBC
value = 1
[../]
[./top]
variable = eta2
boundary = top
type = DirichletBC
value = 0
[../]
[./bottom]
variable = eta2
boundary = bottom
type = DirichletBC
value = 1
[../]
[]
[Materials]
# T1 := (eta1+1)^4
[./term]
type = DerivativeParsedMaterial
f_name= T1
args = 'eta1'
function = '(eta1+1)^4'
derivative_order = 4
[../]
# in this material we substitute T1 explicitly
[./full]
type = DerivativeParsedMaterial
args = 'eta1 eta2'
f_name = F1
function = '(1-eta2)^4+(eta1+1)^4'
[../]
# in this material we utilize the T1 derivative material property
[./subs]
type = DerivativeParsedMaterial
args = 'eta1 eta2'
f_name = F2
function = '(1-eta2)^4+T1'
material_property_names = 'T1(eta1)'
[../]
# calculate differences between the explicit and indirect substitution version
# the use if the T1 property should include dT1/deta1 contributions!
# This also demonstrated the explicit use of material property derivatives using
# the D[...] syntax.
[./diff0]
type = ParsedMaterial
f_name = D0
function = '(F1-F2)^2'
material_property_names = 'F1 F2'
[../]
[./diff1]
type = ParsedMaterial
f_name = D1
function = '(dF1-dF2)^2'
material_property_names = 'dF1:=D[F1,eta1] dF2:=D[F2,eta1]'
[../]
[./diff2]
type = ParsedMaterial
f_name = D2
function = '(d2F1-d2F2)^2'
material_property_names = 'd2F1:=D[F1,eta1,eta1] d2F2:=D[F2,eta1,eta1]'
[../]
# check that explicitly pulling a derivative yields the correct result by
# taking the difference of the manually calculated 1st derivative of T1 and the
# automatic derivative dT1 pulled in through dT1:=D[T1,eta1]
[./diff3]
type = ParsedMaterial
f_name = E0
function = '(dTd1-(4*(eta1+1)^3))^2'
args = eta1
material_property_names = 'dTd1:=D[T1,eta1]'
[../]
[]
[Kernels]
[./eta1diff]
type = Diffusion
variable = eta1
[../]
[./eta2diff]
type = Diffusion
variable = eta2
[../]
[]
[Postprocessors]
[./D0]
type = ElementIntegralMaterialProperty
mat_prop = D0
[../]
[./D1]
type = ElementIntegralMaterialProperty
mat_prop = D1
[../]
[./D2]
type = ElementIntegralMaterialProperty
mat_prop = D2
[../]
[./E0]
type = ElementIntegralMaterialProperty
mat_prop = E0
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
l_tol = 1e-03
[]
[Outputs]
execute_on = 'TIMESTEP_END'
csv = true
print_linear_residuals = false
[]
(modules/heat_conduction/test/tests/heat_conduction/3d_quadrature_gap_heat_transfer/nonmatching.i)
[Mesh]
file = nonmatching.e
[]
[Variables]
[./temp]
[../]
[]
[Kernels]
[./hc]
type = HeatConduction
variable = temp
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = temp
boundary = leftleft
value = 1000
[../]
[./right]
type = DirichletBC
variable = temp
boundary = rightright
value = 400
[../]
[]
[ThermalContact]
[./left_to_right]
secondary = leftright
quadrature = true
primary = rightleft
variable = temp
emissivity_primary = 0
emissivity_secondary = 0
type = GapHeatTransfer
[../]
[]
[Materials]
[./hcm]
type = HeatConductionMaterial
block = 'left right'
specific_heat = 1
thermal_conductivity = 1
[../]
[]
[Postprocessors]
[./left]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = leftright
diffusivity = thermal_conductivity
[../]
[./right]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = rightleft
diffusivity = thermal_conductivity
[../]
[]
[Executioner]
type = Steady
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/misc/stop_for_debugger/stop_for_debugger.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/geomsearch/3d_penetration_locator/3d_penetration_locator_test.i)
[Mesh]
file = 3d_penetration_test.e
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./penetration]
order = FIRST
family = LAGRANGE
[../]
[./tangential_distance]
order = FIRST
family = LAGRANGE
[../]
[./normal_x]
order = FIRST
family = LAGRANGE
[../]
[./normal_y]
order = FIRST
family = LAGRANGE
[../]
[./normal_z]
order = FIRST
family = LAGRANGE
[../]
[./closest_point_x]
order = FIRST
family = LAGRANGE
[../]
[./closest_point_y]
order = FIRST
family = LAGRANGE
[../]
[./closest_point_z]
order = FIRST
family = LAGRANGE
[../]
[./element_id]
order = FIRST
family = LAGRANGE
[../]
[./side]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = penetration
boundary = 2
paired_boundary = 3
[../]
[./penetrate2]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 2
paired_boundary = 3
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 3
paired_boundary = 2
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 2
paired_boundary = 3
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 3
paired_boundary = 2
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 2
paired_boundary = 3
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 3
paired_boundary = 2
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = normal_z
boundary = 2
paired_boundary = 3
quantity = normal_z
[../]
[./penetrate10]
type = PenetrationAux
variable = normal_z
boundary = 3
paired_boundary = 2
quantity = normal_z
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_x
boundary = 2
paired_boundary = 3
quantity = closest_point_x
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_x
boundary = 3
paired_boundary = 2
quantity = closest_point_x
[../]
[./penetrate13]
type = PenetrationAux
variable = closest_point_y
boundary = 2
paired_boundary = 3
quantity = closest_point_y
[../]
[./penetrate14]
type = PenetrationAux
variable = closest_point_y
boundary = 3
paired_boundary = 2
quantity = closest_point_y
[../]
[./penetrate15]
type = PenetrationAux
variable = closest_point_z
boundary = 2
paired_boundary = 3
quantity = closest_point_z
[../]
[./penetrate16]
type = PenetrationAux
variable = closest_point_z
boundary = 3
paired_boundary = 2
quantity = closest_point_z
[../]
[./penetrate17]
type = PenetrationAux
variable = element_id
boundary = 2
paired_boundary = 3
quantity = element_id
[../]
[./penetrate18]
type = PenetrationAux
variable = element_id
boundary = 3
paired_boundary = 2
quantity = element_id
[../]
[./penetrate19]
type = PenetrationAux
variable = side
boundary = 2
paired_boundary = 3
quantity = side
[../]
[./penetrate20]
type = PenetrationAux
variable = side
boundary = 3
paired_boundary = 2
quantity = side
[../]
[]
[BCs]
active = 'block1_left block1_right block2_left block2_right'
[./block1_left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./block1_right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[./block2_left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./block2_right]
type = DirichletBC
variable = u
boundary = 4
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/markers/q_point_marker/q_point_marker.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
nz = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
solve_type = PJFNK
[]
[Adaptivity]
[./Markers]
[./marker]
type = QPointMarker
variable = u
[../]
[../]
[]
[Outputs]
exodus = true
[]
(test/tests/vectorpostprocessors/cylindrical_average/cylindrical_average.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 10
ny = 10
nz = 1
xmin = -5
xmax = 5
ymin = -5
ymax = 5
zmin = 0
zmax = 1
[]
[Problem]
kernel_coverage_check = false
[]
[Variables]
[./c]
[../]
[]
[AuxVariables]
[./d]
[../]
[]
[AuxKernels]
[./d]
type = FunctionAux
variable = d
function = set_d
execute_on = initial
[../]
[]
[Functions]
[./set_d]
type = ParsedFunction
value = 'r := sqrt(x * x + y * y); r'
[../]
[]
[VectorPostprocessors]
[./average]
type = CylindricalAverage
variable = d
radius = 5
bin_number = 10
origin = '0 0 0'
cylinder_axis = '0 0 1'
execute_on = 'initial timestep_end'
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
execute_on = 'initial timestep_end'
csv = true
[]
(test/tests/auxkernels/diffusion_flux/diffusion_flux.i)
[Mesh]
type = GeneratedMesh # Can generate simple lines, rectangles and rectangular prisms
dim = 2 # Dimension of the mesh
nx = 10 # Number of elements in the x direction
ny = 10 # Number of elements in the y direction
xmax = 1.0
ymax = 1.0
[]
[Variables]
[./T]
[../]
[]
[AuxVariables]
[./flux_x]
order = FIRST
family = MONOMIAL
[../]
[./flux_y]
order = FIRST
family = MONOMIAL
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = MatDiffusionTest # A Laplacian operator
variable = T
prop_name = 'thermal_conductivity'
[../]
[./diff_ad]
type = ADMatDiffusion # A Laplacian operator
variable = T
diffusivity = 'thermal_conductivity'
[../]
[]
[AuxKernels]
[./flux_x]
type = DiffusionFluxAux
diffusivity = 'thermal_conductivity'
variable = flux_x
diffusion_variable = T
component = x
[../]
[./flux_y]
type = DiffusionFluxAux
diffusivity = 'thermal_conductivity'
variable = flux_y
diffusion_variable = T
component = y
[../]
[]
[BCs]
[./inlet]
type = DirichletBC # Simple u=value BC
variable = T
boundary = left
value = 4000 # K
[../]
[./outlet]
type = DirichletBC
variable = T
boundary = right
value = 400 # K
[../]
[]
[Materials]
[./k]
type = GenericConstantMaterial
prop_names = 'thermal_conductivity'
prop_values = '10' # in W/mK
[../]
[]
[VectorPostprocessors]
# avoid sampling an element variable on faces
[./line_sample]
type = LineValueSampler
variable = 'T flux_x flux_y'
start_point = '0.01 0.01 0'
end_point = '0.98 0.01 0'
num_points = 11
sort_by = id
[../]
[]
[Executioner]
type = Steady # Steady state problem
solve_type = PJFNK #Preconditioned Jacobian Free Newton Krylov
nl_rel_tol = 1e-12
petsc_options_iname = '-pc_type -pc_hypre_type' #Matches with the values below
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true # Output Exodus format
execute_on = 'initial timestep_end'
csv = true
[]
(test/tests/meshgenerators/mesh_extruder_generator/extrude_remap_layer1.i)
[Mesh]
[./fmg]
type = FileMeshGenerator
file = multiblock.e
[]
[./extrude]
type = MeshExtruderGenerator
input = fmg
num_layers = 6
extrusion_vector = '0 0 2'
bottom_sideset = 'new_bottom'
top_sideset = 'new_top'
# Remap layers
existing_subdomains = '1 2 5'
layers = '1 3 5'
new_ids = '10 12 15
30 32 35
50 52 55'
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = u
boundary = 'new_bottom'
value = 0
[../]
[./top]
type = DirichletBC
variable = u
boundary = 'new_top'
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(modules/richards/test/tests/jacobian_1/jn_fu_06.i)
# unsaturated = true
# gravity = false
# supg = true
# transient = false
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = -1
xmax = 1
ymin = -1
ymax = 1
zmin = -1
zmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGstandard
sat_UO = Saturation
seff_UO = SeffVG
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0 # notice small quantity, so the PETSc constant state works
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1 # notice small quantity, so the PETSc constant state works
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.2
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 0.1
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = RandomIC
block = 0
min = -1
max = 0
[../]
[../]
[]
[Kernels]
active = 'richardsf'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFullyUpwindFlux
variable = pressure
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
viscosity = 1E-3
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -snes_type'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000 test'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = jn06
exodus = false
[]
(modules/porous_flow/test/tests/newton_cooling/nc06.i)
# Newton cooling from a bar. 1-phase and heat, steady
[Mesh]
type = GeneratedMesh
dim = 2
nx = 100
ny = 1
xmin = 0
xmax = 100
ymin = 0
ymax = 1
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pressure temp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureVG
m = 0.8
alpha = 1e-5
[]
[]
[Variables]
[pressure]
[]
[temp]
[]
[]
[ICs]
# have to start these reasonably close to their steady-state values
[pressure]
type = FunctionIC
variable = pressure
function = '(2-x/100)*1E6'
[]
[temperature]
type = FunctionIC
variable = temp
function = 100+0.1*x
[]
[]
[Kernels]
[flux]
type = PorousFlowAdvectiveFlux
fluid_component = 0
gravity = '0 0 0'
variable = pressure
[]
[heat_advection]
type = PorousFlowHeatAdvection
gravity = '0 0 0'
variable = temp
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 1e6
density0 = 1000
thermal_expansion = 0
viscosity = 1e-3
cv = 1e6
porepressure_coefficient = 0
[]
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
temperature = temp
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pressure
capillary_pressure = pc
[]
[massfrac]
type = PorousFlowMassFraction
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1E-15 0 0 0 1E-15 0 0 0 1E-15'
[]
[relperm]
type = PorousFlowRelativePermeabilityCorey # irrelevant in this fully-saturated situation
n = 2
phase = 0
[]
[]
[BCs]
[leftp]
type = DirichletBC
variable = pressure
boundary = left
value = 2E6
[]
[leftt]
type = DirichletBC
variable = temp
boundary = left
value = 100
[]
[newtonp]
type = PorousFlowPiecewiseLinearSink
variable = pressure
boundary = right
pt_vals = '0 100000 200000 300000 400000 500000 600000 700000 800000 900000 1000000 1100000 1200000 1300000 1400000 1500000 1600000 1700000 1800000 1900000 2000000'
multipliers = '0. 5.6677197748570516e-6 0.000011931518841831313 0.00001885408740732065 0.000026504708864284114 0.000034959953203725676 0.000044304443352900224 0.00005463170211001232 0.00006604508815181467 0.00007865883048198513 0.00009259917167338928 0.00010800563134618119 0.00012503240252705603 0.00014384989486488752 0.00016464644014777016 0.00018763017719085535 0.0002130311349595711 0.00024110353477682344 0.00027212833465544285 0.00030641604122040985 0.00034430981736352295'
use_mobility = false
use_relperm = false
fluid_phase = 0
flux_function = 1
[]
[newton]
type = PorousFlowPiecewiseLinearSink
variable = temp
boundary = right
pt_vals = '0 100000 200000 300000 400000 500000 600000 700000 800000 900000 1000000 1100000 1200000 1300000 1400000 1500000 1600000 1700000 1800000 1900000 2000000'
multipliers = '0. 5.6677197748570516e-6 0.000011931518841831313 0.00001885408740732065 0.000026504708864284114 0.000034959953203725676 0.000044304443352900224 0.00005463170211001232 0.00006604508815181467 0.00007865883048198513 0.00009259917167338928 0.00010800563134618119 0.00012503240252705603 0.00014384989486488752 0.00016464644014777016 0.00018763017719085535 0.0002130311349595711 0.00024110353477682344 0.00027212833465544285 0.00030641604122040985 0.00034430981736352295'
use_mobility = false
use_relperm = false
use_internal_energy = true
fluid_phase = 0
flux_function = 1
[]
[]
[VectorPostprocessors]
[porepressure]
type = LineValueSampler
variable = pressure
start_point = '0 0.5 0'
end_point = '100 0.5 0'
sort_by = x
num_points = 11
execute_on = timestep_end
[]
[temperature]
type = LineValueSampler
variable = temp
start_point = '0 0.5 0'
end_point = '100 0.5 0'
sort_by = x
num_points = 11
execute_on = timestep_end
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -snes_max_it -sub_pc_factor_shift_type -pc_asm_overlap -snes_atol -snes_rtol '
petsc_options_value = 'gmres asm lu 100 NONZERO 2 1E-8 1E-15'
[]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
file_base = nc06
execute_on = timestep_end
exodus = true
[along_line]
type = CSV
execute_vector_postprocessors_on = timestep_end
[]
[]
(test/tests/kernels/kernel_precompute/kernel_precompute_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
nz = 0
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
active = 'convected'
[./convected]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff conv'
[./diff]
type = DiffusionPrecompute
variable = convected
[../]
[./conv]
type = ConvectionPrecompute
variable = convected
velocity = '1.0 0.0 0.0'
[../]
[]
[BCs]
active = 'bottom top'
[./bottom]
type = DirichletBC
variable = convected
boundary = 'left'
value = 0
[../]
[./top]
type = DirichletBC
variable = convected
boundary = 'right'
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
file_base = out
exodus = true
[]
(test/tests/misc/save_in/diag_save_in_soln_var_err_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./saved]
[../]
[./bc_saved]
[../]
[./accumulated]
[../]
[./diag_saved]
[../]
[./bc_diag_saved]
[../]
[./saved_dirichlet]
[../]
[./diag_saved_dirichlet]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
save_in = 'saved accumulated saved_dirichlet'
diag_save_in = 'u diag_saved diag_saved_dirichlet'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
save_in = saved_dirichlet
diag_save_in = diag_saved_dirichlet
[../]
[./nbc]
type = NeumannBC
variable = u
boundary = right
value = 1
save_in = 'bc_saved accumulated'
diag_save_in = bc_diag_saved
[../]
[]
[Postprocessors]
[./left_flux]
type = NodalSum
variable = saved
boundary = 1
[../]
[./saved_norm]
type = NodalL2Norm
variable = saved
execute_on = timestep_end
block = 0
[../]
[./saved_dirichlet_norm]
type = NodalL2Norm
variable = saved_dirichlet
execute_on = timestep_end
block = 0
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/ray_tracing/test/tests/coord_type/rz_line_integral.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 5
ny = 2
xmin = 0
xmax = 2
ymin = 0
ymax = 1
[]
[]
[Variables/u]
[]
[BCs]
[fixed]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Kernels]
[diffusion]
type = Diffusion
variable = u
[]
[source]
type = BodyForce
variable = u
value = 10
[]
[]
[UserObjects]
[study]
type = RepeatableRayStudy
names = 'ray0 ray1'
start_points = '0 0.5 0
0 0.1 0'
end_points = '2.0 0.5 0
2.0 0.9 0'
[]
[]
[RayKernels]
[variable_integral]
type = VariableIntegralRayKernel
study = study
variable = u
[]
[]
[Postprocessors]
[ray0_value]
type = RayIntegralValue
ray_kernel = variable_integral
ray = ray0
[]
[ray1_value]
type = RayIntegralValue
ray_kernel = variable_integral
ray = ray1
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Problem]
coord_type = RZ
[]
[Outputs]
exodus = true
csv = true
[]
(test/tests/outputs/debug/show_top_residuals.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[./debug] # This is only a test, this should be turned on via the [Debug] block
type = TopResidualDebugOutput
num_residuals = 1
[../]
[]
(test/tests/kernels/array_kernels/array_diffusion_reaction.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 4
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
components = 2
[]
[]
[Kernels]
[diff]
type = ArrayDiffusion
variable = u
diffusion_coefficient = dc
[]
[reaction]
type = ArrayReaction
variable = u
reaction_coefficient = rc
[]
[]
[BCs]
[left]
type = ArrayDirichletBC
variable = u
boundary = 1
values = '0 0'
[]
[right]
type = ArrayDirichletBC
variable = u
boundary = 2
values = '1 2'
[]
[]
[Materials]
[dc]
type = GenericConstantArray
prop_name = dc
prop_value = '1 1'
[]
[rc]
type = GenericConstant2DArray
prop_name = rc
prop_value = '1 0; -0.1 1'
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(modules/level_set/test/tests/functions/olsson_bubble/olsson_bubble.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
[]
[Adaptivity]
initial_marker = marker
initial_steps = 2
max_h_level = 2
[./Markers]
[./marker]
type = BoxMarker
bottom_left = '0 0 0'
top_right = '0.5 0.5 0'
inside = REFINE
outside = DO_NOTHING
[../]
[../]
[]
[AuxVariables]
[./bubble]
[../]
[]
[AuxKernels]
[./bubble_aux]
type = FunctionAux
variable = bubble
function = bubble_func
execute_on = initial
[../]
[]
[Functions]
[./bubble_func]
type = LevelSetOlssonBubble
center = '0.25 0.25 0'
radius = 0.15
[../]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
execute_on = 'TIMESTEP_END'
exodus = true
[]
(modules/heat_conduction/test/tests/heat_conduction/3d_quadrature_gap_heat_transfer/second.i)
[Mesh]
file = nonmatching.e
second_order = true
[]
[Variables]
[./temp]
order = SECOND
[../]
[]
[Kernels]
[./hc]
type = HeatConduction
variable = temp
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = temp
boundary = leftleft
value = 1000
[../]
[./right]
type = DirichletBC
variable = temp
boundary = rightright
value = 400
[../]
[]
[ThermalContact]
[./left_to_right]
secondary = leftright
quadrature = true
primary = rightleft
variable = temp
emissivity_primary = 0
emissivity_secondary = 0
type = GapHeatTransfer
order = SECOND
[../]
[]
[Materials]
[./hcm]
type = HeatConductionMaterial
block = 'left right'
specific_heat = 1
thermal_conductivity = 1
[../]
[]
[Postprocessors]
[./left]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = leftright
diffusivity = thermal_conductivity
[../]
[./right]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = rightleft
diffusivity = thermal_conductivity
[../]
[]
[Executioner]
type = Steady
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/thermal_hydraulics/test/tests/postprocessors/function_element_integral_rz/err.rz_domain.i)
[Mesh]
[mg]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 2
[]
[]
[Problem]
coord_type = RSPHERICAL
[]
[Postprocessors]
[el_int]
type = FunctionElementIntegralRZ
axis_point = '0 0 0'
axis_dir = '0 1 0'
function = 1
execute_on = 'initial'
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
(modules/richards/test/tests/jacobian_1/jn03.i)
# unsaturated = false
# gravity = true
# supg = false
# transient = false
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = -1
xmax = 1
ymin = -1
ymax = 1
zmin = -1
zmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0 # notice small quantity, so the PETSc constant state works
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1 # notice small quantity, so the PETSc constant state works
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.2
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGnone]
type = RichardsSUPGnone
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = RandomIC
block = 0
min = 0
max = 1
[../]
[../]
[]
[Kernels]
active = 'richardsf'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGnone
sat_UO = Saturation
seff_UO = SeffVG
viscosity = 1E-3
gravity = '1 2 3'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -snes_type'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000 test'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = jn03
exodus = false
[]
(modules/fluid_properties/test/tests/functions/saturation_temperature_function/saturation_temperature_function.i)
# TestTwoPhaseFluidProperties has the following saturation temperature function:
# T_sat(p) = 2 p
# Thus for p = 5, T_sat should be 10.
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
[]
[Modules]
[./FluidProperties]
[./fp_liquid]
type = IdealGasFluidProperties
[../]
[./fp_vapor]
type = IdealGasFluidProperties
[../]
[./fp_2phase]
type = TestTwoPhaseFluidProperties
fp_liquid = fp_liquid
fp_vapor = fp_vapor
[../]
[]
[]
[Functions]
[./p]
type = ConstantFunction
value = 5
[../]
[./T_sat]
type = SaturationTemperatureFunction
p = p
fp_2phase = fp_2phase
[../]
[]
[Postprocessors]
[./T_sat_pp]
type = FunctionValuePostprocessor
function = T_sat
execute_on = 'INITIAL'
[../]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
[]
(test/tests/outputs/output_interface/marker.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Adaptivity]
[./Indicators]
[./indicator_0]
type = GradientJumpIndicator
variable = u
outputs = none
[../]
[./indicator_1]
type = GradientJumpIndicator
variable = u
outputs = none
[../]
[../]
[./Markers]
[./marker_0]
type = ValueThresholdMarker
outputs = markers
refine = 0.5
variable = u
[../]
[./marker_1]
type = BoxMarker
bottom_left = '0.25 0.25 0'
top_right = '0.75 0.75 0'
inside = REFINE
outside = DONT_MARK
outputs = markers
[../]
[../]
[]
[Outputs]
[./markers]
type = Exodus
[../]
[./no_markers]
type = Exodus
[../]
[]
(test/tests/mesh_modifiers/add_side_sets_from_bounding_box/multiple_boundary_ids.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[createNewSidesetOne]
type = SideSetsFromBoundingBoxGenerator
input = gen
block_id = 0
boundary_id_old = 'left bottom'
boundary_id_new = 10
bottom_left = '-0.1 -0.1 0'
top_right = '0.2 0.9 0'
[]
[createNewSidesetTwo]
type = SideSetsFromBoundingBoxGenerator
input = createNewSidesetOne
block_id = 0
boundary_id_old = 'right'
boundary_id_new = 11
bottom_left = '0.5 0.5 0'
top_right = '1.1 1.1 0'
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[leftBC]
type = DirichletBC
variable = u
boundary = 10
value = 1
[]
[rightBC]
type = DirichletBC
variable = u
boundary = 11
value = 0
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/peridynamics/test/tests/restart/2D_mesh_restartable_H1NOSPD_second.i)
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Problem]
restart_file_base = 2D_mesh_restartable_hnospd_out_cp/LATEST
[]
[Mesh]
file = 2D_mesh_restartable_hnospd_out_cp/LATEST
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[BCs]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = 1003
value = 0.0
[../]
[./left_y]
type = DirichletBC
variable = disp_y
boundary = 1003
value = 0.0
[../]
[./right_x]
type = DirichletBC
variable = disp_x
boundary = 1001
value = 0.001
[../]
[]
[Modules/Peridynamics/Mechanics/Master]
[./all]
formulation = NONORDINARY_STATE
stabilization = BOND_HORIZON_I
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 2.1e8
poissons_ratio = 0.3
[../]
[./strain]
type = ComputePlaneSmallStrainNOSPD
stabilization = BOND_HORIZON_I
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
[./Quadrature]
type = GAUSS_LOBATTO
order = FIRST
[../]
[]
[Outputs]
file_base = 2D_mesh_restartable_H1NOSPD_second_out
exodus = true
[]
(tutorials/tutorial01_app_development/step08_test_harness/test/tests/kernels/darcy_pressure/darcy_pressure_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[pressure]
[]
[]
[Kernels]
[diffusion]
type = DarcyPressure
variable = pressure
permeability = 0.8451e-09
[]
[]
[BCs]
[left]
type = ADDirichletBC
variable = pressure
boundary = left
value = 0
[]
[right]
type = ADDirichletBC
variable = pressure
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/ics/data_struct_ic/data_struct_ic_test.i)
[Mesh]
type = GeneratedMesh
nx = 10
ny = 10
dim = 2
# DataStructIC creates an IC based on node numbering
parallel_type = replicated
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[ICs]
[./ds_ic]
type = DataStructIC
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(test/tests/postprocessors/point_value/point_value_error.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Postprocessors]
[./value]
type = PointValue
variable = u
point = '14.371 .41 0'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/auxkernels/quotient_aux/quotient_aux.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[./v]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./ratio]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[AuxKernels]
[./ratio_auxkernel]
type = QuotientAux
variable = ratio
numerator = u
denominator = v
[../]
[]
[BCs]
[./left_u]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 2
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = 3
value = 2
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/mesh_modifiers/modifier_depend_order/modifier_depend_order.i)
[Mesh]
[file]
type = FileMeshGenerator
file = square.e
[]
# Mesh Modifiers
# If no dependencies are defined, the order of execution is not defined (based on pointer locations) so
# this test case has several dependencies to minimize the chance of getting lucky when things aren't defined properly.
# Rotations along different axes must occur in a defined order to end up at the right orientation at the end.
# The final mesh will be angled at 45 degrees with new sidesets where there were none before.
[add_side_sets]
type = SideSetsFromNormalsGenerator
input = last_rotate
normals = ' 0.70710678118 0.70710678118 0
-0.70710678118 -0.70710678118 0'
new_boundary = 'up_right down_left'
variance = 1e-3
fixed_normal = true
[]
[last_rotate]
type = TransformGenerator
input = rotate4
transform = ROTATE
vector_value = '-45 0 0'
[]
[rotate1]
type = TransformGenerator
input = file
transform = ROTATE
vector_value = '0 0 82'
[]
[rotate3]
type = TransformGenerator
input = rotate2
transform = ROTATE
vector_value = '0 36 0'
[]
[rotate4]
type = TransformGenerator
input = rotate3
transform = ROTATE
vector_value = '0 0 -82'
[]
[rotate2]
type = TransformGenerator
input = rotate1
transform = ROTATE
vector_value = '0 -36 0'
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[bottom]
type = DirichletBC
variable = u
boundary = down_left
value = 0
[]
[top]
type = DirichletBC
variable = u
boundary = up_right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/mixing_length_total_viscosity_material/steady-action.i)
von_karman_const = 0.41
H = 1 #halfwidth of the channel
L = 150
Re = 100
rho = 1
bulk_u = 1
mu = ${fparse rho * bulk_u * 2 * H / Re}
[Mesh]
[gen]
type = CartesianMeshGenerator
dim = 2
dx = '${L}'
dy = '0.667 0.333'
ix = '200'
iy = '10 1'
[]
[]
[Modules]
[NavierStokesFV]
compressibility = 'incompressible'
turbulence_handling = 'mixing-length'
density = ${rho}
dynamic_viscosity = ${mu}
initial_velocity = '1e-6 1e-6 0'
initial_pressure = 0.0
inlet_boundaries = 'left'
momentum_inlet_types = 'fixed-velocity'
momentum_inlet_function = '1 0'
wall_boundaries = 'top bottom'
momentum_wall_types = 'wallfunction symmetry'
outlet_boundaries = 'right'
momentum_outlet_types = 'fixed-pressure'
pressure_function = '0'
von_karman_const = ${von_karman_const}
mixing_length_delta = 0.5
mixing_length_walls = 'top'
mixing_length_aux_execute_on ='initial'
momentum_advection_interpolation = 'upwind'
mass_advection_interpolation = 'upwind'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 200 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(test/tests/actions/meta_action_multiple_tasks/circle_quads.i)
[Mesh]
file = circle-quads.e
[]
[Functions]
[./all_bc_fn]
type = ParsedFunction
value = x*x+y*y
[../]
[./f_fn]
type = ParsedFunction
value = -4
[../]
[./analytical_normal_x]
type = ParsedFunction
value = x
[../]
[./analytical_normal_y]
type = ParsedFunction
value = y
[../]
[]
# An Action that adds an Action that satisfies multiple tasks!
[MetaNodalNormals]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = f_fn
[../]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
boundary = '1'
function = 'all_bc_fn'
[../]
[]
[Postprocessors]
[./nx_pps]
type = NodalL2Error
variable = nodal_normal_x
boundary = '1'
function = analytical_normal_x
[../]
[./ny_pps]
type = NodalL2Error
variable = nodal_normal_y
boundary = '1'
function = analytical_normal_y
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
nl_rel_tol = 1e-13
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(modules/phase_field/test/tests/initial_conditions/ClosePackIC.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 5
ymax = .5
uniform_refine = 5
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./phi]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
[ICs]
[./close_pack]
radius = 0.07
outvalue = 0
variable = phi
invalue = 1
type = ClosePackIC
[../]
[]
(test/tests/misc/check_error/incomplete_fvkernel_variable_coverage_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
[./u]
order = CONSTANT
family = MONOMIAL
fv = true
[../]
[./v]
order = CONSTANT
family = MONOMIAL
fv = true
[../]
[]
[FVKernels]
active = 'diff body_force'
[./diff]
type = FVDiffusion
variable = u
coeff = 1
[../]
[./body_force]
type = FVBodyForce
variable = u
value = 10
[../]
[]
[FVBCs]
active = 'right'
[./left]
type = FVDirichletBC
variable = u
boundary = 3
value = 1
[../]
[./right]
type = FVDirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/xfem/test/tests/single_var_constraint_2d/equal_value.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 1
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.5 1.0 0.5 0.0'
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[Constraints]
[./xfem_constraint]
type = XFEMEqualValueAtInterface
geometric_cut_userobject = 'line_seg_cut_uo'
use_displaced_mesh = false
variable = u
value = 1
alpha = 1e5
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
l_tol = 1e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
[]
[Outputs]
interval = 1
execute_on = timestep_end
exodus = true
perf_graph = true
[./console]
type = Console
output_linear = true
[../]
[]
(test/tests/transfers/multiapp_high_order_variable_transfer/master_L2_Lagrange_userobject.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
parallel_type = replicated
[]
[Variables]
[power_density]
family = L2_LAGRANGE
order = FIRST
[]
[]
[AuxVariables]
[./multi_layered_average]
family = LAGRANGE
order = FIRST
[../]
[]
[UserObjects]
[./multi_layered_average]
type = LayeredAverage
variable = power_density
direction = y
num_layers = 4
[../]
[]
[AuxKernels]
[./layered_aux]
type = SpatialUserObjectAux
variable = multi_layered_average
execute_on = 'nonlinear TIMESTEP_END'
user_object = multi_layered_average
[../]
[]
[Functions]
[pwr_func]
type = ParsedFunction
value = '1e3*x*(1-x)+5e2'
[]
[]
[Kernels]
[diff]
type = Reaction
variable = power_density
[]
[coupledforce]
type = BodyForce
variable = power_density
function = pwr_func
[]
[]
[Postprocessors]
[layered_avg]
type = ElementAverageValue
block = '0'
variable = multi_layered_average
execute_on = 'initial timestep_end'
[]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart '
petsc_options_value = 'hypre boomeramg 100'
nl_abs_tol = 1e-8
nl_rel_tol = 1e-12
[]
[MultiApps]
[sub]
type = FullSolveMultiApp
app_type = MooseTestApp
positions = '0 0 0'
input_files = sub_L2_Lagrange.i
execute_on = 'timestep_end'
[]
[]
[Transfers]
[p_to_sub]
type = MultiAppUserObjectTransfer
user_object = multi_layered_average
variable = power_density
to_multi_app = sub
execute_on = 'timestep_end'
[]
[]
[Outputs]
exodus = true
perf_graph = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/lid_driven/ad_lid_driven_stabilized.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
nx = 64
ny = 64
[]
[./corner_node]
type = ExtraNodesetGenerator
new_boundary = 'pinned_node'
nodes = '0'
input = gen
[../]
[]
[AuxVariables]
[vel_x]
[]
[vel_y]
[]
[]
[AuxKernels]
[vel_x]
type = VectorVariableComponentAux
variable = vel_x
vector_variable = velocity
component = 'x'
[]
[vel_y]
type = VectorVariableComponentAux
variable = vel_y
vector_variable = velocity
component = 'y'
[]
[]
[Variables]
[./velocity]
family = LAGRANGE_VEC
[../]
[./p]
[../]
[]
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[./mass_pspg]
type = INSADMassPSPG
variable = p
[../]
[./momentum_convection]
type = INSADMomentumAdvection
variable = velocity
[../]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
integrate_p_by_parts = true
[../]
[./momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[../]
[]
[BCs]
[./no_slip]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom right left'
[../]
[./lid]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'top'
function_x = 'lid_function'
[../]
[./pressure_pin]
type = DirichletBC
variable = p
boundary = 'pinned_node'
value = 0
[../]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[ins_mat]
type = INSADTauMaterial
velocity = velocity
pressure = p
alpha = .1
[]
[]
[Functions]
[./lid_function]
# We pick a function that is exactly represented in the velocity
# space so that the Dirichlet conditions are the same regardless
# of the mesh spacing.
type = ParsedFunction
value = '4*x*(1-x)'
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
line_search = 'none'
nl_rel_tol = 1e-12
nl_abs_tol = 1e-13
nl_max_its = 6
l_tol = 1e-6
l_max_its = 500
[]
[Outputs]
exodus = true
file_base = lid_driven_stabilized_out
[]
[Postprocessors]
[lin]
type = NumLinearIterations
[]
[nl]
type = NumNonlinearIterations
[]
[lin_tot]
type = CumulativeValuePostprocessor
postprocessor = 'lin'
[]
[nl_tot]
type = CumulativeValuePostprocessor
postprocessor = 'nl'
[]
[]
(modules/tensor_mechanics/test/tests/elasticitytensor/composite.i)
# This input file is designed to test the RankTwoAux and RankFourAux
# auxkernels, which report values out of the Tensors used in materials
# properties.
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
xmax = 1
[]
[AuxVariables]
[./c]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = x
[../]
[../]
[./C1111_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./C1122_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./C1133_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./C3313_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./dC1111_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./dC1122_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./dC1133_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./dC3313_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./d2C1111_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./d2C1122_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./d2C1133_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./d2C3313_aux]
order = CONSTANT
family = MONOMIAL
[../]
[]
#[Kernels]
# [./diff]
# type = Diffusion
# variable = diffused
# [../]
#[]
[AuxKernels]
[./matl_C1111]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 0
variable = C1111_aux
execute_on = initial
[../]
[./matl_C1122]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 1
index_l = 1
variable = C1122_aux
execute_on = initial
[../]
[./matl_C1133]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 2
index_l = 2
variable = C1133_aux
execute_on = initial
[../]
[./matl_C3313]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 0
index_l = 2
variable = C3313_aux
execute_on = initial
[../]
[./matl_dC1111]
type = RankFourAux
rank_four_tensor = delasticity_tensor/dc
index_i = 0
index_j = 0
index_k = 0
index_l = 0
variable = dC1111_aux
execute_on = initial
[../]
[./matl_dC1122]
type = RankFourAux
rank_four_tensor = delasticity_tensor/dc
index_i = 0
index_j = 0
index_k = 1
index_l = 1
variable = dC1122_aux
execute_on = initial
[../]
[./matl_dC1133]
type = RankFourAux
rank_four_tensor = delasticity_tensor/dc
index_i = 0
index_j = 0
index_k = 2
index_l = 2
variable = dC1133_aux
execute_on = initial
[../]
[./matl_dC3313]
type = RankFourAux
rank_four_tensor = delasticity_tensor/dc
index_i = 2
index_j = 2
index_k = 0
index_l = 2
variable = dC3313_aux
execute_on = initial
[../]
[./matl_d2C1111]
type = RankFourAux
rank_four_tensor = d^2elasticity_tensor/dc^2
index_i = 0
index_j = 0
index_k = 0
index_l = 0
variable = d2C1111_aux
execute_on = initial
[../]
[./matl_d2C1122]
type = RankFourAux
rank_four_tensor = d^2elasticity_tensor/dc^2
index_i = 0
index_j = 0
index_k = 1
index_l = 1
variable = d2C1122_aux
execute_on = initial
[../]
[./matl_d2C1133]
type = RankFourAux
rank_four_tensor = d^2elasticity_tensor/dc^2
index_i = 0
index_j = 0
index_k = 2
index_l = 2
variable = d2C1133_aux
execute_on = initial
[../]
[./matl_d2C3313]
type = RankFourAux
rank_four_tensor = d^2elasticity_tensor/dc^2
index_i = 2
index_j = 2
index_k = 0
index_l = 2
variable = d2C3313_aux
execute_on = initial
[../]
[]
[Materials]
[./Ca]
type = ComputeElasticityTensor
base_name = Ca
block = 0
fill_method = symmetric21
C_ijkl ='1111 .1122 1133 1123 1113 1112 2222 2233 2223 2213 2212 3333 3323 3313 3312 2323 2313 2312 1313 1312 1212'
[../]
[./Cb]
type = ComputeElasticityTensor
base_name = Cb
block = 0
fill_method = symmetric21
C_ijkl ='.1111 1122 .1133 .1123 .1113 .1112 .2222 .2233 .2223 .2213 .2212 .3333 .3323 .3313 .3312 .2323 .2313 .2312 .1313 .1312 .1212'
[../]
[./Fa]
type = DerivativeParsedMaterial
block = 0
f_name = Fa
function = c^2
args = c
[../]
[./Fb]
type = DerivativeParsedMaterial
block = 0
f_name = Fb
function = (1-c)^3
args = c
[../]
[./C]
type = CompositeElasticityTensor
block = 0
args = c
tensors = 'Ca Cb'
weights = 'Fa Fb'
[../]
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/ray_tracing/test/tests/base/ray_tracing_object/errors.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
[]
[]
[UserObjects/study]
type = RayTracingStudyTest
[]
[RayKernels/test]
type = RayTracingObjectTest
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
(test/tests/fvkernels/mms/advection-diffusion.i)
diff=1.1
a=1.1
[GlobalParams]
advected_interp_method = 'average'
[]
[Mesh]
[./gen_mesh]
type = GeneratedMeshGenerator
dim = 1
xmin = -0.6
xmax = 0.6
nx = 64
[../]
[]
[Variables]
[./v]
family = MONOMIAL
order = CONSTANT
fv = true
[../]
[]
[FVKernels]
[./advection]
type = FVAdvection
variable = v
velocity = '${a} 0 0'
[../]
[./diffusion]
type = FVDiffusion
variable = v
coeff = coeff
[../]
[body_v]
type = FVBodyForce
variable = v
function = 'forcing'
[]
[]
[FVBCs]
[boundary]
type = FVFunctionDirichletBC
boundary = 'left right'
function = 'exact'
variable = v
[]
[]
[Materials]
[diff]
type = ADGenericFunctorMaterial
prop_names = 'coeff'
prop_values = '${diff}'
[]
[]
[Functions]
[exact]
type = ParsedFunction
value = '3*x^2 + 2*x + 1'
[]
[forcing]
type = ParsedFunction
value = '-${diff}*6 + ${a} * (6*x + 2)'
# value = '-${diff}*6'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[./error]
type = ElementL2Error
variable = v
function = exact
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/lid-driven/rz-gravity-quiescent-fluid.i)
mu=.01
rho=1
[GlobalParams]
velocity_interp_method = 'rc'
advected_interp_method = 'average'
two_term_boundary_expansion = true
rhie_chow_user_object = 'rc'
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 1
xmax = 2
ymin = 0
ymax = 1
nx = 10
ny = 10
[]
[]
[Problem]
coord_type = 'RZ'
[]
[Variables]
[u]
type = INSFVVelocityVariable
[]
[v]
type = INSFVVelocityVariable
[]
[pressure]
type = INSFVPressureVariable
[]
[lambda]
family = SCALAR
order = FIRST
[]
[]
[AuxVariables]
[U]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[]
[AuxKernels]
[mag]
type = VectorMagnitudeAux
variable = U
x = u
y = v
[]
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
rho = ${rho}
[]
[mean_zero_pressure]
type = FVScalarLagrangeMultiplier
variable = pressure
lambda = lambda
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = 'mu'
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[u_gravity]
type = INSFVMomentumGravity
variable = u
momentum_component = 'x'
rho = ${rho}
gravity = '0 -1 0'
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = 'mu'
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[v_gravity]
type = INSFVMomentumGravity
variable = v
momentum_component = 'y'
rho = ${rho}
gravity = '0 -1 0'
[]
[]
[FVBCs]
[free_slip_x]
type = INSFVNaturalFreeSlipBC
variable = u
boundary = 'left right top bottom'
momentum_component = 'x'
[]
[free_slip_y]
type = INSFVNaturalFreeSlipBC
variable = v
boundary = 'left right top bottom'
momentum_component = 'y'
[]
[]
[Materials]
[mu]
type = ADGenericFunctorMaterial
prop_names = 'mu'
prop_values = '${mu}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/variables/show_hide.i)
# Solving for 2 variables, putting one into hide list and the other one into show list
# We should only see the variable that is in show list in the output.
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
elem_type = QUAD4
[]
[Functions]
[./bc_fn]
type = ParsedFunction
value = x
[../]
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[BCs]
[./lr_u]
type = FunctionDirichletBC
variable = u
boundary = '1 3'
function = bc_fn
[../]
[./lr_v]
type = FunctionDirichletBC
variable = v
boundary = '1 3'
function = bc_fn
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
console = true
[./out]
type = Exodus
show = 'u'
hide = 'v'
[../]
[]
(test/tests/restart/restart_transient_from_steady/steady.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[../]
[]
[Postprocessors]
[./unorm]
type = ElementL2Norm
variable = u
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
checkpoint = true
[]
(test/tests/restart/restartable_types/restartable_types.i)
###########################################################
# This is a simple test of the restart/recover capability.
# The test object "RestartableTypesChecker" is used
# to reload data from a previous simulation written out
# with the object "RestartableTypes".
#
# See "restartable_types2.i"
#
# @Requirement F1.60
###########################################################
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[UserObjects]
[./restartable_types]
type = RestartableTypes
[../]
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[./out]
type = Checkpoint
num_files = 1
[../]
[]
(modules/combined/test/tests/concentration_dependent_elasticity_tensor/concentration_dependent_elasticity_tensor.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
xmin = -0.5
ymin = -0.5
xmax = 0.5
ymax = 0.5
elem_type = QUAD4
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./TensorMechanics]
disp_x = disp_x
disp_y = disp_y
[../]
[]
[AuxVariables]
[./c]
[../]
[./C11_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./s11_aux]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./matl_s11]
type = RankTwoAux
variable = s11_aux
rank_two_tensor = stress
index_i = 0
index_j = 0
[../]
[./matl_C11]
type = RankFourAux
variable = C11_aux
rank_four_tensor = elasticity_tensor
index_l = 0
index_j = 0
index_k = 0
index_i = 0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeConcentrationDependentElasticityTensor
block = 0
c = c
C1_ijkl = '6 6'
C0_ijkl = '1 1'
fill_method1 = symmetric_isotropic
fill_method0 = symmetric_isotropic
[../]
[./stress]
type = ComputeLinearElasticStress
block = 0
[../]
[./strain]
type = ComputeSmallStrain
block = 0
disp_x = disp_x
disp_y = disp_y
[../]
[]
[BCs]
[./bottom_y]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0
[../]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = left
value = 0
[../]
[./right_x]
type = DirichletBC
variable = disp_x
boundary = right
value = 0
[../]
[./top_y]
type = DirichletBC
variable = disp_y
boundary = top
value = 0.5
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart'
petsc_options_value = 'hypre boomeramg 31'
l_max_its = 20
nl_max_its = 10
l_tol = 1.0e-4
nl_rel_tol = 1.0e-6
nl_abs_tol = 1.0e-8
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
[ICs]
[./c_IC]
int_width = 0.2
x1 = 0
y1 = 0
radius = 0.25
outvalue = 0
variable = c
invalue = 1
type = SmoothCircleIC
[../]
[]
(test/tests/fvkernels/constraints/point_value.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 4
[]
[Variables]
[v]
type = MooseVariableFVReal
[]
[lambda]
type = MooseVariableScalar
[]
[]
[FVKernels]
[diff]
type = FVDiffusion
variable = v
coeff = coeff
[]
[average]
type = FVPointValueConstraint
variable = v
phi0 = 13
lambda = lambda
point = '0.3 0 0'
[]
[]
[FVBCs]
[left]
type = FVDirichletBC
variable = v
boundary = left
value = 7
[]
[]
[Materials]
[diff]
type = ADGenericFunctorMaterial
prop_names = 'coeff'
prop_values = '1'
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
[]
[Outputs]
exodus = true
[]
(test/tests/kernels/diffusion_with_hanging_node/ad_simple_diffusion.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 1
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = ADDiffusion
variable = u
[../]
[force]
type = ADBodyForce
variable = u
function = '0'
[]
[]
[BCs]
# BCs cannot be preset due to Jacobian test
[./left]
type = DirichletBC
preset = false
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
preset = false
variable = u
boundary = right
value = 1
[../]
[]
[Preconditioning]
[./pre]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options = '-pc_svd_monitor'
petsc_options_iname = '-pc_type'
petsc_options_value = 'svd'
[]
[Outputs]
exodus = true
[]
[Adaptivity]
marker = box
max_h_level = 1
initial_steps = 1
[./Markers]
[./box]
type = BoxMarker
bottom_left = '0.5 0 0'
top_right = '1 1 0'
inside = 'refine'
outside = 'do_nothing'
[../]
[../]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/mms/skew-correction/skewed-vortex-action.i)
mu=1.0
rho=1.0
[Mesh]
[gen_mesh]
type = FileMeshGenerator
file = skewed.msh
[]
[]
[Modules]
[NavierStokesFV]
compressibility = 'incompressible'
density = 'rho'
dynamic_viscosity = 'mu'
wall_boundaries = 'top left right bottom'
momentum_wall_types = 'noslip noslip noslip noslip'
initial_velocity = '1 1 0'
pin_pressure = true
pinned_pressure_type = average
pinned_pressure_value = 0
momentum_face_interpolation = skewness-corrected
pressure_face_interpolation = skewness-corrected
momentum_advection_interpolation = skewness-corrected
mass_advection_interpolation = skewness-corrected
[]
[]
[FVKernels]
[u_forcing]
type = INSFVBodyForce
variable = vel_x
functor = forcing_u
momentum_component = 'x'
rhie_chow_user_object = 'ins_rhie_chow_interpolator'
[]
[v_forcing]
type = INSFVBodyForce
variable = vel_y
functor = forcing_v
momentum_component = 'y'
rhie_chow_user_object = 'ins_rhie_chow_interpolator'
[]
[]
[Materials]
[const]
type = ADGenericFunctorMaterial
prop_names = 'rho mu'
prop_values = '${rho} ${mu}'
[]
[]
[Functions]
[exact_u]
type = ParsedFunction
value = 'x^2*(1-x)^2*(2*y-6*y^2+4*y^3)'
[]
[exact_v]
type = ParsedFunction
value = '-y^2*(1-y)^2*(2*x-6*x^2+4*x^3)'
[]
[exact_p]
type = ParsedFunction
value = 'x*(1-x)-2/12'
[]
[forcing_u]
type = ADParsedFunction
value = '-4*mu/rho*(-1+2*y)*(y^2-6*x*y^2+6*x^2*y^2-y+6*x*y-6*x^2*y+3*x^2-6*x^3+3*x^4)+1-2*x+4*x^3*y^2*(2*y^2-2*y+1)*(y-1)^2*(-1+2*x)*(x-1)^3'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[forcing_v]
type = ADParsedFunction
value = '4*mu/rho*(-1+2*x)*(x^2-6*y*x^2+6*x^2*y^2-x+6*x*y-6*x*y^2+3*y^2-6*y^3+3*y^4)+4*y^3*x^2*(2*x^2-2*x+1)*(x-1)^2*(-1+2*y)*(y-1)^3'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'bjacobi 30 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-8
[]
[Outputs]
[out]
type = Exodus
hide = lambda
[]
csv = true
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2u]
type = ElementL2Error
variable = vel_x
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2v]
type = ElementL2Error
variable = vel_y
function = exact_v
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2p]
variable = pressure
function = exact_p
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(modules/porous_flow/test/tests/newton_cooling/nc02.i)
# Newton cooling from a bar. 1-phase steady
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1000
ny = 1
xmin = 0
xmax = 100
ymin = 0
ymax = 1
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pressure'
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureVG
m = 0.8
alpha = 1e-5
[]
[]
[Variables]
[pressure]
[]
[]
[ICs]
[pressure]
type = FunctionIC
variable = pressure
function = '(2-x/100)*1E6'
[]
[]
[Kernels]
[flux]
type = PorousFlowAdvectiveFlux
fluid_component = 0
gravity = '0 0 0'
variable = pressure
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 1e6
density0 = 1000
thermal_expansion = 0
viscosity = 1e-3
[]
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pressure
capillary_pressure = pc
[]
[massfrac]
type = PorousFlowMassFraction
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[porosity]
type = PorousFlowPorosityConst
porosity = 0.1
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1E-15 0 0 0 1E-15 0 0 0 1E-15'
[]
[relperm]
type = PorousFlowRelativePermeabilityCorey # irrelevant in this fully-saturated situation
n = 2
phase = 0
[]
[]
[BCs]
[left]
type = DirichletBC
variable = pressure
boundary = left
value = 2E6
[]
[newton]
type = PorousFlowPiecewiseLinearSink
variable = pressure
boundary = right
pt_vals = '0 100000 200000 300000 400000 500000 600000 700000 800000 900000 1000000 1100000 1200000 1300000 1400000 1500000 1600000 1700000 1800000 1900000 2000000'
multipliers = '0. 5.6677197748570516e-6 0.000011931518841831313 0.00001885408740732065 0.000026504708864284114 0.000034959953203725676 0.000044304443352900224 0.00005463170211001232 0.00006604508815181467 0.00007865883048198513 0.00009259917167338928 0.00010800563134618119 0.00012503240252705603 0.00014384989486488752 0.00016464644014777016 0.00018763017719085535 0.0002130311349595711 0.00024110353477682344 0.00027212833465544285 0.00030641604122040985 0.00034430981736352295'
use_mobility = false
use_relperm = false
fluid_phase = 0
flux_function = 1
[]
[]
[VectorPostprocessors]
[porepressure]
type = LineValueSampler
variable = pressure
start_point = '0 0.5 0'
end_point = '100 0.5 0'
sort_by = x
num_points = 20
execute_on = timestep_end
[]
[]
[Preconditioning]
active = 'andy'
[andy]
type = SMP
full = true
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -snes_max_it -sub_pc_factor_shift_type -pc_asm_overlap -snes_atol -snes_rtol '
petsc_options_value = 'gmres asm lu 100 NONZERO 2 1E-12 1E-15'
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
file_base = nc02
execute_on = timestep_end
exodus = false
[along_line]
type = CSV
execute_vector_postprocessors_on = timestep_end
[]
[]
(modules/ray_tracing/test/tests/raykernels/variable_integral_ray_kernel/simple_diffusion_line_integral.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 5
ny = 5
xmax = 5
ymax = 5
[]
[]
[Variables/u]
[]
[Kernels/diff]
type = Diffusion
variable = u
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = false
csv = true
[rays]
type = RayTracingExodus
study = study
output_data = false # enable for data output
output_data_nodal = false # enable for nodal data output
execute_on = NONE # TIMESTEP_END for Ray mesh output
[]
[]
[UserObjects/study]
type = RepeatableRayStudy
names = 'diag
right_up'
start_points = '0 0 0
5 0 0'
end_points = '5 5 0
5 5 0'
execute_on = TIMESTEP_END
# Needed to cache trace information for RayTracingMeshOutput
# always_cache_traces = true
# Needed to cache Ray data for RayTracingMeshOutput
# data_on_cache_traces = true
[]
[RayKernels/u_integral]
type = VariableIntegralRayKernel
variable = u
[]
[Postprocessors]
[diag_line_integral]
type = RayIntegralValue
ray_kernel = u_integral
ray = diag
[]
[right_up_line_integral]
type = RayIntegralValue
ray_kernel = u_integral
ray = right_up
[]
[]
(test/tests/markers/error_fraction_marker/error_fraction_marker_fv.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[u]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[]
[Functions]
[solution]
type = ParsedFunction
value = (exp(x)-1)/(exp(1)-1)
[]
[]
[FVKernels]
[diff]
type = FVDiffusion
variable = u
coeff = coeff
[]
[conv]
type = FVAdvection
variable = u
velocity = '1 0 0'
[]
[]
[FVBCs]
[left]
type = FVDirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = FVDirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Materials]
[diff]
type = ADGenericFunctorMaterial
prop_names = 'coeff'
prop_values = '1'
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Adaptivity]
[Indicators]
[error]
type = AnalyticalIndicator
variable = u
function = solution
[]
[]
[Markers]
[marker]
type = ErrorFractionMarker
coarsen = 0.1
indicator = error
refine = 0.3
[]
[]
[]
[Outputs]
exodus = true
[]
(test/tests/mortar/continuity-2d-conforming/conforming-2nd-order.i)
[Mesh]
[file]
type = FileMeshGenerator
file = 2blk-conf-2nd.e
[]
[secondary]
input = file
type = LowerDBlockFromSidesetGenerator
sidesets = '101'
new_block_id = '10001'
new_block_name = 'secondary_lower'
[]
[primary]
input = secondary
type = LowerDBlockFromSidesetGenerator
sidesets = '100'
new_block_id = '10000'
new_block_name = 'primary_lower'
[]
[]
[Problem]
kernel_coverage_check = false
[]
[Functions]
[./exact_sln]
type = ParsedFunction
value = x*x+y*y
[../]
[./ffn]
type = ParsedFunction
value = -4
[../]
[]
[Variables]
[./u]
order = SECOND
family = LAGRANGE
block = '1 2'
[../]
[./lm]
order = SECOND
family = LAGRANGE
block = secondary_lower
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = ffn
[../]
[]
[Constraints]
[./ced]
type = EqualValueConstraint
variable = lm
secondary_variable = u
primary_boundary = 100
primary_subdomain = 10000
secondary_boundary = 101
secondary_subdomain = 10001
[../]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
boundary = '1 2 3 4'
function = exact_sln
[../]
[]
[Postprocessors]
[./l2_error]
type = ElementL2Error
variable = u
function = exact_sln
block = '1 2'
execute_on = 'initial timestep_end'
[../]
[]
[Preconditioning]
[./fmp]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-14
l_tol = 1e-14
[]
[Outputs]
exodus = true
[]
(test/tests/userobjects/function_layered_integral/function_layered_integral.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 20
nz = 2
[]
[Problem]
type = FEProblem
solve = false
[]
[AuxVariables]
[layered_integral]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[liaux]
type = SpatialUserObjectAux
variable = layered_integral
execute_on = timestep_end
user_object = layered_integral
[]
[]
[UserObjects]
# the results of the layered integral are directly compared against the analytic integral
# of sin(y) from a to b, or cos(a) - cos(b)
[layered_integral]
type = FunctionLayeredIntegral
direction = y
num_layers = 20
function = 'sin(y)'
[]
[]
[VectorPostprocessors]
[li]
type = SpatialUserObjectVectorPostprocessor
userobject = layered_integral
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
csv = true
[]
(test/tests/materials/derivative_material_interface/ad_multiblock.i)
[Mesh]
type = FileMesh
file = rectangle.e
[]
[Variables]
[./c]
[../]
[]
[Materials]
[./mat1]
type = ADDefaultMatPropConsumerMaterial
block = 1
[../]
[./mat2]
type = ADDefaultMatPropConsumerMaterial
block = 2
[../]
[./mat1b]
type = ADDefaultMatPropConsumerMaterial
mat_prop = prop2
block = 1
[../]
[./mat2b]
type = ADDefaultMatPropConsumerMaterial
mat_prop = prop2
block = 2
[../]
[./generic]
type = ADGenericConstantMaterial
block = '1 2'
prop_names = prop3
prop_values = 9
[../]
[./mat1c]
type = ADDefaultMatPropConsumerMaterial
mat_prop = prop3
block = 1
[../]
[./mat2c]
type = ADDefaultMatPropConsumerMaterial
mat_prop = prop3
block = 2
[../]
[]
[Kernels]
[./kern1]
type = ADDefaultMatPropConsumerKernel
variable = c
block = 1
[../]
[./kern2]
type = ADDefaultMatPropConsumerKernel
variable = c
block = 2
[../]
[./kern1b]
type = ADDefaultMatPropConsumerKernel
variable = c
mat_prop = prop3
block = 1
[../]
[./kern2b]
type = ADDefaultMatPropConsumerKernel
variable = c
mat_prop = prop3
block = 2
[../]
[]
[Executioner]
type = Steady
[]
[Debug]
show_material_props = true
[]
[Problem]
solve = false
[]
[Outputs]
exodus = true
[]
(test/tests/transfers/multiapp_conservative_transfer/sub_power_density.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0.01 # to make sure the meshes don't align
xmax = 0.49 # to make sure the meshes don't align
ymax = 1
nx = 10
ny = 10
[]
[block1]
input = gen
type = SubdomainBoundingBoxGenerator
block_id = 1
bottom_left = '0.2 0.2 0'
top_right = '0.3 0.8 0'
[]
[]
[Variables]
[sink]
family = MONOMIAL
order = CONSTANT
[]
[]
[Functions]
[sink_func]
type = ParsedFunction
value = '5e2*x*(0.5-x)+5e1'
[]
[]
[Kernels]
[reaction]
type = Reaction
variable = sink
[]
[coupledforce]
type = BodyForce
variable = sink
function = sink_func
[]
[]
[AuxVariables]
[from_master]
block = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Postprocessors]
[sink]
type = ElementIntegralVariablePostprocessor
block = 1
variable = sink
[]
[from_master_pp]
type = ElementIntegralVariablePostprocessor
block = 1
variable = from_master
execute_on = 'transfer'
[]
[]
[Outputs]
exodus = true
[]
(test/tests/transfers/multiapp_conservative_transfer/master_power_density.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmax = 1
ymax = 1
nx = 10
ny = 10
[]
[block1]
input = gen
type = SubdomainBoundingBoxGenerator
block_id = 1
bottom_left = '0.5 0 0'
top_right = '1 1 0'
[]
[]
[Variables]
[power_density]
[]
[]
[Functions]
[pwr_func]
type = ParsedFunction
value = '1e3*x*(1-x)+5e2'
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = power_density
[]
[coupledforce]
type = BodyForce
variable = power_density
function = pwr_func
[]
[]
[BCs]
[left]
type = DirichletBC
variable = power_density
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = power_density
boundary = right
value = 1e3
[]
[]
[AuxVariables]
[from_sub]
[]
[]
[Postprocessors]
[pwr0]
type = ElementIntegralVariablePostprocessor
block = 0
variable = power_density
[]
[pwr1]
type = ElementIntegralVariablePostprocessor
block = 1
variable = power_density
[]
[from_sub0]
type = ElementIntegralVariablePostprocessor
block = 0
variable = from_sub
execute_on = 'transfer'
[]
[from_sub1]
type = ElementIntegralVariablePostprocessor
block = 1
variable = from_sub
execute_on = 'transfer'
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[MultiApps]
[sub]
type = FullSolveMultiApp
input_files = sub_power_density.i
positions = '0 0 0 0.5 0 0'
execute_on = timestep_end
[]
[]
[Transfers]
[to_sub]
type = MultiAppMeshFunctionTransfer
source_variable = power_density
variable = from_master
to_multi_app = sub
execute_on = timestep_end
# The following inputs specify what postprocessors should be conserved
# N pps are specified on the master side, where N is the number of subapps
# 1 pp is specified on the subapp side
from_postprocessors_to_be_preserved = 'pwr0 pwr1'
to_postprocessors_to_be_preserved = 'from_master_pp'
[]
[from_sub]
type = MultiAppMeshFunctionTransfer
source_variable = sink
variable = from_sub
from_multi_app = sub
execute_on = timestep_end
# The following inputs specify what postprocessors should be conserved
# N pps are specified on the master side, where N is the number of subapps
# 1 pp is specified on the subapp side
to_postprocessors_to_be_preserved = 'from_sub0 from_sub1'
from_postprocessors_to_be_preserved = 'sink'
[]
[]
[Outputs]
exodus = true
[]
(test/tests/misc/deprecation/deprecation.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
(test/tests/controls/syntax_based_naming_access/object_param.i)
[Mesh]
type = GeneratedMesh
dim = 2
elem_type = QUAD4
# use odd numbers so points do not fall on element boundaries
nx = 31
ny = 31
[]
[Variables]
[./diffused]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = diffused
[../]
[]
[DiracKernels]
[./test_object]
type = MaterialPointSource
point = '0.5 0.5 0'
variable = diffused
[../]
[]
[BCs]
[./bottom_diffused]
type = DirichletBC
variable = diffused
boundary = 'bottom'
value = 2
[../]
[./top_diffused]
type = DirichletBC
variable = diffused
boundary = 'top'
value = 0
[../]
[]
[Materials]
[./mat]
type = GenericConstantMaterial
prop_names = 'matp'
prop_values = '1'
block = 0
[../]
[]
[Postprocessors]
[./test_object]
type = FunctionValuePostprocessor
function = '2*(x+y)'
point = '0.5 0.5 0'
[../]
[./other_point_test_object]
type = FunctionValuePostprocessor
function = '3*(x+y)'
point = '0.5 0.5 0'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
[Controls]
[./point_control]
type = TestControl
test_type = 'point'
parameter = '*/test_object/point'
execute_on = 'initial'
[../]
[]
(test/tests/kernels/vector_fe/coupled_scalar_vector.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
xmin = -1
ymin = -1
elem_type = QUAD9
[]
[Variables]
[./u]
family = NEDELEC_ONE
order = FIRST
[../]
[./v]
[../]
[]
[Kernels]
[./wave]
type = VectorFEWave
variable = u
x_forcing_func = 'x_ffn'
y_forcing_func = 'y_ffn'
[../]
[./diff]
type = Diffusion
variable = v
[../]
[./source]
type = BodyForce
variable = v
[../]
[./advection]
type = EFieldAdvection
variable = v
efield = u
charge = 'positive'
mobility = 100
[../]
[]
[BCs]
[./bnd]
type = VectorCurlPenaltyDirichletBC
boundary = 'left right top bottom'
penalty = 1e10
function_x = 'x_sln'
function_y = 'y_sln'
variable = u
[../]
[./bnd_v]
type = DirichletBC
boundary = 'left right top bottom'
value = 0
variable = v
[../]
[]
[Functions]
[./x_ffn]
type = ParsedFunction
value = '(2*pi*pi + 1)*cos(pi*x)*sin(pi*y)'
[../]
[./y_ffn]
type = ParsedFunction
value = '-(2*pi*pi + 1)*sin(pi*x)*cos(pi*y)'
[../]
[./x_sln]
type = ParsedFunction
value = 'cos(pi*x)*sin(pi*y)'
[../]
[./y_sln]
type = ParsedFunction
value = '-sin(pi*x)*cos(pi*y)'
[../]
[]
[Preconditioning]
[./pre]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type'
petsc_options_value = 'asm'
petsc_options = '-snes_converged_reason -ksp_converged_reason -snes_linesearch_monitor'
[]
[Outputs]
exodus = true
[]
(modules/chemical_reactions/test/tests/jacobian/coupled_diffreact2.i)
# Test the Jacobian terms for the CoupledDiffusionReactionSub Kernel using
# activity coefficients not equal to unity
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
[./a]
order = FIRST
family = LAGRANGE
[../]
[./b]
order = FIRST
family = LAGRANGE
[../]
[./pressure]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./pressure]
type = RandomIC
variable = pressure
min = 1
max = 5
[../]
[./a]
type = RandomIC
variable = a
max = 1
min = 0
[../]
[./b]
type = RandomIC
variable = b
max = 1
min = 0
[../]
[]
[Kernels]
[./diff]
type = DarcyFluxPressure
variable = pressure
[../]
[./diff_b]
type = Diffusion
variable = b
[../]
[./a1diff]
type = CoupledDiffusionReactionSub
variable = a
v = b
log_k = 2
weight = 2
sto_v = 1.5
sto_u = 2
gamma_eq = 2
gamma_u = 2.5
gamma_v = 1.5
[../]
[]
[Materials]
[./porous]
type = GenericConstantMaterial
prop_names = 'diffusivity conductivity porosity'
prop_values = '1e-4 1e-4 0.2'
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
perf_graph = true
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
(modules/ray_tracing/test/tests/outputs/ray_tracing_mesh_output/ray_mesh_output_3d.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 3
nx = 5
ny = 5
nz = 5
xmax = 5
ymax = 5
zmax = 5
elem_type = HEX8
[]
[middle_block]
type = SubdomainBoundingBoxGenerator
input = gmg
block_id = 1
bottom_left = '2 0 0'
top_right = '3 5 5'
[]
[middle_block_sideset]
type = SideSetsBetweenSubdomainsGenerator
input = middle_block
primary_block = 1
paired_block = 0
new_boundary = 7
[]
[]
[RayBCs]
[kill]
type = 'KillRayBC'
boundary = 'top right front left'
rays = 'to_top_right
along_edge
within'
[]
[kill_left]
type = 'KillRayBC'
boundary = 'left'
rays = 'reflect_three_times
reflect_at_nodes
reflect_internal'
[]
[reflect]
type = 'ReflectRayBC'
boundary = 'back right top'
rays = 'reflect_three_times
reflect_at_nodes'
[]
[reflect_internal]
type = 'ReflectRayBC'
boundary = 7
rays = 'reflect_internal'
[]
[kill_internal]
type = 'KillRayBC'
boundary = 7
rays = 'kill_internal'
[]
[nothing_internal]
type = 'NullRayBC'
boundary = 7
rays = 'to_top_right
reflect_three_times
reflect_at_nodes'
[]
[]
[UserObjects/study]
type = RepeatableRayStudy
ray_kernel_coverage_check = false
start_points = '0 0 0
0 5 0
0.6 0.6 0
0 1.2 0.8
3 0 1
0 1.3 2.5
5 0 2'
directions = '1 1 1
0 0 1
0 0 1
1 0.6 -0.4
2 2 1
0.8 0.5 0.4
-1 1 1'
names = 'to_top_right
along_edge
within
reflect_three_times
reflect_at_nodes
reflect_internal
kill_internal'
execute_on = initial
always_cache_traces = true
use_internal_sidesets = true
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Outputs]
exodus = false
[rays]
type = RayTracingExodus
study = study
execute_on = final
[]
[]
(modules/combined/test/tests/multiphase_mechanics/multiphasestress.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
xmin = 0
xmax = 2
ymin = 0
ymax = 2
elem_type = QUAD4
[]
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./eta1]
[./InitialCondition]
type = FunctionIC
function = 'x/2'
[../]
[../]
[./eta2]
[./InitialCondition]
type = FunctionIC
function = 'y/2'
[../]
[../]
[./eta3]
[./InitialCondition]
type = FunctionIC
function = '(2^0.5-(y-1)^2=(y-1)^2)/2'
[../]
[../]
[./e11_aux]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./matl_e11]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 0
variable = e11_aux
[../]
[]
[Kernels]
[./TensorMechanics]
[../]
[]
[Materials]
[./elasticity_tensor_A]
type = ComputeElasticityTensor
base_name = A
fill_method = symmetric9
C_ijkl = '1e6 1e5 1e5 1e6 0 1e6 .4e6 .2e6 .5e6'
[../]
[./strain_A]
type = ComputeSmallStrain
base_name = A
eigenstrain_names = eigenstrain
[../]
[./stress_A]
type = ComputeLinearElasticStress
base_name = A
[../]
[./eigenstrain_A]
type = ComputeEigenstrain
base_name = A
eigen_base = '0.1 0.05 0 0 0 0.01'
prefactor = -1
eigenstrain_name = eigenstrain
[../]
[./elasticity_tensor_B]
type = ComputeElasticityTensor
base_name = B
fill_method = symmetric9
C_ijkl = '1e6 0 0 1e6 0 1e6 .5e6 .5e6 .5e6'
[../]
[./strain_B]
type = ComputeSmallStrain
base_name = B
eigenstrain_names = 'B_eigenstrain'
[../]
[./stress_B]
type = ComputeLinearElasticStress
base_name = B
[../]
[./eigenstrain_B]
type = ComputeEigenstrain
base_name = B
eigen_base = '0.1 0.05 0 0 0 0.01'
prefactor = -1
eigenstrain_name = 'B_eigenstrain'
[../]
[./elasticity_tensor_C]
type = ComputeElasticityTensor
base_name = C
fill_method = symmetric9
C_ijkl = '1.1e6 1e5 0 1e6 0 1e6 .5e6 .2e6 .5e6'
[../]
[./strain_C]
type = ComputeSmallStrain
base_name = C
eigenstrain_names = 'C_eigenstrain'
[../]
[./stress_C]
type = ComputeLinearElasticStress
base_name = C
[../]
[./eigenstrain_C]
type = ComputeEigenstrain
base_name = C
eigen_base = '0.1 0.05 0 0 0 0.01'
prefactor = -1
eigenstrain_name = 'C_eigenstrain'
[../]
[./switching_A]
type = SwitchingFunctionMaterial
function_name = h1
eta = eta1
[../]
[./switching_B]
type = SwitchingFunctionMaterial
function_name = h2
eta = eta2
[../]
[./switching_C]
type = SwitchingFunctionMaterial
function_name = h3
eta = eta3
[../]
[./combined]
type = MultiPhaseStressMaterial
phase_base = 'A B C'
h = 'h1 h2 h3'
[../]
[]
[BCs]
[./bottom_y]
type = DirichletBC
variable = disp_y
boundary = 'bottom'
value = 0
[../]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = 'left'
value = 0
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(test/tests/markers/error_tolerance_marker/error_tolerance_marker_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
nz = 10
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
[./solution]
type = ParsedFunction
value = (exp(x)-1)/(exp(1)-1)
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./conv]
type = Convection
variable = u
velocity = '1 0 0'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Adaptivity]
[./Indicators]
[./error]
type = AnalyticalIndicator
variable = u
function = solution
[../]
[../]
[./Markers]
[./marker]
type = ErrorToleranceMarker
coarsen = 4e-9
indicator = error
refine = 1e-8
[../]
[../]
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/heat_conduction/coupled_convective_heat_flux/coupled_convective_heat_flux.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Functions]
[./T_infinity_fn]
type = ParsedFunction
value = (x*x+y*y)+500
[../]
[./Hw_fn]
type = ParsedFunction
value = ((1-x)*(1-x)+(1-y)*(1-y))+1000
[../]
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./T_infinity]
[../]
[./Hw]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./force]
type = BodyForce
variable = u
value = 1000
[../]
[]
[AuxKernels]
[./T_infinity_ak]
type = FunctionAux
variable = T_infinity
function = T_infinity_fn
execute_on = initial
[../]
[./Hw_ak]
type = FunctionAux
variable = Hw
function = Hw_fn
execute_on = initial
[../]
[]
[BCs]
[./right]
type = CoupledConvectiveHeatFluxBC
variable = u
boundary = right
htc = Hw
T_infinity = T_infinity
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/dgkernels/2d_diffusion_dg/no_functor_additions.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
elem_type = QUAD4
[]
[Variables]
[./u]
order = FIRST
family = MONOMIAL
[./InitialCondition]
type = ConstantIC
value = 1
[../]
[../]
[]
[AuxVariables]
[v]
order = FIRST
family = MONOMIAL
[]
[]
[Functions]
[./forcing_fn]
type = ParsedFunction
value = 2*pow(e,-x-(y*y))*(1-2*y*y)
[../]
[./exact_fn]
type = ParsedGradFunction
value = pow(e,-x-(y*y))
grad_x = -pow(e,-x-(y*y))
grad_y = -2*y*pow(e,-x-(y*y))
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./abs] # u * v
type = Reaction
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[DGKernels]
[regular_dg_diffusion]
type = DGDiffusion
variable = u
epsilon = -1
sigma = 6
[]
[]
[DGDiffusionAction]
variable = u
kernels_to_add = 'COUPLED'
coupled_var = v
[]
[BCs]
[./all]
type = DGFunctionDiffusionDirichletBC
variable = u
boundary = '0 1 2 3'
function = exact_fn
epsilon = -1
sigma = 6
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
csv = true
[console]
type = Console
system_info = 'framework mesh aux nonlinear relationship execution'
[]
[]
[Problem]
error_on_jacobian_nonzero_reallocation = true
[]
[Postprocessors]
[num_rm]
type = NumRelationshipManagers
[]
[]
(test/tests/fvkernels/mms/non-orthogonal/extended-adr.i)
a=1.1
diff=1.1
[Mesh]
[./gen_mesh]
type = GeneratedMeshGenerator
dim = 2
xmin = 2
xmax = 3
ymin = 0
ymax = 1
nx = 2
ny = 2
elem_type = TRI3
[../]
[]
[Variables]
[./v]
family = MONOMIAL
order = CONSTANT
fv = true
initial_condition = 1
type = MooseVariableFVReal
face_interp_method = vertex-based
[../]
[]
[FVKernels]
[./advection]
type = FVAdvection
variable = v
velocity = '${a} ${fparse 2*a} 0'
advected_interp_method = 'average'
[../]
[reaction]
type = FVReaction
variable = v
[]
[diff_v]
type = FVDiffusion
variable = v
coeff = ${diff}
use_point_neighbors = true
[]
[body_v]
type = FVBodyForce
variable = v
function = 'forcing'
[]
[]
[FVBCs]
[exact]
type = FVFunctionDirichletBC
boundary = 'left right top bottom'
function = 'exact'
variable = v
[]
[]
[Functions]
[exact]
type = ParsedFunction
value = 'sin(x)*cos(y)'
[]
[forcing]
type = ParsedFunction
value = '-2*a*sin(x)*sin(y) + a*cos(x)*cos(y) + 2*diff*sin(x)*cos(y) + sin(x)*cos(y)'
vars = 'a diff'
vals = '${a} ${diff}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type'
petsc_options_value = 'hypre'
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[./error]
type = ElementL2Error
variable = v
function = exact
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(test/tests/meshgenerators/stitched_mesh_generator/stitched_mesh_generator2.i)
[Mesh]
[./fmg_left]
type = FileMeshGenerator
file = left.e
[]
[./fmg_center]
type = FileMeshGenerator
file = center.e
[]
[./fmg_right]
type = FileMeshGenerator
file = right.e
[]
[./smg]
type = StitchedMeshGenerator
inputs = 'fmg_left fmg_center fmg_right'
clear_stitched_boundary_ids = true
stitch_boundaries_pairs = 'right left;
right left'
[]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/ray_tracing/test/tests/raykernels/ray_distance_aux/ray_distance_aux.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
xmax = 5
ymax = 5
[]
[AuxVariables/distance]
order = CONSTANT
family = MONOMIAL
[]
[RayKernels/distance]
type = RayDistanceAux
variable = distance
[]
[UserObjects/study]
type = LotsOfRaysRayStudy
vertex_to_vertex = false
centroid_to_vertex = false
centroid_to_centroid = true
execute_on = initial
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/override_name_variable_test.i)
# Two non-linear variables with the same name
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 5
ny = 5
elem_type = QUAD9
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
# Note this section is a repeat of the one above
[./u]
order = SECOND
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/auxkernels/grad_component/grad_component_monomial.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmax = 2
nx = 20
ny = 10
[]
[Variables]
[./not_u]
[../]
[]
[AuxVariables]
[./u]
family = MONOMIAL
order = FIRST
[../]
[./grad_u_x]
order = CONSTANT
family = MONOMIAL
[../]
[]
[ICs]
[./u]
type = FunctionIC
variable = u
function = 'if(x>0.5,if(x<1.5,2*x,3),0)'
[../]
[]
[AuxKernels]
[./grad_u_x_aux]
type = VariableGradientComponent
variable = grad_u_x
component = x
gradient_variable = u
execute_on = initial
[../]
[]
[Problem]
type = FEProblem
solve = false
kernel_coverage_check = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/phase_field/test/tests/feature_volume_vpp_test/percolation_test.i)
# This tests the percolation detection capability in FeatureFloodCount. One feature
# exists that intersects both left and right boundaries, so the FeatureVolumeVPP
# will return true for that feature based on the specified values of parameters
# primary_percolation_boundaries and secondary_percolation_boundaries.
# It also tests the capabilility of FeatureFloodCount to detect whether each feature
# is in contact with the boundaries set by the specified_boundaries parameter.
[Mesh]
type = GeneratedMesh
dim = 2
nx = 60
ny = 60
xmin = 0
xmax = 50
ymin = 0
ymax = 50
elem_type = QUAD4
[]
[Variables]
[./c]
order = FIRST
family = LAGRANGE
[]
[]
[AuxVariables]
[./unique_regions]
family = MONOMIAL
order = CONSTANT
[../]
[]
[ICs]
[./c]
type = MultiSmoothCircleIC
variable = c
invalue = 1.0
outvalue = 0.0001
radius = 4.0
int_width = 2.0
numbub = 35
bubspac = 2
[]
[]
[Postprocessors]
[./flood_count]
type = FeatureFloodCount
variable = c
# Must be turned out to build data structures necessary for FeatureVolumeVPP
compute_var_to_feature_map = true
threshold = 0.5
outputs = none
execute_on = INITIAL
primary_percolation_boundaries = 'left'
secondary_percolation_boundaries = 'right'
specified_boundaries = 'left right'
[../]
[]
[VectorPostprocessors]
[./features]
type = FeatureVolumeVectorPostprocessor
flood_counter = flood_count
# Turn on centroid output
output_centroids = true
execute_on = INITIAL
[../]
[]
[Kernels]
[diff]
type = Diffusion
variable = c
[]
[]
[AuxKernels]
[./unique_regions]
type = FeatureFloodCountAux
variable = unique_regions
flood_counter = flood_count
field_display = UNIQUE_REGION
[../]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
execute_on = INITIAL
[]
(test/tests/kernels/array_kernels/array_body_force.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 4
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
components = 2
scaling = '.9 .9'
[]
[]
[Kernels]
[diff]
type = ArrayDiffusion
variable = u
diffusion_coefficient = dc
[]
[source]
type = ArrayBodyForce
variable = u
function = '1 x'
[]
[]
[BCs]
[left]
type = ArrayDirichletBC
variable = u
boundary = 'left right bottom top'
values = '0 0'
[]
[]
[Materials]
[dc]
type = GenericConstantArray
prop_name = dc
prop_value = '1 1'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(modules/combined/test/tests/heat_convection/heat_convection_rz_test.i)
# Test cases for convective boundary conditions. TKLarson, 11/01/11, rev. 0.
# Input file for htc_2dtest1
# TKLarson
# 11/01/11
# Revision 0
#
# Goals of this test are:
# 1) show that expected results ensue from application of convective boundary conditions
# Convective boundary condition:
# q = h*A*(Tw - Tf)
# where
# q - heat transfer rate (w)
# h - heat transfer coefficient (w/m^2-K)
# A - surface area (m^2)
# Tw - surface temperature (K)
# Tf - fluid temperature adjacent to the surface (K)
# The heat transfer coefficient (h) is input as a variable called 'rate'
# Tf is a two valued function specified by 'initial' and 'final' along with a variable
# called 'duration,' the length of time in seconds that it takes initial to linearly ramp
# to 'final.'
# The mesh for this test case is based on an ASTM standard for the so-called Brazillian Cylinder test
# (ASTM International, Standard Test Method for Splitting Tensile Strength of Cylindrical Concrete
# Specimens, C 496/C 496M-04, 2004) (because I already had a version of the model). While the
# Brazillian Cylinder test is for dynamic tensile testing of concrete, the model works for the present
# purposes. The model is 2-d RZ coordinates.
#
# Brazillian Cylinder sample dimensions:
# L = 20.3 cm, 0.203 m, (8 in)
# r = 5.08 cm, 0.0508 m, (2 in)
# Material properties are:
# density = 2405.28 km/m^3
# specific heat = 826.4 J/kg-K
# thermal conductivity 1.937 w/m-K
# alpha (thermal conductivity/(density*specific heat) is then 9.74e-7 m^2/s
#
# Initial cylinder temperature is room temperature 294.26 K (70 F)
# The initial fluid temperature is room temperature. We will ramp it to 477.6 K (400 F) in 10 minutes.
# We will use a natural convection h (284 w/m^2-K (50 BTU/hr-ft^2-F)) on all faces of the cylinder.
# This is akin to putting the cylinder in an oven (nonconvection type) and turning the oven on.
# What we expect for this problem:
# 1) Use of h = 284 should cause the cylinder to slowly warm up
# 2) The fluid temperature should rise from initial (294 K) to final (477 K) in 600 s.
# 3) 1) and 2) should cause the cylinder to become soaked at 477.6 K after sufficient time(i.e. ~ 1/2 hr).
# This is a simple thermal soak problem.
[Problem]
coord_type = RZ
[]
[Mesh] # Mesh Start
# 10cm x 20cm cylinder not so detailed mesh, 2 radial, 6 axial nodes
# Only one block (Block 1), all concrete
# Sideset 1 - top of cylinder, Sideset 2 - length of cylinder, Sideset 3 - bottom of cylinder
file = heat_convection_rz_mesh.e
[] # Mesh END
[Variables] # Variables Start
[./temp]
order = FIRST
family = LAGRANGE
initial_condition = 294.26 # Initial cylinder temperature
[../]
[] # Variables END
[Kernels] # Kernels Start
[./heat]
type = HeatConduction
variable = temp
[../]
[./heat_ie]
type = HeatConductionTimeDerivative
variable = temp
[../]
[] # Kernels END
[BCs] # Boundary Conditions Start
# Heat transfer coefficient on outer cylinder radius and ends
[./convective_clad_surface] # Convective Start
type = ConvectiveFluxBC # Convective flux, e.g. q'' = h*(Tw - Tf)
boundary = '1 2 3' # BC applied on top, along length, and bottom
variable = temp
rate = 284. # (w/m^2-K)[50 BTU/hr/-ft^2-F]
# the above h is a reasonable natural convection value
initial = 294.26 # initial ambient (lab or oven) temperature (K)
final = 477.6 # final ambient (lab or oven) temperature (K)
duration = 600. # length of time in seconds that it takes the ambient
# temperature to ramp from initial to final
[../] # Convective End
[] # BCs END
[Materials] # Materials Start
[./thermal]
type = HeatConductionMaterial
block = 1
specific_heat = 826.4
# thermal_conductivity = 1.937 # this makes alpha 9.74e-7 m^2/s
# thermal_conductivity = 19.37 # this makes alpha 9.74e-6 m^2/s
# thermal conductivity arbitrarily increased by a decade to
# make the cylinder thermally soak faster (only for the purposes
# of this test problem
thermal_conductivity = 193.7 # this makes alpha 9.74e-5 m^2/s
# thermal conductivity arbitrarily increased by 2 decade to
# make the cylinder thermally soak faster (only for the purposes
# of this test problem
[../]
[./density]
type = Density
block = 1
density = 2405.28
[../]
[] # Materials END
[Executioner] # Executioner Start
type = Transient
# type = Steady
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew '
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type'
petsc_options_value = '70 hypre boomeramg'
l_max_its = 60
nl_rel_tol = 1e-8
nl_abs_tol = 1e-10
l_tol = 1e-5
start_time = 0.0
dt = 60.
num_steps = 20 # Total run time 1200 s
[] # Executioner END
[Outputs] # Output Start
# Output Start
file_base = out_rz
exodus = true
[] # Output END
# # Input file END
(modules/richards/test/tests/jacobian_1/jn_fu_02.i)
# unsaturated = true
# gravity = false
# supg = false
# transient = false
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = -1
xmax = 1
ymin = -1
ymax = 1
zmin = -1
zmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGnone
sat_UO = Saturation
seff_UO = SeffVG
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0 # notice small quantity, so the PETSc constant state works
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1 # notice small quantity, so the PETSc constant state works
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.2
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGnone]
type = RichardsSUPGnone
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = RandomIC
block = 0
min = -1
max = 0
[../]
[../]
[]
[Kernels]
active = 'richardsf'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFullyUpwindFlux
variable = pressure
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
viscosity = 1E-3
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -snes_type'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000 test'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = jn02
exodus = false
[]
(modules/richards/test/tests/gravity_head_1/gh02.i)
# unsaturated = true
# gravity = false
# supg = false
# transient = false
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
xmin = -1
xmax = 1
[]
[BCs]
[./left]
type = DirichletBC
boundary = left
value = -1
variable = pressure
[../]
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0E3
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGnone]
type = RichardsSUPGnone
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = RandomIC
block = 0
min = -1
max = 0
[../]
[../]
[]
[Kernels]
active = 'richardsf'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGnone
sat_UO = Saturation
seff_UO = SeffVG
viscosity = 1E-3
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = gh02
exodus = true
[]
(test/tests/functions/piecewise_linear/piecewise_linear.i)
[Mesh]
type = GeneratedMesh
dim = 1
xmin = 0
xmax = 5
[]
[Problem]
solve = false
[]
[Functions]
[piecewise_linear]
type = PiecewiseLinear
axis = x
x = '1 2 3 4'
y = '4 6 10 7'
[]
[]
[VectorPostprocessors]
[function_vpp]
type = LineFunctionSampler
functions = 'piecewise_linear'
start_point = '0 0 0'
end_point = '5 0 0'
num_points = 6
sort_by = x
execute_on = 'INITIAL'
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
file_base = 'no_extrap'
execute_on = 'INITIAL'
[]
(modules/ray_tracing/test/tests/raykernels/ray_kernel/errors.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
[]
[]
[UserObjects/study]
type = RepeatableRayStudy
start_points = '0 0 0'
directions = '1 0 0'
names = 'ray'
execute_on = PRE_KERNELS
[]
[Variables/u]
[]
[RayKernels/line_source]
type = LineSourceRayKernel
variable = u
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
(test/tests/mesh_modifiers/add_side_sets/cylinder_normals.i)
[Mesh]
[file]
type = FileMeshGenerator
file = cylinder.e
[]
# Mesh Modifiers
[add_side_sets]
type = SideSetsFromNormalsGenerator
input = file
normals = '0 0 1
0 1 0
0 0 -1'
# This parameter allows the normal
# to vary slightly from adjacent element
# to element so that a sidset can follow
# a curve. It is false by default.
fixed_normal = false
new_boundary = 'top side bottom'
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[bottom]
type = DirichletBC
variable = u
boundary = bottom
value = 0
[]
[top]
type = DirichletBC
variable = u
boundary = top
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/invalid_aux_coupling_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./nodal_aux]
order = FIRST
family = LAGRANGE
[../]
[./elemental_aux]
# order = FIRST
# family = LAGRANGE
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./nodal]
type = CoupledAux
variable = nodal_aux
coupled = elemental_aux
[../]
[./elemental]
type = ConstantAux
variable = elemental_aux
value = 6
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/controls/tag_based_naming_access/object_param.i)
[Mesh]
type = GeneratedMesh
dim = 2
elem_type = QUAD4
# use odd numbers so points do not fall on element boundaries
nx = 31
ny = 31
[]
[Variables]
[./diffused]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = diffused
[../]
[]
[DiracKernels]
[./test_object]
type = MaterialPointSource
point = '0.5 0.5 0'
variable = diffused
control_tags = 'tag'
[../]
[]
[BCs]
[./bottom_diffused]
type = DirichletBC
variable = diffused
boundary = 'bottom'
value = 2
[../]
[./top_diffused]
type = DirichletBC
variable = diffused
boundary = 'top'
value = 0
[../]
[]
[Materials]
[./mat]
type = GenericConstantMaterial
prop_names = 'matp'
prop_values = '1'
block = 0
[../]
[]
[Postprocessors]
[./test_object]
type = FunctionValuePostprocessor
function = '2*(x+y)'
point = '0.5 0.5 0'
control_tags = 'tag'
[../]
[./other_point_test_object]
type = FunctionValuePostprocessor
function = '3*(x+y)'
point = '0.5 0.5 0'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
[Controls]
[./point_control]
type = TestControl
test_type = 'point'
parameter = 'tag::*/point'
execute_on = 'initial'
[../]
[]
(modules/combined/test/tests/thermal_elastic/derivatives.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 2
[]
[Variables]
[./a]
[./InitialCondition]
type = RandomIC
min = -1
max = 1
[../]
[../]
[./b]
[./InitialCondition]
type = RandomIC
min = -1
max = 1
[../]
[../]
[]
[Debug]
[./MaterialDerivativeTest]
[./elastic]
prop_name = elasticity_tensor
prop_type = RankFourTensor
derivative_order = 1
args = 'a b'
[../]
[../]
[]
[Problem]
kernel_coverage_check = false
[]
[Materials]
[./youngs_modulus]
type = DerivativeParsedMaterial
f_name = youngs_modulus
function = '23.1 * a^4 + 10.7 * b^2'
args = 'a b'
[../]
[./poissons_ratio]
type = DerivativeParsedMaterial
f_name = poissons_ratio
function = '0.2 * a^2 + 0.29 * b^3'
args = 'a b'
[../]
[./elasticity_tensor]
type = ComputeVariableIsotropicElasticityTensor
args = 'a b'
youngs_modulus = youngs_modulus
poissons_ratio = poissons_ratio
[../]
[]
[Executioner]
type = Steady
[]
(modules/heat_conduction/test/tests/postprocessors/convective_ht_side_integral.i)
[Mesh]
type = MeshGeneratorMesh
[./cartesian]
type = CartesianMeshGenerator
dim = 2
dx = '0.45 0.1 0.45'
ix = '5 1 5'
dy = '0.45 0.1 0.45'
iy = '5 1 5'
subdomain_id = '1 1 1
1 2 1
1 1 1'
[../]
[./add_iss_1]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 1
paired_block = 2
new_boundary = 'interface'
input = cartesian
[../]
[./block_deleter]
type = BlockDeletionGenerator
block = 2
input = add_iss_1
[../]
[]
[Variables]
[./temperature]
initial_condition = 300
[../]
[]
[AuxVariables]
[./channel_T]
family = MONOMIAL
order = CONSTANT
initial_condition = 400
[../]
[./channel_Hw]
family = MONOMIAL
order = CONSTANT
initial_condition = 1000
[../]
[]
[Kernels]
[./graphite_diffusion]
type = HeatConduction
variable = temperature
diffusion_coefficient = 'k_s'
[../]
[]
[BCs]
## boundary conditions for the thm channels in the reflector
[./channel_heat_transfer]
type = CoupledConvectiveHeatFluxBC
variable = temperature
htc = channel_Hw
T_infinity = channel_T
boundary = 'interface'
[../]
# hot boundary on the left
[./left]
type = DirichletBC
variable = temperature
value = 1000
boundary = 'left'
[../]
# cool boundary on the right
[./right]
type = DirichletBC
variable = temperature
value = 300
boundary = 'right'
[../]
[]
[Materials]
[./thermal]
type = GenericConstantMaterial
prop_names = 'k_s'
prop_values = '12'
[../]
[./htc_material]
type = GenericConstantMaterial
prop_names = 'alpha_wall'
prop_values = '1000'
[../]
[./tfluid_mat]
type = PiecewiseLinearInterpolationMaterial
property = tfluid_mat
variable = channel_T
x = '400 500'
y = '400 500'
[../]
[]
[Postprocessors]
[./Qw1]
type = ConvectiveHeatTransferSideIntegral
T_fluid_var = channel_T
htc_var = channel_Hw
T_solid = temperature
boundary = interface
[../]
[./Qw2]
type = ConvectiveHeatTransferSideIntegral
T_fluid_var = channel_T
htc = alpha_wall
T_solid = temperature
boundary = interface
[../]
[./Qw3]
type = ConvectiveHeatTransferSideIntegral
T_fluid = tfluid_mat
htc = alpha_wall
T_solid = temperature
boundary = interface
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/lid-driven/lid-driven.i)
mu=.01
rho=1
[GlobalParams]
velocity_interp_method = 'rc'
advected_interp_method = 'average'
rhie_chow_user_object = 'rc'
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = .1
ymin = 0
ymax = .1
nx = 20
ny = 20
[]
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
[]
[vel_y]
type = INSFVVelocityVariable
[]
[pressure]
type = INSFVPressureVariable
[]
[lambda]
family = SCALAR
order = FIRST
[]
[]
[AuxVariables]
[U]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[]
[AuxKernels]
[mag]
type = VectorMagnitudeAux
variable = U
x = vel_x
y = vel_y
[]
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
rho = ${rho}
[]
[mean_zero_pressure]
type = FVIntegralValueConstraint
variable = pressure
lambda = lambda
phi0 = 0.0
[]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = 'mu'
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = 'mu'
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
[]
[]
[FVBCs]
[top_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'top'
function = 1
[]
[no_slip_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'left right bottom'
function = 0
[]
[no_slip_y]
type = INSFVNoSlipWallBC
variable = vel_y
boundary = 'left right top bottom'
function = 0
[]
[]
[Materials]
[mu]
type = ADGenericFunctorMaterial
prop_names = 'mu'
prop_values = '${mu}'
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(tutorials/tutorial01_app_development/step05_kernel_object/test/tests/kernels/simple_diffusion/simple_diffusion.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/mesh/mesh_generation/disc_sector.i)
# Generates a sector of a Disc Mesh between angle=Pi/4 and angle=3Pi/4
# Radius of outside circle=5
# Solves the diffusion equation with u=-5 at origin, and u=0 on outside
# as well as u=-5+r at angle=Pi/4 and u=-5+r^4/125 at angle=3Pi/4
[Mesh]
type = AnnularMesh
nr = 10
nt = 12
rmin = 0
rmax = 5
dmin = 45
dmax = 135
growth_r = 1.3
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./inner]
type = DirichletBC
variable = u
value = -5.0
boundary = rmin
[../]
[./outer]
type = FunctionDirichletBC
variable = u
function = 0
boundary = rmax
[../]
[./tmin]
type = FunctionDirichletBC
variable = u
function = '-5.0+sqrt(x*x + y*y)'
boundary = dmin
[../]
[./tmax]
type = FunctionDirichletBC
variable = u
function = '-5.0+pow(x*x + y*y, 2)/125'
boundary = dmax
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
[]
[Outputs]
exodus = true
[]
(test/tests/postprocessors/interface_value/interface_fv_variable_value_postprocessor.i)
postprocessor_type = InterfaceAverageVariableValuePostprocessor
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 6
xmax = 3
ny = 9
ymax = 3
elem_type = QUAD4
[]
[./subdomain_id]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '0 0 0'
top_right = '2 1 0'
block_id = 1
[../]
[./interface]
type = SideSetsBetweenSubdomainsGenerator
input = subdomain_id
primary_block = '0'
paired_block = '1'
new_boundary = 'interface'
[../]
[]
[Functions]
[./fn_exact]
type = ParsedFunction
value = 'x*x+y*y'
[../]
[./ffn]
type = ParsedFunction
value = -4
[../]
[]
[Variables]
[./u]
family = MONOMIAL
order = CONSTANT
fv = true
[../]
[]
[FVKernels]
[./diff]
type = FVDiffusion
variable = u
coeff = 1
[../]
[./ffn]
type = FVBodyForce
variable = u
function = ffn
[../]
[]
[FVBCs]
[./all]
type = FVFunctionDirichletBC
variable = u
boundary = '0 1 2 3'
function = fn_exact
[../]
[]
[Materials]
[./stateful1]
type = GenericConstantMaterial
block = 0
prop_names = 'diffusivity'
prop_values = 10
[../]
[./stateful2]
type = GenericConstantMaterial
block = 1
prop_names = 'diffusivity'
prop_values = 4
[../]
[]
[AuxKernels]
[./diffusivity_1]
type = MaterialRealAux
property = diffusivity
variable = diffusivity_1
[]
[./diffusivity_2]
type = MaterialRealAux
property = diffusivity
variable = diffusivity_2
[]
[]
[AuxVariables]
[./diffusivity_1]
family = MONOMIAL
order = CONSTANT
[]
[./diffusivity_2]
family = MONOMIAL
order = CONSTANT
[]
[]
[Postprocessors]
[./diffusivity_average]
type = ${postprocessor_type}
interface_value_type = average
variable = diffusivity_1
neighbor_variable = diffusivity_2
execute_on = TIMESTEP_END
boundary = 'interface'
[../]
[./diffusivity_jump_primary_secondary]
type = ${postprocessor_type}
interface_value_type = jump_primary_minus_secondary
variable = diffusivity_1
neighbor_variable = diffusivity_2
execute_on = TIMESTEP_END
boundary = 'interface'
[../]
[./diffusivity_jump_secondary_primary]
type = ${postprocessor_type}
interface_value_type = jump_secondary_minus_primary
variable = diffusivity_1
neighbor_variable = diffusivity_2
execute_on = TIMESTEP_END
boundary = 'interface'
[../]
[./diffusivity_jump_abs]
type = ${postprocessor_type}
interface_value_type = jump_abs
variable = diffusivity_1
neighbor_variable = diffusivity_2
execute_on = TIMESTEP_END
boundary = 'interface'
[../]
[./diffusivity_primary]
type = ${postprocessor_type}
interface_value_type = primary
variable = diffusivity_1
neighbor_variable = diffusivity_2
execute_on = TIMESTEP_END
boundary = 'interface'
[../]
[./diffusivity_secondary]
type = ${postprocessor_type}
interface_value_type = secondary
variable = diffusivity_1
neighbor_variable = diffusivity_2
execute_on = TIMESTEP_END
boundary = 'interface'
[../]
[./diffusivity_single_variable]
type = ${postprocessor_type}
interface_value_type = primary
variable = diffusivity_1
execute_on = TIMESTEP_END
boundary = 'interface'
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
file_base = ${raw ${postprocessor_type} _fv}
exodus = true
[]
(test/tests/vectorpostprocessors/1d_line_sampler/1d_line_sampler.i)
# Tests the ability of a line sampler to correctly sample a coincident line. In
# 1-D, it was found that sometimes only the first few elements would be found,
# due to floating point precision error in equality tests for the points. This
# test uses a mesh configuration for which this has occurred and ensures that
# the output CSV file contains all points for the LineMaterialRealSampler vector
# postprocessor.
my_xmax = 1.2
[Mesh]
type = GeneratedMesh
parallel_type = replicated # Until RayTracing.C is fixed
dim = 1
nx = 10
xmin = 0
xmax = ${my_xmax}
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Materials]
[./my_mat]
type = GenericConstantMaterial
prop_names = 'my_prop'
prop_values = 5
[../]
[]
[VectorPostprocessors]
[./my_vpp]
type = LineMaterialRealSampler
property = my_prop
start = '0 0 0'
end = '${my_xmax} 0 0'
sort_by = x
[../]
[]
[Outputs]
[./out]
type = CSV
execute_vector_postprocessors_on = 'timestep_end'
show = 'my_vpp'
precision = 5
[../]
[]
(modules/thermal_hydraulics/test/tests/materials/reynolds_number/test.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
allow_renumbering = false
[]
[Variables]
[arhoA]
[]
[arhouA]
[]
[arhoEA]
[]
[]
[AuxVariables]
[Re]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[Re_ak]
type = MaterialRealAux
variable = Re
property = my_Re
[]
[]
[Materials]
[rho_mat]
type = ConstantMaterial
property_name = rho
derivative_vars = 'arhoA'
value = 1000
[]
[vel_mat]
type = ConstantMaterial
property_name = vel
derivative_vars = 'arhoA arhouA'
value = 5
[]
[D_h_mat]
type = ConstantMaterial
property_name = D_h
value = 0.002
[]
[mu_mat]
type = ConstantMaterial
property_name = mu
derivative_vars = 'arhoA arhouA arhoEA'
value = 0.1
[]
[Re_material]
type = ReynoldsNumberMaterial
arhoA = arhoA
arhouA = arhouA
arhoEA = arhoEA
Re = my_Re
rho = rho
vel = vel
D_h = D_h
mu = mu
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[Re]
type = ElementalVariableValue
elementid = 0
variable = Re
[]
[]
[Outputs]
csv = true
execute_on = timestep_end
[]
(test/tests/geomsearch/quadrature_penetration_locator/1d_quadrature_penetration.i)
[Mesh]
type = FileMesh
file = 1d_penetration.e
construct_side_list_from_node_list = true
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./penetration]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 2
paired_boundary = 3
[../]
[]
[BCs]
[./block1_left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./block1_right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[./block2_left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./block2_right]
type = DirichletBC
variable = u
boundary = 4
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/fvkernels/mms/diffusion.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 2
[]
[Variables]
# [u]
# []
[v]
family = MONOMIAL
order = CONSTANT
fv = true
[]
[]
[FVKernels]
[diff_v]
type = FVDiffusion
variable = v
coeff = coeff
[]
[body_v]
type = FVBodyForce
variable = v
function = 'forcing'
[]
[]
[FVBCs]
[boundary]
type = FVFunctionDirichletBC
boundary = 'left right'
function = 'exact'
variable = v
[]
[]
[Materials]
[diff]
type = ADGenericFunctorMaterial
prop_names = 'coeff'
prop_values = '1'
[]
[]
[Functions]
[exact]
type = ParsedFunction
value = '3*x^2 + 2*x + 1'
[]
[forcing]
type = ParsedFunction
value = '-6'
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
# [./L2u]
# type = ElementL2Error
# variable = u
# function = exact
# outputs = 'console'
# execute_on = 'timestep_end'
# [../]
[./error]
type = ElementL2Error
variable = v
function = exact
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(test/tests/vectorpostprocessors/constant_vector_postprocessor/constant_vector_postprocessor.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[VectorPostprocessors]
[./constant]
type = ConstantVectorPostprocessor
value = '1.5 2.7'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
csv = true
[]
(test/tests/transfers/multiapp_copy_transfer/third_monomial_to_sub/sub.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
family = MONOMIAL
order = THIRD
[../]
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/postprocessors/element_extreme_value/element_proxy_extreme_value.i)
[Problem]
type = FEProblem
solve = false
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 40
ny = 40
[]
[AuxVariables]
[u]
[]
[w]
[]
[v_x]
[]
[v_y]
[]
[]
[AuxKernels]
[u]
type = FunctionAux
variable = u
function = u
[]
[w]
type = FunctionAux
variable = w
function = w
[]
[v_x]
type = FunctionAux
variable = v_x
function = v_x
[]
[v_y]
type = FunctionAux
variable = v_y
function = v_y
[]
[]
[Functions]
[u] # reaches a maximum value at (0.5, 0.6)
type = ParsedFunction
value = 'sin(pi*x)*sin(pi*y/1.2)'
[]
[w] # reaches a minium value at (0.7, 0.8)
type = ParsedFunction
value = '-sin(pi*x/1.4)*sin(pi*y/1.6)'
[]
[v_x]
type = ParsedFunction
value = 'x'
[]
[v_y]
type = ParsedFunction
value = 'y'
[]
[]
[Postprocessors]
# because we set v_x and v_y equal to the x and y coordinates, these two postprocessors
# should just return the point at which u reaches a maximum value
[max_v_from_proxy_x]
type = ElementExtremeValue
variable = v_x
proxy_variable = u
value_type = max
[]
[max_v_from_proxy_y]
type = ElementExtremeValue
variable = v_y
proxy_variable = u
value_type = max
[]
# because we set v_x and v_y equal to the x and y coordinates, these two postprocessors
# should just return the point at which w reaches a minimum value
[min_v_from_proxy_x]
type = ElementExtremeValue
variable = v_x
proxy_variable = w
value_type = min
[]
[min_v_from_proxy_y]
type = ElementExtremeValue
variable = v_y
proxy_variable = w
value_type = min
[]
[]
[Executioner]
type = Steady
# increase the quadrature order to get more quadrature points so that were closer
# to hitting the expect max/min
[Quadrature]
type = GAUSS
order = SECOND
[]
[]
[Outputs]
exodus = true
csv = true
[]
(test/tests/utils/mffd/mffd_test.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
preset = false
boundary = 'left'
value = 0
[../]
[./right]
type = DirichletBC
variable = u
preset = false
boundary = 'right'
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
mffd_type = 'ds'
[]
(test/tests/multiapps/picard_multilevel/fullsolve_multilevel/master.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 10
ny = 10
[]
[Variables]
[u]
[]
[]
[AuxVariables]
[v]
initial_condition = 50
[]
[]
[Kernels]
[diffusion]
type = Diffusion
variable = u
[]
[source]
type = CoupledForce
variable = u
v = v
[]
[]
[BCs]
[dirichlet0]
type = DirichletBC
variable = u
boundary = '3'
value = 0
[]
[dirichlet]
type = DirichletBC
variable = u
boundary = '1'
value = 100
[]
[]
[Postprocessors]
[avg_u]
type = ElementAverageValue
variable = u
execute_on = 'initial linear'
[]
[avg_v]
type = ElementAverageValue
variable = v
execute_on = 'initial linear'
[]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart '
petsc_options_value = 'hypre boomeramg 100'
fixed_point_rel_tol = 1E-3
fixed_point_abs_tol = 1.0e-05
fixed_point_max_its = 12
[]
[MultiApps]
[level1-]
type = FullSolveMultiApp
app_type = MooseTestApp
positions = '0 0 0'
input_files = sub_level1.i
execute_on = 'timestep_end'
# We have to make backups of the full tree in order to do a proper restore for the Picard iteration.
no_backup_and_restore = false
[]
[]
[Transfers]
[u_to_sub]
type = MultiAppMeshFunctionTransfer
source_variable = u
variable = u
to_multi_app = level1-
execute_on = 'timestep_end'
[]
[v_from_sub]
type = MultiAppMeshFunctionTransfer
source_variable = v
variable = v
from_multi_app = level1-
execute_on = 'timestep_end'
[]
[]
[Outputs]
exodus = true
csv = true
perf_graph = true
[]
(test/tests/misc/max_var_n_dofs_per_elem/max_var_n_dofs_per_elem.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
nz = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = ADDiffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
# Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Postprocessors]
[./max_dofs]
type = MaxVarNDofsPerElemPP
[../]
[]
[Outputs]
exodus = true
[]
(test/tests/mesh/mesh_generation/annulus_sector.i)
# Generates a sector of an Annular Mesh between angle=Pi/4 and angle=3Pi/4
# Radius of inside circle=1
# Radius of outside circle=5
# Solves the diffusion equation with
# u=0 on inside
# u=log(5) on outside
# u=log(r) at angle=Pi/4 and angle=3Pi/4
[Mesh]
type = AnnularMesh
nr = 10
nt = 12
rmin = 1
rmax = 5
dmin = 45
dmax = 135
growth_r = 1.3
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./inner]
type = DirichletBC
variable = u
value = 0.0
boundary = rmin
[../]
[./outer]
type = FunctionDirichletBC
variable = u
function = log(5)
boundary = rmax
[../]
[./min_angle]
type = FunctionDirichletBC
variable = u
function = 'log(sqrt(x*x + y*y))'
boundary = 'dmin dmax'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/oversample/ex02_oversample.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
nz = 0
zmax = 0
elem_type = QUAD9
[]
[Variables]
[./diffused]
order = SECOND
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = diffused
[../]
[]
[DiracKernels]
[./foo]
variable = diffused
type = ConstantPointSource
value = 1
point = '0.3 0.3 0.0'
[../]
[]
[BCs]
active = 'all'
[./all]
type = DirichletBC
variable = diffused
boundary = 'bottom left right top'
value = 0.0
[../]
[]
[Executioner]
type = Steady
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[./os2]
type = Exodus
refinements = 2
[../]
[./os4]
type = Exodus
refinements = 4
[../]
[]
(test/tests/bcs/nodal_normals/cylinder_hexes.i)
[Mesh]
file = cylinder-hexes.e
[]
[Functions]
[./all_bc_fn]
type = ParsedFunction
value = x*x+y*y
[../]
[./f_fn]
type = ParsedFunction
value = -4
[../]
[]
[NodalNormals]
boundary = '1'
corner_boundary = 100
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = f_fn
[../]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
boundary = '1'
function = 'all_bc_fn'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
nl_rel_tol = 1e-13
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(test/tests/misc/check_error/function_file_test14.i)
# Test for usage of missing function
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = ic_function
[../]
[../]
[]
[Functions]
[./ic_function]
type = PiecewiseLinear
data_file = piecewise_linear_rows_more_data.csv # will generate an error because of more data lines than 2
scale_factor = 1.0
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/postprocessors/vector_postprocessor_component/vpp_component.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[VectorPostprocessors]
[reader]
type = CSVReader
csv_file = test_data.csv
outputs = none
[]
[]
[Postprocessors]
[component]
type = VectorPostprocessorComponent
vectorpostprocessor = reader
vector_name = data
index = 2
execute_on = 'initial timestep_end'
[]
[]
[Outputs]
csv = true
[]
(modules/porous_flow/test/tests/fluids/simple_fluid_yr_MPa_C.i)
# Test the properties calculated by the simple fluid Material
# Pressure unit is chosen to be MPa
# Time unit is chosen to be years
# Temperature unit is chosen to be Celsius
# Pressure 10 MPa
# Temperature = 26.85 C
# Density should equal 1500*exp(1E7/1E9-2E-4*300)=1426.844 kg/m^3
# Viscosity should equal 3.49E-17 MPa.yr
# Energy density should equal 4000 * 300 = 1.2E6 J/kg
# Specific enthalpy should equal 4000 * 300 + 10e6 / 1426.844 = 1.207008E6 J/kg
[Modules]
[FluidProperties]
[the_simple_fluid]
type = SimpleFluidProperties
thermal_expansion = 2.0E-4
cv = 4000.0
cp = 5000.0
bulk_modulus = 1.0E9
thermal_conductivity = 1.0
viscosity = 1.1E-3
density0 = 1500.0
[]
[]
[]
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp T'
number_fluid_phases = 1
number_fluid_components = 1
[]
[]
[Variables]
[pp]
initial_condition = 10
[]
[T]
initial_condition = 26.85
[]
[]
[Kernels]
[dummy_p]
type = Diffusion
variable = pp
[]
[dummy_T]
type = Diffusion
variable = T
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
temperature = T
[]
[ppss]
type = PorousFlow1PhaseFullySaturated
porepressure = pp
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
temperature_unit = Celsius
pressure_unit = MPa
time_unit = years
fp = the_simple_fluid
phase = 0
[]
[]
[Postprocessors]
[pressure]
type = ElementIntegralVariablePostprocessor
variable = pp
[]
[temperature]
type = ElementIntegralVariablePostprocessor
variable = T
[]
[density]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_fluid_phase_density_qp0'
[]
[viscosity]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_viscosity_qp0'
[]
[internal_energy]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_fluid_phase_internal_energy_qp0'
[]
[enthalpy]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_fluid_phase_enthalpy_qp0'
[]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
csv = true
[]
(modules/navier_stokes/test/tests/auxkernels/reynolds-number-functor-aux/fv.i)
mu=1
rho=1
[GlobalParams]
velocity_interp_method = 'rc'
advected_interp_method = 'average'
rhie_chow_user_object = 'rc'
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
[]
[v]
type = INSFVVelocityVariable
[]
[pressure]
type = INSFVPressureVariable
[]
[lambda]
family = SCALAR
order = FIRST
[]
[]
[AuxVariables]
[Reynolds]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[Reynolds]
type = ReynoldsNumberFunctorAux
variable = Reynolds
speed = speed
rho = ${rho}
mu = ${mu}
[]
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
rho = ${rho}
[]
[mean_zero_pressure]
type = FVScalarLagrangeMultiplier
variable = pressure
lambda = lambda
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = 'mu'
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = 'mu'
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[]
[FVBCs]
[top_x]
type = INSFVNoSlipWallBC
variable = u
boundary = 'top'
function = 1
[]
[no_slip_x]
type = INSFVNoSlipWallBC
variable = u
boundary = 'left right bottom'
function = 0
[]
[no_slip_y]
type = INSFVNoSlipWallBC
variable = v
boundary = 'left right top bottom'
function = 0
[]
[]
[Materials]
[mu]
type = ADGenericFunctorMaterial
prop_names = 'mu'
prop_values = '${mu}'
[]
[speed]
type = ADVectorMagnitudeFunctorMaterial
x_functor = u
y_functor = v
vector_magnitude_name = speed
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(test/tests/bcs/ad_bcs/vector_ad_bc.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
family = LAGRANGE_VEC
[../]
[]
[Kernels]
[./diff]
type = ADVectorDiffusion
variable = u
[../]
[]
[BCs]
[./left]
type = ADVectorFunctionDirichletBC
variable = u
boundary = left
function_x = '1'
function_y = '1'
[../]
[./right]
type = ADVectorRobinBC
variable = u
boundary = right
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(modules/combined/test/tests/linear_elasticity/tensor.i)
# This input file is designed to test the RankTwoAux and RankFourAux
# auxkernels, which report values out of the Tensors used in materials
# properties.
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
nz = 0
xmin = 0
xmax = 2
ymin = 0
ymax = 2
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
[./diffused]
[./InitialCondition]
type = RandomIC
[../]
[../]
[]
[AuxVariables]
[./C11]
order = CONSTANT
family = MONOMIAL
[../]
[./C12]
order = CONSTANT
family = MONOMIAL
[../]
[./C13]
order = CONSTANT
family = MONOMIAL
[../]
[./C14]
order = CONSTANT
family = MONOMIAL
[../]
[./C15]
order = CONSTANT
family = MONOMIAL
[../]
[./C16]
order = CONSTANT
family = MONOMIAL
[../]
[./C22]
order = CONSTANT
family = MONOMIAL
[../]
[./C23]
order = CONSTANT
family = MONOMIAL
[../]
[./C24]
order = CONSTANT
family = MONOMIAL
[../]
[./C25]
order = CONSTANT
family = MONOMIAL
[../]
[./C26]
order = CONSTANT
family = MONOMIAL
[../]
[./C33]
order = CONSTANT
family = MONOMIAL
[../]
[./C34]
order = CONSTANT
family = MONOMIAL
[../]
[./C35]
order = CONSTANT
family = MONOMIAL
[../]
[./C36]
order = CONSTANT
family = MONOMIAL
[../]
[./C44]
order = CONSTANT
family = MONOMIAL
[../]
[./C45]
order = CONSTANT
family = MONOMIAL
[../]
[./C46]
order = CONSTANT
family = MONOMIAL
[../]
[./C55]
order = CONSTANT
family = MONOMIAL
[../]
[./C56]
order = CONSTANT
family = MONOMIAL
[../]
[./C66]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Modules/TensorMechanics/Master/All]
strain = SMALL
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx'
[]
[Kernels]
[./diff]
type = Diffusion
variable = diffused
[../]
[]
[AuxKernels]
[./matl_C11]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 0
variable = C11
[../]
[./matl_C12]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 1
index_l = 1
variable = C12
[../]
[./matl_C13]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 2
index_l = 2
variable = C13
[../]
[./matl_C14]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 1
index_l = 2
variable = C14
[../]
[./matl_C15]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 2
variable = C15
[../]
[./matl_C16]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 1
variable = C16
[../]
[./matl_C22]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 1
index_l = 1
variable = C22
[../]
[./matl_C23]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 2
index_l = 2
variable = C23
[../]
[./matl_C24]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 1
index_l = 2
variable = C24
[../]
[./matl_C25]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 0
index_l = 2
variable = C25
[../]
[./matl_C26]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 0
index_l = 1
variable = C26
[../]
[./matl_C33]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 2
index_l = 2
variable = C33
[../]
[./matl_C34]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 1
index_l = 2
variable = C34
[../]
[./matl_C35]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 0
index_l = 2
variable = C35
[../]
[./matl_C36]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 0
index_l = 1
variable = C36
[../]
[./matl_C44]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 2
index_k = 1
index_l = 2
variable = C44
[../]
[./matl_C45]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 2
index_k = 0
index_l = 2
variable = C45
[../]
[./matl_C46]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 2
index_k = 0
index_l = 1
variable = C46
[../]
[./matl_C55]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 2
index_k = 0
index_l = 2
variable = C55
[../]
[./matl_C56]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 2
index_k = 0
index_l = 1
variable = C56
[../]
[./matl_C66]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 1
index_k = 0
index_l = 1
variable = C66
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeElasticityTensor
fill_method = symmetric21
C_ijkl ='1111 1122 1133 1123 1113 1112 2222 2233 2223 2213 2212 3333 3323 3313 3312 2323 2313 2312 1313 1312 1212'
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = diffused
boundary = '1'
value = 1
[../]
[./top]
type = DirichletBC
variable = diffused
boundary = '2'
value = 0
[../]
[./disp_x_BC]
type = DirichletBC
variable = disp_x
boundary = '0 2'
value = 0.5
[../]
[./disp_x_BC2]
type = DirichletBC
variable = disp_x
boundary = '1 3'
value = 0.01
[../]
[./disp_y_BC]
type = DirichletBC
variable = disp_y
boundary = '0 2'
value = 0.8
[../]
[./disp_y_BC2]
type = DirichletBC
variable = disp_y
boundary = '1 3'
value = 0.02
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/postprocessor/postprocessor_console.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./diff_v]
type = CoefDiffusion
variable = v
coef = 2
[../]
[]
[BCs]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[./left_u]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = right
value = 3
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = left
value = 2
[../]
[]
[Postprocessors]
[./var1]
type = NumVars
system = 'NL'
[../]
[./var2]
type = NumVars
system = 'NL'
outputs = 'console'
execute_on = 'timestep_begin timestep_end'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
csv = true
[]
(test/tests/meshgenerators/subdomain_bounding_box_generator/oriented_subdomain_bounding_box_generator.i)
[Mesh]
[./gmg]
type = GeneratedMeshGenerator
dim = 3
xmin = -6
xmax = 4
nx = 10
ymin = -2
ymax = 10
ny = 12
zmin = -5
zmax = 7
nz = 12
[]
[./subdomains]
type = OrientedSubdomainBoundingBoxGenerator
input = gmg
center = '-1 4 1'
width = 5
length = 10
height = 4
width_direction = '2 1 0'
length_direction = '-1 2 2'
block_id = 10
[]
[]
[Problem]
type = FEProblem
solve = false
kernel_coverage_check = false
[]
[Variables]
[./u]
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
[]
[Outputs]
exodus = true
[]
(test/tests/fvkernels/fv_simple_diffusion/1d_dirichlet.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 2
[]
[Variables]
[v]
family = MONOMIAL
order = CONSTANT
fv = true
[]
[]
[FVKernels]
[diff]
type = FVDiffusion
variable = v
coeff = coeff
[]
[]
[FVBCs]
[left]
type = FVDirichletBC
variable = v
boundary = left
value = 7
[]
[right]
type = FVDirichletBC
variable = v
boundary = right
value = 42
[]
[]
[Materials]
[diff]
type = ADGenericFunctorMaterial
prop_names = 'coeff'
prop_values = '1'
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/cylindrical/2d-average-no-slip.i)
mu=1
rho=1
advected_interp_method='average'
velocity_interp_method='average'
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 4
nx = 10
ny = 40
[]
[]
[Problem]
fv_bcs_integrity_check = true
coord_type = 'RZ'
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = u
function = 0
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = v
function = 1
[]
[no-slip-wall-u]
type = INSFVNoSlipWallBC
boundary = 'right'
variable = u
function = 0
[]
[no-slip-wall-v]
type = INSFVNoSlipWallBC
boundary = 'right'
variable = v
function = 0
[]
[outlet-p]
type = INSFVOutletPressureBC
boundary = 'top'
variable = pressure
function = 0
[]
[axis-u]
type = INSFVSymmetryVelocityBC
boundary = 'left'
variable = u
u = u
v = v
mu = ${mu}
momentum_component = x
[]
[axis-v]
type = INSFVSymmetryVelocityBC
boundary = 'left'
variable = v
u = u
v = v
mu = ${mu}
momentum_component = y
[]
[axis-p]
type = INSFVSymmetryPressureBC
boundary = 'left'
variable = pressure
[]
[]
[Postprocessors]
[in]
type = SideIntegralVariablePostprocessor
variable = v
boundary = 'bottom'
[]
[out]
type = SideIntegralVariablePostprocessor
variable = v
boundary = 'top'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[]
(test/tests/outputs/xda_xdr/xda_xdr.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
xda = true
xdr = true
[]
(test/tests/transfers/multiapp_copy_transfer/tagged_solution/sub.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 4
[]
[Problem]
extra_tag_solutions = tagged_aux_sol
[]
[Variables/u][]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[force]
type = CoupledForceLagged
variable = u
v = force
tag = tagged_aux_sol
[]
[]
[BCs]
[all]
type = VacuumBC
variable = u
boundary = '0 1 2 3'
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
[AuxVariables/force][]
(modules/ray_tracing/test/tests/userobjects/ray_tracing_study/multiple_subdomains/multiple_subdomains.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 3
ny = 5
xmax = 3
ymax = 5
[]
[subdomain1]
type = ParsedSubdomainMeshGenerator
input = gmg
combinatorial_geometry = 'x > 1 & x < 2'
block_id = 1
[]
[subdomain2]
type = ParsedSubdomainMeshGenerator
input = subdomain1
combinatorial_geometry = 'x > 2'
block_id = 2
[]
[]
[AuxVariables/aux]
order = CONSTANT
family = MONOMIAL
[]
[RayKernels]
[aux0] # add the value of 1 to aux for all Rays that pass through block 0
type = FunctionAuxRayKernelTest
variable = aux
function = 1
block = 0
[]
[aux1] # add the value of 2 to aux for all Rays that pass through block 1
type = FunctionAuxRayKernelTest
variable = aux
function = 2
block = 1
[]
[aux2] # add the value of 3 to aux for all Rays that pass through block 2
type = FunctionAuxRayKernelTest
variable = aux
function = 3
block = 2
[]
[]
[UserObjects/lots]
type = LotsOfRaysRayStudy
execute_on = initial
vertex_to_vertex = false
centroid_to_vertex = false
centroid_to_centroid = true
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/gmv/gmv.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
gmv = true
[]
(tutorials/darcy_thermo_mech/step05_heat_conduction/problems/step5a_steady.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 100
ny = 10
xmax = 0.304 # Length of test chamber
ymax = 0.0257 # Test chamber radius
[]
[Variables]
[temperature]
[]
[]
[Kernels]
[heat_conduction]
type = ADHeatConduction
variable = temperature
[]
[]
[BCs]
[inlet_temperature]
type = DirichletBC
variable = temperature
boundary = left
value = 350 # (K)
[]
[outlet_temperature]
type = DirichletBC
variable = temperature
boundary = right
value = 300 # (K)
[]
[]
[Materials]
[steel]
type = ADGenericConstantMaterial
prop_names = thermal_conductivity
prop_values = 18 # K: (W/m*K) from wikipedia @296K
[]
[]
[Problem]
type = FEProblem
coord_type = RZ
rz_coord_axis = X
[]
[Executioner]
type = Steady
solve_type = NEWTON
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/vectorpostprocessors/spatial_userobject_vector_postprocessor/spatial_userobject.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 10
ny = 10
nz = 10
[]
[Variables]
[dummy]
[]
[]
[Kernels]
[diffusion]
type = Diffusion
variable = dummy
[]
[]
[AuxVariables]
[u]
[]
[np_layered_average]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[u]
type = FunctionAux
variable = u
function = u
[]
[np_layered_average]
type = SpatialUserObjectAux
variable = np_layered_average
user_object = npla
execute_on = timestep_end
[]
[]
[Functions]
[u]
type = ParsedFunction
value = 'x+2*y+3*z'
[]
[]
[UserObjects]
[npla]
type = NearestPointLayeredAverage
direction = x
points = '0.5 0.25 0.25
0.5 0.75 0.25
0.5 0.25 0.75
0.5 0.75 0.75'
num_layers = 3
variable = u
[]
[]
[VectorPostprocessors]
[vpp]
type = SpatialUserObjectVectorPostprocessor
userobject = npla
points_file = points.txt
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
csv = true
execute_on = 'final'
hide = 'dummy'
[]
(modules/navier_stokes/test/tests/finite_volume/cns/mms/1d-with-bcs/varying-eps-hllc.i)
[GlobalParams]
fp = fp
[]
[Mesh]
[cartesian]
type = GeneratedMeshGenerator
dim = 1
xmin = .1
xmax = .6
nx = 2
[]
[]
[Modules]
[FluidProperties]
[fp]
type = IdealGasFluidProperties
[]
[]
[]
[Problem]
fv_bcs_integrity_check = false
[]
[Variables]
[pressure]
type = MooseVariableFVReal
[]
[sup_mom_x]
type = MooseVariableFVReal
[]
[T_fluid]
type = MooseVariableFVReal
[]
[]
[ICs]
[pressure]
type = FunctionIC
variable = pressure
function = 'exact_p'
[]
[sup_mom_x]
type = FunctionIC
variable = sup_mom_x
function = 'exact_rho_ud'
[]
[T_fluid]
type = FunctionIC
variable = T_fluid
function = 'exact_T'
[]
[]
[FVKernels]
[mass_advection]
type = PCNSFVMassHLLC
variable = pressure
[]
[mass_fn]
type = FVBodyForce
variable = pressure
function = 'forcing_rho'
[]
[momentum_x_advection]
type = PCNSFVMomentumHLLC
variable = sup_mom_x
momentum_component = x
[]
[eps_grad]
type = PNSFVPGradEpsilon
variable = sup_mom_x
momentum_component = 'x'
epsilon_function = 'eps'
[]
[momentum_fn]
type = FVBodyForce
variable = sup_mom_x
function = 'forcing_rho_ud'
[]
[fluid_energy_advection]
type = PCNSFVFluidEnergyHLLC
variable = T_fluid
[]
[energy_fn]
type = FVBodyForce
variable = T_fluid
function = 'forcing_rho_et'
[]
[]
[FVBCs]
[mass_left]
variable = pressure
type = PCNSFVStrongBC
boundary = left
T_fluid = 'exact_T'
superficial_velocity = 'exact_superficial_velocity'
eqn = 'mass'
[]
[momentum_left]
variable = sup_mom_x
type = PCNSFVStrongBC
boundary = left
T_fluid = 'exact_T'
superficial_velocity = 'exact_superficial_velocity'
eqn = 'momentum'
momentum_component = 'x'
[]
[energy_left]
variable = T_fluid
type = PCNSFVStrongBC
boundary = left
T_fluid = 'exact_T'
superficial_velocity = 'exact_superficial_velocity'
eqn = 'energy'
[]
[mass_right]
variable = pressure
type = PCNSFVStrongBC
boundary = right
eqn = 'mass'
pressure = 'exact_p'
[]
[momentum_right]
variable = sup_mom_x
type = PCNSFVStrongBC
boundary = right
eqn = 'momentum'
momentum_component = 'x'
pressure = 'exact_p'
[]
[energy_right]
variable = T_fluid
type = PCNSFVStrongBC
boundary = right
eqn = 'energy'
pressure = 'exact_p'
[]
[]
[Materials]
[var_mat]
type = PorousMixedVarMaterial
pressure = pressure
superficial_rhou = sup_mom_x
T_fluid = T_fluid
porosity = porosity
[]
[porosity]
type = GenericFunctionMaterial
prop_names = 'porosity'
prop_values = 'eps'
[]
[]
[Functions]
[exact_rho]
type = ParsedFunction
value = '3.48788261470924*cos(x)'
[]
[forcing_rho]
type = ParsedFunction
value = '-3.83667087618017*sin(1.1*x)*cos(1.3*x) - 4.53424739912202*sin(1.3*x)*cos(1.1*x)'
[]
[exact_rho_ud]
type = ParsedFunction
value = '3.48788261470924*cos(1.1*x)*cos(1.3*x)'
[]
[forcing_rho_ud]
type = ParsedFunction
value = '(-(10.6975765229419*cos(1.5*x)/cos(x) - 0.697576522941849*cos(1.1*x)^2/cos(x)^2)*sin(x) + (10.6975765229419*sin(x)*cos(1.5*x)/cos(x)^2 - 1.3951530458837*sin(x)*cos(1.1*x)^2/cos(x)^3 + 1.53466835047207*sin(1.1*x)*cos(1.1*x)/cos(x)^2 - 16.0463647844128*sin(1.5*x)/cos(x))*cos(x))*cos(1.3*x) + 3.48788261470924*sin(x)*cos(1.1*x)^2*cos(1.3*x)/cos(x)^2 - 7.67334175236034*sin(1.1*x)*cos(1.1*x)*cos(1.3*x)/cos(x) - 4.53424739912202*sin(1.3*x)*cos(1.1*x)^2/cos(x)'
[]
[exact_rho_et]
type = ParsedFunction
value = '26.7439413073546*cos(1.5*x)'
[]
[forcing_rho_et]
type = ParsedFunction
value = '1.0*(3.48788261470924*(3.06706896551724*cos(1.5*x)/cos(x) - 0.2*cos(1.1*x)^2/cos(x)^2)*cos(x) + 26.7439413073546*cos(1.5*x))*sin(x)*cos(1.1*x)*cos(1.3*x)/cos(x)^2 - 1.1*(3.48788261470924*(3.06706896551724*cos(1.5*x)/cos(x) - 0.2*cos(1.1*x)^2/cos(x)^2)*cos(x) + 26.7439413073546*cos(1.5*x))*sin(1.1*x)*cos(1.3*x)/cos(x) - 1.3*(3.48788261470924*(3.06706896551724*cos(1.5*x)/cos(x) - 0.2*cos(1.1*x)^2/cos(x)^2)*cos(x) + 26.7439413073546*cos(1.5*x))*sin(1.3*x)*cos(1.1*x)/cos(x) + 1.0*(-(10.6975765229419*cos(1.5*x)/cos(x) - 0.697576522941849*cos(1.1*x)^2/cos(x)^2)*sin(x) + (10.6975765229419*sin(x)*cos(1.5*x)/cos(x)^2 - 1.3951530458837*sin(x)*cos(1.1*x)^2/cos(x)^3 + 1.53466835047207*sin(1.1*x)*cos(1.1*x)/cos(x)^2 - 16.0463647844128*sin(1.5*x)/cos(x))*cos(x) - 40.1159119610319*sin(1.5*x))*cos(1.1*x)*cos(1.3*x)/cos(x)'
[]
[exact_T]
type = ParsedFunction
value = '0.0106975765229418*cos(1.5*x)/cos(x) - 0.000697576522941848*cos(1.1*x)^2/cos(x)^2'
[]
[exact_eps_p]
type = ParsedFunction
value = '3.48788261470924*(3.06706896551724*cos(1.5*x)/cos(x) - 0.2*cos(1.1*x)^2/cos(x)^2)*cos(x)*cos(1.3*x)'
[]
[exact_p]
type = ParsedFunction
value = '3.48788261470924*(3.06706896551724*cos(1.5*x)/cos(x) - 0.2*cos(1.1*x)^2/cos(x)^2)*cos(x)'
[]
[exact_sup_vel_x]
type = ParsedFunction
value = '1.0*cos(1.1*x)*cos(1.3*x)/cos(x)'
[]
[eps]
type = ParsedFunction
value = 'cos(1.3*x)'
[]
[exact_superficial_velocity]
type = ParsedVectorFunction
value_x = '1.0*cos(1.1*x)*cos(1.3*x)/cos(x)'
[]
[]
[Executioner]
solve_type = NEWTON
type = Steady
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
nl_max_its = 50
line_search = bt
nl_rel_tol = 1e-12
nl_abs_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[]
[Debug]
show_var_residual_norms = true
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2pressure]
type = ElementL2Error
variable = pressure
function = exact_p
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2sup_mom_x]
variable = sup_mom_x
function = exact_rho_ud
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2T_fluid]
variable = T_fluid
function = exact_T
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(test/tests/ics/depend_on_uo/scalar_ic_from_uo.i)
# This test sets an initial condition of a scalar variable from an user object
[Mesh]
type = GeneratedMesh
dim = 2
nx = 8
ny = 8
# We are testing geometric ghosted functors
# so we have to use distributed mesh
parallel_type = distributed
[]
[Variables]
[./u]
[../]
[./a]
family = SCALAR
order = FIRST
[../]
[]
[ICs]
[./ghost_ic]
type = ScalarUOIC
variable = a
user_object = scalar_uo
[../]
[]
[UserObjects]
[./scalar_uo]
type = MTUserObject
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
show = 'a'
[]
[Problem]
kernel_coverage_check = false
[]
(test/tests/ics/component_ic/component_ic.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[./v]
order = SECOND
family = SCALAR
[../]
[]
[AuxVariables]
[./a]
order = SECOND
family = SCALAR
[../]
[]
[ICs]
[./v_ic]
type = ScalarComponentIC
variable = 'v'
values = '1 2'
[../]
[./a_ic]
type = ScalarComponentIC
variable = 'a'
values = '4 5'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[ScalarKernels]
[./ask]
type = AlphaCED
variable = v
value = 100
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Postprocessors]
[./v1]
type = ScalarVariable
variable = v
component = 0
execute_on = 'initial timestep_end'
[../]
[./v2]
type = ScalarVariable
variable = v
component = 1
execute_on = 'initial timestep_end'
[../]
[./a1]
type = ScalarVariable
variable = a
component = 0
execute_on = 'initial timestep_end'
[../]
[./a2]
type = ScalarVariable
variable = a
component = 1
execute_on = 'initial timestep_end'
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
[./out]
type = Exodus
execute_scalars_on = none
[../]
[]
(test/tests/interfacekernels/3d_interface/coupled_value_coupled_flux.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
nx = 2
xmax = 2
ny = 2
ymax = 2
nz = 2
zmax = 2
[]
[./subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '0 0 0'
top_right = '1 1 1'
block_id = 1
[../]
[./break_boundary]
input = subdomain1
type = BreakBoundaryOnSubdomainGenerator
[../]
[./interface]
type = SideSetsBetweenSubdomainsGenerator
input = break_boundary
primary_block = '0'
paired_block = '1'
new_boundary = 'primary0_interface'
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
block = 0
[../]
[./v]
order = FIRST
family = LAGRANGE
block = 1
[../]
[]
[Kernels]
[./diff_u]
type = CoeffParamDiffusion
variable = u
D = 4
block = 0
[../]
[./diff_v]
type = CoeffParamDiffusion
variable = v
D = 2
block = 1
[../]
[./source_u]
type = BodyForce
variable = u
value = 1
[../]
[]
[InterfaceKernels]
[./interface]
type = PenaltyInterfaceDiffusion
variable = u
neighbor_var = v
boundary = primary0_interface
penalty = 1e6
[../]
[]
[BCs]
[./u]
type = VacuumBC
variable = u
boundary = 'left_to_0 bottom_to_0 back_to_0 right top front'
[../]
[./v]
type = VacuumBC
variable = v
boundary = 'left_to_1 bottom_to_1 back_to_1'
[../]
[]
[Postprocessors]
[./u_int]
type = ElementIntegralVariablePostprocessor
variable = u
block = 0
[../]
[./v_int]
type = ElementIntegralVariablePostprocessor
variable = v
block = 1
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
print_linear_residuals = true
[]
(modules/porous_flow/test/tests/pressure_pulse/pressure_pulse_1d_steady_action.i)
# Pressure pulse in 1D with 1 phase - steady
# This file employs the PorousFlowFullySaturated Action. For the non-Action version see pressure_pulse_1d.i
[Mesh]
type = GeneratedMesh
dim = 1
nx = 10
xmin = 0
xmax = 100
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Variables]
[pp]
initial_condition = 2E6
[]
[]
[PorousFlowFullySaturated]
porepressure = pp
gravity = '0 0 0'
fp = simple_fluid
stabilization = Full
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 2e9
density0 = 1000
thermal_expansion = 0
viscosity = 1e-3
[]
[]
[]
[Materials]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1E-15 0 0 0 1E-15 0 0 0 1E-15'
[]
[]
[BCs]
[left]
type = DirichletBC
boundary = left
value = 3E6
variable = pp
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Postprocessors]
[p000]
type = PointValue
variable = pp
point = '0 0 0'
execute_on = 'initial timestep_end'
[]
[p010]
type = PointValue
variable = pp
point = '10 0 0'
execute_on = 'initial timestep_end'
[]
[p020]
type = PointValue
variable = pp
point = '20 0 0'
execute_on = 'initial timestep_end'
[]
[p030]
type = PointValue
variable = pp
point = '30 0 0'
execute_on = 'initial timestep_end'
[]
[p040]
type = PointValue
variable = pp
point = '40 0 0'
execute_on = 'initial timestep_end'
[]
[p050]
type = PointValue
variable = pp
point = '50 0 0'
execute_on = 'initial timestep_end'
[]
[p060]
type = PointValue
variable = pp
point = '60 0 0'
execute_on = 'initial timestep_end'
[]
[p070]
type = PointValue
variable = pp
point = '70 0 0'
execute_on = 'initial timestep_end'
[]
[p080]
type = PointValue
variable = pp
point = '80 0 0'
execute_on = 'initial timestep_end'
[]
[p090]
type = PointValue
variable = pp
point = '90 0 0'
execute_on = 'initial timestep_end'
[]
[p100]
type = PointValue
variable = pp
point = '100 0 0'
execute_on = 'initial timestep_end'
[]
[]
[Outputs]
file_base = pressure_pulse_1d_steady
print_linear_residuals = false
csv = true
[]
(modules/heat_conduction/test/tests/sideset_heat_transfer/gap_thermal_ktemp_1D.i)
[Mesh]
[mesh]
type = GeneratedMeshGenerator
dim = 1
nx = 2
xmax = 2
[]
[split]
type = SubdomainBoundingBoxGenerator
input = mesh
block_id = 1
bottom_left = '1 0 0'
top_right = '2 0 0'
[]
[interface]
type = SideSetsBetweenSubdomainsGenerator
input = split
primary_block = 1
paired_block = 0
new_boundary = 'interface0'
[]
uniform_refine = 4
[]
[Variables]
[T]
order = FIRST
family = MONOMIAL
[]
[]
[AuxVariables]
[Tbulk]
order = FIRST
family = LAGRANGE
initial_condition = 300 # K
[]
[]
[Kernels]
[diff]
type = MatDiffusion
variable = T
diffusivity = conductivity
[]
[source]
type = BodyForce
variable = T
value = 1.0
[]
[]
[DGKernels]
[dg_diff]
type = DGDiffusion
variable = T
epsilon = -1
sigma = 6
diff = conductivity
exclude_boundary = 'interface0'
[]
[]
[InterfaceKernels]
[gap_var]
type = SideSetHeatTransferKernel
variable = T
neighbor_var = T
boundary = 'interface0'
Tbulk_var = Tbulk
[]
[]
[Functions]
# Defining temperature dependent fucntion for conductivity across side set
[kgap]
type = ParsedFunction
value = 't / 200'
[]
[bc_func]
type = ConstantFunction
value = 300
[]
[exact]
type = ParsedFunction
value = '
A := if(x < 1, -0.5, -0.25);
B := if(x < 1, -0.293209850655001, 0.0545267662299068);
C := if(x < 1, 300.206790149345, 300.19547323377);
d := -1;
A * (x+d) * (x+d) + B * (x+d) + C'
[]
[]
[BCs]
[bc_left]
type = DGFunctionDiffusionDirichletBC
boundary = 'left'
variable = T
diff = 'conductivity'
epsilon = -1
sigma = 6
function = bc_func
[]
[bc_right]
type = DGFunctionDiffusionDirichletBC
boundary = 'right'
variable = T
diff = 'conductivity'
epsilon = -1
sigma = 6
function = bc_func
[]
[]
[Materials]
[k0]
type = GenericConstantMaterial
prop_names = 'conductivity'
prop_values = 1.0
block = 0
[]
[k1]
type = GenericConstantMaterial
prop_names = 'conductivity'
prop_values = 2.0
block = 1
[]
[gap_mat]
type = SideSetHeatTransferMaterial
boundary = 'interface0'
# Using temperature dependent function for gap conductivity
conductivity_temperature_function = kgap
# Variable to evaluate conductivity with
gap_temperature = Tbulk
gap_length = 1.0
h_primary = 1
h_neighbor = 1
emissivity_primary = 1
emissivity_neighbor = 1
[]
[]
[Postprocessors]
[error]
type = ElementL2Error
variable = T
function = exact
[]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(test/tests/markers/error_tolerance_marker/error_tolerance_marker_adapt_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 4
nz = 4
uniform_refine = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
[./solution]
type = ParsedFunction
value = (exp(x)-1)/(exp(1)-1)
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./conv]
type = Convection
variable = u
velocity = '1 0 0'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Adaptivity]
steps = 1
marker = marker
[./Indicators]
[./error]
type = AnalyticalIndicator
variable = u
function = solution
[../]
[../]
[./Markers]
[./marker]
type = ErrorToleranceMarker
coarsen = 3e-10
indicator = error
refine = 7e-10
[../]
[../]
[]
[Outputs]
exodus = true
[]
(test/tests/fvkernels/mms/grad-reconstruction/mat-cartesian.i)
a=1.1
diff=1.1
[Mesh]
[gen_mesh]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
[]
[]
[Variables]
[v]
family = MONOMIAL
order = CONSTANT
fv = true
initial_condition = 1
[]
[]
[FVKernels]
[advection]
type = FVElementalAdvection
variable = v
velocity = '${a} ${fparse 2 * a} 0'
advected_quantity = 'mat_u'
grad_advected_quantity = 'mat_grad_u'
[]
[reaction]
type = FVReaction
variable = v
[]
[diff_v]
type = FVDiffusion
variable = v
coeff = ${diff}
[]
[body_v]
type = FVBodyForce
variable = v
function = 'forcing'
[]
[]
[FVBCs]
[diri]
type = FVFunctionDirichletBC
boundary = 'left right top bottom'
function = 'exact'
variable = v
[]
[]
[Materials]
[mat]
type = ADCoupledGradientMaterial
mat_prop = 'mat_u'
grad_mat_prop = 'mat_grad_u'
u = v
[]
[]
[Functions]
[exact]
type = ParsedFunction
value = 'sin(x)*cos(y)'
[]
[forcing]
type = ParsedFunction
value = '-2*a*sin(x)*sin(y) + a*cos(x)*cos(y) + 2*diff*sin(x)*cos(y) + sin(x)*cos(y)'
vars = 'a diff'
vals = '${a} ${diff}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_shift_type -sub_pc_type'
petsc_options_value = 'asm NONZERO lu'
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[error]
type = ElementL2Error
variable = v
function = exact
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(test/tests/outputs/format/output_test_gnuplot.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
nz = 0
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[]
[Postprocessors]
[./dofs]
type = NumDOFs
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
gnuplot = true
[]
(test/tests/dirackernels/aux_scalar_variable/aux_scalar_variable.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
uniform_refine = 2
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./shared]
family = SCALAR
initial_condition = 2
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Postprocessors]
[./source_value]
type = ScalarVariable
variable = shared
execute_on = 'initial timestep_end'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
hide = shared
exodus = true
[]
[DiracKernels]
[./source_0]
variable = u
shared = shared
type = ReportingConstantSource
point = '0.2 0.2'
[../]
[./source_1]
point = '0.8 0.8'
factor = 2
variable = u
shared = shared
type = ReportingConstantSource
[../]
[]
(modules/geochemistry/test/tests/geochemistry_console_output/console.i)
# An example of manually adding a GeochemistryConsoleOutput
[TimeDependentReactionSolver]
model_definition = definition
geochemistry_reactor_name = reactor_name
charge_balance_species = "Cl-"
constraint_species = "H2O H+ Cl- Fe+++"
constraint_value = " 1.0 1.0E-2 1.3E-2 1.0E-3"
constraint_meaning = "kg_solvent_water bulk_composition bulk_composition bulk_composition"
constraint_unit = "kg moles moles moles"
ramp_max_ionic_strength_initial = 0
ramp_max_ionic_strength_subsequent = 1 # so can see the solver_info in the GeochemistryConsoleOutput
kinetic_species_name = "Fe(OH)3(ppd)_nosorb"
kinetic_species_initial_value = "1.0E-6"
kinetic_species_unit = moles
execute_console_output_on = 'final' # can compare with the specially_added one, below
[]
[UserObjects]
[definition]
type = GeochemicalModelDefinition
database_file = "../../database/ferric_hydroxide_sorption.json"
basis_species = "H2O H+ Cl- Fe+++"
kinetic_minerals = "Fe(OH)3(ppd)_nosorb"
[]
[nearest_node]
type = NearestNodeNumberUO
point = '0 0 0' # in this case there is no spatial dependence, so the point is rather irrelevant
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
[specially_added]
type = GeochemistryConsoleOutput
geochemistry_reactor = reactor_name
precision = 8 # 8 digits of precision
mol_cutoff = 1E-8 # species with molality or mole-number lower than this are not outputted
solver_info = true
nearest_node_number_UO = nearest_node
execute_on = 'final' # just output at the end of the simulation
[]
[]
(test/tests/fvkernels/fv_adapt/steady-adapt.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 1
elem_type = QUAD4
[]
[]
[Variables]
[u]
order = CONSTANT
family = MONOMIAL
fv = true
type = MooseVariableFVReal
[]
[]
[Functions]
[exact]
type = ParsedFunction
value = x
[]
[]
[FVKernels]
[diff]
type = FVDiffusion
variable = u
coeff = coeff
use_point_neighbors = true
[]
[]
[FVBCs]
[right]
type = FVDirichletBC
variable = u
boundary = right
value = 1
[]
[left]
type = FVDirichletBC
variable = u
boundary = left
value = 0
[]
[]
[Materials]
[diff]
type = ADGenericFunctorMaterial
prop_names = 'coeff'
prop_values = '1'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type'
petsc_options_value = 'hypre'
[]
[Adaptivity]
marker = box
initial_steps = 1
[Markers]
[box]
bottom_left = '0.5 0 0'
inside = refine
top_right = '1 1 0'
outside = do_nothing
type = BoxMarker
[]
[]
[]
[Outputs]
exodus = true
csv = true
[console]
type = Console
system_info = 'framework mesh aux nonlinear relationship execution'
[]
[]
[Postprocessors]
[error]
type = ElementL2Error
variable = u
function = exact
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(test/tests/parser/parse_double_index/parse_double_index.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[UserObjects]
[./double_index]
type = ReadDoubleIndex
real_di = ' 1.1 ; 2.1 2.2 2.3 ; 3.1 3.2'
uint_di = ' 11 ; 21 22 23 ;
31 32'
int_di = ' 11 ; -21 -22 -23 ;
31 32'
long_di = ' -11 ; 21 22 23 ; -31 -32'
subid_di = '22 ; 32 33 34 ; 42 43'
bid_di = '21 ; 31 32 33 ; 41 42'
str_di = 'string00 ; string10 string11 string12 ; string20 string21 '
file_di = 'file00; file10 file11 file12; file20 file21'
file_no_di = 'file_no00; file_no10 file_no11 file_no12; file_no20 file_no21'
mesh_file_di = 'mesh_file00; mesh_file10 mesh_file11 mesh_file12; mesh_file20 mesh_file21'
subdomain_name_di = 'subdomain_name00; subdomain_name10 subdomain_name11 subdomain_name12; subdomain_name20 subdomain_name21'
boundary_name_di = 'boundary_name00; boundary_name10 boundary_name11 boundary_name12; boundary_name20 boundary_name21'
function_name_di = 'function_name00; function_name10 function_name11 function_name12; function_name20 function_name21'
userobject_name_di = 'userobject_name00; userobject_name10 userobject_name11 userobject_name12; userobject_name20 userobject_name21'
indicator_name_di = 'indicator_name00; indicator_name10 indicator_name11 indicator_name12; indicator_name20 indicator_name21'
marker_name_di = 'marker_name00; marker_name10 marker_name11 marker_name12; marker_name20 marker_name21'
multiapp_name_di = 'multiapp_name00; multiapp_name10 multiapp_name11 multiapp_name12; multiapp_name20 multiapp_name21'
postprocessor_name_di = 'postprocessor_name00; postprocessor_name10 postprocessor_name11 postprocessor_name12; postprocessor_name20 postprocessor_name21'
vector_postprocessor_name_di = 'vector_postprocessor_name00; vector_postprocessor_name10 vector_postprocessor_name11 vector_postprocessor_name12; vector_postprocessor_name20 vector_postprocessor_name21'
output_name_di = 'output_name00; output_name10 output_name11 output_name12; output_name20 output_name21'
material_property_name_di = 'material_property_name00; material_property_name10 material_property_name11 material_property_name12; material_property_name20 material_property_name21'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
file_base = parse_double_index
[]
(modules/heat_conduction/test/tests/radiative_bcs/radiative_bc_cyl.i)
#
# Thin cylindrical shell with very high thermal conductivity
# so that temperature is almost uniform at 500 K. Radiative
# boundary conditions is applied. Heat flux out of boundary
# 'right' should be 3723.36; this is approached as the mesh
# is refined
#
[Mesh]
type = MeshGeneratorMesh
[./cartesian]
type = CartesianMeshGenerator
dim = 2
dx = '1 1'
ix = '1 10'
dy = '1 1'
subdomain_id = '1 2 1 2'
[../]
[./remove_1]
type = BlockDeletionGenerator
block = 1
input = cartesian
[../]
[./readd_left]
type = ParsedGenerateSideset
combinatorial_geometry = 'abs(x - 1) < 1e-4'
new_sideset_name = left
input = remove_1
[../]
[]
[Problem]
coord_type = RZ
[]
[Variables]
[./temp]
initial_condition = 800.0
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[]
[BCs]
[./lefttemp]
type = DirichletBC
boundary = left
variable = temp
value = 800
[../]
[./radiative_bc]
type = InfiniteCylinderRadiativeBC
boundary = right
variable = temp
boundary_radius = 2
boundary_emissivity = 0.2
cylinder_radius = 3
cylinder_emissivity = 0.7
Tinfinity = 500
[../]
[]
[Materials]
[./density]
type = GenericConstantMaterial
prop_names = 'density thermal_conductivity'
prop_values = '1 1.0e5'
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
petsc_options = '-snes_converged_reason'
line_search = none
nl_rel_tol = 1e-6
nl_abs_tol = 1e-7
[]
[Postprocessors]
[./right]
type = SideDiffusiveFluxAverage
variable = temp
boundary = right
diffusivity = thermal_conductivity
[../]
[./min_temp]
type = ElementExtremeValue
variable = temp
value_type = min
[../]
[./max_temp]
type = ElementExtremeValue
variable = temp
value_type = max
[../]
[]
[Outputs]
csv = true
[]
(test/tests/markers/expected_error/displaced_error.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 4
uniform_refine = 1
[]
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[AuxVariables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Steady
[]
[Adaptivity]
[./Markers]
[./test]
type = UniformMarker
# this triggers the expected error
use_displaced_mesh = true
mark = DONT_MARK
[../]
[../]
[]
(test/tests/mesh/mesh_generation/disc_sector_deprecated.i)
# Generates a sector of a Disc Mesh between angle=Pi/4 and angle=3Pi/4
# Radius of outside circle=5
# Solves the diffusion equation with u=-5 at origin, and u=0 on outside
# as well as u=-5+r at angle=Pi/4 and u=-5+r^4/125 at angle=3Pi/4
[Mesh]
type = AnnularMesh
nr = 10
nt = 12
rmin = 0
rmax = 5
tmin = 0.785398163
tmax = 2.356194490
growth_r = 1.3
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./inner]
type = DirichletBC
variable = u
value = -5.0
boundary = rmin
[../]
[./outer]
type = FunctionDirichletBC
variable = u
function = 0
boundary = rmax
[../]
[./tmin]
type = FunctionDirichletBC
variable = u
function = '-5.0+sqrt(x*x + y*y)'
boundary = tmin
[../]
[./tmax]
type = FunctionDirichletBC
variable = u
function = '-5.0+pow(x*x + y*y, 2)/125'
boundary = tmax
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
[]
[Outputs]
exodus = true
[]
(test/tests/kernels/vector_fe/coupled_scalar_default_vector_value.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmin = -1.1
ymin = -1.1
xmax = 1.1
ymax = 1.1
[]
[Variables]
[./v]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = v
[../]
[./source]
type = BodyForce
variable = v
[../]
[./advection]
type = EFieldAdvection
variable = v
charge = 'positive'
mobility = 1
[../]
[]
[BCs]
[left]
type = DirichletBC
variable = v
value = 0
boundary = left
[]
[right]
type = DirichletBC
variable = v
value = 1
boundary = right
[]
[]
[Preconditioning]
[./pre]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type'
petsc_options_value = 'asm'
petsc_options = '-snes_converged_reason -ksp_converged_reason -snes_linesearch_monitor'
[]
[Outputs]
exodus = true
[]
(test/tests/utils/spline_interpolation/bicubic_spline_interpolation_y_normal.i)
[Mesh]
type = GeneratedMesh
dim = 3
ny = 1 # needed to ensure Z is the problem dimension
nx = 4
nz = 4
xmax = 4
zmax = 4
[]
[Functions]
[./yx1]
type = ParsedFunction
value = '3*z^2'
[../]
[./yx2]
type = ParsedFunction
value = '6*x^2'
[../]
[./spline_fn]
type = BicubicSplineFunction
normal_component = y
x1 = '0 2 4'
x2 = '0 2 4 6'
y = '0 16 128 432 8 24 136 440 64 80 192 496'
yx11 = '0 0 0 0'
yx1n = '48 48 48 48'
yx21 = '0 0 0'
yx2n = '216 216 216'
yx1 = 'yx1'
yx2 = 'yx2'
[../]
[./u_func]
type = ParsedFunction
value = 'z^3 + 2*x^3'
[../]
[./u2_forcing_func]
type = ParsedFunction
value = '-6*z - 12*x'
[../]
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./bi_func_value]
order = FIRST
family = LAGRANGE
[../]
[./x_deriv]
order = FIRST
family = LAGRANGE
[../]
[./z_deriv]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./bi_func_value]
type = FunctionAux
variable = bi_func_value
function = spline_fn
[../]
[./deriv_1]
type = FunctionDerivativeAux
function = spline_fn
variable = z_deriv
component = z
[../]
[./deriv_2]
type = FunctionDerivativeAux
function = spline_fn
variable = x_deriv
component = x
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./body_force]
type = BodyForce
variable = u
function = u2_forcing_func
[../]
[]
[BCs]
[./sides]
type = FunctionDirichletBC
variable = u
boundary = 'left right front back'
function = u_func
[../]
[]
[Postprocessors]
[./nodal_l2_err_spline]
type = NodalL2Error
variable = u
function = spline_fn
execute_on = 'initial timestep_end'
[../]
[./nodal_l2_err_analytic]
type = NodalL2Error
variable = u
function = u_func
execute_on = 'initial timestep_end'
[../]
[./x_deriv_err_analytic]
type = NodalL2Error
variable = x_deriv
function = yx2
execute_on = 'initial timestep_end'
[../]
[./z_deriv_err_analytic]
type = NodalL2Error
variable = z_deriv
function = yx1
execute_on = 'initial timestep_end'
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(modules/porous_flow/test/tests/poroperm/PermFromPoro01.i)
# Testing permeability from porosity
# Trivial test, checking calculated permeability is correct
# k = k_anisotropic * f * d^2 * phi^n / (1-phi)^m
[Mesh]
type = GeneratedMesh
dim = 1
nx = 3
xmin = 0
xmax = 3
[]
[GlobalParams]
block = 0
PorousFlowDictator = dictator
[]
[Variables]
[pp]
[InitialCondition]
type = ConstantIC
value = 0
[]
[]
[]
[Kernels]
[flux]
type = PorousFlowAdvectiveFlux
gravity = '0 0 0'
variable = pp
[]
[]
[BCs]
[ptop]
type = DirichletBC
variable = pp
boundary = right
value = 0
[]
[pbase]
type = DirichletBC
variable = pp
boundary = left
value = 1
[]
[]
[AuxVariables]
[poro]
order = CONSTANT
family = MONOMIAL
[]
[perm_x]
order = CONSTANT
family = MONOMIAL
[]
[perm_y]
order = CONSTANT
family = MONOMIAL
[]
[perm_z]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[poro]
type = PorousFlowPropertyAux
property = porosity
variable = poro
[]
[perm_x]
type = PorousFlowPropertyAux
property = permeability
variable = perm_x
row = 0
column = 0
[]
[perm_y]
type = PorousFlowPropertyAux
property = permeability
variable = perm_y
row = 1
column = 1
[]
[perm_z]
type = PorousFlowPropertyAux
property = permeability
variable = perm_z
row = 2
column = 2
[]
[]
[Postprocessors]
[perm_x_bottom]
type = PointValue
variable = perm_x
point = '0 0 0'
[]
[perm_y_bottom]
type = PointValue
variable = perm_y
point = '0 0 0'
[]
[perm_z_bottom]
type = PointValue
variable = perm_z
point = '0 0 0'
[]
[perm_x_top]
type = PointValue
variable = perm_x
point = '3 0 0'
[]
[perm_y_top]
type = PointValue
variable = perm_y
point = '3 0 0'
[]
[perm_z_top]
type = PointValue
variable = perm_z
point = '3 0 0'
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureVG
# unimportant in this fully-saturated test
m = 0.8
alpha = 1e-4
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 2.2e9
viscosity = 1e-3
density0 = 1000
thermal_expansion = 0
[]
[]
[]
[Materials]
[permeability]
type = PorousFlowPermeabilityKozenyCarman
k_anisotropy = '1 0 0 0 2 0 0 0 0.1'
poroperm_function = kozeny_carman_fd2
f = 0.1
d = 5
m = 2
n = 7
[]
[temperature]
type = PorousFlowTemperature
[]
[massfrac]
type = PorousFlowMassFraction
[]
[eff_fluid_pressure]
type = PorousFlowEffectiveFluidPressure
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pp
capillary_pressure = pc
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[porosity]
type = PorousFlowPorosity
porosity_zero = 0.1
[]
[relperm]
type = PorousFlowRelativePermeabilityCorey
n = 0 # unimportant in this fully-saturated situation
phase = 0
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
[]
[]
[Executioner]
solve_type = Newton
type = Steady
l_tol = 1E-5
nl_abs_tol = 1E-3
nl_rel_tol = 1E-8
l_max_its = 200
nl_max_its = 400
petsc_options_iname = '-pc_type -pc_asm_overlap -sub_pc_type -ksp_type -ksp_gmres_restart'
petsc_options_value = ' asm 2 lu gmres 200'
[]
[Outputs]
csv = true
execute_on = 'timestep_end'
[]
(test/tests/postprocessors/function_sideintegral/function_sideintegral.i)
# calculates the integral of various functions over
# boundaries of the mesh. See [Postprocessors] for
# a description of the functions
[Mesh]
type = GeneratedMesh
dim = 3
nx = 5
ny = 5
nz = 5
xmin = -1
xmax = 1
ymin = -2
ymax = 2
zmin = 0
zmax = 6
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[ICs]
[./u]
type = ConstantIC
variable = u
value = 0
[../]
[]
[Postprocessors]
[./zmin]
# no function is provided, so it should default to 1
# yielding postprocessor = 8
type = FunctionSideIntegral
boundary = back
[../]
[./zmax]
# result should be -6*area_of_zmax_sideset = -48
type = FunctionSideIntegral
boundary = front
function = '-z'
[../]
[./ymin]
# since the integrand is odd in x, the result should be zero
type = FunctionSideIntegral
boundary = bottom
function = 'x*pow(z,4)'
[../]
[./ymax]
# result should be 24
type = FunctionSideIntegral
boundary = top
function = 'y*(1+x)*(z-2)'
[../]
[./xmin_and_xmax]
# here the integral is over two sidesets
# result should be 432
type = FunctionSideIntegral
boundary = 'left right'
function = '(3+x)*z'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
file_base = function_sideintegral
[./csv]
type = CSV
[../]
[]
(modules/stochastic_tools/test/tests/surrogates/poly_chaos/sub.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 100
xmax = 10
[]
[Variables]
[u]
[]
[]
[Kernels]
[diffusion]
type = MatDiffusion
variable = u
diffusivity = D
[]
[absorption]
type = MaterialReaction
variable = u
coefficient = sig
[]
[source]
type = BodyForce
variable = u
value = 1.0
[]
[]
[Materials]
[diffusivity]
type = GenericConstantMaterial
prop_names = D
prop_values = 2.0
[]
[xs]
type = GenericConstantMaterial
prop_names = sig
prop_values = 2.0
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 0
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Controls]
[stochastic]
type = SamplerReceiver
[]
[]
[Postprocessors]
[avg]
type = AverageNodalVariableValue
variable = u
[]
[max]
type = NodalExtremeValue
variable = u
value_type = max
[]
[]
[Outputs]
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_mortar/closed_gap_prescribed_pressure.i)
## Units in the input file: m-Pa-s-K
[Mesh]
[left_rectangle]
type = GeneratedMeshGenerator
dim = 2
nx = 40
ny = 10
xmax = 1
ymin = 0
ymax = 0.5
boundary_name_prefix = moving_block
[]
[left_block]
type = SubdomainIDGenerator
input = left_rectangle
subdomain_id = 1
[]
[right_rectangle]
type = GeneratedMeshGenerator
dim = 2
nx = 40
ny = 10
xmin = 1
xmax = 2
ymin = 0
ymax = 0.5
boundary_name_prefix = fixed_block
boundary_id_offset = 4
[]
[right_block]
type = SubdomainIDGenerator
input = right_rectangle
subdomain_id = 2
[]
[two_blocks]
type = MeshCollectionGenerator
inputs = 'left_block right_block'
[]
[block_rename]
type = RenameBlockGenerator
input = two_blocks
old_block = '1 2'
new_block = 'left_block right_block'
[]
[interface_secondary_subdomain]
type = LowerDBlockFromSidesetGenerator
sidesets = 'fixed_block_left'
new_block_id = 3
new_block_name = 'interface_secondary_subdomain'
input = block_rename
[]
[interface_primary_subdomain]
type = LowerDBlockFromSidesetGenerator
sidesets = 'moving_block_right'
new_block_id = 4
new_block_name = 'interface_primary_subdomain'
input = interface_secondary_subdomain
[]
[]
[Variables]
[temperature]
initial_condition = 525.0
[]
[temperature_interface_lm]
block = 'interface_secondary_subdomain'
[]
[]
[AuxVariables]
[interface_normal_lm]
order = FIRST
family = LAGRANGE
block = 'interface_secondary_subdomain'
initial_condition = 100.0
[]
[]
[Kernels]
[HeatDiff_steel]
type = ADHeatConduction
variable = temperature
thermal_conductivity = steel_thermal_conductivity
block = 'left_block'
[]
[HeatDiff_aluminum]
type = ADHeatConduction
variable = temperature
thermal_conductivity = aluminum_thermal_conductivity
block = 'right_block'
[]
[]
[BCs]
[temperature_left]
type = ADDirichletBC
variable = temperature
value = 800
boundary = 'moving_block_left'
[]
[temperature_right]
type = ADDirichletBC
variable = temperature
value = 250
boundary = 'fixed_block_right'
[]
[]
[Constraints]
[thermal_contact]
type = ModularGapConductanceConstraint
variable = temperature_interface_lm
secondary_variable = temperature
primary_boundary = moving_block_right
primary_subdomain = interface_primary_subdomain
secondary_boundary = fixed_block_left
secondary_subdomain = interface_secondary_subdomain
gap_flux_models = 'closed'
[]
[]
[Materials]
[steel_thermal_properties]
type = ADGenericConstantMaterial
prop_names = 'steel_density steel_thermal_conductivity steel_hardness'
prop_values = '8e3 16.2 129' ## for stainless steel 304
block = 'left_block'
[]
[aluminum_thermal_properties]
type = ADGenericConstantMaterial
prop_names = 'aluminum_density aluminum_thermal_conductivity aluminum_hardness'
prop_values = ' 2.7e3 210 15' #for 99% pure Al
block = 'right_block'
[]
[]
[UserObjects]
[closed]
type = GapFluxModelPressureDependentConduction
primary_conductivity = steel_thermal_conductivity
secondary_conductivity = aluminum_thermal_conductivity
temperature = temperature
contact_pressure = interface_normal_lm
primary_hardness = steel_hardness
secondary_hardness = aluminum_hardness
boundary = moving_block_right
[]
[]
[Postprocessors]
[steel_interface_temperature]
type = AverageNodalVariableValue
variable = temperature
block = interface_primary_subdomain
[]
[aluminum_interface_temperature]
type = AverageNodalVariableValue
variable = temperature
block = interface_secondary_subdomain
[]
[interface_heat_flux_steel]
type = ADSideDiffusiveFluxAverage
variable = temperature
boundary = moving_block_right
diffusivity = steel_thermal_conductivity
[]
[interface_heat_flux_aluminum]
type = ADSideDiffusiveFluxAverage
variable = temperature
boundary = fixed_block_left
diffusivity = aluminum_thermal_conductivity
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
automatic_scaling = false
nl_rel_tol = 1e-14
nl_max_its = 20
[]
[Outputs]
csv = true
perf_graph = true
[]
(modules/thermal_hydraulics/test/tests/vectorpostprocessors/sampler_1d_vector/sampler_1d_vector.i)
# Tests the Sampler1DVector vector post-processor, which samples
# a component of a vector-valued material on a block of a 1-D mesh.
[Mesh]
type = GeneratedMesh
xmax = 10
dim = 1
nx = 5
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Materials]
[mat]
type = VectorPropertyTestMaterial
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[VectorPostprocessors]
[test_property_vpp]
type = Sampler1DVector
block = 0
property = test_property
index = 1
sort_by = x
[]
[]
[Outputs]
[out]
type = CSV
file_base = out
execute_vector_postprocessors_on = timestep_end
show = 'test_property_vpp'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/cylindrical/cartesian-version/2d-rc-rz-symmetry.i)
mu=1.1
rho=1.1
offset=0e0
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = ${offset}
xmax = ${fparse 1 + offset}
ymin = -1
ymax = 1
nx = 2
ny = 2
[]
[]
[Problem]
fv_bcs_integrity_check = false
coord_type = 'RZ'
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
two_term_boundary_expansion = true
advected_interp_method = 'average'
velocity_interp_method = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
[]
[v]
type = INSFVVelocityVariable
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[ICs]
[u]
type = FunctionIC
function = 'exact_u'
variable = u
[]
[v]
type = FunctionIC
function = 'exact_v'
variable = v
[]
[pressure]
type = FunctionIC
function = 'exact_p'
variable = pressure
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
rho = ${rho}
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[u_forcing]
type = INSFVBodyForce
variable = u
functor = forcing_u
momentum_component = 'x'
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[v_forcing]
type = INSFVBodyForce
variable = v
functor = forcing_v
momentum_component = 'y'
[]
[]
[FVBCs]
[u_wall]
type = INSFVNoSlipWallBC
variable = u
boundary = 'right'
function = 'exact_u'
[]
[v_wall]
type = INSFVNoSlipWallBC
variable = v
boundary = 'right'
function = 'exact_v'
[]
[p]
type = INSFVOutletPressureBC
variable = pressure
function = 'exact_p'
boundary = 'top'
[]
[inlet_u]
type = INSFVInletVelocityBC
variable = u
function = 'exact_u'
boundary = 'bottom'
[]
[inlet_v]
type = INSFVInletVelocityBC
variable = v
function = 'exact_v'
boundary = 'bottom'
[]
[]
[Functions]
[exact_u]
type = ParsedFunction
value = 'sin(x*pi)^2*cos(y*pi)'
[]
[forcing_u]
type = ADParsedFunction
value = 'pi^2*mu*sin(x*pi)^2*cos(y*pi) - 2*pi*rho*sin(x*pi)^2*sin(y*pi)*cos(x*pi)*cos(y*pi) - pi*sin(x*pi)*cos(1.6*y) + (4*x*pi*rho*sin(x*pi)^3*cos(x*pi)*cos(y*pi)^2 + rho*sin(x*pi)^4*cos(y*pi)^2)/x - (-2*x*pi^2*mu*sin(x*pi)^2*cos(y*pi) + 2*x*pi^2*mu*cos(x*pi)^2*cos(y*pi) + 2*pi*mu*sin(x*pi)*cos(x*pi)*cos(y*pi))/x'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_v]
type = ParsedFunction
value = 'cos(x*pi)*cos(y*pi)'
[]
[forcing_v]
type = ADParsedFunction
value = 'pi^2*mu*cos(x*pi)*cos(y*pi) - 2*pi*rho*sin(y*pi)*cos(x*pi)^2*cos(y*pi) - 1.6*sin(1.6*y)*cos(x*pi) - (-x*pi^2*mu*cos(x*pi)*cos(y*pi) - pi*mu*sin(x*pi)*cos(y*pi))/x + (-x*pi*rho*sin(x*pi)^3*cos(y*pi)^2 + 2*x*pi*rho*sin(x*pi)*cos(x*pi)^2*cos(y*pi)^2 + rho*sin(x*pi)^2*cos(x*pi)*cos(y*pi)^2)/x'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_p]
type = ParsedFunction
value = 'cos(1.6*y)*cos(x*pi)'
[]
[forcing_p]
type = ParsedFunction
value = '-pi*rho*sin(y*pi)*cos(x*pi) + (2*x*pi*rho*sin(x*pi)*cos(x*pi)*cos(y*pi) + rho*sin(x*pi)^2*cos(y*pi))/x'
vars = 'rho'
vals = '${rho}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_shift_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu NONZERO superlu_dist'
line_search = 'none'
nl_rel_tol = 1e-12
nl_abs_tol = 1e-12
[]
[Outputs]
exodus = false
csv = true
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[./L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2v]
type = ElementL2Error
variable = v
function = exact_v
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2p]
variable = pressure
function = exact_p
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[p_avg]
type = ElementAverageValue
variable = pressure
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(test/tests/bcs/bc_preset_nodal/bc_preset_nodal.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
nz = 0
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
# We will use preset BCs
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = bc_preset_out
exodus = true
[]
(tutorials/tutorial01_app_development/step09_mat_props/problems/pressure_diffusion.i)
[Mesh]
type = GeneratedMesh # Can generate simple lines, rectangles and rectangular prisms
dim = 2 # Dimension of the mesh
nx = 100 # Number of elements in the x direction
ny = 10 # Number of elements in the y direction
xmax = 0.304 # Length of test chamber
ymax = 0.0257 # Test chamber radius
[]
[Problem]
type = FEProblem # This is the "normal" type of Finite Element Problem in MOOSE
coord_type = RZ # Axisymmetric RZ
rz_coord_axis = X # Which axis the symmetry is around
[]
[Variables]
[pressure]
# Adds a Linear Lagrange variable by default
[]
[]
[Kernels]
[diffusion]
type = DarcyPressure # Zero-gravity, divergence-free form of Darcy's law
variable = pressure # Operate on the "pressure" variable from above
[]
[]
[Materials]
[filter]
type = PackedColumn # Provides permeability and viscosity of water through packed 1mm spheres
[]
[]
[BCs]
[inlet]
type = ADDirichletBC # Simple u=value BC
variable = pressure # Variable to be set
boundary = left # Name of a sideset in the mesh
value = 4000 # (Pa) From Figure 2 from paper. First data point for 1mm spheres.
[]
[outlet]
type = ADDirichletBC
variable = pressure
boundary = right
value = 0 # (Pa) Gives the correct pressure drop from Figure 2 for 1mm spheres
[]
[]
[Executioner]
type = Steady # Steady state problem
solve_type = NEWTON # Perform a Newton solve
# Set PETSc parameters to optimize solver efficiency
petsc_options_iname = '-pc_type -pc_hypre_type' # PETSc option pairs with values below
petsc_options_value = ' hypre boomeramg'
[]
[Outputs]
exodus = true # Output Exodus format
[]
(modules/thermal_hydraulics/test/tests/jacobians/bcs/external_app_convection_heat_transfer_bc/external_app_convection_heat_transfer_bc.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
[]
[Variables]
[T]
initial_condition = 300
[]
[]
[AuxVariables]
[T_ext]
initial_condition = 400
[]
[htc_ext]
initial_condition = 0.5
[]
[]
[BCs]
[bc]
type = ExternalAppConvectionHeatTransferBC
variable = T
boundary = 0
htc_ext = htc_ext
T_ext = T_ext
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Problem]
kernel_coverage_check = false
[]
[Executioner]
type = Steady
petsc_options = '-snes_test_jacobian'
petsc_options_iname = '-snes_test_error'
petsc_options_value = '1e-8'
[]
(test/tests/outputs/variables/hide_output_via_variables_block.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 10
ny = 10
elem_type = QUAD9
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
outputs = none
[../]
[./v]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./elemental]
order = CONSTANT
family = MONOMIAL
outputs = none
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[AuxKernels]
[./elemental]
type = ConstantAux
variable = elemental
value = 1
[../]
[]
[BCs]
[./left_u]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 3
value = 9
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/mesh/boundary_subdomain_list/2D_9reg.i)
# Create a mesh that looks like:
# -------------
# | 7 | 6 | 5 |
# -------------
# | 8 | 0 | 4 |
# ------------
# | 1 | 2 | 3 |
# -------------
# Where there is an internal interface around block 0
[Mesh]
[mesh]
type = CartesianMeshGenerator
dim = 2
dx = '1 1 1'
dy = '1 1 1'
subdomain_id = '7 6 5
8 0 4
1 2 3'
[]
[interface]
type = SideSetsAroundSubdomainGenerator
input = mesh
block = 0
new_boundary = 'interface'
[]
uniform_refine = 5
[]
# Here we output all the connections as vectorpostprocessors
[VectorPostprocessors]
[interface]
type = SubdomainBoundaryConnectivity
boundary = interface
interface_boundary = true
[]
[interface_master]
type = SubdomainBoundaryConnectivity
boundary = interface
[]
[block_0]
type = SubdomainBoundaryConnectivity
block = 0
[]
[block_1]
type = SubdomainBoundaryConnectivity
block = 1
interface_boundary = true
[]
[block_2]
type = SubdomainBoundaryConnectivity
block = 2
interface_boundary = true
[]
[block_2_master]
type = SubdomainBoundaryConnectivity
block = 2
[]
[]
[Variables]
[u]
[]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
kernel_coverage_check = false
[]
[Outputs]
exodus = false
csv = true
[]
(test/tests/outputs/tecplot/tecplot_append.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
[./out]
type = Tecplot
ascii_append = true
[../]
[]
(modules/porous_flow/test/tests/actions/addjoiner_exception.i)
# Tests that including a PorousFlowJoiner material throws the
# informative deprecation warning rather than a duplicate material property error
[GlobalParams]
PorousFlowDictator = dictator
[]
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Variables]
[p0]
[]
[p1]
[]
[]
[Kernels]
[p0]
type = Diffusion
variable = p0
[]
[p1]
type = Diffusion
variable = p1
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
at_nodes = true
[]
[temperature_qp]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow2PhasePP
at_nodes = true
phase0_porepressure = p0
phase1_porepressure = p1
capillary_pressure = pc
[]
[relperm0]
type = PorousFlowRelativePermeabilityConst
at_nodes = true
kr = 0.5
phase = 0
[]
[relperm1]
type = PorousFlowRelativePermeabilityConst
at_nodes = true
kr = 0.8
phase = 1
[]
[relperm]
type = PorousFlowJoiner
at_nodes = true
material_property = PorousFlow_relative_permeability_nodal
[]
[]
[Executioner]
type = Steady
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'p0 p1'
number_fluid_phases = 2
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureConst
pc = 0
[]
[]
(test/tests/postprocessors/side_average_value/side_average_value_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmin = 0
xmax = 2
ymin = 0
ymax = 1
[]
[Variables]
active = 'u'
[u]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
active = 'diff'
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
active = 'left right'
[left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Postprocessors]
[average]
type = SideAverageValue
boundary = 0
variable = u
[]
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/mesh/mesh_generation/annulus_sector_deprecated.i)
# Generates a sector of an Annular Mesh between angle=Pi/4 and angle=3Pi/4
# Radius of inside circle=1
# Radius of outside circle=5
# Solves the diffusion equation with
# u=0 on inside
# u=log(5) on outside
# u=log(r) at angle=Pi/4 and angle=3Pi/4
[Mesh]
type = AnnularMesh
nr = 10
nt = 12
rmin = 1
rmax = 5
tmin = 0.785398163
tmax = 2.356194490
growth_r = 1.3
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./inner]
type = DirichletBC
variable = u
value = 0.0
boundary = rmin
[../]
[./outer]
type = FunctionDirichletBC
variable = u
function = log(5)
boundary = rmax
[../]
[./min_angle]
type = FunctionDirichletBC
variable = u
function = 'log(sqrt(x*x + y*y))'
boundary = 'tmin tmax'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
[]
[Outputs]
exodus = true
[]
(test/tests/tag/2d_diffusion_vector_tag_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
initial_condition = 1.0
[../]
[]
[AuxVariables]
[./tag_variable1]
order = FIRST
family = LAGRANGE
[../]
[./tag_variable2]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./reaction1]
type = Reaction
variable = u
extra_vector_tags = 'vec_tag1 vec_tag2'
[../]
[./reaction2]
type = Reaction
variable = u
extra_vector_tags = 'vec_tag1 vec_tag2'
[../]
[./reaction3]
type = Reaction
variable = u
[../]
[./reaction4]
type = Reaction
variable = u
[../]
[]
[AuxKernels]
[./TagVectorAux1]
type = TagVectorAux
variable = tag_variable1
v = u
vector_tag = vec_tag1
execute_on = timestep_end
[../]
[./TagVectorAux2]
type = TagVectorAux
variable = tag_variable2
v = u
vector_tag = vec_tag2
execute_on = timestep_end
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
preset = false
boundary = 3
value = 10
extra_vector_tags = vec_tag1
[../]
[./right]
type = DirichletBC
variable = u
preset = false
boundary = 1
value = 100
extra_vector_tags = vec_tag2
[../]
[./right1]
type = DirichletBC
variable = u
preset = false
boundary = 1
value = 100
[../]
[./right2]
type = DirichletBC
variable = u
preset = false
boundary = 1
value = 100
[../]
[]
[Problem]
type = TagTestProblem
extra_tag_vectors = 'vec_tag1 vec_tag2'
test_tag_vectors = 'vec_tag1 vec_tag2'
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
file_base = vector_tag_test_out
exodus = true
[]
(test/tests/postprocessors/element_average_value/element_average_value_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmin = 0
xmax = 2
ymin = 0
ymax = 2
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Postprocessors]
[./average]
type = ElementAverageValue
variable = u
[../]
[]
[Outputs]
exodus = true
csv = true
file_base = out
[]
(test/tests/postprocessors/nodal_sum/nodal_sum_block.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 2
[]
[./left]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '0 0 0'
top_right = '0.5 1 0'
block_id = 100
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Postprocessors]
[./nodal_sum]
type = NodalSum
variable = u
execute_on = 'initial timestep_end'
block = '0 100'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
csv = true
[]
(test/tests/dirackernels/reporter_point_source/3d_vpp.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 10
ny = 10
nz = 10
[]
[Variables]
active = 'u'
[u]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[DiracKernels]
[point_source]
type = ReporterPointSource
variable = u
x_coord_name = csv_reader/x3
y_coord_name = csv_reader/y3
z_coord_name = csv_reader/z3
value_name = csv_reader/value3
[]
[]
[VectorPostprocessors]
[csv_reader]
type = CSVReader
csv_file = point_value_file.csv
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/bcs/coupled_dirichlet_bc/coupled_dirichlet_bc.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[./v]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./coupled_force_u]
type = CoupledForce
variable = u
v = v
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[BCs]
# BCs on left
# u: u=1
# v: v=2
[./left_u]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = 3
value = 2
[../]
# BCs on right
# u: c*u + u^2 + v^2 = 9
# v: no flux
[./right_u]
type = CoupledDirichletBC
variable = u
boundary = 1
value = 9
v=v
[../]
[]
[Preconditioning]
[./precond]
type = SMP
# 'full = true' is required for computeOffDiagJacobian() to get
# called. If you comment this out, you should see that this test
# requires a different number of linear and nonlinear iterations.
full = true
[../]
[]
[Executioner]
type = Steady
# solve_type = 'PJFNK'
solve_type = 'NEWTON'
# Uncomment next line to disable line search. With line search enabled, you must use full=true with Newton or else it will fail.
# line_search = 'none'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
nl_rel_tol = 1e-10
l_tol = 1e-12
nl_max_its = 10
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/materials/functor_properties/1d_dirichlet.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 10
xmax = 2
[]
[Variables]
[v]
type = MooseVariableFVReal
[]
[]
[AuxVariables]
[sink]
type = MooseVariableFVReal
[]
[]
[ICs]
[sink]
type = FunctionIC
variable = sink
function = 'x^3'
[]
[]
[FVKernels]
[diff]
type = FVDiffusion
variable = v
coeff = 1
[]
[sink]
type = FVFunctorElementalKernel
variable = v
functor_name = 'sink_mat'
[]
[]
[FVBCs]
[bounds]
type = FVDirichletBC
variable = v
boundary = 'left right'
value = 0
[]
[]
[Materials]
active = 'functor'
[functor]
type = ADGenericFunctorMaterial
prop_names = sink_mat
prop_values = sink
[]
[overlapping_functor]
type = ADGenericFunctorMaterial
prop_names = 'sink_mat'
prop_values = v
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(modules/porous_flow/test/tests/relperm/corey4.i)
# Test Corey relative permeability curve by varying saturation over the mesh
# Residual saturation of phase 0: s0r = 0.2
# Residual saturation of phase 1: s1r = 0.3
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Variables]
[p0]
initial_condition = 1e6
[]
[s1]
family = LAGRANGE
order = FIRST
[]
[]
[AuxVariables]
[s0aux]
family = MONOMIAL
order = CONSTANT
[]
[s1aux]
family = MONOMIAL
order = CONSTANT
[]
[kr0aux]
family = MONOMIAL
order = CONSTANT
[]
[kr1aux]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[s0]
type = PorousFlowPropertyAux
property = saturation
phase = 0
variable = s0aux
[]
[s1]
type = PorousFlowPropertyAux
property = saturation
phase = 1
variable = s1aux
[]
[kr0]
type = PorousFlowPropertyAux
property = relperm
phase = 0
variable = kr0aux
[]
[kr1]
type = PorousFlowPropertyAux
property = relperm
phase = 1
variable = kr1aux
[]
[]
[Functions]
[s1]
type = ParsedFunction
value = x
[]
[]
[ICs]
[s1]
type = FunctionIC
variable = s1
function = s1
[]
[]
[Kernels]
[p0]
type = Diffusion
variable = p0
[]
[s1]
type = Diffusion
variable = s1
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'p0 s1'
number_fluid_phases = 2
number_fluid_components = 2
[]
[pc]
type = PorousFlowCapillaryPressureConst
pc = 0
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow2PhasePS
phase0_porepressure = p0
phase1_saturation = s1
capillary_pressure = pc
[]
[kr0]
type = PorousFlowRelativePermeabilityCorey
scaling = 0.1
phase = 0
n = 2
s_res = 0.2
sum_s_res = 0.5
[]
[kr1]
type = PorousFlowRelativePermeabilityCorey
scaling = 10.0
phase = 1
n = 2
s_res = 0.3
sum_s_res = 0.5
[]
[]
[VectorPostprocessors]
[vpp]
type = LineValueSampler
warn_discontinuous_face_values = false
variable = 's0aux s1aux kr0aux kr1aux'
start_point = '0 0 0'
end_point = '1 0 0'
num_points = 20
sort_by = id
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
nl_abs_tol = 1e-8
[]
[BCs]
[sleft]
type = DirichletBC
variable = s1
value = 0
boundary = left
[]
[sright]
type = DirichletBC
variable = s1
value = 1
boundary = right
[]
[]
[Outputs]
csv = true
execute_on = timestep_end
[]
(test/tests/postprocessors/element_integral/element_block_integral_test.i)
[Mesh]
file = rectangle.e
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Postprocessors]
[./integral_left]
type = ElementIntegralVariablePostprocessor
variable = u
block = 1
[../]
[./integral_right]
type = ElementIntegralVariablePostprocessor
variable = u
block = 2
[../]
[./integral_all]
type = ElementIntegralVariablePostprocessor
variable = u
[../]
[]
[Outputs]
file_base = out_block
exodus = false
csv = true
[]
(test/tests/outputs/debug/show_material_props_debug.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[./subdomains]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '0.1 0.1 0'
block_id = 1
top_right = '0.9 0.9 0'
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Materials]
[./block]
type = GenericConstantMaterial
block = '0 1'
prop_names = 'property0 property1 property2 property3 property4 property5 property6 property7 property8 property9 property10'
prop_values = '0 1 2 3 4 5 6 7 8 9 10'
[../]
[./boundary]
type = GenericConstantMaterial
prop_names = bnd_prop
boundary = top
prop_values = 12345
[../]
[./restricted]
type = GenericConstantMaterial
block = 1
prop_names = 'restricted0 restricted1'
prop_values = '10 11'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
[Debug]
show_material_props = true
[]
(modules/geochemistry/test/tests/time_dependent_reactions/except6.i)
#Exception: incorrectly sized controlled_activity vectors
[TimeDependentReactionSolver]
model_definition = definition
geochemistry_reactor_name = reactor
charge_balance_species = "Cl-"
constraint_species = "H2O H+ Na+ K+ Ca++ Mg++ Al+++ SiO2(aq) Cl- SO4-- HCO3-"
constraint_value = " 1.0 1E-5 1E-5 1E-5 1E-5 1E-5 1E-5 1E-5 1E-5 1E-5 1E-5"
constraint_meaning = "kg_solvent_water activity bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition"
constraint_unit = "kg dimensionless moles moles moles moles moles moles moles moles moles"
controlled_activity_name = "H+"
controlled_activity_value = '1E-5 0'
[]
[Executioner]
type = Steady
[]
[UserObjects]
[definition]
type = GeochemicalModelDefinition
database_file = "../../../database/moose_geochemdb.json"
basis_species = "H2O H+ Na+ K+ Ca++ Mg++ Al+++ SiO2(aq) Cl- SO4-- HCO3-"
[]
[]
(test/tests/problems/no_material_coverage_check/no_material_coverage_check.i)
[Mesh]
file = rectangle.e
[]
[Problem]
material_coverage_check = false
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./body_force]
type = BodyForce
variable = u
block = 1
value = 10
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Materials]
[./mat1]
type = GenericConstantMaterial
block = 1
prop_names = 'diff1'
prop_values = '1'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/dofmap/simple_screen.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[AuxVariables]
[./w]
[../]
[]
[Kernels]
[./diffu]
type = Diffusion
variable = u
[../]
[./diffv]
type = Diffusion
variable = v
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
[./dofmap]
type = DOFMap
output_screen = true
output_file = false
[../]
[]
(modules/reactor/test/tests/meshgenerators/core_mesh_generator/core.i)
[Mesh]
[rmp]
type = ReactorMeshParams
dim = 3
geom = "Square"
assembly_pitch = 2.84126
axial_regions = '1.0'
axial_mesh_intervals = '1'
top_boundary_id = 201
bottom_boundary_id = 202
radial_boundary_id = 200
[]
[pin1]
type = PinMeshGenerator
reactor_params = rmp
pin_type = 1
pitch = 1.42063
num_sectors = 2
ring_radii = '0.2'
duct_halfpitch = '0.68'
mesh_intervals = '1 1 1'
region_ids='1 2 5'
quad_center_elements = true
[]
[pin2]
type = PinMeshGenerator
reactor_params = rmp
pin_type = 2
pitch = 1.42063
num_sectors = 2
mesh_intervals = '2'
region_ids='2'
quad_center_elements = true
[]
[pin3]
type = PinMeshGenerator
reactor_params = rmp
pin_type = 3
pitch = 1.42063
num_sectors = 2
ring_radii = '0.3818'
mesh_intervals = '1 1'
region_ids='3 4'
quad_center_elements = true
[]
[amg1]
type = AssemblyMeshGenerator
assembly_type = 1
inputs = 'pin2'
pattern = '0 0;
0 0'
[]
[amg2]
type = AssemblyMeshGenerator
assembly_type = 2
inputs = 'pin3 pin1 pin2'
pattern = '0 1;
1 2'
[]
[cmg]
type = CoreMeshGenerator
inputs = 'amg2 amg1 empty'
dummy_assembly_name = empty
pattern = '1 0;
0 1'
extrude = true
[]
[]
[AuxVariables]
[assembly_id]
family = MONOMIAL
order = CONSTANT
[]
[assembly_type_id]
family = MONOMIAL
order = CONSTANT
[]
[plane_id]
family = MONOMIAL
order = CONSTANT
[]
[pin_id]
family = MONOMIAL
order = CONSTANT
[]
[pin_type_id]
family = MONOMIAL
order = CONSTANT
[]
[region_id]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[assembly_id]
type = ExtraElementIDAux
variable = assembly_id
extra_id_name = assembly_id
[]
[assembly_type_id]
type = ExtraElementIDAux
variable = assembly_type_id
extra_id_name = assembly_type_id
[]
[plane_id]
type = ExtraElementIDAux
variable = plane_id
extra_id_name = plane_id
[]
[pin_id]
type = ExtraElementIDAux
variable = pin_id
extra_id_name = pin_id
[]
[pin_type_id]
type = ExtraElementIDAux
variable = pin_type_id
extra_id_name = pin_type_id
[]
[region_id]
type = ExtraElementIDAux
variable = region_id
extra_id_name = region_id
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
file_base = core_in
[]
(test/tests/outputs/format/output_test_gmv.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
nz = 0
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
gmv = true
[]
(test/tests/constraints/tied_value_constraint/tied_value_constraint_test.i)
# [Debug]
# show_top_residuals = 5
# []
[Mesh]
type = FileMesh
file = constraint_test.e
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
# active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
# active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 4
value = 1
[../]
[]
[Constraints]
[./value]
type = TiedValueConstraint
variable = u
secondary = 2
primary = 3
primary_variable = u
[../]
[]
[Preconditioning]
# active = 'FDP'
active = ''
[./FDP]
# full = true
# off_diag_row = 'v'
# off_diag_column = 'u'
type = FDP
[../]
[]
[Executioner]
# l_tol = 1e-1
# l_tol = 1e-
# nl_rel_tol = 1e-14
type = Steady
solve_type = NEWTON
l_max_its = 100
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/tensor_mechanics/test/tests/crack_loop/crack_loop.i)
[Mesh]
file = crack_loop.e
[]
[Problem]
type = FEProblem
solve = false
[]
[UserObjects]
[./crack]
type = CrackFrontDefinition
crack_direction_method = CurvedCrackFront
boundary = 1001
[../]
[]
[Executioner]
type = Steady
[]
(test/tests/misc/check_error/check_dynamic_name_block_mismatch.i)
[Mesh]
file = three_block.e
# These names will be applied on the fly to the
# mesh so they can be used in the input file
# In addition they will show up in the input file
block_id = '1 2'
block_name = 'wood steel copper'
boundary_id = '1 2'
boundary_name = 'left right'
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[../]
[]
[Materials]
active = empty
[./empty]
type = MTMaterial
block = 'wood steel copper'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/mesh/uniform_refine/3d_diffusion.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 16
ny = 16
nz = 16
dim = 3
[../]
parallel_type = distributed
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[ghosting0]
order = CONSTANT
family = MONOMIAL
[]
[ghosting1]
order = CONSTANT
family = MONOMIAL
[]
[ghosting2]
order = CONSTANT
family = MONOMIAL
[]
[]
[UserObjects]
[ghosting_uo0]
type = ElemSideNeighborLayersGeomTester
execute_on = initial
element_side_neighbor_layers = 2
rank = 0
[]
[ghosting_uo1]
type = ElemSideNeighborLayersGeomTester
execute_on = initial
element_side_neighbor_layers = 2
rank = 1
[]
[ghosting_uo2]
type = ElemSideNeighborLayersGeomTester
execute_on = initial
element_side_neighbor_layers = 2
rank = 2
[]
[]
[AuxKernels]
[ghosting0]
type = ElementUOAux
variable = ghosting0
element_user_object = ghosting_uo0
field_name = "ghosted"
execute_on = initial
[]
[ghosting1]
type = ElementUOAux
variable = ghosting1
element_user_object = ghosting_uo1
field_name = "ghosted"
execute_on = initial
[]
[ghosting2]
type = ElementUOAux
variable = ghosting2
element_user_object = ghosting_uo2
field_name = "ghosted"
execute_on = initial
[]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
preset = false
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
preset = false
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
nemesis = true
[]
(modules/ray_tracing/test/tests/raykernels/dependencies/ray_kernel_dependencies.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
[]
[]
[UserObjects/study]
type = RepeatableRayStudy
start_points = '0 0 0'
directions = '1 0 0'
names = ray
ray_data_names = data
initial_ray_data = 1
[]
[RayBCs/kill]
type = KillRayBC
boundary = right
[]
[RayKernels]
[add_1]
type = ChangeRayRayKernelTest
data_name = data
add_value = 1
depends_on = add_10
[]
[scale_5]
type = ChangeRayRayKernelTest
data_name = data
scale_value = 5
depends_on = scale_9
[]
[add_10]
type = ChangeRayRayKernelTest
data_name = data
add_value = 10
[]
[scale_9]
type = ChangeRayRayKernelTest
data_name = data
scale_value = 9
depends_on = add_1
[]
[]
[Postprocessors/value]
type = RayDataValue
study = study
ray_name = ray
data_name = data
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
[]
(test/tests/problems/external_problem/external_steady.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
[]
[Executioner]
type = Steady
[]
[Problem]
type = DummyExternalProblem
[]
(python/peacock/tests/common/bad_mesh.i)
[Mesh]
type = GeneratedMesh
dim = 20
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
# Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/ad_rz_cone_no_parts_steady_stabilized.i)
[GlobalParams]
order = FIRST
integrate_p_by_parts = false
[]
[Mesh]
file = '2d_cone.msh'
[]
[Problem]
coord_type = RZ
[]
[AuxVariables]
[vel_x]
[]
[vel_y]
[]
[]
[AuxKernels]
[vel_x]
type = VectorVariableComponentAux
variable = vel_x
vector_variable = velocity
component = 'x'
[]
[vel_y]
type = VectorVariableComponentAux
variable = vel_y
vector_variable = velocity
component = 'y'
[]
[]
[Variables]
[./velocity]
family = LAGRANGE_VEC
[../]
[./p]
[../]
[]
# Need to set a non-zero initial condition because we have a velocity norm in
# the denominator for the tau coefficient of the stabilization term
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[mass_pspg]
type = INSADMassPSPG
variable = p
[]
[momentum_advection]
type = INSADMomentumAdvection
variable = velocity
[]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
[../]
[momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[]
[]
[BCs]
[p_corner]
type = DirichletBC
boundary = top_right
value = 0
variable = p
[]
[inlet]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom'
function_x = 0
function_y = 'inlet_func'
[../]
[wall]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'right'
function_x = 0
function_y = 0
[]
[axis]
type = ADVectorFunctionDirichletBC
variable = velocity
boundary = 'left'
set_y_comp = false
function_x = 0
[]
[]
[Functions]
[./inlet_func]
type = ParsedFunction
value = '-4 * x^2 + 1'
[../]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[ins_mat]
type = INSADTauMaterial
velocity = velocity
pressure = p
[]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = 'bjacobi ilu 4'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
csv = true
console = true
[./out]
type = Exodus
[../]
[]
[Postprocessors]
[./flow_in]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'bottom'
execute_on = 'timestep_end'
[../]
[./flow_out]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'top'
execute_on = 'timestep_end'
[../]
[]
(test/tests/reporters/base/errors.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
[]
[]
[Reporters/error_test]
type = TestDeclareErrorsReporter
value = value_name
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
(test/tests/postprocessors/nodal_sum/nodal_sum.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 2
[]
[./left]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '0 0 0'
top_right = '0.5 1 0'
block_id = 100
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Postprocessors]
[./nodal_sum]
type = NodalSum
variable = u
execute_on = 'initial timestep_end'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
csv = true
[]
(test/tests/geomsearch/1d_penetration_locator/1d_penetration_locator.i)
[Mesh]
file = 1d_contact.e
dim = 2
construct_side_list_from_node_list = true
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./gap_distance]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left_left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right_right
value = 1
[../]
[]
[AuxKernels]
[./distance]
type = PenetrationAux
variable = gap_distance
boundary = left_right
paired_boundary = right_left
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/heated/2d-rc-heated.i)
mu=1
rho=1
k=1e-3
cp=1
u_inlet=1
T_inlet=200
advected_interp_method='average'
velocity_interp_method='rc'
[Mesh]
[mesh]
type = CartesianMeshGenerator
dim = 2
dx = '5 5'
dy = '1.0'
ix = '50 50'
iy = '20'
subdomain_id = '1 2'
[]
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = PINSFVRhieChowInterpolator
u = superficial_vel_x
v = superficial_vel_y
pressure = pressure
porosity = porosity
[]
[]
[Variables]
inactive = 'T_solid'
[superficial_vel_x]
type = PINSFVSuperficialVelocityVariable
initial_condition = ${u_inlet}
[]
[superficial_vel_y]
type = PINSFVSuperficialVelocityVariable
initial_condition = 1e-6
[]
[pressure]
type = INSFVPressureVariable
[]
[T_fluid]
type = INSFVEnergyVariable
[]
[T_solid]
family = 'MONOMIAL'
order = 'CONSTANT'
fv = true
[]
[]
[AuxVariables]
[T_solid]
family = 'MONOMIAL'
order = 'CONSTANT'
fv = true
initial_condition = 100
[]
[porosity]
family = MONOMIAL
order = CONSTANT
fv = true
initial_condition = 0.5
[]
[]
[FVKernels]
inactive = 'solid_energy_diffusion solid_energy_convection'
[mass]
type = PINSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = PINSFVMomentumAdvection
variable = superficial_vel_x
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
porosity = porosity
momentum_component = 'x'
[]
[u_viscosity]
type = PINSFVMomentumDiffusion
variable = superficial_vel_x
mu = ${mu}
porosity = porosity
momentum_component = 'x'
[]
[u_pressure]
type = PINSFVMomentumPressure
variable = superficial_vel_x
momentum_component = 'x'
pressure = pressure
porosity = porosity
[]
[v_advection]
type = PINSFVMomentumAdvection
variable = superficial_vel_y
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
porosity = porosity
momentum_component = 'y'
[]
[v_viscosity]
type = PINSFVMomentumDiffusion
variable = superficial_vel_y
mu = ${mu}
porosity = porosity
momentum_component = 'y'
[]
[v_pressure]
type = PINSFVMomentumPressure
variable = superficial_vel_y
momentum_component = 'y'
pressure = pressure
porosity = porosity
[]
[energy_advection]
type = PINSFVEnergyAdvection
variable = T_fluid
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
[]
[energy_diffusion]
type = PINSFVEnergyDiffusion
k = ${k}
variable = T_fluid
porosity = porosity
[]
[energy_convection]
type = PINSFVEnergyAmbientConvection
variable = T_fluid
is_solid = false
T_fluid = 'T_fluid'
T_solid = 'T_solid'
h_solid_fluid = 'h_cv'
[]
[solid_energy_diffusion]
type = FVDiffusion
coeff = ${k}
variable = T_solid
[]
[solid_energy_convection]
type = PINSFVEnergyAmbientConvection
variable = T_solid
is_solid = true
T_fluid = 'T_fluid'
T_solid = 'T_solid'
h_solid_fluid = 'h_cv'
[]
[]
[FVBCs]
inactive = 'heated-side'
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = superficial_vel_x
function = ${u_inlet}
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = superficial_vel_y
function = 0
[]
[inlet-T]
type = FVNeumannBC
variable = T_fluid
value = ${fparse u_inlet * rho * cp * T_inlet}
boundary = 'left'
[]
[no-slip-u]
type = INSFVNoSlipWallBC
boundary = 'top'
variable = superficial_vel_x
function = 0
[]
[no-slip-v]
type = INSFVNoSlipWallBC
boundary = 'top'
variable = superficial_vel_y
function = 0
[]
[heated-side]
type = FVDirichletBC
boundary = 'top'
variable = 'T_solid'
value = 150
[]
[symmetry-u]
type = PINSFVSymmetryVelocityBC
boundary = 'bottom'
variable = superficial_vel_x
u = superficial_vel_x
v = superficial_vel_y
mu = ${mu}
momentum_component = 'x'
[]
[symmetry-v]
type = PINSFVSymmetryVelocityBC
boundary = 'bottom'
variable = superficial_vel_y
u = superficial_vel_x
v = superficial_vel_y
mu = ${mu}
momentum_component = 'y'
[]
[symmetry-p]
type = INSFVSymmetryPressureBC
boundary = 'bottom'
variable = pressure
[]
[outlet-p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 0.1
[]
[]
[Materials]
[constants]
type = ADGenericFunctorMaterial
prop_names = 'h_cv'
prop_values = '1'
[]
[functor_constants]
type = ADGenericFunctorMaterial
prop_names = 'cp'
prop_values = '${cp}'
[]
[ins_fv]
type = INSFVEnthalpyMaterial
rho = ${rho}
temperature = 'T_fluid'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-14
[]
# Some basic Postprocessors to examine the solution
[Postprocessors]
[inlet-p]
type = SideAverageValue
variable = pressure
boundary = 'left'
[]
[outlet-u]
type = SideAverageValue
variable = superficial_vel_x
boundary = 'right'
[]
[outlet-temp]
type = SideAverageValue
variable = T_fluid
boundary = 'right'
[]
[solid-temp]
type = ElementAverageValue
variable = T_solid
[]
[]
[Outputs]
exodus = true
csv = false
[]
(test/tests/dirackernels/reporter_point_source/2d_vpp.i)
[Mesh]
[square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[]
uniform_refine = 4
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[DiracKernels]
inactive = 'reporter_point_source_err'
[vpp_point_source]
type = ReporterPointSource
variable = u
value_name = 'csv_reader/u'
x_coord_name = 'csv_reader/x'
y_coord_name = 'csv_reader/y'
z_coord_name = 'csv_reader/z'
[]
[reporter_point_source]
type = ReporterPointSource
variable = u
value_name = 'reporterData2/u2'
x_coord_name = 'reporterData1/x'
y_coord_name = 'reporterData1/y'
z_coord_name = 'reporterData1/z'
[]
[reporter_point_source_err]
type = ReporterPointSource
variable = u
value_name = 'reporterData2/u2'
x_coord_name = 'reporterData2/x2'
y_coord_name = 'reporterData1/y'
z_coord_name = 'reporterData1/z'
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[]
[]
[VectorPostprocessors]
[csv_reader]
type = CSVReader
csv_file = point_value_file.csv
[]
[]
[Reporters]
[reporterData1]
type = ConstantReporter
real_vector_names = 'x y z u'
real_vector_values = '0.2 0.2 0.0; 0.3 0.8 0.0; 0 0 0; 5 5 5'
[]
[reporterData2]
type = ConstantReporter
real_vector_names = 'x2 y2 z2 u2'
real_vector_values = '0.2 0.2; 0.3 0.8 0.0; 0 0 0; 1 -.5 0'
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/radiation_transfer_action/cavity_with_pillar_vf.i)
[Mesh]
[cartesian]
type = CartesianMeshGenerator
dim = 3
dx = '0.1 0.3 0.4 0.3 0.1'
ix = ' 1 3 4 3 1'
dy = '0.1 0.3 0.4 0.3 0.1'
iy = ' 1 3 4 3 1'
dz = '0.1 0.8 0.2 0.1'
iz = ' 1 8 2 1'
subdomain_id = '1 1 1 1 1
1 15 15 15 1
1 15 1 15 1
1 15 15 15 1
1 1 1 1 1
1 12 12 12 1
11 0 103 0 14
11 104 2 102 14
11 0 101 0 14
1 13 13 13 1
1 12 12 12 1
11 0 0 0 14
11 0 105 0 14
11 0 0 0 14
1 13 13 13 1
1 1 1 1 1
1 16 16 16 1
1 16 16 16 1
1 16 16 16 1
1 1 1 1 1'
[]
[left_interior]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 11
paired_block = '0 101 102 103 104 105'
new_boundary = left_interior_wall
input = cartesian
[]
[right_interior]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 14
paired_block = '0 101 102 103 104 105'
new_boundary = right_interior_wall
input = left_interior
[]
[bottom_interior]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 12
paired_block = '0 101 102 103 104 105'
new_boundary = bottom_interior_wall
input = right_interior
[]
[top_interior]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 13
paired_block = '0 101 102 103 104 105'
new_boundary = top_interior_wall
input = bottom_interior
[]
[front_interior]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 15
paired_block = '0 101 102 103 104 105'
new_boundary = front_interior_wall
input = top_interior
[]
[back_interior]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 16
paired_block = '0 101 102 103 104 105'
new_boundary = back_interior_wall
input = front_interior
[]
[pillar_left]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 2
paired_block = 104
new_boundary = pillar_left
input = 'back_interior'
[]
[pillar_right]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 2
paired_block = 102
new_boundary = pillar_right
input = 'pillar_left'
[]
[pillar_bottom]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 2
paired_block = 103
new_boundary = pillar_bottom
input = 'pillar_right'
[]
[pillar_top]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 2
paired_block = 101
new_boundary = pillar_top
input = 'pillar_bottom'
[]
[pillar_back]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 2
paired_block = 105
new_boundary = pillar_back
input = 'pillar_top'
[]
[rename_block]
type = RenameBlockGenerator
old_block = '2 11 12 13 14 15 16 101 102 103 104 105'
new_block = '2 1 1 1 1 1 1 0 0 0 0 0'
input = 'pillar_back'
[]
[]
[GrayDiffuseRadiation]
[cavity]
sidesets = '6 7 8 9 10 11 12 13 14 15 16'
emissivity = '0.8 0.8 0.8 0.8 0.8 0.8 0.8 0.8 0.8 0.8 0.8'
n_patches = '5 5 5 5 5 5 5 5 5 5 5'
partitioners = 'metis metis metis metis metis metis metis metis metis metis metis'
temperature = temperature
ray_tracing_face_order = SECOND
[]
[]
[Variables]
[temperature]
initial_condition = 300
block = '1 2'
[]
[]
[Kernels]
[hc]
type = HeatConduction
variable = temperature
block = '1 2'
[]
[]
[BCs]
[left]
type = DirichletBC
variable = temperature
boundary = left
value = 500
[]
[front]
type = DirichletBC
variable = temperature
boundary = front
value = 300
[]
[]
[Materials]
[hcmat]
type = HeatConductionMaterial
thermal_conductivity = 25.0
specific_heat = 490.0
block = '1 2'
[]
[density]
type = GenericConstantMaterial
prop_names = 'density'
prop_values = '80'
block = '1 2'
[]
[]
[Executioner]
type = Steady
nl_abs_tol = 1e-8
nl_rel_tol = 1e-8
[]
[Outputs]
exodus = true
[]
(test/tests/controls/syntax_based_naming_access/system_object_param.i)
[Mesh]
type = GeneratedMesh
dim = 2
elem_type = QUAD4
# use odd numbers so points do not fall on element boundaries
nx = 31
ny = 31
[]
[Variables]
[./diffused]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = diffused
[../]
[]
[DiracKernels]
[./test_object]
type = MaterialPointSource
point = '0.5 0.5 0'
variable = diffused
[../]
[]
[BCs]
[./bottom_diffused]
type = DirichletBC
variable = diffused
boundary = 'bottom'
value = 2
[../]
[./top_diffused]
type = DirichletBC
variable = diffused
boundary = 'top'
value = 0
[../]
[]
[Materials]
[./mat]
type = GenericConstantMaterial
prop_names = 'matp'
prop_values = '1'
block = 0
[../]
[]
[Postprocessors]
[./test_object]
type = FunctionValuePostprocessor
function = '2*(x+y)'
point = '0.5 0.5 0'
[../]
[./other_point_test_object]
type = FunctionValuePostprocessor
function = '3*(x+y)'
point = '0.5 0.5 0'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
[Controls]
[./point_control]
type = TestControl
test_type = 'point'
parameter = 'DiracKernels/test_object/point'
execute_on = 'initial'
[../]
[]
(test/tests/outputs/console/console_print_toggles.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
# This block is needed so cli_args in the tests files is available
[./console]
type = Console
[../]
[]
(modules/porous_flow/test/tests/gravity/grav01a.i)
# Checking that gravity head is established
# 1phase, vanGenuchten, constant fluid-bulk, constant viscosity, constant permeability, Corey relative perm
# fully saturated
# For better agreement with the analytical solution (ana_pp), just increase nx
[Mesh]
type = GeneratedMesh
dim = 1
nx = 100
xmin = -1
xmax = 0
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Variables]
[pp]
[InitialCondition]
type = RandomIC
min = 0
max = 1
[]
[]
[]
[Kernels]
[flux0]
type = PorousFlowAdvectiveFlux
fluid_component = 0
variable = pp
gravity = '-1 0 0'
[]
[]
[Functions]
[ana_pp]
type = ParsedFunction
vars = 'g B p0 rho0'
vals = '1 1.2 0 1'
value = '-B*log(exp(-p0/B)+g*rho0*x/B)' # expected pp at base
[]
[]
[BCs]
[z]
type = DirichletBC
variable = pp
boundary = right
value = 0
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureVG
m = 0.5
alpha = 1
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 1.2
density0 = 1
viscosity = 1
thermal_expansion = 0
[]
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pp
capillary_pressure = pc
[]
[massfrac]
type = PorousFlowMassFraction
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1 0 0 0 2 0 0 0 3'
[]
[relperm]
type = PorousFlowRelativePermeabilityCorey
n = 1
phase = 0
[]
[]
[Postprocessors]
[pp_base]
type = PointValue
variable = pp
point = '-1 0 0'
[]
[pp_analytical]
type = FunctionValuePostprocessor
function = ana_pp
point = '-1 0 0'
[]
[pp_00]
type = PointValue
variable = pp
point = '0 0 0'
[]
[pp_01]
type = PointValue
variable = pp
point = '-0.1 0 0'
[]
[pp_02]
type = PointValue
variable = pp
point = '-0.2 0 0'
[]
[pp_03]
type = PointValue
variable = pp
point = '-0.3 0 0'
[]
[pp_04]
type = PointValue
variable = pp
point = '-0.4 0 0'
[]
[pp_05]
type = PointValue
variable = pp
point = '-0.5 0 0'
[]
[pp_06]
type = PointValue
variable = pp
point = '-0.6 0 0'
[]
[pp_07]
type = PointValue
variable = pp
point = '-0.7 0 0'
[]
[pp_08]
type = PointValue
variable = pp
point = '-0.8 0 0'
[]
[pp_09]
type = PointValue
variable = pp
point = '-0.9 0 0'
[]
[pp_10]
type = PointValue
variable = pp
point = '-1 0 0'
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = grav01a
[csv]
type = CSV
[]
[]
(test/tests/outputs/exodus/variable_toggles.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[AuxVariables]
[./aux0]
order = SECOND
family = SCALAR
[../]
[./aux1]
family = SCALAR
initial_condition = 5
[../]
[./aux2]
family = SCALAR
initial_condition = 10
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./diff_v]
type = CoefDiffusion
variable = v
coef = 2
[../]
[]
[BCs]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[./left_u]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = right
value = 3
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = left
value = 2
[../]
[]
[Postprocessors]
[./num_vars]
type = NumVars
system = 'NL'
[../]
[./num_aux]
type = NumVars
system = 'AUX'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
[./out]
type = Exodus
[../]
[]
[ICs]
[./aux0_IC]
variable = aux0
values = '12 13'
type = ScalarComponentIC
[../]
[]
(modules/richards/test/tests/newton_cooling/nc02.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1000
ny = 1
xmin = 0
xmax = 100
ymin = 0
ymax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1000
bulk_mod = 1.0E6
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1E-5
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.0
sum_s_res = 0.0
[../]
[./SUPGnone]
type = RichardsSUPGnone
[../]
[]
[Variables]
active = 'pressure'
[./pressure]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = initial_pressure
[../]
[../]
[]
[Functions]
active = 'initial_pressure'
[./initial_pressure]
type = ParsedFunction
value = 2000000-x*1000000/100
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = pressure
boundary = left
value = 2E6
[../]
[./newton]
type = RichardsPiecewiseLinearSink
variable = pressure
boundary = right
pressures = '0 100000 200000 300000 400000 500000 600000 700000 800000 900000 1000000 1100000 1200000 1300000 1400000 1500000 1600000 1700000 1800000 1900000 2000000'
bare_fluxes = '0. 5.6677197748570516e-6 0.000011931518841831313 0.00001885408740732065 0.000026504708864284114 0.000034959953203725676 0.000044304443352900224 0.00005463170211001232 0.00006604508815181467 0.00007865883048198513 0.00009259917167338928 0.00010800563134618119 0.00012503240252705603 0.00014384989486488752 0.00016464644014777016 0.00018763017719085535 0.0002130311349595711 0.00024110353477682344 0.00027212833465544285 0.00030641604122040985 0.00034430981736352295'
use_mobility = false
use_relperm = false
[../]
[]
[Kernels]
active = 'richardsf'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-15 0 0 0 1E-15 0 0 0 1E-15'
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGnone
sat_UO = Saturation
seff_UO = SeffVG
viscosity = 1E-3
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
active = 'andy'
[./andy]
type = SMP
full = true
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-12 1E-15 10000'
[../]
[]
[Executioner]
type = Steady
snesmf_reuse_base = false
[]
[Outputs]
execute_on = 'timestep_end'
file_base = nc02
exodus = true
[]
(test/tests/actions/aux_scalar_variable/aux_scalar_variable.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./a_very_unique_auxiliary_variable_name_good_for_error_checking]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Debug]
show_var_residual_norms = true
[]
(test/tests/variables/second_derivative/interface_kernels.i)
# This is testing a scenario where volumetric system (like kernels) asks for second derivatives
# and the formulation includes a system using neighbor elements (like DGKernels or
# InterfaceKernels)
# If the latter did not request the second derivatives MOOSE should not be computing those.
# The PDEs solved are quite contrived, the Biharmonic kernel is there just to trigger the
# computation of second derivatives.
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 2
xmax = 2
ymax = 2
[]
[./subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '0 0 0'
top_right = '1 2 0'
block_id = 1
[../]
[./interface]
type = SideSetsBetweenSubdomainsGenerator
input = subdomain1
primary_block = '0'
paired_block = '1'
new_boundary = 'middle'
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
block = 0
[../]
[./v]
order = FIRST
family = LAGRANGE
block = 1
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[./bh]
type = Biharmonic
variable = u
[../]
[]
[InterfaceKernels]
[./interface]
type = InterfaceDiffusion
variable = u
neighbor_var = v
boundary = middle
D = 4
D_neighbor = 2
[../]
[]
[BCs]
[./u]
type = DirichletBC
variable = u
value = 1
boundary = 'right middle'
[../]
[./v]
type = DirichletBC
variable = v
value = 2
boundary = 'left middle'
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/action/two_block_new.i)
[Mesh]
[generated_mesh]
type = GeneratedMeshGenerator
dim = 2
nx = 4
ny = 4
[]
[block1]
type = SubdomainBoundingBoxGenerator
block_id = 1
bottom_left = '0 0 0'
top_right = '0.5 1 0'
input = generated_mesh
[]
[block2]
type = SubdomainBoundingBoxGenerator
block_id = 2
bottom_left = '0.5 0 0'
top_right = '1 1 0'
input = block1
[]
[]
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Modules/TensorMechanics/Master]
# parameters that apply to all subblocks are specified at this level. They
# can be overwritten in the subblocks.
add_variables = true
strain = FINITE
generate_output = 'stress_xx'
[./block1]
# the `block` parameter is only valid insde a subblock.
block = 1
[../]
[./block2]
block = 2
# the `additional_generate_output` parameter is also only valid inside a
# subblock. Values specified here are appended to the `generate_output`
# parameter values.
additional_generate_output = 'strain_yy'
[../]
[]
[AuxVariables]
[./stress_theta]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_theta]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./stress_theta]
type = RankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 2
variable = stress_theta
execute_on = timestep_end
[../]
[./strain_theta]
type = RankTwoAux
rank_two_tensor = total_strain
index_i = 2
index_j = 2
variable = strain_theta
execute_on = timestep_end
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e10
poissons_ratio = 0.345
[../]
[./_elastic_stress1]
type = ComputeFiniteStrainElasticStress
block = 1
[../]
[./_elastic_stress2]
type = ComputeFiniteStrainElasticStress
block = 2
[../]
[]
[BCs]
[./left]
type = DirichletBC
boundary = 'left'
variable = disp_x
value = 0.0
[../]
[./top]
type = DirichletBC
boundary = 'top'
variable = disp_y
value = 0.0
[../]
[./right]
type = DirichletBC
boundary = 'right'
variable = disp_x
value = 0.01
[../]
[./bottom]
type = DirichletBC
boundary = 'bottom'
variable = disp_y
value = 0.01
[../]
[]
[Debug]
show_var_residual_norms = true
[]
[Executioner]
type = Steady
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = ' 201 hypre boomeramg 10'
line_search = 'none'
nl_rel_tol = 5e-9
nl_abs_tol = 1e-10
nl_max_its = 15
l_tol = 1e-3
l_max_its = 50
[]
[Outputs]
exodus = true
[]
(test/tests/kernels/array_kernels/array_diffusion_reaction_coupling.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 4
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
components = 2
[]
[v]
[]
[]
[Kernels]
[diff]
type = ArrayDiffusion
variable = u
diffusion_coefficient = dc
[]
[reaction]
type = ArrayReaction
variable = u
reaction_coefficient = rc
[]
[diffv]
type = Diffusion
variable = v
[]
[vu]
type = ArrayCoupledForce
variable = u
v = v
coef = '0 0.5'
[]
[]
[BCs]
[left]
type = ArrayDirichletBC
variable = u
boundary = 1
values = '0 0'
[]
[right]
type = ArrayDirichletBC
variable = u
boundary = 2
values = '1 2'
[]
[leftv]
type = DirichletBC
variable = v
boundary = 1
value = 0
[]
[rightv]
type = DirichletBC
variable = v
boundary = 2
value = 2
[]
[]
[Materials]
[dc]
type = GenericConstantArray
prop_name = dc
prop_value = '1 1'
[]
[rc]
type = GenericConstant2DArray
prop_name = rc
prop_value = '1 0; -0.1 1'
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Postprocessors]
[intu0]
type = ElementIntegralArrayVariablePostprocessor
variable = u
component = 0
[]
[intu1]
type = ElementIntegralArrayVariablePostprocessor
variable = u
component = 1
[]
[intv]
type = ElementIntegralVariablePostprocessor
variable = v
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(test/tests/meshgenerators/mesh_extruder_generator/extrude_angle.i)
[Mesh]
[./fmg]
type = FileMeshGenerator
file = chimney_quad.e
[]
[./extrude]
type = MeshExtruderGenerator
input = fmg
num_layers = 20
extrusion_vector = '1e-2 1e-2 0'
bottom_sideset = '10'
top_sideset = '20'
[]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = u
boundary = 10
value = 0
[../]
[./top]
type = DirichletBC
variable = u
boundary = 20
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out_quad_angle
exodus = true
[]
(modules/porous_flow/test/tests/fluids/simple_fluid_MPa.i)
# Test the properties calculated by the simple fluid Material
# Pressure unit is chosen to be MPa
# Pressure 10 MPa
# Temperature = 300 K (temperature unit = K)
# Density should equal 1500*exp(1E7/1E9-2E-4*300)=1426.844 kg/m^3
# Viscosity should equal 1.1E-9 MPa.s
# Energy density should equal 4000 * 300 = 1.2E6 J/kg
# Specific enthalpy should equal 4000 * 300 + 10e6 / 1426.844 = 1.207008E6 J/kg
[Modules]
[FluidProperties]
[the_simple_fluid]
type = SimpleFluidProperties
thermal_expansion = 2.0E-4
cv = 4000.0
cp = 5000.0
bulk_modulus = 1.0E9
thermal_conductivity = 1.0
viscosity = 1.1E-3
density0 = 1500.0
[]
[]
[]
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp T'
number_fluid_phases = 1
number_fluid_components = 1
[]
[]
[Variables]
[pp]
initial_condition = 10
[]
[T]
initial_condition = 300.0
[]
[]
[Kernels]
[dummy_p]
type = Diffusion
variable = pp
[]
[dummy_T]
type = Diffusion
variable = T
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
temperature = T
[]
[ppss]
type = PorousFlow1PhaseFullySaturated
porepressure = pp
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
temperature_unit = Kelvin
pressure_unit = MPa
fp = the_simple_fluid
phase = 0
[]
[]
[Postprocessors]
[pressure]
type = ElementIntegralVariablePostprocessor
variable = pp
[]
[temperature]
type = ElementIntegralVariablePostprocessor
variable = T
[]
[density]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_fluid_phase_density_qp0'
[]
[viscosity]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_viscosity_qp0'
[]
[internal_energy]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_fluid_phase_internal_energy_qp0'
[]
[enthalpy]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_fluid_phase_enthalpy_qp0'
[]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
csv = true
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_mortar/gap_heat_transfer_mortar_displaced.i)
[Mesh]
displacements = 'disp_x disp_y'
[file]
type = FileMeshGenerator
file = 2blk-gap.e
[]
[secondary]
type = LowerDBlockFromSidesetGenerator
sidesets = '101'
new_block_id = 10001
new_block_name = 'secondary_lower'
input = file
[]
[primary]
type = LowerDBlockFromSidesetGenerator
sidesets = '100'
new_block_id = 10000
new_block_name = 'primary_lower'
input = secondary
[]
[]
[Problem]
kernel_coverage_check = false
material_coverage_check = false
[]
[Variables]
[./temp]
order = FIRST
family = LAGRANGE
block = '1 2'
[../]
[./disp_x]
order = FIRST
family = LAGRANGE
block = '1 2'
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
block = '1 2'
[../]
[./lm]
order = FIRST
family = LAGRANGE
block = 'secondary_lower'
[../]
[]
[Materials]
[./left]
type = ADHeatConductionMaterial
block = 1
thermal_conductivity = 1000
specific_heat = 1
[../]
[./right]
type = ADHeatConductionMaterial
block = 2
thermal_conductivity = 500
specific_heat = 1
[../]
[]
[Kernels]
[./hc_displaced_block]
type = ADHeatConduction
variable = temp
use_displaced_mesh = true
block = '1'
[../]
[./hc_undisplaced_block]
type = ADHeatConduction
variable = temp
use_displaced_mesh = false
block = '2'
[../]
[disp_x]
type = Diffusion
variable = disp_x
block = '1 2'
[]
[disp_y]
type = Diffusion
variable = disp_y
block = '1 2'
[]
[]
[Constraints]
[./ced]
type = GapConductanceConstraint
variable = lm
secondary_variable = temp
k = 100
use_displaced_mesh = true
primary_boundary = 100
primary_subdomain = 10000
secondary_boundary = 101
secondary_subdomain = 10001
displacements = 'disp_x disp_y'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = temp
boundary = 'left'
value = 1
[../]
[./right]
type = DirichletBC
variable = temp
boundary = 'right'
value = 0
[../]
[left_disp_x]
type = DirichletBC
preset = false
variable = disp_x
boundary = 'left'
value = .1
[]
[right_disp_x]
type = DirichletBC
preset = false
variable = disp_x
boundary = 'right'
value = 0
[]
[bottom_disp_y]
type = DirichletBC
preset = false
variable = disp_y
boundary = 'bottom'
value = 0
[]
[]
[Preconditioning]
[./fmp]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-11
[]
[Outputs]
exodus = true
show = 'temp disp_x disp_y'
[dof]
type = DOFMap
execute_on = 'initial'
[]
[]
(test/tests/markers/box_marker/box_marker_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
nz = 0
zmax = 0
elem_type = QUAD4
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Adaptivity]
[./Markers]
[./box]
type = BoxMarker
bottom_left = '0.3 0.3 0'
top_right = '0.6 0.6 0'
inside = refine
outside = do_nothing
[../]
[../]
[]
[Outputs]
exodus = true
[]
(test/tests/problems/dump_objects/add_mat_and_kernel.i)
[Mesh]
type = GeneratedMesh
dim = 2
[]
[AddMatAndKernel]
[]
[Problem]
type = DumpObjectsProblem
dump_path = AddMatAndKernel
[]
[Executioner]
type = Steady
[]
(test/tests/mesh/periodic_node_map/test.i)
[Mesh]
type = GeneratedMesh
nx = 4
ny = 4
nz = 4
[../]
[Variables]
[./c]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = c
[../]
[]
[BCs]
[./Periodic]
[./all]
[../]
[../]
[]
[UserObjects]
[./test]
type = PeriodicNodeMapTester
v = c
execute_on = 'INITIAL'
[../]
[]
[Executioner]
type = Steady
nl_abs_step_tol = 1e-9
[]
[Outputs]
perf_graph = true
[]
(test/tests/ics/from_exodus_solution/nodal_part2.i)
# Use the exodus file for restarting the problem:
# - restart one variable
# - and have one extra variable with IC
#
[Mesh]
file = out_nodal_part1.e
[]
[Functions]
[./exact_fn]
type = ParsedFunction
value = ((x*x)+(y*y))
[../]
[./forcing_fn]
type = ParsedFunction
value = -4
[../]
[]
[Variables]
active = 'u v'
[./u]
order = FIRST
family = LAGRANGE
initial_from_file_var = u
initial_from_file_timestep = 6
[../]
[./v]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = BoundingBoxIC
x1 = 0.0
x2 = 1.0
y1 = 0.0
y2 = 1.0
inside = 3.0
outside = 1.0
[../]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = forcing_fn
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
boundary = '0 1 2 3'
function = exact_fn
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = '3'
value = 0
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = '1'
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out_nodal_var_restart
exodus = true
[]
(tutorials/darcy_thermo_mech/step02_darcy_pressure/tests/kernels/darcy_pressure/darcy_pressure.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 100
ny = 10
xmax = 0.304 # Length of test chamber
ymax = 0.0257 # Test chamber radius
[]
[Variables]
[pressure]
[]
[]
[Kernels]
[darcy_pressure]
type = DarcyPressure
variable = pressure
permeability = 0.8451e-9 # (m^2) 1mm spheres.
[]
[]
[BCs]
[inlet]
type = DirichletBC
variable = pressure
boundary = left
value = 4000 # (Pa) From Figure 2 from paper. First dot for 1mm spheres.
[]
[outlet]
type = DirichletBC
variable = pressure
boundary = right
value = 0 # (Pa) Gives the correct pressure drop from Figure 2 for 1mm spheres
[]
[]
[Problem]
type = FEProblem
coord_type = RZ
rz_coord_axis = X
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/variables/high_order_monomial/high_order_monomial.i)
###########################################################
# This is a simple test demonstrating the use of the
# Higher order monomial variable type.
#
# @Requirement F3.10
###########################################################
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
[]
[Variables]
[./u]
[../]
[]
# Monomial variable types
[AuxVariables]
[./first]
family = MONOMIAL
[../]
[./second]
order = SECOND
family = MONOMIAL
[../]
[./third]
order = THIRD
family = MONOMIAL
[../]
[]
[Functions]
[./first]
type = ParsedFunction
value = 1+2*x+2*y
[../]
[./second]
type = ParsedFunction
value = 1+2*x+4*x*x+2*y+4*y*y+4*x*y
[../]
[./third]
type = ParsedFunction
value = 1+2*x+4*x*x+8*x*x*x+2*y+4*y*y+8*y*y*y+4*x*y+8*x*x*y
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./first]
type = FunctionAux
variable = first
function = first
execute_on = timestep_end
[../]
[./second]
type = FunctionAux
variable = second
function = second
execute_on = timestep_end
[../]
[./third]
type = FunctionAux
variable = third
function = third
execute_on = timestep_end
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Postprocessors]
[./first_error]
type = ElementL2Error
variable = first
function = first
execute_on = 'initial timestep_end'
[../]
[./second_error]
type = ElementL2Error
variable = second
function = second
execute_on = 'initial timestep_end'
[../]
[./third_error]
type = ElementL2Error
variable = third
function = third
execute_on = 'initial timestep_end'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/thermal_hydraulics/test/tests/jacobians/bcs/radiation_heat_flux_bc/radiation_heat_flux_bc.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
[]
[Variables]
[T]
initial_condition = 1000
[]
[]
[BCs]
[bc]
type = RadiativeHeatFluxBC
variable = T
boundary = 0
Tinfinity = 1500
boundary_emissivity = 0.3
view_factor = 0.5
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Problem]
kernel_coverage_check = false
[]
[Executioner]
type = Steady
petsc_options = '-snes_test_jacobian'
petsc_options_iname = '-snes_test_error'
petsc_options_value = '1e-8'
[]
(test/tests/materials/multiple_materials/multiple_materials_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 3
ny = 3
nz = 0
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
active = 'u v'
[./u]
order = FIRST
family = LAGRANGE
[../]
[./v]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./diff1]
order = CONSTANT
family = MONOMIAL
[../]
[./diff2]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff1]
type = DiffMKernel
variable = u
mat_prop = diff1
[../]
[./diff2]
type = DiffMKernel
variable = v
mat_prop = diff2
[../]
[]
[AuxKernels]
[./diff1]
type = MaterialRealAux
variable = diff1
property = diff1
[../]
[./diff2]
type = MaterialRealAux
variable = diff2
property = diff2
[../]
[]
[BCs]
# Mesh Generation produces boundaries in counter-clockwise fashion
[./left_u]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = 3
value = 1
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = 1
value = 0
[../]
[]
[Materials]
[./dm1]
type = GenericConstantMaterial
block = 0
prop_names = 'diff1'
prop_values = '2'
[../]
[./dm2]
type = GenericConstantMaterial
block = 0
prop_names = 'diff2'
prop_values = '4'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[]
(test/tests/misc/check_error/function_file_test5.i)
# Test for usage of missing function
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = ic_function
[../]
[../]
[]
[Functions]
[./ic_function]
type = PiecewiseLinear
data_file = dummy
xy_data = '1 2'
scale_factor = 1.0
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/postprocessors/element_extreme_value/element_extreme_value.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Postprocessors]
[max]
type = ElementExtremeValue
variable = u
[]
[min]
type = ElementExtremeValue
variable = u
value_type = min
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/steady_no_converge.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1e10
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
l_max_its = 10
[]
[Outputs]
exodus = true
[]
(test/tests/userobjects/layered_side_integral/layered_side_integral_fv.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 6
ny = 6
nz = 6
[]
[Variables]
[./u]
order = CONSTANT
family = MONOMIAL
fv = true
[../]
[]
[AuxVariables]
[./layered_integral]
order = CONSTANT
family = MONOMIAL
[../]
[]
[FVKernels]
[./diff]
type = FVDiffusion
variable = u
coeff = 1
[../]
[]
[FVBCs]
[./bottom]
type = FVDirichletBC
variable = u
boundary = bottom
value = 0
[../]
[./top]
type = FVDirichletBC
variable = u
boundary = top
value = 1
[../]
[]
[AuxKernels]
[./liaux]
type = SpatialUserObjectAux
variable = layered_integral
boundary = right
user_object = layered_integral
[../]
[]
[UserObjects]
[./layered_integral]
type = LayeredSideIntegral
direction = y
num_layers = 3
variable = u
execute_on = linear
boundary = right
[../]
[]
[Executioner]
type = Steady
nl_abs_tol = 1e-14
nl_rel_tol = 1e-14
l_abs_tol = 1e-14
l_tol = 1e-6
[]
[Outputs]
exodus = true
[]
(modules/fluid_properties/test/tests/tabulated/tabulated.i)
# Test thermophysical property calculations using TabulatedFluidProperties.
# Calculations for density, internal energy and enthalpy using bicubic spline
# interpolation of data generated using CO2FluidProperties.
[Mesh]
type = GeneratedMesh
dim = 2
# This test uses ElementalVariableValue postprocessors on specific
# elements, so element numbering needs to stay unchanged
allow_renumbering = false
[]
[Variables]
[./dummy]
[../]
[]
[AuxVariables]
[./pressure]
initial_condition = 2e6
family = MONOMIAL
order = CONSTANT
[../]
[./temperature]
initial_condition = 350
family = MONOMIAL
order = CONSTANT
[../]
[./rho]
family = MONOMIAL
order = CONSTANT
[../]
[./mu]
family = MONOMIAL
order = CONSTANT
[../]
[./e]
family = MONOMIAL
order = CONSTANT
[../]
[./h]
family = MONOMIAL
order = CONSTANT
[../]
[./s]
family = MONOMIAL
order = CONSTANT
[../]
[./cv]
family = MONOMIAL
order = CONSTANT
[../]
[./cp]
family = MONOMIAL
order = CONSTANT
[../]
[./c]
family = MONOMIAL
order = CONSTANT
[../]
[]
[AuxKernels]
[./rho]
type = MaterialRealAux
variable = rho
property = density
[../]
[./my]
type = MaterialRealAux
variable = mu
property = viscosity
[../]
[./internal_energy]
type = MaterialRealAux
variable = e
property = e
[../]
[./enthalpy]
type = MaterialRealAux
variable = h
property = h
[../]
[./entropy]
type = MaterialRealAux
variable = s
property = s
[../]
[./cv]
type = MaterialRealAux
variable = cv
property = cv
[../]
[./cp]
type = MaterialRealAux
variable = cp
property = cp
[../]
[./c]
type = MaterialRealAux
variable = c
property = c
[../]
[]
[Modules]
[./FluidProperties]
[./co2]
type = CO2FluidProperties
[../]
[./tabulated]
type = TabulatedFluidProperties
fp = co2
fluid_property_file = fluid_properties.csv
[../]
[]
[]
[Materials]
[./fp_mat]
type = FluidPropertiesMaterialPT
pressure = pressure
temperature = temperature
fp = tabulated
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = dummy
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Postprocessors]
[./rho]
type = ElementalVariableValue
elementid = 0
variable = rho
[../]
[./mu]
type = ElementalVariableValue
elementid = 0
variable = mu
[../]
[./e]
type = ElementalVariableValue
elementid = 0
variable = e
[../]
[./h]
type = ElementalVariableValue
elementid = 0
variable = h
[../]
[./s]
type = ElementalVariableValue
elementid = 0
variable = s
[../]
[./cv]
type = ElementalVariableValue
elementid = 0
variable = cv
[../]
[./cp]
type = ElementalVariableValue
elementid = 0
variable = cp
[../]
[./c]
type = ElementalVariableValue
elementid = 0
variable = c
[../]
[]
[Outputs]
csv = true
file_base = tabulated_out
execute_on = 'TIMESTEP_END'
perf_graph = true
[]
(test/tests/misc/block_boundary_material_check/side_uo_check.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Variables]
[./u]
[../]
[]
[UserObjects]
[./side_uo]
type = MatSideUserObject
mat_prop = 'foo'
boundary = 1
[../]
[]
[Problem]
type = FEProblem
solve = false
kernel_coverage_check = false
[]
[Executioner]
type = Steady
[]
[Outputs]
[]
(test/tests/outputs/exodus/exodus_nodal.i)
##
# \file exodus/exodus_nodal.i
# \example exodus/exodus_nodal.i
# Input file for testing nodal data output
#
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[AuxVariables]
[./aux0]
order = SECOND
family = SCALAR
[../]
[./aux1]
family = SCALAR
initial_condition = 5
[../]
[./aux2]
family = SCALAR
initial_condition = 10
[../]
[./aux3]
family = MONOMIAL
order = CONSTANT
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./diff_v]
type = CoefDiffusion
variable = v
coef = 2
[../]
[]
[BCs]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[./left_u]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = right
value = 3
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = left
value = 2
[../]
[]
[Postprocessors]
[./num_vars]
type = NumVars
system = 'NL'
[../]
[./num_aux]
type = NumVars
system = 'AUX'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
[./out]
type = Exodus
hide = 'u v aux0 aux1'
scalar_as_nodal = true
elemental_as_nodal = true
execute_elemental_on = none
execute_scalars_on = none
execute_postprocessors_on = none
[../]
[]
[ICs]
[./aux0_IC]
variable = aux0
values = '12 13'
type = ScalarComponentIC
[../]
[]
(test/tests/adaptivity/steady/steady.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[subdomain]
type = SubdomainBoundingBoxGenerator
input = gen
bottom_left = '0.25 0.25 0'
top_right = '0.75 0.75 0'
block_id = 100
[]
[]
[Variables/u]
[]
[Kernels/diff]
type = Diffusion
variable = u
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Adaptivity]
initial_marker = uniform
initial_steps = 1
[Markers/uniform]
type = UniformMarker
mark = REFINE
block = 100
[]
[]
[Outputs]
exodus = true
[]
(modules/richards/test/tests/gravity_head_1/gh07.i)
# unsaturated = false
# gravity = true
# supg = true
# transient = false
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
xmin = -1
xmax = 1
[]
[BCs]
[./left]
type = DirichletBC
boundary = left
value = 1
variable = pressure
[../]
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0E3
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 0.1
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = RandomIC
block = 0
min = 0
max = 1
[../]
[../]
[]
[Kernels]
active = 'richardsf'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGstandard
sat_UO = Saturation
seff_UO = SeffVG
viscosity = 1E-3
gravity = '-1 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = gh07
exodus = true
[]
(test/tests/functions/pps_function/pp_function.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./function_force]
function = pp_func
variable = u
type = BodyForce
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
[Functions]
[./pp_func]
pp = right_value
type = PostprocessorFunction
[../]
[]
[Postprocessors]
[./right_value]
variable = u
execute_on = linear
boundary = 1
type = SideAverageValue
[../]
[]
(test/tests/multiapps/steffensen_postprocessor/steady_sub.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
parallel_type = replicated
uniform_refine = 1
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[sink]
type = BodyForce
variable = u
value = -1
[]
[]
[BCs]
[right]
type = PostprocessorDirichletBC
variable = u
boundary = right
postprocessor = 'from_main'
[]
[]
[Postprocessors]
[from_main]
type = Receiver
default = 0
[]
[to_main]
type = SideAverageValue
variable = u
boundary = left
[]
[average]
type = ElementAverageValue
variable = u
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
nl_abs_tol = 1e-14
fixed_point_algorithm = 'steffensen'
[]
[Outputs]
csv = true
exodus = false
[]
(test/tests/dgkernels/advection_diffusion_mixed_bcs_test_resid_jac/dg_advection_diffusion_test.i)
[Mesh]
type = GeneratedMesh
nx = 2
dim = 1
[]
[Kernels]
[./source]
type = BodyForce
variable = u
function = 'forcing_func'
[../]
[./convection]
type = ConservativeAdvection
variable = u
velocity = '1 0 0'
[../]
[./diffusion]
type = MatDiffusionTest
variable = u
prop_name = 'k'
[../]
[]
[DGKernels]
[./convection]
type = DGConvection
variable = u
velocity = '1 0 0'
[../]
[./diffusion]
type = DGDiffusion
variable = u
diff = 'k'
sigma = 6
epsilon = -1
[../]
[]
[BCs]
[./advection]
type = OutflowBC
boundary = 'right'
variable = u
velocity = '1 0 0'
[../]
[./diffusion_left]
type = DGFunctionDiffusionDirichletBC
boundary = 'left'
variable = u
sigma = 6
epsilon = -1
function = 'boundary_left_func'
diff = 'k'
[../]
[]
[Variables]
[./u]
family = MONOMIAL
order = THIRD
[../]
[]
[Materials]
[./test]
block = 0
type = GenericFunctionMaterial
prop_names = 'k'
prop_values = 'k_func'
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Functions]
[./forcing_func]
type = ParsedFunction
value = '1'
[../]
[./boundary_left_func]
type = ParsedFunction
value = '0'
[../]
[./k_func]
type = ParsedFunction
value = '1 + x'
[../]
[]
[Outputs]
exodus = true
execute_on = 'timestep_end'
[]
(test/tests/userobjects/layered_average/layered_average.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./layered_average]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./layered_average]
type = SpatialUserObjectAux
variable = layered_average
execute_on = timestep_end
user_object = average
[../]
[]
[BCs]
[./top]
type = DirichletBC
variable = u
boundary = top
value = 1
[../]
[./bottom]
type = DirichletBC
variable = u
boundary = bottom
value = 0
[../]
[]
[UserObjects]
[./average]
type = LayeredAverage
variable = u
direction = y
num_layers = 2
[../]
[]
[VectorPostprocessors]
[avg]
type = SpatialUserObjectVectorPostprocessor
userobject = average
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
csv = true
[]
(modules/thermal_hydraulics/test/tests/materials/ad_convective_heat_transfer_coefficient/test.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
allow_renumbering = false
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = ADDiffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[AuxVariables]
[Hw]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[Hw_ak]
type = ADMaterialRealAux
variable = Hw
property = Hw
[]
[]
[Materials]
[props]
type = ADGenericConstantMaterial
prop_names = 'Nu k D_h'
prop_values = '1000 2 20'
[]
[Hw_material]
type = ADConvectiveHeatTransferCoefficientMaterial
Nu = Nu
D_h = D_h
k = k
[]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[Hw]
type = ElementalVariableValue
elementid = 0
variable = Hw
[]
[]
[Outputs]
csv = true
execute_on = timestep_end
[]
(test/tests/meshgenerators/distributed_rectilinear/generator/distributed_rectilinear_mesh_generator.i)
[Mesh]
[gmg]
type = DistributedRectilinearMeshGenerator
dim = 2
nx = 100
ny = 100
[]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[pid]
family = MONOMIAL
order = CONSTANT
[]
[npid]
family = Lagrange
order = first
[]
[]
[AuxKernels]
[pid_aux]
type = ProcessorIDAux
variable = pid
execute_on = 'INITIAL'
[]
[npid_aux]
type = ProcessorIDAux
variable = npid
execute_on = 'INITIAL'
[]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
preset = false
boundary = 'left'
value = 0
[../]
[./right]
type = DirichletBC
variable = u
preset = false
boundary = 'right'
value = 1
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type'
petsc_options_value = 'hypre'
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/uo_pps_name_collision_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 5
ny = 5
elem_type = QUAD4
[]
[UserObjects]
[./ud]
type = MTUserObject
scalar = 2
vector = '9 7 5'
[../]
[]
[Functions]
[./forcing_fn]
type = ParsedFunction
value = -2
[../]
[./exact_fn]
type = ParsedFunction
value = x*x
[../]
[]
[Variables]
[./u]
family = LAGRANGE
order = FIRST
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./ffn]
type = UserObjectKernel
variable = u
user_object = ud
[]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
function = exact_fn
boundary = '0 1 2 3'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Postprocessors]
[./ud]
type = NumDOFs
[]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = out
exodus = true
[]
(test/tests/userobjects/solution_user_object/discontinuous_value_solution_uo_p1.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./discontinuous_variable]
order = CONSTANT
family = MONOMIAL
[../]
[./continuous_variable]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
[./discontinuous_function]
type = ParsedFunction
value = 'if(x<0.5,3,5)'
[../]
[./continuous_function]
type = ParsedFunction
value = 'if(x<0.5,x,2*x-0.5)'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[ICs]
[./discontinuous_variable]
type = FunctionIC
variable = discontinuous_variable
function = discontinuous_function
[../]
[./continuous_variable]
type = FunctionIC
variable = continuous_variable
function = continuous_function
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./one]
type = DirichletBC
variable = u
boundary = 'right top bottom'
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
file_base = discontinuous_value_solution_uo_p1
exodus = true
[]
(modules/ray_tracing/test/tests/userobjects/repeatable_ray_study/errors.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
[]
[]
[UserObjects/study]
type = RepeatableRayStudy
names = 'ray'
start_points = '0 0 0'
[]
[RayKernels/null]
type = NullRayKernel
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
(test/tests/misc/serialized_solution/uniform_refine.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
uniform_refine = 1
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./lag]
initial_condition = 2
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Postprocessors]
[./aux]
type = TestSerializedSolution
system = aux
execute_on = 'initial timestep_end'
[../]
[./nl]
type = TestSerializedSolution
system = nl
execute_on = 'initial timestep_end'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/fvkernels/mms/cylindrical/advection-diffusion-reaction.i)
a=1.1
diff=1.1
[Mesh]
[./gen_mesh]
type = GeneratedMeshGenerator
dim = 2
xmin = 2
xmax = 3
ymin = 0
ymax = 1
nx = 2
ny = 2
[../]
[]
[Problem]
coord_type = 'RZ'
[]
[Variables]
[./v]
family = MONOMIAL
order = CONSTANT
fv = true
initial_condition = 1
[../]
[]
[FVKernels]
[./advection]
type = FVAdvection
variable = v
velocity = '${a} ${a} 0'
advected_interp_method = 'average'
[../]
[reaction]
type = FVReaction
variable = v
[]
[diff_v]
type = FVDiffusion
variable = v
coeff = ${diff}
[]
[body_v]
type = FVBodyForce
variable = v
function = 'forcing'
[]
[]
[FVBCs]
[exact]
type = FVFunctionDirichletBC
boundary = 'left right top bottom'
function = 'exact'
variable = v
[]
[]
[Functions]
[exact]
type = ParsedFunction
value = 'sin(x)*cos(y)'
[]
[forcing]
type = ParsedFunction
value = '-a*sin(x)*sin(y) + diff*sin(x)*cos(y) + sin(x)*cos(y) + (x*a*cos(x)*cos(y) + a*sin(x)*cos(y))/x - (-x*diff*sin(x)*cos(y) + diff*cos(x)*cos(y))/x'
vars = 'a diff'
vals = '${a} ${diff}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_shift_type -sub_pc_type'
petsc_options_value = 'asm NONZERO lu'
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[./error]
type = ElementL2Error
variable = v
function = exact
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(test/tests/materials/discrete/recompute_boundary_error.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 1
[]
[left_domain]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '0 0 0'
top_right = '0.5 1 0'
block_id = 10
[]
[]
[Variables]
[u]
initial_condition = 2
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 2
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 3
[]
[]
[Materials]
[recompute_props]
type = RecomputeMaterial
boundary = 'left'
f_name = 'f'
f_prime_name = 'f_prime'
p_name = 'p'
outputs = all
output_properties = 'f f_prime p'
[]
[newton]
type = NewtonMaterial
boundary = 'left right'
outputs = all
f_name = 'f'
f_prime_name = 'f_prime'
p_name = 'p'
material = 'recompute_props'
[]
[left]
type = GenericConstantMaterial
prop_names = 'f f_prime'
prop_values = '1 0.5 '
block = '10 0'
outputs = all
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
print_linear_residuals = true
perf_graph = true
[]
(test/tests/mesh/mixed_dim/1d_2d.i)
[Mesh]
file = 1d_2d.e
# 1d_2d.e contains QUAD4 and BEAM2 elements.
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 4
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[./bottom]
type = DirichletBC
variable = u
boundary = 100
value = 0
[../]
[./top]
type = DirichletBC
variable = u
boundary = 101
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/restart/scalar-var/part1.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 21
[]
[Variables]
[v]
type = MooseVariableFVReal
two_term_boundary_expansion = false
[]
[lambda]
family = SCALAR
order = FIRST
[]
[]
[FVKernels]
[advection]
type = FVElementalAdvection
variable = v
velocity = '1 0 0'
[]
[lambda]
type = FVIntegralValueConstraint
variable = v
lambda = lambda
phi0 = 1
[]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
nl_rel_tol = 1e-12
solve_type = NEWTON
[]
[Outputs]
[out]
type = Exodus
execute_on = 'final'
[]
[]
(modules/thermal_hydraulics/test/tests/materials/ad_prandtl_number/test.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
allow_renumbering = false
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = ADDiffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[AuxVariables]
[Pr]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[RPr_ak]
type = ADMaterialRealAux
variable = Pr
property = Pr
[]
[]
[Materials]
[props]
type = ADGenericConstantMaterial
prop_names = 'cp mu k'
prop_values = '1 2 4'
[]
[Pr_material]
type = ADPrandtlNumberMaterial
cp = cp
k = k
mu = mu
[]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[Pr]
type = ElementalVariableValue
elementid = 0
variable = Pr
[]
[]
[Outputs]
csv = true
execute_on = timestep_end
[]
(test/tests/materials/derivative_material_interface/ad_warn.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
[]
[AuxVariables]
[./dummy]
[../]
[]
[Materials]
[./provider]
type = ADDerivativeMaterialInterfaceTestProvider
block = 0
[../]
[./client]
type = ADDerivativeMaterialInterfaceTestClient
prop_name = prop
block = 0
outputs = exodus
[../]
[./client2]
type = ADDerivativeMaterialInterfaceTestClient
prop_name = 1.0
block = 0
outputs = exodus
[../]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Outputs]
exodus = true
[]
(test/tests/postprocessors/element_integral_var_pps/pps_old_value_fv.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 4
ny = 4
elem_type = QUAD4
[]
[Variables]
[./u]
order = CONSTANT
family = MONOMIAL
fv = true
initial_condition = 1
[../]
[]
[Functions]
[./force_fn]
type = ParsedFunction
value = '1'
[../]
[./exact_fn]
type = ParsedFunction
value = 't'
[../]
[]
[FVKernels]
[./diff_u]
type = FVDiffusion
variable = u
coeff = '1'
block = '0'
[../]
[./ffn_u]
type = FVBodyForce
variable = u
function = force_fn
[../]
[]
[FVBCs]
[./all_u]
type = FVFunctionDirichletBC
variable = u
boundary = '0 1 2 3'
function = exact_fn
[../]
[]
[Postprocessors]
[./a]
type = ElementIntegralVariablePostprocessor
variable = u
execute_on = 'initial timestep_end'
[../]
[./total_a]
type = TimeIntegratedPostprocessor
value = a
execute_on = 'initial timestep_end'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(test/tests/misc/check_error/missing_req_par_action_obj_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
uniform_refine = 4
[]
# This meta-Action is not a MooseObjectAction so we are testing
# missing required parameters on standard Actions (variables)
[ConvectionDiffusion]
[]
[BCs]
active = 'left_convected right_convected left_diffused right_diffused'
[./left_convected]
type = DirichletBC
variable = convected
boundary = '3'
value = 0
[../]
[./right_convected]
type = DirichletBC
variable = convected
boundary = '1'
value = 1
some_var = diffused
[../]
[./left_diffused]
type = DirichletBC
variable = diffused
boundary = '3'
value = 0
[../]
[./right_diffused]
type = DirichletBC
variable = diffused
boundary = '1'
value = 1
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
execute_on = 'timestep_end'
file_base = out
exodus = true
[]
(test/tests/multiapps/command_line/master_common.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
[]
[MultiApps]
[sub]
type = FullSolveMultiApp
positions = '0 0 0
1 1 1'
input_files = 'sub.i'
cli_args = 'Mesh/nx=42'
[]
[]
(test/tests/materials/get_material_property_names/get_material_property_any_boundary_id.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[./add_subdomain]
input = gen
type = SubdomainBoundingBoxGenerator
top_right = '1 1 0'
bottom_left = '0 0.5 0'
block_id = 100
block_name = 'top'
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Materials]
[./boundary]
type = GenericConstantMaterial
prop_names = boundary_prop
boundary = ANY_BOUNDARY_ID
prop_values = 54321
[../]
[]
[UserObjects]
[./get_material_boundary_names_test]
type = GetMaterialPropertyBoundaryBlockNamesTest
expected_names = 'ANY_BOUNDARY_ID'
property_name = 'boundary_prop'
test_type = 'boundary'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/reactor/test/tests/meshgenerators/reporting_id/hexagonal_id/core_reporting_id.i)
[Mesh]
[pin1]
type = PolygonConcentricCircleMeshGenerator
preserve_volumes = true
ring_radii = 0.4
ring_intervals = 1
background_intervals = 1
num_sides = 6
num_sectors_per_side = '2 2 2 2 2 2'
polygon_size = 0.5
[]
[pin2]
type = PolygonConcentricCircleMeshGenerator
preserve_volumes = true
ring_radii = 0.4
ring_intervals = 1
background_intervals = 1
num_sides = 6
num_sectors_per_side = '2 2 2 2 2 2'
polygon_size = 0.5
[]
[assembly1]
type = HexIDPatternedMeshGenerator
inputs = 'pin1 pin2'
pattern_boundary = hexagon
pattern = ' 1 0 1;
0 0 0 0;
1 0 1 0 1;
0 0 0 0;
1 0 1'
hexagon_size = 2.6
duct_sizes = '2.4 2.5'
duct_intervals = '1 1'
id_name = 'pin_id'
assign_type = 'cell'
[]
[assembly2]
type = HexIDPatternedMeshGenerator
inputs = 'pin1 pin2'
pattern_boundary = hexagon
pattern = ' 0 0 0;
0 1 1 0;
0 1 0 1 0;
0 1 1 0;
0 0 0'
hexagon_size = 2.6
duct_sizes = '2.4 2.5'
duct_intervals = '1 1'
id_name = 'pin_id'
assign_type = 'cell'
[]
[core]
type = HexIDPatternedMeshGenerator
inputs = 'assembly1 assembly2'
pattern_boundary = none
pattern = '1 1;
1 0 1;
1 1'
generate_core_metadata = true
id_name = 'assembly_id'
assign_type = 'cell'
[]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[AuxVariables]
[pin_id]
family = MONOMIAL
order = CONSTANT
[]
[assembly_id]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[set_pin_id]
type = ExtraElementIDAux
variable = pin_id
extra_id_name = pin_id
[]
[set_assembly_id]
type = ExtraElementIDAux
variable = assembly_id
extra_id_name = assembly_id
[]
[]
[Outputs]
exodus = true
execute_on = timestep_end
[]
(modules/heat_conduction/test/tests/postprocessors/ad_convective_ht_side_integral.i)
[Mesh]
[./cartesian]
type = CartesianMeshGenerator
dim = 2
dx = '0.45 0.1 0.45'
ix = '5 1 5'
dy = '0.45 0.1 0.45'
iy = '5 1 5'
subdomain_id = '1 1 1
1 2 1
1 1 1'
[../]
[./add_iss_1]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 1
paired_block = 2
new_boundary = 'interface'
input = cartesian
[../]
[./block_deleter]
type = BlockDeletionGenerator
block = 2
input = add_iss_1
[../]
[]
[Variables]
[./temperature]
initial_condition = 300
[../]
[]
[AuxVariables]
[./channel_T]
family = MONOMIAL
order = CONSTANT
initial_condition = 400
[../]
[./channel_Hw]
family = MONOMIAL
order = CONSTANT
initial_condition = 1000
[../]
[]
[Kernels]
[./graphite_diffusion]
type = ADHeatConduction
variable = temperature
thermal_conductivity = 'thermal_conductivity'
[../]
[]
[BCs]
## boundary conditions for the thm channels in the reflector
[./channel_heat_transfer]
type = CoupledConvectiveHeatFluxBC
variable = temperature
htc = channel_Hw
T_infinity = channel_T
boundary = 'interface'
[../]
# hot boundary on the left
[./left]
type = DirichletBC
variable = temperature
value = 1000
boundary = 'left'
[../]
# cool boundary on the right
[./right]
type = DirichletBC
variable = temperature
value = 300
boundary = 'right'
[../]
[]
[Materials]
[./pronghorn_solid_material]
type = ADHeatConductionMaterial
temp = temperature
thermal_conductivity = 25
specific_heat = 1000
[../]
[./htc_material]
type = ADGenericConstantMaterial
prop_names = 'alpha_wall'
prop_values = '1000'
[../]
[./tfluid_mat]
type = ADPiecewiseLinearInterpolationMaterial
property = tfluid_mat
variable = channel_T
x = '400 500'
y = '400 500'
[../]
[]
[Postprocessors]
[./Qw1]
type = ADConvectiveHeatTransferSideIntegral
T_fluid_var = channel_T
htc_var = channel_Hw
T_solid = temperature
boundary = interface
[../]
[./Qw2]
type = ADConvectiveHeatTransferSideIntegral
T_fluid_var = channel_T
htc = alpha_wall
T_solid = temperature
boundary = interface
[../]
[./Qw3]
type = ADConvectiveHeatTransferSideIntegral
T_fluid = tfluid_mat
htc = alpha_wall
T_solid = temperature
boundary = interface
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
[]
(test/tests/parser/map_param/test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 4
[]
[Variables]
[u]
[]
[v]
[]
[w]
[]
[]
[Kernels]
inactive = 'odd_entries bad_value'
[diff]
type = ADDiffusion
variable = u
[]
[diff_v]
type = ADDiffusion
variable = v
[]
[diff_w]
type = ADDiffusion
variable = w
[]
[map]
type = MapMultiplyCoupledVars
variable = u
v = v
w = w
coupled_var_multipliers = 'v 2 w 3'
dummy_string_to_string_map = 'a 1 b c'
dummy_ullong_to_uint_map = '5000000000 1 2 0'
dummy_uint_to_uint_map = '50 1 2 0'
dummy_ulong_to_uint_map = '50 1 2 0'
[]
[odd_entries]
type = MapMultiplyCoupledVars
variable = u
v = v
w = w
coupled_var_multipliers = 'v 2 w'
dummy_string_to_string_map = 'a 1 b c'
dummy_ullong_to_uint_map = '5000000000 1 2 0'
dummy_uint_to_uint_map = '50 1 2 0'
dummy_ulong_to_uint_map = '50 1 2 0'
[]
[bad_value]
type = MapMultiplyCoupledVars
variable = u
v = v
w = w
coupled_var_multipliers = 'v 2 w a'
dummy_string_to_string_map = 'a 1 b c'
dummy_ullong_to_uint_map = '5000000000 1 2 0'
dummy_uint_to_uint_map = '50 1 2 0'
dummy_ulong_to_uint_map = '50 1 2 0'
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[left_v]
type = DirichletBC
variable = v
boundary = left
value = 0
[]
[right_v]
type = DirichletBC
variable = v
boundary = right
value = 1
[]
[left_w]
type = DirichletBC
variable = w
boundary = left
value = 0
[]
[right_w]
type = DirichletBC
variable = w
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'Newton'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(examples/ex12_pbp/ex12.i)
[Mesh]
file = square.e
[]
[Variables]
[./diffused]
order = FIRST
family = LAGRANGE
[../]
[./forced]
order = FIRST
family = LAGRANGE
[../]
[]
# The Preconditioning block
[Preconditioning]
[./PBP]
type = PBP
solve_order = 'diffused forced'
preconditioner = 'LU LU'
off_diag_row = 'forced'
off_diag_column = 'diffused'
[../]
[]
[Kernels]
[./diff_diffused]
type = Diffusion
variable = diffused
[../]
[./conv_forced]
type = CoupledForce
variable = forced
v = diffused
[../]
[./diff_forced]
type = Diffusion
variable = forced
[../]
[]
[BCs]
#Note we have active on and neglect the right_forced BC
active = 'left_diffused right_diffused left_forced'
[./left_diffused]
type = DirichletBC
variable = diffused
boundary = 'left'
value = 0
[../]
[./right_diffused]
type = DirichletBC
variable = diffused
boundary = 'right'
value = 100
[../]
[./left_forced]
type = DirichletBC
variable = forced
boundary = 'left'
value = 0
[../]
[./right_forced]
type = DirichletBC
variable = forced
boundary = 'right'
value = 0
[../]
[]
[Executioner]
type = Steady
solve_type = JFNK
[]
[Outputs]
exodus = true
[]
(modules/functional_expansion_tools/test/tests/errors/invalid_order.i)
[Mesh]
type = GeneratedMesh
dim = 3
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diffusion]
type = Diffusion
variable = u
[../]
[]
[Functions]
[./series]
type = FunctionSeries
series_type = Cartesian
x = Legendre
disc = Zernike
orders = '0 1'
physical_bounds = '-1 1 0 3'
[../]
[]
[Executioner]
type = Steady
[]
(test/tests/misc/check_error/function_file_test9.i)
# Test for usage of missing function
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = ic_function
[../]
[../]
[]
[Functions]
[./ic_function]
type = PiecewiseLinear
scale_factor = 1.0
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/transfers/multiapp_projection_transfer/high_order_sub.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 4
[]
[Functions]
[./test_function]
type = ParsedFunction
value = '2.5*x^2 + 0.75*y^2 + 0.15*x*y'
[../]
[]
[AuxVariables]
[./from_master]
family = monomial
order = first
[../]
[./test_var]
family = monomial
order = first
[./InitialCondition]
type = FunctionIC
function = test_function
[../]
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(test/tests/outputs/format/pps_screen_out_warn.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
nz = 0
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Postprocessors]
[./avg_block]
type = ElementAverageValue
variable = u
outputs = 'console'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
[./console]
type = Console
execute_postprocessors_on = none
[../]
[]
(test/tests/mortar/convergence-studies/continuity-3d/continuity.i)
[Mesh]
second_order = true
[file]
type = FileMeshGenerator
file = hex_mesh.e
[]
[secondary]
input = file
type = LowerDBlockFromSidesetGenerator
new_block_id = 11
new_block_name = "secondary"
sidesets = '101'
[]
[primary]
input = secondary
type = LowerDBlockFromSidesetGenerator
new_block_id = 12
new_block_name = "primary"
sidesets = '102'
[]
[]
[Problem]
kernel_coverage_check = false
[]
[Variables]
[T]
block = '1 2'
order = SECOND
[]
[lambda]
block = 'secondary'
# family = MONOMIAL
# order = CONSTANT
family = LAGRANGE
order = SECOND
use_dual = true
[]
[]
[BCs]
[neumann]
type = FunctionGradientNeumannBC
exact_solution = exact_soln_primal
variable = T
boundary = '1 2'
[]
[]
[Kernels]
[conduction]
type = Diffusion
variable = T
block = '1 2'
[]
[sink]
type = Reaction
variable = T
block = '1 2'
[]
[forcing_function]
type = BodyForce
variable = T
function = forcing_function
block = '1 2'
[]
[]
[Functions]
[forcing_function]
type = ParsedFunction
value = 'sin(x*pi)*sin(y*pi)*sin(z*pi) + 3*pi^2*sin(x*pi)*sin(y*pi)*sin(z*pi)'
[]
[exact_soln_primal]
type = ParsedFunction
value = 'sin(x*pi)*sin(y*pi)*sin(z*pi)'
[]
[exact_soln_lambda]
type = ParsedFunction
value = 'pi*sin(pi*y)*sin(pi*z)*cos(pi*x)'
[]
[]
[Debug]
show_var_residual_norms = 1
[]
[Constraints]
[mortar]
type = EqualValueConstraint
primary_boundary = 2
secondary_boundary = 1
primary_subdomain = '12'
secondary_subdomain = '11'
variable = lambda
secondary_variable = T
# delta = 0.1
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
solve_type = NEWTON
type = Steady
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_shift_type '
'-pc_factor_shift_amount'
petsc_options_value = 'lu basic NONZERO 1e-15'
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[L2lambda]
type = ElementL2Error
variable = lambda
function = exact_soln_lambda
execute_on = 'timestep_end'
block = 'secondary'
[]
[L2u]
type = ElementL2Error
variable = T
function = exact_soln_primal
execute_on = 'timestep_end'
block = '1 2'
[]
[h]
type = AverageElementSize
block = '1 2'
[]
[]
(modules/ray_tracing/test/tests/traceray/internal_sidesets/internal_sidesets_1d.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
xmax = 6
nx = 6
[]
[central_block]
type = SubdomainBoundingBoxGenerator
input = gmg
block_id = 1
bottom_left = '2 0 0'
top_right = '4 0 0'
[]
[central_boundary]
type = SideSetsBetweenSubdomainsGenerator
input = central_block
primary_block = 1
paired_block = 0
new_boundary = 7
[]
[]
[RayBCs]
active = 'kill_internal'
# active = 'kill_external reflect_internal'
# for testing internal kill
[kill_internal]
type = KillRayBC
boundary = 7
[]
# for testing internal reflect
[kill_external]
type = KillRayBC
boundary = 'left right'
[]
[reflect_internal]
type = ReflectRayBC
boundary = 7
[]
[]
[UserObjects/study]
type = RepeatableRayStudy
start_points = '0 0 0
2 0 0
6 0 0
4 0 0
3 0 0'
directions = '1 0 0
1 0 0
-1 0 0
-1 0 0
-1 0 0'
names = 'left_in at_left right_in at_right inside_left'
ray_distance = 10
execute_on = initial
ray_kernel_coverage_check = false
use_internal_sidesets = true
[]
[Postprocessors/total_distance]
type = RayTracingStudyResult
study = study
result = total_distance
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Outputs]
exodus = false
csv = true
[]
(test/tests/interfacekernels/1d_interface/no-failed-point-inversions.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 10
xmax = 2
[]
[subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '1.0 0 0'
block_id = 1
top_right = '2.0 1.0 0'
[]
[interface]
input = subdomain1
type = SideSetsBetweenSubdomainsGenerator
primary_block = '0'
paired_block = '1'
new_boundary = 'primary0_interface'
[]
[break]
type = BreakMeshByBlockGenerator
input = interface
[]
displacements = 'disp_x'
[]
[AuxVariables]
[disp_x][]
[]
[ICs]
[right]
type = ConstantIC
variable = disp_x
block = 1
value = 1
[]
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
block = '0'
[]
[v]
order = FIRST
family = LAGRANGE
block = '1'
[]
[]
[Kernels]
[diff_u]
type = CoeffParamDiffusion
variable = u
D = 4
block = 0
[]
[diff_v]
type = CoeffParamDiffusion
variable = v
D = 2
block = 1
[]
[]
[InterfaceKernels]
[penalty_interface]
type = PenaltyInterfaceDiffusion
variable = u
neighbor_var = v
boundary = primary0_interface
penalty = 1e6
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 1
[]
[right]
type = DirichletBC
variable = v
boundary = 'right'
value = 0
[]
[]
[Materials]
[block0]
type = GenericConstantMaterial
block = '0'
prop_names = 'D'
prop_values = '4'
[]
[block1]
type = GenericConstantMaterial
block = '1'
prop_names = 'D'
prop_values = '2'
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
print_linear_residuals = true
[]
[Debug]
show_var_residual_norms = true
[]
[Postprocessors]
[area]
type = AreaPostprocessor
use_displaced_mesh = true
boundary = 'right'
[]
[]
(test/tests/ics/bounding_box_ic/bounding_box_ic_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
uniform_refine = 3
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = BoundingBoxIC
x1 = 0.1
y1 = 0.1
x2 = 0.6
y2 = 0.6
inside = 2.3
outside = 4.6
[../]
[../]
[]
[AuxVariables]
active = 'u_aux'
[./u_aux]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = BoundingBoxIC
x1 = 0.1
y1 = 0.1
x2 = 0.6
y2 = 0.6
inside = 1.34
outside = 6.67
[../]
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(python/peacock/tests/input_tab/InputTree/gold/fsp_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
[]
[v]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
[diff_u]
type = Diffusion
variable = u
[]
[conv_v]
type = CoupledForce
variable = v
v = 'u'
[]
[diff_v]
type = Diffusion
variable = v
[]
[]
[BCs]
inactive = 'right_v'
[left_u]
type = DirichletBC
variable = u
boundary = '1'
value = 0
[]
[right_u]
type = DirichletBC
variable = u
boundary = '2'
value = 100
[]
[left_v]
type = DirichletBC
variable = v
boundary = '1'
value = 0
[]
[right_v]
type = DirichletBC
variable = v
boundary = '2'
value = 0
[]
[]
[Executioner]
# This is setup automatically in MOOSE (SetupPBPAction.C)
# petsc_options = '-snes_mf_operator'
# petsc_options_iname = '-pc_type'
# petsc_options_value = 'asm'
type = Steady
[]
[Preconditioning]
[FSP]
# It is the starting point of splitting
type = FSP
topsplit = 'uv' # uv should match the following block name
[uv]
# Generally speaking, there are four types of splitting we could choose
# <additive,multiplicative,symmetric_multiplicative,schur>
# An approximate solution to the original system
# | A_uu A_uv | | u | _ |f_u|
# | 0 A_vv | | v | - |f_v|
# is obtained by solving the following subsystems
# A_uu u = f_u and A_vv v = f_v
# If splitting type is specified as schur, we may also want to set more options to
# control how schur works using PETSc options
# petsc_options_iname = '-pc_fieldsplit_schur_fact_type -pc_fieldsplit_schur_precondition'
# petsc_options_value = 'full selfp'
splitting = 'u v' # u and v are the names of subsolvers
splitting_type = additive
[]
[u]
# PETSc options for this subsolver
# A prefix will be applied, so just put the options for this subsolver only
vars = 'u'
petsc_options_iname = '-pc_type -ksp_type'
petsc_options_value = ' hypre preonly'
[]
[v]
# PETSc options for this subsolver
vars = 'v'
petsc_options_iname = '-pc_type -ksp_type'
petsc_options_value = ' hypre preonly'
[]
[]
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/ray_tracing/test/tests/outputs/ray_tracing_mesh_output/ray_mesh_output.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 5
ny = 5
xmax = 5
ymax = 5
elem_type = QUAD4
[]
[middle_block]
type = SubdomainBoundingBoxGenerator
input = gmg
block_id = 1
bottom_left = '2 0 0'
top_right = '3 5 0'
[]
[middle_block_sideset]
type = SideSetsBetweenSubdomainsGenerator
input = middle_block
primary_block = 1
paired_block = 0
new_boundary = 7
[]
[]
[RayBCs]
[kill_top_right]
type = 'KillRayBC'
boundary = 'top right'
rays = 'to_top_right
centroid_left_to_right
along_top'
[]
[kill_bottom_left]
type = 'KillRayBC'
boundary = 'left bottom'
rays = 'reflect_right_and_top
reflect_right_at_node
reflect_internal'
[]
[reflect]
type = 'ReflectRayBC'
boundary = 'top right'
rays = 'reflect_right_and_top
reflect_right_at_node'
[]
[reflect_internal]
type = 'ReflectRayBC'
boundary = 7
rays = 'reflect_internal'
[]
[kill_internal]
type = 'KillRayBC'
boundary = 7
rays = 'kill_internal'
[]
[nothing_internal]
type = 'NullRayBC'
boundary = 7
rays = 'to_top_right
centroid_left_to_right
along_top
reflect_right_and_top
reflect_right_at_node'
[]
[]
[UserObjects/study]
type = RepeatableRayStudy
ray_kernel_coverage_check = false
start_points = '0 0 0
0.5 2.6 0
0 5 0
0 0.23 0
3 0 0
0 2.25 0
4.8 0.2 0'
directions = '1 1 0
1 0 0
1 0 0
1 0.6 0
1 0.5 0
1 0.58 0
-1 0.2 0'
names = 'to_top_right
centroid_left_to_right
along_top
reflect_right_and_top
reflect_right_at_node
reflect_internal
kill_internal'
execute_on = initial
always_cache_traces = true
use_internal_sidesets = true
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Outputs]
exodus = false
[rays]
type = RayTracingExodus
study = study
execute_on = final
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-rc-friction.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 5
ymin = -1
ymax = 1
nx = 50
ny = 10
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = 1
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[FVKernels]
inactive='u_friction_quad v_friction_quad'
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
[]
[u_friction_linear]
type = INSFVMomentumFriction
variable = vel_x
linear_coef_name = friction_coefficient
momentum_component = 'x'
[]
[u_friction_quad]
type = INSFVMomentumFriction
variable = vel_x
quadratic_coef_name = friction_coefficient
momentum_component = 'x'
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
[]
[v_friction_linear]
type = INSFVMomentumFriction
variable = vel_y
linear_coef_name = friction_coefficient
momentum_component = 'y'
[]
[v_friction_quad]
type = INSFVMomentumFriction
variable = vel_y
quadratic_coef_name = friction_coefficient
momentum_component = 'y'
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_x
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_y
function = '0'
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = vel_x
function = 0
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = vel_y
function = 0
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = '0'
[]
[]
[Materials]
[friction_coefficient]
type = ADGenericFunctorMaterial
prop_names = 'friction_coefficient'
prop_values = '25'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 200 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/fvbcs/wall_function/Re_t395.i)
von_karman_const = 0.41
H = 1 #halfwidth of the channel
L = 150
Re = 13700
rho = 1
bulk_u = 1
mu = ${fparse rho * bulk_u * 2 * H / Re}
advected_interp_method='upwind'
velocity_interp_method='rc'
[GlobalParams]
two_term_boundary_expansion = true
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[Mesh]
[gen]
type = CartesianMeshGenerator
dim = 2
dx = '${L}'
dy = '0.667 0.333'
ix = '200'
iy = '10 1'
[]
[]
[Problem]
fv_bcs_integrity_check = false
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1e-6
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1e-6
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[AuxVariables]
[mixing_len]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[wall_shear_stress]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[wall_yplus]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_viscosity_rans]
type = INSFVMixingLengthReynoldsStress
variable = u
rho = ${rho}
mixing_length = mixing_len
momentum_component = 'x'
u = u
v = v
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
momentum_component = 'y'
[]
[v_viscosity_rans]
type = INSFVMixingLengthReynoldsStress
variable = v
rho = ${rho}
mixing_length = mixing_len
momentum_component = 'y'
u = u
v = v
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[]
[AuxKernels]
[mixing_len]
type = WallDistanceMixingLengthAux
walls = 'top'
variable = mixing_len
execute_on = 'initial'
von_karman_const = ${von_karman_const}
[]
[wall_shear_stress]
type = WallFunctionWallShearStressAux
variable = wall_shear_stress
walls = 'top'
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[wall_yplus]
type = WallFunctionYPlusAux
variable = wall_yplus
walls = 'top'
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = '0'
[]
[wall-u]
type = INSFVWallFunctionBC
variable = u
boundary = 'top'
u = u
v = v
mu = ${mu}
rho = ${rho}
momentum_component = x
[]
[wall-v]
type = INSFVWallFunctionBC
variable = v
boundary = 'top'
u = u
v = v
mu = ${mu}
rho = ${rho}
momentum_component = y
[]
[sym-u]
type = INSFVSymmetryVelocityBC
boundary = 'bottom'
variable = u
u = u
v = v
mu = total_viscosity
momentum_component = x
[]
[sym-v]
type = INSFVSymmetryVelocityBC
boundary = 'bottom'
variable = v
u = u
v = v
mu = total_viscosity
momentum_component = y
[]
[symmetry_pressure]
type = INSFVSymmetryPressureBC
boundary = 'bottom'
variable = pressure
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = '0'
[]
[]
[Materials]
[total_viscosity]
type = MixingLengthTurbulentViscosityMaterial
u = 'u' #computes total viscosity = mu_t + mu
v = 'v' #property is called total_viscosity
mixing_length = mixing_len
mu = ${mu}
rho = ${rho}
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 200 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(modules/porous_flow/test/tests/ics/fluidpropic_celsius.i)
# Test the correct calculation of fluid properties using PorousFlwoFluidPropertyIC
# when temperature is given in Celsius
#
# Variables:
# Pressure: 1 MPa
# Temperature: 50 C
#
# Fluid properties for water (reference values from NIST webbook)
# Density: 988.43 kg/m^3
# Enthalpy: 210.19 kJ/kg
# Internal energy: 2019.18 kJ/kg
[Mesh]
type = GeneratedMesh
dim = 2
[]
[Variables]
[pressure]
initial_condition = 1e6
[]
[temperature]
initial_condition = 50
[]
[]
[AuxVariables]
[enthalpy]
[]
[internal_energy]
[]
[density]
[]
[]
[ICs]
[enthalpy]
type = PorousFlowFluidPropertyIC
variable = enthalpy
property = enthalpy
porepressure = pressure
temperature = temperature
temperature_unit = Celsius
fp = water
[]
[internal_energy]
type = PorousFlowFluidPropertyIC
variable = internal_energy
property = internal_energy
porepressure = pressure
temperature = temperature
temperature_unit = Celsius
fp = water
[]
[density]
type = PorousFlowFluidPropertyIC
variable = density
property = density
porepressure = pressure
temperature = temperature
temperature_unit = Celsius
fp = water
[]
[]
[Modules]
[FluidProperties]
[water]
type = Water97FluidProperties
[]
[]
[]
[Kernels]
[pressure]
type = Diffusion
variable = pressure
[]
[temperature]
type = Diffusion
variable = temperature
[]
[]
[Executioner]
type = Steady
nl_abs_tol = 1e-12
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Postprocessors]
[enthalpy]
type = ElementAverageValue
variable = enthalpy
execute_on = 'initial timestep_end'
[]
[internal_energy]
type = ElementAverageValue
variable = internal_energy
execute_on = 'initial timestep_end'
[]
[density]
type = ElementAverageValue
variable = density
execute_on = 'initial timestep_end'
[]
[]
[Outputs]
csv = true
file_base = fluidpropic_out
execute_on = initial
[]
(modules/combined/examples/stochastic/graphite_ring_thermomechanics.i)
# Generate 1/4 of a 2-ring disk and extrude it by half to obtain
# 1/8 of a 3D tube. Mirror boundary conditions will exist on the
# cut portions.
[Mesh]
[disk]
type = ConcentricCircleMeshGenerator
num_sectors = 10
radii = '1.0 1.1 1.2'
rings = '1 1 1'
has_outer_square = false
preserve_volumes = false
portion = top_right
[]
[ring]
type = BlockDeletionGenerator
input = disk
block = 1
new_boundary = 'inner'
[]
[cylinder]
type = MeshExtruderGenerator
input = ring
extrusion_vector = '0 0 1.5'
num_layers = 15
bottom_sideset = 'back'
top_sideset = 'front'
[]
[]
[Variables]
[T]
initial_condition = 300
[]
[disp_x]
[]
[disp_y]
[]
[disp_z]
[]
[]
[Kernels]
[hc]
type = HeatConduction
variable = T
[]
[TensorMechanics]
displacements = 'disp_x disp_y disp_z'
[]
[]
[BCs]
[temp_inner]
type = FunctionNeumannBC
variable = T
boundary = 'inner'
function = surface_source
[]
[temp_front]
type = ConvectiveHeatFluxBC
variable = T
boundary = 'front'
T_infinity = 300
heat_transfer_coefficient = 10
[]
[temp_outer]
type = ConvectiveHeatFluxBC
variable = T
boundary = 'outer'
T_infinity = 300
heat_transfer_coefficient = 10
[]
# mirror boundary conditions.
[disp_x]
type = DirichletBC
variable = disp_x
boundary = 'left'
value = 0.0
[]
[disp_y]
type = DirichletBC
variable = disp_y
boundary = 'bottom'
value = 0.0
[]
[disp_z]
type = DirichletBC
variable = disp_z
boundary = 'back'
value = 0.0
[]
[]
[Materials]
[cond_inner]
type = GenericConstantMaterial
block = 2
prop_names = thermal_conductivity
prop_values = 25
[]
[cond_outer]
type = GenericConstantMaterial
block = 3
prop_names = thermal_conductivity
prop_values = 100
[]
[elasticity_tensor_inner]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 2.1e5
poissons_ratio = 0.3
block = 2
[]
[elasticity_tensor_outer]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 3.1e5
poissons_ratio = 0.2
block = 3
[]
[thermal_strain_inner]
type = ComputeThermalExpansionEigenstrain
thermal_expansion_coeff = 2e-6
temperature = T
stress_free_temperature = 300
eigenstrain_name = eigenstrain_inner
block = 2
[]
[thermal_strain_outer]
type = ComputeThermalExpansionEigenstrain
thermal_expansion_coeff = 1e-6
temperature = T
stress_free_temperature = 300
eigenstrain_name = eigenstrain_outer
block = 3
[]
[strain_inner] #We use small deformation mechanics
type = ComputeSmallStrain
displacements = 'disp_x disp_y disp_z'
eigenstrain_names = 'eigenstrain_inner'
block = 2
[]
[strain_outer] #We use small deformation mechanics
type = ComputeSmallStrain
displacements = 'disp_x disp_y disp_z'
eigenstrain_names = 'eigenstrain_outer'
block = 3
[]
[stress] #We use linear elasticity
type = ComputeLinearElasticStress
[]
[]
[Functions]
[surface_source]
type = ParsedFunction
value = 'Q_t*pi/2.0/3.0 * cos(pi/3.0*z)'
vars = 'Q_t'
vals = heat_source
[]
[]
[Executioner]
type = Steady
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart'
petsc_options_value = 'hypre boomeramg 101'
l_max_its = 30
nl_max_its = 100
nl_abs_tol = 1e-9
l_tol = 1e-04
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[Controls]
[stochastic]
type = SamplerReceiver
[]
[]
[VectorPostprocessors]
[temp_center]
type = LineValueSampler
variable = T
start_point = '1 0 0'
end_point = '1.2 0 0'
num_points = 11
sort_by = 'x'
[]
[temp_end]
type = LineValueSampler
variable = T
start_point = '1 0 1.5'
end_point = '1.2 0 1.5'
num_points = 11
sort_by = 'x'
[]
[dispx_center]
type = LineValueSampler
variable = disp_x
start_point = '1 0 0'
end_point = '1.2 0 0'
num_points = 11
sort_by = 'x'
[]
[dispx_end]
type = LineValueSampler
variable = disp_x
start_point = '1 0 1.5'
end_point = '1.2 0 1.5'
num_points = 11
sort_by = 'x'
[]
[dispz_end]
type = LineValueSampler
variable = disp_z
start_point = '1 0 1.5'
end_point = '1.2 0 1.5'
num_points = 11
sort_by = 'x'
[]
[]
[Postprocessors]
[heat_source]
type = FunctionValuePostprocessor
function = 1
scale_factor = 10000
execute_on = linear
[]
[temp_center_inner]
type = PointValue
variable = T
point = '1 0 0'
[]
[temp_center_outer]
type = PointValue
variable = T
point = '1.2 0 0'
[]
[temp_end_inner]
type = PointValue
variable = T
point = '1 0 1.5'
[]
[temp_end_outer]
type = PointValue
variable = T
point = '1.2 0 1.5'
[]
[dispx_center_inner]
type = PointValue
variable = disp_x
point = '1 0 0'
[]
[dispx_center_outer]
type = PointValue
variable = disp_x
point = '1.2 0 0'
[]
[dispx_end_inner]
type = PointValue
variable = disp_x
point = '1 0 1.5'
[]
[dispx_end_outer]
type = PointValue
variable = disp_x
point = '1.2 0 1.5'
[]
[dispz_inner]
type = PointValue
variable = disp_z
point = '1 0 1.5'
[]
[dispz_outer]
type = PointValue
variable = disp_z
point = '1.2 0 1.5'
[]
[]
[Outputs]
exodus = false
csv = false
[]
(test/tests/misc/check_error/multi_precond_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Preconditioning]
active = 'PBP FDP'
[./PBP]
type = PBP
solve_order = 'u v'
preconditioner = 'LU LU'
off_diag_row = 'v'
off_diag_column = 'u'
[../]
[./FDP]
type = FDP
off_diag_row = 'v'
off_diag_column = 'u'
[../]
[]
[Variables]
active = 'u v'
[./u]
order = FIRST
family = LAGRANGE
[../]
[./v]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff_u conv_v diff_v'
[./diff_u]
type = Diffusion
variable = u
[../]
[./conv_v]
type = CoupledForce
variable = v
v = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[BCs]
active = 'left_u right_u left_v'
[./left_u]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 100
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = 3
value = 0
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Steady
l_max_its = 1
nl_max_its = 1
solve_type = JFNK
[]
[Outputs]
file_base = pbp_out
exodus = true
[]
(modules/ray_tracing/test/tests/outputs/ray_tracing_mesh_output/ray_mesh_output_errors.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
[]
[]
[RayBCs/kill]
type = 'KillRayBC'
boundary = 'left right'
[]
[UserObjects/study]
type = RepeatableRayStudy
start_points = '0 0 0'
directions = '1 0 0'
names = 'ray'
ray_kernel_coverage_check = false
execute_on = INITIAL
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Outputs]
exodus = false
[rays]
type = RayTracingExodus
study = study
execute_on = final
[]
[]
(test/tests/kernels/ad_coupled_value/ad_coupled_value.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 4
elem_type = quad9
[]
[Problem]
error_on_jacobian_nonzero_reallocation = true
[]
[Variables]
[./u]
[../]
[./v]
[../]
[./w]
order = SECOND
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[./diff_w]
type = Diffusion
variable = w
[../]
[./ad_coupled_value]
type = ADCoupledValueTest
variable = u
v = v
[../]
[./ad_coupled_value_w]
type = ADCoupledValueTest
variable = u
v = w
[../]
[./ad_coupled_value_x]
type = ADCoupledValueTest
variable = u
# v = 2.0 (Using the default value)
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = left
value = 0
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = right
value = 1
[../]
[./left_w]
type = DirichletBC
variable = w
boundary = left
value = 0
[../]
[./right_w]
type = DirichletBC
variable = w
boundary = right
value = 1
[../]
[]
[Preconditioning]
active = ''
[./smp]
type = SMP
[../]
[]
[Executioner]
type = Steady
solve_type = 'Newton'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
l_tol = 1e-10
nl_rel_tol = 1e-9
nl_max_its = 1
[]
[Outputs]
exodus = true
[]
(modules/porous_flow/test/tests/poroperm/PermFromPoro03.i)
# Testing permeability from porosity
# Trivial test, checking calculated permeability is correct
# k = k_anisotropic * B * exp(A * phi)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 3
xmin = 0
xmax = 3
[]
[GlobalParams]
block = 0
PorousFlowDictator = dictator
[]
[Variables]
[pp]
[InitialCondition]
type = ConstantIC
value = 0
[]
[]
[]
[Kernels]
[flux]
type = PorousFlowAdvectiveFlux
gravity = '0 0 0'
variable = pp
[]
[]
[BCs]
[ptop]
type = DirichletBC
variable = pp
boundary = right
value = 0
[]
[pbase]
type = DirichletBC
variable = pp
boundary = left
value = 1
[]
[]
[AuxVariables]
[poro]
order = CONSTANT
family = MONOMIAL
[]
[perm_x]
order = CONSTANT
family = MONOMIAL
[]
[perm_y]
order = CONSTANT
family = MONOMIAL
[]
[perm_z]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[poro]
type = PorousFlowPropertyAux
property = porosity
variable = poro
[]
[perm_x]
type = PorousFlowPropertyAux
property = permeability
variable = perm_x
row = 0
column = 0
[]
[perm_y]
type = PorousFlowPropertyAux
property = permeability
variable = perm_y
row = 1
column = 1
[]
[perm_z]
type = PorousFlowPropertyAux
property = permeability
variable = perm_z
row = 2
column = 2
[]
[]
[Postprocessors]
[perm_x_bottom]
type = PointValue
variable = perm_x
point = '0 0 0'
[]
[perm_y_bottom]
type = PointValue
variable = perm_y
point = '0 0 0'
[]
[perm_z_bottom]
type = PointValue
variable = perm_z
point = '0 0 0'
[]
[perm_x_top]
type = PointValue
variable = perm_x
point = '3 0 0'
[]
[perm_y_top]
type = PointValue
variable = perm_y
point = '3 0 0'
[]
[perm_z_top]
type = PointValue
variable = perm_z
point = '3 0 0'
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureVG
# unimportant in this fully-saturated test
m = 0.8
alpha = 1e-4
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 2.2e9
viscosity = 1e-3
density0 = 1000
thermal_expansion = 0
[]
[]
[]
[Materials]
[permeability]
type = PorousFlowPermeabilityExponential
k_anisotropy = '1 0 0 0 2 0 0 0 0.1'
poroperm_function = exp_k
A = 10
B = 1e-8
[]
[temperature]
type = PorousFlowTemperature
[]
[massfrac]
type = PorousFlowMassFraction
[]
[eff_fluid_pressure]
type = PorousFlowEffectiveFluidPressure
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pp
capillary_pressure = pc
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[porosity]
type = PorousFlowPorosity
porosity_zero = 0.1
[]
[relperm]
type = PorousFlowRelativePermeabilityCorey
n = 0 # unimportant in this fully-saturated situation
phase = 0
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
[]
[]
[Executioner]
solve_type = Newton
type = Steady
l_tol = 1E-5
nl_abs_tol = 1E-3
nl_rel_tol = 1E-8
l_max_its = 200
nl_max_its = 400
petsc_options_iname = '-pc_type -pc_asm_overlap -sub_pc_type -ksp_type -ksp_gmres_restart'
petsc_options_value = ' asm 2 lu gmres 200'
[]
[Outputs]
csv = true
execute_on = 'timestep_end'
[]
(test/tests/problems/eigen_problem/eigensolvers/ne_coupled_picard_subT.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 10
ymin = 0
ymax = 10
elem_type = QUAD4
nx = 8
ny = 8
[]
[Variables]
[./T]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./power]
order = FIRST
family = LAGRANGE
initial_condition = 0.1
[../]
[]
[Kernels]
[./diff_T]
type = Diffusion
variable = T
[../]
[./src_T]
type = CoupledForce
variable = T
v = power
[../]
[]
[BCs]
[./homogeneousT]
type = DirichletBC
variable = T
boundary = '0 1 2 3'
value = 0
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
nl_abs_tol = 1e-8
nl_rel_tol = 1e-6
fixed_point_max_its = 20
fixed_point_rel_tol = 1e-6
[]
[MultiApps]
[./sub]
type = FullSolveMultiApp
keep_solution_during_restore = true
input_files = ne_coupled_picard_subT_sub.i
execute_on = timestep_end
[../]
[]
[Transfers]
[./T_to_sub]
type = MultiAppMeshFunctionTransfer
to_multi_app = sub
source_variable = T
variable = T
execute_on = timestep_end
[../]
[./power_from_sub]
type = MultiAppMeshFunctionTransfer
from_multi_app = sub
source_variable = power
variable = power
execute_on = timestep_end
[../]
[]
[Outputs]
csv = true
exodus =true
execute_on = 'timestep_end'
[]
(test/tests/fvkernels/mms/non-orthogonal/advection-diffusion-reaction.i)
a=1.1
diff=1.1
[Mesh]
[./gen_mesh]
type = GeneratedMeshGenerator
dim = 2
xmin = 2
xmax = 3
ymin = 0
ymax = 1
nx = 2
ny = 2
elem_type = TRI3
[../]
[]
[Variables]
[./v]
family = MONOMIAL
order = CONSTANT
fv = true
initial_condition = 1
[../]
[]
[FVKernels]
[./advection]
type = FVAdvection
variable = v
velocity = '${a} ${fparse 2*a} 0'
advected_interp_method = 'average'
[../]
[reaction]
type = FVReaction
variable = v
[]
[diff_v]
type = FVDiffusion
variable = v
coeff = ${diff}
[]
[body_v]
type = FVBodyForce
variable = v
function = 'forcing'
[]
[]
[FVBCs]
[exact]
type = FVFunctionDirichletBC
boundary = 'left right top bottom'
function = 'exact'
variable = v
[]
[]
[Functions]
[exact]
type = ParsedFunction
value = 'sin(x)*cos(y)'
[]
[forcing]
type = ParsedFunction
value = '-2*a*sin(x)*sin(y) + a*cos(x)*cos(y) + 2*diff*sin(x)*cos(y) + sin(x)*cos(y)'
vars = 'a diff'
vals = '${a} ${diff}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type'
petsc_options_value = 'hypre'
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[./error]
type = ElementL2Error
variable = v
function = exact
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/rz_cone_no_parts_steady_stabilized.i)
# This input file tests several different things:
# .) The axisymmetric (RZ) form of the governing equations.
# .) An open boundary.
# .) Not integrating the pressure by parts, thereby requiring a pressure pin.
# .) Natural boundary condition at the outlet.
[GlobalParams]
integrate_p_by_parts = false
laplace = true
gravity = '0 0 0'
supg = true
pspg = true
order = FIRST
[]
[Mesh]
file = '2d_cone.msh'
[]
[Problem]
coord_type = RZ
[]
[Preconditioning]
[./SMP_PJFNK]
type = SMP
full = true
solve_type = Newton
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = 'bjacobi ilu 4'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
csv = true
console = true
[./out]
type = Exodus
[../]
[]
[Variables]
[./vel_x]
# Velocity in radial (r) direction
[../]
[./vel_y]
# Velocity in axial (z) direction
[../]
[./p]
[../]
[]
[BCs]
[./p_corner]
# This is required, because pressure term is *not* integrated by parts.
type = DirichletBC
boundary = top_right
value = 0
variable = p
[../]
[./u_in]
type = DirichletBC
boundary = bottom
variable = vel_x
value = 0
[../]
[./v_in]
type = FunctionDirichletBC
boundary = bottom
variable = vel_y
function = 'inlet_func'
[../]
[./u_axis_and_walls]
type = DirichletBC
boundary = 'left right'
variable = vel_x
value = 0
[../]
[./v_no_slip]
type = DirichletBC
boundary = 'right'
variable = vel_y
value = 0
[../]
[]
[Kernels]
[./mass]
type = INSMassRZ
variable = p
u = vel_x
v = vel_y
pressure = p
[../]
[./x_momentum_space]
type = INSMomentumLaplaceFormRZ
variable = vel_x
u = vel_x
v = vel_y
pressure = p
component = 0
[../]
[./y_momentum_space]
type = INSMomentumLaplaceFormRZ
variable = vel_y
u = vel_x
v = vel_y
pressure = p
component = 1
[../]
[]
[Materials]
[./const]
type = GenericConstantMaterial
block = 'volume'
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[]
[Functions]
[./inlet_func]
type = ParsedFunction
value = '-4 * x^2 + 1'
[../]
[]
[Postprocessors]
[./flow_in]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'bottom'
execute_on = 'timestep_end'
[../]
[./flow_out]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'top'
execute_on = 'timestep_end'
[../]
[]
(tutorials/darcy_thermo_mech/step01_diffusion/tests/kernels/simple_diffusion/simple_diffusion.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Problem]
type = FEProblem
coord_type = RZ
rz_coord_axis = X
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/fvkernels/fv_simple_diffusion/dirichlet_rz.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
# x can't start at zero because FV's weak dirichlet BCs need a non-zero area
# on the left so their numerical flux contribution isn't zero'd out -
# causing there to basically be no BC on the left.
xmin = .1
xmax = 1
[]
[Variables]
[u]
[]
[v]
family = MONOMIAL
order = CONSTANT
fv = true
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[FVKernels]
[diff]
type = FVDiffusion
variable = v
coeff = coeff
[]
[]
[FVBCs]
[left]
type = FVDirichletBC
variable = v
boundary = left
value = 7
[]
[right]
type = FVDirichletBC
variable = v
boundary = right
value = 42
[]
[]
[Materials]
[diff]
type = ADGenericFunctorMaterial
prop_names = 'coeff'
prop_values = '1'
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 7
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 42
[]
[]
[Problem]
type = FEProblem
coord_type = RZ
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/materials/functor_properties/bc/bc.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[v][]
[]
[Kernels]
[diff]
type = FunctorMatDiffusion
variable = v
diffusivity = 1
[]
[source]
type = BodyForce
variable = v
function = 'x + y'
[]
[]
[BCs]
[bounds]
type = MatPropBC
variable = v
boundary = 'left right top bottom'
mat_prop = 'prop'
[]
[]
[Materials]
[functor]
type = ADGenericFunctorMaterial
prop_names = 'prop'
prop_values = 'v'
execute_on = 'LINEAR NONLINEAR'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(modules/porous_flow/test/tests/fluids/h2o.i)
# Test the density and viscosity calculated by the water Material
# Region 1 density
# Pressure 80 MPa
# Temperature 300K (26.85C)
# Water density should equal 1.0 / 0.971180894e-3 = 1029.7 kg/m^3 (IAPWS IF97)
# Water viscosity should equal 0.00085327 Pa.s (NIST webbook)
# Results are within expected accuracy
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[]
[Variables]
[pp]
initial_condition = 80e6
[]
[]
[Kernels]
[dummy]
type = Diffusion
variable = pp
[]
[]
[AuxVariables]
[temp]
initial_condition = 300.0
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
temperature = temp
[]
[ppss]
type = PorousFlow1PhaseFullySaturated
porepressure = pp
[]
[water]
type = PorousFlowSingleComponentFluid
temperature_unit = Kelvin
fp = water
phase = 0
[]
[]
[Modules]
[FluidProperties]
[water]
type = Water97FluidProperties
[]
[]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Postprocessors]
[pressure]
type = ElementIntegralVariablePostprocessor
variable = pp
[]
[temperature]
type = ElementIntegralVariablePostprocessor
variable = temp
[]
[density]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_fluid_phase_density_qp0'
[]
[viscosity]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_viscosity_qp0'
[]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = h2o
csv = true
[]
(test/tests/mesh_modifiers/add_side_sets_from_bounding_box/error_no_elements_in_bounding_box.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[createNewSidesetOne]
type = SideSetsFromBoundingBoxGenerator
input = gen
block_id = 0
boundary_id_old = 'left bottom'
boundary_id_new = 10
bottom_left = '-0.1 -0.1 0'
top_right = '0.8 0.2 0'
[]
[createNewSidesetTwo]
type = SideSetsFromBoundingBoxGenerator
input = createNewSidesetOne
block_id = 0
boundary_id_old = 'right top'
boundary_id_new = 11
bottom_left = '1.7 0.7 0'
top_right = '2.1 1.1 0'
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[leftBC]
type = DirichletBC
variable = u
boundary = 10
value = 1
[]
[rightBC]
type = DirichletBC
variable = u
boundary = 11
value = 0
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/rz_cone_no_parts_steady.i)
# This input file tests several different things:
# .) The axisymmetric (RZ) form of the governing equations.
# .) An open boundary.
# .) Not integrating the pressure by parts, thereby requiring a pressure pin.
# .) Natural boundary condition at the outlet.
[GlobalParams]
integrate_p_by_parts = false
laplace = true
gravity = '0 0 0'
[]
[Mesh]
file = '2d_cone.msh'
[]
[Problem]
coord_type = RZ
[]
[Preconditioning]
[./SMP_PJFNK]
type = SMP
full = true
solve_type = Newton
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = 'bjacobi ilu 4'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
csv = true
console = true
[./out]
type = Exodus
[../]
[]
[Variables]
[./vel_x]
# Velocity in radial (r) direction
family = LAGRANGE
order = SECOND
[../]
[./vel_y]
# Velocity in axial (z) direction
family = LAGRANGE
order = SECOND
[../]
[./p]
family = LAGRANGE
order = FIRST
[../]
[]
[BCs]
[./p_corner]
# This is required, because pressure term is *not* integrated by parts.
type = DirichletBC
boundary = top_right
value = 0
variable = p
[../]
[./u_in]
type = DirichletBC
boundary = bottom
variable = vel_x
value = 0
[../]
[./v_in]
type = FunctionDirichletBC
boundary = bottom
variable = vel_y
function = 'inlet_func'
[../]
[./u_axis_and_walls]
type = DirichletBC
boundary = 'left right'
variable = vel_x
value = 0
[../]
[./v_no_slip]
type = DirichletBC
boundary = 'right'
variable = vel_y
value = 0
[../]
[]
[Kernels]
[./mass]
type = INSMassRZ
variable = p
u = vel_x
v = vel_y
pressure = p
[../]
[./x_momentum_space]
type = INSMomentumLaplaceFormRZ
variable = vel_x
u = vel_x
v = vel_y
pressure = p
component = 0
[../]
[./y_momentum_space]
type = INSMomentumLaplaceFormRZ
variable = vel_y
u = vel_x
v = vel_y
pressure = p
component = 1
[../]
[]
[Materials]
[./const]
type = GenericConstantMaterial
block = 'volume'
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[]
[Functions]
[./inlet_func]
type = ParsedFunction
value = '-4 * x^2 + 1'
[../]
[]
[Postprocessors]
[./flow_in]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'bottom'
execute_on = 'timestep_end'
[../]
[./flow_out]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'top'
execute_on = 'timestep_end'
[../]
[]
(test/tests/transfers/multiapp_transfer_transformation/transfer_transformation_sub.i)
[Mesh]
[./gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 5
ny = 5
nz = 0
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[./subdomain_id]
type = ElementSubdomainIDGenerator
input = gmg
subdomain_ids = '0 1 2 3 4
0 1 2 3 4
0 1 2 3 4
0 1 2 3 4
0 1 2 3 4'
[]
[./boundary01]
type = SideSetsBetweenSubdomainsGenerator
input = subdomain_id
primary_block = '0'
paired_block = '1'
new_boundary = 'boundary01'
[]
[./boundary10]
type = SideSetsBetweenSubdomainsGenerator
input = boundary01
primary_block = '1'
paired_block = '0'
new_boundary = 'boundary10'
[]
[./boundary12]
type = SideSetsBetweenSubdomainsGenerator
input = boundary10
primary_block = '1'
paired_block = '2'
new_boundary = 'boundary12'
[]
[./boundary21]
type = SideSetsBetweenSubdomainsGenerator
input = boundary12
primary_block = '2'
paired_block = '1'
new_boundary = 'boundary21'
[]
[./boundary23]
type = SideSetsBetweenSubdomainsGenerator
input = boundary21
primary_block = '2'
paired_block = '3'
new_boundary = 'boundary23'
[]
[./boundary32]
type = SideSetsBetweenSubdomainsGenerator
input = boundary23
primary_block = '3'
paired_block = '2'
new_boundary = 'boundary32'
[]
[./boundary34]
type = SideSetsBetweenSubdomainsGenerator
input = boundary32
primary_block = '3'
paired_block = '4'
new_boundary = 'boundary34'
[]
[./boundary43]
type = SideSetsBetweenSubdomainsGenerator
input = boundary34
primary_block = '4'
paired_block = '3'
new_boundary = 'boundary43'
[]
uniform_refine = 3
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxVariables]
[./frommaster]
[]
[./frommasterelem]
order = constant
family = monomial
[../]
[]
[BCs]
[./left0]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right0]
type = DirichletBC
variable = u
boundary = boundary01
value = 1
[../]
[./right1]
type = DirichletBC
variable = u
boundary = boundary12
value = 1
[../]
[./right2]
type = DirichletBC
variable = u
boundary = boundary23
value = 0
[../]
[./right3]
type = DirichletBC
variable = u
boundary = boundary34
value = 0
[../]
[./right4]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/1d-rc.i)
mu=1.1
rho=1.1
advected_interp_method='upwind'
velocity_interp_method='rc'
[Mesh]
[mesh]
type = CartesianMeshGenerator
dim = 1
dx = '1 1'
ix = '30 30'
subdomain_id = '1 2'
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
pressure = pressure
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = '1'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Postprocessors]
[inlet_p]
type = SideAverageValue
variable = 'pressure'
boundary = 'left'
[]
[outlet-u]
type = SideIntegralVariablePostprocessor
variable = u
boundary = 'right'
[]
[]
[Outputs]
exodus = true
csv = true
[]
(modules/heat_conduction/test/tests/radiative_bcs/ad_radiative_bc_cyl.i)
#
# Thin cylindrical shell with very high thermal conductivity
# so that temperature is almost uniform at 500 K. Radiative
# boundary conditions is applied. Heat flux out of boundary
# 'right' should be 3723.36; this is approached as the mesh
# is refined
#
[Mesh]
type = MeshGeneratorMesh
[cartesian]
type = CartesianMeshGenerator
dim = 2
dx = '1 1'
ix = '1 10'
dy = '1 1'
subdomain_id = '1 2 1 2'
[]
[remove_1]
type = BlockDeletionGenerator
block = 1
input = cartesian
[]
[readd_left]
type = ParsedGenerateSideset
combinatorial_geometry = 'abs(x - 1) < 1e-4'
new_sideset_name = left
input = remove_1
[]
[]
[Problem]
coord_type = RZ
[]
[Variables]
[temp]
initial_condition = 800.0
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temp
[]
[]
[BCs]
[lefttemp]
type = ADDirichletBC
boundary = left
variable = temp
value = 800
[]
[radiative_bc]
type = ADInfiniteCylinderRadiativeBC
boundary = right
variable = temp
boundary_radius = 2
boundary_emissivity = 0.2
cylinder_radius = 3
cylinder_emissivity = 0.7
Tinfinity = 500
[]
[]
[Materials]
[density]
type = ADGenericConstantMaterial
prop_names = 'density thermal_conductivity'
prop_values = '1 1.0e5'
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
petsc_options = '-snes_converged_reason'
line_search = none
nl_rel_tol = 1e-6
nl_abs_tol = 1e-7
[]
[Postprocessors]
[right]
type = ADSideDiffusiveFluxAverage
variable = temp
boundary = right
diffusivity = thermal_conductivity
[]
[min_temp]
type = ElementExtremeValue
variable = temp
value_type = min
[]
[max_temp]
type = ElementExtremeValue
variable = temp
value_type = max
[]
[]
[Outputs]
csv = true
[]
(test/tests/materials/functor_properties/functor-mat-props.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 10
xmax = 2
[]
[subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '1.0 0 0'
block_id = 1
top_right = '2.0 1.0 0'
[]
[interface]
input = subdomain1
type = SideSetsBetweenSubdomainsGenerator
primary_block = '0'
paired_block = '1'
new_boundary = 'primary0_interface'
[]
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
[diff_u]
type = FunctorMatDiffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 1
[]
[right]
type = DirichletBC
variable = u
boundary = 'right'
value = 0
[]
[]
[Materials]
[block0]
type = GenericFunctorMaterial
block = '0'
prop_names = 'D'
prop_values = '4'
[]
[block1]
type = GenericFunctorMaterial
block = '1'
prop_names = 'D'
prop_values = '2'
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(test/tests/meshgenerators/sidesets_bounding_box_generator/multiple_boundary_ids_3d.i)
[Mesh]
[./gmg]
type = GeneratedMeshGenerator
dim = 3
nx = 10
ny = 10
nz = 10
#parallel_type = replicated
[]
[./createNewSidesetOne]
type = SideSetsFromBoundingBoxGenerator
input = gmg
boundary_id_old = 'left bottom front'
boundary_id_new = 10
bottom_left = '-0.1 -0.1 -0.1'
top_right = '0.1 0.2 0.3'
block_id = 0
[]
[./createNewSidesetTwo]
type = SideSetsFromBoundingBoxGenerator
input = createNewSidesetOne
boundary_id_old = 'right top back'
boundary_id_new = 11
bottom_left = '0.6 0.7 0.8'
top_right = '1.1 1.1 1.1'
block_id = 0
[]
[./createNewSidesetThree]
type = SideSetsFromBoundingBoxGenerator
input = createNewSidesetTwo
boundary_id_old = 'left top back'
boundary_id_new = 12
bottom_left = '-0.1 0.9 0.9'
top_right = '0.1 1.1 1.1'
block_id = 0
[]
[./createNewSidesetFour]
type = SideSetsFromBoundingBoxGenerator
input = createNewSidesetThree
boundary_id_old = 'front'
boundary_id_new = 13
bottom_left = '0.4 0.4 0.9'
top_right = '0.6 0.6 1.1'
block_id = 0
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./firstBC]
type = DirichletBC
variable = u
boundary = 10
value = 1
[../]
[./secondBC]
type = DirichletBC
variable = u
boundary = 11
value = 0
[../]
[./thirdBC]
type = DirichletBC
variable = u
boundary = 12
value = 0
[../]
[./fourthBC]
type = DirichletBC
variable = u
boundary = 13
value = 0.5
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/cylindrical/no-slip-tris.i)
mu=1
rho=1
advected_interp_method='average'
velocity_interp_method='rc'
[GlobalParams]
two_term_boundary_expansion = true
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Mesh]
type = GeneratedMesh
nx = 4
ny = 4
xmax = 3.9
ymax = 4.1
elem_type = TRI3
dim = 2
[]
[Problem]
fv_bcs_integrity_check = true
coord_type = 'RZ'
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = 1e-15
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 1e-15
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
# we can think of the axis as a slip wall boundary, no normal velocity and no viscous shear
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
[]
[]
[FVBCs]
active = 'inlet-u inlet-v free-slip-wall-u free-slip-wall-v outlet-p axis-u axis-v'
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = vel_x
function = 0
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = vel_y
function = 1
[]
[free-slip-wall-u]
type = INSFVNaturalFreeSlipBC
boundary = 'right'
variable = vel_x
momentum_component = 'x'
[]
[free-slip-wall-v]
type = INSFVNaturalFreeSlipBC
boundary = 'right'
variable = vel_y
momentum_component = 'y'
[]
[no-slip-wall-u]
type = INSFVNoSlipWallBC
boundary = 'right'
variable = vel_x
function = 0
[]
[no-slip-wall-v]
type = INSFVNoSlipWallBC
boundary = 'right'
variable = vel_y
function = 0
[]
[outlet-p]
type = INSFVOutletPressureBC
boundary = 'top'
variable = pressure
function = 0
[]
[axis-u]
type = INSFVSymmetryVelocityBC
boundary = 'left'
variable = vel_x
u = vel_x
v = vel_y
mu = ${mu}
momentum_component = x
[]
[axis-v]
type = INSFVSymmetryVelocityBC
boundary = 'left'
variable = vel_y
u = vel_x
v = vel_y
mu = ${mu}
momentum_component = y
[]
[axis-p]
type = INSFVSymmetryPressureBC
boundary = 'left'
variable = pressure
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options = '-options_left'
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_shift_type -ksp_gmres_restart'
petsc_options_value = 'asm lu NONZERO 200'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Debug]
show_var_residual_norms = true
[]
[Postprocessors]
[in]
type = SideIntegralVariablePostprocessor
variable = vel_y
boundary = 'bottom'
[]
[out]
type = SideIntegralVariablePostprocessor
variable = vel_y
boundary = 'top'
[]
[num_lin]
type = NumLinearIterations
outputs = 'console'
[]
[num_nl]
type = NumNonlinearIterations
outputs = 'console'
[]
[cum_lin]
type = CumulativeValuePostprocessor
outputs = 'console'
postprocessor = 'num_lin'
[]
[cum_nl]
type = CumulativeValuePostprocessor
outputs = 'console'
postprocessor = 'num_nl'
[]
[]
[Outputs]
exodus = true
csv = true
[]
(modules/heat_conduction/test/tests/code_verification/cylindrical_test_no1.i)
# Problem II.1
#
# An infinitely long hollow cylinder has an inner radius ri and
# outer radius ro. It has a constant thermal conductivity k and
# internal heat generation q. It is allowed to reach thermal
# equilibrium while being exposed to constant temperatures on its
# inside and outside boundaries: u(ri) = ui and u(ro) = uo.
#
# REFERENCE:
# A. Toptan, et al. (Mar.2020). Tech. rep. CASL-U-2020-1939-000, SAND2020-3887 R. DOI:10.2172/1614683.
[Mesh]
[./geom]
type = GeneratedMeshGenerator
dim = 1
elem_type = EDGE2
xmin = 0.2
nx = 4
[../]
[]
[Variables]
[./u]
order = FIRST
[../]
[]
[Problem]
coord_type = RZ
[]
[Functions]
[./exact]
type = ParsedFunction
vars = 'ri ro ui uo'
vals = '0.2 1.0 300 0'
value = '( uo * log(ri) - ui * log(ro) + (ui-uo) * log(x) ) / log(ri/ro)'
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = u
[../]
[]
[BCs]
[./ui]
type = DirichletBC
boundary = left
variable = u
value = 300
[../]
[./uo]
type = DirichletBC
boundary = right
variable = u
value = 0
[../]
[]
[Materials]
[./property]
type = GenericConstantMaterial
prop_names = 'density specific_heat thermal_conductivity'
prop_values = '1.0 1.0 5.0'
[../]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[./error]
type = ElementL2Error
function = exact
variable = u
[../]
[./h]
type = AverageElementSize
[]
[]
[Outputs]
csv = true
[]
(modules/fluid_properties/test/tests/co2/co2.i)
# Test thermophysical property calculations in CO2FluidProperties
#
# Comparison with values from Span and Wagner, "A New Equation of State for
# Carbon Dioxide Covering the Fluid Region from the Triple-Point Temperature
# to 1100K at Pressures up to 800 MPa", J. Phys. Chem. Ref. Data, 25 (1996)
#
# Viscosity values from Fenghour et al., "The viscosity of carbon dioxide",
# J. Phys. Chem. Ref. Data, 27, 31-44 (1998)
#
#
# --------------------------------------------------------------
# Pressure (Mpa) | 1 | 1 | 1
# Temperature (K) | 280 | 360 | 500
# --------------------------------------------------------------
# Expected values
# --------------------------------------------------------------
# Density (kg/m^3) | 20.199 | 15.105 | 10.664
# Internal energy (kJ/kg/K) | -75.892 | -18.406 | 91.829
# Enthalpy (kJ/kg) | -26.385 | 47.797 | 185.60
# Entropy (kJ/kg/K) | -0.51326 | -0.28033 | 0.04225
# cv (kJ/kg/K) | 0.67092 | 0.72664 | 0.82823
# cp (kJ/kg/K) | 0.92518 | 0.94206 | 1.0273
# Speed of sound (m/s) | 252.33 | 289.00 | 339.81
# Viscosity (1e-6Pa.s) | 14.15 | 17.94 | 24.06
# --------------------------------------------------------------
# Calculated values
# --------------------------------------------------------------
# Density (kg/m^3) | 20.199 | 15.105 | 10.664
# Internal energy (kJ/kg/K) | -75.892 | -18.406 | 91.829
# Enthalpy (kJ/kg) | -26.385 | 47.797 | 185.60
# Entropy (kJ/kg/K) | -0.51326 | -0.28033 | 0.04225
# cv (kJ/kg/K) | 0.67092 | 0.72664 | 0.82823
# cp (kJ/kg/K) | 0.92518 | 0.94206 | 1.0273
# Speed of sound (m/s) | 252.33 | 289.00 | 339.81
# Viscosity (1e-6 Pa.s) | 14.15 | 17.94 | 24.06
# --------------------------------------------------------------
[Mesh]
type = GeneratedMesh
dim = 2
nx = 3
xmax = 3
# This test uses ElementalVariableValue postprocessors on specific
# elements, so element numbering needs to stay unchanged
allow_renumbering = false
[]
[Variables]
[./dummy]
[../]
[]
[AuxVariables]
[./pressure]
initial_condition = 1e6
family = MONOMIAL
order = CONSTANT
[../]
[./temperature]
family = MONOMIAL
order = CONSTANT
[../]
[./rho]
family = MONOMIAL
order = CONSTANT
[../]
[./mu]
family = MONOMIAL
order = CONSTANT
[../]
[./e]
family = MONOMIAL
order = CONSTANT
[../]
[./h]
family = MONOMIAL
order = CONSTANT
[../]
[./s]
family = MONOMIAL
order = CONSTANT
[../]
[./cv]
family = MONOMIAL
order = CONSTANT
[../]
[./cp]
family = MONOMIAL
order = CONSTANT
[../]
[./c]
family = MONOMIAL
order = CONSTANT
[../]
[]
[Functions]
[./tic]
type = ParsedFunction
value = if(x<1,280,if(x<2,360,500))
[../]
[]
[ICs]
[./t_ic]
type = FunctionIC
function = tic
variable = temperature
[../]
[]
[AuxKernels]
[./rho]
type = MaterialRealAux
variable = rho
property = density
[../]
[./my]
type = MaterialRealAux
variable = mu
property = viscosity
[../]
[./internal_energy]
type = MaterialRealAux
variable = e
property = e
[../]
[./enthalpy]
type = MaterialRealAux
variable = h
property = h
[../]
[./entropy]
type = MaterialRealAux
variable = s
property = s
[../]
[./cv]
type = MaterialRealAux
variable = cv
property = cv
[../]
[./cp]
type = MaterialRealAux
variable = cp
property = cp
[../]
[./c]
type = MaterialRealAux
variable = c
property = c
[../]
[]
[Modules]
[./FluidProperties]
[./co2]
type = CO2FluidProperties
[../]
[]
[]
[Materials]
[./fp_mat]
type = FluidPropertiesMaterialPT
pressure = pressure
temperature = temperature
fp = co2
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = dummy
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Postprocessors]
[./rho0]
type = ElementalVariableValue
elementid = 0
variable = rho
[../]
[./rho1]
type = ElementalVariableValue
elementid = 1
variable = rho
[../]
[./rho2]
type = ElementalVariableValue
elementid = 2
variable = rho
[../]
[./mu0]
type = ElementalVariableValue
elementid = 0
variable = mu
[../]
[./mu1]
type = ElementalVariableValue
elementid = 1
variable = mu
[../]
[./mu2]
type = ElementalVariableValue
elementid = 2
variable = mu
[../]
[./e0]
type = ElementalVariableValue
elementid = 0
variable = e
[../]
[./e1]
type = ElementalVariableValue
elementid = 1
variable = e
[../]
[./e2]
type = ElementalVariableValue
elementid = 2
variable = e
[../]
[./h0]
type = ElementalVariableValue
elementid = 0
variable = h
[../]
[./h1]
type = ElementalVariableValue
elementid = 1
variable = h
[../]
[./h2]
type = ElementalVariableValue
elementid = 2
variable = h
[../]
[./s0]
type = ElementalVariableValue
elementid = 0
variable = s
[../]
[./s1]
type = ElementalVariableValue
elementid = 1
variable = s
[../]
[./s2]
type = ElementalVariableValue
elementid = 2
variable = s
[../]
[./cv0]
type = ElementalVariableValue
elementid = 0
variable = cv
[../]
[./cv1]
type = ElementalVariableValue
elementid = 1
variable = cv
[../]
[./cv2]
type = ElementalVariableValue
elementid = 2
variable = cv
[../]
[./cp0]
type = ElementalVariableValue
elementid = 0
variable = cp
[../]
[./cp1]
type = ElementalVariableValue
elementid = 1
variable = cp
[../]
[./cp2]
type = ElementalVariableValue
elementid = 2
variable = cp
[../]
[./c0]
type = ElementalVariableValue
elementid = 0
variable = c
[../]
[./c1]
type = ElementalVariableValue
elementid = 1
variable = c
[../]
[./c2]
type = ElementalVariableValue
elementid = 2
variable = c
[../]
[]
[Outputs]
csv = true
execute_on = 'TIMESTEP_END'
[]
(modules/fluid_properties/test/tests/auxkernels/fluid_density_aux.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./pressure]
[../]
[./temperature]
[../]
[./density]
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./pressure_ak]
type = ConstantAux
variable = pressure
value = 10e6
[../]
[./temperature_ak]
type = ConstantAux
variable = temperature
value = 400.0
[../]
[./density]
type = FluidDensityAux
variable = density
fp = eos
p = pressure
T = temperature
[../]
[]
[Modules]
[./FluidProperties]
[./eos]
type = StiffenedGasFluidProperties
gamma = 2.35
q = -1167e3
q_prime = 0.0
p_inf = 1e9
cv = 1816.0
[../]
[]
[]
[BCs]
[./left_u]
type = DirichletBC
variable = u
boundary = 0
value = 1
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 2
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(tutorials/tutorial01_app_development/step01_moose_app/test/tests/kernels/simple_diffusion/simple_diffusion.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/fluid_properties/test/tests/auxkernels/stagnation_temperature_aux.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./specific_internal_energy]
[../]
[./specific_volume]
[../]
[./velocity]
[../]
[./stagnation_temperature]
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./specific_internal_energy_ak]
type = ConstantAux
variable = specific_internal_energy
value = 1026.2e3
[../]
[./specific_volume_ak]
type = ConstantAux
variable = specific_volume
value = 0.0012192
[../]
[./velocity_ak]
type = ConstantAux
variable = velocity
value = 10.0
[../]
[./stagnation_temperature_ak]
type = StagnationTemperatureAux
variable = stagnation_temperature
e = specific_internal_energy
v = specific_volume
vel = velocity
fp = eos
[../]
[]
[Modules]
[./FluidProperties]
[./eos]
type = StiffenedGasFluidProperties
gamma = 2.35
q = -1167e3
q_prime = 0.0
p_inf = 1e9
cv = 1816.0
[../]
[]
[]
[BCs]
[./left_u]
type = DirichletBC
variable = u
boundary = 0
value = 1
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 2
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/variables/fe_monomial_const/monomial-const-1d.i)
[Mesh]
type = GeneratedMesh
dim = 1
xmin = -1
xmax = 1
nx = 100
elem_type = EDGE3
[]
[Functions]
[./bc_fn]
type=ParsedFunction
value=0
[../]
[./forcing_fn]
type = MTPiecewiseConst1D
[../]
[./solution]
type = MTPiecewiseConst1D
[../]
[]
[Variables]
[./u]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
active = 'diff forcing reaction'
[./diff]
type = Diffusion
variable = u
[../]
[./reaction]
type = Reaction
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
# Note: MOOSE's DirichletBCs do not work properly with shape functions that do not
# have DOFs at the element edges. This test works because the solution
# has been designed to be zero at the boundary which is satisfied by the IC
# Ticket #1352
active = ''
[./bc_all]
type=FunctionDirichletBC
variable = u
boundary = 'left right'
function = bc_fn
[../]
[]
[Postprocessors]
[./dofs]
type = NumDOFs
[../]
[./h]
type = AverageElementSize
[../]
[./L2error]
type = ElementL2Error
variable = u
function = solution
[../]
[./H1error]
type = ElementH1Error
variable = u
function = solution
[../]
[./H1Semierror]
type = ElementH1SemiError
variable = u
function = solution
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
nl_rel_tol = 1.e-9
[./Adaptivity]
[../]
[]
[Outputs]
execute_on = 'timestep_end'
csv = true
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[]
(python/chigger/tests/input/simple_diffusion_new_var.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
uniform_refine = 2
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./aux]
family = MONOMIAL
order = CONSTANT
[../]
[./New_0]
[../]
[]
[AuxKernels]
[./aux_kernel]
type = FunctionAux
variable = aux
function = sin(2*pi*x)*sin(2*pi*y)
execute_on = 'initial'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/markers/error_fraction_marker/error_fraction_marker_no_clear_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
nz = 10
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
[./solution]
type = ParsedFunction
value = (exp(x)-1)/(exp(1)-1)
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./conv]
type = Convection
variable = u
velocity = '1 0 0'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Adaptivity]
steps = 2
marker = marker
[./Indicators]
[./error]
type = AnalyticalIndicator
variable = u
function = solution
[../]
[../]
[./Markers]
[./marker]
type = ErrorFractionMarker
indicator = error
refine = 0.3
clear_extremes = false
[../]
[../]
[]
[Outputs]
exodus = true
[]
(test/tests/functions/solution_function/solution_function_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
# This test uses SolutionUserObject which doesn't work with DistributedMesh.
parallel_type = replicated
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = initial_cond_func
[../]
[../]
[]
[AuxVariables]
[./u_aux]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = initial_cond_func
[../]
[../]
[]
[Functions]
[./initial_cond_func]
type = SolutionFunction
solution = ex_soln
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[UserObjects]
[./ex_soln]
type = SolutionUserObject
system_variables = u
mesh = build_out_0001_mesh.xda
es = build_out_0001.xda
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
nl_rel_tol = 1e-10
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/bcs/array_vacuum/array_vacuum.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 4
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
components = 2
[]
[]
[Kernels]
[diff]
type = ArrayDiffusion
variable = u
diffusion_coefficient = dc
[]
[reaction]
type = ArrayReaction
variable = u
reaction_coefficient = rc
[]
[]
[BCs]
[left]
type = ArrayVacuumBC
variable = u
boundary = 1
alpha = '1 1.2'
[]
[right]
type = ArrayDirichletBC
variable = u
boundary = 2
values = '1 2'
[]
[]
[Materials]
[dc]
type = GenericConstantArray
prop_name = dc
prop_value = '1 1'
[]
[rc]
type = GenericConstant2DArray
prop_name = rc
prop_value = '1 0; -0.1 1'
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(test/tests/userobjects/nearest_point_layered_average/nearest_radius_layered_average.i)
# This input tests the NearestRadiusLayeredAverage object by taking the average
# of layered rings and using the variable u(x,y,x) = r + z, where r sqrt(x^2 + y^2)
# Given a ring of inner and outer radii r1 and r2, respectively, and of height z1 and z2,
# the analytical solution is given by:
# avg(r1,r2,z1,z2) = 2/3 * (r1^2 + r1*r2 + r2^2) / (r1 + r2) + (z1 + z2) / 2
# Convergence to these values as num_sectors is increased is verified.
[Mesh]
[./ccmg]
type = ConcentricCircleMeshGenerator
num_sectors = 8
radii = '0.1 0.2 0.3 0.4 0.5'
rings = '2 2 2 2 2'
has_outer_square = false
preserve_volumes = true
smoothing_max_it = 3
[]
[./extruder]
type = MeshExtruderGenerator
input = ccmg
extrusion_vector = '0 0 1'
num_layers = 4
[]
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./ring_average]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./reac]
type = Reaction
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = func
[../]
[]
[Functions]
[func]
type = ParsedFunction
value = 'sqrt(x * x + y * y) + z'
[]
[]
[AuxKernels]
[./np_layered_average]
type = SpatialUserObjectAux
variable = ring_average
execute_on = timestep_end
user_object = nrla
[../]
[]
[UserObjects]
[./nrla]
type = NearestRadiusLayeredAverage
direction = z
num_layers = 2
points = '0.05 0 0
0.15 0 0
0.25 0 0
0.35 0 0
0.45 0 0'
variable = u
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/materials/functor_properties/vector-magnitude/test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[u]
type = MooseVariableFVReal
[]
[v]
type = MooseVariableFVReal
[]
[]
[AuxVariables]
[mag]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[mag]
type = ADFunctorElementalAux
variable = mag
functor = mat_mag
[]
[]
[FVKernels]
[v_diff]
type = FVDiffusion
variable = v
coeff = 1
[]
[u_diff]
type = FVDiffusion
variable = u
coeff = 1
[]
[]
[FVBCs]
[v_left]
type = FVDirichletBC
variable = v
boundary = 'left'
value = 0
[]
[v_right]
type = FVDirichletBC
variable = v
boundary = 'right'
value = 1
[]
[u_bottom]
type = FVDirichletBC
variable = u
boundary = 'bottom'
value = 0
[]
[u_top]
type = FVDirichletBC
variable = u
boundary = 'top'
value = 1
[]
[]
[Materials]
[functor]
type = ADVectorMagnitudeFunctorMaterial
x_functor = u
y_functor = v
vector_magnitude_name = mat_mag
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(test/tests/utils/mathutils/clamp.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Problem]
solve = false
[]
[Functions]
[./clamp]
type = ClampTestFunction
[../]
[./exact]
type = PiecewiseLinear
x = '0 0.2 0.8 1.0'
y = '0.2 0.2 0.8 0.8'
axis = x
[../]
[]
[VectorPostprocessors]
[./functions]
type = LineFunctionSampler
functions = 'clamp exact'
start_point = '0 0 0'
end_point = '1 0 0'
num_points = 10
sort_by = x
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
[]
(test/tests/markers/boundary_marker/adjacent.i)
###########################################################
# This is a test of the Mesh Marker System. It marks
# elements with flags indicating whether they should be
# refined, coarsened, or left alone. This system
# has the ability to use the Mesh Indicator System.
#
# @Requirement F2.50
###########################################################
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
# Mesh Marker System
[Adaptivity]
[Markers]
[boundary]
type = BoundaryMarker
next_to = right
mark = refine
[]
[]
initial_marker = boundary
initial_steps = 2
[]
[Outputs]
exodus = true
[]
(test/tests/kernels/kernel_precompute/adkernel_precompute_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
nz = 0
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
[./convected]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = ADDiffusion
variable = convected
[../]
[./conv]
type = ADConvectionPrecompute
variable = convected
velocity = '1.0 0.0 0.0'
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = convected
preset = false
boundary = 'left'
value = 0
[../]
[./top]
type = DirichletBC
variable = convected
preset = false
boundary = 'right'
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
execute_on = 'timestep_end'
file_base = out
exodus = true
[]
(test/tests/misc/check_error/missing_material_prop_test2.i)
[Mesh]
file = rectangle.e
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff_km_kernel]
type = DiffMKernel
variable = u
mat_prop = diff1
[../]
[./body_force]
type = BodyForce
variable = u
block = 1
value = 10
[../]
[]
[BCs]
active = 'right'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Materials]
[./mat11]
type = GenericConstantMaterial
block = 1
prop_names = 'diff1'
prop_values = '1'
[../]
[./mat12]
type = GenericConstantMaterial
block = 1
prop_names = 'diff2'
prop_values = '1'
[../]
[./mat22]
type = GenericConstantMaterial
block = 2
prop_names = 'diff2'
prop_values = '1'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
[Debug]
show_material_props = true
[]
(modules/stochastic_tools/examples/surrogates/gaussian_process/sub.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 100
xmax = 0.03
elem_type = EDGE3
[]
[Variables]
[T]
order = SECOND
family = LAGRANGE
[]
[]
[Kernels]
[diffusion]
type = MatDiffusion
variable = T
diffusivity = k
[]
[source]
type = BodyForce
variable = T
value = 10000
[]
[]
[Materials]
[conductivity]
type = GenericConstantMaterial
prop_names = k
prop_values = 5.0
[]
[]
[BCs]
[right]
type = DirichletBC
variable = T
boundary = right
value = 300
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Postprocessors]
[avg]
type = AverageNodalVariableValue
variable = T
[]
[max]
type = NodalExtremeValue
variable = T
value_type = max
[]
[]
[Outputs]
[]
(test/tests/postprocessors/mms_slope/mms_slope_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
# do not use uniform refine, we are using adaptive refining
# uniform_refine = 6
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
active = 'forcing_func u_func'
[./forcing_func]
type = ParsedFunction
value = alpha*alpha*pi*pi*sin(alpha*pi*x)
vars = 'alpha'
vals = '4'
[../]
[./u_func]
type = ParsedGradFunction
value = sin(alpha*pi*x)
grad_x = alpha*pi*sin(alpha*pi*x)
vars = 'alpha'
vals = '4'
[../]
[]
[Kernels]
active = 'diff forcing'
[./diff]
type = Diffusion
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_func
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = '3'
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = '1'
value = 0
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
nl_abs_tol = 1e-14
[./Adaptivity]
# if the refine fraction is 1 it will refine every element
# remember < 1 means only refine that percentage of elements
refine_fraction = 1
steps = 6
# do not coarsen at all
coarsen_fraction = 0
# maximum level of refinement steps, make sure this is > max_r_steps
max_h_level = 10
# leave this as is
error_estimator = KellyErrorEstimator
[../]
[]
# print l2 and h1 errors from the Postprocessors too so I can compare
[Postprocessors]
active = 'l2_error h1_error dofs'
# active = ' '
[./l2_error]
type = ElementL2Error
variable = u
function = u_func
[../]
[./h1_error]
type = ElementH1Error
variable = u
function = u_func
[../]
[./dofs]
type = NumDOFs
[../]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = out
exodus = true
[]
(test/tests/transfers/multiapp_copy_transfer/linear_lagrange_to_sub/sub.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(tutorials/tutorial01_app_development/step02_input_file/problems/pressure_diffusion.i)
[Mesh]
type = GeneratedMesh # Can generate simple lines, rectangles and rectangular prisms
dim = 2 # Dimension of the mesh
nx = 100 # Number of elements in the x direction
ny = 10 # Number of elements in the y direction
xmax = 0.304 # Length of test chamber
ymax = 0.0257 # Test chamber radius
[]
[Problem]
type = FEProblem # This is the "normal" type of Finite Element Problem in MOOSE
coord_type = RZ # Axisymmetric RZ
rz_coord_axis = X # Which axis the symmetry is around
[]
[Variables]
[pressure]
# Adds a Linear Lagrange variable by default
[]
[]
[Kernels]
[diffusion]
type = ADDiffusion # Laplacian operator
variable = pressure # Operate on the "pressure" variable from above
[]
[]
[BCs]
[inlet]
type = ADDirichletBC # Simple u=value BC
variable = pressure # Variable to be set
boundary = left # Name of a sideset in the mesh
value = 4000 # (Pa) From Figure 2 from paper. First data point for 1mm spheres.
[]
[outlet]
type = ADDirichletBC
variable = pressure
boundary = right
value = 0 # (Pa) Gives the correct pressure drop from Figure 2 for 1mm spheres
[]
[]
[Executioner]
type = Steady # Steady state problem
solve_type = NEWTON # Perform a Newton solve
# Set PETSc parameters to optimize solver efficiency
petsc_options_iname = '-pc_type -pc_hypre_type' # PETSc option pairs with values below
petsc_options_value = ' hypre boomeramg'
[]
[Outputs]
exodus = true # Output Exodus format
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/3d-rc.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
xmin = 0
xmax = 10
ymin = -1
ymax = 1
zmin = -1
zmax = 1
nx = 21
ny = 7
nz = 7
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
w = w
pressure = pressure
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1e-6
[]
[w]
type = INSFVVelocityVariable
initial_condition = 1e-6
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[w_advection]
type = INSFVMomentumAdvection
variable = w
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'z'
[]
[w_viscosity]
type = INSFVMomentumDiffusion
variable = w
mu = ${mu}
momentum_component = 'z'
[]
[w_pressure]
type = INSFVMomentumPressure
variable = w
momentum_component = 'z'
pressure = pressure
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = 0
[]
[inlet-w]
type = INSFVInletVelocityBC
boundary = 'left'
variable = w
function = 0
[]
[walls-u]
type = INSFVNaturalFreeSlipBC
boundary = 'top bottom front back'
variable = u
momentum_component = 'x'
[]
[walls-v]
type = INSFVNaturalFreeSlipBC
boundary = 'top bottom front back'
variable = v
momentum_component = 'y'
[]
[walls-w]
type = INSFVNaturalFreeSlipBC
boundary = 'top bottom front back'
variable = w
momentum_component = 'z'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 0
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_abs_tol = 1e-13
[]
[Outputs]
exodus = true
csv = true
[]
(test/tests/userobjects/layered_side_integral/layered_side_diffusive_flux_average_fv.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 6
ny = 6
nz = 6
[]
[Variables]
[./u]
order = CONSTANT
family = MONOMIAL
fv = true
[../]
[]
[AuxVariables]
[./layered_side_flux_average]
order = CONSTANT
family = MONOMIAL
[../]
[]
[FVKernels]
[./diff]
type = FVDiffusion
variable = u
coeff = 1
[../]
[]
[FVBCs]
[./bottom]
type = FVDirichletBC
variable = u
boundary = bottom
value = 0
[../]
[./top]
type = FVDirichletBC
variable = u
boundary = top
value = 1
[../]
[]
[AuxKernels]
[./lsfa]
type = SpatialUserObjectAux
variable = layered_side_flux_average
boundary = top
user_object = layered_side_flux_average
[../]
[]
[Materials]
[./gcm]
type = GenericConstantMaterial
prop_values = 2
prop_names = diffusivity
boundary = 'right top'
[../]
[]
[UserObjects]
[./layered_side_flux_average]
type = LayeredSideDiffusiveFluxAverage
direction = y
diffusivity = diffusivity
num_layers = 1
variable = u
execute_on = linear
boundary = top
[../]
[]
[Executioner]
type = Steady
nl_abs_tol = 1e-14
nl_rel_tol = 1e-14
l_abs_tol = 1e-14
l_tol = 1e-6
[]
[Outputs]
exodus = true
[]
[Debug]
show_material_props = true
[]
(modules/tensor_mechanics/test/tests/ad_action/two_coord.i)
[Mesh]
[generated_mesh]
type = GeneratedMeshGenerator
dim = 2
nx = 16
ny = 8
xmin = -1
xmax = 1
[]
[block1]
type = SubdomainBoundingBoxGenerator
block_id = 1
bottom_left = '-1 0 0'
top_right = '0 1 0'
input = generated_mesh
[]
[block2]
type = SubdomainBoundingBoxGenerator
block_id = 2
bottom_left = '0 0 0'
top_right = '1 1 0'
input = block1
[]
[]
[Problem]
coord_type = 'XYZ RZ'
block = '1 2'
[]
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Modules/TensorMechanics/Master]
active = 'block1 block2'
[./error]
strain = SMALL
add_variables = true
[../]
[./block1]
strain = SMALL
add_variables = true
block = 1
use_automatic_differentiation = true
[../]
[./block2]
strain = SMALL
add_variables = true
block = 2
use_automatic_differentiation = true
[../]
[]
[AuxVariables]
[./vmstress]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./vmstress]
type = ADRankTwoScalarAux
rank_two_tensor = total_strain
variable = vmstress
scalar_type = VonMisesStress
execute_on = timestep_end
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1e10
poissons_ratio = 0.345
[../]
[./_elastic_stress]
type = ADComputeLinearElasticStress
block = '1 2'
[../]
[]
[BCs]
[./topx]
type = DirichletBC
boundary = 'top'
variable = disp_x
value = 0.0
[../]
[./topy]
type = DirichletBC
boundary = 'top'
variable = disp_y
value = 0.0
[../]
[./bottomx]
type = DirichletBC
boundary = 'bottom'
variable = disp_x
value = 0.0
[../]
[./bottomy]
type = DirichletBC
boundary = 'bottom'
variable = disp_y
value = 0.05
[../]
[]
[Debug]
show_var_residual_norms = true
[]
[Preconditioning]
[./full]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = ' 201 hypre boomeramg 10'
line_search = 'none'
nl_rel_tol = 5e-9
nl_abs_tol = 1e-10
nl_max_its = 15
l_tol = 1e-3
l_max_its = 50
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/exodus/exodus_discontinuous.i)
##
# \file exodus/exodus_discontinuous.i
# \example exodus/exodus_discontinuous.i
# Input file for testing discontinuous data output
#
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./disc_u]
family = monomial
order = first
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = disc_u
[../]
[./forcing]
type = BodyForce
variable = disc_u
value = 7
[../]
[]
[DGKernels]
[./diff_dg]
type = DGDiffusion
variable = disc_u
sigma = 1
epsilon = 1
[../]
[]
[Functions]
[./zero_fn]
type = ParsedFunction
value = 0.0
[../]
[]
[BCs]
[./all]
type = DGFunctionDiffusionDirichletBC
variable = disc_u
boundary = 'left right top bottom'
function = zero_fn
sigma = 1
epsilon = 1
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
[./exo_out]
type = Exodus
discontinuous = true
file_base = 'exodus_discontinuous_out'
[../]
[]
(test/tests/mesh_modifiers/subdomain_bounding_box/oriented_subdomain_bounding_box_inside.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
xmin = -6
xmax = 4
nx = 10
ymin = -2
ymax = 10
ny = 12
zmin = -5
zmax = 7
nz = 12
[]
[subdomains]
type = OrientedSubdomainBoundingBoxGenerator
input = gen
center = '-1 4 1'
width = 5
length = 10
height = 4
width_direction = '2 1 0'
length_direction = '-1 2 2'
block_id = 10
location = INSIDE
[]
[]
[Problem]
type = FEProblem
solve = false
kernel_coverage_check = false
[]
[Variables]
[u]
[]
[]
[Materials]
[mat10]
type = GenericConstantMaterial
block = 10
outputs = all
prop_values = 6.24
prop_names = prop
[]
[mat0]
type = GenericConstantMaterial
block = 0
prop_names = prop
prop_values = 0
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
[]
[Outputs]
exodus = true
[]
(test/tests/controls/tag_based_naming_access/system_asterisk_param.i)
[Mesh]
type = GeneratedMesh
dim = 2
elem_type = QUAD4
# use odd numbers so points do not fall on element boundaries
nx = 31
ny = 31
[]
[Variables]
[./diffused]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = diffused
[../]
[]
[DiracKernels]
[./test_object]
type = MaterialPointSource
point = '0.5 0.5 0'
variable = diffused
[../]
[]
[BCs]
[./bottom_diffused]
type = DirichletBC
variable = diffused
boundary = 'bottom'
value = 2
[../]
[./top_diffused]
type = DirichletBC
variable = diffused
boundary = 'top'
value = 0
[../]
[]
[Materials]
[./mat]
type = GenericConstantMaterial
prop_names = 'matp'
prop_values = '1'
block = 0
[../]
[]
[Postprocessors]
[./test_object]
type = FunctionValuePostprocessor
function = '2*(x+y)'
point = '0.5 0.5 0'
control_tags = 'tag'
[../]
[./other_point_test_object]
type = FunctionValuePostprocessor
function = '3*(x+y)'
point = '0.5 0.5 0'
control_tags = 'tag'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
[Controls]
[./point_control]
type = TestControl
test_type = 'point'
parameter = 'tag/*/point'
execute_on = 'initial'
[../]
[]
(test/tests/materials/material/adv_mat_couple_test2.i)
[Mesh]
file = rectangle.e
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff body_force'
[./diff]
type = Diffusion
variable = u
[../]
[./body_force]
type = BodyForce
variable = u
block = 1
value = 10
[../]
[]
[BCs]
active = 'right'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Materials]
[./mat_3]
type = GenericConstantMaterial
prop_names = 'prop3'
prop_values = '300'
block = '1 2'
[../]
[./mat_2]
type = CoupledMaterial
mat_prop = 'prop2'
coupled_mat_prop = 'prop3'
block = '1 2'
[../]
[./mat_1]
type = CoupledMaterial2
mat_prop = 'prop1'
coupled_mat_prop1 = 'prop2'
coupled_mat_prop2 = 'prop3'
block = '1 2'
[../]
[]
[Executioner]
type = Steady
# solve_type = 'PJFNK'
# preconditioner = 'ILU'
solve_type = 'PJFNK'
# petsc_options_iname = '-pc_type -pc_hypre_type'
# petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
file_base = out_adv_coupled2
exodus = true
[]
(modules/phase_field/test/tests/new_initial_conditions/SmoothCircleIC_tanh.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 25
ny = 25
xmax = 30
ymax = 30
elem_type = QUAD4
[]
[Variables]
[./c]
order = THIRD
family = HERMITE
[../]
[]
[ICs]
[./c]
type = SmoothCircleIC
variable = c
x1 = 15.0
y1 = 15.0
radius = 8.0
invalue = 1.0
outvalue = -0.8
int_width = 8.0
profile = TANH
[../]
[]
[BCs]
[./Periodic]
[./all]
auto_direction = 'x y'
[../]
[../]
[]
[Executioner]
type = Steady
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[Outputs]
exodus = false
[./out]
type = Exodus
refinements = 1
[../]
[]
(test/tests/misc/check_error/scalar_dot_integrity_check.i)
# Test that coupling a time derivative of a scalar variable (ScalarDotCouplingAux) and
# using a Steady executioner errors out
[Mesh]
type = GeneratedMesh
dim = 2
[]
[Functions]
[./a_fn]
type = ParsedFunction
value = t
[../]
[]
[AuxVariables]
[./v]
[../]
[./a]
family = SCALAR
order = FIRST
[../]
[]
[AuxScalarKernels]
[./a_sak]
type = FunctionScalarAux
variable = a
function = a_fn
[../]
[]
[AuxKernels]
[./ak_v]
type = ScalarDotCouplingAux
variable = v
v = a
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./td]
type = TimeDerivative
variable = u
[../]
[]
[Executioner]
type = Steady
[]
(test/tests/multiapps/picard_multilevel/2level_picard/mutilevel_app.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 10
ny = 10
[]
[Variables]
[u]
[]
[]
[AuxVariables]
[v]
initial_condition = 50
[]
[]
[Kernels]
[diffusion]
type = Diffusion
variable = u
[]
[source]
type = CoupledForce
variable = u
v = v
[]
[]
[BCs]
[dirichlet0]
type = DirichletBC
variable = u
boundary = '3'
value = 0
[]
[dirichlet]
type = DirichletBC
variable = u
boundary = '1'
value = 100
[]
[]
[Postprocessors]
[avg_u]
type = ElementAverageValue
variable = u
execute_on = 'initial timestep_begin timestep_end'
[]
[avg_v]
type = ElementAverageValue
variable = v
execute_on = 'initial timestep_begin timestep_end'
[]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart '
petsc_options_value = 'hypre boomeramg 100'
fixed_point_rel_tol = 1E-3
fixed_point_abs_tol = 1.0e-05
fixed_point_max_its = 2
accept_on_max_fixed_point_iteration = true
[]
[MultiApps]
[level1-]
type = FullSolveMultiApp
app_type = MooseTestApp
positions = '0 0 0'
input_files = sub_level1.i
execute_on = 'timestep_end'
keep_solution_during_restore = true
[]
[]
[Transfers]
[u_to_sub]
type = MultiAppMeshFunctionTransfer
source_variable = u
variable = u
to_multi_app = level1-
execute_on = 'timestep_end'
[]
[v_from_sub]
type = MultiAppMeshFunctionTransfer
source_variable = v
variable = v
from_multi_app = level1-
execute_on = 'timestep_end'
[]
[]
[Outputs]
exodus = true
csv = true
perf_graph = true
[screen]
type = Console
execute_postprocessors_on= "timestep_end timestep_begin"
[]
[]
(test/tests/dirackernels/constant_point_source/1d_point_source.i)
###########################################################
# This is test of the Dirac delta function System. The
# ConstantPointSource object is used to apply a constant
# Dirac delta contribution at a specified point in the
# domain.
#
# @Requirement F3.50
###########################################################
[Mesh]
type = GeneratedMesh
dim = 1
nx = 10
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[./v]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[DiracKernels]
[./point_source1]
type = ConstantPointSource
variable = u
value = 1.0
point = '0.2 0 0'
[../]
[./point_source2]
type = ConstantPointSource
variable = u
value = -0.5
point = '0.7 0 0'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = 1d_out
exodus = true
[]
(test/tests/postprocessors/side_diffusive_flux_average/side_diffusive_flux_average.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Functions]
[./right_bc]
# Flux BC for computing the analytical solution in the postprocessor
type = ParsedFunction
value = exp(y)+1
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = FunctionNeumannBC
variable = u
boundary = right
function = right_bc
[../]
[]
[Materials]
[./mat_props]
type = GenericConstantMaterial
block = 0
prop_names = diffusivity
prop_values = 2
[../]
[./mat_props_bnd]
type = GenericConstantMaterial
boundary = right
prop_names = diffusivity
prop_values = 1
[../]
[]
[Postprocessors]
[./avg_flux_right]
# Computes -\int(exp(y)+1) from 0 to 1 which is -2.718281828
type = SideDiffusiveFluxAverage
variable = u
boundary = right
diffusivity = diffusivity
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/heat_conduction_patch/heat_conduction_patch_hex20_aniso.i)
# This problem is taken from the Abaqus verification manual:
# "1.5.8 Patch test for heat transfer elements"
#
# The temperature on the exterior nodes is 200x+100y+200z.
#
# This gives a constant flux at all Gauss points.
#
# In addition, the temperature at all nodes follows the same formula.
#
# Node x y z Temperature
# 1 1.000E+00 0.000E+00 1.000E+00 4.0000E+02
# 2 6.770E-01 3.050E-01 6.830E-01 3.0250E+02
# 3 3.200E-01 1.860E-01 6.430E-01 2.1120E+02
# 4 0.000E+00 0.000E+00 1.000E+00 2.0000E+02
# 5 1.000E+00 1.000E+00 1.000E+00 5.0000E+02
# 6 7.880E-01 6.930E-01 6.440E-01 3.5570E+02
# 7 1.650E-01 7.450E-01 7.020E-01 2.4790E+02
# 8 0.000E+00 1.000E+00 1.000E+00 3.0000E+02
# 9 8.385E-01 1.525E-01 8.415E-01 3.5125E+02
# 10 4.985E-01 2.455E-01 6.630E-01 2.5685E+02
# 11 1.600E-01 9.300E-02 8.215E-01 2.0560E+02
# 12 5.000E-01 0.000E+00 1.000E+00 3.0000E+02
# 13 1.000E+00 5.000E-01 1.000E+00 4.5000E+02
# 14 7.325E-01 4.990E-01 6.635E-01 3.2910E+02
# 15 2.425E-01 4.655E-01 6.725E-01 2.2955E+02
# 16 0.000E+00 5.000E-01 1.000E+00 2.5000E+02
# 17 8.940E-01 8.465E-01 8.220E-01 4.2785E+02
# 18 4.765E-01 7.190E-01 6.730E-01 3.0180E+02
# 19 8.250E-02 8.725E-01 8.510E-01 2.7395E+02
# 20 5.000E-01 1.000E+00 1.000E+00 4.0000E+02
# 21 1.000E+00 0.000E+00 0.000E+00 2.0000E+02
# 22 0.000E+00 0.000E+00 0.000E+00 0.0000E+00
# 23 8.260E-01 2.880E-01 2.880E-01 2.5160E+02
# 24 2.490E-01 3.420E-01 1.920E-01 1.2240E+02
# 25 1.000E+00 0.000E+00 5.000E-01 3.0000E+02
# 26 5.000E-01 0.000E+00 0.000E+00 1.0000E+02
# 27 0.000E+00 0.000E+00 5.000E-01 1.0000E+02
# 28 9.130E-01 1.440E-01 1.440E-01 2.2580E+02
# 29 1.245E-01 1.710E-01 9.600E-02 6.1200E+01
# 30 7.515E-01 2.965E-01 4.855E-01 2.7705E+02
# 31 5.375E-01 3.150E-01 2.400E-01 1.8700E+02
# 32 2.845E-01 2.640E-01 4.175E-01 1.6680E+02
# 33 2.730E-01 7.500E-01 2.300E-01 1.7560E+02
# 34 0.000E+00 1.000E+00 0.000E+00 1.0000E+02
# 35 2.610E-01 5.460E-01 2.110E-01 1.4900E+02
# 36 0.000E+00 5.000E-01 0.000E+00 5.0000E+01
# 37 2.190E-01 7.475E-01 4.660E-01 2.1175E+02
# 38 1.365E-01 8.750E-01 1.150E-01 1.3780E+02
# 39 0.000E+00 1.000E+00 5.000E-01 2.0000E+02
# 40 8.500E-01 6.490E-01 2.630E-01 2.8750E+02
# 41 8.380E-01 4.685E-01 2.755E-01 2.6955E+02
# 42 8.190E-01 6.710E-01 4.535E-01 3.2160E+02
# 43 5.615E-01 6.995E-01 2.465E-01 2.3155E+02
# 44 1.000E+00 1.000E+00 0.000E+00 3.0000E+02
# 45 1.000E+00 5.000E-01 0.000E+00 2.5000E+02
# 46 1.000E+00 1.000E+00 5.000E-01 4.0000E+02
# 47 9.250E-01 8.245E-01 1.315E-01 2.9375E+02
# 48 5.000E-01 1.000E+00 0.000E+00 2.0000E+02
[Mesh]#Comment
file = heat_conduction_patch_hex20.e
[] # Mesh
[Functions]
[./temp_function]
type = ParsedFunction
value='200*x+100*y+200*z'
[../]
[] # Functions
[Variables]
[./temp]
order = SECOND
family = LAGRANGE
[../]
[] # Variables
[Kernels]
[./heat_r]
type = AnisoHeatConduction
variable = temp
[../]
[] # Kernels
[BCs]
[./temperatures]
type = FunctionDirichletBC
variable = temp
boundary = 10
function = temp_function
[../]
[] # BCs
[Materials]
[./heat]
type = AnisoHeatConductionMaterial
block = 1
specific_heat = 0.116
thermal_conductivity = '4.85e-4 0 0 0 4.85e-4 0 0 0 4.85e-4'
temperature = temp
[../]
[] # Materials
[Executioner]
type = Steady
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -ksp_gmres_restart'
petsc_options_value = 'lu 101'
line_search = 'none'
nl_abs_tol = 1e-11
nl_rel_tol = 1e-10
l_max_its = 20
[./Quadrature]
order = THIRD
[../]
[] # Executioner
[Outputs]
file_base = heat_conduction_patch_hex20_out
exodus = true
[] # Output
(test/tests/tag/2d_diffusion_dg_tag.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 4
xmin = 0
xmax = 1
ymin = 0
ymax = 1
elem_type = QUAD4
[]
[Variables]
[./u]
order = FIRST
family = MONOMIAL
[./InitialCondition]
type = ConstantIC
value = 1
[../]
[../]
[]
[AuxVariables]
[./tag_variable1]
order = FIRST
family = MONOMIAL
[../]
[./tag_variable2]
order = FIRST
family = MONOMIAL
[../]
[]
[AuxKernels]
[./TagVectorAux1]
type = TagVectorAux
variable = tag_variable1
v = u
vector_tag = vec_tag2
execute_on = timestep_end
[../]
[./TagVectorAux2]
type = TagMatrixAux
variable = tag_variable2
v = u
matrix_tag = mat_tag2
execute_on = timestep_end
[../]
[]
[Functions]
[./forcing_fn]
type = ParsedFunction
value = 2*pow(e,-x-(y*y))*(1-2*y*y)
[../]
[./exact_fn]
type = ParsedGradFunction
value = pow(e,-x-(y*y))
grad_x = -pow(e,-x-(y*y))
grad_y = -2*y*pow(e,-x-(y*y))
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
extra_matrix_tags = 'mat_tag1 mat_tag2'
extra_vector_tags = 'vec_tag1 vec_tag2'
[../]
[./abs]
type = Reaction
variable = u
extra_matrix_tags = 'mat_tag1 mat_tag2'
extra_vector_tags = 'vec_tag1 vec_tag2'
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
extra_matrix_tags = 'mat_tag1 mat_tag2'
extra_vector_tags = 'vec_tag1'
[../]
[]
[DGKernels]
[./dg_diff]
type = DGDiffusion
variable = u
epsilon = -1
sigma = 6
extra_matrix_tags = 'mat_tag1 mat_tag2'
extra_vector_tags = 'vec_tag1 vec_tag2'
[../]
[]
[BCs]
[./all]
type = DGFunctionDiffusionDirichletBC
variable = u
boundary = '0 1 2 3'
function = exact_fn
epsilon = -1
sigma = 6
extra_matrix_tags = 'mat_tag1 mat_tag2'
extra_vector_tags = 'vec_tag1 vec_tag2'
[../]
[]
[Problem]
type = TagTestProblem
test_tag_vectors = 'nontime residual vec_tag1 vec_tag2'
test_tag_matrices = 'mat_tag1 mat_tag2'
extra_tag_matrices = 'mat_tag1 mat_tag2'
extra_tag_vectors = 'vec_tag1 vec_tag2'
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
nl_rel_tol = 1e-10
[]
[Postprocessors]
[./h]
type = AverageElementSize
[../]
[./dofs]
type = NumDOFs
[../]
[./l2_err]
type = ElementL2Error
variable = u
function = exact_fn
[../]
[]
[Outputs]
exodus = true
[]
(test/tests/preconditioners/smp/smp_group_test.i)
###########################################################
# This test exercises the customer Preconditioner System.
# A Single Matrix Preconditioner is built using
# coupling specified by the user.
#
# @Requirement F1.40
###########################################################
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 10
ny = 10
elem_type = QUAD4
[]
[Variables]
[./u]
[../]
[./v]
[../]
[./p]
[../]
[./q]
[../]
[]
# Single Matrix Preconditioner
[Preconditioning]
[./SMP]
type = SMP
coupled_groups = 'u,v p,q'
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./conv_u]
type = CoupledForce
variable = u
v = v
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[./diff_p]
type = Diffusion
variable = p
[../]
[./conv_p]
type = CoupledForce
variable = p
v = q
[../]
[./diff_q]
type = Diffusion
variable = q
[../]
[]
[BCs]
[./left_u]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[./bottom_v]
type = DirichletBC
variable = v
boundary = 0
value = 5
[../]
[./top_v]
type = DirichletBC
variable = v
boundary = 2
value = 2
[../]
[./left_p]
type = DirichletBC
variable = p
boundary = 1
value = 2
[../]
[./bottom_q]
type = DirichletBC
variable = q
boundary = 0
value = 3
[../]
[./top_q]
type = DirichletBC
variable = q
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
nl_max_its = 2
[]
[Outputs]
exodus = true
[]
(modules/porous_flow/test/tests/actions/addjoiner.i)
# Tests that including PorousFlowJoiner materials doesn't cause the simulation
# to fail due to the PorousFlowAddMaterialJoiner action adding duplicate
# PorousFlowJoiner materials
[GlobalParams]
PorousFlowDictator = dictator
[]
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Variables]
[p0]
[]
[p1]
[]
[]
[Kernels]
[p0]
type = Diffusion
variable = p0
[]
[p1]
type = Diffusion
variable = p1
[]
[]
[Modules]
[FluidProperties]
[fluid0]
type = SimpleFluidProperties
[]
[fluid1]
type = SimpleFluidProperties
[]
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
at_nodes = true
[]
[temperature_qp]
type = PorousFlowTemperature
[]
[ppss_nodal]
type = PorousFlow2PhasePP
at_nodes = true
phase0_porepressure = p0
phase1_porepressure = p1
capillary_pressure = pc
[]
[ppss_qp]
type = PorousFlow2PhasePP
phase0_porepressure = p0
phase1_porepressure = p1
capillary_pressure = pc
[]
[fluid0_nodal]
type = PorousFlowSingleComponentFluid
fp = fluid0
at_nodes = true
phase = 0
[]
[fluid1_nodal]
type = PorousFlowSingleComponentFluid
fp = fluid1
at_nodes = true
phase = 1
[]
[fluid0_qp]
type = PorousFlowSingleComponentFluid
fp = fluid0
phase = 0
[]
[fluid1_qp]
type = PorousFlowSingleComponentFluid
fp = fluid1
phase = 1
[]
[density_nodal]
type = PorousFlowJoiner
at_nodes = true
material_property = PorousFlow_fluid_phase_density_nodal
[]
[density_qp]
type = PorousFlowJoiner
material_property = PorousFlow_fluid_phase_density_qp
[]
[viscosity_nodal]
type = PorousFlowJoiner
material_property = PorousFlow_viscosity_nodal
at_nodes = true
[]
[viscosity_qp]
type = PorousFlowJoiner
material_property = PorousFlow_viscosity_qp
[]
[energy_ndoal]
type = PorousFlowJoiner
at_nodes = true
material_property = PorousFlow_fluid_phase_internal_energy_nodal
[]
[energy_qp]
type = PorousFlowJoiner
material_property = PorousFlow_fluid_phase_internal_energy_qp
[]
[enthalpy_nodal]
type = PorousFlowJoiner
material_property = PorousFlow_fluid_phase_enthalpy_nodal
at_nodes = true
[]
[enthalpy_qp]
type = PorousFlowJoiner
material_property = PorousFlow_fluid_phase_enthalpy_qp
[]
[relperm0_nodal]
type = PorousFlowRelativePermeabilityConst
at_nodes = true
kr = 0.5
phase = 0
[]
[relperm1_nodal]
type = PorousFlowRelativePermeabilityConst
at_nodes = true
kr = 0.8
phase = 1
[]
[relperm_nodal]
type = PorousFlowJoiner
at_nodes = true
material_property = PorousFlow_relative_permeability_nodal
[]
[]
[Executioner]
type = Steady
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'p0 p1'
number_fluid_phases = 2
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureConst
pc = 0
[]
[]
(modules/tensor_mechanics/test/tests/ad_linear_elasticity/extra_stresses.i)
# This input file is designed to test adding extra stress to ADComputeLinearElasticStress
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmax = 50
ymax = 50
[]
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Modules/TensorMechanics/Master/All]
strain = SMALL
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx hydrostatic_stress vonmises_stress'
use_automatic_differentiation = true
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0
[../]
[./stress]
type = ADComputeLinearElasticStress
extra_stress_names = 'stress_one stress_two'
[../]
[./stress_one]
type = GenericConstantRankTwoTensor
tensor_name = stress_one
tensor_values = '0 1e3 1e3 1e3 0 1e3 1e3 1e3 0'
[../]
[./stress_two]
type = GenericConstantRankTwoTensor
tensor_name = stress_two
tensor_values = '1e3 0 0 0 1e3 0 0 0 1e3'
[../]
[]
[BCs]
[./disp_x_BC]
type = ADDirichletBC
variable = disp_x
boundary = 'bottom top'
value = 0.5
[../]
[./disp_x_BC2]
type = ADDirichletBC
variable = disp_x
boundary = 'left right'
value = 0.01
[../]
[./disp_y_BC]
type = ADDirichletBC
variable = disp_y
boundary = 'bottom top'
value = 0.8
[../]
[./disp_y_BC2]
type = ADDirichletBC
variable = disp_y
boundary = 'left right'
value = 0.02
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Postprocessors]
[./hydrostatic]
type = ElementAverageValue
variable = hydrostatic_stress
[../]
[./von_mises]
type = ElementAverageValue
variable = vonmises_stress
[../]
[]
[Outputs]
exodus = true
[]
(modules/level_set/test/tests/kernels/advection/advection_mms.i)
[Mesh]
type = GeneratedMesh
dim = 1
xmin = 0
xmax = 12
nx = 48
[]
[Adaptivity]
steps = 5
marker = marker
[./Markers]
[./marker]
type = UniformMarker
mark = REFINE
[../]
[../]
[]
[Variables]
[./phi]
[../]
[]
[AuxVariables]
[./velocity]
family = LAGRANGE_VEC
[../]
[]
[ICs]
[./vel_ic]
type = VectorFunctionIC
variable = velocity
function = velocity_func
[]
[]
[BCs]
[./left]
type = FunctionDirichletBC
boundary = 'left'
function = phi_exact
variable = phi
[../]
[]
[Functions]
[./phi_exact]
type = ParsedFunction
value = 'a*sin(pi*x/b)*cos(pi*x)'
vars = 'a b'
vals = '2 12'
[../]
[./phi_mms]
type = ParsedFunction
value = '-2*pi*a*sin(pi*x)*sin(pi*x/b) + 2*pi*a*cos(pi*x)*cos(pi*x/b)/b'
vars = 'a b'
vals = '2 12'
[../]
[./velocity_func]
type = ParsedVectorFunction
value_x = '2'
value_y = '2'
[../]
[]
[Kernels]
[./phi_advection]
type = LevelSetAdvection
variable = phi
velocity = velocity
[../]
[./phi_forcing]
type = BodyForce
variable = phi
function = phi_mms
[../]
[]
[Postprocessors]
[./error]
type = ElementL2Error
function = phi_exact
variable = phi
[../]
[./h]
type = AverageElementSize
[../]
[]
[VectorPostprocessors]
active = ''
[./results]
type = LineValueSampler
variable = phi
start_point = '0 0 0'
end_point = '12 0 0'
num_points = 500
sort_by = x
[../]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-10
solve_type = NEWTON
# A steady-state pure advection problem is numerically challenging,
# it has a zero diagonal in the Jabocian matrix. The following solver
# settings seem to reliably solve this problem.
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
[]
[Outputs]
execute_on = 'TIMESTEP_END'
csv = true
[]
(modules/porous_flow/test/tests/pressure_pulse/pressure_pulse_1d_steady.i)
# Pressure pulse in 1D with 1 phase - steady
[Mesh]
type = GeneratedMesh
dim = 1
nx = 10
xmin = 0
xmax = 100
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Variables]
[pp]
initial_condition = 2E6
[]
[]
[Kernels]
active = flux
[mass0]
type = PorousFlowMassTimeDerivative
fluid_component = 0
variable = pp
[]
[flux]
type = PorousFlowAdvectiveFlux
variable = pp
gravity = '0 0 0'
fluid_component = 0
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureVG
m = 0.5
alpha = 1e-7
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 2e9
density0 = 1000
thermal_expansion = 0
viscosity = 1e-3
[]
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pp
capillary_pressure = pc
[]
[massfrac]
type = PorousFlowMassFraction
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[porosity]
type = PorousFlowPorosityConst
porosity = 0.1
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1E-15 0 0 0 1E-15 0 0 0 1E-15'
[]
[relperm]
type = PorousFlowRelativePermeabilityCorey
n = 0
phase = 0
[]
[]
[BCs]
[left]
type = DirichletBC
boundary = left
value = 3E6
variable = pp
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-20 10000'
[]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Postprocessors]
[p000]
type = PointValue
variable = pp
point = '0 0 0'
execute_on = 'initial timestep_end'
[]
[p010]
type = PointValue
variable = pp
point = '10 0 0'
execute_on = 'initial timestep_end'
[]
[p020]
type = PointValue
variable = pp
point = '20 0 0'
execute_on = 'initial timestep_end'
[]
[p030]
type = PointValue
variable = pp
point = '30 0 0'
execute_on = 'initial timestep_end'
[]
[p040]
type = PointValue
variable = pp
point = '40 0 0'
execute_on = 'initial timestep_end'
[]
[p050]
type = PointValue
variable = pp
point = '50 0 0'
execute_on = 'initial timestep_end'
[]
[p060]
type = PointValue
variable = pp
point = '60 0 0'
execute_on = 'initial timestep_end'
[]
[p070]
type = PointValue
variable = pp
point = '70 0 0'
execute_on = 'initial timestep_end'
[]
[p080]
type = PointValue
variable = pp
point = '80 0 0'
execute_on = 'initial timestep_end'
[]
[p090]
type = PointValue
variable = pp
point = '90 0 0'
execute_on = 'initial timestep_end'
[]
[p100]
type = PointValue
variable = pp
point = '100 0 0'
execute_on = 'initial timestep_end'
[]
[]
[Outputs]
file_base = pressure_pulse_1d_steady
print_linear_residuals = false
csv = true
[]
(test/tests/meshgenerators/file_mesh_generator/2d_diffusion_test.i)
[Mesh]
[square]
type = GeneratedMeshGenerator
nx = 4
ny = 4
dim = 2
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/format/output_test_gnuplot_ps.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
nz = 0
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[]
[Postprocessors]
[./dofs]
type = NumDOFs
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
[./out]
type = Gnuplot
extension = ps
[../]
[]
(modules/heat_conduction/test/tests/heat_source_bar/ad_heat_source_bar.i)
# This is a simple 1D test of the volumetric heat source with material properties
# of a representative ceramic material. A bar is uniformly heated, and a temperature
# boundary condition is applied to the left side of the bar.
# Important properties of problem:
# Length: 0.01 m
# Thermal conductivity = 3.0 W/(mK)
# Specific heat = 300.0 J/K
# density = 10431.0 kg/m^3
# Prescribed temperature on left side: 600 K
# When it has reached steady state, the temperature as a function of position is:
# T = -q/(2*k) (x^2 - 2*x*length) + 600
# or
# T = -6.3333e+7 * (x^2 - 0.02*x) + 600
# on left side: T=600, on right side, T=6933.3
[Mesh]
type = GeneratedMesh
dim = 1
xmax = 0.01
nx = 20
[]
[Variables]
[./temp]
initial_condition = 300.0
[../]
[]
[Kernels]
[./heat]
type = ADHeatConduction
variable = temp
thermal_conductivity = thermal_conductivity
[../]
[./heatsource]
type = ADMatHeatSource
material_property = volumetric_heat
variable = temp
scalar = 10
[../]
[]
[BCs]
[./lefttemp]
type = DirichletBC
boundary = left
variable = temp
value = 600
[../]
[]
[Materials]
[./density]
type = ADGenericConstantMaterial
prop_names = 'density thermal_conductivity volumetric_heat '
prop_values = '10431.0 3.0 3.8e7'
[../]
[]
[Preconditioning]
[./full]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[./right]
type = SideAverageValue
variable = temp
boundary = right
[../]
[./error]
type = NodalL2Error
function = '-3.8e+8/(2*3) * (x^2 - 2*x*0.01) + 600'
variable = temp
[../]
[]
[Outputs]
execute_on = FINAL
exodus = true
[]
(modules/ray_tracing/test/tests/postprocessors/ray_integral_value/ray_integral_value_errors.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
[]
[]
[AuxVariables/u]
[]
[UserObjects]
active = 'repeatable'
[repeatable]
type = RepeatableRayStudy
start_points = '0 0 0'
directions = '1 0 0'
names = ray
[]
[lots]
type = LotsOfRaysRayStudy
ray_kernel_coverage_check = false
[]
[no_banking_study]
type = DisableRayBankingStudy
start_points = '0 0 0'
directions = '1 0 0'
names = ray
[]
[]
[RayBCs/kill]
type = KillRayBC
boundary = 'left right'
[]
[RayKernels]
active = ''
[null]
type = NullRayKernel
[]
[variable_integral]
type = VariableIntegralRayKernel
variable = u
[]
[]
[Postprocessors]
active = ''
[not_integral_ray_kernel]
type = RayIntegralValue
ray_kernel = null
ray = ray
[]
[kernel_not_found]
type = RayIntegralValue
ray_kernel = dummy
ray = ray
[]
[ray_not_found]
type = RayIntegralValue
ray_kernel = variable_integral
ray = dummy
[]
[no_registration]
type = RayIntegralValue
ray_kernel = variable_integral
ray = dummy
[]
[no_banking]
type = RayIntegralValue
ray_kernel = variable_integral
ray = dummy
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
(test/tests/misc/check_error/coupling_field_into_scalar.i)
[Mesh]
type = GeneratedMesh
dim = 2
[]
[AuxVariables]
[./v]
[../]
[]
[Variables]
[./u]
[../]
[./a]
family = SCALAR
order = FIRST
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./slm]
type = ScalarLagrangeMultiplier
variable = u
# this should trigger an error message, lambda is scalar
lambda = v
[../]
[]
[ScalarKernels]
[./alpha]
type = AlphaCED
variable = a
value = 1
[../]
[]
[BCs]
[./all]
type = DirichletBC
boundary = 'left right top bottom'
variable = u
value = 0
[../]
[]
[Executioner]
type = Steady
[]
(test/tests/materials/derivative_material_interface/test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
[]
[Materials]
[./provider]
type = DerivativeMaterialInterfaceTestProvider
block = 0
outputs = exodus
output_properties = 'dprop/db dprop/da d^2prop/dadb d^2prop/dadc d^3prop/dadbdc'
[../]
[./client]
type = DerivativeMaterialInterfaceTestClient
block = 0
[../]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Debug]
show_material_props = true
[]
[Outputs]
exodus = true
[]
(test/tests/bcs/nodal_normals/circle_tris.i)
[Mesh]
file = circle-tris.e
[]
[Functions]
[./all_bc_fn]
type = ParsedFunction
value = x*x+y*y
[../]
[./f_fn]
type = ParsedFunction
value = -4
[../]
[./analytical_normal_x]
type = ParsedFunction
value = x
[../]
[./analytical_normal_y]
type = ParsedFunction
value = y
[../]
[]
[NodalNormals]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = f_fn
[../]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
boundary = '1'
function = 'all_bc_fn'
[../]
[]
[Postprocessors]
[./nx_pps]
type = NodalL2Error
variable = nodal_normal_x
boundary = '1'
function = analytical_normal_x
[../]
[./ny_pps]
type = NodalL2Error
variable = nodal_normal_y
boundary = '1'
function = analytical_normal_y
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
nl_rel_tol = 1e-13
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(test/tests/meshgenerators/sidesets_bounding_box_generator/overlapping_sidesets_not_found.i)
[Mesh]
[./gmg]
type = GeneratedMeshGenerator
dim = 3
nx = 10
ny = 10
nz = 10
[]
[./createNewSidesetOne]
type = SideSetsFromBoundingBoxGenerator
input = gmg
boundary_id_old = 'bottom top'
boundary_id_new = 11
bottom_left = '-1.1 -1.1 -1.1'
top_right = '1.1 1.1 1.1'
block_id = 0
boundary_id_overlap = true
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./BCone]
type = DirichletBC
variable = u
boundary = 'left'
value = 1
[../]
[./BCtwo]
type = DirichletBC
variable = u
boundary = 11
value = 0
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/lid_driven/ad_lid_driven_stabilized_with_temp.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
nx = 16
ny = 16
[]
[./corner_node]
type = ExtraNodesetGenerator
new_boundary = 'pinned_node'
nodes = '0'
input = gen
[../]
[]
[Variables]
[./velocity]
family = LAGRANGE_VEC
[../]
[./p]
[../]
[temperature][]
[]
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[./mass_pspg]
type = INSADMassPSPG
variable = p
[../]
[./momentum_convection]
type = INSADMomentumAdvection
variable = velocity
[../]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
integrate_p_by_parts = true
[../]
[./momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[../]
[./temperature_advection]
type = INSADEnergyAdvection
variable = temperature
[../]
[./temperature_conduction]
type = ADHeatConduction
variable = temperature
thermal_conductivity = 'k'
[../]
[temperature_supg]
type = INSADEnergySUPG
variable = temperature
velocity = velocity
[]
[]
[BCs]
[./no_slip]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom right left'
[../]
[./lid]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'top'
function_x = 'lid_function'
[../]
[./pressure_pin]
type = DirichletBC
variable = p
boundary = 'pinned_node'
value = 0
[../]
[./temperature_hot]
type = DirichletBC
variable = temperature
boundary = 'bottom'
value = 1
[../]
[./temperature_cold]
type = DirichletBC
variable = temperature
boundary = 'top'
value = 0
[../]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu cp k'
prop_values = '1 1 1 .01'
[../]
[ins_mat]
type = INSADStabilized3Eqn
velocity = velocity
pressure = p
temperature = temperature
[]
[]
[Functions]
[./lid_function]
# We pick a function that is exactly represented in the velocity
# space so that the Dirichlet conditions are the same regardless
# of the mesh spacing.
type = ParsedFunction
value = '4*x*(1-x)'
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_levels -ksp_gmres_restart'
petsc_options_value = 'asm 6 200'
line_search = 'none'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
exodus = true
[]
(test/tests/auxkernels/vector_postprocessor_visualization/vector_postprocessor_visualization.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
parallel_type = REPLICATED
partitioner = linear
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
[AuxVariables]
[num_elems]
family = MONOMIAL
order = CONSTANT
[]
[partition_surface_area]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[wb_num_elems]
type = VectorPostprocessorVisualizationAux
vpp = 'wb'
vector_name = num_elems
variable = num_elems
execute_on = 'TIMESTEP_END'
[]
[wb_partition_surface_area]
type = VectorPostprocessorVisualizationAux
vpp = 'wb'
vector_name = partition_surface_area
variable = partition_surface_area
execute_on = 'TIMESTEP_END'
[]
[]
[VectorPostprocessors]
[wb]
type = WorkBalance
sync_to_all_procs = 'true'
execute_on = 'INITIAL'
[]
[]
(test/tests/interfacekernels/1d_interface/mixed_shapes.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 10
xmax = 2
[]
[./subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '1.0 0 0'
block_id = 1
top_right = '2.0 1.0 0'
[../]
[./interface]
input = subdomain1
type = SideSetsBetweenSubdomainsGenerator
primary_block = '0'
paired_block = '1'
new_boundary = 'primary0_interface'
[../]
[./interface_again]
input = interface
type = SideSetsBetweenSubdomainsGenerator
primary_block = '1'
paired_block = '0'
new_boundary = 'primary1_interface'
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
block = '0'
[../]
[./v]
order = FIRST
family = MONOMIAL
block = '1'
[../]
[]
[Kernels]
[./diff_u]
type = CoeffParamDiffusion
variable = u
D = 4
block = 0
[../]
[./diff_v]
type = CoeffParamDiffusion
variable = v
D = 2
block = 1
[../]
[./body_u]
type = BodyForce
variable = u
block = 0
function = 'x^3+x^2+x+1'
[../]
[./body_v]
type = BodyForce
variable = v
block = 1
function = 'x^3+x^2+x+1'
[../]
[]
[DGKernels]
[./dg_diff_v]
type = DGDiffusion
variable = v
block = 1
diff = 2
sigma = 6
epsilon = -1
[../]
[]
[InterfaceKernels]
[./interface]
type = OneSideDiffusion
variable = u
neighbor_var = v
boundary = primary0_interface
D = 4
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 'left'
value = 1
[../]
# [./right]
# type = DirichletBC
# variable = v
# boundary = 'right'
# value = 0
# [../]
[./right]
type = DGFunctionDiffusionDirichletBC
variable = v
boundary = 'right'
function = 0
epsilon = -1
sigma = 6
[../]
[./middle]
type = NeumannBC
variable = u
boundary = 'primary0_interface'
value = '.5'
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
print_linear_residuals = true
[]
[Debug]
show_var_residual_norms = true
[]
(test/tests/bcs/coupled_var_neumann/on_off.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 10
ny = 10
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxVariables]
[./coupled_bc_var]
[../]
[./active]
initial_condition = 1
[../]
[]
[AuxKernels]
[./active_right]
type = ConstantAux
variable = active
value = 0.5
boundary = 1
[../]
[]
[ICs]
[./coupled_bc_var]
type = FunctionIC
variable = coupled_bc_var
function = set_coupled_bc_var
[../]
[]
[Functions]
[./set_coupled_bc_var]
type = ParsedFunction
value = 'y - 0.5'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = CoupledVarNeumannBC
variable = u
boundary = 1
v = coupled_bc_var
scale_factor = active
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/ics/array_function_ic/array_function_ic_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 8
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[Variables]
[u]
components = 2
[]
[u0]
[]
[u1]
[]
[]
[AuxVariables]
[v]
components = 2
[]
[]
[Functions]
[sinx]
type = ParsedFunction
value = sin(x)
[]
[siny]
type = ParsedFunction
value = sin(y)
[]
[]
[ICs]
[uic]
type = ArrayFunctionIC
variable = u
function = 'sinx siny'
[]
[u0ic]
type = FunctionIC
variable = u0
function = sinx
[]
[u1ic]
type = FunctionIC
variable = u1
function = siny
[]
[vic]
type = ArrayFunctionIC
variable = v
function = 'sinx siny'
[]
[]
[Postprocessors]
[uint0]
type = ElementIntegralArrayVariablePostprocessor
variable = u
component = 0
[]
[uint1]
type = ElementIntegralArrayVariablePostprocessor
variable = u
component = 1
[]
[u0int]
type = ElementIntegralVariablePostprocessor
variable = u0
[]
[u1int]
type = ElementIntegralVariablePostprocessor
variable = u1
[]
[vint0]
type = ElementIntegralArrayVariablePostprocessor
variable = v
component = 0
[]
[vint1]
type = ElementIntegralArrayVariablePostprocessor
variable = v
component = 1
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/auxkernels/solution_aux/aux_nonlinear_solution_xdr.i)
[Mesh]
# This test uses SolutionUserObject which doesn't work with DistributedMesh.
type = GeneratedMesh
parallel_type = replicated
dim = 2
nx = 2
ny = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./u_aux]
[../]
[]
[Functions]
[./u_xdr_func]
type = SolutionFunction
solution = xdr_u
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./aux_xdr_kernel]
type = SolutionAux
variable = u_aux
solution = xdr_u_aux
execute_on = initial
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 2
[../]
[]
[UserObjects]
[./xdr_u_aux]
type = SolutionUserObject
system = aux0
mesh = aux_nonlinear_solution_xdr_0001_mesh.xdr
es = aux_nonlinear_solution_xdr_0001.xdr
execute_on = initial
[../]
[./xdr_u]
type = SolutionUserObject
system = nl0
mesh = aux_nonlinear_solution_xdr_0001_mesh.xdr
es = aux_nonlinear_solution_xdr_0001.xdr
execute_on = initial
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
nl_rel_tol = 1e-10
[]
[Outputs]
exodus = true
[]
[ICs]
[./u_func_ic]
function = u_xdr_func
variable = u
type = FunctionIC
[../]
[]
(test/tests/controls/restrict_exec_flag/sub.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Variables]
[u]
initial_condition = 1980
[]
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/postprocessors/num_residual_eval/num_residual_eval.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
xmin = 0
xmax = 2
ymin = 0
ymax = 2
# Since this test prints the number of residual evaluations, its
# output strongly depends on the number of processors you run it on,
# and, apparently, the type of Mesh. To reduce this variability, we
# limit it to run with ReplicatedMesh only.
parallel_type = replicated
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Postprocessors]
[./nodes]
type = NumNodes
execute_on = 'initial timestep_end'
[../]
[./elements]
type = NumElems
execute_on = 'initial timestep_end'
[../]
[./dofs]
type = NumDOFs
execute_on = 'initial timestep_end'
[../]
[./residuals]
type = NumResidualEvaluations
execute_on = 'initial timestep_end'
[../]
[]
[Outputs]
file_base = out
exodus = false
csv = true
[]
(test/tests/geomsearch/quadrature_locator_plus_constraint/quadrature_locator_plus_constraint.i)
[Mesh]
file = nodal_normals_test_offset_nonmatching_gap.e
displacements = 'disp_x disp_y'
[]
[AuxVariables]
[disp_x][]
[disp_y][]
[]
[Materials]
[gap]
type = QuadratureLocatorTestMaterial
boundary = 1
paired_boundary = 2
[]
[]
[Variables]
[T][]
[]
[Kernels]
[T]
type = Diffusion
variable = T
[]
[]
[Constraints]
[demo]
type = TiedValueConstraint
variable = T
primary_variable = T
secondary = 1
primary = 2
[]
[]
[Executioner]
type = Steady
[]
(test/tests/kernels/hfem/variable_dirichlet.i)
[Mesh]
[square]
type = GeneratedMeshGenerator
nx = 3
ny = 3
dim = 2
[]
build_all_side_lowerd_mesh = true
[]
[Variables]
[u]
order = THIRD
family = MONOMIAL
block = 0
components = 2
[]
[lambda]
order = CONSTANT
family = MONOMIAL
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
components = 2
[]
[lambdab]
order = CONSTANT
family = MONOMIAL
block = BOUNDARY_SIDE_LOWERD_SUBDOMAIN
components = 2
[]
[]
[AuxVariables]
[v]
order = CONSTANT
family = MONOMIAL
block = 0
initial_condition = '1'
[]
[uhat]
order = CONSTANT
family = MONOMIAL
block = BOUNDARY_SIDE_LOWERD_SUBDOMAIN
components = 2
[]
[]
[Kernels]
[diff]
type = ArrayDiffusion
variable = u
block = 0
diffusion_coefficient = dc
[]
[source]
type = ArrayCoupledForce
variable = u
v = v
coef = '1 2'
block = 0
[]
[]
[DGKernels]
[surface]
type = ArrayHFEMDiffusion
variable = u
lowerd_variable = lambda
[]
[]
[BCs]
[all]
type = ArrayHFEMDirichletBC
boundary = 'left right top bottom'
variable = u
lowerd_variable = lambdab
uhat = uhat
[]
[]
[Materials]
[dc]
type = GenericConstantArray
prop_name = dc
prop_value = '1 1'
[]
[]
[Postprocessors]
[intu]
type = ElementIntegralArrayVariablePostprocessor
variable = u
block = 0
[]
[lambdanorm]
type = ElementArrayL2Norm
variable = lambda
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu basic mumps'
[]
[Outputs]
[out]
# we hide lambda because it may flip sign due to element
# renumbering with distributed mesh
type = Exodus
hide = lambda
[]
csv = true
[]
(modules/phase_field/test/tests/MultiPhase/thirdphasesuppressionmaterial.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
nz = 0
xmin = 0
xmax = 1
ymin = 0
ymax = 1
elem_type = QUAD4
[]
[AuxVariables]
[./eta1]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
variable = eta1
function = x
[../]
[../]
[./eta2]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
variable = eta2
function = 1-x
[../]
[../]
[./eta3]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
variable = eta3
function = y
[../]
[../]
[]
[BCs]
[./Periodic]
[./All]
auto_direction = 'x y'
[../]
[../]
[]
[Materials]
[./suppressionbarrier]
type = ThirdPhaseSuppressionMaterial
etas = 'eta1 eta2 eta3'
function_name = g
outputs = exodus
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Problem]
solve = false
[]
[Outputs]
exodus = true
[]
(test/tests/vectorpostprocessors/point_value_sampler/not_found.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = left
value = 1
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = right
value = 0
[../]
[]
[VectorPostprocessors]
[./point_sample]
type = PointValueSampler
variable = 'u v'
points = '0.1 0.1 0 0.23 0.4 0 0.78 0.2 0 1.2 0.2 0'
sort_by = x
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
csv = true
[]
(test/tests/auxkernels/nodal_aux_var/multi_update_elem_var_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./tt]
order = CONSTANT
family = MONOMIAL
initial_condition = 100
[../]
[./ten]
order = CONSTANT
family = MONOMIAL
initial_condition = 1
[../]
[./2k]
order = CONSTANT
family = MONOMIAL
initial_condition = 2
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./all]
variable = tt
type = MultipleUpdateElemAux
vars = 'ten 2k'
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out_multi_elem_var
exodus = true
[]
(test/tests/kernels/scalar_constraint/scalar_constraint_kernel.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 2
ny = 2
elem_type = QUAD9
[]
[Functions]
[./exact_fn]
type = ParsedFunction
value = 'x*x+y*y'
[../]
[./ffn]
type = ParsedFunction
value = -4
[../]
[./bottom_bc_fn]
type = ParsedFunction
value = -2*y
[../]
[./right_bc_fn]
type = ParsedFunction
value = 2*x
[../]
[./top_bc_fn]
type = ParsedFunction
value = 2*y
[../]
[./left_bc_fn]
type = ParsedFunction
value = -2*x
[../]
[]
[Variables]
[./u]
family = LAGRANGE
order = SECOND
[../]
[./lambda]
family = SCALAR
order = FIRST
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./ffnk]
type = BodyForce
variable = u
function = ffn
[../]
[./sk_lm]
type = ScalarLagrangeMultiplier
variable = u
lambda = lambda
[../]
[]
[ScalarKernels]
[./constraint]
type = AverageValueConstraint
variable = lambda
pp_name = pp
value = 2.666666666666666
[../]
[]
[BCs]
[./bottom]
type = FunctionNeumannBC
variable = u
boundary = 'bottom'
function = bottom_bc_fn
[../]
[./right]
type = FunctionNeumannBC
variable = u
boundary = 'right'
function = right_bc_fn
[../]
[./top]
type = FunctionNeumannBC
variable = u
boundary = 'top'
function = top_bc_fn
[../]
[./left]
type = FunctionNeumannBC
variable = u
boundary = 'left'
function = left_bc_fn
[../]
[]
[Postprocessors]
[./pp]
type = ElementIntegralVariablePostprocessor
variable = u
execute_on = linear
[../]
[./l2_err]
type = ElementL2Error
variable = u
function = exact_fn
execute_on = 'initial timestep_end'
[../]
[]
[Preconditioning]
[./pc]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-9
l_tol = 1.e-10
nl_max_its = 10
# This example builds an indefinite matrix, so "-pc_type hypre -pc_hypre_type boomeramg" cannot
# be used reliably on this problem. ILU(0) seems to do OK in both serial and parallel in my testing,
# I have not seen any zero pivot issues.
petsc_options_iname = '-pc_type -sub_pc_type'
petsc_options_value = 'bjacobi ilu'
# This is a linear problem, so we don't need to recompute the
# Jacobian. This isn't a big deal for a Steady problems, however, as
# there is only one solve.
solve_type = 'LINEAR'
[]
[Outputs]
exodus = true
hide = lambda
[]
(modules/richards/test/tests/jacobian_1/jn_fu_04.i)
# unsaturated = true
# gravity = true
# supg = false
# transient = false
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = -1
xmax = 1
ymin = -1
ymax = 1
zmin = -1
zmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGnone
sat_UO = Saturation
seff_UO = SeffVG
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0 # notice small quantity, so the PETSc constant state works
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1 # notice small quantity, so the PETSc constant state works
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.2
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGnone]
type = RichardsSUPGnone
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = RandomIC
block = 0
min = -1
max = 0
[../]
[../]
[]
[Kernels]
active = 'richardsf'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFullyUpwindFlux
variable = pressure
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
viscosity = 1E-3
gravity = '1 2 3'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -snes_type'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000 test'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = jn04
exodus = false
[]
(modules/navier_stokes/test/tests/finite_volume/ins/exceptions/bad-restriction.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'
restricted_blocks = '1'
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
block = '1 2'
pressure = pressure
[]
[]
[Mesh]
parallel_type = 'replicated'
[mesh]
type = CartesianMeshGenerator
dim = 2
dx = '1 1'
dy = '1'
ix = '7 7'
iy = 10
subdomain_id = '1 2'
[]
[mid]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 1
paired_block = 2
input = mesh
new_boundary = 'middle'
[]
[break_top]
type = PatchSidesetGenerator
boundary = 'top'
n_patches = 2
input = mid
[]
[break_bottom]
type = PatchSidesetGenerator
boundary = 'bottom'
n_patches = 2
input = break_top
[]
[]
[Problem]
kernel_coverage_check = false
fv_bcs_integrity_check = true
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
block = ${restricted_blocks}
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
block = ${restricted_blocks}
[]
[pressure]
type = INSFVPressureVariable
block = ${restricted_blocks}
[]
[temperature]
type = INSFVEnergyVariable
block = ${restricted_blocks}
[]
[scalar]
type = INSFVScalarFieldVariable
block = ${restricted_blocks}
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[energy_advection]
type = INSFVEnergyAdvection
variable = temperature
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
[]
[energy_diffusion]
type = FVDiffusion
coeff = 1.1
variable = temperature
[]
[energy_loss]
type = FVBodyForce
variable = temperature
value = -0.1
[]
[scalar_advection]
type = INSFVScalarFieldAdvection
variable = scalar
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
[]
[scalar_diffusion]
type = FVDiffusion
coeff = 1
variable = scalar
[]
[scalar_src]
type = FVBodyForce
variable = scalar
value = 0.1
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = 0
[]
[top-wall-u]
type = INSFVNoSlipWallBC
boundary = 'top_0'
variable = u
function = 0
[]
[top-wall-v]
type = INSFVNoSlipWallBC
boundary = 'top_0'
variable = v
function = 0
[]
[bottom-wall-u]
type = INSFVSymmetryVelocityBC
boundary = 'bottom_0'
variable = u
mu = ${mu}
u = u
v = v
momentum_component = 'x'
[]
[bottom-wall-v]
type = INSFVSymmetryVelocityBC
boundary = 'bottom_0'
variable = v
mu = ${mu}
u = u
v = v
momentum_component = 'y'
[]
[bottom-wall-p]
type = INSFVSymmetryPressureBC
boundary = 'bottom_0'
variable = pressure
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'middle'
variable = pressure
function = 0
[]
[inlet_t]
type = FVDirichletBC
boundary = 'left'
variable = temperature
value = 1
[]
[outlet_scalar]
type = FVDirichletBC
boundary = 'middle'
variable = scalar
value = 1
[]
[]
[Materials]
[ins_fv]
type = INSFVEnthalpyMaterial
temperature = 'temperature'
rho = ${rho}
block = ${restricted_blocks}
[]
[const]
type = ADGenericFunctorMaterial
prop_names = 'cp'
prop_values = '2'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[]
(test/tests/misc/check_error/subdomain_restricted_kernel_mismatch.i)
[Mesh]
file = rectangle.e
[]
[Variables]
active = 'u v'
[./u]
order = FIRST
family = LAGRANGE
[../]
[./v]
order = FIRST
family = LAGRANGE
block = 1
[../]
[]
[Kernels]
active = 'diff body_force'
[./diff]
type = Diffusion
variable = u
[../]
[./body_force]
type = BodyForce
variable = v
block = 2
value = 10
[../]
[]
[BCs]
active = 'right'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
# petsc_options = '-snes_mf_operator'
# petsc_options_iname = '-pc_type -pc_hypre_type'
# petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/misc/check_error/old_integrity_check.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = 0
ymax = 1
nx = 20
ny = 10
elem_type = QUAD9
[]
[Functions]
[./bc_fn_v]
type = ParsedFunction
value = (x*x+y*y)
[../]
[]
[Variables]
[./v]
family = LAGRANGE
order = SECOND
[../]
[./u]
family = LAGRANGE
order = SECOND
[../]
[]
[Kernels]
[./diff_v]
type = CoefDiffusion
variable = u
coef = 0.5
[../]
[./conv_v]
type = CoupledConvection
variable = v
velocity_vector = u
lag_coupling = true # Here we are asking for an old value but this is a steady test!
[../]
[]
[BCs]
[./top_v]
type = FunctionDirichletBC
variable = v
boundary = top
function = bc_fn_v
[../]
[./left_u]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(test/tests/materials/derivative_material_interface/const.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
[]
[AuxVariables]
[./dummy]
[../]
[]
[Materials]
[./provider]
type = DerivativeMaterialInterfaceTestProvider
block = 0
[../]
[./client]
type = DerivativeMaterialInterfaceTestClient
prop_name = prop
block = 0
outputs = exodus
[../]
[./client2]
type = DerivativeMaterialInterfaceTestClient
prop_name = 1.0
block = 0
outputs = exodus
[../]
[./dummy]
type = GenericConstantMaterial
prop_names = prop
block = 0
prop_values = 0
[../]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Outputs]
exodus = true
[]
(test/tests/mesh_modifiers/boundingbox_nodeset/boundingbox_nodeset_outside_test.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 2
[]
[middle_node]
type = BoundingBoxNodeSetGenerator
input = gen
new_boundary = middle_node
top_right = '1.1 1.1 0'
bottom_left = '0.51 0.51 0'
location = OUTSIDE
[]
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[]
[middle]
type = DirichletBC
variable = u
boundary = middle_node
value = -1
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
[]
[Outputs]
file_base = boundingbox_nodeset_outside_out
exodus = true
[]
(test/tests/auxkernels/gap_value/gap_value.i)
[Mesh]
file = nonmatching.e
dim = 2
# This test will not work in parallel with DistributedMesh enabled
# due to a bug in the GeometricSearch system. See #2121 for more
# information.
parallel_type = replicated
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./gap_value]
block = left
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = u
boundary = 'leftbottom rightbottom'
value = 0
[../]
[./top]
type = DirichletBC
variable = u
boundary = 'lefttop righttop'
value = 1
[../]
[]
[AuxKernels]
[./gap_value_aux]
type = GapValueAux
variable = gap_value
boundary = leftright
paired_variable = u
paired_boundary = rightleft
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/xda/xdr.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
xdr = true
[]
(modules/reactor/test/tests/meshgenerators/reporting_id/cartesian_id/core_reporting_id.i)
[Mesh]
[pin1]
type = ConcentricCircleMeshGenerator
num_sectors = 2
radii = '0.4 0.5'
rings = '1 1 1'
has_outer_square = on
pitch = 1.26
preserve_volumes = yes
smoothing_max_it = 3
[]
[pin2]
type = ConcentricCircleMeshGenerator
num_sectors = 2
radii = '0.3 0.4'
rings = '1 1 1'
has_outer_square = on
pitch = 1.26
preserve_volumes = yes
smoothing_max_it = 3
[]
[assembly1]
type = CartesianIDPatternedMeshGenerator
inputs = 'pin1 pin2'
pattern = ' 1 0 1 0;
0 1 0 1;
1 0 1 0;
0 1 0 1'
assign_type = 'cell'
id_name = 'pin_id'
[]
[assembly2]
type = CartesianIDPatternedMeshGenerator
inputs = 'pin1 pin2'
pattern = ' 0 1 1 0;
1 0 0 1;
1 0 0 1;
0 1 1 0'
assign_type = 'cell'
id_name = 'pin_id'
[]
[core]
type = CartesianIDPatternedMeshGenerator
inputs = 'assembly1 assembly2'
pattern = '0 1;
1 0'
assign_type = 'cell'
id_name = 'assembly_id'
[]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[AuxVariables]
[pin_id]
family = MONOMIAL
order = CONSTANT
[]
[assembly_id]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[set_pin_id]
type = ExtraElementIDAux
variable = pin_id
extra_id_name = pin_id
[]
[set_assembly_id]
type = ExtraElementIDAux
variable = assembly_id
extra_id_name = assembly_id
[]
[]
[Outputs]
exodus = true
execute_on = timestep_end
[]
(test/tests/mesh_modifiers/mesh_extruder/extruder_tri.i)
[Mesh]
[file]
type = FileMeshGenerator
file = ellipse_tri.e
[]
[extrude]
type = MeshExtruderGenerator
input = file
num_layers = 20
extrusion_vector = '0 0 5'
bottom_sideset = '2'
top_sideset = '4'
[]
[]
[Variables]
active = 'u'
[u]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
active = 'diff'
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[bottom]
type = DirichletBC
variable = u
boundary = 2
value = 0
[]
[top]
type = DirichletBC
variable = u
boundary = 4
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out_tri
exodus = true
[]
[Debug]
show_actions = true
[]
(examples/ex14_pps/ex14_compare_solutions_2.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 11
ny = 11
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
[]
[Variables]
[./forced]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = forced
[../]
[./forcing]
type = BodyForce
variable = forced
function = 'x*x+y*y' # Any object expecting a function name can also receive a ParsedFunction string
[../]
[]
[BCs]
[./all]
type = DirichletBC
variable = forced
boundary = 'bottom right top left'
value = 0
[../]
[]
[UserObjects]
[./fine_solution]
# Read in the fine grid solution
type = SolutionUserObject
system_variables = forced
mesh = ex14_compare_solutions_1_out_0000_mesh.xda
es = ex14_compare_solutions_1_out_0000.xda
[../]
[]
[Functions]
[./fine_function]
# Create a Function out of the fine grid solution
# Note: This references the SolutionUserObject above
type = SolutionFunction
solution = fine_solution
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[./Quadrature]
# The integration of the error happens on the coarse mesh
# To reduce integration error of the finer solution we can
# raise the integration order.
# Note: This will slow down the calculation a bit
order = SIXTH
[../]
[]
[Postprocessors]
[./error]
# Compute the error between the computed solution and the fine-grid solution
type = ElementL2Error
variable = forced
function = fine_function
[../]
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/coupled-force/gravity-through-coupled-force.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
nx = 16
ny = 16
[]
[./corner_node]
type = ExtraNodesetGenerator
new_boundary = 'pinned_node'
nodes = '0'
input = gen
[../]
[]
[Variables]
[./velocity]
family = LAGRANGE_VEC
[../]
[./p]
[../]
[u]
family = LAGRANGE_VEC
[]
[]
[AuxVariables]
[gravity]
family = LAGRANGE_VEC
[]
[]
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[gravity]
type = VectorConstantIC
x_value = '0'
y_value = '-9.81'
variable = gravity
[]
[]
[Kernels]
inactive = 'momentum_coupled_forces_two_vars momentum_coupled_forces_two_funcs'
[./mass]
type = INSADMass
variable = p
[../]
[./mass_pspg]
type = INSADMassPSPG
variable = p
[../]
[./momentum_convection]
type = INSADMomentumAdvection
variable = velocity
[../]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
integrate_p_by_parts = true
[../]
[momentum_coupled_forces_var_and_func]
type = INSADMomentumCoupledForce
variable = velocity
coupled_vector_var = u
vector_function = 'vector_gravity_func'
[]
[momentum_coupled_forces_two_vars]
type = INSADMomentumCoupledForce
variable = velocity
coupled_vector_var = 'u gravity'
[]
[momentum_coupled_forces_two_funcs]
type = INSADMomentumCoupledForce
variable = velocity
vector_function = 'vector_func vector_gravity_func'
[]
[./momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[../]
[u_diff]
type = VectorDiffusion
variable = u
[]
[]
[BCs]
[./no_slip]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom right left top'
[../]
[./pressure_pin]
type = DirichletBC
variable = p
boundary = 'pinned_node'
value = 0
[../]
[u_left]
type = VectorFunctionDirichletBC
variable = u
boundary = 'left'
function_x = 1
function_y = 1
[]
[u_right]
type = VectorFunctionDirichletBC
variable = u
boundary = 'right'
function_x = -1
function_y = -1
[]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[ins_mat]
type = INSADTauMaterial
velocity = velocity
pressure = p
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_levels -ksp_gmres_restart'
petsc_options_value = 'asm 6 200'
line_search = 'none'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
[out]
type = Exodus
hide = 'gravity'
[]
[]
[Functions]
[vector_func]
type = ParsedVectorFunction
value_x = '-2*x + 1'
value_y = '-2*x + 1'
[]
[vector_gravity_func]
type = ParsedVectorFunction
value_x = '0'
value_y = '-9.81'
[]
[]
(modules/navier_stokes/test/tests/finite_element/ins/lid_driven/lid_driven_stabilized_action.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
nx = 64
ny = 64
[]
[]
[Modules]
[IncompressibleNavierStokes]
equation_type = steady-state
block = 0
velocity_boundary = 'bottom right top left'
velocity_function = '0 0 0 0 lid_function 0 0 0'
pressure_pinned_node = 0
density_name = rho
dynamic_viscosity_name = mu
# There are multiple types of stabilization possible in incompressible
# Navier Stokes. The user can specify supg = true to apply streamline
# upwind petrov-galerkin stabilization to the momentum equations. This
# is most useful for high Reynolds numbers, e.g. when inertial effects
# dominate over viscous effects. The user can also specify pspg = true
# to apply pressure stabilized petrov-galerkin stabilization to the mass
# equation. PSPG is a form of Galerkin Least Squares. This stabilization
# allows equal order interpolations to be used for pressure and velocity.
# Finally, the alpha parameter controls the amount of stabilization.
# For PSPG, decreasing alpha leads to increased accuracy but may induce
# spurious oscillations in the pressure field. Some numerical experiments
# suggest that alpha between .1 and 1 may be optimal for accuracy and
# robustness.
supg = true
pspg = true
alpha = 1e-1
laplace = true
integrate_p_by_parts = true
gravity = '0 0 0'
family = LAGRANGE
order = FIRST
[]
[]
[Materials]
[const]
type = GenericConstantMaterial
block = 0
prop_names = 'rho mu'
prop_values = '1 1'
[]
[]
[Functions]
[lid_function]
# We pick a function that is exactly represented in the velocity
# space so that the Dirichlet conditions are the same regardless
# of the mesh spacing.
type = ParsedFunction
value = '4*x*(1-x)'
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_asm_overlap -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = 'asm 2 ilu 4'
line_search = 'none'
nl_rel_tol = 1e-12
nl_abs_tol = 1e-13
nl_max_its = 6
l_tol = 1e-6
l_max_its = 500
[]
[Outputs]
file_base = lid_driven_stabilized_out
exodus = true
[]
[Postprocessors]
[lin]
type = NumLinearIterations
[]
[nl]
type = NumNonlinearIterations
[]
[lin_tot]
type = CumulativeValuePostprocessor
postprocessor = 'lin'
[]
[nl_tot]
type = CumulativeValuePostprocessor
postprocessor = 'nl'
[]
[]
(test/tests/bcs/ad_1d_neumann/1d_neumann.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 10
construct_side_list_from_node_list = true
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = ADNeumannBC
variable = u
boundary = right
value = 2
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/perf_graph/multi_app/master_full.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
perf_graph = true
[]
[MultiApps]
[./full_solve]
type = FullSolveMultiApp
execute_on = initial
positions = '0 0 0'
input_files = sub_full.i
[../]
[]
(modules/richards/test/tests/jacobian_1/jn07.i)
# unsaturated = false
# gravity = true
# supg = true
# transient = false
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = -1
xmax = 1
ymin = -1
ymax = 1
zmin = -1
zmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0 # notice small quantity, so the PETSc constant state works
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1 # notice small quantity, so the PETSc constant state works
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.2
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 0.1
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = RandomIC
block = 0
min = 0
max = 1
[../]
[../]
[]
[Kernels]
active = 'richardsf'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGstandard
sat_UO = Saturation
seff_UO = SeffVG
viscosity = 1E-3
gravity = '1 2 3'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -snes_type'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000 test'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = jn07
exodus = false
[]
(modules/navier_stokes/test/tests/finite_element/ins/wall_convection/steady.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
nx = 16
ny = 16
[]
[./corner_node]
type = ExtraNodesetGenerator
new_boundary = 'pinned_node'
nodes = '0'
input = gen
[../]
[]
[Variables]
[./velocity]
family = LAGRANGE_VEC
[../]
[./p]
[../]
[temperature][]
[]
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[./mass_pspg]
type = INSADMassPSPG
variable = p
[../]
[./momentum_convection]
type = INSADMomentumAdvection
variable = velocity
[../]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
integrate_p_by_parts = true
[../]
[./momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[../]
[./temperature_advection]
type = INSADEnergyAdvection
variable = temperature
[../]
[./temperature_conduction]
type = ADHeatConduction
variable = temperature
thermal_conductivity = 'k'
[../]
[temperature_ambient_convection]
type = INSADEnergyAmbientConvection
variable = temperature
alpha = 1
T_ambient = 0.5
[]
[temperature_supg]
type = INSADEnergySUPG
variable = temperature
velocity = velocity
[]
[]
[BCs]
[./no_slip]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom right left'
[../]
[./lid]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'top'
function_x = 'lid_function'
[../]
[./pressure_pin]
type = DirichletBC
variable = p
boundary = 'pinned_node'
value = 0
[../]
[./temperature_hot]
type = DirichletBC
variable = temperature
boundary = 'bottom'
value = 1
[../]
[./temperature_cold]
type = DirichletBC
variable = temperature
boundary = 'top'
value = 0
[../]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu cp k'
prop_values = '1 1 1 .01'
[../]
[ins_mat]
type = INSADStabilized3Eqn
velocity = velocity
pressure = p
temperature = temperature
[]
[]
[Functions]
[./lid_function]
# We pick a function that is exactly represented in the velocity
# space so that the Dirichlet conditions are the same regardless
# of the mesh spacing.
type = ParsedFunction
value = '4*x*(1-x)'
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_levels -ksp_gmres_restart'
petsc_options_value = 'asm 6 200'
line_search = 'none'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/exodus/exodus_enable_initial.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
[./out]
type = Exodus
execute_on = 'initial timestep_end'
[../]
[]
[Debug]
show_var_residual_norms = true
#show_actions = true
[]
(test/tests/dgkernels/2d_diffusion_dg/no_mallocs_with_action.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
elem_type = QUAD4
[]
[Variables]
[./u]
order = FIRST
family = MONOMIAL
[./InitialCondition]
type = ConstantIC
value = 1
[../]
[../]
[]
[AuxVariables]
[v]
order = FIRST
family = MONOMIAL
[]
[]
[Functions]
[./forcing_fn]
type = ParsedFunction
value = 2*pow(e,-x-(y*y))*(1-2*y*y)
[../]
[./exact_fn]
type = ParsedGradFunction
value = pow(e,-x-(y*y))
grad_x = -pow(e,-x-(y*y))
grad_y = -2*y*pow(e,-x-(y*y))
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./abs] # u * v
type = Reaction
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[DGDiffusionAction]
variable = u
epsilon = -1
sigma = 6
# We couple in an auxiliary variable in order to ensure that we've properly
# ghosted both non-linear and auxiliary solution vectors
coupled_var = v
[]
[BCs]
[./all]
type = DGFunctionDiffusionDirichletBC
variable = u
boundary = '0 1 2 3'
function = exact_fn
epsilon = -1
sigma = 6
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
csv = true
[console]
type = Console
system_info = 'framework mesh aux nonlinear relationship execution'
[]
[]
[Problem]
error_on_jacobian_nonzero_reallocation = true
[]
[Postprocessors]
active = 'num_rm'
[num_rm]
type = NumRelationshipManagers
[]
[num_internal_sides]
type = NumInternalSides
[]
[]
(test/tests/actions/debug_block/debug_print_actions_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
nz = 0
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 0
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
[]
[Debug]
show_action_dependencies = true
show_actions = true
show_top_residuals = 5
[]
(tutorials/tutorial01_app_development/step09_mat_props/test/tests/kernels/simple_diffusion/simple_diffusion.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/function_file_test16.i)
# Test for usage of missing function
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = ic_function
[../]
[../]
[]
[Functions]
[./ic_function]
type = PiecewiseLinear
data_file = piecewise_linear_rows_more_data.csv
xy_in_file_only = false
y_index_in_file = 3 # will generate an error because no forth row of data
scale_factor = 1.0
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/boussinesq/boussinesq_stabilized_action.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmax = .05
ymax = .05
nx = 20
ny = 20
elem_type = QUAD9
[]
[]
[Preconditioning]
[Newton_SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
nl_rel_tol = 1e-12
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_shift_type -ksp_gmres_restart'
petsc_options_value = 'bjacobi lu NONZERO 200'
[]
[Debug]
show_var_residual_norms = true
[]
[Outputs]
file_base = boussinesq_stabilized_out
[out]
type = Exodus
execute_on = 'final'
[]
[]
[Modules]
[IncompressibleNavierStokes]
equation_type = steady-state
gravity = '0 -9.81 0'
velocity_boundary = 'bottom right top left'
velocity_function = '0 0 0 0 0 0 0 0'
# Even though we are integrating by parts, because there are no integrated
# boundary conditions on the velocity p doesn't appear in the system of
# equations. Thus we must pin the pressure somewhere in order to ensure a
# unique solution
pressure_pinned_node = 0
density_name = rho
dynamic_viscosity_name = mu
initial_velocity = '1e-15 1e-15 0'
use_ad = true
add_standard_velocity_variables_for_ad = false
pspg = true
supg = true
family = LAGRANGE
order = FIRST
add_temperature_equation = true
temperature_variable = temp
temperature_scaling = 1e-4
initial_temperature = 340
thermal_conductivity_name = k
specific_heat_name = cp
natural_temperature_boundary = 'top bottom'
fixed_temperature_boundary = 'left right'
temperature_function = '300 400'
boussinesq_approximation = true
# material property for reference temperature does not need to be AD material property
reference_temperature_name = temp_ref
thermal_expansion_name = alpha
[]
[]
[Materials]
[ad_const]
type = ADGenericConstantMaterial
# alpha = coefficient of thermal expansion where rho = rho0 -alpha * rho0 * delta T
prop_names = 'mu rho alpha k cp'
prop_values = '30.74e-6 .5757 2.9e-3 46.38e-3 1054'
[]
[const]
type = GenericConstantMaterial
prop_names = 'temp_ref'
prop_values = '900'
[]
[]
(modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/ad_rz_cone_by_parts_steady_nobcbc.i)
[GlobalParams]
integrate_p_by_parts = true
[]
[Mesh]
file = '2d_cone.msh'
[]
[Problem]
coord_type = RZ
[]
[AuxVariables]
[vel_x]
order = SECOND
[]
[vel_y]
order = SECOND
[]
[]
[AuxKernels]
[vel_x]
type = VectorVariableComponentAux
variable = vel_x
vector_variable = velocity
component = 'x'
[]
[vel_y]
type = VectorVariableComponentAux
variable = vel_y
vector_variable = velocity
component = 'y'
[]
[]
[Variables]
[./velocity]
order = SECOND
family = LAGRANGE_VEC
[../]
[./p]
[../]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[./momentum_convection]
type = INSADMomentumAdvection
variable = velocity
[../]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
[../]
[]
[BCs]
[inlet]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom'
function_x = 0
function_y = 'inlet_func'
[../]
[wall]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'right'
function_x = 0
function_y = 0
[]
[axis]
type = ADVectorFunctionDirichletBC
variable = velocity
boundary = 'left'
set_y_comp = false
function_x = 0
[]
[outlet]
type = INSADMomentumNoBCBC
variable = velocity
pressure = p
boundary = 'top'
[]
# When the NoBCBC is applied on the outlet boundary then there is nothing
# constraining the pressure. Thus we must pin the pressure somewhere to ensure
# that the problem is not singular. If the below BC is not applied then
# -pc_type svd -pc_svd_monitor reveals a singular value
[p_corner]
type = DirichletBC
boundary = top_right
value = 0
variable = p
[]
[]
[Functions]
[./inlet_func]
type = ParsedFunction
value = '-4 * x^2 + 1'
[../]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[ins_mat]
type = INSADMaterial
velocity = velocity
pressure = p
[]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = 'bjacobi ilu 4'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
csv = true
console = true
[./out]
type = Exodus
[../]
[]
[Postprocessors]
[./flow_in]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'bottom'
execute_on = 'timestep_end'
[../]
[./flow_out]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'top'
execute_on = 'timestep_end'
[../]
[]
(test/tests/dgkernels/adaptivity/adaptivity.i)
# This input file is used for two tests:
# 1) Check that DGKernels work with mesh adaptivity
# 2) Error out when DGKernels are used with adaptivity
# and stateful material prpoerties
[Mesh]
type = GeneratedMesh
dim = 3
nx = 2
ny = 2
nz = 2
parallel_type = 'replicated'
[]
[Variables]
[./u]
order = FIRST
family = MONOMIAL
[./InitialCondition]
type = ConstantIC
value = 1
[../]
[../]
[]
[Functions]
[./forcing_fn]
type = ParsedFunction
value = (x*x*x)-6.0*x
[../]
[./bc_fn]
type = ParsedFunction
value = (x*x*x)
[../]
[]
[Kernels]
[./diff]
type = MatDiffusionTest
variable = u
prop_name = diffusivity
[../]
[./abs]
type = Reaction
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[DGKernels]
[./dgdiff]
type = DGDiffusion
variable = u
sigma = 6
epsilon = -1.0
diff = diffusivity
[../]
[]
[BCs]
active = 'all'
[./all]
type = DGMDDBC
variable = u
boundary = '1 2 3 4'
function = bc_fn
prop_name = diffusivity
sigma = 6
epsilon = -1.0
[../]
[]
[Materials]
active = 'constant'
[./stateful]
type = StatefulTest
prop_names = 'diffusivity'
prop_values = '1'
[../]
[./constant]
type = GenericConstantMaterial
prop_names = 'diffusivity'
prop_values = '1'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Adaptivity]
marker = 'marker'
steps = 1
[./Indicators]
[./error]
type = GradientJumpIndicator
variable = u
[../]
[../]
[./Markers]
[./marker]
type = ErrorFractionMarker
coarsen = 0.5
indicator = error
refine = 0.5
[../]
[../]
[]
[Outputs]
exodus = true
[]
(test/tests/multiapps/secant/steady_sub.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[v]
[]
[]
[AuxVariables]
[u]
[]
[]
[Kernels]
[diff_v]
type = Diffusion
variable = v
[]
[force_v]
type = CoupledForce
variable = v
v = u
[]
[]
[BCs]
[left_v]
type = DirichletBC
variable = v
boundary = left
value = 1
[]
[right_v]
type = DirichletBC
variable = v
boundary = right
value = 0
[]
[]
[Postprocessors]
[vnorm]
type = ElementL2Norm
variable = v
[]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
nl_abs_tol = 1e-14
fixed_point_algorithm = 'secant'
[]
[Outputs]
csv = true
exodus = false
[]
(test/tests/transfers/from_full_solve/master.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
# This test currently diffs when run in parallel with DistributedMesh enabled,
# most likely due to the fact that CONSTANT MONOMIALS are currently not written
# out correctly in this case. For more information, see #2122.
parallel_type = replicated
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./from_full]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
[MultiApps]
[./full_solve]
type = FullSolveMultiApp
app_type = MooseTestApp
execute_on = initial
positions = '0 0 0'
input_files = sub.i
[../]
[]
[Transfers]
[./from_full]
type = MultiAppNearestNodeTransfer
from_multi_app = full_solve
source_variable = u
variable = from_full
[../]
[]
(modules/heat_conduction/test/tests/heat_conduction/2d_quadrature_gap_heat_transfer/perfectQ9.i)
[GlobalParams]
order = SECOND
[]
[Mesh]
file = perfectQ9.e
[]
[Variables]
[./temp]
[../]
[]
[Kernels]
[./hc]
type = HeatConduction
variable = temp
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = temp
boundary = leftleft
value = 300
[../]
[./right]
type = DirichletBC
variable = temp
boundary = rightright
value = 400
[../]
[]
[ThermalContact]
[./left_to_right]
secondary = leftright
quadrature = true
primary = rightleft
emissivity_primary = 0
emissivity_secondary = 0
variable = temp
type = GapHeatTransfer
[../]
[]
[Materials]
[./hcm]
type = HeatConductionMaterial
block = 'left right'
specific_heat = 1
thermal_conductivity = 1
[../]
[]
[Executioner]
type = Steady
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
[./Quadrature]
order = THIRD
[../]
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/pins/mms/porosity_change/1d-rc-continuous.i)
mu=1.5
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'
[Mesh]
[mesh]
type = CartesianMeshGenerator
dim = 1
dx = '1 1'
ix = '15 15'
[]
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = PINSFVRhieChowInterpolator
u = u
porosity = porosity
pressure = pressure
[]
[]
[Problem]
error_on_jacobian_nonzero_reallocation = true
[]
[Variables]
[u]
type = PINSFVSuperficialVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[AuxVariables]
[porosity]
family = MONOMIAL
order = CONSTANT
fv = true
[]
[]
[ICs]
[porosity_continuous]
type = FunctionIC
variable = porosity
function = smooth_jump
[]
[]
[Functions]
[smooth_jump]
type = ParsedFunction
value = '1 - 0.5 * 1 / (1 + exp(-30*(x-1)))'
[]
# Generated by compute-functions-1d.py
[exact_u]
type = ParsedFunction
value = 'cos((1/2)*x*pi)'
[]
[forcing_u]
type = ADParsedFunction
value = '-mu*(1 - 0.5/(exp(30 - 30*x) + 1))*(-1/4*pi^2*cos((1/2)*x*pi)/(1 - 0.5/(exp(30 - 30*x) + 1)) - 15.0*pi*exp(30 - 30*x)*sin((1/2)*x*pi)/((1 - 0.5/(exp(30 - 30*x) + 1))^2*(exp(30 - 30*x) + 1)^2) - 450.0*exp(30 - 30*x)*cos((1/2)*x*pi)/((1 - 0.5/(exp(30 - 30*x) + 1))^2*(exp(30 - 30*x) + 1)^2) + 900.0*exp(60 - 60*x)*cos((1/2)*x*pi)/((1 - 0.5/(exp(30 - 30*x) + 1))^2*(exp(30 - 30*x) + 1)^3) + 450.0*exp(60 - 60*x)*cos((1/2)*x*pi)/((1 - 0.5/(exp(30 - 30*x) + 1))^3*(exp(30 - 30*x) + 1)^4)) + 15.0*mu*(-1/2*pi*sin((1/2)*x*pi)/(1 - 0.5/(exp(30 - 30*x) + 1)) + 15.0*exp(30 - 30*x)*cos((1/2)*x*pi)/((1 - 0.5/(exp(30 - 30*x) + 1))^2*(exp(30 - 30*x) + 1)^2))*exp(30 - 30*x)/(exp(30 - 30*x) + 1)^2 - pi*rho*sin((1/2)*x*pi)*cos((1/2)*x*pi)/(1 - 0.5/(exp(30 - 30*x) + 1)) + 15.0*rho*exp(30 - 30*x)*cos((1/2)*x*pi)^2/((1 - 0.5/(exp(30 - 30*x) + 1))^2*(exp(30 - 30*x) + 1)^2) + (1 - 0.5/(exp(30 - 30*x) + 1))*cos(x)'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_p]
type = ParsedFunction
value = 'sin(x)'
[]
[forcing_p]
type = ParsedFunction
value = '-1/2*pi*rho*sin((1/2)*x*pi)'
vars = 'rho'
vals = '${rho}'
[]
[]
[FVKernels]
[mass]
type = PINSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[u_advection]
type = PINSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
porosity = porosity
momentum_component = 'x'
[]
[u_viscosity]
type = PINSFVMomentumDiffusion
variable = u
mu = ${mu}
porosity = porosity
momentum_component = 'x'
[]
[u_pressure]
type = PINSFVMomentumPressure
variable = u
pressure = pressure
porosity = porosity
momentum_component = 'x'
[]
[u_forcing]
type = INSFVBodyForce
variable = u
functor = forcing_u
momentum_component = 'x'
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = 'exact_u'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 'exact_p'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 200 lu NONZERO'
line_search = 'none'
# ksp_gmres_restart bumped to 200 for linear convergence
nl_max_its = 100
[]
[Postprocessors]
[inlet_p]
type = SideAverageValue
variable = 'pressure'
boundary = 'left'
[]
[outlet-u]
type = SideIntegralVariablePostprocessor
variable = u
boundary = 'right'
[]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2p]
variable = pressure
function = exact_p
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
[Outputs]
exodus = true
csv = true
[]
(test/tests/kernels/ad_coupled_value/ad_aux_coupled_value.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 4
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[v]
initial_condition = 2
[]
[exact]
[]
[]
[ICs]
[exact]
type = FunctionIC
function = 'x*(2-x)'
variable = exact
[]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./ad_coupled_value]
type = ADCoupledValueTest
variable = u
v = v
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'Newton'
[]
[Outputs]
exodus = true
[]
(modules/phase_field/test/tests/feature_volume_vpp_test/boundary_area_3D.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
nx = 6
ny = 25
nz = 15
xmin = 20
xmax = 30
ymin = 0
ymax = 50
zmin = 10
zmax = 40
elem_type = HEX8
[]
[./left_side]
input = gen
type = SubdomainBoundingBoxGenerator
block_id = 1
bottom_left = '0 0 0'
top_right = '24.9 50 50'
[../]
[./right_side]
input = left_side
type = SubdomainBoundingBoxGenerator
block_id = 2
bottom_left = '25.1 0 0'
top_right = '50 50 50'
[../]
[./iface_u]
input = right_side
type = SideSetsBetweenSubdomainsGenerator
primary_block = 1
paired_block = 2
new_boundary = 10
[../]
[]
[Variables]
[./c]
order = FIRST
family = LAGRANGE
[]
[]
[ICs]
[./c]
type = SpecifiedSmoothCircleIC
variable = c
invalue = 1.0
outvalue = 0.0
radii = '4 5 10'
x_positions = '25 25 25'
y_positions = '40 25 0'
z_positions = '25 25 25'
int_width = 2.0
[]
[]
[Postprocessors]
[./flood_count]
type = FeatureFloodCount
variable = c
# Must be turned on to build data structures necessary for FeatureVolumeVPP
compute_var_to_feature_map = true
threshold = 0.001
execute_on = INITIAL
[../]
[]
[VectorPostprocessors]
[./features]
type = FeatureVolumeVectorPostprocessor
flood_counter = flood_count
# Turn on centroid output
output_centroids = true
execute_on = INITIAL
boundary = 10
single_feature_per_element = false
[../]
[]
[Kernels]
[diff]
type = Diffusion
variable = c
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
execute_on = INITIAL
[]
(test/tests/vectorpostprocessors/element_id_counters/interface_element_counter.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
xmax = 1
ymax = 1
extra_element_integers = foo_id
[]
[id0]
type = SubdomainBoundingBoxGenerator
input = gmg
bottom_left = '0 0 0'
block_id = 0
top_right = '1 1 0'
integer_name = foo_id
[]
[id1]
type = SubdomainBoundingBoxGenerator
input = id0
bottom_left = '0.4 0.4 0'
block_id = 1
top_right = '0.9 0.9 0'
integer_name = foo_id
[]
[id2]
type = SubdomainBoundingBoxGenerator
input = id1
bottom_left = '0.1 0.1 0'
block_id = 2
top_right = '0.6 0.6 0'
integer_name = foo_id
[]
[subdomain]
type = SubdomainBoundingBoxGenerator
input = id2
bottom_left = '0 0.6 0'
block_id = 1
top_right = '1 1 0'
[]
[side0to1]
type = SideSetsBetweenSubdomainsGenerator
input = subdomain
primary_block = 0
paired_block = 1
new_boundary = side0to1
[]
[]
[AuxVariables]
[foo_id_var]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[foo_id]
type = ExtraElementIDAux
variable = foo_id_var
extra_id_name = foo_id
[]
[]
[VectorPostprocessors]
[elem_counter]
type = InterfaceElementCounterWithID
boundary = side0to1
id_name = foo_id
[]
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
csv = true
execute_on = 'timestep_end'
[]
(test/tests/mesh_modifiers/add_side_sets_from_bounding_box/overlapping_sidesets_not_found.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
nx = 10
ny = 10
nz = 10
[]
[createNewSidesetOne]
type = SideSetsFromBoundingBoxGenerator
input = gen
block_id = 0
boundary_id_old = 'bottom top'
boundary_id_new = 11
bottom_left = '-1.1 -1.1 -1.1'
top_right = '1.1 1.1 1.1'
boundary_id_overlap = true
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[BCone]
type = DirichletBC
variable = u
boundary = 'left'
value = 1
[]
[BCtwo]
type = DirichletBC
variable = u
boundary = 11
value = 0
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/ics/integral_preserving_function_ic/sinusoidal_z.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 5
ny = 5
nz = 20
xmax = 1.5
ymax = 1.7
zmax = 1.9
xmin = 0.0
ymin = 0.0
zmin = 0.0
[]
[Problem]
type = FEProblem
solve = false
[]
[AuxVariables]
[power]
family = MONOMIAL
order = CONSTANT
[]
[]
[ICs]
[power]
type = IntegralPreservingFunctionIC
variable = power
magnitude = 550.0
function = 'sin(pi * z / 1.9)'
integral = vol
[]
[]
[Postprocessors]
[vol]
type = FunctionElementIntegral
function = 'sin(pi * z / 1.9)'
execute_on = 'initial'
[]
[integrated_power] # should equal 550
type = ElementIntegralVariablePostprocessor
variable = power
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/relationship_managers/two_rm/two_rm.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 8
ny = 8
output_ghosting = true
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
[]
[]
[AuxVariables]
[proc]
order = 'CONSTANT'
family = 'MONOMIAL'
[]
[]
[AuxKernels]
[proc]
type = ProcessorIDAux
variable = proc
execute_on = 'initial'
[]
[]
[UserObjects]
[evaluable_uo0]
type = TwoRMTester
execute_on = 'initial'
element_side_neighbor_layers = 2
rank = 0
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
[Problem]
solve = false
kernel_coverage_check = false
[]
(modules/ray_tracing/test/tests/postprocessors/ray_data_value/ray_data_value_errors.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
[]
[]
[UserObjects]
active = ''
[lots]
type = LotsOfRaysRayStudy
vertex_to_vertex = false
centroid_to_centroid = false
centroid_to_vertex = false
ray_kernel_coverage_check = false
[]
[repeatable]
type = RepeatableRayStudy
start_points = '0 0 0'
directions = '1 0 0'
ray_data_names = data
names = ray
ray_kernel_coverage_check = false
[]
[no_banking_study]
type = DisableRayBankingStudy
start_points = '0 0 0'
directions = '1 0 0'
ray_data_names = data
names = ray
ray_kernel_coverage_check = false
[]
[]
[RayBCs]
active = ''
[kill]
type = KillRayBC
boundary = right
[]
[]
[Postprocessors]
active = ''
[no_registration]
type = RayDataValue
study = lots
ray_name = dummy
data_name = dummy
[]
[no_banking]
type = RayDataValue
study = no_banking_study
ray_name = ray
data_name = data
[]
[ray_name_not_found]
type = RayDataValue
study = repeatable
ray_name = dummy
data_name = data
execute_on = initial
[]
[data_name_not_found]
type = RayDataValue
study = repeatable
ray_name = ray
data_name = dummy
execute_on = initial
[]
[aux_data_name_not_found]
type = RayDataValue
study = repeatable
ray_name = ray
data_name = dummy
aux = true
execute_on = initial
[]
[id_not_found]
type = RayDataValue
study = repeatable
ray_id = 1
data_name = data
execute_on = final
[]
[neither_provided]
type = RayDataValue
study = repeatable
data_name = data
execute_on = initial
[]
[both_provided]
type = RayDataValue
study = repeatable
data_name = data
ray_id = 0
ray_name = dummy
execute_on = initial
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
(test/tests/preconditioners/pbp/pbp_test_options.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
# init_unif_refine = 6
[]
[Variables]
active = 'u v'
[./u]
order = FIRST
family = LAGRANGE
[../]
[./v]
order = FIRST
family = LAGRANGE
[../]
[]
[Preconditioning]
active = 'PBP'
[./PBP]
type = PBP
solve_order = 'u v'
preconditioner = 'LU LU'
off_diag_row = 'v'
off_diag_column = 'u'
petsc_options = '' # Test petsc options in PBP block
[../]
[]
[Kernels]
active = 'diff_u conv_v diff_v'
[./diff_u]
type = Diffusion
variable = u
[../]
[./conv_v]
type = CoupledForce
variable = v
v = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[BCs]
active = 'left_u right_u left_v'
[./left_u]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 100
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = 3
value = 0
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Steady
l_max_its = 1
nl_max_its = 1
solve_type = JFNK
[]
[Outputs]
file_base = out_dummy
exodus = true
[]
(test/tests/dirackernels/constant_point_source/1d_point_source_fv.i)
[Mesh]
[mesh]
type = GeneratedMeshGenerator
dim = 1
nx = 10
[]
[]
[Variables]
[u]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[]
[FVKernels]
[diff]
type = FVDiffusion
variable = u
coeff = coeff
[]
[]
[Materials]
[diff]
type = ADGenericFunctorMaterial
prop_names = 'coeff'
prop_values = '1'
[]
[]
[DiracKernels]
[point_source1]
type = ConstantPointSource
variable = u
value = 1.0
point = '0.15 0 0'
[]
[point_source2]
type = ConstantPointSource
variable = u
value = -0.5
point = '0.65 0 0'
[]
[]
[FVBCs]
[left]
type = FVDirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = FVDirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
file_base = 1d_fv_out
exodus = true
[]
(modules/richards/test/tests/gravity_head_2/gh01.i)
# unsaturated = true
# gravity = false
# supg = false
# transient = false
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
xmin = 0
xmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = 'pwater pgas'
[../]
[./DensityWater]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0E2
[../]
[./DensityGas]
type = RichardsDensityConstBulk
dens0 = 0.5
bulk_mod = 0.5E2
[../]
[./SeffWater]
type = RichardsSeff2waterVG
m = 0.8
al = 1
[../]
[./SeffGas]
type = RichardsSeff2gasVG
m = 0.8
al = 1
[../]
[./RelPermWater]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./RelPermGas]
type = RichardsRelPermPower
simm = 0.0
n = 3
[../]
[./SatWater]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.15
[../]
[./SatGas]
type = RichardsSat
s_res = 0.05
sum_s_res = 0.15
[../]
[./SUPGwater]
type = RichardsSUPGnone
[../]
[./SUPGgas]
type = RichardsSUPGnone
[../]
[]
[Variables]
[./pwater]
order = FIRST
family = LAGRANGE
[../]
[./pgas]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./water_ic]
type = RandomIC
min = 0.4
max = 0.6
variable = pwater
[../]
[./gas_ic]
type = RandomIC
min = 1.4
max = 1.6
variable = pgas
[../]
[]
[Kernels]
active = 'richardsfwater richardsfgas'
[./richardstwater]
type = RichardsMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFlux
variable = pwater
[../]
[./richardstgas]
type = RichardsMassChange
variable = pgas
[../]
[./richardsfgas]
type = RichardsFlux
variable = pgas
[../]
[]
[AuxVariables]
[./seffgas]
[../]
[./seffwater]
[../]
[]
[AuxKernels]
[./seffgas_kernel]
type = RichardsSeffAux
pressure_vars = 'pwater pgas'
seff_UO = SeffGas
variable = seffgas
[../]
[./seffwater_kernel]
type = RichardsSeffAux
pressure_vars = 'pwater pgas'
seff_UO = SeffWater
variable = seffwater
[../]
[]
[Postprocessors]
[./mwater_init]
type = RichardsMass
variable = pwater
execute_on = timestep_begin
outputs = none
[../]
[./mgas_init]
type = RichardsMass
variable = pgas
execute_on = timestep_begin
outputs = none
[../]
[./mwater_fin]
type = RichardsMass
variable = pwater
execute_on = timestep_end
outputs = none
[../]
[./mgas_fin]
type = RichardsMass
variable = pgas
execute_on = timestep_end
outputs = none
[../]
[./mass_error_water]
type = FunctionValuePostprocessor
function = fcn_mass_error_w
outputs = none # no reason why mass should be conserved
[../]
[./mass_error_gas]
type = FunctionValuePostprocessor
function = fcn_mass_error_g
outputs = none # no reason why mass should be conserved
[../]
[./pw_left]
type = PointValue
point = '0 0 0'
variable = pwater
outputs = none
[../]
[./pw_right]
type = PointValue
point = '1 0 0'
variable = pwater
outputs = none
[../]
[./error_water]
type = FunctionValuePostprocessor
function = fcn_error_water
[../]
[./pg_left]
type = PointValue
point = '0 0 0'
variable = pgas
outputs = none
[../]
[./pg_right]
type = PointValue
point = '1 0 0'
variable = pgas
outputs = none
[../]
[./error_gas]
type = FunctionValuePostprocessor
function = fcn_error_gas
[../]
[]
[Functions]
[./fcn_mass_error_w]
type = ParsedFunction
value = 'abs(0.5*(mi-mf)/(mi+mf))'
vars = 'mi mf'
vals = 'mwater_init mwater_fin'
[../]
[./fcn_mass_error_g]
type = ParsedFunction
value = 'abs(0.5*(mi-mf)/(mi+mf))'
vars = 'mi mf'
vals = 'mgas_init mgas_fin'
[../]
[./fcn_error_water]
type = ParsedFunction
value = 'abs((p0-p1)/p1)'
vars = 'b gdens0 p0 xval p1'
vals = '1E2 -1 pw_left 1 pw_right'
[../]
[./fcn_error_gas]
type = ParsedFunction
value = 'abs((p0-p1)/p1)'
vars = 'b gdens0 p0 xval p1'
vals = '0.5E2 -0.5 pg_left 1 pg_right'
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
density_UO = 'DensityWater DensityGas'
relperm_UO = 'RelPermWater RelPermGas'
SUPG_UO = 'SUPGwater SUPGgas'
sat_UO = 'SatWater SatGas'
seff_UO = 'SeffWater SeffGas'
viscosity = '1E-3 0.5E-3'
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -sub_pc_factor_shift_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'gmres asm lu NONZERO 1E-10 1E-10 10000'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = gh01
csv = true
[]
(modules/phase_field/test/tests/boundary_intersecting_features/boundary_intersecting_features.i)
[Mesh]
# ImageMesh ignores nx, xmin, xmax (and similarly for y and z) and
# tries to read them from the image file...
type = ImageMesh
dim = 2
# Be sure to choose a corresponding image name below!
# file = image001_cropped3_closing_298.png # full size, 157 Mb Exodus file!
# file = eighth_image001_cropped3_closing_298.png # 1/8
file = sixteenth_image001_cropped3_closing_298.png # 1/16
# Uncomment to maintain 1:1 ratio between number of pixels and mesh size.
# scale_to_one = false
# Uncomment to set cells_per_pixel to something other than the default value of 1.0.
# Must be <= 1.
# cells_per_pixel = .75
# To crop an image to e.g. 1/8th size, install ImageMagick and run:
# convert image001_cropped3_closing_298.png -crop 230x198+100+100 eighth_image001_cropped3_closing_298.png
# Note: Do not use 'sips' on OSX to crop! It actually interpolates
# the colors in the image instead of just cropping.
[]
[Variables]
[./u]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxVariables]
[./grain_auxvar]
order = CONSTANT
family = MONOMIAL
[../]
[./centroids]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./nodal_flood_aux]
variable = grain_auxvar
type = FeatureFloodCountAux
flood_counter = flood_count_pp
execute_on = 'initial timestep_end'
[../]
[./centroids]
type = FeatureFloodCountAux
variable = centroids
flood_counter = flood_count_pp
field_display = CENTROID
execute_on = 'initial timestep_end'
[../]
[]
[Functions]
[./tif]
# ImageFunction gets its file range parameters from ImageMesh,
# when it is present. This prevents duplicating information in
# input files.
type = ImageFunction
# In these sample images the features we want to analyze are RED (or close to pure red). The
# background is BLUE so we can easily distinguish between the two by selecting only the red channel.
component = 0
[../]
[]
[ICs]
[./u_ic]
type = FunctionIC
function = tif
variable = u
[../]
[]
[Postprocessors]
[./flood_count_pp]
type = FeatureFloodCount
variable = u
threshold = 1.0
compute_var_to_feature_map = true
execute_on = 'initial timestep_end'
[../]
[]
[VectorPostprocessors]
[./grain_volumes]
type = FeatureVolumeVectorPostprocessor
flood_counter = flood_count_pp
execute_on = 'initial timestep_end'
[../]
[]
[Problem]
type = FEProblem
solve = false
[../]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
csv = true
[]
(modules/stochastic_tools/examples/surrogates/sub.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 100
xmax = 1
elem_type = EDGE3
[]
[Variables]
[T]
order = SECOND
family = LAGRANGE
[]
[]
[Kernels]
[diffusion]
type = MatDiffusion
variable = T
diffusivity = k
[]
[source]
type = BodyForce
variable = T
value = 1.0
[]
[]
[Materials]
[conductivity]
type = GenericConstantMaterial
prop_names = k
prop_values = 2.0
[]
[]
[BCs]
[right]
type = DirichletBC
variable = T
boundary = right
value = 300
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Postprocessors]
[avg]
type = AverageNodalVariableValue
variable = T
[]
[max]
type = NodalExtremeValue
variable = T
value_type = max
[]
[]
[Outputs]
[]
(modules/tensor_mechanics/test/tests/isotropic_elasticity_tensor/youngs_modulus_poissons_ratio_test.i)
[Mesh]
type = GeneratedMesh
dim = 3
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./stress_11]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
add_variables = true
[../]
[]
[AuxKernels]
[./stress_11]
type = RankTwoAux
variable = stress_11
rank_two_tensor = stress
index_j = 1
index_i = 1
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0
[../]
[./left]
type = DirichletBC
variable = disp_x
boundary = left
value = 0
[../]
[./back]
type = DirichletBC
variable = disp_z
boundary = back
value = 0
[../]
[./top]
type = DirichletBC
variable = disp_y
boundary = top
value = 0.001
[../]
[]
[Materials]
[./stress]
type = ComputeLinearElasticStress
[../]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
poissons_ratio = 0.1
youngs_modulus = 1e6
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
l_max_its = 20
nl_max_its = 10
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(test/tests/functions/function_ic/function_ic_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = initial_cond_func
[../]
[../]
[]
[AuxVariables]
active = 'u_aux'
[./u_aux]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = initial_cond_func
[../]
[../]
[]
[Functions]
[./initial_cond_func]
type = ParsedFunction
value = x+2
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
nl_rel_tol = 1e-10
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/fvkernels/mms/advective-outflow/advection-outflow.i)
a=1.1
[GlobalParams]
advected_interp_method = 'average'
[]
[Mesh]
[./gen_mesh]
type = GeneratedMeshGenerator
dim = 1
xmin = 0
xmax = 1.1
nx = 2
[../]
[]
[Variables]
[./u]
family = MONOMIAL
order = CONSTANT
fv = true
two_term_boundary_expansion = false
type = MooseVariableFVReal
[../]
[./v]
family = MONOMIAL
order = CONSTANT
fv = true
two_term_boundary_expansion = true
type = MooseVariableFVReal
[../]
[]
[FVKernels]
[./advection_u]
type = FVAdvection
variable = u
velocity = '${a} 0 0'
[../]
[body_u]
type = FVBodyForce
variable = u
function = 'forcing'
[]
[./advection_v]
type = FVAdvection
variable = v
velocity = '${a} 0 0'
[../]
[body_v]
type = FVBodyForce
variable = v
function = 'forcing'
[]
[]
[FVBCs]
[left_u]
type = FVFunctionDirichletBC
boundary = 'left'
function = 'exact'
variable = u
[]
[right_u]
type = FVConstantScalarOutflowBC
variable = u
velocity = '${a} 0 0'
boundary = 'right'
[]
[left_v]
type = FVFunctionDirichletBC
boundary = 'left'
function = 'exact'
variable = v
[]
[right_v]
type = FVConstantScalarOutflowBC
variable = v
velocity = '${a} 0 0'
boundary = 'right'
[]
[]
[Functions]
[exact]
type = ParsedFunction
value = 'cos(x)'
[]
[forcing]
type = ParsedFunction
value = '-${a} * sin(x)'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[./L2u]
type = ElementL2Error
variable = u
function = exact
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2v]
type = ElementL2Error
variable = v
function = exact
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(modules/reactor/test/tests/meshgenerators/patterned_hex_peripheral_modifier/single_hex_pin_id.i)
[Mesh]
[hex]
type = PolygonConcentricCircleMeshGenerator
num_sides = 6
num_sectors_per_side = '2 2 2 2 2 2'
background_intervals = 1
ring_radii = 4.0
ring_intervals = 2
ring_block_ids = '10 15'
ring_block_names = 'center_tri center'
background_block_ids = 20
background_block_names = background
polygon_size = 5.0
preserve_volumes = on
[]
[pattern]
type = HexIDPatternedMeshGenerator
inputs = 'hex'
pattern = '0 0;
0 0 0;
0 0'
background_intervals = 2
hexagon_size = 17
assign_type = 'cell'
id_name = 'pin_id'
[]
[pmg]
type = PatternedHexPeripheralModifier
input = pattern
input_mesh_external_boundary = 10000
new_num_sector = 10
num_layers = 2
[]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[AuxVariables]
[pin_id]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[set_pin_id]
type = ExtraElementIDAux
variable = pin_id
extra_id_name = pin_id
[]
[]
[Outputs]
[exodus_1]
type = Exodus
enable = false
execute_on = TIMESTEP_END
[]
[exodus_2]
type = Exodus
enable = false
execute_on = TIMESTEP_END
[]
[]
(test/tests/outputs/output_dimension/output_dimension.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[./diff_z]
type = Diffusion
variable = disp_z
[../]
[./conv_x]
type = Convection
variable = disp_x
velocity = '2 0 0'
[../]
[./conv_y]
type = Convection
variable = disp_y
velocity = '2 0 0'
[../]
[./conv_z]
type = Convection
variable = disp_z
velocity = '2 0 0'
[../]
[]
[BCs]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = left
value = 0
[../]
[./right_x]
type = DirichletBC
variable = disp_x
boundary = right
value = 1
[../]
[./left_y]
type = DirichletBC
variable = disp_y
boundary = left
value = 0
[../]
[./right_y]
type = DirichletBC
variable = disp_y
boundary = right
value = 1
[../]
[./left_z]
type = DirichletBC
variable = disp_z
boundary = left
value = 0
[../]
[./right_z]
type = DirichletBC
variable = disp_z
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
[./out]
type = Exodus
output_dimension = 3
[../]
[]
(test/tests/misc/check_error/check_dynamic_name_block.i)
[Mesh]
file = three_block.e
# These names will be applied on the fly to the
# mesh so they can be used in the input file
# In addition they will show up in the input file
block_id = '1 2 3'
block_name = 'wood steel wood' # Can't have duplicate names
boundary_id = '1 2'
boundary_name = 'left right'
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[../]
[]
[Materials]
active = empty
[./empty]
type = MTMaterial
block = 'wood steel'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(modules/phase_field/test/tests/feature_volume_vpp_test/boundary_area_3D_single.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
nx = 6
ny = 25
nz = 15
xmin = 20
xmax = 30
ymin = 0
ymax = 50
zmin = 10
zmax = 40
elem_type = HEX8
[]
[./left_side]
input = gen
type = SubdomainBoundingBoxGenerator
block_id = 1
bottom_left = '0 0 0'
top_right = '24.9 50 50'
[../]
[./right_side]
input = left_side
type = SubdomainBoundingBoxGenerator
block_id = 2
bottom_left = '25.1 0 0'
top_right = '50 50 50'
[../]
[./iface_u]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 1
paired_block = 2
new_boundary = 10
input = right_side
[../]
[]
[Variables]
[./c]
order = FIRST
family = LAGRANGE
[]
[]
[ICs]
[./c]
type = SpecifiedSmoothCircleIC
variable = c
invalue = 1.0
outvalue = 0.0
radii = '4 5 10'
x_positions = '25 25 25'
y_positions = '40 25 0'
z_positions = '25 25 25'
int_width = 2.0
[]
[]
[Postprocessors]
[./flood_count]
type = FeatureFloodCount
variable = c
# Must be turned on to build data structures necessary for FeatureVolumeVPP
compute_var_to_feature_map = true
threshold = 0.5
execute_on = INITIAL
[../]
[]
[VectorPostprocessors]
[./features]
type = FeatureVolumeVectorPostprocessor
flood_counter = flood_count
# Turn on centroid output
output_centroids = true
execute_on = INITIAL
boundary = 10
single_feature_per_element = true
[../]
[]
[Kernels]
[diff]
type = Diffusion
variable = c
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
execute_on = INITIAL
[]
(modules/navier_stokes/test/tests/ics/test.i)
p_initial=1.01e5
T=273.15
[Mesh]
[cartesian]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 1
ymax = 2
nx = 4
ny = 4
[]
[]
[Modules]
[FluidProperties]
[fp]
type = IdealGasFluidProperties
[]
[]
[]
[Problem]
kernel_coverage_check = false
solve = false
skip_nl_system_check = true
[]
[AuxVariables]
[pressure]
type = MooseVariableFVReal
[]
[vel_x]
type = MooseVariableFVReal
[]
[vel_y]
type = MooseVariableFVReal
[]
[vel_z]
type = MooseVariableFVReal
[]
[temperature]
type = MooseVariableFVReal
[]
[ht]
type = MooseVariableFVReal
[]
[e]
type = MooseVariableFVReal
[]
[Mach]
type = MooseVariableFVReal
[]
[rho]
type = MooseVariableFVReal
[]
[rhou]
type = MooseVariableFVReal
[]
[rhov]
type = MooseVariableFVReal
[]
[rhow]
type = MooseVariableFVReal
[]
[rho_et]
type = MooseVariableFVReal
[]
[specific_volume]
type = MooseVariableFVReal
[]
[pressure_2]
[]
[vel_x_2]
[]
[vel_y_2]
[]
[vel_z_2]
[]
[temperature_2]
[]
[ht_2]
[]
[e_2]
[]
[Mach_2]
[]
[rho_2]
[]
[rhou_2]
[]
[rhov_2]
[]
[rhow_2]
[]
[rho_et_2]
[]
[specific_volume_2]
[]
[]
[GlobalParams]
fluid_properties = 'fp'
initial_pressure = ${p_initial}
initial_temperature = ${T}
initial_velocity = '1 0.2 18'
[]
[ICs]
[p]
type = NSInitialCondition
variable = 'pressure'
[]
[vel_x]
type = NSInitialCondition
variable = 'vel_x'
[]
[vel_y]
type = NSInitialCondition
variable = 'vel_y'
[]
[vel_z]
type = NSInitialCondition
variable = 'vel_z'
[]
[temperature]
type = NSInitialCondition
variable = 'temperature'
[]
[ht]
type = NSInitialCondition
variable = 'ht'
[]
[e]
type = NSInitialCondition
variable = 'e'
[]
[Mach]
type = NSInitialCondition
variable = 'Mach'
[]
[rho]
type = NSInitialCondition
fluid_properties = 'fp'
initial_pressure = ${p_initial}
initial_temperature = ${T}
initial_velocity = '1 0.2 18'
variable = 'rho'
[]
[rhou]
type = NSInitialCondition
variable = 'rhou'
[]
[rhov]
type = NSInitialCondition
variable = 'rhov'
[]
[rhow]
type = NSInitialCondition
variable = 'rhow'
[]
[rho_et]
type = NSInitialCondition
variable = 'rho_et'
[]
[specific_volume]
type = NSInitialCondition
variable = 'specific_volume'
[]
[p_2]
type = NSInitialCondition
variable = 'pressure_2'
variable_type = 'pressure'
[]
[vel_x_2]
type = NSInitialCondition
variable = 'vel_x_2'
variable_type = 'vel_x'
[]
[vel_y_2]
type = NSInitialCondition
variable = 'vel_y_2'
variable_type = 'vel_y'
[]
[vel_z_2]
type = NSInitialCondition
variable = 'vel_z_2'
variable_type = 'vel_z'
[]
[temperature_2]
type = NSInitialCondition
variable = 'temperature_2'
variable_type = 'temperature'
[]
[ht_2]
type = NSInitialCondition
variable = 'ht_2'
variable_type = 'ht'
[]
[e_2]
type = NSInitialCondition
variable = 'e_2'
variable_type = 'e'
[]
[Mach_2]
type = NSInitialCondition
variable = 'Mach_2'
variable_type = 'Mach'
[]
[rho_2]
type = NSInitialCondition
variable = 'rho_2'
variable_type = 'rho'
[]
[rhou_2]
type = NSInitialCondition
variable = 'rhou_2'
variable_type = 'rhou'
[]
[rhov_2]
type = NSInitialCondition
variable = 'rhov_2'
variable_type = 'rhov'
[]
[rhow_2]
type = NSInitialCondition
variable = 'rhow_2'
variable_type = 'rhow'
[]
[rho_et_2]
type = NSInitialCondition
variable = 'rho_et_2'
variable_type = 'rho_et'
[]
[specific_volume_2]
type = NSInitialCondition
variable = 'specific_volume_2'
variable_type = 'specific_volume'
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/ray_tracing/test/tests/raykernels/material_integral_ray_kernel/material_integral_ray_kernel.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 5
ny = 5
xmax = 5
ymax = 5
[]
[modify_subdomain]
type = ParsedSubdomainMeshGenerator
input = gmg
block_id = 1
combinatorial_geometry = 'x > 2'
[]
[]
[Materials]
[generic_mat_block0]
type = GenericFunctionMaterial
block = 0
prop_names = 'mat'
prop_values = 'parsed_block0'
[]
[generic_mat_block1]
type = GenericFunctionMaterial
block = 1
prop_names = 'mat'
prop_values = 'parsed_block1'
[]
[]
[Functions]
[parsed_block0]
type = ParsedFunction
value = 'x + 2 * y'
[]
[parsed_block1] # continuous at the interface
type = ParsedFunction
value = '2 * x + 2 * y - 2'
[]
[]
[UserObjects]
[study]
type = RepeatableRayStudy
names = 'diag
top_across
bottom_across
partial'
start_points = '0 0 0
0 5 0
0 0 0
0.5 0.5 0'
end_points = '5 5 0
5 5 0
5 0 0
4.5 0.5 0'
[]
[]
[RayKernels]
[material_integral]
type = MaterialIntegralRayKernel
study = study
mat_prop = mat
[]
[]
[Postprocessors]
[diag_value]
type = RayIntegralValue
ray_kernel = material_integral
ray = diag
[]
[top_across_value]
type = RayIntegralValue
ray_kernel = material_integral
ray = top_across
[]
[bottom_across_value]
type = RayIntegralValue
ray_kernel = material_integral
ray = bottom_across
[]
[partial_value]
type = RayIntegralValue
ray_kernel = material_integral
ray = partial
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = false
csv = true
[]
(test/tests/userobjects/solution_user_object/discontinuous_value_solution_uo_p2.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./one]
type = DirichletBC
variable = u
boundary = 'right top bottom'
value = 1
[../]
[]
[UserObjects]
[./soln]
type = SolutionUserObject
mesh = discontinuous_value_solution_uo_p1.e
system_variables = 'discontinuous_variable continuous_variable'
[../]
[]
[Postprocessors]
[./discontinuous_value_left]
type = TestDiscontinuousValuePP
variable = discontinuous_variable
point = '0.25 0.25 0.0'
solution = soln
[../]
[./discontinuous_value_face]
type = TestDiscontinuousValuePP
variable = discontinuous_variable
point = '0.5 0.25 0.0'
solution = soln
[../]
[./discontinuous_value_right]
type = TestDiscontinuousValuePP
variable = discontinuous_variable
point = '0.75 0.25 0.0'
solution = soln
[../]
[./continuous_gradient_left]
type = TestDiscontinuousValuePP
variable = continuous_variable
evaluate_gradient = true
gradient_component = x
point = '0.25 0.25 0.0'
solution = soln
[../]
[./continuous_gradient_value_face]
type = TestDiscontinuousValuePP
variable = continuous_variable
evaluate_gradient = true
gradient_component = x
point = '0.5 0.25 0.0'
solution = soln
[../]
[./continuous_gradient_right]
type = TestDiscontinuousValuePP
variable = continuous_variable
evaluate_gradient = true
gradient_component = x
point = '0.75 0.25 0.0'
solution = soln
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
file_base = discontinuous_value_solution_uo_p2
exodus = false
csv = true
[]
(test/tests/auxkernels/normalization_aux/normalization_aux.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
initial_condition = 1.0
[../]
[]
[AuxVariables]
[./u_normalized]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./normalization_auxkernel]
type = NormalizationAux
variable = u_normalized
source_variable = u
normal_factor = 2.0
execute_on = timestep_end
# Note: 'normalization' or 'shift' are provided as CLI args
[../]
[]
[BCs]
[./left_u]
type = DirichletBC
variable = u
boundary = left
value = 1
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 2
[../]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[./unorm]
type = ElementIntegralVariablePostprocessor
variable = u
execute_on = 'initial timestep_end'
[../]
[./u_normalized_norm]
type = ElementIntegralVariablePostprocessor
variable = u_normalized
execute_on = 'initial timestep_end'
[../]
[./u0]
type = PointValue
variable = u
point = '0 0 0'
execute_on = 'initial timestep_end'
[../]
[]
[Outputs]
exodus = true
[]
(test/tests/mesh_modifiers/add_side_sets/cylinder_points.i)
[Mesh]
[file]
type = FileMeshGenerator
file = cylinder.e
[]
# Mesh Modifiers
[add_side_sets]
type = SideSetsFromPointsGenerator
input = file
points = '0 0 0.5
0.1 0 0
0 0 -0.5'
new_boundary = 'top side bottom'
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[bottom]
type = DirichletBC
variable = u
boundary = bottom
value = 0
[]
[top]
type = DirichletBC
variable = u
boundary = top
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/materials/piecewise_by_block_material/test.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 10
xmax = 2
[]
[subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '1.0 0 0'
block_id = 1
top_right = '2.0 1.0 0'
[]
[middle]
input = subdomain1
type = SideSetsBetweenSubdomainsGenerator
new_boundary = middle
paired_block = 1
primary_block = 0
[]
[]
[Variables]
[dummy]
type = MooseVariableFVReal
[]
[]
# This is added to have sufficient ghosting layers, see #19534
[FVKernels]
[diff]
type = FVDiffusion
variable = 'dummy'
coeff = 1
[]
[]
[AuxVariables]
[u]
type = MooseVariableFVReal
[]
[v]
type = MooseVariableFVReal
[InitialCondition]
type = FunctionIC
function = '4 * (x - 7) * (x - 8)'
[]
[]
[]
[AuxKernels]
# to trigger off-boundary element computations
[to_var]
type = ADMaterialRealAux
variable = 'u'
property = coeff
[]
[]
[Materials]
[coeff_mat]
type = ADPiecewiseConstantByBlockMaterial
prop_name = 'coeff'
subdomain_to_prop_value = '0 4
1 2'
[]
[]
[Postprocessors]
# to trigger on boundary element computations
[flux]
type = ADSideDiffusiveFluxIntegral
boundary = left
variable = v
diffusivity = 'coeff'
[]
# to trigger ghost evaluations
[flux_mid]
type = ADInterfaceDiffusiveFluxIntegral
boundary = middle
variable = v
diffusivity = 'coeff'
[]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Outputs]
exodus = true
# To get level of ghosting
[console]
type = Console
system_info = 'framework mesh aux nonlinear execution relationship'
[]
[]
(modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/rz_cone_by_parts_steady_nobcbc.i)
# This input file tests several different things:
# .) The axisymmetric (RZ) form of the governing equations.
# .) An open boundary.
# .) Not integrating the pressure by parts, thereby requiring a pressure pin.
# .) Natural boundary condition at the outlet.
[GlobalParams]
integrate_p_by_parts = true
laplace = true
gravity = '0 0 0'
[]
[Mesh]
file = '2d_cone.msh'
[]
[Problem]
coord_type = RZ
[]
[Preconditioning]
[./SMP_PJFNK]
type = SMP
full = true
solve_type = Newton
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = 'bjacobi ilu 4'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
csv = true
console = true
[./out]
type = Exodus
[../]
[]
[Variables]
[./vel_x]
# Velocity in radial (r) direction
family = LAGRANGE
order = SECOND
[../]
[./vel_y]
# Velocity in axial (z) direction
family = LAGRANGE
order = SECOND
[../]
[./p]
family = LAGRANGE
order = FIRST
[../]
[]
[BCs]
[./u_in]
type = DirichletBC
boundary = bottom
variable = vel_x
value = 0
[../]
[./v_in]
type = FunctionDirichletBC
boundary = bottom
variable = vel_y
function = 'inlet_func'
[../]
[./u_axis_and_walls]
type = DirichletBC
boundary = 'left right'
variable = vel_x
value = 0
[../]
[./v_no_slip]
type = DirichletBC
boundary = 'right'
variable = vel_y
value = 0
[../]
[./u_out]
type = INSMomentumNoBCBCLaplaceForm
boundary = top
variable = vel_x
u = vel_x
v = vel_y
pressure = p
component = 0
[../]
[./v_out]
type = INSMomentumNoBCBCLaplaceForm
boundary = top
variable = vel_y
u = vel_x
v = vel_y
pressure = p
component = 1
[../]
# When the NoBCBC is applied on the outlet boundary then there is nothing
# constraining the pressure. Thus we must pin the pressure somewhere to ensure
# that the problem is not singular. If the below BC is not applied then
# -pc_type svd -pc_svd_monitor reveals a singular value
[p_corner]
type = DirichletBC
boundary = top_right
value = 0
variable = p
[]
[]
[Kernels]
[./mass]
type = INSMassRZ
variable = p
u = vel_x
v = vel_y
pressure = p
[../]
[./x_momentum_space]
type = INSMomentumLaplaceFormRZ
variable = vel_x
u = vel_x
v = vel_y
pressure = p
component = 0
[../]
[./y_momentum_space]
type = INSMomentumLaplaceFormRZ
variable = vel_y
u = vel_x
v = vel_y
pressure = p
component = 1
[../]
[]
[Materials]
[./const]
type = GenericConstantMaterial
block = 'volume'
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[]
[Functions]
[./inlet_func]
type = ParsedFunction
value = '-4 * x^2 + 1'
[../]
[]
[Postprocessors]
[./flow_in]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'bottom'
execute_on = 'timestep_end'
[../]
[./flow_out]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'top'
execute_on = 'timestep_end'
[../]
[]
(tutorials/darcy_thermo_mech/step03_darcy_material/problems/step3b.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 100
ny = 10
xmax = 0.304 # Length of test chamber
ymax = 0.0257 # Test chamber radius
[]
[Variables/pressure]
[]
[Kernels]
[darcy_pressure]
type = DarcyPressure
variable = pressure
[]
[]
[BCs]
[inlet]
type = DirichletBC
variable = pressure
boundary = left
value = 4000 # (Pa) From Figure 2 from paper. First data point for 1mm spheres.
[]
[outlet]
type = DirichletBC
variable = pressure
boundary = right
value = 0 # (Pa) Gives the correct pressure drop from Figure 2 for 1mm spheres
[]
[]
[Materials]
[column]
type = PackedColumn
radius = '1 + 2/3.04*x'
outputs = exodus
[]
[]
[Problem]
type = FEProblem
coord_type = RZ
rz_coord_axis = X
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/functions/image_function/image_2d_elemental.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
[]
[Variables]
[u]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[image_func]
type = ImageFunction
file_base = stack/test
file_suffix = png
# file range is parsed as a vector of unsigned. If it only has 1
# entry, only a single file is read.
file_range = '0'
[]
[]
[ICs]
[u_ic]
type = FunctionIC
function = image_func
variable = u
[]
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(examples/ex11_prec/smp.i)
[Mesh]
file = square.e
[]
[Variables]
[./diffused]
order = FIRST
family = LAGRANGE
[../]
[./forced]
order = FIRST
family = LAGRANGE
[../]
[]
# The Preconditioning block
[Preconditioning]
active = 'SMP_jfnk'
[./SMP_jfnk]
type = SMP
off_diag_row = 'forced'
off_diag_column = 'diffused'
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
[../]
[./SMP_jfnk_full]
type = SMP
full = true
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
[../]
[./SMP_n]
type = SMP
off_diag_row = 'forced'
off_diag_column = 'diffused'
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
[../]
[]
[Kernels]
[./diff_diffused]
type = Diffusion
variable = diffused
[../]
[./conv_forced]
type = CoupledForce
variable = forced
v = diffused
[../]
[./diff_forced]
type = Diffusion
variable = forced
[../]
[]
[BCs]
#Note we have active on and neglect the right_forced BC
active = 'left_diffused right_diffused left_forced'
[./left_diffused]
type = DirichletBC
variable = diffused
boundary = 1
value = 0
[../]
[./right_diffused]
type = DirichletBC
variable = diffused
boundary = 2
value = 100
[../]
[./left_forced]
type = DirichletBC
variable = forced
boundary = 1
value = 0
[../]
[./right_forced]
type = DirichletBC
variable = forced
boundary = 2
value = 0
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/userobjects/internal_side_user_object/internal_side_user_object.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
ymin = -1
xmax = 1
ymax = 1
nx = 2
ny = 2
elem_type = QUAD4
[]
[Functions]
[./fn_exact]
type = ParsedFunction
value = 'x*x+y*y'
[../]
[./ffn]
type = ParsedFunction
value = -4
[../]
[]
[UserObjects]
[./isuo]
type = InsideUserObject
variable = u
[../]
[]
[Variables]
[./u]
family = LAGRANGE
order = FIRST
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = ffn
[../]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
boundary = '0 1 2 3'
function = fn_exact
[../]
[]
[Postprocessors]
[./value]
type = InsideValuePPS
user_object = isuo
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/meshgenerators/combiner_generator/combiner_generator.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[cmbn]
type = CombinerGenerator
inputs = 'gen'
positions = '1 0 0 2 2 2 3 0 0'
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/userobjects/coupling_to_kernel/user_object_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 5
ny = 5
elem_type = QUAD4
[]
[UserObjects]
[./ud]
type = MTUserObject
scalar = 2
vector = '9 7 5'
[../]
[]
[Functions]
[./forcing_fn]
type = ParsedFunction
value = -2
[../]
[./exact_fn]
type = ParsedFunction
value = x*x
[../]
[]
[Variables]
[./u]
family = LAGRANGE
order = FIRST
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
# this kernel will user user data object from above
[./ffn]
type = UserObjectKernel
variable = u
user_object = ud
[]
[]
[BCs]
active = 'all'
[./all]
type = FunctionDirichletBC
variable = u
function = exact_fn
boundary = '0 1 2 3'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
file_base = out
exodus = true
[]
(test/tests/postprocessors/vector_postprocessor_comparison/vector_postprocessor_comparison.i)
# This tests the VectorPostprocessorComparison post-processor, which takes two
# vector post-processors and compares them.
[Mesh]
type = GeneratedMesh
dim = 1
nx = 3
xmin = 0
xmax = 2
[]
[Functions]
# Sampled values will be [2, 2, 2]
[./a_fn]
type = ConstantFunction
value = 2
[../]
# Sampled values will be [0, 1, 2]
[./b_fn]
type = ParsedFunction
value = 'x'
[../]
[]
[VectorPostprocessors]
[./a_vpp]
type = LineFunctionSampler
functions = 'a_fn'
num_points = 3
start_point = '0 0 0'
end_point = '2 0 0'
sort_by = x
execute_on = 'initial'
[../]
[./b_vpp]
type = LineFunctionSampler
functions = 'b_fn'
num_points = 3
start_point = '0 0 0'
end_point = '2 0 0'
sort_by = x
execute_on = 'initial'
[../]
[]
[Postprocessors]
[./vpp_comparison]
type = VectorPostprocessorComparison
vectorpostprocessor_a = a_vpp
vectorpostprocessor_b = b_vpp
vector_name_a = a_fn
vector_name_b = b_fn
comparison_type = greater_than_equals
execute_on = 'initial'
[../]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
file_base = greater_than_equals
csv = true
show = 'vpp_comparison'
execute_on = 'initial'
[]
(modules/heat_conduction/test/tests/gray_lambert_radiator/coupled_heat_conduction.i)
[Problem]
kernel_coverage_check = false
[]
[Mesh]
type = MeshGeneratorMesh
[./cartesian]
type = CartesianMeshGenerator
dim = 2
dx = '1 1 1'
ix = '2 2 2'
dy = '5'
iy = '10'
subdomain_id = '1 2 3'
[../]
[./break_sides]
type = BreakBoundaryOnSubdomainGenerator
boundaries = 'bottom top'
input = cartesian
[../]
[./left_interior]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 1
paired_block = 2
new_boundary = left_interior
input = break_sides
[../]
[./right_interior]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 3
paired_block = 2
new_boundary = right_interior
input = left_interior
[../]
[./rename]
type = RenameBlockGenerator
input = right_interior
old_block = '1 2 3'
new_block = '1 4 3'
[../]
[]
[Variables]
[./temperature]
initial_condition = 300
block = '1 3'
[../]
[]
[Kernels]
[./heat_conduction]
type = HeatConduction
variable = temperature
diffusion_coefficient = 1
block = '1 3'
[../]
[]
[UserObjects]
[./cavity_radiation]
type = ConstantViewFactorSurfaceRadiation
boundary = 'left_interior right_interior bottom_to_2 top_to_2'
temperature = temperature
emissivity = '0.8 0.8 0.8 0.8'
adiabatic_boundary = 'bottom_to_2 top_to_2'
# these view factors are made up to exactly balance energy
# transfer through the cavity
view_factors = '0 0.8 0.1 0.1;
0.8 0 0.1 0.1;
0.45 0.45 0 0.1;
0.45 0.45 0.1 0'
execute_on = 'INITIAL LINEAR TIMESTEP_END'
[../]
[]
[BCs]
[./bottom_left]
type = DirichletBC
preset = false
variable = temperature
boundary = bottom_to_1
value = 1500
[../]
[./top_right]
type = DirichletBC
preset = false
variable = temperature
boundary = top_to_3
value = 300
[../]
[./radiation]
type = GrayLambertNeumannBC
variable = temperature
reconstruct_emission = false
surface_radiation_object_name = cavity_radiation
boundary = 'left_interior right_interior'
[../]
[]
[Postprocessors]
[./qdot_left]
type = GrayLambertSurfaceRadiationPP
boundary = left_interior
surface_radiation_object_name = cavity_radiation
return_type = HEAT_FLUX_DENSITY
[../]
[./qdot_right]
type = GrayLambertSurfaceRadiationPP
boundary = right_interior
surface_radiation_object_name = cavity_radiation
return_type = HEAT_FLUX_DENSITY
[../]
[./qdot_top]
type = GrayLambertSurfaceRadiationPP
boundary = top_to_2
surface_radiation_object_name = cavity_radiation
return_type = HEAT_FLUX_DENSITY
[../]
[./qdot_bottom]
type = GrayLambertSurfaceRadiationPP
boundary = bottom_to_2
surface_radiation_object_name = cavity_radiation
return_type = HEAT_FLUX_DENSITY
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/reactor/test/tests/meshgenerators/reporting_id/hexagonal_id/assembly_reporting_id.i)
[Mesh]
[pin1]
type = PolygonConcentricCircleMeshGenerator
preserve_volumes = true
ring_radii = 0.4
ring_intervals = 1
background_intervals = 1
num_sides = 6
num_sectors_per_side = '2 2 2 2 2 2'
polygon_size = 0.5
[]
[pin2]
type = PolygonConcentricCircleMeshGenerator
preserve_volumes = true
ring_radii = 0.4
ring_intervals = 1
background_intervals = 1
num_sides = 6
num_sectors_per_side = '2 2 2 2 2 2'
polygon_size = 0.5
[]
[assembly]
type = HexIDPatternedMeshGenerator
inputs = 'pin1 pin2'
pattern_boundary = hexagon
pattern = ' 1 0 1;
0 0 0 0;
1 0 1 0 1;
0 0 0 0;
1 0 1'
hexagon_size = 2.6
duct_sizes = '2.4 2.5'
duct_intervals = '1 1'
assign_type = 'cell'
id_name = 'pin_id'
[]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[AuxVariables]
[pin_id]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[set_pin_id]
type = ExtraElementIDAux
variable = pin_id
extra_id_name = pin_id
[]
[]
[Outputs]
exodus = true
execute_on = timestep_end
[]
(test/tests/mesh_modifiers/image_subdomain/image_3d.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
nx = 20
ny = 20
nz = 20
[]
[image]
type = ImageSubdomainGenerator
input = gen
file_base = stack/test
file_suffix = png
threshold = 2.7e4
[]
[]
[Variables]
[u]
[]
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(test/tests/postprocessors/axisymmetric_centerline_average_value/axisymmetric_centerline_average_value_test.i)
[Problem]
coord_type = RZ
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmin = 0
xmax = 2
ymin = 0
ymax = 1
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'top bottom'
[./top]
type = DirichletBC
variable = u
boundary = top
value = 0
[../]
[./bottom]
type = DirichletBC
variable = u
boundary = bottom
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Postprocessors]
[./average]
type = AxisymmetricCenterlineAverageValue
boundary = left
variable = u
[../]
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/combined/test/tests/linear_elasticity/linear_elastic_material.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
nz = 0
xmin = 0
xmax = 50
ymin = 0
ymax = 50
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Variables]
[./diffused]
[./InitialCondition]
type = RandomIC
[../]
[../]
[]
[Modules/TensorMechanics/Master/All]
strain = SMALL
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx'
[]
[Kernels]
[./diff]
type = Diffusion
variable = diffused
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeElasticityTensor
fill_method = symmetric9
#reading C_11 C_12 C_13 C_22 C_23 C_33 C_44 C_55 C_66
C_ijkl ='1.0e6 0.0 0.0 1.0e6 0.0 1.0e6 0.5e6 0.5e6 0.5e6'
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = diffused
boundary = '1'
value = 1
[../]
[./top]
type = DirichletBC
variable = diffused
boundary = '2'
value = 0
[../]
[./disp_x_BC]
type = DirichletBC
variable = disp_x
boundary = '0 2'
value = 0.5
[../]
[./disp_x_BC2]
type = DirichletBC
variable = disp_x
boundary = '1 3'
value = 0.01
[../]
[./disp_y_BC]
type = DirichletBC
variable = disp_y
boundary = '0 2'
value = 0.8
[../]
[./disp_y_BC2]
type = DirichletBC
variable = disp_y
boundary = '1 3'
value = 0.02
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(test/tests/meshgenerators/sidesets_from_normals_generator/sidesets_cylinder_normals_fixed.i)
[Mesh]
[./fmg]
type = FileMeshGenerator
file = cylinder.e
#parallel_type = replicated
[]
[./sidesets]
type = SideSetsFromNormalsGenerator
input = fmg
normals = '0 1 0
0 -1 0'
fixed_normal = true
new_boundary = 'front back'
variance = 0.5
[]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./front]
type = DirichletBC
variable = u
boundary = front
value = 0
[../]
[./back]
type = DirichletBC
variable = u
boundary = back
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/mortar/aux-gap/mismatch.i)
[Mesh]
second_order = true
[file]
type = FileMeshGenerator
file = nodal_normals_test_offset_nonmatching_gap.e
[]
[primary]
input = file
type = LowerDBlockFromSidesetGenerator
sidesets = '2'
new_block_id = '20'
[]
[secondary]
input = primary
type = LowerDBlockFromSidesetGenerator
sidesets = '1'
new_block_id = '10'
[]
[]
[Variables]
[T]
block = '1 2'
order = SECOND
[]
[lambda]
block = '10'
use_dual = true
order = SECOND
[]
[]
[AuxVariables]
[gap]
block = '10'
[]
[]
[AuxKernels]
[gap]
type = WeightedGapAux
variable = gap
primary_boundary = 2
secondary_boundary = 1
primary_subdomain = 20
secondary_subdomain = 10
[]
[]
[BCs]
[neumann]
type = FunctionGradientNeumannBC
exact_solution = exact_soln
variable = T
boundary = '3 4 5 6 7 8'
[]
[]
[Kernels]
[conduction]
type = Diffusion
variable = T
block = '1 2'
[]
[sink]
type = Reaction
variable = T
block = '1 2'
[]
[forcing_function]
type = BodyForce
variable = T
function = forcing_function
block = '1 2'
[]
[]
[Functions]
[forcing_function]
type = ParsedFunction
value = '-4 + x^2 + y^2'
[]
[exact_soln]
type = ParsedFunction
value = 'x^2 + y^2'
[]
[]
[Debug]
show_var_residual_norms = 1
[]
[Constraints]
[mortar]
type = EqualValueConstraint
primary_boundary = 2
secondary_boundary = 1
primary_subdomain = 20
secondary_subdomain = 10
variable = lambda
secondary_variable = T
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
solve_type = NEWTON
type = Steady
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_shift_type -pc_factor_shift_amount'
petsc_options_value = 'lu basic NONZERO 1e-15'
[]
[Outputs]
exodus = true
[dofmap]
type = DOFMap
execute_on = 'initial'
[]
[]
(test/tests/mesh_modifiers/image_subdomain/image_2d.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 176
ny = 287
[]
[image]
type = ImageSubdomainGenerator
input = gen
file = kitten.png #../../functions/image_function/stack/test
threshold = 100
[]
[]
[Variables]
[u]
[]
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/jacobian_test/jacobian_stabilized_test.i)
# This input file tests the jacobians of many of the INS kernels
[GlobalParams]
gravity = '1.1 1.1 1.1'
u = vel_x
v = vel_y
w = vel_z
pressure = p
integrate_p_by_parts = true
laplace = true
pspg = true
supg = true
alpha = 1.1
[]
[Mesh]
type = GeneratedMesh
dim = 3
xmin = 0
xmax = 3.0
ymin = 0
ymax = 1.5
zmax = 1.1
nx = 1
ny = 1
nz = 1
elem_type = HEX27
[]
[Variables]
[./vel_x]
order = SECOND
family = LAGRANGE
[../]
[./vel_y]
order = SECOND
family = LAGRANGE
[../]
[./vel_z]
order = SECOND
family = LAGRANGE
[../]
[./p]
order = SECOND
family = LAGRANGE
[../]
[]
[Kernels]
[./mass]
type = INSMass
variable = p
[../]
[./x_momentum_space]
type = INSMomentumLaplaceForm
variable = vel_x
component = 0
[../]
[./y_momentum_space]
type = INSMomentumLaplaceForm
variable = vel_y
component = 1
[../]
[./z_momentum_space]
type = INSMomentumLaplaceForm
variable = vel_z
component = 2
[../]
[]
[Materials]
[./const]
type = GenericConstantMaterial
block = 0
prop_names = 'rho mu'
prop_values = '0.5 1.5'
[../]
[]
[Preconditioning]
[./SMP_PJFNK]
type = SMP
full = true
[../]
[]
[Executioner]
solve_type = NEWTON
type = Steady
petsc_options_iname = '-snes_type'
petsc_options_value = 'test'
[]
[ICs]
[./p]
type = RandomIC
variable = p
min = 0.5
max = 1.5
[../]
[./vel_x]
type = RandomIC
variable = vel_x
min = 0.5
max = 1.5
[../]
[./vel_y]
type = RandomIC
variable = vel_y
min = 0.5
max = 1.5
[../]
[./vel_z]
type = RandomIC
variable = vel_z
min = 0.5
max = 1.5
[../]
[]
(test/tests/outputs/output_interface/indicator.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Adaptivity]
[./Indicators]
[./indicator_0]
type = GradientJumpIndicator
variable = u
outputs = indicators
[../]
[./indicator_1]
type = GradientJumpIndicator
variable = u
outputs = indicators
[../]
[../]
[]
[Outputs]
[./indicators]
type = Exodus
[../]
[./no_indicators]
type = Exodus
[../]
[]
(test/tests/ics/boundary_ic/boundary_ic.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 4
ny = 4
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./u_ic]
type = ConstantIC
variable = u
block = 0
value = -1
[../]
[./u_ic_bnd]
type = ConstantIC
variable = u
boundary = 'left right'
value = -2
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(modules/phase_field/test/tests/free_energy_material/RegularSolutionFreeEnergy_plog.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 50
xmax = 1
[]
[Variables]
[./c]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = x
[../]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = c
[../]
[]
[BCs]
[./left]
type = FunctionDirichletBC
variable = c
boundary = left
function = x
[../]
[./right]
type = FunctionDirichletBC
variable = c
boundary = right
function = x
[../]
[]
[Materials]
[./free_energy]
type = RegularSolutionFreeEnergy
f_name = F
c = c
outputs = out
log_tol = 0.2
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
l_max_its = 1
nl_max_its = 1
nl_abs_tol = 1
[]
[Outputs]
execute_on = 'timestep_end'
[./out]
type = Exodus
execute_on = timestep_end
[../]
[]
(modules/thermal_hydraulics/test/tests/auxkernels/weighted_average/weighted_average.i)
# Tests the weighted average aux, which computes a weighted average of an
# arbitrary number of aux variables, using other aux variables as the weights.
# For this example, the values being averaged are
# value1 = 4
# value2 = 9
# and the weights are
# weight1 = 2
# weight2 = 3
# The result should then be
# weighted_average = (weight1 * value1 + weight2 * value2) / (weight1 + weight2)
# = (2 * 4 + 3 * 9) / (2 + 3)
# = 35 / 5
# = 7
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
allow_renumbering = false
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[AuxVariables]
[weighted_average]
family = MONOMIAL
order = CONSTANT
[]
[value1]
family = MONOMIAL
order = CONSTANT
[]
[value2]
family = MONOMIAL
order = CONSTANT
[]
[weight1]
family = MONOMIAL
order = CONSTANT
[]
[weight2]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[weighted_average_auxkernel]
type = WeightedAverageAux
variable = weighted_average
values = 'value1 value2'
weights = 'weight1 weight2'
[]
[value1_kernel]
type = ConstantAux
variable = value1
value = 4
[]
[value2_kernel]
type = ConstantAux
variable = value2
value = 9
[]
[weight1_kernel]
type = ConstantAux
variable = weight1
value = 2
[]
[weight2_kernel]
type = ConstantAux
variable = weight2
value = 3
[]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[weighted_average_pp]
type = ElementalVariableValue
elementid = 0
variable = weighted_average
[]
[]
[Outputs]
csv = true
execute_on = timestep_end
[]
(test/tests/transfers/multiapp_copy_transfer/tagged_solution/main.i)
[Problem]
solve = false
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 4
[]
[MultiApps/sub]
type = FullSolveMultiApp
input_files = sub.i
[]
[Transfers/to_sub]
type = MultiAppCopyTransfer
to_multi_app = sub
source_variable = x
to_solution_tag = tagged_aux_sol
variable = force
[]
[AuxVariables/x]
initial_condition = 1
[]
[Executioner]
type = Steady
[]
(modules/heat_conduction/test/tests/code_verification/spherical_test_no1.i)
# Problem III.1
#
# A spherical shell has a constant thermal conductivity k and internal
# heat generation q. It has inner radius ri and outer radius ro.
# Both surfaces are exposed to constant temperatures: u(ri) = ui and u(ro) = uo.
#
# REFERENCE:
# A. Toptan, et al. (Mar.2020). Tech. rep. CASL-U-2020-1939-000, SAND2020-3887 R. DOI:10.2172/1614683.
[Mesh]
[./geom]
type = GeneratedMeshGenerator
dim = 1
elem_type = EDGE2
xmin = 0.2
nx = 4
[../]
[]
[Variables]
[./u]
order = FIRST
[../]
[]
[Problem]
coord_type = RSPHERICAL
[]
[Functions]
[./exact]
type = ParsedFunction
vars = 'ri ro ui uo'
vals = '0.2 1.0 300 0'
value = '( uo * (1/ri-1/x) - ui * (1/ro-1/x)) / (1/ri-1/ro)'
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = u
[../]
[]
[BCs]
[./ui]
type = DirichletBC
boundary = left
variable = u
value = 300
[../]
[./uo]
type = DirichletBC
boundary = right
variable = u
value = 0
[../]
[]
[Materials]
[./property]
type = GenericConstantMaterial
prop_names = 'density specific_heat thermal_conductivity'
prop_values = '1.0 1.0 5.0'
[../]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[./error]
type = ElementL2Error
function = exact
variable = u
[../]
[./h]
type = AverageElementSize
[]
[]
[Outputs]
csv = true
[]
(python/peacock/tests/common/simple_diffusion.i)
[Mesh]
[generate]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
# Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/multiapps/initial_transfer/master.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
[]
[Problem]
kernel_coverage_check = false
[]
[Variables][dummy][][]
[Functions]
[func]
type = ConstantFunction
value = 1
[]
[]
[Postprocessors]
[c]
type = FunctionValuePostprocessor
function = func
execute_on = initial
# this will force this postprocessor to be evaluated before transfer on initial
force_preic = true
[]
[]
[Executioner]
type = Steady
[]
[MultiApps]
[sub]
type = FullSolveMultiApp
input_files = sub.i
execute_on = initial
[../]
[]
[Transfers]
[to_sub]
type = MultiAppPostprocessorTransfer
to_multi_app = sub
from_postprocessor = c
to_postprocessor = receiver
[]
[]
(modules/navier_stokes/test/tests/finite_element/ins/mms/pspg/pspg_mms_test.i)
mu=1.5
rho=2.5
[GlobalParams]
gravity = '0 0 0'
pspg = true
convective_term = true
integrate_p_by_parts = true
laplace = true
u = vel_x
v = vel_y
pressure = p
alpha = 1e-6
order = FIRST
family = LAGRANGE
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
elem_type = QUAD9
nx = 4
ny = 4
[]
[./corner_node]
type = ExtraNodesetGenerator
new_boundary = 'pinned_node'
nodes = '0'
input = gen
[../]
[]
[Variables]
[./vel_x]
[../]
[./vel_y]
[../]
[./p]
[../]
[]
[Kernels]
# mass
[./mass]
type = INSMass
variable = p
x_vel_forcing_func = vel_x_source_func
y_vel_forcing_func = vel_y_source_func
[../]
# x-momentum, space
[./x_momentum_space]
type = INSMomentumLaplaceForm
variable = vel_x
component = 0
forcing_func = vel_x_source_func
[../]
# y-momentum, space
[./y_momentum_space]
type = INSMomentumLaplaceForm
variable = vel_y
component = 1
forcing_func = vel_y_source_func
[../]
[./p_source]
type = BodyForce
function = p_source_func
variable = p
[../]
[]
[BCs]
[./vel_x]
type = FunctionDirichletBC
boundary = 'left right top bottom'
function = vel_x_func
variable = vel_x
[../]
[./vel_y]
type = FunctionDirichletBC
boundary = 'left right top bottom'
function = vel_y_func
variable = vel_y
[../]
[./p]
type = FunctionDirichletBC
boundary = 'left right top bottom'
function = p_func
variable = p
[../]
[]
[Functions]
[./vel_x_source_func]
type = ParsedFunction
value = '-${mu}*(-0.028*pi^2*x^2*sin(0.2*pi*x*y) - 0.028*pi^2*y^2*sin(0.2*pi*x*y) - 0.1*pi^2*sin(0.5*pi*x) - 0.4*pi^2*sin(pi*y)) + ${rho}*(0.14*pi*x*cos(0.2*pi*x*y) + 0.4*pi*cos(pi*y))*(0.6*sin(0.8*pi*x) + 0.3*sin(0.3*pi*y) + 0.2*sin(0.3*pi*x*y) + 0.3) + ${rho}*(0.14*pi*y*cos(0.2*pi*x*y) + 0.2*pi*cos(0.5*pi*x))*(0.4*sin(0.5*pi*x) + 0.4*sin(pi*y) + 0.7*sin(0.2*pi*x*y) + 0.5) + 0.1*pi*y*cos(0.2*pi*x*y) + 0.25*pi*cos(0.5*pi*x)'
[../]
[./vel_y_source_func]
type = ParsedFunction
value = '-${mu}*(-0.018*pi^2*x^2*sin(0.3*pi*x*y) - 0.018*pi^2*y^2*sin(0.3*pi*x*y) - 0.384*pi^2*sin(0.8*pi*x) - 0.027*pi^2*sin(0.3*pi*y)) + ${rho}*(0.06*pi*x*cos(0.3*pi*x*y) + 0.09*pi*cos(0.3*pi*y))*(0.6*sin(0.8*pi*x) + 0.3*sin(0.3*pi*y) + 0.2*sin(0.3*pi*x*y) + 0.3) + ${rho}*(0.06*pi*y*cos(0.3*pi*x*y) + 0.48*pi*cos(0.8*pi*x))*(0.4*sin(0.5*pi*x) + 0.4*sin(pi*y) + 0.7*sin(0.2*pi*x*y) + 0.5) + 0.1*pi*x*cos(0.2*pi*x*y) + 0.3*pi*cos(0.3*pi*y)'
[../]
[./p_source_func]
type = ParsedFunction
value = '-0.06*pi*x*cos(0.3*pi*x*y) - 0.14*pi*y*cos(0.2*pi*x*y) - 0.2*pi*cos(0.5*pi*x) - 0.09*pi*cos(0.3*pi*y)'
[../]
[./vel_x_func]
type = ParsedFunction
value = '0.4*sin(0.5*pi*x) + 0.4*sin(pi*y) + 0.7*sin(0.2*pi*x*y) + 0.5'
[../]
[./vel_y_func]
type = ParsedFunction
value = '0.6*sin(0.8*pi*x) + 0.3*sin(0.3*pi*y) + 0.2*sin(0.3*pi*x*y) + 0.3'
[../]
[./p_func]
type = ParsedFunction
value = '0.5*sin(0.5*pi*x) + 1.0*sin(0.3*pi*y) + 0.5*sin(0.2*pi*x*y) + 0.5'
[../]
[./vxx_func]
type = ParsedFunction
value = '0.14*pi*y*cos(0.2*pi*x*y) + 0.2*pi*cos(0.5*pi*x)'
[../]
[./px_func]
type = ParsedFunction
value = '0.1*pi*y*cos(0.2*pi*x*y) + 0.25*pi*cos(0.5*pi*x)'
[../]
[]
[Materials]
[./const]
type = GenericConstantMaterial
block = 0
prop_names = 'rho mu'
prop_values = '${rho} ${mu}'
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
petsc_options = '-snes_converged_reason -ksp_converged_reason'
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
nl_abs_tol = 1e-13
nl_max_its = 6
l_tol = 1e-6
l_max_its = 500
[]
[Outputs]
[./exodus]
type = Exodus
[../]
[./csv]
type = CSV
[../]
[]
[Postprocessors]
[./L2vel_x]
type = ElementL2Error
variable = vel_x
function = vel_x_func
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2vel_y]
variable = vel_y
function = vel_y_func
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2p]
variable = p
function = p_func
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2vxx]
variable = vxx
function = vxx_func
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2px]
variable = px
function = px_func
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[]
[AuxVariables]
[./vxx]
family = MONOMIAL
order = FIRST
[../]
[./px]
family = MONOMIAL
order = FIRST
[../]
[]
[AuxKernels]
[./vxx]
type = VariableGradientComponent
component = x
variable = vxx
gradient_variable = vel_x
[../]
[./px]
type = VariableGradientComponent
component = x
variable = px
gradient_variable = p
[../]
[]
(test/tests/meshgenerators/plane_deletion/plane_deletion.i)
[Mesh]
[deleter]
type = PlaneDeletionGenerator
point = '0.5 0.5 0'
normal = '-1 0 0'
input = generated
new_boundary = 6
[]
[generated]
type = GeneratedMeshGenerator
dim = 3
nx = 4
ny = 4
nz = 4
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/materials/generic_materials/generic_constant_material.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 3
ny = 3
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[Kernels]
[./diff1]
type = DiffMKernel
variable = u
mat_prop = diff1
[../]
[./diff2]
type = DiffMKernel
variable = v
mat_prop = diff2
[../]
[]
[BCs]
[./left_u]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = 3
value = 1
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = 1
value = 0
[../]
[]
[Materials]
[./dm1]
type = GenericConstantMaterial
prop_names = 'diff1'
prop_values = '2'
[../]
[./dm2]
type = GenericConstantMaterial
prop_names = 'diff2'
prop_values = '4'
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/ics/constant_ic/subdomain_constant_ic_test.i)
[Mesh]
file = sq-2blk.e
uniform_refine = 1
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./u_aux]
order = CONSTANT
family = MONOMIAL
[../]
[]
[ICs]
[./ic_u_1]
type = ConstantIC
variable = u
value = 42
block = '1 2'
[../]
[./ic_u_aux_1]
type = ConstantIC
variable = u_aux
value = 6.25
block = '1'
[../]
[./ic_u_aux_2]
type = ConstantIC
variable = u_aux
value = 9.99
block = '2'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
nl_rel_tol = 1e-10
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/coupled-force/steady-action-function.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
nx = 16
ny = 16
[]
[]
[Variables]
[u]
family = LAGRANGE_VEC
[]
[]
[Modules]
[IncompressibleNavierStokes]
equation_type = steady-state
velocity_boundary = 'bottom right top left'
velocity_function = '0 0 0 0 0 0 0 0'
add_standard_velocity_variables_for_ad = false
pressure_pinned_node = 0
density_name = rho
dynamic_viscosity_name = mu
use_ad = true
laplace = true
family = LAGRANGE
order = FIRST
supg = true
pspg = true
has_coupled_force = true
coupled_force_vector_function = 'vector_func'
[]
[]
[Kernels]
[u_diff]
type = VectorDiffusion
variable = u
[]
[]
[BCs]
[u_left]
type = VectorFunctionDirichletBC
variable = u
boundary = 'left'
function_x = 1
function_y = 1
[]
[u_right]
type = VectorFunctionDirichletBC
variable = u
boundary = 'right'
function_x = -1
function_y = -1
[]
[]
[Materials]
[const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '1 1'
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_levels -ksp_gmres_restart'
petsc_options_value = 'asm 6 200'
line_search = 'none'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
exodus = true
[]
[Functions]
[vector_func]
type = ParsedVectorFunction
value_x = '-2*x + 1'
value_y = '-2*x + 1'
[]
[]
(modules/navier_stokes/test/tests/finite_element/ins/coupled-force/gravity-through-coupled-force-action.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
nx = 16
ny = 16
[]
[]
[Variables]
[u]
family = LAGRANGE_VEC
[]
[]
[AuxVariables]
[gravity]
family = LAGRANGE_VEC
[]
[]
[ICs]
[gravity]
type = VectorConstantIC
x_value = '0'
y_value = '-9.81'
variable = gravity
[]
[]
[Modules]
[IncompressibleNavierStokes]
equation_type = steady-state
velocity_boundary = 'bottom right top left'
velocity_function = '0 0 0 0 0 0 0 0'
add_standard_velocity_variables_for_ad = false
pressure_pinned_node = 0
density_name = rho
dynamic_viscosity_name = mu
use_ad = true
laplace = true
family = LAGRANGE
order = FIRST
supg = true
pspg = true
has_coupled_force = true
[]
[]
[Kernels]
[u_diff]
type = VectorDiffusion
variable = u
[]
[]
[BCs]
[u_left]
type = VectorFunctionDirichletBC
variable = u
boundary = 'left'
function_x = 1
function_y = 1
[]
[u_right]
type = VectorFunctionDirichletBC
variable = u
boundary = 'right'
function_x = -1
function_y = -1
[]
[]
[Materials]
[const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '1 1'
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_levels -ksp_gmres_restart'
petsc_options_value = 'asm 6 200'
line_search = 'none'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
[out]
type = Exodus
hide = 'gravity'
[]
[]
[Functions]
[vector_func]
type = ParsedVectorFunction
value_x = '-2*x + 1'
value_y = '-2*x + 1'
[]
[vector_gravity_func]
type = ParsedVectorFunction
value_x = '0'
value_y = '-9.81'
[]
[]
(modules/porous_flow/test/tests/gravity/fully_saturated_upwinded_grav01c.i)
# Checking that gravity head is established
# 1phase, 2-component, constant fluid-bulk, constant viscosity, constant permeability
# fully saturated with fully-saturated Kernel with upwinding
# For better agreement with the analytical solution (ana_pp), just increase nx
# NOTE: this test is numerically delicate because the steady-state configuration is independent of the mass fraction, so the frac variable can assume any value as long as mass-fraction is conserved
[Mesh]
type = GeneratedMesh
dim = 1
nx = 100
xmin = -1
xmax = 0
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Variables]
[pp]
[InitialCondition]
type = RandomIC
min = 0
max = 1
[]
[]
[frac]
[InitialCondition]
type = RandomIC
min = 0
max = 1
[]
[]
[]
[Kernels]
[flux1]
type = PorousFlowFullySaturatedAdvectiveFlux
variable = pp
fluid_component = 1
gravity = '-1 0 0'
[]
[flux0]
type = PorousFlowFullySaturatedAdvectiveFlux
variable = frac
fluid_component = 0
gravity = '-1 0 0'
[]
[]
[Functions]
[ana_pp]
type = ParsedFunction
vars = 'g B p0 rho0'
vals = '1 1.2 0 1'
value = '-B*log(exp(-p0/B)+g*rho0*x/B)' # expected pp at base
[]
[]
[BCs]
[z]
type = DirichletBC
variable = pp
boundary = right
value = 0
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp frac'
number_fluid_phases = 1
number_fluid_components = 2
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 1.2
density0 = 1
viscosity = 1
thermal_expansion = 0
[]
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow1PhaseFullySaturated
porepressure = pp
[]
[massfrac]
type = PorousFlowMassFraction
mass_fraction_vars = frac
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1 0 0 0 2 0 0 0 3'
[]
[]
[Postprocessors]
[pp_base]
type = PointValue
variable = pp
point = '-1 0 0'
[]
[pp_analytical]
type = FunctionValuePostprocessor
function = ana_pp
point = '-1 0 0'
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = Newton
nl_rel_tol = 1E-12
petsc_options_iname = '-pc_factor_shift_type'
petsc_options_value = 'NONZERO'
nl_max_its = 100
[]
[Outputs]
csv = true
[]
(test/tests/dgkernels/2d_diffusion_dg/dg_stateful.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
elem_type = QUAD4
[]
[Variables]
[./u]
order = FIRST
family = MONOMIAL
[./InitialCondition]
type = ConstantIC
value = 1
[../]
[../]
[]
[Functions]
[./forcing_fn]
type = ParsedFunction
value = 2*pow(e,-x-(y*y))*(1-2*y*y)
[../]
[./exact_fn]
type = ParsedGradFunction
value = pow(e,-x-(y*y))
grad_x = -pow(e,-x-(y*y))
grad_y = -2*y*pow(e,-x-(y*y))
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./abs]
type = Reaction
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[DGKernels]
[./dg_diff]
type = DGDiffusion
variable = u
epsilon = -1
sigma = 6
[../]
[]
[BCs]
[./all]
type = DGFunctionDiffusionDirichletBC
variable = u
boundary = '0 1 2 3'
function = exact_fn
epsilon = -1
sigma = 6
[../]
[]
[Materials]
[./stateful]
type = StatefulMaterial
initial_diffusivity = 1
boundary = 'left'
[../]
[./general]
type = GenericConstantMaterial
block = '0'
prop_names = 'dummy'
prop_values = '1'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
nl_rel_tol = 1e-10
[]
(test/tests/ics/vector_constant_ic/vector_constant_ic.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 2
ny = 2
nz = 2
[]
[Problem]
solve = false
kernel_coverage_check = false
[]
[Variables]
[./A]
family = LAGRANGE_VEC
order = FIRST
[../]
[]
[ICs]
[./A]
type = VectorConstantIC
variable = A
x_value = 2
y_value = 3
z_value = 4
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(modules/richards/test/tests/gravity_head_1/gh_fu_02.i)
# unsaturated = true
# gravity = false
# supg = false
# transient = false
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
xmin = -1
xmax = 1
[]
[BCs]
[./left]
type = DirichletBC
boundary = left
value = -1
variable = pressure
[../]
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGnone
sat_UO = Saturation
seff_UO = SeffVG
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0E3
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGnone]
type = RichardsSUPGnone
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = RandomIC
block = 0
min = -1
max = 0
[../]
[../]
[]
[Kernels]
active = 'richardsf'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFullyUpwindFlux
variable = pressure
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
viscosity = 1E-3
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = gh_fu_02
exodus = true
[]
(test/tests/fvkernels/mms/advective-outflow/advection-diffusion.i)
diff=1
a=1
[GlobalParams]
advected_interp_method = 'average'
[]
[Mesh]
[./gen_mesh]
type = GeneratedMeshGenerator
dim = 1
xmin = -1
xmax = 0
nx = 2
[../]
[]
[Variables]
[./v]
family = MONOMIAL
order = CONSTANT
fv = true
[../]
[]
[FVKernels]
[./advection]
type = FVAdvection
variable = v
velocity = '${a} 0 0'
force_boundary_execution = true
[../]
[./diffusion]
type = FVDiffusion
variable = v
coeff = coeff
[../]
[body_v]
type = FVBodyForce
variable = v
function = 'forcing'
[]
[]
[FVBCs]
[left]
type = FVFunctionDirichletBC
boundary = 'left'
function = 'exact'
variable = v
[]
[]
[Materials]
[diff]
type = ADGenericFunctorMaterial
prop_names = 'coeff'
prop_values = '${diff}'
[]
[]
[Functions]
[exact]
type = ParsedFunction
value = 'cos(x)'
[]
[forcing]
type = ParsedFunction
value = 'cos(x) - sin(x)'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[./error]
type = ElementL2Error
variable = v
function = exact
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(test/tests/auxkernels/solution_aux/build.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 2
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 3
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
nl_rel_tol = 1e-10
[]
[Outputs]
exodus = true
xda = true
[]
(test/tests/kernels/hfem/array_dirichlet.i)
[Mesh]
[square]
type = GeneratedMeshGenerator
nx = 3
ny = 3
dim = 2
[]
build_all_side_lowerd_mesh = true
[]
[Variables]
[u]
order = THIRD
family = MONOMIAL
block = 0
components = 2
[]
[lambda]
order = CONSTANT
family = MONOMIAL
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
components = 2
[]
[lambdab]
order = CONSTANT
family = MONOMIAL
block = BOUNDARY_SIDE_LOWERD_SUBDOMAIN
components = 2
[]
[]
[AuxVariables]
[v]
order = CONSTANT
family = MONOMIAL
block = 0
initial_condition = '1'
[]
[]
[Kernels]
[diff]
type = ArrayDiffusion
variable = u
block = 0
diffusion_coefficient = dc
[]
[source]
type = ArrayCoupledForce
variable = u
v = v
coef = '1 2'
block = 0
[]
[]
[DGKernels]
[surface]
type = ArrayHFEMDiffusion
variable = u
lowerd_variable = lambda
[]
[]
[BCs]
[all]
type = ArrayHFEMDirichletBC
boundary = 'left right top bottom'
variable = u
lowerd_variable = lambdab
[]
[]
[Materials]
[dc]
type = GenericConstantArray
prop_name = dc
prop_value = '1 1'
[]
[]
[Postprocessors]
[intu]
type = ElementIntegralArrayVariablePostprocessor
variable = u
block = 0
[]
[lambdanorm]
type = ElementArrayL2Norm
variable = lambda
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu basic mumps'
[]
[Outputs]
[out]
# we hide lambda because it may flip sign due to element
# renumbering with distributed mesh
type = Exodus
hide = lambda
[]
csv = true
[]
(modules/heat_conduction/test/tests/code_verification/cartesian_test_no3.i)
# Problem I.3
#
# The thermal conductivity of an infinite plate varies linearly with
# temperature: k = ko(1+beta*u). It has a constant internal heat generation q,
# and has the boundary conditions du/dx = 0 at x= L and u(L) = uo.
#
# REFERENCE:
# A. Toptan, et al. (Mar.2020). Tech. rep. CASL-U-2020-1939-000, SAND2020-3887 R. DOI:10.2172/1614683.
[Mesh]
[./geom]
type = GeneratedMeshGenerator
dim = 1
elem_type = EDGE2
nx = 4
[../]
[]
[Variables]
[./u]
order = FIRST
[../]
[]
[Functions]
[./exact]
type = ParsedFunction
vars = 'q L beta uo ko'
vals = '1200 1 1e-3 0 1'
value = 'uo+(1/beta)*( ( 1 + (1-(x/L)^2) * (beta*q*L^2) / ko )^0.5 - 1)'
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = u
[../]
[./heatsource]
type = HeatSource
function = 1200
variable = u
[../]
[]
[BCs]
[./ui]
type = NeumannBC
boundary = left
variable = u
value = 0
[../]
[./uo]
type = DirichletBC
boundary = right
variable = u
value = 0
[../]
[]
[Materials]
[./property]
type = GenericConstantMaterial
prop_names = 'density specific_heat'
prop_values = '1.0 1.0'
[../]
[./thermal_conductivity]
type = ParsedMaterial
f_name = 'thermal_conductivity'
args = u
function = '1 * (1 + 1e-3*u)'
[../]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[./error]
type = ElementL2Error
function = exact
variable = u
[../]
[./h]
type = AverageElementSize
[]
[]
[Outputs]
csv = true
[]
(test/tests/dgkernels/jacobian_testing/coupled_dg_jac_test.i)
###########################################################
# This is a test of the off diagonal jacobian machinery of
# the Discontinuous Galerkin System.
###########################################################
[Mesh]
type = GeneratedMesh
dim = 1
nx = 2
elem_type = EDGE2
[]
[Variables]
[./u]
order = FIRST
family = MONOMIAL
[../]
[./v]
order = FIRST
family = MONOMIAL
[../]
[]
[DGKernels]
[./dg_diff]
type = DGCoupledDiffusion
variable = u
v = v
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Problem]
kernel_coverage_check = false
[]
[ICs]
[./u]
type = RandomIC
min = 0.1
max = 0.9
variable = u
[../]
[./v]
type = RandomIC
min = 0.1
max = 0.9
variable = v
[../]
[]
(test/tests/userobjects/threaded_general_user_object/test.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 2
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./l]
type = DirichletBC
variable = u
boundary = left
value = 1
[../]
[]
[Executioner]
type = Steady
[]
[UserObjects]
[./prime_product]
type = PrimeProductUserObject
execute_on = timestep_end
[../]
[]
[Postprocessors]
[./product]
type = PrimeProductPostprocessor
prime_product = prime_product
[../]
[]
[Outputs]
csv = true
[]
(test/tests/fvkernels/constraints/integral.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 4
[]
[Variables]
[v]
type = MooseVariableFVReal
[]
[lambda]
type = MooseVariableScalar
[]
[]
[FVKernels]
[diff]
type = FVDiffusion
variable = v
coeff = coeff
[]
[average]
type = FVIntegralValueConstraint
variable = v
phi0 = 13
lambda = lambda
[]
[]
[FVBCs]
[left]
type = FVDirichletBC
variable = v
boundary = left
value = 7
[]
[]
[Materials]
[diff]
type = ADGenericFunctorMaterial
prop_names = 'coeff'
prop_values = '1'
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/add_aux_variable_multiple_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./q]
family = MONOMIAL
order = third
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
[MoreAuxVariables]
[./q]
family = MONOMIAL
order = CONSTANT
[../]
[]
(test/tests/misc/jacobian/offdiag.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./s]
[./InitialCondition]
type = FunctionIC
function = sin(10*x+y)
[../]
[../]
[./t]
[./InitialCondition]
type = FunctionIC
function = sin(13*y+x)
[../]
[../]
[]
[Kernels]
[./diffs]
type = WrongJacobianDiffusion
variable = s
coupled = t
[../]
[./difft]
type = WrongJacobianDiffusion
variable = t
coupled = s
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
(test/tests/variables/caching_fv_variables/fv_caching.i)
[Mesh]
[cmg]
type = CartesianMeshGenerator
dim = 2
dx = '1.5 2.4 0.1'
dy = '1.3 0.9'
ix = '2 1 1'
iy = '2 3'
subdomain_id = '0 1 1 2 2 2'
[]
[]
[Variables]
[u]
type = MooseVariableFVReal
[]
[]
[FVKernels]
[diff]
type = FVDiffusion
variable = u
coeff = 1
[]
[adv]
type = FVMatAdvection
variable = u
vel = v_mat
[]
[body_force]
type = FVBodyForce
variable = u
value = 10
[]
[]
[FVBCs]
[left]
type = FVDirichletBC
variable = u
boundary = 'left'
value = 1
[]
[right]
type = FVDirichletBC
variable = u
boundary = 'right'
value = 1
[]
[top]
type = FVNeumannBC
variable = u
value = 1
boundary = 'top'
[]
[]
[Materials]
[v_mat]
type = ADGenericVectorFunctorMaterial
prop_names = 'v_mat'
prop_values = '4 0 0'
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/postprocessors/flow_rates/conservation_INSFV.i)
mu=1
rho=1
advected_interp_method='average'
velocity_interp_method='rc'
[GlobalParams]
rhie_chow_user_object = 'rc'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[Mesh]
inactive = 'mesh internal_boundary_bot internal_boundary_top'
[mesh]
type = CartesianMeshGenerator
dim = 2
dx = '1'
dy = '1 1 1'
ix = '5'
iy = '5 5 5'
subdomain_id = '1
2
3'
[]
[internal_boundary_bot]
type = SideSetsBetweenSubdomainsGenerator
input = mesh
new_boundary = 'internal_bot'
primary_block = 1
paired_block = 2
[]
[internal_boundary_top]
type = SideSetsBetweenSubdomainsGenerator
input = internal_boundary_bot
new_boundary = 'internal_top'
primary_block = 2
paired_block = 3
[]
[diverging_mesh]
type = FileMeshGenerator
file = 'expansion_quad.e'
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 0
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[temperature]
type = INSFVEnergyVariable
[]
[]
[AuxVariables]
[advected_density]
type = MooseVariableFVReal
initial_condition = ${rho}
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
force_boundary_execution = true
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
force_boundary_execution = true
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[temp_advection]
type = INSFVEnergyAdvection
variable = temperature
advected_interp_method = 'upwind'
[]
[temp_source]
type = FVBodyForce
variable = temperature
function = 10
block = 1
[]
[]
[FVBCs]
inactive = 'noslip-u noslip-v'
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = u
function = 0
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = v
function = 1
[]
[noslip-u]
type = INSFVNoSlipWallBC
boundary = 'right'
variable = u
function = 0
[]
[noslip-v]
type = INSFVNoSlipWallBC
boundary = 'right'
variable = v
function = 0
[]
[free-slip-u]
type = INSFVNaturalFreeSlipBC
boundary = 'right'
variable = u
momentum_component = 'x'
[]
[free-slip-v]
type = INSFVNaturalFreeSlipBC
boundary = 'right'
variable = v
momentum_component = 'y'
[]
[axis-u]
type = INSFVSymmetryVelocityBC
boundary = 'left'
variable = u
u = u
v = v
mu = ${mu}
momentum_component = x
[]
[axis-v]
type = INSFVSymmetryVelocityBC
boundary = 'left'
variable = v
u = u
v = v
mu = ${mu}
momentum_component = y
[]
[axis-p]
type = INSFVSymmetryPressureBC
boundary = 'left'
variable = pressure
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'top'
variable = pressure
function = 0
[]
[inlet_temp]
type = FVNeumannBC
boundary = 'bottom'
variable = temperature
value = 300
[]
[]
[Materials]
[ins_fv]
type = INSFVEnthalpyMaterial
temperature = 'temperature'
rho = ${rho}
[]
[advected_material_property]
type = ADGenericFunctorMaterial
prop_names = 'advected_rho cp'
prop_values ='${rho} 1'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 200 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Postprocessors]
[inlet_mass_variable]
type = VolumetricFlowRate
boundary = bottom
vel_x = u
vel_y = v
advected_quantity = advected_density
[]
[inlet_mass_constant]
type = VolumetricFlowRate
boundary = bottom
vel_x = u
vel_y = v
advected_quantity = ${rho}
[]
[inlet_mass_matprop]
type = VolumetricFlowRate
boundary = bottom
vel_x = u
vel_y = v
advected_quantity = 'advected_rho'
[]
[mid1_mass]
type = VolumetricFlowRate
boundary = internal_bot
vel_x = u
vel_y = v
advected_quantity = ${rho}
[]
[mid2_mass]
type = VolumetricFlowRate
boundary = internal_top
vel_x = u
vel_y = v
advected_quantity = ${rho}
[]
[outlet_mass]
type = VolumetricFlowRate
boundary = top
vel_x = u
vel_y = v
advected_quantity = ${rho}
[]
[inlet_momentum_x]
type = VolumetricFlowRate
boundary = bottom
vel_x = u
vel_y = v
advected_quantity = u
[]
[inlet_momentum_y]
type = VolumetricFlowRate
boundary = bottom
vel_x = u
vel_y = v
advected_quantity = v
[]
[mid1_advected_energy]
type = VolumetricFlowRate
boundary = internal_bot
vel_x = u
vel_y = v
advected_quantity = 'rho_cp_temp'
advected_interp_method = 'upwind'
[]
[mid2_advected_energy]
type = VolumetricFlowRate
boundary = internal_top
vel_x = u
vel_y = v
advected_quantity = 'rho_cp_temp'
advected_interp_method = 'upwind'
[]
[outlet_advected_energy]
type = VolumetricFlowRate
boundary = top
vel_x = u
vel_y = v
advected_quantity = 'rho_cp_temp'
advected_interp_method = 'upwind'
[]
[]
[Outputs]
exodus = true
csv = true
[]
(tutorials/tutorial01_app_development/step10_auxkernels/test/tests/kernels/simple_diffusion/simple_diffusion.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/mesh/nemesis/nemesis_repartitioning_test.i)
[Mesh]
file = cylinder/cylinder.e
nemesis = true
# leaving skip_partitioning off lets us exodiff against a gold
# standard generated with default libMesh settings
# skip_partitioning = true
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
[]
[]
[AuxVariables]
[pid]
family = MONOMIAL
order = CONSTANT
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[AuxKernels]
[pid_aux]
type = ProcessorIDAux
variable = pid
execute_on = 'INITIAL'
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
nl_rel_tol = 1e-6
nl_abs_tol = 1e-14
[Adaptivity]
steps = 1
refine_fraction = 0.1
coarsen_fraction = 0.1
max_h_level = 2
[]
[]
[Postprocessors]
[sum_sides]
type = StatVector
stat = sum
object = nl_wb_element
vector = num_partition_sides
[]
[min_elems]
type = StatVector
stat = min
object = nl_wb_element
vector = num_elems
[]
[max_elems]
type = StatVector
stat = max
object = nl_wb_element
vector = num_elems
[]
[]
[VectorPostprocessors]
[nl_wb_element]
type = WorkBalance
execute_on = initial
system = nl
balances = 'num_elems num_partition_sides'
outputs = none
[]
[]
[Outputs]
[out]
type = CSV
execute_on = FINAL
[]
[]
(test/tests/materials/material/adv_mat_couple_test.i)
[Mesh]
file = rectangle.e
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff body_force'
[./diff]
type = Diffusion
variable = u
[../]
[./body_force]
type = BodyForce
variable = u
block = 1
value = 10
[../]
[]
[BCs]
active = 'right'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Materials]
# This material is global and uses a coupled property
[./mat_global]
type = CoupledMaterial
mat_prop = 'some_prop'
coupled_mat_prop = 'mp1'
block = '1 2'
[../]
# This material supplies a value for block 1 ONLY
[./mat_0]
type = GenericConstantMaterial
block = 1
prop_names = 'mp1'
prop_values = 2
[../]
# This material supplies a value for block 2 ONLY
[./mat_1]
type = GenericConstantMaterial
block = 2
prop_names = 'mp1'
prop_values = 200
[../]
[]
[Executioner]
type = Steady
# solve_type = 'PJFNK'
# preconditioner = 'ILU'
solve_type = 'PJFNK'
# petsc_options_iname = '-pc_type -pc_hypre_type'
# petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
file_base = out_adv_coupled
exodus = true
[]
[Debug]
show_material_props = true
[]
(test/tests/auxkernels/solution_aux/solution_aux_scale.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
xmin = 1
xmax = 4
ymin = 1
ymax = 3
# This test uses SolutionUserObject which doesn't work with DistributedMesh.
parallel_type = replicated
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./u_aux]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./initial_cond_aux]
type = SolutionAux
solution = xda_soln
execute_on = initial
variable = u_aux
[../]
[]
[UserObjects]
[./xda_soln]
type = SolutionUserObject
mesh = build_out_0001_mesh.xda
es = build_out_0001.xda
system_variables = u
scale = '3 2 1'
translation = '1 1 0'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
nl_rel_tol = 1e-10
[]
[Outputs]
exodus = true
xda = true
[]
(test/tests/mesh_modifiers/assign_element_subdomain_id/quad_with_elementid_subdomainid_test.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 2
nz = 0
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[subdomain_id]
type = ElementSubdomainIDGenerator
input = gen
element_ids = '1 2 3'
subdomain_ids = '1 1 1'
[]
[]
[Variables]
active = 'u'
[u]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
active = 'diff'
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
active = 'left right'
# Mesh Generation produces boundaries in counter-clockwise fashion
[left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out_quad_subdomain_id
exodus = true
[]
(test/tests/ics/function_ic/parsed_function.i)
#
# Test the automatically generated gradients in ParsedFunction and the gradient pass-through in FunctionIC
# OLD MOOSE behavior was for parsed_function to behave the same as parsed_zerograd_function
# NEW MOOSE behavior is for parsed_function to behave the same as parsed_grad_function
#
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 3.141
ymin = 0
ymax = 3.141
nx = 10
ny = 10
[]
[Variables]
[./u]
order = THIRD
family = HERMITE
[../]
[]
[Functions]
[./parsed_function]
type = ParsedFunction
value = 'sin(x)-cos(y/2)'
[../]
[./parsed_grad_function]
type =ParsedGradFunction
value = 'sin(x)-cos(y/2)'
grad_x = 'cos(x)'
grad_y = 'sin(y/2)/2'
[../]
[./parsed_zerograd_function]
type = ParsedGradFunction
value = 'sin(x)-cos(y/2)'
grad_x = '0'
grad_y = '0'
[../]
[]
[ICs]
[./u_ic]
type = FunctionIC
variable = 'u'
function = parsed_function
[../]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Outputs]
file_base = parsed
[./OverSampling]
type = Exodus
refinements = 3
[../]
[]
(python/pyhit/tests/input_modified.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
xmax = 3
x_max = 4 # Changed from 3 to 4
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = ADDiffusion
variable = u
[]
[]
[BCs]
[left]
type = ADDirichletBC
variable = u
boundary = left
value = 300
[]
[right]
type = ADNeumannBC
variable = u
boundary = right
value = 100
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
csv = true
[]
(modules/fluid_properties/test/tests/ideal_gas/test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
elem_type = QUAD4
[]
[Functions]
[./f_fn]
type = ParsedFunction
value = -4
[../]
[./bc_fn]
type = ParsedFunction
value = 'x*x+y*y'
[../]
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./e]
initial_condition = 6232.5
[../]
[./v]
initial_condition = 0.02493
[../]
[./p]
family = MONOMIAL
order = CONSTANT
[../]
[./T]
family = MONOMIAL
order = CONSTANT
[../]
[./cp]
family = MONOMIAL
order = CONSTANT
[../]
[./cv]
family = MONOMIAL
order = CONSTANT
[../]
[./c]
family = MONOMIAL
order = CONSTANT
[../]
[./mu]
family = MONOMIAL
order = CONSTANT
[../]
[./k]
family = MONOMIAL
order = CONSTANT
[../]
[./g]
family = MONOMIAL
order = CONSTANT
[../]
[]
[AuxKernels]
[./p]
type = MaterialRealAux
variable = p
property = pressure
[../]
[./T]
type = MaterialRealAux
variable = T
property = temperature
[../]
[./cp]
type = MaterialRealAux
variable = cp
property = cp
[../]
[./cv]
type = MaterialRealAux
variable = cv
property = cv
[../]
[./c]
type = MaterialRealAux
variable = c
property = c
[../]
[./mu]
type = MaterialRealAux
variable = mu
property = mu
[../]
[./k]
type = MaterialRealAux
variable = k
property = k
[../]
[./g]
type = MaterialRealAux
variable = g
property = g
[../]
[]
[Modules]
[./FluidProperties]
[./ideal_gas]
type = IdealGasFluidProperties
gamma = 1.4
molar_mass = 1.000536678700361
[../]
[]
[]
[Materials]
[./fp_mat]
type = FluidPropertiesMaterial
e = e
v = v
fp = ideal_gas
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = f_fn
[../]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
boundary = 'left right top bottom'
function = bc_fn
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(test/tests/dampers/max_increment/max_increment_damper_test.i)
# This model tests the MaxIncrement damper. The converged solution field
# u varies from 0 to 1 across the domain due to the BCs applied. A value
# for the maximum allowed increment to the solution vector for each
# NL iteration is specified. The more restrictive this value is, the
# larger the number of NL iterations will be. This test ensures that a
# minimum number of NL iterations are taken under those conditions.
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
elem_type = QUAD9
[]
[Variables]
[./u]
order = SECOND
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
preset = false
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
preset = false
boundary = right
value = 1
[../]
[]
[Dampers]
[./max_inc_damp]
type = MaxIncrement
max_increment = 0.1
variable = u
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
(test/tests/fvkernels/block-restriction/fv-and-fe-block-restriction.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 80
xmax = 4
[]
[./subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '2.0 0 0'
block_id = 1
top_right = '4.0 1.0 0'
[../]
[./left_right]
input = subdomain1
type = SideSetsBetweenSubdomainsGenerator
primary_block = '0'
paired_block = '1'
new_boundary = 'left_right'
[../]
[./right_left]
input = left_right
type = SideSetsBetweenSubdomainsGenerator
primary_block = '1'
paired_block = '0'
new_boundary = 'right_left'
[../]
[]
[Variables]
[left_fv]
family = MONOMIAL
order = CONSTANT
fv = true
initial_condition = 1
block = 0
[]
[left_fe]
initial_condition = 1
block = 0
[]
[right_fv]
family = MONOMIAL
order = CONSTANT
fv = true
initial_condition = 1
block = 1
[]
[right_fe]
initial_condition = 1
block = 1
[]
[]
[FVKernels]
active = 'bad_left_diff left_coupled bad_right_diff right_coupled'
[bad_left_diff]
type = FVDiffusion
variable = left_fv
coeff = fv_prop
block = 0
[]
[good_left_diff]
type = FVDiffusion
variable = left_fv
coeff = left_fv_prop
block = 0
[]
[left_coupled]
type = FVCoupledForce
v = left_fv
variable = left_fv
block = 0
[]
[bad_right_diff]
type = FVDiffusion
variable = right_fv
coeff = fv_prop
block = 1
[]
[good_right_diff]
type = FVDiffusion
variable = right_fv
coeff = right_fv_prop
block = 1
[]
[right_coupled]
type = FVCoupledForce
v = right_fv
variable = right_fv
block = 1
[]
[]
[Kernels]
[left_diff]
type = ADFunctorMatDiffusion
variable = left_fe
diffusivity = fe_prop
[]
[left_coupled]
type = CoupledForce
v = left_fv
variable = left_fe
[]
[right_diff]
type = ADFunctorMatDiffusion
variable = right_fe
diffusivity = fe_prop
[]
[right_coupled]
type = CoupledForce
v = right_fv
variable = right_fe
[]
[]
[FVBCs]
[left]
type = FVDirichletBC
variable = left_fv
boundary = left
value = 0
[]
[left_right]
type = FVDirichletBC
variable = left_fv
boundary = left_right
value = 1
[]
[right_left]
type = FVDirichletBC
variable = right_fv
boundary = right_left
value = 0
[]
[right]
type = FVDirichletBC
variable = right_fv
boundary = right
value = 1
[]
[]
[BCs]
[left]
type = DirichletBC
variable = left_fe
boundary = left
value = 0
[]
[left_right]
type = DirichletBC
variable = left_fe
boundary = left_right
value = 1
[]
[right_left]
type = DirichletBC
variable = right_fe
boundary = right_left
value = 0
[]
[right]
type = DirichletBC
variable = right_fe
boundary = right
value = 1
[]
[]
[Materials]
active = 'fe_mat_left bad_fv_mat_left fe_mat_right bad_fv_mat_right'
[fe_mat_left]
type = FEFVCouplingMaterial
fe_var = left_fe
block = 0
[]
[bad_fv_mat_left]
type = FEFVCouplingMaterial
fv_var = left_fv
block = 0
[]
[good_fv_mat_left]
type = FEFVCouplingMaterial
fv_var = left_fv
fv_prop_name = 'left_fv_prop'
block = 0
[]
[fe_mat_right]
type = FEFVCouplingMaterial
fe_var = right_fe
block = 1
[]
[bad_fv_mat_right]
type = FEFVCouplingMaterial
fv_var = right_fv
block = 1
[]
[good_fv_mat_right]
type = FEFVCouplingMaterial
fv_var = right_fv
fv_prop_name = 'right_fv_prop'
block = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
[]
[Outputs]
exodus = true
[dof]
type = DOFMap
execute_on = 'initial'
[]
[]
(test/tests/preconditioners/multi_cycle_hypre/multi_cycle_hypre.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
uniform_refine = 2
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
# This option appears to modify the behavior in PETSc 3.6.0
petsc_options = '-pc_hypre_boomeramg_print_statistics'
petsc_options_iname = '-pc_type -pc_hypre_type -pc_hypre_boomeramg_tol -pc_hypre_boomeramg_max_iter'
petsc_options_value = 'hypre boomeramg 1e-4 20'
[]
[Outputs]
exodus = true
[]
(test/tests/vectorpostprocessors/line_value_sampler/csv_delimiter.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./v]
initial_condition = 1.23456789
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[VectorPostprocessors]
[./line_sample]
type = LineValueSampler
variable = 'u v'
start_point = '0 0.5 0'
end_point = '1 0.5 0'
num_points = 11
sort_by = id
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[./csv]
type = CSV
delimiter = ' '
precision = 5
[../]
[]
(modules/ray_tracing/test/tests/userobjects/ray_tracing_study/errors/errors.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
nx = 2
[]
[]
[UserObjects]
active = 'study'
[study]
type = RayTracingStudyTest
ray_kernel_coverage_check = false
[]
[repeatable]
type = RepeatableRayStudy
start_points = '0 0 0'
directions = '1 0 0'
names = 'ray'
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
(test/tests/kernels/block_kernel/block_vars.i)
[Mesh]
file = rect-2blk.e
[]
[Variables]
active = 'u v'
[./u]
order = FIRST
family = LAGRANGE
block = 1
[../]
[./v]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff_u diff_v'
[./diff_u]
type = Diffusion
variable = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[BCs]
active = 'left_u right_u left_v right_v'
[./left_u]
type = DirichletBC
variable = u
boundary = 6
value = 0
[../]
[./right_u]
type = NeumannBC
variable = u
boundary = 8
value = 4
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = 6
value = 1
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = 3
value = 6
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
file_base = out_vars
exodus = true
[]
(test/tests/misc/check_error/missing_material_prop_test.i)
[Mesh]
file = rectangle.e
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff body_force'
[./diff]
type = DiffMKernel
variable = u
mat_prop = diff1
[../]
[./body_force]
type = BodyForce
variable = u
block = 1
value = 10
[../]
[]
[BCs]
active = 'right'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Materials]
[./mat1]
type = GenericConstantMaterial
block = 1
prop_names = 'diff1'
prop_values = '1'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/porous_flow/test/tests/relperm/corey2.i)
# Test Corey relative permeability curve by varying saturation over the mesh
# Corey exponent n = 2 for both phases
# No residual saturation in either phase
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Variables]
[p0]
initial_condition = 1e6
[]
[s1]
family = LAGRANGE
order = FIRST
[]
[]
[AuxVariables]
[s0aux]
family = MONOMIAL
order = CONSTANT
[]
[s1aux]
family = MONOMIAL
order = CONSTANT
[]
[kr0aux]
family = MONOMIAL
order = CONSTANT
[]
[kr1aux]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[s0]
type = PorousFlowPropertyAux
property = saturation
phase = 0
variable = s0aux
[]
[s1]
type = PorousFlowPropertyAux
property = saturation
phase = 1
variable = s1aux
[]
[kr0]
type = PorousFlowPropertyAux
property = relperm
phase = 0
variable = kr0aux
[]
[kr1]
type = PorousFlowPropertyAux
property = relperm
phase = 1
variable = kr1aux
[]
[]
[Functions]
[s1]
type = ParsedFunction
value = x
[]
[]
[ICs]
[s1]
type = FunctionIC
variable = s1
function = s1
[]
[]
[Kernels]
[p0]
type = Diffusion
variable = p0
[]
[s1]
type = Diffusion
variable = s1
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'p0 s1'
number_fluid_phases = 2
number_fluid_components = 2
[]
[pc]
type = PorousFlowCapillaryPressureConst
pc = 0
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow2PhasePS
phase0_porepressure = p0
phase1_saturation = s1
capillary_pressure = pc
[]
[kr0]
type = PorousFlowRelativePermeabilityCorey
phase = 0
n = 2
[]
[kr1]
type = PorousFlowRelativePermeabilityCorey
phase = 1
n = 2
[]
[]
[VectorPostprocessors]
[vpp]
type = LineValueSampler
warn_discontinuous_face_values = false
variable = 's0aux s1aux kr0aux kr1aux'
start_point = '0 0 0'
end_point = '1 0 0'
num_points = 20
sort_by = id
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
nl_abs_tol = 1e-8
[]
[BCs]
[sleft]
type = DirichletBC
variable = s1
value = 0
boundary = left
[]
[sright]
type = DirichletBC
variable = s1
value = 1
boundary = right
[]
[]
[Outputs]
csv = true
execute_on = timestep_end
[]
(test/tests/variables/array_variable/array_variable_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 8
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
components = 4
initial_condition = '1 2 3 4'
[../]
[./uu]
order = FIRST
family = LAGRANGE
components = 2
initial_condition = '1 2'
[../]
[./v]
order = FIRST
family = LAGRANGE
components = 2
initial_condition = '5 6'
[../]
[./w]
order = CONSTANT
family = MONOMIAL
components = 3
initial_condition = '7 8 9'
[../]
[./x]
order = THIRD
family = MONOMIAL
components = 2
initial_condition = '10 11'
[../]
[./y]
order = FIRST
family = L2_LAGRANGE
components = 3
initial_condition = '12 13 14'
[../]
[]
[Postprocessors]
[u0int]
type = ElementIntegralArrayVariablePostprocessor
variable = u
component = 0
[]
[u1int]
type = ElementIntegralArrayVariablePostprocessor
variable = u
component = 1
[]
[u2int]
type = ElementIntegralArrayVariablePostprocessor
variable = u
component = 2
[]
[u3int]
type = ElementIntegralArrayVariablePostprocessor
variable = u
component = 3
[]
[uu0int]
type = ElementIntegralArrayVariablePostprocessor
variable = uu
component = 0
[]
[uu1int]
type = ElementIntegralArrayVariablePostprocessor
variable = uu
component = 1
[]
[v0int]
type = ElementIntegralArrayVariablePostprocessor
variable = v
component = 0
[]
[v1int]
type = ElementIntegralArrayVariablePostprocessor
variable = v
component = 1
[]
[w0int]
type = ElementIntegralArrayVariablePostprocessor
variable = w
component = 0
[]
[w1int]
type = ElementIntegralArrayVariablePostprocessor
variable = w
component = 1
[]
[w2int]
type = ElementIntegralArrayVariablePostprocessor
variable = w
component = 2
[]
[x0int]
type = ElementIntegralArrayVariablePostprocessor
variable = x
component = 0
[]
[x1int]
type = ElementIntegralArrayVariablePostprocessor
variable = x
component = 1
[]
[y0int]
type = ElementIntegralArrayVariablePostprocessor
variable = y
component = 0
[]
[y1int]
type = ElementIntegralArrayVariablePostprocessor
variable = y
component = 1
[]
[y2int]
type = ElementIntegralArrayVariablePostprocessor
variable = y
component = 2
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/userobjects/nearest_point_layered_average/radius_points_from_uo.i)
[Mesh]
[ccmg]
type = ConcentricCircleMeshGenerator
num_sectors = 8
radii = '0.1 0.2 0.3 0.4 0.5'
rings = '2 2 2 2 2'
has_outer_square = false
preserve_volumes = true
smoothing_max_it = 3
[]
[extruder]
type = MeshExtruderGenerator
input = ccmg
extrusion_vector = '0 0 1'
num_layers = 4
[]
[]
[Variables]
[u]
[]
[]
[AuxVariables]
[ring_average]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[reac]
type = Reaction
variable = u
[]
[forcing]
type = BodyForce
variable = u
function = func
[]
[]
[Functions]
[func]
type = ParsedFunction
value = 'sqrt(x * x + y * y) + z'
[]
[]
[AuxKernels]
[np_layered_average]
type = SpatialUserObjectAux
variable = ring_average
execute_on = timestep_end
user_object = nrla
[]
[]
[UserObjects]
[nrla]
type = NearestRadiusLayeredAverage
direction = z
num_layers = 2
points = '0.05 0 0
0.15 0 0
0.25 0 0
0.35 0 0
0.45 0 0'
variable = u
[]
[]
[VectorPostprocessors]
# getting the points from the user object itself is here exactly equivalent to the points
# provided in the 'spatial_manually_provided' vector postprocessor
[spatial_from_uo]
type = SpatialUserObjectVectorPostprocessor
userobject = nrla
[]
[spatial_manually_provided]
type = SpatialUserObjectVectorPostprocessor
userobject = nrla
points = '0.05 0 0.25
0.05 0 0.75
0.15 0 0.25
0.15 0 0.75
0.25 0 0.25
0.25 0 0.75
0.35 0 0.25
0.35 0 0.75
0.45 0 0.25
0.45 0 0.75'
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
csv = true
exodus = true
execute_on = final
[]
(modules/navier_stokes/test/tests/finite_element/ins/coupled-force/steady-action.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
nx = 16
ny = 16
[]
[]
[Variables]
[u]
family = LAGRANGE_VEC
[]
[]
[Modules]
[IncompressibleNavierStokes]
equation_type = steady-state
velocity_boundary = 'bottom right top left'
velocity_function = '0 0 0 0 0 0 0 0'
add_standard_velocity_variables_for_ad = false
pressure_pinned_node = 0
density_name = rho
dynamic_viscosity_name = mu
use_ad = true
laplace = true
family = LAGRANGE
order = FIRST
supg = true
pspg = true
has_coupled_force = true
coupled_force_var = u
[]
[]
[Kernels]
[u_diff]
type = VectorDiffusion
variable = u
[]
[]
[BCs]
[u_left]
type = VectorFunctionDirichletBC
variable = u
boundary = 'left'
function_x = 1
function_y = 1
[]
[u_right]
type = VectorFunctionDirichletBC
variable = u
boundary = 'right'
function_x = -1
function_y = -1
[]
[]
[Materials]
[const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '1 1'
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_levels -ksp_gmres_restart'
petsc_options_value = 'asm 6 200'
line_search = 'none'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
exodus = true
[]
(modules/richards/test/tests/pressure_pulse/pp_fu_21.i)
# investigating pressure pulse in 1D with 2 phase
# steadystate
[Mesh]
type = GeneratedMesh
dim = 1
nx = 10
xmin = 0
xmax = 100
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = 'DensityWater DensityGas'
relperm_UO = 'RelPermWater RelPermGas'
SUPG_UO = 'SUPGwater SUPGgas'
sat_UO = 'SatWater SatGas'
seff_UO = 'SeffWater SeffGas'
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = 'pwater pgas'
[../]
[./DensityWater]
type = RichardsDensityConstBulk
dens0 = 1000
bulk_mod = 2E9
[../]
[./DensityGas]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 2E6
[../]
[./SeffWater]
type = RichardsSeff2waterVG
m = 0.8
al = 1E-5
[../]
[./SeffGas]
type = RichardsSeff2gasVG
m = 0.8
al = 1E-5
[../]
[./RelPermWater]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./RelPermGas]
type = RichardsRelPermPower
simm = 0.0
n = 3
[../]
[./SatWater]
type = RichardsSat
s_res = 0.0
sum_s_res = 0.0
[../]
[./SatGas]
type = RichardsSat
s_res = 0.0
sum_s_res = 0.0
[../]
[./SUPGwater]
type = RichardsSUPGstandard
p_SUPG = 1E3
[../]
[./SUPGgas]
type = RichardsSUPGstandard
p_SUPG = 1E3
[../]
[]
[Variables]
[./pwater]
order = FIRST
family = LAGRANGE
[../]
[./pgas]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./water_ic]
type = ConstantIC
value = 2E6
variable = pwater
[../]
[./gas_ic]
type = ConstantIC
value = 2E6
variable = pgas
[../]
[]
[BCs]
[./left]
type = DirichletBC
boundary = left
value = 3E6
variable = pwater
[../]
[./left_gas]
type = DirichletBC
boundary = left
value = 3E6
variable = pgas
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[Kernels]
active = 'richardsfwater richardsfgas pconstraint'
[./richardstwater]
type = RichardsMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFullyUpwindFlux
variable = pwater
[../]
[./richardstgas]
type = RichardsMassChange
variable = pgas
[../]
[./richardsfgas]
type = RichardsFullyUpwindFlux
variable = pgas
[../]
[./pconstraint]
type = RichardsPPenalty
variable = pgas
a = 1E-8
lower_var = pwater
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = SeffWater
pressure_vars = 'pwater pgas'
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-15 0 0 0 1E-15 0 0 0 1E-15'
viscosity = '1E-3 1E-5'
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-pc_factor_shift_type'
petsc_options_value = 'nonzero'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
nl_rel_tol = 1.e-10
nl_max_its = 10
[]
[Outputs]
execute_on = 'timestep_end'
file_base = pp_fu_21
exodus = true
[]
(test/tests/userobjects/internal_side_user_object/internal_side_user_object_two_materials.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = -1
ymin = -1
xmax = 1
ymax = 1
nx = 2
ny = 2
elem_type = QUAD4
[]
[./subdomain_id]
input = gen
type = ElementSubdomainIDGenerator
subdomain_ids = '0 1
1 1'
[../]
[]
[Functions]
[./fn_exact]
type = ParsedFunction
value = 'x*x+y*y'
[../]
[./ffn]
type = ParsedFunction
value = -4
[../]
[]
[UserObjects]
[./isuo]
type = InsideUserObject
variable = u
diffusivity = diffusivity
execute_on = 'initial timestep_end'
[../]
[]
[Variables]
[./u]
family = LAGRANGE
order = FIRST
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = ffn
[../]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
boundary = '0 1 2 3'
function = fn_exact
[../]
[]
[Materials]
[./stateful1]
type = StatefulMaterial
block = 0
initial_diffusivity = 1
[../]
[./stateful2]
type = StatefulMaterial
block = 1
initial_diffusivity = 2
[../]
[]
[Postprocessors]
[./value]
type = InsideValuePPS
user_object = isuo
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/bcs/pp_neumann/pp_neumann.i)
# NOTE: This file is used within the documentation, so please do not change names within the file
# without checking that associated documentation is not affected, see syntax/Postprocessors/index.md.
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[u]
[]
[]
[AuxVariables]
[aux]
initial_condition = 5
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = PostprocessorNeumannBC
variable = u
boundary = right
postprocessor = right_pp
[]
[]
[Postprocessors]
[right_pp]
type = PointValue
point = '0.5 0.5 0'
variable = aux
execute_on = 'initial'
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(test/tests/mesh/mesh_generation/disc.i)
# Generates a Disc Mesh
# Radius of outside circle=5
# Solves the diffusion equation with u=-5 at origin, and u=0 on outside
[Mesh]
type = AnnularMesh
nr = 10
nt = 12
rmin = 0
rmax = 5
growth_r = 1.3
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./inner]
type = DirichletBC
variable = u
value = -5.0
boundary = rmin
[../]
[./outer]
type = DirichletBC
variable = u
value = 0.0
boundary = rmax
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
[]
[Outputs]
exodus = true
[]
(test/tests/postprocessors/side_diffusive_flux_integral/side_diffusive_flux_integral_fv.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
order = CONSTANT
family = MONOMIAL
fv = true
[../]
[]
[FVKernels]
[./diff]
type = FVDiffusion
variable = u
coeff = 1
[../]
[]
[FVBCs]
[./left]
type = FVDirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = FVDirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Materials]
[./mat_props]
type = GenericConstantMaterial
block = 0
prop_names = diffusivity
prop_values = 2
[../]
[./mat_props_bnd]
type = GenericConstantMaterial
boundary = right
prop_names = diffusivity
prop_values = 1
[../]
[./mat_props_vector]
type = GenericConstantVectorMaterial
boundary = 'right top'
prop_names = diffusivity_vec
prop_values = '1 1.5 1'
[../]
[]
[Postprocessors]
inactive = 'avg_flux_top'
[./avg_flux_right]
# Computes flux integral on the boundary, which should be -1
type = SideDiffusiveFluxAverage
variable = u
boundary = right
diffusivity = diffusivity
[../]
[./avg_flux_top]
type = SideVectorDiffusivityFluxIntegral
variable = u
boundary = top
diffusivity = diffusivity_vec
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
nl_abs_tol = 1e-14
nl_rel_tol = 1e-14
l_abs_tol = 1e-14
l_tol = 1e-6
[]
[Outputs]
exodus = true
[]
(test/tests/fvkernels/mms/mat-advection-diffusion.i)
diff=1.1
a=1.1
[GlobalParams]
advected_interp_method = 'average'
[]
[Mesh]
[./gen_mesh]
type = GeneratedMeshGenerator
dim = 1
xmin = -0.6
xmax = 0.6
nx = 64
[../]
[]
[Variables]
[./v]
family = MONOMIAL
order = CONSTANT
fv = true
[../]
[]
[FVKernels]
[./advection]
type = FVMatAdvection
variable = v
vel = 'fv_velocity'
[../]
[./diffusion]
type = FVDiffusion
variable = v
coeff = coeff
[../]
[body_v]
type = FVBodyForce
variable = v
function = 'forcing'
[]
[]
[FVBCs]
[boundary]
type = FVFunctionDirichletBC
boundary = 'left right'
function = 'exact'
variable = v
[]
[]
[Materials]
[diff]
type = ADGenericFunctorMaterial
prop_names = 'coeff'
prop_values = '${diff}'
[]
[adv_material]
type = ADCoupledVelocityMaterial
vel_x = '${a}'
rho = 'v'
velocity = 'fv_velocity'
[]
[]
[Functions]
[exact]
type = ParsedFunction
value = '3*x^2 + 2*x + 1'
[]
[forcing]
type = ParsedFunction
value = '-${diff}*6 + ${a} * (6*x + 2)'
# value = '-${diff}*6'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[./error]
type = ElementL2Error
variable = v
function = exact
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_mortar/large_gap_heat_transfer_test_cylinder.i)
rpv_core_gap_size = 0.15
core_outer_radius = 2
rpv_inner_radius = '${fparse 2 + rpv_core_gap_size}'
rpv_outer_radius = '${fparse 2.5 + rpv_core_gap_size}'
rpv_outer_htc = 10 # W/m^2/K
rpv_outer_Tinf = 300 # K
core_blocks = '1'
rpv_blocks = '3'
[Mesh]
[core_gap_rpv]
type = ConcentricCircleMeshGenerator
num_sectors = 10
radii = '${core_outer_radius} ${rpv_inner_radius} ${rpv_outer_radius}'
rings = '2 1 2'
has_outer_square = false
preserve_volumes = true
portion = full
[]
[rename_core_bdy]
type = SideSetsBetweenSubdomainsGenerator
input = core_gap_rpv
primary_block = 1
paired_block = 2
new_boundary = 'core_outer'
[]
[rename_inner_rpv_bdy]
type = SideSetsBetweenSubdomainsGenerator
input = rename_core_bdy
primary_block = 3
paired_block = 2
new_boundary = 'rpv_inner'
[]
[2d_mesh]
type = BlockDeletionGenerator
input = rename_inner_rpv_bdy
block = 2
[]
allow_renumbering = false
[]
[Variables]
[Tsolid]
initial_condition = 500
[]
[]
[Kernels]
[heat_source]
type = CoupledForce
variable = Tsolid
block = '${core_blocks}'
v = power_density
[]
[heat_conduction]
type = HeatConduction
variable = Tsolid
[]
[]
[BCs]
[RPV_out_BC] # k \nabla T = h (T- T_inf) at RPV outer boundary
type = ConvectiveFluxFunction # (Robin BC)
variable = Tsolid
boundary = 'outer' # outer RPV
coefficient = ${rpv_outer_htc}
T_infinity = ${rpv_outer_Tinf}
[]
[]
[ThermalContact]
[RPV_gap]
type = GapHeatTransfer
gap_geometry_type = 'CYLINDER'
emissivity_primary = 0.8
emissivity_secondary = 0.8
variable = Tsolid
primary = 'core_outer'
secondary = 'rpv_inner'
gap_conductivity = 0.1
quadrature = true
cylinder_axis_point_1 = '0 0 0'
cylinder_axis_point_2 = '0 0 5'
[]
[]
[AuxVariables]
[power_density]
block = '${core_blocks}'
initial_condition = 50e3
[]
[]
[Materials]
[simple_mat]
type = HeatConductionMaterial
thermal_conductivity = 34.6 # W/m/K
[]
[]
[Postprocessors]
[Tcore_avg]
type = ElementAverageValue
variable = Tsolid
block = '${core_blocks}'
[]
[Tcore_max]
type = ElementExtremeValue
value_type = max
variable = Tsolid
block = '${core_blocks}'
[]
[Tcore_min]
type = ElementExtremeValue
value_type = min
variable = Tsolid
block = '${core_blocks}'
[]
[Trpv_avg]
type = ElementAverageValue
variable = Tsolid
block = '${rpv_blocks}'
[]
[Trpv_max]
type = ElementExtremeValue
value_type = max
variable = Tsolid
block = '${rpv_blocks}'
[]
[Trpv_min]
type = ElementExtremeValue
value_type = min
variable = Tsolid
block = '${rpv_blocks}'
[]
[ptot]
type = ElementIntegralVariablePostprocessor
variable = power_density
block = '${core_blocks}'
[]
[rpv_convective_out]
type = ConvectiveHeatTransferSideIntegral
T_solid = Tsolid
boundary = 'outer' # outer RVP
T_fluid = ${rpv_outer_Tinf}
htc = ${rpv_outer_htc}
[]
[heat_balance] # should be equal to 0 upon convergence
type = ParsedPostprocessor
function = '(rpv_convective_out - ptot) / ptot'
pp_names = 'rpv_convective_out ptot'
[]
[]
[VectorPostprocessors]
[NodalTemperature]
type = NodalValueSampler
sort_by = id
boundary = 'rpv_inner core_outer'
variable = Tsolid
[]
[]
[Executioner]
type = Steady
automatic_scaling = true
compute_scaling_once = false
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart '
petsc_options_value = 'hypre boomeramg 100'
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
l_max_its = 100
[Quadrature]
side_order = seventh
[]
line_search = none
[]
[Outputs]
exodus = false
csv = true
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_balance/large_gap_heat_transfer_test_cylinder.i)
rpv_core_gap_size = 0.15
core_outer_radius = 2
rpv_inner_radius = ${fparse 2 + rpv_core_gap_size}
rpv_outer_radius = ${fparse 2.5 + rpv_core_gap_size}
rpv_outer_htc = 10 # W/m^2/K
rpv_outer_Tinf = 300 # K
core_blocks = '1'
rpv_blocks = '3'
[Mesh]
[core_gap_rpv]
type = ConcentricCircleMeshGenerator
num_sectors = 10
radii = '${core_outer_radius} ${rpv_inner_radius} ${rpv_outer_radius}'
rings = '2 1 2'
has_outer_square = false
preserve_volumes = true
portion = full
[]
[rename_core_bdy]
type = SideSetsBetweenSubdomainsGenerator
input = core_gap_rpv
primary_block = 1
paired_block = 2
new_boundary = 'core_outer'
[]
[rename_inner_rpv_bdy]
type = SideSetsBetweenSubdomainsGenerator
input = rename_core_bdy
primary_block = 3
paired_block = 2
new_boundary = 'rpv_inner'
[]
[2d_mesh]
type = BlockDeletionGenerator
input = rename_inner_rpv_bdy
block = 2
[]
[]
[Variables]
[Tsolid]
initial_condition = 500
[]
[]
[Kernels]
[heat_source]
type = CoupledForce
variable = Tsolid
block = '${core_blocks}'
v = power_density
[]
[heat_conduction]
type = HeatConduction
variable = Tsolid
[]
[]
[BCs]
[RPV_out_BC] # k \nabla T = h (T- T_inf) at RPV outer boundary
type = ConvectiveFluxFunction # (Robin BC)
variable = Tsolid
boundary = 'outer' # outer RPV
coefficient = ${rpv_outer_htc}
T_infinity = ${rpv_outer_Tinf}
[]
[]
[ThermalContact]
[RPV_gap]
type = GapHeatTransfer
gap_geometry_type = 'CYLINDER'
emissivity_primary = 0.8
emissivity_secondary = 0.8
variable = Tsolid
primary = 'core_outer'
secondary = 'rpv_inner'
gap_conductivity = 0.1
quadrature = true
cylinder_axis_point_1 = '0 0 0'
cylinder_axis_point_2 = '0 0 5'
[]
[]
[AuxVariables]
[power_density]
block = '${core_blocks}'
initial_condition = 50e3
[]
[]
[Materials]
[simple_mat]
type = HeatConductionMaterial
thermal_conductivity = 34.6 # W/m/K
[]
[]
[Postprocessors]
[Tcore_avg]
type = ElementAverageValue
variable = Tsolid
block = '${core_blocks}'
[]
[Tcore_max]
type = ElementExtremeValue
value_type = max
variable = Tsolid
block = '${core_blocks}'
[]
[Tcore_min]
type = ElementExtremeValue
value_type = min
variable = Tsolid
block = '${core_blocks}'
[]
[Trpv_avg]
type = ElementAverageValue
variable = Tsolid
block = '${rpv_blocks}'
[]
[Trpv_max]
type = ElementExtremeValue
value_type = max
variable = Tsolid
block = '${rpv_blocks}'
[]
[Trpv_min]
type = ElementExtremeValue
value_type = min
variable = Tsolid
block = '${rpv_blocks}'
[]
[ptot]
type = ElementIntegralVariablePostprocessor
variable = power_density
block = '${core_blocks}'
[]
[rpv_convective_out]
type = ConvectiveHeatTransferSideIntegral
T_solid = Tsolid
boundary = 'outer' # outer RVP
T_fluid = ${rpv_outer_Tinf}
htc = ${rpv_outer_htc}
[]
[heat_balance] # should be equal to 0 upon convergence
type = ParsedPostprocessor
function = '(rpv_convective_out - ptot) / ptot'
pp_names = 'rpv_convective_out ptot'
[]
[]
[Executioner]
type = Steady
automatic_scaling = true
compute_scaling_once = false
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart '
petsc_options_value = 'hypre boomeramg 100'
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
l_max_its = 100
[Quadrature]
side_order = seventh
[]
line_search = none
[]
[Outputs]
exodus = false
csv = true
[]
(modules/fluid_properties/test/tests/two_phase_fluid_properties_independent/test.i)
# Tests the TwoPhaseFluidPropertiesIndependent class, which takes the names
# of 2 single-phase fluid properties independently. This test uses a dummy
# aux to make sure that the single-phase fluid properties can be recovered
# from the 2-phase fluid properties. A modification to this test checks that
# an error results if one tries to call a 2-phase fluid properties interface
# using this class, which is designed to ensure that the 2 phases are independent.
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
# Required for NodalVariableValue on distributed mesh
allow_renumbering = false
[]
[Problem]
solve = false
[]
[AuxVariables]
[./p]
initial_condition = 1e5
[../]
[./T]
initial_condition = 300
[../]
[./rho_avg]
[../]
[]
[Modules]
[./FluidProperties]
# rho1 = 1.149425287 kg/m^3
[./fp1]
type = IdealGasFluidProperties
gamma = 1.4
molar_mass = 0.02867055103448276
[../]
# rho2 = 0.6666666667 kg/m^3
[./fp2]
type = IdealGasFluidProperties
gamma = 1.2
molar_mass = 0.0166289196
[../]
[./fp_2phase]
type = TwoPhaseFluidPropertiesIndependent
fp_liquid = fp1
fp_vapor = fp2
[../]
[]
[]
[AuxKernels]
# correct value (0.5*(rho1 + rho2)) should be: 0.90804597685 kg/m^3
[./rho_avg_aux]
type = TwoPhaseAverageDensityAux
variable = rho_avg
p = p
T = T
fp_2phase = fp_2phase
execute_on = 'initial'
[../]
[]
[Postprocessors]
[./rho_avg_value]
type = NodalVariableValue
variable = rho_avg
nodeid = 0
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
execute_on = 'timestep_end'
csv = true
[]
(modules/combined/test/tests/gap_heat_transfer_mortar/small-2d/open_gap_pressure_dependent.i)
## Units in the input file: m-Pa-s-K
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
[left_rectangle]
type = GeneratedMeshGenerator
dim = 2
nx = 40
ny = 10
xmax = 1
ymin = 0
ymax = 0.5
boundary_name_prefix = moving_block
[]
[left_block]
type = SubdomainIDGenerator
input = left_rectangle
subdomain_id = 1
[]
[right_rectangle]
type = GeneratedMeshGenerator
dim = 2
nx = 40
ny = 10
xmin = 1.0001
xmax = 2.0001
ymin = 0
ymax = 0.5
boundary_name_prefix = fixed_block
boundary_id_offset = 4
[]
[right_block]
type = SubdomainIDGenerator
input = right_rectangle
subdomain_id = 2
[]
[two_blocks]
type = MeshCollectionGenerator
inputs = 'left_block right_block'
[]
[block_rename]
type = RenameBlockGenerator
input = two_blocks
old_block = '1 2'
new_block = 'left_block right_block'
[]
[]
[Variables]
[disp_x]
block = 'left_block right_block'
[]
[disp_y]
block = 'left_block right_block'
[]
[temperature]
initial_condition = 525.0
[]
[temperature_interface_lm]
block = 'interface_secondary_subdomain'
[]
[]
[Modules]
[TensorMechanics/Master]
[steel]
strain = SMALL
add_variables = false
use_automatic_differentiation = true
additional_generate_output = 'vonmises_stress'
additional_material_output_family = 'MONOMIAL'
additional_material_output_order = 'FIRST'
block = 'left_block'
[]
[aluminum]
strain = SMALL
add_variables = false
use_automatic_differentiation = true
additional_generate_output = 'vonmises_stress'
additional_material_output_family = 'MONOMIAL'
additional_material_output_order = 'FIRST'
block = 'right_block'
[]
[]
[]
[Kernels]
[HeatDiff_steel]
type = ADHeatConduction
variable = temperature
thermal_conductivity = steel_thermal_conductivity
block = 'left_block'
[]
[HeatDiff_aluminum]
type = ADHeatConduction
variable = temperature
thermal_conductivity = aluminum_thermal_conductivity
block = 'right_block'
[]
[]
[BCs]
[fixed_bottom_edge]
type = ADDirichletBC
variable = disp_y
value = 0
boundary = 'moving_block_bottom fixed_block_bottom'
[]
[fixed_outer_edge]
type = ADDirichletBC
variable = disp_x
value = 0
boundary = 'fixed_block_right'
[]
[pressure_left_block]
type = ADPressure
variable = disp_x
boundary = 'moving_block_left'
component = 0
function = 1*t
[]
[temperature_left]
type = ADDirichletBC
variable = temperature
value = 800
boundary = 'moving_block_left'
[]
[temperature_right]
type = ADDirichletBC
variable = temperature
value = 250
boundary = 'fixed_block_right'
[]
[]
[Contact]
[interface]
primary = moving_block_right
secondary = fixed_block_left
model = frictionless
formulation = mortar
correct_edge_dropping = true
[]
[]
[Constraints]
[thermal_contact]
type = ModularGapConductanceConstraint
variable = temperature_interface_lm
secondary_variable = temperature
primary_boundary = moving_block_right
primary_subdomain = interface_primary_subdomain
secondary_boundary = fixed_block_left
secondary_subdomain = interface_secondary_subdomain
gap_flux_models = 'closed'
use_displaced_mesh = true
[]
[]
[Materials]
[steel_elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1.93e11 #in Pa, 193 GPa, stainless steel 304
poissons_ratio = 0.29
block = 'left_block'
[]
[steel_stress]
type = ADComputeLinearElasticStress
block = 'left_block'
[]
[steel_density]
type = ADGenericConstantMaterial
prop_names = 'steel_density'
prop_values = 8e3 #in kg/m^3, stainless steel 304
block = 'left_block'
[]
[steel_thermal_properties]
type = ADGenericConstantMaterial
prop_names = 'steel_thermal_conductivity steel_heat_capacity steel_emissivity'
prop_values = '16.2 0.5 0.6' ## for stainless steel 304
block = 'left_block'
[]
[aluminum_elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 6.8e10 #in Pa, 68 GPa, aluminum
poissons_ratio = 0.36
block = 'right_block'
[]
[aluminum_stress]
type = ADComputeLinearElasticStress
block = 'right_block'
[]
[aluminum_density]
type = ADGenericConstantMaterial
prop_names = 'aluminum_density'
prop_values = 2.7e3 #in kg/m^3, stainless steel 304
block = 'right_block'
[]
[aluminum_thermal_properties]
type = ADGenericConstantMaterial
prop_names = 'aluminum_thermal_conductivity aluminum_heat_capacity aluminum_emissivity'
prop_values = '210 0.9 0.25'
block = 'right_block'
[]
[]
[UserObjects]
[closed]
type = GapFluxModelPressureDependentConduction
primary_conductivity = steel_thermal_conductivity
secondary_conductivity = aluminum_thermal_conductivity
temperature = temperature
primary_hardness = 1.0
secondary_hardness = 1.0
boundary = moving_block_right
contact_pressure = interface_normal_lm
[]
[]
[Postprocessors]
[steel_pt_interface_temperature]
type = NodalVariableValue
nodeid = 245
variable = temperature
[]
[aluminum_pt_interface_temperature]
type = NodalVariableValue
nodeid = 657
variable = temperature
[]
[interface_heat_flux_steel]
type = ADSideDiffusiveFluxAverage
variable = temperature
boundary = moving_block_right
diffusivity = steel_thermal_conductivity
[]
[interface_heat_flux_aluminum]
type = ADSideDiffusiveFluxAverage
variable = temperature
boundary = fixed_block_left
diffusivity = aluminum_thermal_conductivity
[]
[steel_element_interface_stress]
type = ElementalVariableValue
variable = vonmises_stress
elementid = 199
[]
[aluminum_element_interface_stress]
type = ElementalVariableValue
variable = vonmises_stress
elementid = 560
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
automatic_scaling = false
line_search = 'none'
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
[]
[Outputs]
csv = true
perf_graph = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/multiapp-scalar-transport/fluid-flow.i)
mu=1
rho=1
[GlobalParams]
rhie_chow_user_object = 'rc'
advected_interp_method='average'
velocity_interp_method='rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 10
ymin = -1
ymax = 1
nx = 100
ny = 20
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[AuxVariables]
[ax_out]
type = MooseVariableFVReal
[]
[ay_out]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[ax_out]
type = ADFunctorElementalAux
functor = ax
variable = ax_out
execute_on = timestep_end
[]
[ay_out]
type = ADFunctorElementalAux
functor = ay
variable = ay_out
execute_on = timestep_end
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = 0
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = u
function = 0
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = v
function = 0
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 0
[]
[]
[MultiApps]
[scalar]
type = FullSolveMultiApp
execute_on = 'timestep_end'
input_files = 'scalar-transport.i'
[]
[]
[Transfers]
[ax]
type = MultiAppCopyTransfer
source_variable = ax_out
variable = ax
execute_on = 'timestep_end'
to_multi_app = 'scalar'
[]
[ay]
type = MultiAppCopyTransfer
source_variable = ay_out
variable = ay
execute_on = 'timestep_end'
to_multi_app = 'scalar'
[]
[u]
type = MultiAppCopyTransfer
source_variable = u
variable = u
execute_on = 'timestep_end'
to_multi_app = 'scalar'
[]
[v]
type = MultiAppCopyTransfer
source_variable = v
variable = v
execute_on = 'timestep_end'
to_multi_app = 'scalar'
[]
[pressure]
type = MultiAppCopyTransfer
source_variable = pressure
variable = pressure
execute_on = 'timestep_end'
to_multi_app = 'scalar'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(modules/richards/test/tests/jacobian_1/jn02.i)
# unsaturated = true
# gravity = false
# supg = false
# transient = false
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = -1
xmax = 1
ymin = -1
ymax = 1
zmin = -1
zmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0 # notice small quantity, so the PETSc constant state works
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1 # notice small quantity, so the PETSc constant state works
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.2
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGnone]
type = RichardsSUPGnone
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = RandomIC
block = 0
min = -1
max = 0
[../]
[../]
[]
[Kernels]
active = 'richardsf'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGnone
sat_UO = Saturation
seff_UO = SeffVG
viscosity = 1E-3
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -snes_type'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000 test'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = jn02
exodus = false
[]
(modules/tensor_mechanics/test/tests/elasticitytensor/rotation_matrix_1_rotation.i)
# This input file is designed to rotate an elasticity tensor both with euler angles
# and a rotation matrix. The rotated tensor components should match between the
# two methods.
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
xmax = 1
[]
[AuxVariables]
[./C1111_aux_matrix] # C11
order = CONSTANT
family = MONOMIAL
[../]
[./C1122_aux_matrix] # C12
order = CONSTANT
family = MONOMIAL
[../]
[./C1133_aux_matrix] # C13
order = CONSTANT
family = MONOMIAL
[../]
[./C1112_aux_matrix] # C16
order = CONSTANT
family = MONOMIAL
[../]
[./C1111_aux_euler] # C11
order = CONSTANT
family = MONOMIAL
[../]
[./C1122_aux_euler] # C12
order = CONSTANT
family = MONOMIAL
[../]
[./C1133_aux_euler] # C13
order = CONSTANT
family = MONOMIAL
[../]
[./C1112_aux_euler] # C16
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./matl_C1111_matrix] # C11
type = RankFourAux
rank_four_tensor = rotation_matrix_elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 0
variable = C1111_aux_matrix
execute_on = initial
[../]
[./matl_C1122_matrix] # C12
type = RankFourAux
rank_four_tensor = rotation_matrix_elasticity_tensor
index_i = 0
index_j = 0
index_k = 1
index_l = 1
variable = C1122_aux_matrix
execute_on = initial
[../]
[./matl_C1133_matrix] # C13
type = RankFourAux
rank_four_tensor = rotation_matrix_elasticity_tensor
index_i = 0
index_j = 0
index_k = 2
index_l = 2
variable = C1133_aux_matrix
execute_on = initial
[../]
[./matl_C1112_matrix] # C16
type = RankFourAux
rank_four_tensor = rotation_matrix_elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 1
variable = C1112_aux_matrix
execute_on = initial
[../]
[./matl_C1111_euler] # C11
type = RankFourAux
rank_four_tensor = euler_elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 0
variable = C1111_aux_euler
execute_on = initial
[../]
[./matl_C1122_euler] # C12
type = RankFourAux
rank_four_tensor = euler_elasticity_tensor
index_i = 0
index_j = 0
index_k = 1
index_l = 1
variable = C1122_aux_euler
execute_on = initial
[../]
[./matl_C1133_euler] # C13
type = RankFourAux
rank_four_tensor = euler_elasticity_tensor
index_i = 0
index_j = 0
index_k = 2
index_l = 2
variable = C1133_aux_euler
execute_on = initial
[../]
[./matl_C1112_euler] # C16
type = RankFourAux
rank_four_tensor = euler_elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 1
variable = C1112_aux_euler
execute_on = initial
[../]
[]
[Materials]
[./elasticity_matrix]
type = ComputeElasticityTensor
block = 0
base_name = 'rotation_matrix'
fill_method = symmetric9
C_ijkl = '1111 1122 1133 2222 2233 3333 2323 1313 1212'
# rotation matrix for rotating a vector 30 degrees about the z-axis
rotation_matrix = '0.8660254 -0.5 0.
0.5 0.8660254 0
0 0 1'
[../]
[./elasticity_euler]
type = ComputeElasticityTensor
block = 0
base_name = 'euler'
fill_method = symmetric9
C_ijkl = '1111 1122 1133 2222 2233 3333 2323 1313 1212'
euler_angle_1 = -30. # same as above but opposite direction because _transpose_ gets built from these angles
euler_angle_2 = 0.
euler_angle_3 = 0.
[../]
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[Executioner]
type = Steady
[]
[Postprocessors]
# corresponding values in "matrix" and "euler" postprocessors should match
[./C11_matrix]
type = ElementAverageValue
variable = C1111_aux_matrix
execute_on = 'INITIAL TIMESTEP_END'
[../]
[./C12_matrix]
type = ElementAverageValue
variable = C1122_aux_matrix
execute_on = 'INITIAL TIMESTEP_END'
[../]
[./C13_matrix]
type = ElementAverageValue
variable = C1133_aux_matrix
execute_on = 'INITIAL TIMESTEP_END'
[../]
[./C16_matrix]
type = ElementAverageValue
variable = C1112_aux_matrix
execute_on = 'INITIAL TIMESTEP_END'
[../]
[./C11_euler]
type = ElementAverageValue
variable = C1111_aux_euler
execute_on = 'INITIAL TIMESTEP_END'
[../]
[./C12_euler]
type = ElementAverageValue
variable = C1122_aux_euler
execute_on = 'INITIAL TIMESTEP_END'
[../]
[./C13_euler]
type = ElementAverageValue
variable = C1133_aux_euler
execute_on = 'INITIAL TIMESTEP_END'
[../]
[./C16_euler]
type = ElementAverageValue
variable = C1112_aux_euler
execute_on = 'INITIAL TIMESTEP_END'
[../]
[]
[Outputs]
exodus = true
[]
(modules/richards/test/tests/gravity_head_1/gh05.i)
# unsaturated = false
# gravity = false
# supg = true
# transient = false
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
xmin = -1
xmax = 1
[]
[BCs]
[./left]
type = DirichletBC
boundary = left
value = 1
variable = pressure
[../]
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0E3
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 0.1
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = RandomIC
block = 0
min = 0
max = 1
[../]
[../]
[]
[Kernels]
active = 'richardsf'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGstandard
sat_UO = Saturation
seff_UO = SeffVG
viscosity = 1E-3
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = gh05
exodus = true
[]
(test/tests/vectorpostprocessors/sideset_info/sideset_info.i)
[Mesh]
type = MeshGeneratorMesh
[./uniform]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
nx = 8
ymin = -0.4
ymax = 10.4
ny = 5
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[VectorPostprocessors]
[./side_info]
type = SidesetInfoVectorPostprocessor
boundary = 'left right bottom'
meta_data_types = 'centroid min max area'
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
file_base = out
csv = true
[]
(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/2d-rc-rz-by-parts.i)
mu=1.1
rho=1
advected_interp_method='average'
velocity_interp_method='rc'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 5
ymin = 0
ymax = 1
nx = 40
ny = 10
[]
[]
[Problem]
coord_type = 'RZ'
rz_coord_axis = 'X'
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = PINSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
porosity = porosity
[]
[]
[Variables]
[u]
type = PINSFVSuperficialVelocityVariable
initial_condition = 1
[]
[v]
type = PINSFVSuperficialVelocityVariable
initial_condition = 1e-6
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[AuxVariables]
[porosity]
family = MONOMIAL
order = CONSTANT
fv = true
initial_condition = 0.5
[]
[]
[FVKernels]
inactive = 'v_pressure_volumetric'
[mass]
type = PINSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = PINSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
porosity = porosity
momentum_component = 'x'
[]
[u_viscosity]
type = PINSFVMomentumDiffusion
variable = u
mu = ${mu}
porosity = porosity
momentum_component = 'x'
[]
[u_pressure]
type = PINSFVMomentumPressureFlux
variable = u
momentum_component = 'x'
pressure = pressure
porosity = porosity
[]
[u_friction]
type = PINSFVMomentumFriction
variable = u
momentum_component = 'x'
porosity = porosity
Darcy_name = 'Darcy_coefficient'
Forchheimer_name = 'Forchheimer_coefficient'
rho = ${rho}
[]
[v_advection]
type = PINSFVMomentumAdvection
variable = v
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
porosity = porosity
momentum_component = 'y'
[]
[v_viscosity]
type = PINSFVMomentumDiffusion
variable = v
mu = ${mu}
porosity = porosity
momentum_component = 'y'
[]
[v_pressure_volumetric]
type = PINSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
porosity = porosity
[]
[v_pressure_by_parts_flux]
type = PINSFVMomentumPressureFlux
variable = v
momentum_component = 'y'
pressure = pressure
porosity = porosity
[]
[v_pressure_by_parts_volume_term]
type = PNSFVMomentumPressureFluxRZ
variable = v
pressure = pressure
porosity = porosity
momentum_component = 'y'
[]
[v_friction]
type = PINSFVMomentumFriction
variable = v
momentum_component = 'y'
porosity = porosity
Darcy_name = 'Darcy_coefficient'
Forchheimer_name = 'Forchheimer_coefficient'
rho = ${rho}
[]
[]
[FVBCs]
inactive = 'free-slip-u free-slip-v'
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = 0
[]
[no-slip-u]
type = INSFVNoSlipWallBC
boundary = 'top'
variable = u
function = 0
[]
[no-slip-v]
type = INSFVNoSlipWallBC
boundary = 'top'
variable = v
function = 0
[]
[free-slip-u]
type = INSFVNaturalFreeSlipBC
boundary = 'top'
variable = u
momentum_component = 'x'
[]
[free-slip-v]
type = INSFVNaturalFreeSlipBC
boundary = 'top'
variable = v
momentum_component = 'y'
[]
[symmetry-u]
type = PINSFVSymmetryVelocityBC
boundary = 'bottom'
variable = u
u = u
v = v
mu = ${mu}
momentum_component = 'x'
[]
[symmetry-v]
type = PINSFVSymmetryVelocityBC
boundary = 'bottom'
variable = v
u = u
v = v
mu = ${mu}
momentum_component = 'y'
[]
[symmetry-p]
type = INSFVSymmetryPressureBC
boundary = 'bottom'
variable = pressure
[]
[outlet-p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 0
[]
[]
[Materials]
[darcy]
type = ADGenericVectorFunctorMaterial
prop_names = 'Darcy_coefficient Forchheimer_coefficient'
prop_values = '0.1 0.1 0.1 0.1 0.1 0.1'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 200 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-11
nl_abs_tol = 1e-14
[]
# Some basic Postprocessors to visually examine the solution
[Postprocessors]
[inlet-p]
type = SideAverageValue
variable = pressure
boundary = 'left'
[]
[outlet-u]
type = SideIntegralVariablePostprocessor
variable = u
boundary = 'right'
[]
[]
[Outputs]
exodus = true
[]
(examples/ex17_dirac/ex17.i)
[Mesh]
file = 3-4-torus.e
[]
[Variables]
[./diffused]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = diffused
[../]
[]
[DiracKernels]
[./example_point_source]
type = ExampleDirac
variable = diffused
value = 1.0
point = '-2.1 -5.08 0.7'
[../]
[]
[BCs]
[./right]
type = DirichletBC
variable = diffused
boundary = 'right'
value = 0
[../]
[./left]
type = DirichletBC
variable = diffused
boundary = 'left'
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(test/tests/utils/spline_interpolation/spline_interpolation.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 4
xmin = -1
xmax = 3
elem_type = EDGE2
[]
[Functions]
[./spline_fn]
type = SplineFunction
x = '-1 0 3'
y = '0.5 0 3'
[../]
[]
[Variables]
[./u]
order = THIRD
family = HERMITE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./ufn]
type = SplineFFn
variable = u
function = spline_fn
[../]
[]
[BCs]
[./sides]
type = FunctionDirichletBC
variable = u
boundary = '0 1'
function = spline_fn
[../]
[]
[Postprocessors]
[./l2_err]
type = ElementL2Error
variable = u
function = spline_fn
execute_on = 'initial timestep_end'
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/interface_stress/test.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 10
ny = 10
nz = 10
xmax = 1
ymax = 1
zmax = 1
xmin = -1
ymin = -1
zmin = -1
[]
[GlobalParams]
order = CONSTANT
family = MONOMIAL
rank_two_tensor = extra_stress
[]
[Functions]
[./sphere]
type = ParsedFunction
value = 'r:=sqrt(x^2+y^2+z^2); if(r>1,0,1-3*r^2+2*r^3)'
[../]
[]
[Variables]
[./dummy]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = dummy
[../]
[]
[AuxVariables]
[./eta]
[./InitialCondition]
type = FunctionIC
function = sphere
[../]
order = FIRST
family = LAGRANGE
[../]
[./s00]
[../]
[./s01]
[../]
[./s02]
[../]
[./s10]
[../]
[./s11]
[../]
[./s12]
[../]
[./s20]
[../]
[./s21]
[../]
[./s22]
[../]
[]
[AuxKernels]
[./s00]
type = RankTwoAux
variable = s00
index_i = 0
index_j = 0
[../]
[./s01]
type = RankTwoAux
variable = s01
index_i = 0
index_j = 1
[../]
[./s02]
type = RankTwoAux
variable = s02
index_i = 0
index_j = 2
[../]
[./s10]
type = RankTwoAux
variable = s10
index_i = 1
index_j = 0
[../]
[./s11]
type = RankTwoAux
variable = s11
index_i = 1
index_j = 1
[../]
[./s12]
type = RankTwoAux
variable = s12
index_i = 1
index_j = 2
[../]
[./s20]
type = RankTwoAux
variable = s20
index_i = 2
index_j = 0
[../]
[./s21]
type = RankTwoAux
variable = s21
index_i = 2
index_j = 1
[../]
[./s22]
type = RankTwoAux
variable = s22
index_i = 2
index_j = 2
[../]
[]
[Materials]
[./interface]
type = ComputeInterfaceStress
v = eta
stress = 3.0
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
execute_on = timestep_end
hide = 'dummy eta'
[]
(test/tests/interfacekernels/ik_displaced/different_jxw_displaced.i)
[Mesh]
displacements = 'disp_x disp_y'
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 2
xmax = 2
ny = 1
ymax = 1
[]
[./subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '0 0 0'
top_right = '1 1 0'
block_id = 1
[../]
[./break_boundary]
input = subdomain1
type = BreakMeshByBlockGenerator
[../]
[]
[AuxVariables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
use_displaced_mesh = true
[../]
[]
[InterfaceKernels]
[./interface]
type = InterfacialSource
variable = u
neighbor_var = u
boundary = interface
use_displaced_mesh = true
[../]
[]
[BCs]
[./u]
type = DirichletBC
variable = u
boundary = 'left right'
value = 0
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
[Functions]
[./disp_x_func]
type = ParsedFunction
value = 1
[../]
[./disp_y_func]
type = ParsedFunction
value = y
[../]
[]
[ICs]
[./disp_x_ic]
block = 0
function = disp_x_func
variable = disp_x
type = FunctionIC
[../]
[./disp_y_ic]
block = 0
function = disp_y_func
variable = disp_y
type = FunctionIC
[../]
[]
(test/tests/bcs/periodic/periodic_subdomain_restricted_test.i)
[Mesh]
file = rect-2blk.e
[]
[Variables]
active = 'u v'
[./u]
order = FIRST
family = LAGRANGE
block = 1
[../]
[./v]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff_u diff_v'
[./diff_u]
type = Diffusion
variable = u
block = 1
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[BCs]
active = 'Periodic left_u right_u left_v right_v'
[./Periodic]
[./u]
variable = u
primary = 1
secondary = 5
translation = '0 1 0'
[../]
[./v1]
variable = v
primary = 1
secondary = 5
translation = '0 1 0'
[../]
[./v2]
variable = v
primary = 2
secondary = 4
translation = '0 1 0'
[../]
[../]
[./left_u]
type = DirichletBC
variable = u
boundary = 6
value = 0
[../]
[./right_u]
type = NeumannBC
variable = u
boundary = 8
value = 4
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = 6
value = 1
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = 3
value = 6
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
file_base = out_restrict
exodus = true
[]
(test/tests/fvkernels/fv-to-fe-coupling/1d.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 40
xmax = 2
[]
[]
[Variables]
[fv]
family = MONOMIAL
order = CONSTANT
fv = true
initial_condition = 1
[]
[fe]
initial_condition = 1
[]
[]
[FVKernels]
[diff]
type = FVDiffusion
variable = fv
coeff = fv_prop
[]
[coupled]
type = FVCoupledForce
v = fv
variable = fv
[]
[]
[Kernels]
[diff]
type = ADFunctorMatDiffusion
variable = fe
diffusivity = fe_prop
[]
[coupled]
type = CoupledForce
v = fv
variable = fe
[]
[]
[FVBCs]
[left]
type = FVDirichletBC
variable = fv
boundary = left
value = 0
[]
[right]
type = FVDirichletBC
variable = fv
boundary = right
value = 1
[]
[]
[BCs]
[left]
type = DirichletBC
variable = fe
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = fe
boundary = right
value = 1
[]
[]
[Materials]
active = 'fe_mat fv_mat'
[bad_mat]
type = FEFVCouplingMaterial
fe_var = fe
fv_var = fv
execute_on = 'linear nonlinear'
[]
[fe_mat]
type = FEFVCouplingMaterial
fe_var = fe
execute_on = 'linear nonlinear'
[]
[fv_mat]
type = FEFVCouplingMaterial
fv_var = fv
[]
[fe_mat_bad_dep]
type = FEFVCouplingMaterial
fe_var = fe
declared_prop_name = bad
[]
[fv_mat_bad_dep]
type = FEFVCouplingMaterial
fv_var = fv
retrieved_prop_name = bad
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
[]
[Outputs]
exodus = true
[dof]
type = DOFMap
execute_on = 'initial'
[]
[]
(tutorials/tutorial01_app_development/step08_test_harness/test/tests/kernels/simple_diffusion/simple_diffusion.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/ray_tracing/test/tests/userobjects/ray_tracing_study/tolerate_failure/tolerate_failure.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
nx = 10
[]
[]
[UserObjects/study]
type = RepeatableRayStudy
start_points = '0 0 0
0 0 0'
directions = '1 0 0
1 0 0'
names = 'ray0 ray1'
ray_kernel_coverage_check = false
tolerate_failure = true
[]
[RayBCs]
[kill]
type = KillRayBC
rays = 'ray1'
boundary = 'right'
[]
[null]
type = NullRayBC
rays = 'ray0'
boundary = 'right'
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
(test/tests/bcs/ad_function_neumann_bc/test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
dim = 2
nx = 32
ny = 32
[../]
[]
[Variables]
[./u]
[../]
[]
[Functions]
[./exact_func]
type = ParsedFunction
value = x*x
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = 2
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = FunctionNeumannBC
function = x
variable = u
boundary = right
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
execute_on = 'timestep_end'
file_base = neumannbc_out
exodus = true
[]
(modules/thermal_hydraulics/test/tests/materials/ad_average_wall_temperature_3eqn/ad_average_wall_temperature_3eqn.i)
# Tests the average wall temperature aux for 1-phase flow. With the following
# inputs, the value should be equal to 1.25:
#
# i h_wall T_wall P_hf
# --------------------------
# 1 10 26/10 1
# 2 6 1/2 3
#
# T_fluid = 1/4
#
# With these values,
# P_tot = 1 + 3 = 4
# h_wall_avg = (1 * 10 + 3 * 6) / 4 = 28 / 4 = 7
# denominator = P_tot * h_wall_avg = 4 * 7 = 28
# numerator = 10 * (26/10 - 1/4) * 1 + 6 * (1/2 - 1/4) * 3 = 28
# T_wall_avg = T_fluid + numerator / denominator = 1/4 + 1
#
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
allow_renumbering = false
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = ADDiffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[AuxVariables]
[Hw_avg]
family = MONOMIAL
order = CONSTANT
[]
[T_wall_avg]
family = MONOMIAL
order = CONSTANT
[]
[T_wall1]
family = MONOMIAL
order = CONSTANT
[]
[T_wall2]
family = MONOMIAL
order = CONSTANT
[]
[P_hf1]
family = MONOMIAL
order = CONSTANT
[]
[P_hf2]
family = MONOMIAL
order = CONSTANT
[]
[P_hf_total]
family = MONOMIAL
order = CONSTANT
[]
[T_fluid]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[T_wall_avg_auxkernel]
type = ADMaterialRealAux
variable = T_wall_avg
property = T_wall
[]
[T_wall1_auxkernel]
type = ConstantAux
variable = T_wall1
value = 2.6
[]
[T_wall2_auxkernel]
type = ConstantAux
variable = T_wall2
value = 0.5
[]
[P_hf_total_auxkernel]
type = SumAux
variable = P_hf_total
values = 'P_hf1 P_hf2'
[]
[P_hf1_auxkernel]
type = ConstantAux
variable = P_hf1
value = 1
[]
[P_hf2_auxkernel]
type = ConstantAux
variable = P_hf2
value = 3
[]
[T_fluid_auxkernel]
type = ConstantAux
variable = T_fluid
value = 0.25
[]
[]
[Materials]
[const_materials]
type = ADGenericConstantMaterial
prop_names = 'Hw1 Hw2'
prop_values = '10 6'
[]
[Hw_avg_material]
type = ADWeightedAverageMaterial
prop_name = Hw_avg
values = 'Hw1 Hw2'
weights = 'P_hf1 P_hf2'
[]
[T_wall_avg_material]
type = ADAverageWallTemperature3EqnMaterial
T_wall_sources = 'T_wall1 T_wall2'
Hw_sources = 'Hw1 Hw2'
P_hf_sources = 'P_hf1 P_hf2'
T_fluid = T_fluid
Hw_average = Hw_avg
P_hf_total = P_hf_total
[]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[T_wall_avg_pp]
type = ElementalVariableValue
elementid = 0
variable = T_wall_avg
[]
[]
[Outputs]
csv = true
execute_on = timestep_end
[]
(test/tests/interfaces/vectorpostprocessorinterface/vppi_errors.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
[]
[]
[UserObjects/error_test]
type = VectorPostprocessorInterfaceErrorTest
vpp = constant_vpp
[]
[VectorPostprocessors/constant_vpp]
type = ConstantVectorPostprocessor
vector_names = 'vpp_val'
value = '1'
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
(modules/combined/test/tests/eigenstrain/variable.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
xmax = 0.5
ymax = 0.5
elem_type = QUAD4
[]
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./TensorMechanics]
[../]
[]
[AuxVariables]
[./e11_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./e22_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./c]
[../]
[./eigen_strain00]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./matl_e11]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 0
variable = e11_aux
[../]
[./matl_e22]
type = RankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 1
variable = e22_aux
[../]
[./eigen_strain00]
type = RankTwoAux
variable = eigen_strain00
rank_two_tensor = eigenstrain
index_j = 0
index_i = 0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeElasticityTensor
block = 0
C_ijkl = '1 1'
fill_method = symmetric_isotropic
[../]
[./stress]
type = ComputeLinearElasticStress
block = 0
[../]
[./var_dependence]
type = DerivativeParsedMaterial
block = 0
function = 0.5*c^2
args = c
outputs = exodus
output_properties = 'var_dep'
f_name = var_dep
enable_jit = true
derivative_order = 2
[../]
[./eigenstrain]
type = ComputeVariableEigenstrain
block = 0
eigen_base = '1 1 1 0 0 0'
prefactor = var_dep
args = c
eigenstrain_name = eigenstrain
[../]
[./strain]
type = ComputeSmallStrain
block = 0
displacements = 'disp_x disp_y'
eigenstrain_names = eigenstrain
[../]
[]
[BCs]
active = 'left_x bottom_y'
[./bottom_y]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0
[../]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = left
value = 0
[../]
[./right_x]
type = DirichletBC
variable = disp_x
boundary = right
value = 0
[../]
[./top_y]
type = DirichletBC
variable = disp_y
boundary = top
value = 0.01
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart'
petsc_options_value = 'hypre boomeramg 31'
l_max_its = 20
nl_max_its = 10
l_tol = 1.0e-4
nl_rel_tol = 1.0e-10
nl_abs_tol = 1.0e-50
[]
[Outputs]
exodus = true
[]
[ICs]
[./c_IC]
int_width = 0.075
x1 = 0
y1 = 0
radius = 0.25
outvalue = 0
variable = c
invalue = 1
type = SmoothCircleIC
[../]
[]
(test/tests/kernels/hfem/array_robin.i)
[Mesh]
[square]
type = GeneratedMeshGenerator
nx = 3
ny = 3
dim = 2
[]
build_all_side_lowerd_mesh = true
[]
[Variables]
[u]
order = THIRD
family = MONOMIAL
block = 0
components = 2
[]
[lambda]
order = CONSTANT
family = MONOMIAL
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
components = 2
[]
[]
[AuxVariables]
[v]
order = CONSTANT
family = MONOMIAL
block = 0
initial_condition = '1'
[]
[]
[Kernels]
[diff]
type = ArrayDiffusion
variable = u
block = 0
diffusion_coefficient = dc
[]
[source]
type = ArrayCoupledForce
variable = u
v = v
coef = '1 2'
block = 0
[]
[]
[DGKernels]
[surface]
type = ArrayHFEMDiffusion
variable = u
lowerd_variable = lambda
[]
[]
[BCs]
[all]
type = ArrayVacuumBC
boundary = 'left right top bottom'
variable = u
[]
[]
[Materials]
[dc]
type = GenericConstantArray
prop_name = dc
prop_value = '1 1'
[]
[]
[Postprocessors]
[intu]
type = ElementIntegralArrayVariablePostprocessor
variable = u
block = 0
[]
[lambdanorm]
type = ElementArrayL2Norm
variable = lambda
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu basic mumps'
[]
[Outputs]
[out]
# we hide lambda because it may flip sign due to element
# renumbering with distributed mesh
type = Exodus
hide = lambda
[]
csv = true
[]
(test/tests/userobjects/shape_element_user_object/shape_side_uo_physics_test.i)
u_left = 0.5
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
parallel_type = replicated
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[./pot]
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./adv_u]
type = PotentialAdvection
variable = u
potential = pot
[../]
[./diff_pot]
type = Diffusion
variable = pot
[../]
[]
[BCs]
[./left]
boundary = left
type = DirichletBC
value = ${u_left}
variable = u
[../]
[./right]
boundary = right
type = DirichletBC
variable = u
value = 0
[../]
[./left_pot]
boundary = left
type = ExampleShapeSideIntegratedBC
variable = pot
num_user_object = num_user_object
denom_user_object = denom_user_object
v = u
Vb = 1
[../]
[./right_pot]
boundary = right
type = DirichletBC
variable = pot
value = 0
[../]
[]
[UserObjects]
[./num_user_object]
type = NumShapeSideUserObject
u = u
boundary = left
execute_on = 'linear nonlinear'
[../]
[./denom_user_object]
type = DenomShapeSideUserObject
u = u
boundary = left
execute_on = 'linear nonlinear'
[../]
[]
[AuxVariables]
[./u_flux]
family = MONOMIAL
order = CONSTANT
[../]
[]
[AuxKernels]
[./u_flux]
type = DriftDiffusionFluxAux
variable = u_flux
u = u
potential = pot
component = 0
[../]
[]
[Problem]
type = FEProblem
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
petsc_options = '-snes_converged_reason -ksp_converged_reason -snes_linesearch_monitor'
petsc_options_iname = '-pc_type -sub_pc_type -sub_ksp_type'
petsc_options_value = 'asm lu preonly'
[]
[Outputs]
exodus = true
perf_graph = true
[]
[ICs]
[./u]
type = FunctionIC
variable = u
function = ic_u
[../]
[./pot]
type = FunctionIC
variable = pot
function = ic_pot
[../]
[]
[Functions]
[./ic_u]
type = ParsedFunction
value = '${u_left} * (1 - x)'
[../]
[./ic_pot]
type = ParsedFunction
value = '1 - x'
[../]
[]
(test/tests/bcs/misc_bcs/vacuum_bc_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
nz = 0
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right top'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0.0
[../]
[./right]
type = NeumannBC
variable = u
boundary = 1
value = 2.0
[../]
[./top]
type = VacuumBC
variable = u
boundary = 2
alpha = 5.0
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-mixing-length.i)
Re = 1e4
von_karman_const = 0.2
D = 1
rho = 1
bulk_u = 1
mu = ${fparse rho * bulk_u * D / Re}
advected_interp_method='upwind'
velocity_interp_method='rc'
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 5
ymin = 0
ymax = ${fparse 0.5 * D}
nx = 20
ny = 10
bias_y = ${fparse 1 / 1.2}
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = 1
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[scalar]
type = INSFVScalarFieldVariable
[]
[]
[AuxVariables]
[mixing_length]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = ${mu}
momentum_component = 'x'
[]
[u_viscosity_rans]
type = INSFVMixingLengthReynoldsStress
variable = vel_x
rho = ${rho}
mixing_length = 'mixing_length'
momentum_component = 'x'
u = vel_x
v = vel_y
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = ${mu}
momentum_component = 'y'
[]
[v_viscosity_rans]
type = INSFVMixingLengthReynoldsStress
variable = vel_y
rho = ${rho}
mixing_length = 'mixing_length'
momentum_component = 'y'
u = vel_x
v = vel_y
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
[]
[scalar_advection]
type = INSFVScalarFieldAdvection
variable = scalar
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
[]
[scalar_diffusion_rans]
type = INSFVMixingLengthScalarDiffusion
variable = scalar
mixing_length = 'mixing_length'
u = vel_x
v = vel_y
schmidt_number = 1.0
[]
[scalar_src]
type = FVBodyForce
variable = scalar
value = 0.1
[]
[]
[AuxKernels]
[mixing_len]
type = WallDistanceMixingLengthAux
walls = 'top bottom'
variable = 'mixing_length'
execute_on = 'initial'
von_karman_const = ${von_karman_const}
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_x
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_y
function = '0'
[]
[inlet_scalar]
type = FVDirichletBC
boundary = 'left'
variable = scalar
value = 1
[]
[wall-u]
type = INSFVNoSlipWallBC
boundary = 'top'
variable = vel_x
function = 0
[]
[wall-v]
type = INSFVNoSlipWallBC
boundary = 'top'
variable = vel_y
function = 0
[]
[sym-u]
type = INSFVSymmetryVelocityBC
boundary = 'bottom'
variable = vel_x
u = vel_x
v = vel_y
mu = 'total_viscosity'
momentum_component = x
[]
[sym-v]
type = INSFVSymmetryVelocityBC
boundary = 'bottom'
variable = vel_y
u = vel_x
v = vel_y
mu = 'total_viscosity'
momentum_component = y
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = '0'
[]
[]
[Materials]
[total_viscosity]
type = MixingLengthTurbulentViscosityMaterial
u = 'vel_x' #computes total viscosity = mu_t + mu
v = 'vel_y' #property is called total_viscosity
mixing_length = 'mixing_length'
mu = ${mu}
rho = ${rho}
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 200 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(test/tests/postprocessors/side_diffusive_flux_average/side_diffusive_flux_average_fv.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
order = CONSTANT
family = MONOMIAL
fv = true
[../]
[]
[FVKernels]
[./diff]
type = FVDiffusion
variable = u
coeff = 1
[../]
[]
[FVBCs]
[./left]
type = FVDirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = FVDirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Materials]
[./mat_props]
type = GenericConstantMaterial
block = 0
prop_names = diffusivity
prop_values = 2
[../]
[./mat_props_bnd]
type = GenericConstantMaterial
boundary = right
prop_names = diffusivity
prop_values = 1
[../]
[]
[Postprocessors]
[./avg_flux_right]
# Computes flux integral on the boundary, which should be -1
type = SideDiffusiveFluxAverage
variable = u
boundary = right
diffusivity = diffusivity
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
nl_abs_tol = 1e-14
nl_rel_tol = 1e-14
l_abs_tol = 1e-14
l_tol = 1e-6
[]
[Outputs]
exodus = true
[]
(test/tests/mesh_modifiers/add_side_sets_from_bounding_box/error_boundary_number.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[createNewSidesetOne]
type = SideSetsFromBoundingBoxGenerator
input = gen
block_id = 0
boundary_id_old = 'right'
boundary_id_new = 11
bottom_left = '0.5 0.5 0'
top_right = '1.9 1.9 0'
[]
[createNewSidesetTwo]
type = SideSetsFromBoundingBoxGenerator
input = createNewSidesetOne
block_id = 0
boundary_id_old = 'left'
boundary_id_new = 10
bottom_left = '-0.1 -0.1 0'
top_right = '0.3 0.3 0'
boundary_id_overlap = true
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[leftBC]
type = DirichletBC
variable = u
boundary = 10
value = 1
[]
[rightBC]
type = DirichletBC
variable = u
boundary = 11
value = 0
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/mortar/continuity-2d-non-conforming/sequencing-stateful-soln-continuity.i)
[Mesh]
second_order = true
[file]
type = FileMeshGenerator
file = nodal_normals_test_offset_nonmatching_gap.e
[]
[./primary]
input = file
type = LowerDBlockFromSidesetGenerator
sidesets = '2'
new_block_id = '20'
[../]
[./secondary]
input = primary
type = LowerDBlockFromSidesetGenerator
sidesets = '1'
new_block_id = '10'
[../]
[]
[Variables]
[./T]
block = '1 2'
order = SECOND
[../]
[./lambda]
block = '10'
[../]
[]
[AuxVariables]
[ssm]
order = CONSTANT
family = MONOMIAL
block = '1 2'
[]
[]
[BCs]
[./neumann]
type = FunctionGradientNeumannBC
exact_solution = exact_soln
variable = T
boundary = '3 4 5 6 7 8'
[../]
[]
[Kernels]
[./conduction]
type = Diffusion
variable = T
block = '1 2'
[../]
[./sink]
type = Reaction
variable = T
block = '1 2'
[../]
[./forcing_function]
type = BodyForce
variable = T
function = forcing_function
block = '1 2'
[../]
[]
[AuxKernels]
[ssm]
type = MaterialRealAux
variable = ssm
property = diffusivity
block = '1 2'
[]
[]
[Materials]
[./ssm]
type = SpatialStatefulMaterial
block = '1 2'
[../]
[]
[Functions]
[./forcing_function]
type = ParsedFunction
value = '-4 + x^2 + y^2'
[../]
[./exact_soln]
type = ParsedFunction
value = 'x^2 + y^2'
[../]
[]
[Debug]
show_var_residual_norms = 1
[]
[Constraints]
[./mortar]
type = EqualValueConstraint
primary_boundary = 2
secondary_boundary = 1
primary_subdomain = 20
secondary_subdomain = 10
variable = lambda
secondary_variable = T
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
solve_type = NEWTON
type = Steady
nl_abs_tol = 1e-12
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_shift_type -pc_factor_shift_amount'
petsc_options_value = 'lu basic NONZERO 1e-15'
num_grids = 2
[]
[Outputs]
exodus = true
[]
[Adaptivity]
steps = 1
marker = uniform
[Markers]
[uniform]
type = UniformMarker
mark = refine
[]
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-rc-action.i)
mu=1.1
rho=1.1
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 10
ymin = -1
ymax = 1
nx = 100
ny = 20
[]
[]
[Modules]
[NavierStokesFV]
compressibility = 'incompressible'
porous_medium_treatment = false
add_energy_equation = false
density = 'rho'
dynamic_viscosity = 'mu'
initial_velocity = '1 1 0'
initial_pressure = 0.0
inlet_boundaries = 'left'
momentum_inlet_types = 'fixed-velocity'
momentum_inlet_function = '1 0'
wall_boundaries = 'top bottom'
momentum_wall_types = 'slip slip'
outlet_boundaries = 'right'
momentum_outlet_types = 'fixed-pressure'
pressure_function = '0'
[]
[]
[Materials]
[const]
type = ADGenericFunctorMaterial
prop_names = 'rho mu'
prop_values = '${rho} ${mu}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[]
(test/tests/postprocessors/element_average_value/elem_pps_multi_block_test.i)
#
# Tests elemental PPS running on multiple block
#
[Mesh]
type = StripeMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 3
ny = 3
elem_type = QUAD4
stripes = 3
# StripeMesh currently only works correctly with ReplicatedMesh.
parallel_type = replicated
[]
[Functions]
[./forcing_fn]
type = ParsedFunction
value = x
[../]
[]
[Variables]
[./u]
family = MONOMIAL
order = CONSTANT
[../]
[]
[Kernels]
[./uv]
type = Reaction
variable = u
[../]
[./fv]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[Postprocessors]
[./avg_1_2]
type = ElementAverageValue
variable = u
block = '0 1'
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
execute_on = 'timestep_end'
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[]
(test/tests/misc/subdomain_setup/mat_prop_block.i)
[Mesh]
[./generator]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 2
[../]
[./subdomain1]
type = SubdomainBoundingBoxGenerator
input = generator
bottom_left = '0 0 0'
top_right = '0.5 0.5 0'
block_id = 1
[../]
[./subdomain2]
type = SubdomainBoundingBoxGenerator
input = subdomain1
bottom_left = '0.5 0 0'
top_right = '1 0.5 0'
block_id = 2
[../]
[./subdomain3]
type = SubdomainBoundingBoxGenerator
input = subdomain2
bottom_left = '0 0.5 0'
top_right = '0.5 1 0'
block_id = 3
[../]
[./subdomain4]
type = SubdomainBoundingBoxGenerator
input = subdomain3
bottom_left = '0.5 0.5 0'
top_right = '1 1 0'
block_id = 4
[../]
[]
[Debug]
show_material_props = true
[]
[Variables]
[./dummy]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./dummy]
type = Diffusion
variable = dummy
[../]
[]
[BCs]
[./dummy_left]
type = DirichletBC
variable = dummy
boundary = left
value = 0
[../]
[./dummy_right]
type = DirichletBC
variable = dummy
boundary = right
value = 1
[../]
[]
[AuxVariables]
[./var1]
family = MONOMIAL
order = CONSTANT
[../]
[./var2]
family = MONOMIAL
order = CONSTANT
[../]
[./var3]
family = MONOMIAL
order = CONSTANT
[../]
[../]
[AuxKernels]
[./var1]
variable = var1
type = MaterialPropertyBlockAux
mat_prop_name = prop1
[../]
[./var2]
variable = var2
type = MaterialPropertyBlockAux
mat_prop_name = prop2
[../]
[./var3]
variable = var3
type = MaterialRealAux
property = prop3
block = '2 3 4'
[../]
[]
[Materials]
[./mat1]
type = GenericConstantMaterial
block = '1 2 4'
prop_names = 'prop1'
prop_values = '0'
[../]
[./mat2]
type = GenericConstantMaterial
block = '2 3 4'
prop_names = 'prop2'
prop_values = '0'
[../]
[./mat3]
type = SubdomainConstantMaterial
block = '2 3 4'
mat_prop_name = 'prop3'
values = '4 2 1'
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/bcs/bc_preset_nodal/bc_function_preset.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
nz = 0
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
[./left]
type = ParsedFunction
value = 'y'
[../]
[./right]
type = ParsedFunction
value = '1+y'
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = FunctionDirichletBC
variable = u
boundary = 3
function = left
[../]
[./right]
type = FunctionDirichletBC
variable = u
boundary = 1
function = right
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = bc_func_out
exodus = true
[]
(test/tests/scaling/residual-based/residual-based.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
[]
[ICs]
[u]
type = FunctionIC
variable = u
function = '1000 * (1 - x)'
[]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[rxn]
type = PReaction
power = 2
variable = u
[]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 1000
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 0
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
verbose = true
automatic_scaling = true
resid_vs_jac_scaling_param = 1
[]
[Outputs]
exodus = true
[]
(test/tests/variables/multiblock_restricted_var/multiblock_restricted_var_test.i)
[Mesh]
file = cake_layers.e
[]
[Variables]
[./v1]
block = 2
[../]
[./v2]
block = 4
[../]
[./w]
[../]
[]
[Kernels]
[./diff_v1]
type = Diffusion
variable = v1
block = 2
[../]
[./diff_v2]
type = Diffusion
variable = v2
block = 4
[../]
[./diff_w]
type = Diffusion
variable = w
[../]
[]
[BCs]
[./left_w]
type = DirichletBC
variable = w
boundary = left
value = 0
[../]
[./right_w]
type = DirichletBC
variable = w
boundary = right
value = 1
[../]
[./left_v1]
type = DirichletBC
variable = v1
boundary = left_bottom
value = 0
[../]
[./right_v1]
type = DirichletBC
variable = v1
boundary = right_bottom
value = 1
[../]
[./left_v2]
type = DirichletBC
variable = v2
boundary = left_top
value = 0
[../]
[./right_v2]
type = DirichletBC
variable = v2
boundary = right_top
value = 1
[../]
[]
[Preconditioning]
[./smp_full]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/meshgenerators/file_mesh_generator/3d_steady_diffusion_iga.i)
[Mesh]
[cyl2d_iga]
type = FileMeshGenerator
file = Cube_With_Sidesets.e
[]
allow_renumbering = false
parallel_type = replicated
[]
[Variables]
[u]
order = SECOND # Must match mesh order
family = RATIONAL_BERNSTEIN
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
block = 0 # Avoid direct calculations on spline nodes
[]
[null]
type = NullKernel
variable = u
block = 1 # Keep kernel coverage check happy
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
vtk = true
[]
(test/tests/markers/boundary_marker/distance.i)
###########################################################
# This is a test of the Mesh Marker System. It marks
# elements with flags indicating whether they should be
# refined, coarsened, or left alone. This system
# has the ability to use the Mesh Indicator System.
#
# @Requirement F2.50
###########################################################
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
# Mesh Marker System
[Adaptivity]
[Markers]
[boundary]
type = BoundaryMarker
next_to = right
distance = 0.35
mark = refine
[]
[]
initial_marker = boundary
initial_steps = 1
[]
[Outputs]
exodus = true
[]
(test/tests/problems/custom_fe_problem/custom_fe_problem_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 4
ny = 4
elem_type = QUAD4
[]
[Problem]
type = MooseTestProblem
name = 'MOOSE Test problem'
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/action/two_block_base_name.i)
[Mesh]
[generated_mesh]
type = GeneratedMeshGenerator
dim = 2
nx = 4
ny = 4
[]
[block1]
type = SubdomainBoundingBoxGenerator
block_id = 1
bottom_left = '0 0 0'
top_right = '0.5 1 0'
input = generated_mesh
[]
[block2]
type = SubdomainBoundingBoxGenerator
block_id = 2
bottom_left = '0.5 0 0'
top_right = '1 1 0'
input = block1
[]
[]
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Modules/TensorMechanics/Master]
# parameters that apply to all subblocks are specified at this level. They
# can be overwritten in the subblocks.
add_variables = true
strain = FINITE
generate_output = 'stress_xx'
# base_name can be specified inside or outside a block
base_name = 'block1'
[./block1]
# the `block` parameter is only valid insde a subblock.
block = 1
[../]
[./block2]
block = 2
# the `additional_generate_output` parameter is also only valid inside a
# subblock. Values specified here are appended to the `generate_output`
# parameter values.
additional_generate_output = 'strain_yy'
base_name = 'block2'
[../]
[]
[AuxVariables]
[./stress_theta]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_theta]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./stress_theta]
type = RankTwoAux
block = 1
rank_two_tensor = block1_stress
index_i = 2
index_j = 2
variable = stress_theta
execute_on = timestep_end
[../]
[./strain_theta]
type = RankTwoAux
block = 2
rank_two_tensor = block2_total_strain
index_i = 2
index_j = 2
variable = strain_theta
execute_on = timestep_end
[../]
[]
[Materials]
[./elasticity_tensor_1]
type = ComputeIsotropicElasticityTensor
block = 1
base_name = block1
youngs_modulus = 1e10
poissons_ratio = 0.345
[../]
[./elasticity_tensor_2]
type = ComputeIsotropicElasticityTensor
block = 2
base_name = block2
youngs_modulus = 1e10
poissons_ratio = 0.345
[../]
[./_elastic_stress1]
type = ComputeFiniteStrainElasticStress
block = 1
base_name = block1
[../]
[./_elastic_stress2]
type = ComputeFiniteStrainElasticStress
block = 2
base_name = block2
[../]
[]
[BCs]
[./left]
type = DirichletBC
boundary = 'left'
variable = disp_x
value = 0.0
[../]
[./top]
type = DirichletBC
boundary = 'top'
variable = disp_y
value = 0.0
[../]
[./right]
type = DirichletBC
boundary = 'right'
variable = disp_x
value = 0.01
[../]
[./bottom]
type = DirichletBC
boundary = 'bottom'
variable = disp_y
value = 0.01
[../]
[]
[Debug]
show_var_residual_norms = true
[]
[Executioner]
type = Steady
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = ' 201 hypre boomeramg 10'
line_search = 'none'
nl_rel_tol = 5e-9
nl_abs_tol = 1e-10
nl_max_its = 15
l_tol = 1e-3
l_max_its = 50
[]
[Outputs]
exodus = true
[]
(test/tests/postprocessors/receiver_default/defaults.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Postprocessors]
[./receiver]
type = Receiver
default = 12345
execute_on = 'timestep_end initial'
[../]
[./report_old]
type = TestPostprocessor
execute_on = 'timestep_end initial'
test_type = report_old
report_name = receiver
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/variables/mixed_order_variables/mixed_order_variables_test.i)
# FIRST order nodal variables on SECOND order grid
#
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 10
ny = 10
elem_type = QUAD9
[]
[Functions]
[./force_fn]
type = ParsedFunction
value = -4
[../]
[./exact_fn]
type = ParsedFunction
value = (x*x)+(y*y)
[../]
[./aux_fn]
type = ParsedFunction
value = (1-x*x)*(1-y*y)
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = force_fn
[../]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
preset = false
boundary = '0 1 2 3'
function = exact_fn
[../]
[]
[AuxVariables]
[./aux1]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./ak1]
type = FunctionAux
variable = aux1
function = aux_fn
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/postprocessors/element_integral_material_property/element_integral_material_property.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmax = 2
ymax = 2
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Materials]
[./mat]
type = GenericConstantMaterial
block = 0
prop_names = prop
prop_values = 2.0
[../]
[]
[Postprocessors]
[./prop_integral]
type = ElementIntegralMaterialProperty
mat_prop = prop
execute_on = 'initial timestep_end'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/richards/test/tests/gravity_head_1/gh03.i)
# unsaturated = false
# gravity = true
# supg = false
# transient = false
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
xmin = -1
xmax = 1
[]
[BCs]
[./left]
type = DirichletBC
boundary = left
value = 1
variable = pressure
[../]
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0E3
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGnone]
type = RichardsSUPGnone
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = RandomIC
block = 0
min = 0
max = 1
[../]
[../]
[]
[Kernels]
active = 'richardsf'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGnone
sat_UO = Saturation
seff_UO = SeffVG
viscosity = 1E-3
gravity = '-1 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = gh03
exodus = true
[]
(test/tests/quadrature/order/elem5_side7.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
nz = 0
elem_type = QUAD4
[]
[Postprocessors]
[./numsideqps]
type = NumSideQPs
boundary = 0
[../]
[./numelemqps]
type = NumElemQPs
block = 0
[../]
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
[./Quadrature]
order = third
element_order = fifth
side_order = seventh
[]
[]
[Outputs]
execute_on = 'timestep_end'
exodus = false
csv = true
[]
(test/tests/misc/check_error/bad_kernel_var_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = foo # Test for missing variable
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/ray_tracing/test/tests/userobjects/ray_tracing_study/kernel_create_ray/kernel_create_ray.i)
[Mesh]
active = gmg_2d
[gmg_2d]
type = GeneratedMeshGenerator
dim = 2
nx = 3
ny = 3
xmax = 3
ymax = 3
[]
[gmg_3d]
type = GeneratedMeshGenerator
dim = 3
nx = 3
ny = 3
nz = 3
xmax = 3
ymax = 3
zmax = 3
[]
[]
[RayBCs]
active = kill_2d
[kill_2d]
type = KillRayBC
boundary = 'top right bottom left'
[]
[kill_3d]
type = KillRayBC
boundary = 'top right bottom left front back'
[]
[]
[RayKernels/create_ray]
type = CreateRayRayKernelTest
[]
[UserObjects/lots]
type = LotsOfRaysRayStudy
execute_on = initial
vertex_to_vertex = true
centroid_to_vertex = true
centroid_to_centroid = true
[]
[Postprocessors]
[total_distance]
type = RayTracingStudyResult
study = lots
result = total_distance
[]
[total_rays_started]
type = RayTracingStudyResult
study = lots
result = total_rays_started
[]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Outputs]
exodus = false
csv = true
[]
(test/tests/auxkernels/volume_aux/element.i)
[Mesh]
[cmg]
type = CartesianMeshGenerator
dim = 2
dx = '1.5 2.4 0.1'
dy = '1.3 0.9'
ix = '2 1 1'
iy = '2 3'
[]
[]
[AuxVariables/volume]
order = CONSTANT
family = MONOMIAL
[]
[AuxKernels/volume_aux]
type = VolumeAux
variable = volume
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/pressure_channel/open_bc_pressure_BC_fieldSplit.i)
# This input file tests Dirichlet pressure in/outflow boundary conditions for the incompressible NS equations.
[GlobalParams]
gravity = '0 0 0'
[]
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 3.0
ymin = 0
ymax = 1.0
nx = 30
ny = 10
elem_type = QUAD9
[]
[Variables]
[./vel_x]
order = SECOND
family = LAGRANGE
[../]
[./vel_y]
order = SECOND
family = LAGRANGE
[../]
[./p]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./mass]
type = INSMass
variable = p
u = vel_x
v = vel_y
pressure = p
[../]
[./x_momentum_space]
type = INSMomentumLaplaceForm
variable = vel_x
u = vel_x
v = vel_y
pressure = p
component = 0
integrate_p_by_parts = false
[../]
[./y_momentum_space]
type = INSMomentumLaplaceForm
variable = vel_y
u = vel_x
v = vel_y
pressure = p
component = 1
integrate_p_by_parts = false
[../]
[]
[BCs]
[./x_no_slip]
type = DirichletBC
variable = vel_x
boundary = 'top bottom'
value = 0.0
[../]
[./y_no_slip]
type = DirichletBC
variable = vel_y
boundary = 'left top bottom'
value = 0.0
[../]
[./inlet_p]
type = DirichletBC
variable = p
boundary = left
value = 1.0
[../]
[./outlet_p]
type = DirichletBC
variable = p
boundary = right
value = 0.0
[../]
[]
[Materials]
[./const]
type = GenericConstantMaterial
block = 0
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[]
[Preconditioning]
active = FSP
[./FSP]
type = FSP
# It is the starting point of splitting
topsplit = 'up' # 'up' should match the following block name
[./up]
splitting = 'u p' # 'u' and 'p' are the names of subsolvers
splitting_type = schur
# Splitting type is set as schur, because the pressure part of Stokes-like systems
# is not diagonally dominant. CAN NOT use additive, multiplicative and etc.
# Original system:
# | A B | | u | = | f_u |
# | C 0 | | p | | f_v |
# is factorized into
# |I 0 | | A 0| | I A^{-1}B | | u | = | f_u |
# |CA^{-1} I | | 0 -S| | 0 I | | p | | f_v |
# S = CA^{-1}B
# The preconditioning is accomplished via the following steps
# (1) p^{(0)} = f_v - CA^{-1}f_u,
# (2) pressure = (-S)^{-1} p^{(0)}
# (3) u = A^{-1}(f_u-Bp)
petsc_options_iname = '-pc_fieldsplit_schur_fact_type -pc_fieldsplit_schur_precondition'
petsc_options_value = 'full selfp'
# Factorization type here is full, which means we approximate the original system
# exactly. There are three other options:
# diag:
# | A 0|
# | 0 -S|
# lower:
# |I 0 |
# |CA^{-1} -S |
# upper:
# | I A^{-1}B |
# | 0 -S |
# The preconditioning matrix is set as selfp, which means we explicitly form a
# matrix \hat{S} = C(diag(A))^{-1}B. We do not compute the inverse of A, but instead, we compute
# the inverse of diag(A).
[../]
[./u]
vars = 'vel_x vel_y'
# PETSc options for this subsolver
# A prefix will be applied, so just put the options for this subsolver only
petsc_options_iname = '-pc_type -ksp_type -ksp_rtol'
petsc_options_value = ' hypre gmres 1e-4'
# Specify options to solve A^{-1} in the steps (1), (2) and (3).
# Solvers for A^{-1} could be different in different steps. We could
# choose in the following pressure block.
[../]
[./p]
vars = 'p'
# PETSc options for this subsolver in the step (2)
petsc_options_iname = '-pc_type -ksp_type -ksp_rtol'
petsc_options_value = ' jacobi gmres 1e-4'
# Use -inner_ksp_type and -inner_pc_type to override A^{-1} in the step (2)
# Use -lower_ksp_type and -lower_pc_type to override A^{-1} in the step (1)
[../]
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
nl_rel_tol = 1e-12
nl_max_its = 6
l_tol = 1e-6
l_max_its = 300
[]
[Outputs]
file_base = open_bc_out_pressure_BC_fieldSplit
exodus = true
[]
(modules/ray_tracing/test/tests/raytracing/ray/ray_lots.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 4
ny = 4
[]
[]
[RayBCs/kill]
type = KillRayBC
boundary = 'top right bottom left'
study = study
[]
[UserObjects]
[study]
type = TestRayLots
execute_on = initial
vertex_to_vertex = true
centroid_to_vertex = true
centroid_to_centroid = true
side_aq = true
centroid_aq = true
ray_kernel_coverage_check = false
[]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
(test/tests/misc/check_error/unused_param_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
unused_param = 'set_something_important'
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
[]
(modules/porous_flow/test/tests/thm_rehbinder/fixed_outer_rz.i)
# A version of fixed_outer.i that uses the RZ cylindrical coordinate system
[Mesh]
type = GeneratedMesh
dim = 2
nx = 40 # this is the r direction
ny = 1 # this is the height direction
xmin = 0.1
xmax = 1
bias_x = 1.1
ymin = 0.0
ymax = 1.0
[]
[Problem]
coord_type = RZ
[]
[GlobalParams]
displacements = 'disp_r disp_z'
PorousFlowDictator = dictator
biot_coefficient = 1.0
[]
[Variables]
[disp_r]
[]
[disp_z]
[]
[porepressure]
[]
[temperature]
[]
[]
[BCs]
[plane_strain]
type = DirichletBC
variable = disp_z
value = 0
boundary = 'top bottom'
[]
[cavity_temperature]
type = DirichletBC
variable = temperature
value = 1000
boundary = left
[]
[cavity_porepressure]
type = DirichletBC
variable = porepressure
value = 1E6
boundary = left
[]
[cavity_zero_effective_stress_x]
type = Pressure
variable = disp_r
function = 1E6
boundary = left
use_displaced_mesh = false
[]
[outer_temperature]
type = DirichletBC
variable = temperature
value = 0
boundary = right
[]
[outer_pressure]
type = DirichletBC
variable = porepressure
value = 0
boundary = right
[]
[fixed_outer_disp]
type = DirichletBC
variable = disp_r
value = 0
boundary = right
[]
[]
[AuxVariables]
[stress_rr]
family = MONOMIAL
order = CONSTANT
[]
[stress_pp]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[stress_rr]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_rr
index_i = 0
index_j = 0
[]
[stress_pp] # hoop stress
type = RankTwoAux
rank_two_tensor = stress
variable = stress_pp
index_i = 2
index_j = 2
[]
[]
[Modules]
[FluidProperties]
[the_simple_fluid]
type = SimpleFluidProperties
thermal_expansion = 0.0
bulk_modulus = 1E12
viscosity = 1.0E-3
density0 = 1000.0
cv = 1000.0
cp = 1000.0
porepressure_coefficient = 0.0
[]
[]
[]
[PorousFlowBasicTHM]
coupling_type = ThermoHydroMechanical
multiply_by_density = false
add_stress_aux = true
porepressure = porepressure
temperature = temperature
eigenstrain_names = thermal_contribution
gravity = '0 0 0'
fp = the_simple_fluid
[]
[Materials]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1E10
poissons_ratio = 0.2
[]
[strain]
type = ComputeAxisymmetricRZSmallStrain
eigenstrain_names = thermal_contribution
[]
[thermal_contribution]
type = ComputeThermalExpansionEigenstrain
temperature = temperature
thermal_expansion_coeff = 1E-6
eigenstrain_name = thermal_contribution
stress_free_temperature = 0.0
[]
[stress]
type = ComputeLinearElasticStress
[]
[porosity]
type = PorousFlowPorosityConst # only the initial value of this is ever used
porosity = 0.1
[]
[biot_modulus]
type = PorousFlowConstantBiotModulus
solid_bulk_compliance = 1E-10
fluid_bulk_modulus = 1E12
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1E-12 0 0 0 1E-12 0 0 0 1E-12' # note this is ordered: rr, zz, angle-angle
[]
[thermal_expansion]
type = PorousFlowConstantThermalExpansionCoefficient
fluid_coefficient = 1E-6
drained_coefficient = 1E-6
[]
[thermal_conductivity]
type = PorousFlowThermalConductivityIdeal
dry_thermal_conductivity = '1E6 0 0 0 1E6 0 0 0 1E6' # note this is ordered: rr, zz, angle-angle
[]
[]
[VectorPostprocessors]
[P]
type = LineValueSampler
start_point = '0.1 0 0'
end_point = '1.0 0 0'
num_points = 10
sort_by = x
variable = porepressure
[]
[T]
type = LineValueSampler
start_point = '0.1 0 0'
end_point = '1.0 0 0'
num_points = 10
sort_by = x
variable = temperature
[]
[U]
type = LineValueSampler
start_point = '0.1 0 0'
end_point = '1.0 0 0'
num_points = 10
sort_by = x
variable = disp_r
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -snes_rtol'
petsc_options_value = 'gmres asm lu 1E-8'
[]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
file_base = fixed_outer_rz
execute_on = timestep_end
csv = true
[]
(test/tests/outputs/error/duplicate_outputs.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[./exodus]
type = Exodus
[../]
[]
(examples/ex01_inputfile/ex01.i)
[Mesh]
# We use a pre-generated mesh file (in exodus format).
# This mesh file has 'top' and 'bottom' named boundaries defined inside it.
file = mug.e
[]
[Variables]
[./diffused]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = diffused
[../]
[]
[BCs]
[./bottom] # arbitrary user-chosen name
type = DirichletBC
variable = diffused
boundary = 'bottom' # This must match a named boundary in the mesh file
value = 1
[../]
[./top] # arbitrary user-chosen name
type = DirichletBC
variable = diffused
boundary = 'top' # This must match a named boundary in the mesh file
value = 0
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/2d-rc.i)
mu=1.1
rho=1.1
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 5
ymin = 0
ymax = 1
nx = 20
ny = 10
[]
[]
[GlobalParams]
advected_interp_method='average'
velocity_interp_method='rc'
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = PINSFVRhieChowInterpolator
u = superficial_vel_x
v = superficial_vel_y
pressure = pressure
porosity = porosity
[]
[]
[Variables]
inactive = 'lambda'
[superficial_vel_x]
type = PINSFVSuperficialVelocityVariable
initial_condition = 1
[]
[superficial_vel_y]
type = PINSFVSuperficialVelocityVariable
initial_condition = 1e-6
[]
[pressure]
type = INSFVPressureVariable
[]
[lambda]
family = SCALAR
order = FIRST
[]
[]
[AuxVariables]
[porosity]
family = MONOMIAL
order = CONSTANT
fv = true
initial_condition = 0.5
[]
[]
[FVKernels]
inactive = 'mean-pressure'
[mass]
type = PINSFVMassAdvection
variable = pressure
rho = ${rho}
[]
[u_advection]
type = PINSFVMomentumAdvection
variable = superficial_vel_x
rho = ${rho}
porosity = porosity
momentum_component = 'x'
[]
[u_viscosity]
type = PINSFVMomentumDiffusion
variable = superficial_vel_x
mu = ${mu}
porosity = porosity
momentum_component = 'x'
[]
[u_pressure]
type = PINSFVMomentumPressure
variable = superficial_vel_x
momentum_component = 'x'
pressure = pressure
porosity = porosity
[]
[v_advection]
type = PINSFVMomentumAdvection
variable = superficial_vel_y
rho = ${rho}
porosity = porosity
momentum_component = 'y'
[]
[v_viscosity]
type = PINSFVMomentumDiffusion
variable = superficial_vel_y
mu = ${mu}
porosity = porosity
momentum_component = 'y'
[]
[v_pressure]
type = PINSFVMomentumPressure
variable = superficial_vel_y
momentum_component = 'y'
pressure = pressure
porosity = porosity
[]
[mean-pressure]
type = FVScalarLagrangeMultiplier
variable = pressure
lambda = lambda
phi0 = 0.01
[]
[]
[FVBCs]
# Select desired boundary conditions
active = 'inlet-u inlet-v outlet-p free-slip-u free-slip-v'
# Possible inlet boundary conditions
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = superficial_vel_x
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = superficial_vel_y
function = 0
[]
[inlet-p]
type = INSFVOutletPressureBC
boundary = 'left'
variable = pressure
function = 1
[]
# Possible wall boundary conditions
[free-slip-u]
type = INSFVNaturalFreeSlipBC
boundary = 'top bottom'
variable = superficial_vel_x
momentum_component = 'x'
[]
[free-slip-v]
type = INSFVNaturalFreeSlipBC
boundary = 'top bottom'
variable = superficial_vel_y
momentum_component = 'y'
[]
[no-slip-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = superficial_vel_x
function = 0
[]
[no-slip-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = superficial_vel_y
function = 0
[]
[symmetry-u]
type = PINSFVSymmetryVelocityBC
boundary = 'bottom'
variable = superficial_vel_x
u = superficial_vel_x
v = superficial_vel_y
mu = ${mu}
momentum_component = 'x'
[]
[symmetry-v]
type = PINSFVSymmetryVelocityBC
boundary = 'bottom'
variable = superficial_vel_y
u = superficial_vel_x
v = superficial_vel_y
mu = ${mu}
momentum_component = 'y'
[]
[symmetry-p]
type = INSFVSymmetryPressureBC
boundary = 'bottom'
variable = pressure
[]
# Possible outlet boundary conditions
[outlet-p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 0
[]
[outlet-p-novalue]
type = INSFVMassAdvectionOutflowBC
boundary = 'right'
variable = pressure
u = superficial_vel_x
v = superficial_vel_y
rho = ${rho}
[]
[outlet-u]
type = PINSFVMomentumAdvectionOutflowBC
boundary = 'right'
variable = superficial_vel_x
u = superficial_vel_x
v = superficial_vel_y
porosity = porosity
momentum_component = 'x'
rho = ${rho}
[]
[outlet-v]
type = PINSFVMomentumAdvectionOutflowBC
boundary = 'right'
variable = superficial_vel_y
u = superficial_vel_x
v = superficial_vel_y
porosity = porosity
momentum_component = 'y'
rho = ${rho}
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 200 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-11
nl_abs_tol = 1e-14
[]
# Some basic Postprocessors to visually examine the solution
[Postprocessors]
[inlet-p]
type = SideIntegralVariablePostprocessor
variable = pressure
boundary = 'left'
[]
[outlet-u]
type = SideIntegralVariablePostprocessor
variable = superficial_vel_x
boundary = 'right'
[]
[]
[Outputs]
exodus = true
[]
(modules/phase_field/test/tests/misc/coupled_value_function_ic.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[]
# Here we sum up the inverses of the ICs above. This should add up to 2.0 everywhere
[Functions]
[map]
type = ParsedFunction
value = 'x^2+y^3+log(z)+acos(t)'
[]
[]
[Variables]
[out]
[InitialCondition]
type = CoupledValueFunctionIC
function = map
v = 'v1 v2 a3 a4'
[]
[]
[v1]
[InitialCondition]
type = FunctionIC
function = x^(1/2)
[]
[]
[v2]
[InitialCondition]
type = FunctionIC
function = y^(1/3)
[]
[]
[]
[AuxVariables]
[a3]
[InitialCondition]
type = FunctionIC
function = exp(1-x)
[]
[]
[a4]
[InitialCondition]
type = FunctionIC
function = cos(1-y)
[]
[]
[]
[Postprocessors]
[out_min]
type = ElementExtremeValue
variable = out
value_type = min
[]
[out_max]
type = ElementExtremeValue
variable = out
value_type = max
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
execute_on = 'FINAL'
csv = true
[]
(test/tests/interfacekernels/ad_coupled_vector_value/coupled.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 20
xmax = 2
[]
[./subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '1.0 0 0'
block_id = 1
top_right = '2.0 1.0 0'
[../]
[./interface]
input = subdomain1
type = SideSetsBetweenSubdomainsGenerator
primary_block = '0'
paired_block = '1'
new_boundary = 'primary0_interface'
[../]
[]
[Variables]
[./u]
block = '0'
family = LAGRANGE_VEC
[../]
[./v]
block = '1'
family = LAGRANGE_VEC
[../]
[w]
family = LAGRANGE_VEC
[]
[]
[Kernels]
[./diff_u]
type = VectorDiffusion
variable = u
block = 0
[../]
[./diff_v]
type = VectorDiffusion
variable = v
block = 1
[../]
[diff_w]
type = VectorDiffusion
variable = w
[]
[]
[InterfaceKernels]
[./interface]
type = ADVectorCoupledInterfacialSource
variable = u
neighbor_var = v
var_source = w
boundary = primary0_interface
D = 1
D_neighbor = 1
[../]
[]
[BCs]
[./left]
type = VectorDirichletBC
variable = u
boundary = 'left'
values = '0 0 0'
[../]
[./right]
type = VectorDirichletBC
variable = v
boundary = 'right'
values = '10 0 0'
[../]
[./middle]
type = ADVectorMatchedValueBC
variable = v
boundary = 'primary0_interface'
v = u
[../]
[w_left]
type = VectorDirichletBC
variable = w
boundary = 'left'
values = '0 0 0'
[]
[w_right]
type = VectorDirichletBC
variable = w
boundary = 'right'
values = '4 0 0'
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(test/tests/preconditioners/pbp/pbp_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
# init_unif_refine = 6
[]
[Variables]
active = 'u v'
[./u]
order = FIRST
family = LAGRANGE
[../]
[./v]
order = FIRST
family = LAGRANGE
[../]
[]
[Preconditioning]
[./PBP]
type = PBP
solve_order = 'u v'
preconditioner = 'LU LU'
off_diag_row = 'v'
off_diag_column = 'u'
petsc_options = '' # Test petsc options in PBP block
[../]
[]
[Problem]
type = FEProblem
error_on_jacobian_nonzero_reallocation = true
[]
[Kernels]
active = 'diff_u conv_v diff_v'
[./diff_u]
type = Diffusion
variable = u
[../]
[./conv_v]
type = CoupledForce
variable = v
v = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[BCs]
active = 'left_u right_u left_v'
[./left_u]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 100
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = 3
value = 0
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Steady
l_max_its = 10
nl_max_its = 10
solve_type = JFNK
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/porous_flow/test/tests/gravity/fully_saturated_grav01b.i)
# Checking that gravity head is established
# 1phase, constant and large fluid-bulk, constant viscosity, constant permeability
# fully saturated with fully-saturated Kernel
# For better agreement with the analytical solution (ana_pp), just increase nx
[Mesh]
type = GeneratedMesh
dim = 1
nx = 100
xmin = -1
xmax = 0
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Variables]
[pp]
[InitialCondition]
type = RandomIC
min = 0
max = 1
[]
[]
[]
[Kernels]
[flux0]
type = PorousFlowFullySaturatedDarcyBase
variable = pp
gravity = '-1 0 0'
[]
[]
[Functions]
[ana_pp]
type = ParsedFunction
vars = 'g B p0 rho0'
vals = '1 1E3 0 1'
value = '-B*log(exp(-p0/B)+g*rho0*x/B)' # expected pp at base
[]
[]
[BCs]
[z]
type = DirichletBC
variable = pp
boundary = right
value = 0
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 1e3
density0 = 1
viscosity = 1
thermal_expansion = 0
[]
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow1PhaseFullySaturated
porepressure = pp
[]
[massfrac]
type = PorousFlowMassFraction
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1 0 0 0 2 0 0 0 3'
[]
[]
[Postprocessors]
[pp_base]
type = PointValue
variable = pp
point = '-1 0 0'
[]
[pp_analytical]
type = FunctionValuePostprocessor
function = ana_pp
point = '-1 0 0'
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = fully_saturated_grav01b
[csv]
type = CSV
[]
[]
(test/tests/bcs/ad_function_dirichlet_bc/test.i)
###########################################################
# This is a test of Boundary Condition System. The
# FunctionDirichletBC is used to contribute the residuals
# to the boundary term operators in the weak form.
#
# @Requirement F3.40
###########################################################
[Mesh]
[./square]
type = GeneratedMeshGenerator
dim = 2
nx = 32
ny = 32
[../]
[]
[Variables]
[./u]
[../]
[]
[Functions]
[./ff_1]
type = ParsedFunction
value = alpha*alpha*pi
vars = 'alpha'
vals = '16'
[../]
[./ff_2]
type = ParsedFunction
value = pi*sin(alpha*pi*x)
vars = 'alpha'
vals = '16'
[../]
[./forcing_func]
type = CompositeFunction
functions = 'ff_1 ff_2'
[../]
[./bc_func]
type = ParsedFunction
value = sin(alpha*pi*x)
vars = 'alpha'
vals = '16'
[../]
[]
[Kernels]
[./diff]
type = ADDiffusion
variable = u
[../]
[./forcing]
type = ADBodyForce
variable = u
function = forcing_func
[../]
[]
[BCs]
[./all]
type = ADFunctionDirichletBC
variable = u
boundary = 'left right'
function = bc_func
[../]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-12
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(modules/porous_flow/test/tests/capillary_pressure/vangenuchten1.i)
# Test van Genuchten relative permeability curve by varying saturation over the mesh
# van Genuchten exponent m = 0.5 for both phases
# No residual saturation in either phase
[Mesh]
type = GeneratedMesh
dim = 1
nx = 500
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Variables]
[p0]
initial_condition = 1e6
[]
[s1]
[]
[]
[AuxVariables]
[s0aux]
family = MONOMIAL
order = CONSTANT
[]
[s1aux]
family = MONOMIAL
order = CONSTANT
[]
[p0aux]
family = MONOMIAL
order = CONSTANT
[]
[p1aux]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[s0]
type = PorousFlowPropertyAux
property = saturation
phase = 0
variable = s0aux
[]
[s1]
type = PorousFlowPropertyAux
property = saturation
phase = 1
variable = s1aux
[]
[p0]
type = PorousFlowPropertyAux
property = pressure
phase = 0
variable = p0aux
[]
[p1]
type = PorousFlowPropertyAux
property = pressure
phase = 1
variable = p1aux
[]
[]
[Functions]
[s1]
type = ParsedFunction
value = x
[]
[]
[ICs]
[s1]
type = FunctionIC
variable = s1
function = s1
[]
[]
[Kernels]
[p0]
type = Diffusion
variable = p0
[]
[s1]
type = Diffusion
variable = s1
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'p0 s1'
number_fluid_phases = 2
number_fluid_components = 2
[]
[pc]
type = PorousFlowCapillaryPressureVG
alpha = 1e-5
m = 0.5
sat_lr = 0.1
log_extension = false
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow2PhasePS
phase0_porepressure = p0
phase1_saturation = s1
capillary_pressure = pc
[]
[kr0]
type = PorousFlowRelativePermeabilityVG
phase = 0
m = 0.5
[]
[kr1]
type = PorousFlowRelativePermeabilityCorey
phase = 1
n = 2
[]
[]
[VectorPostprocessors]
[vpp]
type = LineValueSampler
variable = 's0aux s1aux p0aux p1aux'
start_point = '0 0 0'
end_point = '1 0 0'
num_points = 500
sort_by = id
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
nl_abs_tol = 1e-6
[]
[BCs]
[sleft]
type = DirichletBC
variable = s1
value = 0
boundary = left
[]
[sright]
type = DirichletBC
variable = s1
value = 1
boundary = right
[]
[]
[Outputs]
csv = true
execute_on = timestep_end
[]
(test/tests/materials/boundary_material/bnd_coupling_vol.i)
#
# Coupling volumetric material property inside boundary restricted material
# Also bringing boundary restricted material inside another boundary restricted
# material
#
# Solving: k \Laplace u + u - f = 0
#
# u = x^2 + y^2
# k = 3, but is decomposed as k3vol = k1vol + k2vol, where k1vol = 1 and k2vol = 2
#
# Boundary material property is computed as k3bnd = k1vol + k2bnd
#
# The material properties with suffix `vol` are volumetric, the ones with suffix `bnd`
# are boundary restricted
#
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 4
ny = 4
elem_type = QUAD9
[]
[Functions]
[./exact_fn]
type = ParsedFunction
value = x*x+y*y
[../]
[./f_fn]
type = ParsedFunction
value = -4*3+x*x+y*y
[../]
[]
[Variables]
[./u]
family = LAGRANGE
order = SECOND
[../]
[]
[Kernels]
[./diff]
type = DiffMKernel
variable = u
offset = 0
mat_prop = k3vol
[../]
[./r]
type = Reaction
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = f_fn
[../]
[]
[BCs]
[./all]
type = MatDivergenceBC
variable = u
prop_name = k3bnd
boundary = 'left right top bottom'
[../]
[]
[Materials]
[./k1vol]
type = GenericConstantMaterial
prop_names = 'k1vol'
prop_values = 1
block = 0
[../]
[./k2vol]
type = GenericConstantMaterial
prop_names = 'k2vol'
prop_values = 2
block = 0
[../]
[./k2bnd]
type = GenericConstantMaterial
prop_names = 'k2bnd'
prop_values = 2
boundary = 'left right top bottom'
[../]
[./k3vol]
type = SumMaterial
sum_prop_name = k3vol
mp1 = k1vol
mp2 = k2vol
block = 0
val1 = 1
val2 = 2
[../]
[./k3bnd]
type = SumMaterial
sum_prop_name = 'k3bnd'
mp1 = k1vol
mp2 = k2bnd
boundary = 'left right top bottom'
val1 = 1
val2 = 2
[../]
[]
[Postprocessors]
[./l2err]
type = ElementL2Error
variable = u
function = exact_fn
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(test/tests/variables/coupled_scalar/coupled_scalar.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./aux_scalar]
order = SECOND
family = SCALAR
[../]
[./coupled]
[../]
[./coupled_1]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./coupled]
type = CoupledScalarAux
variable = coupled
coupled = aux_scalar
[../]
[./coupled_1]
# Coupling to the "1" component of an aux scalar
type = CoupledScalarAux
variable = coupled_1
component = 1
coupled = aux_scalar
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
[ICs]
[./aux_scalar_ic]
variable = aux_scalar
values = '1.2 4.3'
type = ScalarComponentIC
[../]
[]
(test/tests/vectorpostprocessors/elements_along_plane/3d.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 10
ny = 10
nz = 10
# Our CSV diffs here depend on a fixed element id numbering
allow_renumbering = false
parallel_type = replicated
[]
[Problem]
solve = false
[]
[VectorPostprocessors]
[./elems]
type = ElementsAlongPlane
point = '0.525 0.525 0.0'
normal = '1.0 1.0 0.0'
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
[]
(modules/tensor_mechanics/examples/bridge/bridge.i)
#
# Bridge linear elasticity example
#
# This example models a bridge using linear elasticity.
# It can be either steel or concrete.
# Gravity is applied
# A pressure of 0.5 MPa is also applied
#
[Mesh]
displacements = 'disp_x disp_y disp_z' #Define displacements for deformed mesh
type = FileMesh #Read in mesh from file
file = bridge.e
boundary_id = '1 2 3 4 5 6' #Assign names to boundaries to make things clearer
boundary_name = 'top left right bottom1 bottom2 bottom3'
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./gravity_y]
#Gravity is applied to bridge
type = Gravity
variable = disp_y
value = -9.81
[../]
[./TensorMechanics]
#Stress divergence kernels
displacements = 'disp_x disp_y disp_z'
[../]
[]
[AuxVariables]
[./von_mises]
#Dependent variable used to visualize the Von Mises stress
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./von_mises_kernel]
#Calculates the von mises stress and assigns it to von_mises
type = RankTwoScalarAux
variable = von_mises
rank_two_tensor = stress
execute_on = timestep_end
scalar_type = VonMisesStress
[../]
[]
[BCs]
[./Pressure]
[./load]
#Applies the pressure
boundary = top
factor = 5e5 # Pa
[../]
[../]
[./anchor_x]
#Anchors the bottom and sides against deformation in the x-direction
type = DirichletBC
variable = disp_x
boundary = 'left right bottom1 bottom2 bottom3'
value = 0.0
[../]
[./anchor_y]
#Anchors the bottom and sides against deformation in the y-direction
type = DirichletBC
variable = disp_y
boundary = 'left right bottom1 bottom2 bottom3'
value = 0.0
[../]
[./anchor_z]
#Anchors the bottom and sides against deformation in the z-direction
type = DirichletBC
variable = disp_z
boundary = 'left right bottom1 bottom2 bottom3'
value = 0.0
[../]
[]
[Materials]
active = 'density_concrete stress strain elasticity_tensor_concrete'
[./elasticity_tensor_steel]
#Creates the elasticity tensor using steel parameters
youngs_modulus = 210e9 #Pa
poissons_ratio = 0.3
type = ComputeIsotropicElasticityTensor
block = 1
[../]
[./elasticity_tensor_concrete]
#Creates the elasticity tensor using concrete parameters
youngs_modulus = 16.5e9 #Pa
poissons_ratio = 0.2
type = ComputeIsotropicElasticityTensor
block = 1
[../]
[./strain]
#Computes the strain, assuming small strains
type = ComputeSmallStrain
block = 1
displacements = 'disp_x disp_y disp_z'
[../]
[./stress]
#Computes the stress, using linear elasticity
type = ComputeLinearElasticStress
block = 1
[../]
[./density_steel]
#Defines the density of steel
type = GenericConstantMaterial
block = 1
prop_names = density
prop_values = 7850 # kg/m^3
[../]
[./density_concrete]
#Defines the density of concrete
type = GenericConstantMaterial
block = 1
prop_names = density
prop_values = 2400 # kg/m^3
[../]
[]
[Preconditioning]
[./SMP]
#Creates the entire Jacobian, for the Newton solve
type = SMP
full = true
[../]
[]
[Executioner]
#We solve a steady state problem using Newton's iteration
type = Steady
solve_type = NEWTON
nl_rel_tol = 1e-9
l_max_its = 30
l_tol = 1e-4
nl_max_its = 10
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart'
petsc_options_value = 'hypre boomeramg 31'
[]
[Outputs]
exodus = true
perf_graph = true
[]
(test/tests/utils/perf_graph/perf_graph.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
[]
[]
[UserObjects/test]
type = PerfGraphTest
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
(test/tests/misc/check_error/bad_kernel_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
# Test for bad kernel
[./diff]
type = Foo
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/meshgenerators/combiner_generator/combiner_merge_names.i)
[Mesh]
[Top_Block]
type = GeneratedMeshGenerator
dim = 3
nx = 10
ny = 10
nz = 10
xmax = 2
ymax = 2
zmax = 2
xmin = 0
ymin = 0
zmin = 1
boundary_name_prefix = 'Upper'
boundary_id_offset = 10
[]
[Bottom_Block]
type = GeneratedMeshGenerator
dim = 3
nx = 10
ny = 10
nz = 10
xmax = 2
ymax = 2
zmax = 1
boundary_name_prefix = 'Lower'
[]
[Combine]
type = CombinerGenerator
inputs = 'Top_Block Bottom_Block'
positions = '0 0 0 0.12 0.12 0'
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/ics/from_exodus_solution/elem_part2.i)
# Use the exodus file for restarting the problem:
# - restart elemental aux variable
[Mesh]
[fmg]
type = FileMeshGenerator
file = elem_part1_out.e
use_for_exodus_restart = true
[]
# This problem uses ExodusII_IO::copy_elemental_solution(), which only
# works with ReplicatedMesh
parallel_type = replicated
[]
[Functions]
[./exact_fn]
type = ParsedFunction
value = ((x*x)+(y*y))
[../]
[./forcing_fn]
type = ParsedFunction
value = -4
[../]
[]
[AuxVariables]
[./e]
order = CONSTANT
family = MONOMIAL
initial_from_file_var = e
initial_from_file_timestep = 6
[../]
[]
[AuxKernels]
[./ak]
type = SelfAux
variable = e
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
boundary = '0 1 2 3'
function = exact_fn
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/nodal_material_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 4
ny = 4
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
# Nodal Auxvariable that tries to access a material property
[AuxVariables]
active = 'mat'
[./mat]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = MatDiffusionTest
variable = u
prop_name = matp
[../]
[]
[AuxKernels]
active = 'mat'
[./mat]
type = MaterialRealAux
variable = mat
property = matp
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[./right]
type = MTBC
variable = u
boundary = 1
grad = 8
prop_name = matp
[../]
[]
[Materials]
active = mat
[./mat]
type = MTMaterial
block = 0
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/constraints/coupled_tied_value_constraint/coupled_tied_value_constraint.i)
[Mesh]
type = FileMesh
file = split_blocks.e
# NearestNodeLocator, which is needed by CoupledTiedValueConstraint,
# only works with ReplicatedMesh currently
parallel_type = replicated
[]
[Variables]
[./u]
block = left
[../]
[./v]
block = right
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
block = left
[../]
[./diff_v]
type = Diffusion
variable = v
block = right
[../]
[]
[BCs]
active = 'right left'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = v
boundary = 4
value = 1
[../]
[]
[Constraints]
[./value]
type = CoupledTiedValueConstraint
variable = u
secondary = 2
primary = 3
primary_variable = v
[../]
[]
[Preconditioning]
active = 'SMP'
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
l_max_its = 100
nl_max_its = 2
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/auxkernels/ghosting_aux/ghosting_aux.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[Partitioner]
type = GridPartitioner
nx = 2
ny = 2
[]
output_ghosting = true
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[AuxVariables]
[pid]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[pid]
type = ProcessorIDAux
variable = pid
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
[Problem]
default_ghosting = true
[]
(test/tests/mesh/no_mesh_block/no_mesh_block.i)
# No Mesh Block!
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[leftBC]
type = DirichletBC
variable = u
boundary = 10
value = 1
[]
[rightBC]
type = DirichletBC
variable = u
boundary = 11
value = 0
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/code_verification/cartesian_test_no2.i)
# Problem I.2
#
# An infinite plate with a thermal conductivity that varies linearly with
# temperature. Each boundary is exposed to a constant temperature.
#
# REFERENCE:
# A. Toptan, et al. (Mar.2020). Tech. rep. CASL-U-2020-1939-000, SAND2020-3887 R. DOI:10.2172/1614683.
[Mesh]
[./geom]
type = GeneratedMeshGenerator
dim = 1
elem_type = EDGE2
nx = 1
[../]
[]
[Variables]
[./u]
order = FIRST
[../]
[]
[Functions]
[./exact]
type = ParsedFunction
vars = 'L beta ki ko ui uo'
vals = '1 1e-3 5.3 5 300 0'
value = 'uo+(ko/beta)* ( (1 + L*beta*(ki+ko)*(ui-uo)*((L-x)/(ko*L)^2) )^0.5 - 1)'
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = u
[../]
[]
[BCs]
[./ui]
type = DirichletBC
boundary = left
variable = u
value = 300
[../]
[./uo]
type = DirichletBC
boundary = right
variable = u
value = 0
[../]
[]
[Materials]
[./property]
type = GenericConstantMaterial
prop_names = 'density specific_heat'
prop_values = '1.0 1.0'
[../]
[./thermal_conductivity]
type = ParsedMaterial
f_name = 'thermal_conductivity'
args = u
function = '5 + 1e-3 * (u-0)'
[../]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[./error]
type = ElementL2Error
function = exact
variable = u
[../]
[./h]
type = AverageElementSize
[]
[]
[Outputs]
csv = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/variables/caching/3d-rc.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'
pressure_face_gradient_caching = true
velocity_face_gradient_caching = true
pressure_face_value_caching = true
velocity_face_value_caching = true
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
xmin = 0
xmax = 10
ymin = -1
ymax = 1
zmin = -1
zmax = 1
nx = 15
ny = 5
nz = 5
[]
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
w = w
pressure = pressure
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
cache_face_gradients = ${velocity_face_gradient_caching}
cache_face_values = ${velocity_face_value_caching}
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1e-6
cache_face_gradients = ${velocity_face_gradient_caching}
cache_face_values = ${velocity_face_value_caching}
[]
[w]
type = INSFVVelocityVariable
initial_condition = 1e-6
cache_face_gradients = ${velocity_face_gradient_caching}
cache_face_values = ${velocity_face_value_caching}
[]
[pressure]
type = INSFVPressureVariable
cache_face_gradients = ${pressure_face_gradient_caching}
cache_face_values = ${pressure_face_value_caching}
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[w_advection]
type = INSFVMomentumAdvection
variable = w
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'z'
[]
[w_viscosity]
type = INSFVMomentumDiffusion
variable = w
mu = ${mu}
momentum_component = 'z'
[]
[w_pressure]
type = INSFVMomentumPressure
variable = w
momentum_component = 'z'
pressure = pressure
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = 0
[]
[inlet-w]
type = INSFVInletVelocityBC
boundary = 'left'
variable = w
function = 0
[]
[walls-u]
type = INSFVNaturalFreeSlipBC
boundary = 'top bottom front back'
variable = u
momentum_component = 'x'
[]
[walls-v]
type = INSFVNaturalFreeSlipBC
boundary = 'top bottom front back'
variable = v
momentum_component = 'y'
[]
[walls-w]
type = INSFVNaturalFreeSlipBC
boundary = 'top bottom front back'
variable = w
momentum_component = 'z'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 0
[]
[]
[Postprocessors]
[physical]
type = MemoryUsage
mem_type = physical_memory
value_type = total
# by default MemoryUsage reports the peak value for the current timestep
# out of all samples that have been taken (at linear and non-linear iterations)
execute_on = 'INITIAL TIMESTEP_END NONLINEAR LINEAR'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart'
petsc_options_value = 'asm 100 '
line_search = 'none'
nl_abs_tol = 1e-8
[]
[Outputs]
hide = 'physical'
perf_graph = true
exodus = true
csv = true
[]
(modules/porous_flow/test/tests/relperm/vangenuchten1.i)
# Test van Genuchten relative permeability curve by varying saturation over the mesh
# van Genuchten exponent m = 0.5 for both phases
# No residual saturation in either phase
[Mesh]
type = GeneratedMesh
dim = 1
nx = 100
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Variables]
[p0]
initial_condition = 1e6
[]
[s1]
[]
[]
[AuxVariables]
[s0aux]
family = MONOMIAL
order = CONSTANT
[]
[s1aux]
family = MONOMIAL
order = CONSTANT
[]
[kr0aux]
family = MONOMIAL
order = CONSTANT
[]
[kr1aux]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[s0]
type = PorousFlowPropertyAux
property = saturation
phase = 0
variable = s0aux
[]
[s1]
type = PorousFlowPropertyAux
property = saturation
phase = 1
variable = s1aux
[]
[kr0]
type = PorousFlowPropertyAux
property = relperm
phase = 0
variable = kr0aux
[]
[kr1]
type = PorousFlowPropertyAux
property = relperm
phase = 1
variable = kr1aux
[]
[]
[Functions]
[s1]
type = ParsedFunction
value = x
[]
[]
[ICs]
[s1]
type = FunctionIC
variable = s1
function = s1
[]
[]
[Kernels]
[p0]
type = Diffusion
variable = p0
[]
[s1]
type = Diffusion
variable = s1
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'p0 s1'
number_fluid_phases = 2
number_fluid_components = 2
[]
[pc]
type = PorousFlowCapillaryPressureConst
pc = 0
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow2PhasePS
phase0_porepressure = p0
phase1_saturation = s1
capillary_pressure = pc
[]
[kr0]
type = PorousFlowRelativePermeabilityVG
phase = 0
m = 0.5
[]
[kr1]
type = PorousFlowRelativePermeabilityVG
phase = 1
m = 0.5
wetting = false
[]
[]
[VectorPostprocessors]
[vpp]
type = LineValueSampler
warn_discontinuous_face_values = false
variable = 's0aux s1aux kr0aux kr1aux'
start_point = '0 0 0'
end_point = '1 0 0'
num_points = 20
sort_by = id
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
nl_abs_tol = 1e-7
[]
[BCs]
[sleft]
type = DirichletBC
variable = s1
value = 0
boundary = left
[]
[sright]
type = DirichletBC
variable = s1
value = 1
boundary = right
[]
[]
[Outputs]
csv = true
execute_on = timestep_end
[]
(test/tests/meshgenerators/centroid_partitioner/centroid_partitioner_mg.i)
[Mesh]
[./gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 100
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 10.0
# The centroid partitioner orders elements based on
# the position of their centroids
partitioner = centroid
# This will order the elements based on the y value of
# their centroid. Perfect for meshes predominantly in
# one direction
centroid_partitioner_direction = y
# The centroid partitioner behaves differently depending on
# whether you are using Serial or DistributedMesh, so to get
# repeatable results, we restrict this test to using ReplicatedMesh.
parallel_type = replicated
[]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./proc_id]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./proc_id]
type = ProcessorIDAux
variable = proc_id
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[]
(modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/rz_cone_by_parts_traction_steady_stabilized.i)
# This input file tests several different things:
# .) The axisymmetric (RZ) form of the governing equations.
# .) An open boundary.
# .) Not integrating the pressure by parts, thereby requiring a pressure pin.
# .) Natural boundary condition at the outlet.
[GlobalParams]
integrate_p_by_parts = true
laplace = false
gravity = '0 0 0'
supg = true
pspg = true
order = FIRST
[]
[Mesh]
file = '2d_cone.msh'
[]
[Problem]
coord_type = RZ
[]
[Preconditioning]
[./SMP_PJFNK]
type = SMP
full = true
# Jacobian doesn't appear to be correct for RZ traction form
solve_type = PJFNK
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = 'bjacobi ilu 4'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
csv = true
console = true
[./out]
type = Exodus
[../]
[]
[Variables]
[./vel_x]
# Velocity in radial (r) direction
[../]
[./vel_y]
# Velocity in axial (z) direction
[../]
[./p]
[../]
[]
[BCs]
[./u_in]
type = DirichletBC
boundary = bottom
variable = vel_x
value = 0
[../]
[./v_in]
type = FunctionDirichletBC
boundary = bottom
variable = vel_y
function = 'inlet_func'
[../]
[./u_axis_and_walls]
type = DirichletBC
boundary = 'left right'
variable = vel_x
value = 0
[../]
[./v_no_slip]
type = DirichletBC
boundary = 'right'
variable = vel_y
value = 0
[../]
[]
[Kernels]
[./mass]
type = INSMassRZ
variable = p
u = vel_x
v = vel_y
pressure = p
[../]
[./x_momentum_space]
type = INSMomentumTractionFormRZ
variable = vel_x
u = vel_x
v = vel_y
pressure = p
component = 0
[../]
[./y_momentum_space]
type = INSMomentumTractionFormRZ
variable = vel_y
u = vel_x
v = vel_y
pressure = p
component = 1
[../]
[]
[Materials]
[./const]
type = GenericConstantMaterial
block = 'volume'
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[]
[Functions]
[./inlet_func]
type = ParsedFunction
value = '-4 * x^2 + 1'
[../]
[]
[Postprocessors]
[./flow_in]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'bottom'
execute_on = 'timestep_end'
[../]
[./flow_out]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'top'
execute_on = 'timestep_end'
[../]
[]
(modules/heat_conduction/test/tests/sideset_heat_transfer/cfem_gap.i)
[Mesh]
# Build 2-by-2 mesh
[mesh]
type = GeneratedMeshGenerator
dim = 2
nx = 2
xmax = 2
ny = 2
ymax = 2
[]
# Create blocs 0, 1, 2, 3
[block_1]
type = SubdomainBoundingBoxGenerator
input = mesh
block_id = 1
bottom_left = '1 0 0'
top_right = '2 1 0'
[]
[block_2]
type = SubdomainBoundingBoxGenerator
input = block_1
block_id = 2
bottom_left = '0 1 0'
top_right = '1 2 0'
[]
[block_3]
type = SubdomainBoundingBoxGenerator
input = block_2
block_id = 3
bottom_left = '1 1 0'
top_right = '2 2 0'
[]
# Create inner sidesets
[interface_01]
type = SideSetsBetweenSubdomainsGenerator
input = block_3
primary_block = 0
paired_block = 1
new_boundary = 'interface_01'
[]
[interface_13]
type = SideSetsBetweenSubdomainsGenerator
input = interface_01
primary_block = 1
paired_block = 3
new_boundary = 'interface_13'
[]
[interface_32]
type = SideSetsBetweenSubdomainsGenerator
input = interface_13
primary_block = 3
paired_block = 2
new_boundary = 'interface_32'
[]
[interface_20]
type = SideSetsBetweenSubdomainsGenerator
input = interface_32
primary_block = 2
paired_block = 0
new_boundary = 'interface_20'
[]
# Create outer boundaries
[boundary_left_0]
type = SideSetsAroundSubdomainGenerator
input = interface_20
block = 0
normal = '-1 0 0'
new_boundary = 'left_0'
[]
[boundary_bot_0]
type = SideSetsAroundSubdomainGenerator
input = boundary_left_0
block = 0
normal = '0 -1 0'
new_boundary = 'bot_0'
[]
[boundary_bot_1]
type = SideSetsAroundSubdomainGenerator
input = boundary_bot_0
block = 1
normal = '0 -1 0'
new_boundary = 'bot_1'
[]
[boundary_right_1]
type = SideSetsAroundSubdomainGenerator
input = boundary_bot_1
block = 1
normal = '1 0 0'
new_boundary = 'right_1'
[]
[boundary_right_3]
type = SideSetsAroundSubdomainGenerator
input = boundary_right_1
block = 3
normal = '1 0 0'
new_boundary = 'right_3'
[]
[boundary_top_3]
type = SideSetsAroundSubdomainGenerator
input = boundary_right_3
block = 3
normal = '0 1 0'
new_boundary = 'top_3'
[]
[boundary_top_2]
type = SideSetsAroundSubdomainGenerator
input = boundary_top_3
block = 2
normal = '0 1 0'
new_boundary = 'top_2'
[]
[boundary_left_2]
type = SideSetsAroundSubdomainGenerator
input = boundary_top_2
block = 2
normal = '-1 0 0'
new_boundary = 'left_2'
[]
uniform_refine = 4
[]
[Variables]
# Need to have variable for each block to allow discontinuity
[T0]
block = 0
[]
[T1]
block = 1
[]
[T2]
block = 2
[]
[T3]
block = 3
[]
[]
[Kernels]
# Diffusion kernel for each block's variable
[diff_0]
type = MatDiffusion
variable = T0
diffusivity = conductivity
block = 0
[]
[diff_1]
type = MatDiffusion
variable = T1
diffusivity = conductivity
block = 1
[]
[diff_2]
type = MatDiffusion
variable = T2
diffusivity = conductivity
block = 2
[]
[diff_3]
type = MatDiffusion
variable = T3
diffusivity = conductivity
block = 3
[]
# Source for two of the blocks
[source_0]
type = BodyForce
variable = T0
value = 5e5
block = '0'
[]
[source_3]
type = BodyForce
variable = T3
value = 5e5
block = '3'
[]
[]
[InterfaceKernels]
# Side set kernel to represent heat transfer across blocks
# Automatically uses the materials defined in SideSetHeatTransferMaterial
[gap_01]
type = SideSetHeatTransferKernel
# This variable defined on a given block must match the primary_block given when the side set was generated
variable = T0
# This variable defined on a given block must match the paired_block given when the side set was generated
neighbor_var = T1
boundary = 'interface_01'
[]
[gap_13]
type = SideSetHeatTransferKernel
variable = T1
neighbor_var = T3
boundary = 'interface_13'
[]
[gap_32]
type = SideSetHeatTransferKernel
variable = T3
neighbor_var = T2
boundary = 'interface_32'
[]
[gap_20]
type = SideSetHeatTransferKernel
variable = T2
neighbor_var = T0
boundary = 'interface_20'
[]
[]
# Creating auxiliary variable to combine block restricted solutions
# Ignores discontinuity though
[AuxVariables]
[T]
[]
[]
[AuxKernels]
[temp_0]
type = NormalizationAux
variable = T
source_variable = T0
block = 0
[]
[temp_1]
type = NormalizationAux
variable = T
source_variable = T1
block = 1
[]
[temp_2]
type = NormalizationAux
variable = T
source_variable = T2
block = 2
[]
[temp_3]
type = NormalizationAux
variable = T
source_variable = T3
block = 3
[]
[]
[BCs]
# Boundary condition for each block's outer surface
[bc_left_2]
type = DirichletBC
boundary = 'left_2'
variable = T2
value = 300.0
[]
[bc_left_0]
type = DirichletBC
boundary = 'left_0'
variable = T0
value = 300.0
[]
[bc_bot_0]
type = DirichletBC
boundary = 'bot_0'
variable = T0
value = 300.0
[]
[bc_bot_1]
type = DirichletBC
boundary = 'bot_1'
variable = T1
value = 300.0
[]
[./bc_top_2]
type = ConvectiveFluxFunction # (Robin BC)
variable = T2
boundary = 'top_2'
coefficient = 1e3 # W/K/m^2
T_infinity = 600.0
[../]
[./bc_top_3]
type = ConvectiveFluxFunction # (Robin BC)
variable = T3
boundary = 'top_3'
coefficient = 1e3 # W/K/m^2
T_infinity = 600.0
[../]
[./bc_right_3]
type = ConvectiveFluxFunction # (Robin BC)
variable = T3
boundary = 'right_3'
coefficient = 1e3 # W/K/m^2
T_infinity = 600.0
[../]
[./bc_right_1]
type = ConvectiveFluxFunction # (Robin BC)
variable = T1
boundary = 'right_1'
coefficient = 1e3 # W/K/m^2
T_infinity = 600.0
[../]
[]
[Materials]
[fuel]
type = GenericConstantMaterial
prop_names = 'conductivity'
prop_values = 75
block = '0 3'
[]
[mod]
type = GenericConstantMaterial
prop_names = 'conductivity'
prop_values = 7.5
block = '1 2'
[]
# Interface material used for SideSetHeatTransferKernel
# Heat transfer meachnisms ignored if certain properties are not supplied
[gap_mat]
type = SideSetHeatTransferMaterial
boundary = 'interface_01 interface_13 interface_32 interface_20'
conductivity = 0.41
gap_length = 0.002
Tbulk = 750
h_primary = 3000
h_neighbor = 3000
emissivity_primary = 0.85
emissivity_neighbor = 0.85
[]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-12
l_tol = 1e-8
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package -ksp_gmres_restart'
petsc_options_value = 'lu superlu_dist 50'
[]
[Outputs]
exodus = true
[]
(modules/richards/test/tests/gravity_head_1/gh04.i)
# unsaturated = true
# gravity = true
# supg = false
# transient = false
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
xmin = -1
xmax = 1
[]
[BCs]
[./left]
type = DirichletBC
boundary = left
value = -1
variable = pressure
[../]
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0E3
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGnone]
type = RichardsSUPGnone
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = RandomIC
block = 0
min = -1
max = 0
[../]
[../]
[]
[Kernels]
active = 'richardsf'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGnone
sat_UO = Saturation
seff_UO = SeffVG
viscosity = 1E-3
gravity = '-1 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = gh04
exodus = true
[]
(test/tests/misc/exception/2d_diffusion_skip_exception.i)
[Mesh]
type = GeneratedMesh
dim = 2
elem_type = QUAD4
nx = 8
ny = 8
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
skip_exception_check = true
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(modules/stochastic_tools/examples/surrogates/pod_rb/2d_multireg/sub.i)
halfa = 10
fulla = 20
[Problem]
type = FEProblem
extra_tag_vectors = 'diff0 diff1 diff2 diff3 abs0 abs1 abs2 abs3 src0 src1 src2'
[]
[Mesh]
[msh]
type = CartesianMeshGenerator
dim = 2
dx = '10 20 20 20 20 20 20 20 20'
dy = '10 20 20 20 20 20 20 20 20'
ix = '${halfa} ${fulla} ${fulla} ${fulla} ${fulla} ${fulla} ${fulla} ${fulla} ${fulla}'
iy = '${halfa} ${fulla} ${fulla} ${fulla} ${fulla} ${fulla} ${fulla} ${fulla} ${fulla}'
subdomain_id = '1 0 0 0 1 0 0 2 3
0 0 0 0 0 0 0 2 3
0 0 1 0 0 0 2 2 3
0 0 0 0 0 0 2 3 3
1 0 0 0 1 2 2 3 3
0 0 0 0 2 2 3 3 3
0 0 2 2 2 3 3 3 3
2 2 2 3 3 3 3 3 3
3 3 3 3 3 3 3 3 3'
[]
[]
[Variables]
[psi]
[]
[]
[Kernels]
[diff0]
type = MatDiffusion
variable = psi
diffusivity = D0
extra_vector_tags = 'diff0'
block = 0
[]
[diff1]
type = MatDiffusion
variable = psi
diffusivity = D1
extra_vector_tags = 'diff1'
block = 1
[]
[diff2]
type = MatDiffusion
variable = psi
diffusivity = D2
extra_vector_tags = 'diff2'
block = 2
[]
[diff3]
type = MatDiffusion
variable = psi
diffusivity = D3
extra_vector_tags = 'diff3'
block = 3
[]
[abs0]
type = MaterialReaction
variable = psi
coefficient = absxs0
extra_vector_tags = 'abs0'
block = 0
[]
[abs1]
type = MaterialReaction
variable = psi
coefficient = absxs1
extra_vector_tags = 'abs1'
block = 1
[]
[abs2]
type = MaterialReaction
variable = psi
coefficient = absxs2
extra_vector_tags = 'abs2'
block = 2
[]
[abs3]
type = MaterialReaction
variable = psi
coefficient = absxs3
extra_vector_tags = 'abs3'
block = 3
[]
[src0]
type = BodyForce
variable = psi
value = 1
extra_vector_tags = 'src0'
block = 0
[]
[src1]
type = BodyForce
variable = psi
value = 1
extra_vector_tags = 'src1'
block = 1
[]
[src2]
type = BodyForce
variable = psi
value = 1
extra_vector_tags = 'src2'
block = 2
[]
[]
[Materials]
[D0]
type = GenericConstantMaterial
prop_names = D0
prop_values = 1
block = 0
[]
[D1]
type = GenericConstantMaterial
prop_names = D1
prop_values = 1
block = 1
[]
[D2]
type = GenericConstantMaterial
prop_names = D2
prop_values = 1
block = 2
[]
[D3]
type = GenericConstantMaterial
prop_names = D3
prop_values = 1
block = 3
[]
[absxs0]
type = GenericConstantMaterial
prop_names = absxs0
prop_values = 1
block = 0
[]
[absxs1]
type = GenericConstantMaterial
prop_names = absxs1
prop_values = 1
block = 1
[]
[absxs2]
type = GenericConstantMaterial
prop_names = absxs2
prop_values = 1
block = 2
[]
[absxs3]
type = GenericConstantMaterial
prop_names = absxs3
prop_values = 1
block = 3
[]
[]
[BCs]
[left]
type = NeumannBC
variable = psi
boundary = left
value = 0
[]
[bottom]
type = NeumannBC
variable = psi
boundary = bottom
value = 0
[]
[top]
type = DirichletBC
variable = psi
boundary = top
value = 0
[]
[right]
type = DirichletBC
variable = psi
boundary = right
value = 0
[]
[]
[Executioner]
type = Steady
solve_type = linear
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Controls]
[stochastic]
type = SamplerReceiver
[]
[]
[Postprocessors]
[nodal_l2]
type = NodalL2Norm
variable = psi
[]
[]
[Outputs]
[]
(examples/ex02_kernel/ex02.i)
[Mesh]
file = mug.e
[]
[Variables]
[convected]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = convected
[]
[conv]
type = ExampleConvection
variable = convected
velocity = '0.0 0.0 1.0'
[]
[]
[BCs]
[bottom]
type = DirichletBC
variable = convected
boundary = 'bottom'
value = 1
[]
[top]
type = DirichletBC
variable = convected
boundary = 'top'
value = 0
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(modules/porous_flow/test/tests/capillary_pressure/vangenuchten2.i)
# Test van Genuchten relative permeability curve by varying saturation over the mesh
# van Genuchten exponent m = 0.5 for both phases
# No residual saturation in either phase
[Mesh]
type = GeneratedMesh
dim = 1
nx = 500
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Variables]
[p0]
initial_condition = 1e6
[]
[s1]
[]
[]
[AuxVariables]
[s0aux]
family = MONOMIAL
order = CONSTANT
[]
[s1aux]
family = MONOMIAL
order = CONSTANT
[]
[p0aux]
family = MONOMIAL
order = CONSTANT
[]
[p1aux]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[s0]
type = PorousFlowPropertyAux
property = saturation
phase = 0
variable = s0aux
[]
[s1]
type = PorousFlowPropertyAux
property = saturation
phase = 1
variable = s1aux
[]
[p0]
type = PorousFlowPropertyAux
property = pressure
phase = 0
variable = p0aux
[]
[p1]
type = PorousFlowPropertyAux
property = pressure
phase = 1
variable = p1aux
[]
[]
[Functions]
[s1]
type = ParsedFunction
value = x
[]
[]
[ICs]
[s1]
type = FunctionIC
variable = s1
function = s1
[]
[]
[Kernels]
[p0]
type = Diffusion
variable = p0
[]
[s1]
type = Diffusion
variable = s1
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'p0 s1'
number_fluid_phases = 2
number_fluid_components = 2
[]
[pc]
type = PorousFlowCapillaryPressureVG
alpha = 1e-5
m = 0.5
sat_lr = 0.1
log_extension = true
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow2PhasePS
phase0_porepressure = p0
phase1_saturation = s1
capillary_pressure = pc
[]
[kr0]
type = PorousFlowRelativePermeabilityVG
phase = 0
m = 0.5
[]
[kr1]
type = PorousFlowRelativePermeabilityCorey
phase = 1
n = 2
[]
[]
[VectorPostprocessors]
[vpp]
type = LineValueSampler
variable = 's0aux s1aux p0aux p1aux'
start_point = '0 0 0'
end_point = '1 0 0'
num_points = 500
sort_by = id
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
nl_abs_tol = 1e-6
[]
[BCs]
[sleft]
type = DirichletBC
variable = s1
value = 0
boundary = left
[]
[sright]
type = DirichletBC
variable = s1
value = 1
boundary = right
[]
[]
[Outputs]
csv = true
execute_on = timestep_end
[]
(python/chigger/tests/simple/simple_diffusion.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
uniform_refine = 2
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./aux]
family = MONOMIAL
order = CONSTANT
[../]
[]
[AuxKernels]
[./aux_kernel]
type = FunctionAux
variable = aux
function = sin(2*pi*x)*sin(2*pi*y)
execute_on = 'initial'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
# Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/cns/userobject/HLLC/hllc_uo_1D.i)
rho_left = 1.162633159
E_left = 2.1502913276e+05
u_left = 100
rho_right = 1.116127833
E_right = 1.7919094397e+05
u_right = 90
[Mesh]
allow_renumbering = false
[./cartesian]
type = GeneratedMeshGenerator
dim = 1
xmin = 0
xmax = 1
nx = 2
[../]
[]
[Modules]
[./FluidProperties]
[./fp]
type = IdealGasFluidProperties
allow_imperfect_jacobians = true
[../]
[../]
[]
[Problem]
kernel_coverage_check = false
[]
[Variables]
[./rho]
order = CONSTANT
family = MONOMIAL
[../]
[./rho_u]
order = CONSTANT
family = MONOMIAL
[../]
[./rho_E]
order = CONSTANT
family = MONOMIAL
[../]
[]
[ICs]
[./rho_ic]
type = FunctionIC
variable = rho
function = 'if (x < 0.5, ${rho_left}, ${rho_right})'
[../]
[./rho_u_ic]
type = FunctionIC
variable = rho_u
function = 'if (x < 0.5, ${fparse rho_left * u_left}, ${fparse rho_right * u_right})'
[../]
[./rho_E_ic]
type = FunctionIC
variable = rho_E
function = 'if (x < 0.5, ${fparse E_left * rho_left}, ${fparse E_right * rho_right})'
[../]
[]
[Materials]
[./var_mat]
type = ConservedVarValuesMaterial
rho = rho
rhou = rho_u
rho_et = rho_E
fp = fp
[../]
[]
[UserObjects]
[./hllc]
type = HLLCUserObject
fp = fp
[../]
[]
[VectorPostprocessors]
[./wave_speeds]
type = WaveSpeedVPP
hllc_uo = hllc
elem_id = 0
side_id = 1
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
[]
(test/tests/vectorpostprocessors/least_squares_fit/least_squares_fit.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = left
value = 1
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = right
value = 0
[../]
[]
[VectorPostprocessors]
[./line_sample]
type = LineValueSampler
variable = 'u v'
start_point = '0 0.5 0'
end_point = '1 0.5 0'
num_points = 11
sort_by = id
outputs = none
[../]
[./least_squares_fit_sample]
type = LeastSquaresFit
vectorpostprocessor = line_sample
x_name = 'id'
y_name = 'u'
order = 1
num_samples = 20
output = samples
[../]
[./least_squares_fit_coeffs]
type = LeastSquaresFit
vectorpostprocessor = line_sample
x_name = 'id'
y_name = 'u'
order = 1
output = coefficients
[../]
[./shift_and_scale_x_least_squares_fit_sample]
type = LeastSquaresFit
vectorpostprocessor = line_sample
x_name = 'id'
y_name = 'u'
x_shift = 1
x_scale = 10
order = 1
num_samples = 20
output = samples
[../]
[./shift_and_scale_x_least_squares_fit_coeffs]
type = LeastSquaresFit
vectorpostprocessor = line_sample
x_name = 'id'
y_name = 'u'
x_shift = 1
x_scale = 10
order = 1
output = coefficients
[../]
[./shift_and_scale_y_least_squares_fit_sample]
type = LeastSquaresFit
vectorpostprocessor = line_sample
x_name = 'id'
y_name = 'u'
y_shift = 1
y_scale = 10
order = 1
num_samples = 20
output = samples
[../]
[./shift_and_scale_y_least_squares_fit_coeffs]
type = LeastSquaresFit
vectorpostprocessor = line_sample
x_name = 'id'
y_name = 'u'
y_shift = 1
y_scale = 10
order = 1
output = coefficients
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
file_base = out
execute_on = 'timestep_end'
csv = true
[]
(test/tests/postprocessors/perf_graph_data/perf_graph.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 10
ny = 10
nz = 10
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[]
[]
[Postprocessors]
# Getting this information on INITIAL has no practical use, but
# we want to make sure that we can obtain information about
# a section that has not ran yet.
[self]
type = PerfGraphData
section_name = FEProblem::computeResidualInternal
data_type = CALLS
must_exist = false
execute_on = 'INITIAL TIMESTEP_END'
[]
[children]
type = PerfGraphData
section_name = FEProblem::computeResidualInternal
data_type = CHILDREN
execute_on = 'TIMESTEP_END'
[]
[total]
type = PerfGraphData
section_name = FEProblem::computeResidualInternal
data_type = SELF
execute_on = 'TIMESTEP_END'
[]
[self_avg]
type = PerfGraphData
section_name = FEProblem::computeResidualInternal
data_type = SELF_AVG
execute_on = 'TIMESTEP_END'
[]
[children_avg]
type = PerfGraphData
section_name = FEProblem::computeResidualInternal
data_type = CHILDREN_AVG
execute_on = 'TIMESTEP_END'
[]
[total_avg]
type = PerfGraphData
section_name = FEProblem::computeResidualInternal
data_type = TOTAL_AVG
execute_on = 'TIMESTEP_END'
[]
[self_percent]
type = PerfGraphData
section_name = FEProblem::computeResidualInternal
data_type = SELF_PERCENT
execute_on = 'TIMESTEP_END'
[]
[children_percent]
type = PerfGraphData
section_name = FEProblem::computeResidualInternal
data_type = CHILDREN_PERCENT
execute_on = 'TIMESTEP_END'
[]
[total_percent]
type = PerfGraphData
section_name = FEProblem::computeResidualInternal
data_type = TOTAL_PERCENT
execute_on = 'TIMESTEP_END'
[]
[self_memory]
type = PerfGraphData
section_name = FEProblem::computeResidualInternal
data_type = SELF_MEMORY
execute_on = 'TIMESTEP_END'
[]
[children_memory]
type = PerfGraphData
section_name = FEProblem::computeResidualInternal
data_type = CHILDREN_MEMORY
execute_on = 'TIMESTEP_END'
[]
[total_memory]
type = PerfGraphData
section_name = FEProblem::computeResidualInternal
data_type = TOTAL_MEMORY
execute_on = 'TIMESTEP_END'
[]
[calls]
type = PerfGraphData
section_name = FEProblem::computeResidualInternal
data_type = CALLS
execute_on = 'TIMESTEP_END'
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
csv = true
[]
(test/tests/kernels/2d_diffusion/2d_diffusion_neumannbc_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = NeumannBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = neumannbc_out
exodus = true
[]
(test/tests/utils/copy_input_parameters/do_not_copy_parameters.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = DoNotCopyParametersKernel
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/block_restriction/2d-rc.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'
restricted_blocks = '1'
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
block = ${restricted_blocks}
pressure = pressure
[]
[]
[Mesh]
parallel_type = 'replicated'
[mesh]
type = CartesianMeshGenerator
dim = 2
dx = '1 1'
dy = '1'
ix = '7 7'
iy = 10
subdomain_id = '1 2'
[]
[mid]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 1
paired_block = 2
input = mesh
new_boundary = 'middle'
[]
[break_top]
type = PatchSidesetGenerator
boundary = 'top'
n_patches = 2
input = mid
[]
[break_bottom]
type = PatchSidesetGenerator
boundary = 'bottom'
n_patches = 2
input = break_top
[]
[]
[Problem]
kernel_coverage_check = false
fv_bcs_integrity_check = true
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
block = ${restricted_blocks}
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
block = ${restricted_blocks}
[]
[pressure]
type = INSFVPressureVariable
block = ${restricted_blocks}
[]
[temperature]
type = INSFVEnergyVariable
block = ${restricted_blocks}
[]
[scalar]
type = INSFVScalarFieldVariable
block = ${restricted_blocks}
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[energy_advection]
type = INSFVEnergyAdvection
variable = temperature
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
[]
[energy_diffusion]
type = FVDiffusion
coeff = 1.1
variable = temperature
[]
[energy_loss]
type = FVBodyForce
variable = temperature
value = -0.1
[]
[scalar_advection]
type = INSFVScalarFieldAdvection
variable = scalar
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
[]
[scalar_diffusion]
type = FVDiffusion
coeff = 1
variable = scalar
[]
[scalar_src]
type = FVBodyForce
variable = scalar
value = 0.1
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = 0
[]
[top-wall-u]
type = INSFVNoSlipWallBC
boundary = 'top_0'
variable = u
function = 0
[]
[top-wall-v]
type = INSFVNoSlipWallBC
boundary = 'top_0'
variable = v
function = 0
[]
[bottom-wall-u]
type = INSFVSymmetryVelocityBC
boundary = 'bottom_0'
variable = u
mu = ${mu}
u = u
v = v
momentum_component = 'x'
[]
[bottom-wall-v]
type = INSFVSymmetryVelocityBC
boundary = 'bottom_0'
variable = v
mu = ${mu}
u = u
v = v
momentum_component = 'y'
[]
[bottom-wall-p]
type = INSFVSymmetryPressureBC
boundary = 'bottom_0'
variable = pressure
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'middle'
variable = pressure
function = 0
[]
[inlet_t]
type = FVDirichletBC
boundary = 'left'
variable = temperature
value = 1
[]
[outlet_scalar]
type = FVDirichletBC
boundary = 'middle'
variable = scalar
value = 1
[]
[]
[Materials]
[ins_fv]
type = INSFVEnthalpyMaterial
temperature = 'temperature'
rho = ${rho}
block = ${restricted_blocks}
[]
[const]
type = ADGenericFunctorMaterial
prop_names = 'cp'
prop_values = '2'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[]
(test/tests/restart/restart_diffusion/exodus_refined_restart_1_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
uniform_refine = 2
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = exodus_refined_restart_1
exodus = true
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_mortar/large_gap_heat_transfer_test_cylinder_mortar.i)
rpv_core_gap_size = 0.15
core_outer_radius = 2
rpv_inner_radius = ${fparse 2 + rpv_core_gap_size}
rpv_outer_radius = ${fparse 2.5 + rpv_core_gap_size}
rpv_outer_htc = 10 # W/m^2/K
rpv_outer_Tinf = 300 # K
core_blocks = '1'
rpv_blocks = '3'
[Mesh]
[core_gap_rpv]
type = ConcentricCircleMeshGenerator
num_sectors = 10
radii = '${core_outer_radius} ${rpv_inner_radius} ${rpv_outer_radius}'
rings = '2 1 2'
has_outer_square = false
preserve_volumes = true
portion = full
[]
[rename_core_bdy]
type = SideSetsBetweenSubdomainsGenerator
input = core_gap_rpv
primary_block = 1
paired_block = 2
new_boundary = 'core_outer'
[]
[rename_inner_rpv_bdy]
type = SideSetsBetweenSubdomainsGenerator
input = rename_core_bdy
primary_block = 3
paired_block = 2
new_boundary = 'rpv_inner'
[]
[2d_mesh]
type = BlockDeletionGenerator
input = rename_inner_rpv_bdy
block = 2
[]
[secondary]
type = LowerDBlockFromSidesetGenerator
sidesets = 'rpv_inner'
new_block_id = 10001
new_block_name = 'secondary_lower'
input = 2d_mesh
[]
[primary]
type = LowerDBlockFromSidesetGenerator
sidesets = 'core_outer'
new_block_id = 10000
new_block_name = 'primary_lower'
input = secondary
[]
allow_renumbering = false
[]
[Variables]
[Tsolid]
initial_condition = 500
[]
[lm]
order = FIRST
family = LAGRANGE
block = 'secondary_lower'
[]
[]
[Kernels]
[heat_source]
type = CoupledForce
variable = Tsolid
block = '${core_blocks}'
v = power_density
[]
[heat_conduction]
type = HeatConduction
variable = Tsolid
[]
[]
[BCs]
[RPV_out_BC] # k \nabla T = h (T- T_inf) at RPV outer boundary
type = ConvectiveFluxFunction # (Robin BC)
variable = Tsolid
boundary = 'outer' # outer RPV
coefficient = ${rpv_outer_htc}
T_infinity = ${rpv_outer_Tinf}
[]
[]
[UserObjects]
[radiation]
type = GapFluxModelRadiation
temperature = Tsolid
boundary = 'rpv_inner'
primary_emissivity = 0.8
secondary_emissivity = 0.8
[]
[conduction]
type = GapFluxModelConduction
temperature = Tsolid
boundary = 'rpv_inner'
gap_conductivity = 0.1
[]
[]
[Constraints]
[ced]
type = ModularGapConductanceConstraint
variable = lm
secondary_variable = Tsolid
primary_boundary = 'core_outer'
primary_subdomain = 10000
secondary_boundary = 'rpv_inner'
secondary_subdomain = 10001
gap_flux_models = 'radiation conduction'
gap_geometry_type = 'CYLINDER'
cylinder_axis_point_1 = '0 0 0'
cylinder_axis_point_2 = '0 0 5'
[]
[]
[AuxVariables]
[power_density]
block = '${core_blocks}'
initial_condition = 50e3
[]
[]
[Materials]
[simple_mat]
type = HeatConductionMaterial
thermal_conductivity = 34.6 # W/m/K
[]
[]
[Postprocessors]
[Tcore_avg]
type = ElementAverageValue
variable = Tsolid
block = '${core_blocks}'
[]
[Tcore_max]
type = ElementExtremeValue
value_type = max
variable = Tsolid
block = '${core_blocks}'
[]
[Tcore_min]
type = ElementExtremeValue
value_type = min
variable = Tsolid
block = '${core_blocks}'
[]
[Trpv_avg]
type = ElementAverageValue
variable = Tsolid
block = '${rpv_blocks}'
[]
[Trpv_max]
type = ElementExtremeValue
value_type = max
variable = Tsolid
block = '${rpv_blocks}'
[]
[Trpv_min]
type = ElementExtremeValue
value_type = min
variable = Tsolid
block = '${rpv_blocks}'
[]
[ptot]
type = ElementIntegralVariablePostprocessor
variable = power_density
block = '${core_blocks}'
[]
[rpv_convective_out]
type = ConvectiveHeatTransferSideIntegral
T_solid = Tsolid
boundary = 'outer' # outer RVP
T_fluid = ${rpv_outer_Tinf}
htc = ${rpv_outer_htc}
[]
[heat_balance] # should be equal to 0 upon convergence
type = ParsedPostprocessor
function = '(rpv_convective_out - ptot) / ptot'
pp_names = 'rpv_convective_out ptot'
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[VectorPostprocessors]
[NodalTemperature]
type = NodalValueSampler
sort_by = id
boundary = 'rpv_inner core_outer'
variable = 'Tsolid'
[]
[]
[Executioner]
type = Steady
petsc_options = '-snes_converged_reason -pc_svd_monitor'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package -mat_mffd_err -pc_factor_shift_type '
'-pc_factor_shift_amount'
petsc_options_value = ' lu superlu_dist 1e-5 NONZERO '
'1e-15'
snesmf_reuse_base = false
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
l_max_its = 100
line_search = none
[]
[Outputs]
exodus = false
csv = true
[]
(test/tests/kernels/ad_coupled_force/fe_test.i)
[Mesh]
[square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[]
[]
[Variables]
[u]
[]
[v]
[]
[]
[Kernels]
[diff_u]
type = ADDiffusion
variable = u
[]
[force_u]
type = ADCoupledForce
variable = u
v = v
[]
[diff_v]
type = ADDiffusion
variable = v
[]
[]
[BCs]
[left_u]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right_u]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[left_v]
type = DirichletBC
variable = v
boundary = left
value = 5
[]
[right_v]
type = DirichletBC
variable = v
boundary = right
value = 3
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
(test/tests/variables/optionally_coupled/optionally_coupled.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./optional_coupling]
type = OptionallyCoupledForce
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
[Debug]
show_var_residual_norms = true
[]
(test/tests/markers/box_marker/box_marker_adapt_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
nz = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[./top]
type = DirichletBC
variable = u
boundary = top
value = 0
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Adaptivity]
steps = 1
marker = box
[./Markers]
[./box]
bottom_left = '0.3 0.3 0'
inside = refine
top_right = '0.6 0.6 0'
outside = do_nothing
type = BoxMarker
[../]
[../]
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/function_file_test4.i)
# Test for usage of missing function
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = ic_function
[../]
[../]
[]
[Functions]
[./ic_function]
type = PiecewiseLinear
data_file = dummy #we don't get that far
format = rowls
scale_factor = 1.0
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/fvkernels/mms/advection.i)
a=1.1
[GlobalParams]
advected_interp_method = 'average'
[]
[Mesh]
[./gen_mesh]
type = GeneratedMeshGenerator
dim = 1
xmin = -0.6
xmax = 0.6
nx = 2
[../]
[]
[Variables]
[./v]
family = MONOMIAL
order = CONSTANT
fv = true
[../]
[]
[FVKernels]
[./advection]
type = FVAdvection
variable = v
velocity = '${a} 0 0'
[../]
[body_v]
type = FVBodyForce
variable = v
function = 'forcing'
[]
[]
[FVBCs]
[advection]
type = FVAdvectionFunctionBC
boundary = 'left right'
exact_solution = 'exact'
variable = v
velocity = '${a} 0 0'
[]
[]
[Functions]
[exact]
type = ParsedFunction
value = '1.1 * sin(1.1 * x)'
[]
[forcing]
type = ParsedFunction
value = '${a} * 1.1 * 1.1 * cos(1.1 * x)'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm NONZERO'
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[./error]
type = ElementL2Error
variable = v
function = exact
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(test/tests/postprocessors/relative_difference/relative_difference.i)
# Tests the RelativeDifferencePostprocessor post-processor, which computes
# the relative difference between 2 post-processor values.
[Mesh]
type = GeneratedMesh
dim = 1
nx = 2
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[./num_elems]
# number of elements, equal to 2
type = NumElems
[../]
[./num_nodes]
# number of nodes, equal to 3
type = NumNodes
[../]
[./zero]
# zero post-processor value
type = EmptyPostprocessor
[../]
# For the case in this input file, this will be computed as
# y = abs((num_nodes - num_elems) / num_elems)
# y = abs((3 - 2 ) / 2 ) = 0.5
# When the command-line modification "Postprocessors/relative_difference/value2=zero" is used,
# y = abs(num_nodes - zero)
# y = abs(3 - 0 ) = 3
[./relative_difference]
type = RelativeDifferencePostprocessor
value1 = num_nodes
value2 = num_elems
[../]
[]
[Outputs]
[./out]
type = CSV
show = relative_difference
[../]
[]
(modules/porous_flow/test/tests/gravity/grav01c_action.i)
# Checking that gravity head is established
# using the Unsaturated Action
# For better agreement with the analytical solution (ana_pp), just increase nx
[Mesh]
type = GeneratedMesh
dim = 1
nx = 100
xmin = -1
xmax = 0
[]
[GlobalParams]
PorousFlowDictator = dictator
block = 0
[]
[Variables]
[pp]
[InitialCondition]
type = RandomIC
min = -1
max = 1
[]
[]
[]
[Modules]
[FluidProperties]
[the_simple_fluid]
type = SimpleFluidProperties
thermal_expansion = 0.0
bulk_modulus = 2.0
viscosity = 1.0
density0 = 1.0
[]
[]
[]
[PorousFlowUnsaturated]
add_saturation_aux = false
add_darcy_aux = false
porepressure = pp
gravity = '-1 0 0'
fp = the_simple_fluid
van_genuchten_alpha = 1.0
van_genuchten_m = 0.5
relative_permeability_type = Corey
relative_permeability_exponent = 1.0
[]
[Functions]
[ana_pp]
type = ParsedFunction
vars = 'g B p0 rho0'
vals = '1 2 -1 1'
value = '-B*log(exp(-p0/B)+g*rho0*x/B)' # expected pp at base
[]
[]
[BCs]
[z]
type = DirichletBC
variable = pp
boundary = right
value = -1
[]
[]
[Materials]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1 0 0 0 2 0 0 0 3'
[]
[]
[Postprocessors]
[pp_base]
type = PointValue
variable = pp
point = '-1 0 0'
[]
[pp_analytical]
type = FunctionValuePostprocessor
function = ana_pp
point = '-1 0 0'
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = grav01c_action
exodus = true
[csv]
type = CSV
[]
[]
(examples/ex11_prec/default.i)
[Mesh]
file = square.e
[]
[Variables]
[./diffused]
order = FIRST
family = LAGRANGE
[../]
[./forced]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff_diffused]
type = Diffusion
variable = diffused
[../]
[./conv_forced]
type = CoupledForce
variable = forced
v = diffused
[../]
[./diff_forced]
type = Diffusion
variable = forced
[../]
[]
[BCs]
#Note we have active on and neglect the right_forced BC
active = 'left_diffused right_diffused left_forced'
[./left_diffused]
type = DirichletBC
variable = diffused
boundary = 'left'
value = 0
[../]
[./right_diffused]
type = DirichletBC
variable = diffused
boundary = 'right'
value = 100
[../]
[./left_forced]
type = DirichletBC
variable = forced
boundary = 'left'
value = 0
[../]
[./right_forced]
type = DirichletBC
variable = forced
boundary = 'right'
value = 0
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/mesh/centroid_partitioner/centroid_partitioner_test.i)
###########################################################
# This test exercises the parallel computation aspect of
# the framework. A Centroid partitioner is used to split
# the mesh into chunks for several processors along a
# vector (y-axis).
#
# @Requirement F2.30
###########################################################
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 100
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 10.0
[]
# The centroid partitioner orders elements based on
# the position of their centroids
partitioner = centroid
# This will order the elements based on the y value of
# their centroid. Perfect for meshes predominantly in
# one direction
centroid_partitioner_direction = y
# The centroid partitioner behaves differently depending on
# whether you are using Serial or DistributedMesh, so to get
# repeatable results, we restrict this test to using ReplicatedMesh.
parallel_type = replicated
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./proc_id]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./proc_id]
type = ProcessorIDAux
variable = proc_id
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[]
(test/tests/misc/check_error/multi_master.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
perf_graph = true
[]
[MultiApps]
[./full_solve]
# not setting app_type to use the same app type of master, i.e. MooseTestApp
type = FullSolveMultiApp
execute_on = initial
positions = '0 0 0'
input_files = multi_sub.i
[../]
[]
(test/tests/kernels/vector_fe/coupled_scalar_vector_jacobian.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
xmin = -1.1
ymin = -1.1
xmax = 1.1
ymax = 1.1
elem_type = QUAD9
[]
[Variables]
[./u]
family = NEDELEC_ONE
order = FIRST
[../]
[./v]
[../]
[]
[Kernels]
[./wave]
type = VectorFEWave
variable = u
x_forcing_func = 'x_ffn'
y_forcing_func = 'y_ffn'
[../]
[./diff]
type = Diffusion
variable = v
[../]
[./source]
type = BodyForce
variable = v
[../]
[./advection]
type = EFieldAdvection
variable = v
efield = u
charge = 'positive'
mobility = 100
[../]
[]
[Functions]
[./x_ffn]
type = ParsedFunction
value = '(2*pi*pi + 1)*cos(pi*x)*sin(pi*y)'
[../]
[./y_ffn]
type = ParsedFunction
value = '-(2*pi*pi + 1)*sin(pi*x)*cos(pi*y)'
[../]
[]
[Preconditioning]
[./pre]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type'
petsc_options_value = 'asm'
petsc_options = '-snes_converged_reason -ksp_converged_reason -snes_linesearch_monitor'
[]
(modules/porous_flow/test/tests/capillary_pressure/vangenuchten3.i)
# Test van Genuchten relative permeability curve by varying saturation over the mesh
# van Genuchten exponent m = 0.5 for both phases
# No residual saturation in either phase
[Mesh]
type = GeneratedMesh
dim = 1
nx = 500
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Variables]
[p0]
initial_condition = 1e6
[]
[s1]
[]
[]
[AuxVariables]
[s0aux]
family = MONOMIAL
order = CONSTANT
[]
[s1aux]
family = MONOMIAL
order = CONSTANT
[]
[p0aux]
family = MONOMIAL
order = CONSTANT
[]
[p1aux]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[s0]
type = PorousFlowPropertyAux
property = saturation
phase = 0
variable = s0aux
[]
[s1]
type = PorousFlowPropertyAux
property = saturation
phase = 1
variable = s1aux
[]
[p0]
type = PorousFlowPropertyAux
property = pressure
phase = 0
variable = p0aux
[]
[p1]
type = PorousFlowPropertyAux
property = pressure
phase = 1
variable = p1aux
[]
[]
[Functions]
[s1]
type = ParsedFunction
value = x
[]
[]
[ICs]
[s1]
type = FunctionIC
variable = s1
function = s1
[]
[]
[Kernels]
[p0]
type = Diffusion
variable = p0
[]
[s1]
type = Diffusion
variable = s1
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'p0 s1'
number_fluid_phases = 2
number_fluid_components = 2
[]
[pc]
type = PorousFlowCapillaryPressureVG
alpha = 1e-5
m = 0.5
sat_lr = 0.1
s_scale = 0.8
log_extension = false
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow2PhasePS
phase0_porepressure = p0
phase1_saturation = s1
capillary_pressure = pc
[]
[kr0]
type = PorousFlowRelativePermeabilityVG
phase = 0
m = 0.5
[]
[kr1]
type = PorousFlowRelativePermeabilityCorey
phase = 1
n = 2
[]
[]
[VectorPostprocessors]
[vpp]
type = LineValueSampler
variable = 's0aux s1aux p0aux p1aux'
start_point = '0 0 0'
end_point = '1 0 0'
num_points = 500
sort_by = id
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
nl_abs_tol = 1e-6
[]
[BCs]
[sleft]
type = DirichletBC
variable = s1
value = 0
boundary = left
[]
[sright]
type = DirichletBC
variable = s1
value = 1
boundary = right
[]
[]
[Outputs]
csv = true
execute_on = timestep_end
[]
(modules/stochastic_tools/test/tests/ics/random_ic_distribution_test/random_ic_distribution_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 50
ny = 50
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
[]
[]
[AuxVariables]
[u_aux]
order = CONSTANT
family = MONOMIAL
[]
[]
[Distributions]
[uniform]
type = Uniform
lower_bound = 1.0
upper_bound = 3.0
[]
[]
[ICs]
[u_aux]
type = RandomIC
legacy_generator = false
variable = u_aux
distribution = uniform
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[]
[]
[VectorPostprocessors]
[histo]
type = VariableValueVolumeHistogram
variable = u_aux
min_value = 0
max_value = 4
bin_number = 80
execute_on = initial
outputs = initial
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[initial]
type = CSV
execute_on = initial
[]
[]
(test/tests/vectorpostprocessors/parallel_consistency/parallel_consistency.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
# To make this deterministic
[Partitioner]
type = GridPartitioner
nx = 2
ny = 1
nz = 1
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[]
[]
[VectorPostprocessors]
[constant]
type = ConstantVectorPostprocessor
value = '3 4'
execute_on = 'TIMESTEP_END'
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
csv = true
[]
[AuxVariables]
[scattered]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[viewit]
type = VectorPostprocessorVisualizationAux
vpp = 'constant'
vector_name = value
variable = scattered
execute_on = 'TIMESTEP_END'
[]
[]
(test/tests/problems/mixed_coord/mixed_coord_test.i)
[Mesh]
file = rz_xyz.e
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./one]
initial_condition = 1
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[./left_middle]
type = DirichletBC
variable = u
boundary = left_middle
value = 1
[../]
[./right_middle]
type = DirichletBC
variable = u
boundary = right_middle
value = 0
[../]
[]
[Postprocessors]
[./volume]
type = ElementIntegralVariablePostprocessor
variable = one
execute_on = 'initial timestep_end'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
[Problem]
coord_type = 'RZ XYZ'
block = '1 2'
[]
(modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/ad_rz_cone_no_parts_steady.i)
[GlobalParams]
integrate_p_by_parts = false
[]
[Mesh]
file = '2d_cone.msh'
[]
[Problem]
coord_type = RZ
[]
[AuxVariables]
[vel_x]
order = SECOND
[]
[vel_y]
order = SECOND
[]
[]
[AuxKernels]
[vel_x]
type = VectorVariableComponentAux
variable = vel_x
vector_variable = velocity
component = 'x'
[]
[vel_y]
type = VectorVariableComponentAux
variable = vel_y
vector_variable = velocity
component = 'y'
[]
[]
[Variables]
[./velocity]
order = SECOND
family = LAGRANGE_VEC
[../]
[./p]
[../]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[momentum_advection]
type = INSADMomentumAdvection
variable = velocity
[]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
[../]
[]
[BCs]
[p_corner]
type = DirichletBC
boundary = top_right
value = 0
variable = p
[]
[inlet]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom'
function_x = 0
function_y = 'inlet_func'
[../]
[wall]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'right'
function_x = 0
function_y = 0
[]
[axis]
type = ADVectorFunctionDirichletBC
variable = velocity
boundary = 'left'
set_y_comp = false
function_x = 0
[]
[]
[Functions]
[./inlet_func]
type = ParsedFunction
value = '-4 * x^2 + 1'
[../]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[ins_mat]
type = INSADMaterial
velocity = velocity
pressure = p
[]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = 'bjacobi ilu 4'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
csv = true
console = true
[./out]
type = Exodus
[../]
[]
[Postprocessors]
[./flow_in]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'bottom'
execute_on = 'timestep_end'
[../]
[./flow_out]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'top'
execute_on = 'timestep_end'
[../]
[]
(test/tests/materials/get_material_property_names/get_material_property_block_names.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[./add_subdomain]
input = gen
type = SubdomainBoundingBoxGenerator
top_right = '1 1 0'
bottom_left = '0 0.5 0'
block_id = 100
block_name = 'top'
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Materials]
[./material]
type = GenericConstantMaterial
prop_names = combo
block = 100
prop_values = 12345
[../]
[./top]
type = GenericConstantMaterial
prop_names = combo
block = 0
prop_values = 99999
[../]
[]
[UserObjects]
[./get_material_block_names_test]
type = GetMaterialPropertyBoundaryBlockNamesTest
expected_names = 'top 0'
property_name = combo
test_type = 'block'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/ray_tracing/test/tests/outputs/ray_tracing_mesh_output/ray_mesh_output_data.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 5
ny = 5
xmax = 5
ymax = 5
[]
[]
[Variables/u]
[InitialCondition]
type = FunctionIC
variable = u
function = '(x < 2) * (x + 2 * y) + (x >= 2) * (2 * x + 2 * y - 2)'
[]
[]
[UserObjects]
[study]
type = RepeatableRayStudy
names = 'diag
top_across
bottom_across
partial'
start_points = '0 0 0
0 5 0
0 0 0
0.5 0.5 0'
end_points = '5 5 0
5 5 0
5 0 0
4.5 0.5 0'
always_cache_traces = true
data_on_cache_traces = true
aux_data_on_cache_traces = true
ray_aux_data_names = 'test_aux'
initial_ray_aux_data = '1; 2; 3; 4'
[]
[]
[RayKernels]
[variable_integral]
type = VariableIntegralRayKernel
study = study
variable = u
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[rays]
type = RayTracingExodus
study = study
output_data = true
output_aux_data = true
execute_on = final
[]
[rays_nodal]
type = RayTracingExodus
study = study
output_data_nodal = true
execute_on = final
[]
[]
(modules/ray_tracing/test/tests/raybcs/reflect_ray_bc/reflect_ray_bc_nonplanar.i)
[Mesh]
[file]
type = FileMeshGenerator
file = nonplanar.e
[]
[subdomains]
type = ParsedSubdomainMeshGenerator
input = file
combinatorial_geometry = 'x > 0.5'
block_id = 1
[]
[internal_sideset]
type = SideSetsBetweenSubdomainsGenerator
input = subdomains
primary_block = 0
paired_block = 1
new_boundary = internal
[]
[]
[UserObjects/study]
type = RepeatableRayStudy
start_points = '0 0 0'
directions = '1 1 1'
names = 'ray'
warn_non_planar = false
use_internal_sidesets = true
execute_on = initial
tolerate_failure = true
[]
[RayBCs]
[kill]
type = KillRayBC
boundary = 'top right bottom left front back'
[]
[reflect_internal]
type = ReflectRayBC
boundary = internal
[]
[]
[RayKernels/null]
type = NullRayKernel
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/one-elem-wide-channel.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 10
ymin = -1
ymax = 1
nx = 5
ny = 1
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = '0'
[]
[walls-u]
type = INSFVNaturalFreeSlipBC
boundary = 'top bottom'
variable = u
momentum_component = 'x'
[]
[walls-v]
type = INSFVNaturalFreeSlipBC
boundary = 'top bottom'
variable = v
momentum_component = 'y'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = '0'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 200 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[]
(test/tests/partitioners/single_rank_partitioner/single_rank_partitioner.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[Partitioner]
type = SingleRankPartitioner
rank = 2
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Debug]
pid_aux = true
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/check_dynamic_name_boundary.i)
[Mesh]
file = three_block.e
# These names will be applied on the fly to the
# mesh so they can be used in the input file
# In addition they will show up in the input file
block_id = '1 2 3'
block_name = 'wood steel copper'
boundary_id = '1 2'
boundary_name = 'left left' # Can't have duplicate names
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[../]
[]
[Materials]
active = empty
[./empty]
type = MTMaterial
block = 'wood steel copper'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/vectorpostprocessors/element_id_counters/internal_side_element_counter.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
xmax = 1
ymax = 1
extra_element_integers = foo_id
[]
[id0]
type = SubdomainBoundingBoxGenerator
input = gmg
bottom_left = '0 0 0'
block_id = 0
top_right = '1 1 0'
integer_name = foo_id
[]
[id1]
type = SubdomainBoundingBoxGenerator
input = id0
bottom_left = '0.4 0.4 0'
block_id = 1
top_right = '0.9 0.9 0'
integer_name = foo_id
[]
[id2]
type = SubdomainBoundingBoxGenerator
input = id1
bottom_left = '0.1 0.1 0'
block_id = 2
top_right = '0.6 0.6 0'
integer_name = foo_id
[]
[subdomain]
type = SubdomainBoundingBoxGenerator
input = id2
bottom_left = '0 0.6 0'
block_id = 1
top_right = '1 1 0'
[]
[]
[VectorPostprocessors]
[elem_counter]
type = InternalSideElementCounterWithID
id_name = foo_id
[]
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
execute_on = 'timestep_end'
[]
(test/tests/vectorpostprocessors/line_function_sampler/line_function_sampler.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[VectorPostprocessors]
[./func_vals]
type = LineFunctionSampler
functions = 'x+1 x^2+y^2'
start_point = '0 0 0'
end_point = '1 1 0'
num_points = 10
sort_by = id
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
csv = true
[]
(test/tests/meshgenerators/errors/mesh_generator_errors.i)
[Mesh]
[test]
type = TestMeshGeneratorErrors
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
(test/tests/materials/old_cyclic_dep/test.i)
# This test checks that the usage of an old/older (stateful) material property
# does not create a dependency on that property for the purposes of
# dependency resolution for material property evaluation.
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = CoefDiffusion
variable = u
coef = 0.1
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 'left'
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = 'right'
value = 2
[../]
[]
[Materials]
[./mat1]
type = CoupledMaterial
mat_prop = 'prop-a'
coupled_mat_prop = 'prop-b'
use_old_prop = true
block = 0
[../]
[./mat2]
type = CoupledMaterial
mat_prop = 'prop-b'
coupled_mat_prop = 'prop-a'
use_old_prop = false
block = 0
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Debug]
show_material_props = true
[]
(test/tests/controls/control_piecewise/controlled_piecewise.i)
[Mesh]
[./generated]
type = GeneratedMeshGenerator
dim = 1
xmin = 0
xmax = 1
nx = 10
[../]
[]
[Problem]
kernel_coverage_check = false
[]
[Variables]
[./u]
initial_condition = 0.1
[../]
[]
[AuxVariables]
[./v]
[../]
[./x]
[../]
[]
[ICs]
[./x_ic]
type = FunctionIC
variable = x
function = 'x'
[../]
[]
[AuxKernels]
[./v_aux]
type = FunctionAux
variable = v
function = func
[../]
[]
[Controls]
[./func_control]
type = RealFunctionControl
parameter = '*/*/scale_factor'
function = '2'
execute_on = 'initial'
[../]
[]
[Materials]
[./mat]
type = PiecewiseLinearInterpolationMaterial
property = matprop
variable = x
x = '0 1'
y = '0 10'
outputs = all
[../]
[]
[Functions]
[./func]
type = PiecewiseLinear
x = '0 1'
y = '0 10'
axis = x
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/kernels/hfem/array_dirichlet_transform_bc.i)
[Mesh]
[square]
type = GeneratedMeshGenerator
nx = 3
ny = 3
dim = 2
[]
build_all_side_lowerd_mesh = true
[]
[Variables]
[u]
order = THIRD
family = MONOMIAL
block = 0
components = 2
[]
[lambda]
order = CONSTANT
family = MONOMIAL
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
components = 2
[]
[lambdab]
order = CONSTANT
family = MONOMIAL
block = BOUNDARY_SIDE_LOWERD_SUBDOMAIN
components = 2
[]
[]
[AuxVariables]
[v]
order = CONSTANT
family = MONOMIAL
block = 0
initial_condition = '1'
[]
[]
[Kernels]
[diff]
type = ArrayDiffusion
variable = u
block = 0
diffusion_coefficient = dc
[]
[source]
type = ArrayCoupledForce
variable = u
v = v
coef = '1 2'
block = 0
[]
[]
[DGKernels]
[surface]
type = ArrayHFEMDiffusion
variable = u
lowerd_variable = lambda
[]
[]
[BCs]
[all]
type = ArrayHFEMDirichletTestBC
boundary = 'left right top bottom'
variable = u
lowerd_variable = lambdab
[]
[]
[Materials]
[dc]
type = GenericConstantArray
prop_name = dc
prop_value = '1 1'
[]
[]
[Postprocessors]
[intu]
type = ElementIntegralArrayVariablePostprocessor
variable = u
block = 0
[]
[lambdanorm]
type = ElementArrayL2Norm
variable = lambda
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu basic mumps'
[]
[Outputs]
[out]
# we hide lambda because it may flip sign due to element
# renumbering with distributed mesh
type = Exodus
hide = lambda
[]
csv = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/exceptions/bad-ro.i)
mu=.01
rho=1
[GlobalParams]
velocity_interp_method = 'rc'
advected_interp_method = 'average'
rhie_chow_user_object = 'rc'
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = .1
ymin = 0
ymax = .1
nx = 20
ny = 20
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
[]
[v]
type = INSFVVelocityVariable
[]
[pressure]
type = INSFVPressureVariable
[]
[lambda]
family = SCALAR
order = FIRST
[]
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
rho = ${rho}
[]
[mean_zero_pressure]
type = FVScalarLagrangeMultiplier
variable = pressure
lambda = lambda
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = 'mu'
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[u_bad_ro]
type = FVBodyForce
variable = u
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = 'mu'
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[]
[FVBCs]
[top_x]
type = INSFVNoSlipWallBC
variable = u
boundary = 'top'
function = 1
[]
[no_slip_x]
type = INSFVNoSlipWallBC
variable = u
boundary = 'left right bottom'
function = 0
[]
[no_slip_y]
type = INSFVNoSlipWallBC
variable = v
boundary = 'left right top bottom'
function = 0
[]
[]
[Materials]
[mu]
type = ADGenericFunctorMaterial
prop_names = 'mu'
prop_values = '${mu}'
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/format/pps_file_out_warn.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
nz = 0
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Postprocessors]
[./avg_block]
type = ElementAverageValue
variable = u
outputs = gmv
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
gmv = true
[]
(modules/stochastic_tools/test/tests/multiapps/commandline_control/sub.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Variables]
[u]
initial_condition = 1980
[]
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[size]
type = AverageElementSize
execute_on = 'initial'
[]
[]
[Outputs]
csv = true
[]
(test/tests/utils/spline_interpolation/bicubic_spline_interpolation_x_normal.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1 # needed to ensure Z is the problem dimension
ny = 4
nz = 4
ymax = 4
zmax = 4
[]
[Functions]
[./yx1]
type = ParsedFunction
value = '3*y^2'
[../]
[./yx2]
type = ParsedFunction
value = '6*z^2'
[../]
[./spline_fn]
type = BicubicSplineFunction
normal_component = 'x'
x1 = '0 2 4'
x2 = '0 2 4 6'
y = '0 16 128 432 8 24 136 440 64 80 192 496'
yx11 = '0 0 0 0'
yx1n = '48 48 48 48'
yx21 = '0 0 0'
yx2n = '216 216 216'
yx1 = 'yx1'
yx2 = 'yx2'
[../]
[./u_func]
type = ParsedFunction
value = 'y^3 + 2*z^3'
[../]
[./u2_forcing_func]
type = ParsedFunction
value = '-6*y - 12*z'
[../]
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./bi_func_value]
order = FIRST
family = LAGRANGE
[../]
[./y_deriv]
order = FIRST
family = LAGRANGE
[../]
[./z_deriv]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./bi_func_value]
type = FunctionAux
variable = bi_func_value
function = spline_fn
[../]
[./deriv_1]
type = FunctionDerivativeAux
function = spline_fn
variable = y_deriv
component = y
[../]
[./deriv_2]
type = FunctionDerivativeAux
function = spline_fn
variable = z_deriv
component = z
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./body_force]
type = BodyForce
variable = u
function = u2_forcing_func
[../]
[]
[BCs]
[./sides]
type = FunctionDirichletBC
variable = u
boundary = 'left right front back'
function = u_func
[../]
[]
[Postprocessors]
[./nodal_l2_err_spline]
type = NodalL2Error
variable = u
function = spline_fn
execute_on = 'initial timestep_end'
[../]
[./nodal_l2_err_analytic]
type = NodalL2Error
variable = u
function = u_func
execute_on = 'initial timestep_end'
[../]
[./y_deriv_err_analytic]
type = NodalL2Error
variable = y_deriv
function = yx1
execute_on = 'initial timestep_end'
[../]
[./z_deriv_err_analytic]
type = NodalL2Error
variable = z_deriv
function = yx2
execute_on = 'initial timestep_end'
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/ics/pns_test.i)
p_initial=1.01e5
T=273.15
[Mesh]
[cartesian]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 1
ymax = 2
nx = 4
ny = 4
[]
[]
[Modules]
[FluidProperties]
[fp]
type = IdealGasFluidProperties
[]
[]
[]
[Problem]
kernel_coverage_check = false
solve = false
skip_nl_system_check = true
[]
[AuxVariables]
[porosity]
initial_condition = 0.2
[]
[pressure]
type = MooseVariableFVReal
[]
[superficial_vel_x]
type = MooseVariableFVReal
[]
[superficial_vel_y]
type = MooseVariableFVReal
[]
[superficial_vel_z]
type = MooseVariableFVReal
[]
[temperature]
type = MooseVariableFVReal
[]
[vel_x]
type = MooseVariableFVReal
[]
[vel_y]
type = MooseVariableFVReal
[]
[vel_z]
type = MooseVariableFVReal
[]
[superficial_rho_ht]
type = MooseVariableFVReal
[]
[ht]
type = MooseVariableFVReal
[]
[e]
type = MooseVariableFVReal
[]
[Mach]
type = MooseVariableFVReal
[]
[superficial_rho]
type = MooseVariableFVReal
[]
[superficial_rhou]
type = MooseVariableFVReal
[]
[superficial_rhov]
type = MooseVariableFVReal
[]
[superficial_rhow]
type = MooseVariableFVReal
[]
[superficial_rho_et]
type = MooseVariableFVReal
[]
[rho]
type = MooseVariableFVReal
[]
[rhou]
type = MooseVariableFVReal
[]
[rhov]
type = MooseVariableFVReal
[]
[rhow]
type = MooseVariableFVReal
[]
[rho_et]
type = MooseVariableFVReal
[]
[specific_volume]
type = MooseVariableFVReal
[]
[pressure_2]
[]
[superficial_vel_x_2]
[]
[superficial_vel_y_2]
[]
[superficial_vel_z_2]
[]
[vel_x_2]
[]
[vel_y_2]
[]
[vel_z_2]
[]
[temperature_2]
[]
[ht_2]
[]
[superficial_rho_ht_2]
[]
[e_2]
[]
[Mach_2]
[]
[superficial_rho_2]
[]
[superficial_rhou_2]
[]
[superficial_rhov_2]
[]
[superficial_rhow_2]
[]
[superficial_rho_et_2]
[]
[rho_2]
[]
[rhou_2]
[]
[rhov_2]
[]
[rhow_2]
[]
[rho_et_2]
[]
[specific_volume_2]
[]
[]
[GlobalParams]
fluid_properties = 'fp'
initial_pressure = ${p_initial}
initial_temperature = ${T}
initial_superficial_velocity = '1 0.2 18'
porosity = porosity
[]
[ICs]
[p]
type = PNSInitialCondition
variable = 'pressure'
[]
[vel_x]
type = PNSInitialCondition
variable = 'vel_x'
[]
[vel_y]
type = PNSInitialCondition
variable = 'vel_y'
[]
[vel_z]
type = PNSInitialCondition
variable = 'vel_z'
[]
[superficial_vel_x]
type = PNSInitialCondition
variable = 'superficial_vel_x'
[]
[superficial_vel_y]
type = PNSInitialCondition
variable = 'superficial_vel_y'
[]
[superficial_vel_z]
type = PNSInitialCondition
variable = 'superficial_vel_z'
[]
[temperature]
type = PNSInitialCondition
variable = 'temperature'
[]
[ht]
type = PNSInitialCondition
variable = 'ht'
[]
[superficial_rho_ht]
type = PNSInitialCondition
variable = 'superficial_rho_ht'
[]
[e]
type = PNSInitialCondition
variable = 'e'
[]
[Mach]
type = PNSInitialCondition
variable = 'Mach'
[]
[superficial_rho]
type = PNSInitialCondition
variable = 'superficial_rho'
[]
[superficial_rhou]
type = PNSInitialCondition
fluid_properties = 'fp'
initial_pressure = ${p_initial}
initial_temperature = ${T}
initial_superficial_velocity = '1 0.2 18'
porosity = porosity
variable = 'superficial_rhou'
[]
[superficial_rhov]
type = PNSInitialCondition
variable = 'superficial_rhov'
[]
[superficial_rhow]
type = PNSInitialCondition
variable = 'superficial_rhow'
[]
[rho]
type = PNSInitialCondition
variable = 'rho'
[]
[rhou]
type = PNSInitialCondition
variable = 'rhou'
[]
[rhov]
type = PNSInitialCondition
variable = 'rhov'
[]
[rhow]
type = PNSInitialCondition
variable = 'rhow'
[]
[rho_et]
type = PNSInitialCondition
variable = 'rho_et'
[]
[superficial_rho_et]
type = PNSInitialCondition
variable = 'superficial_rho_et'
[]
[specific_volume]
type = PNSInitialCondition
variable = 'specific_volume'
[]
[p_2]
type = PNSInitialCondition
variable = 'pressure_2'
variable_type = 'pressure'
[]
[superficial_vel_x_2]
type = PNSInitialCondition
variable = 'superficial_vel_x_2'
variable_type = 'superficial_vel_x'
[]
[superficial_vel_y_2]
type = PNSInitialCondition
variable = 'superficial_vel_y_2'
variable_type = 'superficial_vel_y'
[]
[superficial_vel_z_2]
type = PNSInitialCondition
variable = 'superficial_vel_z_2'
variable_type = 'superficial_vel_z'
[]
[vel_x_2]
type = PNSInitialCondition
variable = 'vel_x_2'
variable_type = 'vel_x'
[]
[vel_y_2]
type = PNSInitialCondition
variable = 'vel_y_2'
variable_type = 'vel_y'
[]
[vel_z_2]
type = PNSInitialCondition
variable = 'vel_z_2'
variable_type = 'vel_z'
[]
[temperature_2]
type = PNSInitialCondition
variable = 'temperature_2'
variable_type = 'temperature'
[]
[superficial_ht_2]
type = PNSInitialCondition
variable = 'superficial_rho_ht_2'
variable_type = 'superficial_rho_ht'
[]
[ht_2]
type = PNSInitialCondition
variable = 'ht_2'
variable_type = 'ht'
[]
[e_2]
type = PNSInitialCondition
variable = 'e_2'
variable_type = 'e'
[]
[Mach_2]
type = PNSInitialCondition
variable = 'Mach_2'
variable_type = 'Mach'
[]
[superficial_rho_2]
type = PNSInitialCondition
variable = 'superficial_rho_2'
variable_type = 'superficial_rho'
[]
[superficial_rhou_2]
type = PNSInitialCondition
variable = 'superficial_rhou_2'
variable_type = 'superficial_rhou'
[]
[superficial_rhov_2]
type = PNSInitialCondition
variable = 'superficial_rhov_2'
variable_type = 'superficial_rhov'
[]
[superficial_rhow_2]
type = PNSInitialCondition
variable = 'superficial_rhow_2'
variable_type = 'superficial_rhow'
[]
[superficial_rho_et_2]
type = PNSInitialCondition
variable = 'superficial_rho_et_2'
variable_type = 'superficial_rho_et'
[]
[rho_2]
type = PNSInitialCondition
variable = 'rho_2'
variable_type = 'rho'
[]
[rhou_2]
type = PNSInitialCondition
variable = 'rhou_2'
variable_type = 'rhou'
[]
[rhov_2]
type = PNSInitialCondition
variable = 'rhov_2'
variable_type = 'rhov'
[]
[rhow_2]
type = PNSInitialCondition
variable = 'rhow_2'
variable_type = 'rhow'
[]
[rho_et_2]
type = PNSInitialCondition
variable = 'rho_et_2'
variable_type = 'rho_et'
[]
[specific_volume_2]
type = PNSInitialCondition
variable = 'specific_volume_2'
variable_type = 'specific_volume'
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-rc-ambient-convection.i)
mu=1
rho=1
k=1e-3
cp=1
alpha = 1
advected_interp_method='average'
velocity_interp_method='rc'
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 5
ymin = -1
ymax = 1
nx = 50
ny = 16
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = 1
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[T_fluid]
type = INSFVEnergyVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
[]
[energy_advection]
type = INSFVEnergyAdvection
variable = T_fluid
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
[]
[energy_diffusion]
type = FVDiffusion
coeff = ${k}
variable = T_fluid
[]
[ambient_convection]
type = NSFVEnergyAmbientConvection
variable = T_fluid
T_ambient = 100
alpha = 'alpha'
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_x
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_y
function = 0
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = vel_x
function = 0
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = vel_y
function = 0
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 0
[]
[inlet_t]
type = FVDirichletBC
boundary = 'left'
variable = T_fluid
value = 1
[]
[]
[Materials]
[const_functor]
type = ADGenericFunctorMaterial
prop_names = 'cp alpha'
prop_values = '${cp} ${alpha}'
[]
[ins_fv]
type = INSFVEnthalpyMaterial
rho = ${rho}
temperature = 'T_fluid'
[]
[]
[Postprocessors]
[temp]
type = ElementAverageValue
variable = T_fluid
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[]
(test/tests/vectorpostprocessors/element_value_sampler/fv_element_value_sampler.i)
# Tests the ElementValueSampler vector post-processor. In this test, 2 FV
# variables are given distributions by a function and are output to a CSV file.
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Functions]
[./u_fn]
type = ParsedFunction
value = '2 * x + 3 * y'
[../]
[./v_fn]
type = ParsedFunction
value = 'x + y'
[../]
[]
[AuxVariables]
[./u]
family = MONOMIAL
order = CONSTANT
fv = true
[../]
[./v]
family = MONOMIAL
order = CONSTANT
fv = true
[../]
[]
[ICs]
[./u_ic]
type = FunctionIC
variable = u
function = u_fn
[../]
[./v_ic]
type = FunctionIC
variable = v
function = v_fn
[../]
[]
[VectorPostprocessors]
[./element_value_sampler]
type = ElementValueSampler
variable = 'u v'
sort_by = id
execute_on = 'initial'
[../]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
file_base = 'element_value_sampler'
csv = true
execute_on = 'initial'
[]
(test/tests/materials/derivative_material_interface/parsed_material.i)
#
# Test the parsed function free enery Allen-Cahn Bulk kernel
#
[Mesh]
type = GeneratedMesh
dim = 1
nx = 10
xmin = 0
xmax = 1
[]
[AuxVariables]
[./eta]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = x
[../]
[../]
[]
[Materials]
[./consts]
type = ParsedMaterial
args = 'eta'
function ='(eta-0.5)^2'
outputs = exodus
[../]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(test/tests/mortar/3d-periodic/periodic.i)
[Mesh]
[file]
type = FileMeshGenerator
file = flow_test.e
[]
[secondary]
input = file
type = LowerDBlockFromSidesetGenerator
new_block_id = 11
new_block_name = "secondary"
sidesets = '1'
[]
[primary]
input = secondary
type = LowerDBlockFromSidesetGenerator
new_block_id = 12
new_block_name = "primary"
sidesets = '2'
[]
[]
[Variables]
[u]
block = 'bottom middle top'
[]
[lm]
block = 'secondary'
use_dual = true
[]
[]
[Kernels]
[diffusion]
type = Diffusion
variable = u
block = 'bottom middle top'
[]
[force]
type = BodyForce
variable = u
block = 'bottom middle top'
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
value = 1
boundary = 'around'
[]
[]
[Constraints]
[ev]
type = EqualValueConstraint
variable = lm
secondary_variable = u
primary_boundary = top
secondary_boundary = bottom
primary_subdomain = 12
secondary_subdomain = 11
delta = 0.1
periodic = true
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-12
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/2d-rc-action.i)
mu=1.1
rho=1.1
[Problem]
error_on_jacobian_nonzero_reallocation = true
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 5
ymin = 0
ymax = 1
nx = 20
ny = 10
[]
[]
[Modules]
[NavierStokesFV]
compressibility = 'incompressible'
porous_medium_treatment = true
density = 'rho'
dynamic_viscosity = 'mu'
porosity = 'porosity'
initial_velocity = '1 1e-6 0'
initial_pressure = 0.0
inlet_boundaries = 'left'
momentum_inlet_types = 'fixed-velocity'
momentum_inlet_function = '1 0'
wall_boundaries = 'top bottom'
momentum_wall_types = 'slip slip'
outlet_boundaries = 'right'
momentum_outlet_types = 'fixed-pressure'
pressure_function = '0'
[]
[]
[Materials]
[const]
type = ADGenericFunctorMaterial
prop_names = 'rho mu'
prop_values = '${rho} ${mu}'
[]
[]
[AuxVariables]
[porosity]
family = MONOMIAL
order = CONSTANT
fv = true
initial_condition = 0.5
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 200 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-11
nl_abs_tol = 1e-14
[]
# Some basic Postprocessors to visually examine the solution
[Postprocessors]
[inlet-p]
type = SideIntegralVariablePostprocessor
variable = pressure
boundary = 'left'
[]
[outlet-u]
type = SideIntegralVariablePostprocessor
variable = superficial_vel_x
boundary = 'right'
[]
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/fvbcs/FVHeatFluxBC/wall_heat_transfer.i)
flux=10
[GlobalParams]
porosity = 'porosity'
splitting = 'porosity'
locality = 'global'
average_porosity = 'average_eps'
average_k_fluid='average_k_fluid'
average_k_solid='average_k_solid'
average_kappa='average_k_fluid' # because of vector matprop, should be kappa
average_kappa_solid='average_kappa_solid'
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 20
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
[]
[Variables]
[Tf]
type = MooseVariableFVReal
[]
[Ts]
type = MooseVariableFVReal
[]
[]
[AuxVariables]
[k]
type = MooseVariableFVReal
[]
[kappa]
type = MooseVariableFVReal
[]
[k_s]
type = MooseVariableFVReal
[]
[kappa_s]
type = MooseVariableFVReal
[]
[porosity]
type = MooseVariableFVReal
initial_condition = 0.2
[]
[]
[Functions]
[k]
type = ParsedFunction
value = 0.1*(100*y+1)
[]
[kappa]
type = ParsedFunction
value = 0.2*(200*y+1)
[]
[kappa_s]
type = ParsedFunction
value = 0.4*(200*y+1)
[]
[k_s]
type = ParsedFunction
value = 0.2*(200*y+1)+2*x
[]
[]
[FVKernels]
[Tf_diffusion]
type = FVDiffusion
variable = Tf
coeff = 1
[]
[Ts_diffusion]
type = FVDiffusion
variable = Ts
coeff = 1
[]
[]
[FVBCs]
[left_Ts]
type = NSFVHeatFluxBC
variable = Ts
boundary = 'left'
phase = 'solid'
value = ${flux}
[]
[right_Ts]
type = FVDirichletBC
variable = Ts
boundary = 'right'
value = 1000.0
[]
[left_Tf]
type = NSFVHeatFluxBC
variable = Tf
boundary = 'left'
phase = 'fluid'
value = ${flux}
[]
[right_Tf]
type = FVDirichletBC
variable = Tf
boundary = 'right'
value = 1000.0
[]
[]
[AuxKernels]
[k]
type = ADMaterialRealAux
variable = k
property = 'k'
[]
[k_s]
type = ADMaterialRealAux
variable = k_s
property = 'k_s'
[]
[kappa_s]
type = ADMaterialRealAux
variable = kappa_s
property = 'kappa_s'
[]
[]
[Materials]
[thermal_conductivities_k]
type = ADGenericFunctionMaterial
prop_names = 'k'
prop_values = 'k'
[]
[thermal_conductivities_k_s]
type = ADGenericFunctionMaterial
prop_names = 'k_s'
prop_values = 'k_s'
[]
[thermal_conductivities_kappa]
type = ADGenericConstantVectorMaterial
prop_names = 'kappa'
prop_values = '0.1 0.2 .03'
[]
[thermal_conductivities_kappa_s]
type = ADGenericFunctionMaterial
prop_names = 'kappa_s'
prop_values = 'kappa_s'
[]
[]
[Postprocessors]
[average_eps]
type = ElementAverageValue
variable = porosity
# because porosity is constant in time, we evaluate this only once
execute_on = 'initial'
[]
[average_k_fluid]
type = ElementAverageValue
variable = k
[]
[average_k_solid]
type = ElementAverageValue
variable = k_s
[]
[average_kappa_solid]
type = ElementAverageValue
variable = kappa_s
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
hide = 'porosity average_eps'
[]
(modules/thermal_hydraulics/test/tests/materials/average_wall_temperature_3eqn/average_wall_temperature_3eqn.i)
# Tests the average wall temperature aux for 1-phase flow. With the following
# inputs, the value should be equal to 1.25:
#
# i h_wall T_wall P_hf
# --------------------------
# 1 10 26/10 1
# 2 6 1/2 3
#
# T_fluid = 1/4
#
# With these values,
# P_tot = 1 + 3 = 4
# h_wall_avg = (1 * 10 + 3 * 6) / 4 = 28 / 4 = 7
# denominator = P_tot * h_wall_avg = 4 * 7 = 28
# numerator = 10 * (26/10 - 1/4) * 1 + 6 * (1/2 - 1/4) * 3 = 28
# T_wall_avg = T_fluid + numerator / denominator = 1/4 + 1
#
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
allow_renumbering = false
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[AuxVariables]
[Hw_avg]
family = MONOMIAL
order = CONSTANT
[]
[T_wall_avg]
family = MONOMIAL
order = CONSTANT
[]
[T_wall1]
family = MONOMIAL
order = CONSTANT
[]
[T_wall2]
family = MONOMIAL
order = CONSTANT
[]
[P_hf1]
family = MONOMIAL
order = CONSTANT
[]
[P_hf2]
family = MONOMIAL
order = CONSTANT
[]
[P_hf_total]
family = MONOMIAL
order = CONSTANT
[]
[T_fluid]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[T_wall_avg_auxkernel]
type = MaterialRealAux
variable = T_wall_avg
property = T_wall
[]
[T_wall1_auxkernel]
type = ConstantAux
variable = T_wall1
value = 2.6
[]
[T_wall2_auxkernel]
type = ConstantAux
variable = T_wall2
value = 0.5
[]
[P_hf_total_auxkernel]
type = SumAux
variable = P_hf_total
values = 'P_hf1 P_hf2'
[]
[P_hf1_auxkernel]
type = ConstantAux
variable = P_hf1
value = 1
[]
[P_hf2_auxkernel]
type = ConstantAux
variable = P_hf2
value = 3
[]
[T_fluid_auxkernel]
type = ConstantAux
variable = T_fluid
value = 0.25
[]
[]
[Materials]
[const_materials]
type = GenericConstantMaterial
prop_names = 'Hw1 Hw2'
prop_values = '10 6'
[]
[Hw_avg_material]
type = WeightedAverageMaterial
prop_name = Hw_avg
values = 'Hw1 Hw2'
weights = 'P_hf1 P_hf2'
[]
[T_wall_avg_material]
type = AverageWallTemperature3EqnMaterial
T_wall_sources = 'T_wall1 T_wall2'
Hw_sources = 'Hw1 Hw2'
P_hf_sources = 'P_hf1 P_hf2'
T_fluid = T_fluid
Hw_average = Hw_avg
P_hf_total = P_hf_total
[]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[T_wall_avg_pp]
type = ElementalVariableValue
elementid = 0
variable = T_wall_avg
[]
[]
[Outputs]
csv = true
execute_on = timestep_end
[]
(test/tests/samplers/base/global_vs_local.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
ny = 1
[]
[Variables]
[./u]
[../]
[]
[Samplers]
[sample]
type = TestSampler
[]
[]
[Postprocessors]
[test]
type = SamplerTester
sampler = sample
test_type = BASE_GLOBAL_VS_LOCAL
[]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
kernel_coverage_check = false
[]
[Outputs]
[]
(modules/functional_expansion_tools/test/tests/errors/bc_value_bad_function.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Variables]
[./v]
[../]
[]
[BCs]
[./this_could_be_bad]
type = FXValueBC
boundary = right
function = const
variable = v
[../]
[]
[Functions]
[./const]
type = ConstantFunction
value = -1
[../]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
(test/tests/misc/check_error/function_file_test8.i)
# Test for usage of missing function
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = ic_function
[../]
[../]
[]
[Functions]
[./ic_function]
type = PiecewiseLinear
xy_data = '1 2 3'
scale_factor = 1.0
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(tutorials/tutorial01_app_development/step10_auxkernels/test/tests/materials/packed_column/packed_column_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
xmax = 1
ymax = 1
[]
[Problem]
solve = false
[]
[Variables]
[u]
[]
[]
[Materials]
[filter]
type = PackedColumn
diameter = 2
viscosity = 1e-03
output_properties = 'permeability viscosity'
outputs = exodus
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/kernels/array_kernels/array_save_in.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 4
ny = 4
[]
[subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '0.5 0.5 0'
top_right = '1 1 0'
block_id = 1
[]
[]
[Variables]
[u]
order = FIRST
family = L2_LAGRANGE
components = 2
[]
[]
[AuxVariables]
[u_diff_save_in]
order = FIRST
family = L2_LAGRANGE
components = 2
[]
[u_vacuum_save_in]
order = FIRST
family = L2_LAGRANGE
components = 2
[]
[u_dg_save_in]
order = FIRST
family = L2_LAGRANGE
components = 2
[]
[u_diff_diag_save_in]
order = FIRST
family = L2_LAGRANGE
components = 2
[]
[u_vacuum_diag_save_in]
order = FIRST
family = L2_LAGRANGE
components = 2
[]
[u_dg_diag_save_in]
order = FIRST
family = L2_LAGRANGE
components = 2
[]
[]
[Kernels]
[diff]
type = ArrayDiffusion
variable = u
diffusion_coefficient = dc
save_in = u_diff_save_in
diag_save_in = u_diff_diag_save_in
[]
[reaction]
type = ArrayReaction
variable = u
reaction_coefficient = rc
[]
[]
[DGKernels]
[dgdiff]
type = ArrayDGDiffusion
variable = u
diff = dc
save_in = u_dg_save_in
diag_save_in = u_dg_diag_save_in
[]
[]
[BCs]
[left]
type = ArrayVacuumBC
variable = u
boundary = 1
save_in = u_vacuum_save_in
diag_save_in = u_vacuum_diag_save_in
[]
[right]
type = ArrayPenaltyDirichletBC
variable = u
boundary = 2
value = '1 2'
penalty = 4
[]
[]
[Materials]
[dc0]
type = GenericConstantArray
block = 0
prop_name = dc
prop_value = '1 1'
[]
[dc1]
type = GenericConstantArray
block = 1
prop_name = dc
prop_value = '2 1'
[]
[rc]
type = GenericConstant2DArray
block = '0 1'
prop_name = rc
prop_value = '1 0; -0.1 1'
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Postprocessors]
[intu0]
type = ElementIntegralArrayVariablePostprocessor
variable = u
component = 0
[]
[intu1]
type = ElementIntegralArrayVariablePostprocessor
variable = u
component = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/ic_variable_not_specified.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./u_ic]
type = ConstantIC
value = 1
[../]
[../]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/system_interfaces/input.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/problems/no_material_dependency_check/no_material_coverage_check.i)
[Mesh]
[./gen]
type = GeneratedMeshGenerator
dim = 3
[../]
[]
[Problem]
material_dependency_check = false
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./body_force]
type = BodyForce
variable = u
value = 10
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Materials]
[./mat1]
type = GenericConstantMaterial
prop_names = 'diff1'
prop_values = '1'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(modules/reactor/test/tests/meshgenerators/reporting_id/cartesian_id/assembly_reporting_id.i)
[Mesh]
[pin1]
type = ConcentricCircleMeshGenerator
num_sectors = 2
radii = '0.4 0.5'
rings = '1 1 1'
has_outer_square = on
pitch = 1.26
preserve_volumes = yes
smoothing_max_it = 3
[]
[pin2]
type = ConcentricCircleMeshGenerator
num_sectors = 2
radii = '0.3 0.4'
rings = '1 1 1'
has_outer_square = on
pitch = 1.26
preserve_volumes = yes
smoothing_max_it = 3
[]
[assembly]
type = CartesianIDPatternedMeshGenerator
inputs = 'pin1 pin2'
pattern = ' 1 0 1 0;
0 1 0 1;
1 0 1 0;
0 1 0 1'
assign_type = 'cell'
id_name = 'pin_id'
[]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[AuxVariables]
[pin_id]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[set_pin_id]
type = ExtraElementIDAux
variable = pin_id
extra_id_name = pin_id
[]
[]
[Outputs]
exodus = true
execute_on = timestep_end
[]
(test/tests/misc/check_error/missing_var_in_kernel_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
# Test error message for missing variable param.
[./diff]
type = Diffusion
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/porous_flow/test/tests/fluids/brine1.i)
# Test the density and viscosity calculated by the brine material
# Pressure 20 MPa
# Temperature 50C
# xnacl = 0.1047 (equivalent to 2.0 molality)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[]
[Variables]
[pp]
initial_condition = 20e6
[]
[]
[Kernels]
[dummy]
type = Diffusion
variable = pp
[]
[]
[AuxVariables]
[temp]
initial_condition = 50
[]
[xnacl]
initial_condition = 0.1047
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
temperature = temp
[]
[ppss]
type = PorousFlow1PhaseFullySaturated
porepressure = pp
[]
[brine]
type = PorousFlowBrine
temperature_unit = Celsius
xnacl = 0.1047
phase = 0
[]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Postprocessors]
[pressure]
type = ElementIntegralVariablePostprocessor
variable = pp
[]
[temperature]
type = ElementIntegralVariablePostprocessor
variable = temp
[]
[xnacl]
type = ElementIntegralVariablePostprocessor
variable = xnacl
[]
[density]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_fluid_phase_density_qp0'
[]
[viscosity]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_viscosity_qp0'
[]
[enthalpy]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_fluid_phase_enthalpy_qp0'
[]
[internal_energy]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_fluid_phase_internal_energy_qp0'
[]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = brine1
csv = true
[]
(test/tests/dgkernels/dg_block_restrict/2d_dg_diffusion_block_restrict.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmax = 2
nx = 10
ymax = 2
ny = 10
[]
[./subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '0 0 0'
block_id = 1
top_right = '1 1 0'
[../]
[./interface]
input = subdomain1
type = SideSetsBetweenSubdomainsGenerator
primary_block = '1'
paired_block = '0'
new_boundary = 'primary1_interface'
[../]
[./boundaries]
input = interface
type = BreakBoundaryOnSubdomainGenerator
boundaries = 'left bottom'
[../]
[]
[Variables]
[./u]
order = FIRST
family = L2_LAGRANGE
block = 1
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./source]
type = BodyForce
variable = u
[../]
[]
[DGKernels]
[./dg_diffusion]
type = DGDiffusion
variable = u
sigma = 4
epsilon = 1
[../]
[]
[BCs]
[./vacuum]
type = VacuumBC
variable = u
boundary = 'left_to_1 bottom_to_1'
[../]
[./primary1_inteface]
type = VacuumBC
variable = u
boundary = 'primary1_interface'
[../]
[]
[Postprocessors]
[./norm]
type = ElementL2Norm
variable = u
block = 1
[../]
[]
[Executioner]
type = Steady
nl_abs_tol = 1e-12
[]
[Problem]
kernel_coverage_check = false
[]
[Outputs]
exodus = true
[]
(modules/fluid_properties/test/tests/materials/ad_saturation_temperature_material/ad_saturation_temperature_material.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
xmin = 0
xmax = 1
[]
[Modules]
[./FluidProperties]
[./fp_2phase]
type = StiffenedGasTwoPhaseFluidProperties
[../]
[../]
[]
[Materials]
[./p_mat]
type = ADGenericConstantMaterial
prop_names = 'p_test'
prop_values = '1e5'
[../]
[./T_sat_mat]
type = ADSaturationTemperatureMaterial
p = p_test
T_sat = T_sat_test
fp_2phase = fp_2phase
[../]
[]
[Postprocessors]
[./T_sat_pp]
type = ADElementIntegralMaterialProperty
mat_prop = T_sat_test
execute_on = 'INITIAL'
[../]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
execute_on = 'INITIAL'
[]
(examples/ex02_kernel/ex02_oversample.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
nz = 0
zmax = 0
elem_type = QUAD9
[]
[Variables]
[./diffused]
order = SECOND
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = diffused
[../]
[]
[DiracKernels]
[./foo]
variable = diffused
type = ConstantPointSource
value = 1
point = '0.3 0.3 0.0'
[../]
[]
[BCs]
[./all]
type = DirichletBC
variable = diffused
boundary = 'bottom left right top'
value = 0.0
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[./refine_2]
type = Exodus
file_base = oversample_2
refinements = 2
[../]
[./refine_4]
type = Exodus
file_base = oversample_4
refinements = 4
[../]
[]
(python/peacock/tests/common/fsp_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
active = 'u v'
[./u]
order = FIRST
family = LAGRANGE
[../]
[./v]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff_u conv_v diff_v'
[./diff_u]
type = Diffusion
variable = u
[../]
[./conv_v]
type = CoupledForce
variable = v
v = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[BCs]
active = 'left_u right_u left_v'
[./left_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 2
value = 100
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = 1
value = 0
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = 2
value = 0
[../]
[]
[Executioner]
type = Steady
# This is setup automatically in MOOSE (SetupPBPAction.C)
# petsc_options = '-snes_mf_operator'
# petsc_options_iname = '-pc_type'
# petsc_options_value = 'asm'
[]
[Preconditioning]
active = 'FSP'
[./FSP]
type = FSP
# It is the starting point of splitting
topsplit = 'uv' # uv should match the following block name
[./uv]
splitting = 'u v' # u and v are the names of subsolvers
# Generally speaking, there are four types of splitting we could choose
# <additive,multiplicative,symmetric_multiplicative,schur>
splitting_type = additive
# An approximate solution to the original system
# | A_uu A_uv | | u | _ |f_u|
# | 0 A_vv | | v | - |f_v|
# is obtained by solving the following subsystems
# A_uu u = f_u and A_vv v = f_v
# If splitting type is specified as schur, we may also want to set more options to
# control how schur works using PETSc options
# petsc_options_iname = '-pc_fieldsplit_schur_fact_type -pc_fieldsplit_schur_precondition'
# petsc_options_value = 'full selfp'
[../]
[./u]
vars = 'u'
# PETSc options for this subsolver
# A prefix will be applied, so just put the options for this subsolver only
petsc_options_iname = '-pc_type -ksp_type'
petsc_options_value = ' hypre preonly'
[../]
[./v]
vars = 'v'
# PETSc options for this subsolver
petsc_options_iname = '-pc_type -ksp_type'
petsc_options_value = ' hypre preonly'
[../]
[../]
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/mesh_modifiers/subdomain_bounding_box/oriented_subdomain_bounding_box_outside.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
xmin = -6
xmax = 4
nx = 10
ymin = -2
ymax = 10
ny = 12
zmin = -5
zmax = 7
nz = 12
[]
[subdomains]
type = OrientedSubdomainBoundingBoxGenerator
input = gen
center = '-1 4 1'
width = 5
length = 10
height = 4
width_direction = '2 1 0'
length_direction = '-1 2 2'
block_id = 10
location = OUTSIDE
[]
[]
[Problem]
type = FEProblem
solve = false
kernel_coverage_check = false
[]
[Variables]
[u]
[]
[]
[Materials]
[mat10]
type = GenericConstantMaterial
block = 10
outputs = all
prop_values = 6.24
prop_names = prop
[]
[mat0]
type = GenericConstantMaterial
block = 0
prop_names = prop
prop_values = 0
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
[]
[Outputs]
exodus = true
[]
(test/tests/fvkernels/mms/grad-reconstruction/cartesian.i)
a=1.1
diff=1.1
[Mesh]
[./gen_mesh]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
[../]
[]
[Variables]
[./v]
family = MONOMIAL
order = CONSTANT
fv = true
initial_condition = 1
[../]
[]
[FVKernels]
[./advection]
type = FVElementalAdvection
variable = v
velocity = '${a} ${fparse 2 * a} 0'
[../]
[reaction]
type = FVReaction
variable = v
[]
[diff_v]
type = FVDiffusion
variable = v
coeff = ${diff}
[]
[body_v]
type = FVBodyForce
variable = v
function = 'forcing'
[]
[]
[FVBCs]
[diri]
type = FVFunctionDirichletBC
boundary = 'left right top bottom'
function = 'exact'
variable = v
[]
[]
[Functions]
[exact]
type = ParsedFunction
value = 'sin(x)*cos(y)'
[]
[forcing]
type = ParsedFunction
value = '-2*a*sin(x)*sin(y) + a*cos(x)*cos(y) + 2*diff*sin(x)*cos(y) + sin(x)*cos(y)'
vars = 'a diff'
vals = '${a} ${diff}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_shift_type -sub_pc_type'
petsc_options_value = 'asm NONZERO lu'
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[./error]
type = ElementL2Error
variable = v
function = exact
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(test/tests/outputs/oversample/oversample_file.i)
[Mesh]
type = FileMesh
file = square.e
dim = 2
uniform_refine = 1
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
[./exodus]
type = Exodus
refinements = 1
file_base = exodus_oversample_custom_name
[../]
[]
(test/tests/kernels/ad_2d_diffusion/2d_diffusion_neumannbc_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = ADDiffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = ADNeumannBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = neumannbc_out
exodus = true
[]
(modules/tensor_mechanics/test/tests/CylindricalRankTwoAux/test.i)
[Mesh]
[file_mesh]
type = FileMeshGenerator
file = circle.e
[]
[cnode]
type = ExtraNodesetGenerator
coord = '1000.0 0.0'
new_boundary = 10
input = file_mesh
[]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./T]
[../]
[./stress_rr]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_tt]
order = CONSTANT
family = MONOMIAL
[../]
[]
[ICs]
[./T_IC]
type = FunctionIC
variable = T
function = '1000-0.7*sqrt(x^2+y^2)'
[../]
[]
[Kernels]
[./TensorMechanics]
displacements = 'disp_x disp_y'
[../]
[]
[AuxKernels]
[./stress_rr]
type = CylindricalRankTwoAux
variable = stress_rr
rank_two_tensor = stress
index_j = 0
index_i = 0
center_point = '0 0 0'
[../]
[./stress_tt]
type = CylindricalRankTwoAux
variable = stress_tt
rank_two_tensor = stress
index_j = 1
index_i = 1
center_point = '0 0 0'
[../]
[]
[BCs]
[./outer_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./outer_y]
type = DirichletBC
variable = disp_y
boundary = '2 10'
value = 0
[../]
[]
[Materials]
[./iso_C]
type = ComputeElasticityTensor
fill_method = symmetric_isotropic
C_ijkl = '2.15e5 0.74e5'
block = 1
[../]
[./strain]
type = ComputeSmallStrain
displacements = 'disp_x disp_y'
block = 1
eigenstrain_names = eigenstrain
[../]
[./stress]
type = ComputeLinearElasticStress
block = 1
[../]
[./thermal_strain]
type= ComputeThermalExpansionEigenstrain
thermal_expansion_coeff = 1e-6
temperature = T
stress_free_temperature = 273
block = 1
eigenstrain_name = eigenstrain
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart'
petsc_options_value = 'hypre boomeramg 101'
l_max_its = 30
nl_max_its = 10
nl_abs_tol = 1e-9
nl_rel_tol = 1e-14
l_tol = 1e-4
[]
[Outputs]
exodus = true
perf_graph = true
[]
(test/tests/postprocessors/element_l2_difference/element_l2_difference.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
elem_type = QUAD9
[]
[Variables]
[./u]
[../]
[./v]
order = SECOND
family = LAGRANGE
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./force_u]
type = BodyForce
variable = u
function = 'x*x*x+y*y*y'
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[./force_v]
type = BodyForce
variable = v
function = 'x*x*x+y*y*y'
[../]
[]
[BCs]
[./left_u]
type = DirichletBC
variable = u
boundary = 'left bottom right top'
value = 0
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = 'left bottom right top'
value = 0
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Postprocessors]
[./l2_difference]
type = ElementL2Difference
variable = u
other_variable = v
[../]
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/ad_rz_cone_by_parts_steady.i)
[GlobalParams]
integrate_p_by_parts = true
[]
[Mesh]
file = '2d_cone.msh'
[]
[Problem]
coord_type = RZ
[]
[AuxVariables]
[vel_x]
order = SECOND
[]
[vel_y]
order = SECOND
[]
[]
[AuxKernels]
[vel_x]
type = VectorVariableComponentAux
variable = vel_x
vector_variable = velocity
component = 'x'
[]
[vel_y]
type = VectorVariableComponentAux
variable = vel_y
vector_variable = velocity
component = 'y'
[]
[]
[Variables]
[./velocity]
order = SECOND
family = LAGRANGE_VEC
[../]
[./p]
[../]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[./momentum_convection]
type = INSADMomentumAdvection
variable = velocity
[../]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
[../]
[]
[BCs]
[inlet]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom'
function_x = 0
function_y = 'inlet_func'
[../]
[wall]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'right'
function_x = 0
function_y = 0
[]
[axis]
type = ADVectorFunctionDirichletBC
variable = velocity
boundary = 'left'
set_y_comp = false
function_x = 0
[]
[]
[Functions]
[./inlet_func]
type = ParsedFunction
value = '-4 * x^2 + 1'
[../]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[ins_mat]
type = INSADMaterial
velocity = velocity
pressure = p
[]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = 'bjacobi ilu 4'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
csv = true
console = true
[./out]
type = Exodus
[../]
[]
[Postprocessors]
[./flow_in]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'bottom'
execute_on = 'timestep_end'
[../]
[./flow_out]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'top'
execute_on = 'timestep_end'
[../]
[]
(test/tests/fvkernels/mms/cylindrical/advection-reaction.i)
a=1.1
[Mesh]
[./gen_mesh]
type = GeneratedMeshGenerator
dim = 2
xmin = 2
xmax = 3
ymin = 0
ymax = 1
nx = 2
ny = 2
[../]
[]
[Problem]
coord_type = 'RZ'
[]
[Variables]
[./v]
family = MONOMIAL
order = CONSTANT
fv = true
initial_condition = 1
[../]
[]
[FVKernels]
[./advection]
type = FVAdvection
variable = v
velocity = '${a} ${a} 0'
advected_interp_method = 'average'
[../]
[reaction]
type = FVReaction
variable = v
[]
[body_v]
type = FVBodyForce
variable = v
function = 'forcing'
[]
[]
[FVBCs]
[advection]
type = FVAdvectionFunctionBC
boundary = 'left right top bottom'
exact_solution = 'exact'
variable = v
velocity = '${a} ${a} 0'
advected_interp_method = 'average'
[]
[]
[Functions]
[exact]
type = ParsedFunction
value = 'sin(x)*cos(y)'
[]
[forcing]
type = ParsedFunction
value = '-a*sin(x)*sin(y) + sin(x)*cos(y) + (x*a*cos(x)*cos(y) + a*sin(x)*cos(y))/x'
vars = 'a'
vals = '${a}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_shift_type -sub_pc_type'
petsc_options_value = 'asm NONZERO lu'
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[./error]
type = ElementL2Error
variable = v
function = exact
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/2d-rc-friction.i)
mu=1.1
rho=1
advected_interp_method='average'
velocity_interp_method='rc'
[Mesh]
[mesh]
type = CartesianMeshGenerator
dim = 2
dx = '2.5 2.5'
dy = '1.0'
ix = '20 20'
iy = '20'
subdomain_id = '1 2'
[]
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = PINSFVRhieChowInterpolator
u = superficial_vel_x
v = superficial_vel_y
pressure = pressure
porosity = porosity
[]
[]
[Variables]
inactive = 'lambda'
[superficial_vel_x]
type = PINSFVSuperficialVelocityVariable
initial_condition = 1
[]
[superficial_vel_y]
type = PINSFVSuperficialVelocityVariable
initial_condition = 1e-6
[]
[pressure]
type = INSFVPressureVariable
[]
[lambda]
family = SCALAR
order = FIRST
[]
[]
[AuxVariables]
[porosity]
family = MONOMIAL
order = CONSTANT
fv = true
initial_condition = 0.5
[]
[]
[FVKernels]
inactive = 'mean-pressure'
[mass]
type = PINSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = PINSFVMomentumAdvection
variable = superficial_vel_x
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
porosity = porosity
momentum_component = 'x'
[]
[u_viscosity]
type = PINSFVMomentumDiffusion
variable = superficial_vel_x
mu = ${mu}
porosity = porosity
momentum_component = 'x'
[]
[u_pressure]
type = PINSFVMomentumPressure
variable = superficial_vel_x
momentum_component = 'x'
pressure = pressure
porosity = porosity
[]
[u_friction]
type = PINSFVMomentumFriction
variable = superficial_vel_x
momentum_component = 'x'
porosity = porosity
Darcy_name = 'Darcy_coefficient'
Forchheimer_name = 'Forchheimer_coefficient'
rho = ${rho}
[]
[v_advection]
type = PINSFVMomentumAdvection
variable = superficial_vel_y
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
porosity = porosity
momentum_component = 'y'
[]
[v_viscosity]
type = PINSFVMomentumDiffusion
variable = superficial_vel_y
mu = ${mu}
porosity = porosity
momentum_component = 'y'
[]
[v_pressure]
type = PINSFVMomentumPressure
variable = superficial_vel_y
momentum_component = 'y'
pressure = pressure
porosity = porosity
[]
[v_friction]
type = PINSFVMomentumFriction
variable = superficial_vel_y
momentum_component = 'y'
porosity = porosity
Darcy_name = 'Darcy_coefficient'
Forchheimer_name = 'Forchheimer_coefficient'
rho = ${rho}
[]
[mean-pressure]
type = FVScalarLagrangeMultiplier
variable = pressure
lambda = lambda
phi0 = 0.01
[]
[]
[FVBCs]
inactive = 'free-slip-u free-slip-v'
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = superficial_vel_x
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = superficial_vel_y
function = 0
[]
[no-slip-u]
type = INSFVNoSlipWallBC
boundary = 'top'
variable = superficial_vel_x
function = 0
[]
[no-slip-v]
type = INSFVNoSlipWallBC
boundary = 'top'
variable = superficial_vel_y
function = 0
[]
[free-slip-u]
type = INSFVNaturalFreeSlipBC
boundary = 'top'
variable = superficial_vel_x
momentum_component = 'x'
[]
[free-slip-v]
type = INSFVNaturalFreeSlipBC
boundary = 'top'
variable = superficial_vel_y
momentum_component = 'y'
[]
[symmetry-u]
type = PINSFVSymmetryVelocityBC
boundary = 'bottom'
variable = superficial_vel_x
u = superficial_vel_x
v = superficial_vel_y
mu = ${mu}
momentum_component = 'x'
[]
[symmetry-v]
type = PINSFVSymmetryVelocityBC
boundary = 'bottom'
variable = superficial_vel_y
u = superficial_vel_x
v = superficial_vel_y
mu = ${mu}
momentum_component = 'y'
[]
[symmetry-p]
type = INSFVSymmetryPressureBC
boundary = 'bottom'
variable = pressure
[]
[outlet-p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 0
[]
[]
[Materials]
[darcy]
type = ADGenericVectorFunctorMaterial
prop_names = 'Darcy_coefficient Forchheimer_coefficient'
prop_values = '0.1 0.1 0.1 0.1 0.1 0.1'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 200 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-11
nl_abs_tol = 1e-14
[]
# Some basic Postprocessors to visually examine the solution
[Postprocessors]
[inlet-p]
type = SideAverageValue
variable = pressure
boundary = 'left'
[]
[outlet-u]
type = SideIntegralVariablePostprocessor
variable = superficial_vel_x
boundary = 'right'
[]
[]
[Outputs]
exodus = true
[]
(test/tests/postprocessors/nodal_extreme_value/nodal_proxy_extreme_value.i)
[Problem]
type = FEProblem
solve = false
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 40
ny = 40
[]
[AuxVariables]
[u]
[]
[w]
[]
[v_x]
[]
[v_y]
[]
[]
[AuxKernels]
[u]
type = FunctionAux
variable = u
function = u
[]
[w]
type = FunctionAux
variable = w
function = w
[]
[v_x]
type = FunctionAux
variable = v_x
function = v_x
[]
[v_y]
type = FunctionAux
variable = v_y
function = v_y
[]
[]
[Functions]
[u] # reaches a maximum value at (0.5, 0.6)
type = ParsedFunction
value = 'sin(pi*x)*sin(pi*y/1.2)'
[]
[w] # reaches a minium value at (0.7, 0.8)
type = ParsedFunction
value = '-sin(pi*x/1.4)*sin(pi*y/1.6)'
[]
[v_x]
type = ParsedFunction
value = 'x'
[]
[v_y]
type = ParsedFunction
value = 'y'
[]
[]
[Postprocessors]
# because we set v_x and v_y equal to the x and y coordinates, these two postprocessors
# should just return the point at which u reaches a maximum value
[max_v_from_proxy_x]
type = ElementExtremeValue
variable = v_x
proxy_variable = u
value_type = max
[]
[max_v_from_proxy_y]
type = ElementExtremeValue
variable = v_y
proxy_variable = u
value_type = max
[]
# because we set v_x and v_y equal to the x and y coordinates, these two postprocessors
# should just return the point at which w reaches a minimum value
[min_v_from_proxy_x]
type = ElementExtremeValue
variable = v_x
proxy_variable = w
value_type = min
[]
[min_v_from_proxy_y]
type = ElementExtremeValue
variable = v_y
proxy_variable = w
value_type = min
[]
[]
[Executioner]
type = Steady
# increase the quadrature order to get more quadrature points so that were closer
# to hitting the expect max/min
[Quadrature]
type = GAUSS
order = SECOND
[]
[]
[Outputs]
exodus = true
csv = true
[]
(test/tests/constraints/nodal_constraint/nodal_constraint_displaced_test.i)
[Mesh]
file = 2-lines.e
displacements = 'disp_x'
[]
[AuxVariables]
[./disp_x]
[../]
[]
[AuxKernels]
[./disp_x_ak]
type = ConstantAux
variable = disp_x
value = 1
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = 4
value = 3
[../]
[]
[Constraints]
[./c1]
type = EqualValueNodalConstraint
variable = u
primary = 0
secondary = 4
penalty = 100000
use_displaced_mesh = true
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/variables/fe_hier/hier-2-1d.i)
[Mesh]
type = GeneratedMesh
dim = 1
xmin = -1
xmax = 1
nx = 5
elem_type = EDGE3
[]
[Functions]
[./bc_fnl]
type = ParsedFunction
value = -2*x
[../]
[./bc_fnr]
type = ParsedFunction
value = 2*x
[../]
[./forcing_fn]
type = ParsedFunction
value = -2+x*x
[../]
[./solution]
type = ParsedGradFunction
value = x*x
grad_x = 2*x
[../]
[]
[Variables]
[./u]
order = SECOND
family = HIERARCHIC
[../]
[]
[Kernels]
active = 'diff forcing reaction'
[./diff]
type = Diffusion
variable = u
[../]
[./reaction]
type = Reaction
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
[./bc_left]
type = FunctionNeumannBC
variable = u
boundary = 'left'
function = bc_fnl
[../]
[./bc_right]
type = FunctionNeumannBC
variable = u
boundary = 'right'
function = bc_fnr
[../]
[]
[Postprocessors]
[./dofs]
type = NumDOFs
[../]
[./h]
type = AverageElementSize
[../]
[./L2error]
type = ElementL2Error
variable = u
function = solution
[../]
[./H1error]
type = ElementH1Error
variable = u
function = solution
[../]
[./H1Semierror]
type = ElementH1SemiError
variable = u
function = solution
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
csv = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/RZ_cone_high_reynolds.i)
[GlobalParams]
gravity = '0 0 0'
laplace = true
transient_term = false
supg = true
pspg = true
family = LAGRANGE
order = FIRST
[]
[Mesh]
file = 'cone_linear_alltri.e'
[]
[Problem]
coord_type = RZ
[]
[Preconditioning]
[./SMP_PJFNK]
type = SMP
full = true
solve_type = NEWTON
[../]
[]
[Executioner]
# type = Transient
# dt = 0.005
# dtmin = 0.005
# num_steps = 5
# l_max_its = 100
# Block Jacobi works well for this problem, as does "-pc_type asm
# -pc_asm_overlap 2", but an overlap of 1 does not work for some
# reason?
# petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_levels'
# petsc_options_value = 'bjacobi ilu 4'
# Note: The Steady executioner can be used for this problem, if you
# drop the INSMomentumTimeDerivative kernels and use the following
# direct solver options.
type = Steady
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
nl_rel_tol = 1e-12
nl_max_its = 20
[]
[Outputs]
csv = true
console = true
[./out]
type = Exodus
[../]
[]
[Variables]
[./vel_x]
# Velocity in radial (r) direction
[../]
[./vel_y]
# Velocity in axial (z) direction
[../]
[./p]
order = FIRST
[../]
[]
[BCs]
[./u_in]
type = DirichletBC
boundary = bottom
variable = vel_x
value = 0
[../]
[./v_in]
type = FunctionDirichletBC
boundary = bottom
variable = vel_y
function = 'inlet_func'
[../]
[./u_axis_and_walls]
type = DirichletBC
boundary = 'left right'
variable = vel_x
value = 0
[../]
[./v_no_slip]
type = DirichletBC
boundary = 'right'
variable = vel_y
value = 0
[../]
[]
[Kernels]
# [./x_momentum_time]
# type = INSMomentumTimeDerivative
# variable = vel_x
# [../]
# [./y_momentum_time]
# type = INSMomentumTimeDerivative
# variable = vel_y
# [../]
[./mass]
type = INSMassRZ
variable = p
u = vel_x
v = vel_y
pressure = p
[../]
[./x_momentum_space]
type = INSMomentumLaplaceFormRZ
variable = vel_x
u = vel_x
v = vel_y
pressure = p
component = 0
[../]
[./y_momentum_space]
type = INSMomentumLaplaceFormRZ
variable = vel_y
u = vel_x
v = vel_y
pressure = p
component = 1
[../]
[]
[Materials]
[./const]
type = GenericConstantMaterial
block = 1
prop_names = 'rho mu'
prop_values = '1 1e-3'
[../]
[]
[Functions]
[./inlet_func]
type = ParsedFunction
value = '-4 * x^2 + 1'
[../]
[]
[Postprocessors]
[./flow_in]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'bottom'
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./flow_out]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'top'
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[]
(modules/tensor_mechanics/test/tests/ad_isotropic_elasticity_tensor/youngs_modulus_poissons_ratio_test.i)
[Mesh]
type = GeneratedMesh
dim = 3
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./stress_11]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
add_variables = true
use_automatic_differentiation = true
[../]
[]
[AuxKernels]
[./stress_11]
type = ADRankTwoAux
variable = stress_11
rank_two_tensor = stress
index_j = 1
index_i = 1
[../]
[]
[BCs]
[./bottom]
type = ADDirichletBC
variable = disp_y
boundary = bottom
value = 0
[../]
[./left]
type = ADDirichletBC
variable = disp_x
boundary = left
value = 0
[../]
[./back]
type = ADDirichletBC
variable = disp_z
boundary = back
value = 0
[../]
[./top]
type = ADDirichletBC
variable = disp_y
boundary = top
value = 0.001
[../]
[]
[Materials]
[./stress]
type = ADComputeLinearElasticStress
[../]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
poissons_ratio = 0.1
youngs_modulus = 1e6
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
l_max_its = 20
nl_max_its = 10
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(modules/porous_flow/test/tests/newton_cooling/nc08.i)
# Newton cooling from a bar. 1-phase ideal fluid and heat, steady
[Mesh]
type = GeneratedMesh
dim = 2
nx = 100
ny = 1
xmin = 0
xmax = 100
ymin = 0
ymax = 1
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pressure temp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureVG
m = 0.8
alpha = 1e-5
[]
[]
[Variables]
[pressure]
[]
[temp]
[]
[]
[ICs]
# have to start these reasonably close to their steady-state values
[pressure]
type = FunctionIC
variable = pressure
function = '200-0.5*x'
[]
[temperature]
type = FunctionIC
variable = temp
function = 180+0.1*x
[]
[]
[Kernels]
[flux]
type = PorousFlowAdvectiveFlux
fluid_component = 0
gravity = '0 0 0'
variable = pressure
[]
[heat_advection]
type = PorousFlowHeatAdvection
gravity = '0 0 0'
variable = temp
[]
[]
[Modules]
[FluidProperties]
[idealgas]
type = IdealGasFluidProperties
molar_mass = 1.4
gamma = 1.2
mu = 1.2
[]
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
temperature = temp
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pressure
capillary_pressure = pc
[]
[massfrac]
type = PorousFlowMassFraction
[]
[dens0]
type = PorousFlowSingleComponentFluid
fp = idealgas
phase = 0
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1.1 0 0 0 1.1 0 0 0 1.1'
[]
[relperm]
type = PorousFlowRelativePermeabilityCorey # irrelevant in this fully-saturated situation
n = 2
phase = 0
[]
[]
[BCs]
[leftp]
type = DirichletBC
variable = pressure
boundary = left
value = 200
[]
[leftt]
type = DirichletBC
variable = temp
boundary = left
value = 180
[]
[newtonp]
type = PorousFlowPiecewiseLinearSink
variable = pressure
boundary = right
pt_vals = '-200 0 200'
multipliers = '-200 0 200'
use_mobility = true
use_relperm = true
fluid_phase = 0
flux_function = 0.005 # 1/2/L
[]
[newtont]
type = PorousFlowPiecewiseLinearSink
variable = temp
boundary = right
pt_vals = '-200 0 200'
multipliers = '-200 0 200'
use_mobility = true
use_relperm = true
use_enthalpy = true
fluid_phase = 0
flux_function = 0.005 # 1/2/L
[]
[]
[VectorPostprocessors]
[porepressure]
type = LineValueSampler
variable = pressure
start_point = '0 0.5 0'
end_point = '100 0.5 0'
sort_by = x
num_points = 11
execute_on = timestep_end
[]
[temperature]
type = LineValueSampler
variable = temp
start_point = '0 0.5 0'
end_point = '100 0.5 0'
sort_by = x
num_points = 11
execute_on = timestep_end
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = Newton
nl_rel_tol = 1E-10
nl_abs_tol = 1E-15
[]
[Outputs]
file_base = nc08
execute_on = timestep_end
exodus = true
[along_line]
type = CSV
execute_vector_postprocessors_on = timestep_end
[]
[]
(test/tests/misc/check_error/bad_material_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Materials]
active = empty
# Test for bad Material
[./empty]
type = Foo
block = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/indicators/laplacian_jump_indicator/biharmonic.i)
[GlobalParams]
# Parameters used by Functions.
vars = 'c'
vals = '50'
[]
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -.5
xmax = .5
ymin = -.5
ymax = .5
nx = 10
ny = 10
[]
[Variables]
[./u]
order = THIRD
family = HERMITE
[../]
[]
[Kernels]
[./biharmonic]
type = Biharmonic
variable = u
[../]
[./body_force]
type = BodyForce
variable = u
function = forcing_func
[../]
[]
[BCs]
active = 'all_value all_flux'
[./all_value]
type = FunctionPenaltyDirichletBC
variable = u
boundary = 'left right top bottom'
function = u_func
penalty = 1e10
[../]
[./all_flux]
type = FunctionPenaltyFluxBC
variable = u
boundary = 'left right top bottom'
function = u_func
penalty = 1e10
[../]
[./all_laplacian]
type = BiharmonicLapBC
variable = u
boundary = 'left right top bottom'
laplacian_function = lapu_func
[../]
[]
[Adaptivity]
[Indicators]
[error]
type = LaplacianJumpIndicator
variable = u
scale_by_flux_faces = true
[]
[]
[]
[Executioner]
type = Steady
# Note: the unusually tight tolerances here are due to the penalty
# BCs (currently the only way of accurately Dirichlet boundary
# conditions on Hermite elements in MOOSE).
nl_rel_tol = 1.e-15
l_tol = 1.e-15
# We have exact Jacobians
solve_type = 'NEWTON'
# Use 6x6 quadrature to ensure the forcing function is integrated
# accurately.
[./Quadrature]
type = GAUSS
order = ELEVENTH
[../]
[]
[Functions]
[./u_func]
type = ParsedGradFunction
value = 'exp(-c*(x^2+y^2))'
grad_x = '-2*c*exp(-c*(x^2+y^2))*x'
grad_y = '-2*c*exp(-c*(x^2+y^2))*y'
[../]
[./lapu_func]
type = ParsedFunction
value = '4*c*(c*(x^2+y^2) - 1)*exp(-c*(x^2+y^2))'
[../]
[./forcing_func]
type = ParsedFunction
value = '16*c^2*(c^2*(x^2+y^2)^2 - 4*c*(x^2+y^2) + 2)*exp(-c*(x^2+y^2))'
[../]
[]
[Postprocessors]
[./l2_error]
type = ElementL2Error
variable = u
function = u_func
[../]
[./h1_error]
type = ElementH1Error
variable = u
function = u_func
[../]
[]
[Outputs]
exodus = true
[]
(test/tests/dirackernels/material_point_source/material_point_source.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
elem_type = QUAD4
uniform_refine = 4
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[DiracKernels]
[./material_source]
type = MaterialPointSource
variable = u
point = '0.2 0.3 0.0'
material_prop = 'matp'
prop_state = 'current'
[../]
[]
[Materials]
[./xmat]
# MTMaterial provides 'matp', value is the 'shift' added to the x-coordinate
# when computing the Material property value.
type = MTMaterial
block = '0'
value = 0.
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/navier_stokes/test/tests/postprocessors/flow_rates/conservation_PINSFV.i)
mu=1
rho=1
advected_interp_method='average'
velocity_interp_method='rc'
[Mesh]
inactive = 'mesh internal_boundary_bot internal_boundary_top'
[mesh]
type = CartesianMeshGenerator
dim = 2
dx = '1'
dy = '1 1 1'
ix = '5'
iy = '5 5 5'
subdomain_id = '1
2
3'
[]
[internal_boundary_bot]
type = SideSetsBetweenSubdomainsGenerator
input = mesh
new_boundary = 'internal_bot'
primary_block = 1
paired_block = 2
[]
[internal_boundary_top]
type = SideSetsBetweenSubdomainsGenerator
input = internal_boundary_bot
new_boundary = 'internal_top'
primary_block = 2
paired_block = 3
[]
[diverging_mesh]
type = FileMeshGenerator
file = 'expansion_quad.e'
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
[]
[UserObjects]
[rc]
type = PINSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
porosity = porosity
[]
[]
[Variables]
[u]
type = PINSFVSuperficialVelocityVariable
initial_condition = 0
[]
[v]
type = PINSFVSuperficialVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[temperature]
type = INSFVEnergyVariable
[]
[]
[AuxVariables]
[advected_density]
order = CONSTANT
family = MONOMIAL
fv = true
initial_condition = ${rho}
[]
[porosity]
order = CONSTANT
family = MONOMIAL
fv = true
initial_condition = 0.5
[]
[]
[FVKernels]
[mass]
type = PINSFVMassAdvection
variable = pressure
rho = ${rho}
[]
[u_advection]
type = PINSFVMomentumAdvection
variable = u
rho = ${rho}
porosity = porosity
momentum_component = 'x'
[]
[u_viscosity]
type = PINSFVMomentumDiffusion
variable = u
force_boundary_execution = true
porosity = porosity
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = PINSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
porosity = porosity
[]
[v_advection]
type = PINSFVMomentumAdvection
variable = v
rho = ${rho}
porosity = porosity
momentum_component = 'y'
[]
[v_viscosity]
type = PINSFVMomentumDiffusion
variable = v
force_boundary_execution = true
porosity = porosity
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = PINSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
porosity = porosity
[]
[temp_advection]
type = PINSFVEnergyAdvection
variable = temperature
advected_interp_method = 'upwind'
[]
[temp_source]
type = FVBodyForce
variable = temperature
function = 10
block = 1
[]
[]
[FVBCs]
inactive = 'noslip-u noslip-v'
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = u
function = 0
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = v
function = 1
[]
[noslip-u]
type = INSFVNoSlipWallBC
boundary = 'right'
variable = u
function = 0
[]
[noslip-v]
type = INSFVNoSlipWallBC
boundary = 'right'
variable = v
function = 0
[]
[free-slip-u]
type = INSFVNaturalFreeSlipBC
boundary = 'right'
variable = u
momentum_component = 'x'
[]
[free-slip-v]
type = INSFVNaturalFreeSlipBC
boundary = 'right'
variable = v
momentum_component = 'y'
[]
[axis-u]
type = PINSFVSymmetryVelocityBC
boundary = 'left'
variable = u
u = u
v = v
mu = ${mu}
momentum_component = x
[]
[axis-v]
type = PINSFVSymmetryVelocityBC
boundary = 'left'
variable = v
u = u
v = v
mu = ${mu}
momentum_component = y
[]
[axis-p]
type = INSFVSymmetryPressureBC
boundary = 'left'
variable = pressure
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'top'
variable = pressure
function = 0
[]
[inlet_temp]
type = FVNeumannBC
boundary = 'bottom'
variable = temperature
value = 300
[]
[]
[Materials]
[ins_fv]
type = INSFVEnthalpyMaterial
temperature = 'temperature'
rho = ${rho}
[]
[advected_material_property]
type = ADGenericFunctorMaterial
prop_names = 'advected_rho cp'
prop_values ='${rho} 1'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 200 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Postprocessors]
[inlet_mass_variable]
type = VolumetricFlowRate
boundary = bottom
vel_x = u
vel_y = v
advected_quantity = advected_density
[]
[inlet_mass_constant]
type = VolumetricFlowRate
boundary = bottom
vel_x = u
vel_y = v
advected_quantity = ${rho}
[]
[inlet_mass_matprop]
type = VolumetricFlowRate
boundary = bottom
vel_x = u
vel_y = v
advected_quantity = 'advected_rho'
[]
[mid1_mass]
type = VolumetricFlowRate
boundary = internal_bot
vel_x = u
vel_y = v
advected_quantity = ${rho}
[]
[mid2_mass]
type = VolumetricFlowRate
boundary = internal_top
vel_x = u
vel_y = v
advected_quantity = ${rho}
[]
[outlet_mass]
type = VolumetricFlowRate
boundary = top
vel_x = u
vel_y = v
advected_quantity = ${rho}
[]
[inlet_momentum_x]
type = VolumetricFlowRate
boundary = bottom
vel_x = u
vel_y = v
advected_quantity = u
[]
[inlet_momentum_y]
type = VolumetricFlowRate
boundary = bottom
vel_x = u
vel_y = v
advected_quantity = v
[]
[mid1_advected_energy]
type = VolumetricFlowRate
boundary = internal_bot
vel_x = u
vel_y = v
advected_quantity = 'rho_cp_temp'
advected_interp_method = 'upwind'
[]
[mid2_advected_energy]
type = VolumetricFlowRate
boundary = internal_top
vel_x = u
vel_y = v
advected_quantity = 'rho_cp_temp'
advected_interp_method = 'upwind'
[]
[outlet_advected_energy]
type = VolumetricFlowRate
boundary = top
vel_x = u
vel_y = v
advected_quantity = 'rho_cp_temp'
advected_interp_method = 'upwind'
[]
[]
[Outputs]
exodus = true
csv = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/cylindrical/no-slip-tris-action.i)
mu=1
rho=1
[Mesh]
type = GeneratedMesh
nx = 4
ny = 4
xmax = 3.9
ymax = 4.1
elem_type = TRI3
dim = 2
[]
[Problem]
coord_type = 'RZ'
[]
[Modules]
[NavierStokesFV]
compressibility = 'incompressible'
density = 'rho'
dynamic_viscosity = 'mu'
porosity = 'porosity'
initial_velocity = '1e-15 1e-15 0'
initial_pressure = 0.0
inlet_boundaries = 'bottom'
momentum_inlet_types = 'fixed-velocity'
momentum_inlet_function = '0 1'
wall_boundaries = 'left right'
momentum_wall_types = 'symmetry noslip'
outlet_boundaries = 'top'
momentum_outlet_types = 'fixed-pressure'
pressure_function = '0'
momentum_two_term_bc_expansion = true
pressure_two_term_bc_expansion = true
[]
[]
[Materials]
[const]
type = ADGenericFunctorMaterial
prop_names = 'rho mu'
prop_values = '${rho} ${mu}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options = '-options_left'
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_shift_type -ksp_gmres_restart'
petsc_options_value = 'asm lu NONZERO 200'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Postprocessors]
[in]
type = SideIntegralVariablePostprocessor
variable = vel_y
boundary = 'bottom'
[]
[out]
type = SideIntegralVariablePostprocessor
variable = vel_y
boundary = 'top'
[]
[num_lin]
type = NumLinearIterations
outputs = 'console'
[]
[num_nl]
type = NumNonlinearIterations
outputs = 'console'
[]
[cum_lin]
type = CumulativeValuePostprocessor
outputs = 'console'
postprocessor = 'num_lin'
[]
[cum_nl]
type = CumulativeValuePostprocessor
outputs = 'console'
postprocessor = 'num_nl'
[]
[]
[Outputs]
exodus = true
csv = true
[]
(modules/porous_flow/test/tests/thm_rehbinder/fixed_outer.i)
[Mesh]
[annular]
type = AnnularMeshGenerator
nr = 40
nt = 16
rmin = 0.1
rmax = 1
dmin = 0.0
dmax = 90
growth_r = 1.1
[]
[make3D]
input = annular
type = MeshExtruderGenerator
bottom_sideset = bottom
top_sideset = top
extrusion_vector = '0 0 1'
num_layers = 1
[]
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
PorousFlowDictator = dictator
biot_coefficient = 1.0
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[disp_z]
[]
[porepressure]
[]
[temperature]
[]
[]
[BCs]
[plane_strain]
type = DirichletBC
variable = disp_z
value = 0
boundary = 'top bottom'
[]
[ymin]
type = DirichletBC
variable = disp_y
value = 0
boundary = dmin
[]
[xmin]
type = DirichletBC
variable = disp_x
value = 0
boundary = dmax
[]
[cavity_temperature]
type = DirichletBC
variable = temperature
value = 1000
boundary = rmin
[]
[cavity_porepressure]
type = DirichletBC
variable = porepressure
value = 1E6
boundary = rmin
[]
[cavity_zero_effective_stress_x]
type = Pressure
variable = disp_x
function = 1E6
boundary = rmin
use_displaced_mesh = false
[]
[cavity_zero_effective_stress_y]
type = Pressure
variable = disp_y
function = 1E6
boundary = rmin
use_displaced_mesh = false
[]
[outer_temperature]
type = DirichletBC
variable = temperature
value = 0
boundary = rmax
[]
[outer_pressure]
type = DirichletBC
variable = porepressure
value = 0
boundary = rmax
[]
[fixed_outer_x]
type = DirichletBC
variable = disp_x
value = 0
boundary = rmax
[]
[fixed_outer_y]
type = DirichletBC
variable = disp_y
value = 0
boundary = rmax
[]
[]
[AuxVariables]
[stress_rr]
family = MONOMIAL
order = CONSTANT
[]
[stress_pp]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[stress_rr]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = stress_rr
scalar_type = RadialStress
point1 = '0 0 0'
point2 = '0 0 1'
[]
[stress_pp]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = stress_pp
scalar_type = HoopStress
point1 = '0 0 0'
point2 = '0 0 1'
[]
[]
[Modules]
[FluidProperties]
[the_simple_fluid]
type = SimpleFluidProperties
thermal_expansion = 0.0
bulk_modulus = 1E12
viscosity = 1.0E-3
density0 = 1000.0
cv = 1000.0
cp = 1000.0
porepressure_coefficient = 0.0
[]
[]
[]
[PorousFlowBasicTHM]
coupling_type = ThermoHydroMechanical
multiply_by_density = false
add_stress_aux = true
porepressure = porepressure
temperature = temperature
eigenstrain_names = thermal_contribution
gravity = '0 0 0'
fp = the_simple_fluid
[]
[Materials]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1E10
poissons_ratio = 0.2
[]
[strain]
type = ComputeSmallStrain
eigenstrain_names = thermal_contribution
[]
[thermal_contribution]
type = ComputeThermalExpansionEigenstrain
temperature = temperature
thermal_expansion_coeff = 1E-6
eigenstrain_name = thermal_contribution
stress_free_temperature = 0.0
[]
[stress]
type = ComputeLinearElasticStress
[]
[porosity]
type = PorousFlowPorosityConst # only the initial value of this is ever used
porosity = 0.1
[]
[biot_modulus]
type = PorousFlowConstantBiotModulus
solid_bulk_compliance = 1E-10
fluid_bulk_modulus = 1E12
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1E-12 0 0 0 1E-12 0 0 0 1E-12'
[]
[thermal_expansion]
type = PorousFlowConstantThermalExpansionCoefficient
fluid_coefficient = 1E-6
drained_coefficient = 1E-6
[]
[thermal_conductivity]
type = PorousFlowThermalConductivityIdeal
dry_thermal_conductivity = '1E6 0 0 0 1E6 0 0 0 1E6'
[]
[]
[VectorPostprocessors]
[P]
type = LineValueSampler
start_point = '0.1 0 0'
end_point = '1.0 0 0'
num_points = 10
sort_by = x
variable = porepressure
[]
[T]
type = LineValueSampler
start_point = '0.1 0 0'
end_point = '1.0 0 0'
num_points = 10
sort_by = x
variable = temperature
[]
[U]
type = LineValueSampler
start_point = '0.1 0 0'
end_point = '1.0 0 0'
num_points = 10
sort_by = x
variable = disp_x
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -snes_rtol'
petsc_options_value = 'gmres asm lu 1E-8'
[]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
file_base = fixed_outer
execute_on = timestep_end
csv = true
[]
(test/tests/mesh/side_list_from_node_list/side_list_from_node_list.i)
[Mesh]
type = FileMesh
file = square_nodesets_only.e
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = NeumannBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/preconditioners/smp/smp_single_test.i)
#
# This is not very strong test since the problem being solved is linear, so the difference between
# full Jacobian and block diagonal preconditioner are not that big
#
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 10
ny = 10
elem_type = QUAD4
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[./v]
order = FIRST
family = LAGRANGE
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
off_diag_row = 'u'
off_diag_column = 'v'
[../]
[]
[Kernels]
active = 'diff_u conv_u diff_v'
[./diff_u]
type = Diffusion
variable = u
[../]
[./conv_u]
type = CoupledForce
variable = u
v = v
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[BCs]
active = 'left_u top_v bottom_v'
[./left_u]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 3
value = 9
[../]
[./bottom_v]
type = DirichletBC
variable = v
boundary = 0
value = 5
[../]
[./top_v]
type = DirichletBC
variable = v
boundary = 2
value = 2
[../]
[]
[Executioner]
type = Steady
# l_max_its = 1
# nl_max_its = 1
# nl_rel_tol = 1e-10
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/variables/optionally_coupled/optionally_coupled_twovar.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./v]
initial_condition = 1
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./optional_coupling]
type = OptionallyVectorCoupledForce
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_mortar/ref.i)
[Mesh]
file = 3blk.e
[]
[Variables]
[./temp]
order = FIRST
family = LAGRANGE
block = '1 2 3'
[../]
[]
[Materials]
[./left]
type = HeatConductionMaterial
block = 1
thermal_conductivity = 1000
specific_heat = 1
[../]
[./right]
type = HeatConductionMaterial
block = 2
thermal_conductivity = 500
specific_heat = 1
[../]
[./middle]
type = HeatConductionMaterial
block = 3
thermal_conductivity = 100
specific_heat = 1
[../]
[]
[Kernels]
[./hc]
type = HeatConduction
variable = temp
use_displaced_mesh = false
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = temp
boundary = 'left'
value = 1
[../]
[./right]
type = DirichletBC
variable = temp
boundary = 'right'
value = 0
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
nl_rel_tol = 1e-11
l_tol = 1e-11
[]
[Outputs]
exodus = true
[]
(test/tests/problems/action_custom_fe_problem/action_custom_fe_problem_test.i)
# This test demonstrates that a Problem can be created through an Action (possibly associated with
# special syntax), that may or may not even have a type specified.
# See the custom "TestProblem" block below.
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 4
ny = 4
elem_type = QUAD4
[]
[TestProblem]
# Creates a custom problem through a meta-action.
name = 'MOOSE Action Test problem'
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
[]
(modules/combined/test/tests/linear_elasticity/extra_stress.i)
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 128
ny = 1
xmax = 3.2
ymax = 0.025
elem_type = QUAD4
[]
[Modules/TensorMechanics/Master/All]
add_variables = true
generate_output = 'stress_xx stress_xy stress_yy stress_zz strain_xx strain_xy strain_yy'
[]
[AuxVariables]
[./c]
[../]
[]
[ICs]
[./c_IC]
type = BoundingBoxIC
variable = c
x1 = -1
y1 = -1
x2 = 1.6
y2 = 1
inside = 0
outside = 1
block = 0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeElasticityTensor
block = 0
C_ijkl = '104 74 74 104 74 104 47.65 47.65 47.65'
fill_method = symmetric9
base_name = matrix
[../]
[./stress]
type = ComputeLinearElasticStress
block = 0
base_name = matrix
[../]
[./strain]
type = ComputeSmallStrain
block = 0
base_name = matrix
[../]
[./elasticity_tensor_ppt]
type = ComputeElasticityTensor
block = 0
C_ijkl = '0.104 0.074 0.074 0.104 0.074 0.104 0.04765 0.04765 0.04765'
fill_method = symmetric9
base_name = ppt
[../]
[./stress_ppt]
type = ComputeLinearElasticStress
block = 0
base_name = ppt
[../]
[./strain_ppt]
type = ComputeSmallStrain
block = 0
base_name = ppt
[../]
[./const_stress]
type = ComputeExtraStressConstant
block = 0
base_name = ppt
extra_stress_tensor = '-0.288 -0.373 -0.2747 0 0 0'
[../]
[./global_stress]
type = TwoPhaseStressMaterial
base_A = matrix
base_B = ppt
[../]
[./switching]
type = SwitchingFunctionMaterial
eta = c
[../]
[]
[BCs]
active = 'left_x right_x bottom_y top_y'
[./bottom_y]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0
[../]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = left
value = 0
[../]
[./right_x]
type = DirichletBC
variable = disp_x
boundary = right
value = 0
[../]
[./top_y]
type = DirichletBC
variable = disp_y
boundary = top
value = 0
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/console/console_no_outputs_block.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
(test/tests/kernels/tag_errors/tag_doesnt_exist/bad_transient.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = CoefDiffusion
variable = u
coef = 0.1
[../]
[./time]
type = TimeDerivative
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
# Preconditioned JFNK (default)
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/interfacekernels/gmsh_sidesets/coupled_value_coupled_flux.i)
[Mesh]
file = gmsh_mesh.msh
[]
[Variables]
[./u]
block = 6
[../]
[./v]
block = 5
[../]
[]
[Kernels]
[./diff_u]
type = CoeffParamDiffusion
variable = u
D = 4
block = 6
[../]
[./diff_v]
type = CoeffParamDiffusion
variable = v
D = 2
block = 5
[../]
[./source_u]
type = BodyForce
variable = u
value = 1
[../]
[]
[InterfaceKernels]
[./interface]
type = PenaltyInterfaceDiffusion
variable = u
neighbor_var = v
boundary = '1 2'
penalty = 1e6
[../]
[]
[BCs]
[./u]
type = VacuumBC
variable = u
boundary = 4
[../]
[./v]
type = VacuumBC
variable = v
boundary = 3
[../]
[]
[Postprocessors]
[./u_int]
type = ElementIntegralVariablePostprocessor
variable = u
block = 6
[../]
[./v_int]
type = ElementIntegralVariablePostprocessor
variable = v
block = 5
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
print_linear_residuals = true
[]
(modules/functional_expansion_tools/test/tests/errors/missing_series_x.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Functions]
[./series]
type = FunctionSeries
series_type = Cartesian
orders = '0'
physical_bounds = '-1 1'
[../]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
(modules/heat_conduction/test/tests/code_verification/cylindrical_test_no4.i)
# Problem II.4
#
# An infinitely long hollow cylinder has thermal conductivity k and internal
# heat generation q. Its inner radius is ri and outer radius is ro.
# A constant heat flux is applied to the inside surface qin and
# the outside surface is exposed to a fluid temperature T and heat transfer
# coefficient h, which results in the convective boundary condition.
#
# REFERENCE:
# A. Toptan, et al. (Mar.2020). Tech. rep. CASL-U-2020-1939-000, SAND2020-3887 R. DOI:10.2172/1614683.
[Mesh]
[./geom]
type = GeneratedMeshGenerator
dim = 1
elem_type = EDGE2
xmin = 0.2
nx = 4
[../]
[]
[Variables]
[./u]
order = FIRST
[../]
[]
[Problem]
coord_type = RZ
[]
[Functions]
[./exact]
type = ParsedFunction
vars = 'qin q k ri ro uf h'
vals = '100 1200 1.0 0.2 1 100 10'
value = 'uf+ (0.25*q/k) * ( 2*k*(ro^2-ri^2)/(h*ro) + ro^2-x^2 + 2*ri^2*log(x/ro)) + (k/(h*ro) - log(x/ro)) * qin * ri / k'
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = u
[../]
[./heatsource]
type = HeatSource
function = 1200
variable = u
[../]
[]
[BCs]
[./ui]
type = NeumannBC
boundary = left
variable = u
value = 100
[../]
[./uo]
type = CoupledConvectiveHeatFluxBC
boundary = right
variable = u
htc = 10.0
T_infinity = 100
[../]
[]
[Materials]
[./property]
type = GenericConstantMaterial
prop_names = 'density specific_heat thermal_conductivity'
prop_values = '1.0 1.0 1.0'
[../]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[./error]
type = ElementL2Error
function = exact
variable = u
[../]
[./h]
type = AverageElementSize
[]
[]
[Outputs]
csv = true
[]
(test/tests/auxkernels/aux_nodal_scalar_kernel/aux_nodal_scalar_kernel.i)
[Mesh]
type = GeneratedMesh
dim = 1
xmin = 0
xmax = 1
nx = 10
parallel_type = replicated
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 0
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 2
[../]
[]
[AuxVariables]
[./bc_sum]
family = SCALAR
order = FIRST
[../]
[]
[AuxScalarKernels]
[./sk]
type = SumNodalValuesAux
variable = bc_sum
nodes = '0 10'
sum_var = u
[../]
[]
[Postprocessors]
[./sum]
type = ScalarVariable
variable = bc_sum
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
hide = bc_sum
[]
(test/tests/ics/vector_constant_ic/vector_short_constant_ic.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 2
ny = 2
nz = 2
[]
[Problem]
solve = false
kernel_coverage_check = false
[]
[Variables]
[./A]
family = LAGRANGE_VEC
order = FIRST
initial_condition = '2 3 4'
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(test/tests/auxkernels/error_function_aux/error_function_aux.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./element_l2_error]
# Aux field variable representing the L2 error on each element
order = CONSTANT
family = MONOMIAL
[../]
[./element_h1_error]
# Aux field variable representing the H1 error on each element
order = CONSTANT
family = MONOMIAL
[../]
[./element_l2_norm]
# Aux field variable representing the L^2 norm of the solution variable
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./exact_fn]
type = ParsedFunction
value = sin(2*pi*x)*sin(2*pi*y)
[../]
[./forcing_fn]
type = ParsedFunction
value = 8*pi^2*sin(2*pi*x)*sin(2*pi*y)
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[AuxKernels]
[./l2_norm_aux]
type = ElementLpNormAux
variable = element_l2_norm
coupled_variable = u
[../]
[./l2_error_aux]
type = ElementL2ErrorFunctionAux
variable = element_l2_error
# A function representing the exact solution for the solution
function = exact_fn
# The nonlinear variable representing the FEM solution
coupled_variable = u
[../]
[./h1_error_aux]
type = ElementH1ErrorFunctionAux
variable = element_h1_error
# A function representing the exact solution for the solution
function = exact_fn
# The nonlinear variable representing the FEM solution
coupled_variable = u
[../]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
boundary = 'bottom left right top'
function = exact_fn
[../]
[]
[Postprocessors]
[./L2_error]
# The L2 norm of the error over the entire mesh. Note: this is
# *not* equal to the sum over all the elements of the L2-error
# norms.
type = ElementL2Error
variable = u
function = exact_fn
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/ics/test_function.i)
[Mesh]
[cartesian]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 1
ymax = 2
nx = 3
ny = 3
[]
[]
[Modules]
[FluidProperties]
[fp]
type = IdealGasFluidProperties
[]
[]
[]
[Problem]
kernel_coverage_check = false
solve = false
skip_nl_system_check = true
[]
[AuxVariables]
[pressure]
type = MooseVariableFVReal
[]
[vel_x]
type = MooseVariableFVReal
[]
[vel_y]
type = MooseVariableFVReal
[]
[vel_z]
type = MooseVariableFVReal
[]
[temperature]
type = MooseVariableFVReal
[]
[ht]
type = MooseVariableFVReal
[]
[e]
type = MooseVariableFVReal
[]
[Mach]
type = MooseVariableFVReal
[]
[rho]
type = MooseVariableFVReal
[]
[rhou]
type = MooseVariableFVReal
[]
[rhov]
type = MooseVariableFVReal
[]
[rhow]
type = MooseVariableFVReal
[]
[rho_et]
type = MooseVariableFVReal
[]
[specific_volume]
type = MooseVariableFVReal
[]
[pressure_2]
[]
[vel_x_2]
[]
[vel_y_2]
[]
[vel_z_2]
[]
[temperature_2]
[]
[ht_2]
[]
[e_2]
[]
[Mach_2]
[]
[rho_2]
[]
[rhou_2]
[]
[rhov_2]
[]
[rhow_2]
[]
[rho_et_2]
[]
[specific_volume_2]
[]
[]
[GlobalParams]
fluid_properties = 'fp'
initial_pressure = p_func
initial_temperature = T_func
initial_velocity = 'vx vy vz'
[]
[Functions]
[p_func]
type = ParsedFunction
value = '3+3+1e5 - x'
[]
[T_func]
type = ParsedFunction
value = '273.15 + x*y*2'
[]
[vx]
type = ParsedFunction
value = '14'
[]
[vy]
type = ParsedFunction
value = '10 + x'
[]
[vz]
type = ParsedFunction
value = '12 -7*y'
[]
[]
[ICs]
[p]
type = NSFunctionInitialCondition
variable = 'pressure'
[]
[vel_x]
type = NSFunctionInitialCondition
variable = 'vel_x'
[]
[vel_y]
type = NSFunctionInitialCondition
variable = 'vel_y'
[]
[vel_z]
type = NSFunctionInitialCondition
variable = 'vel_z'
[]
[temperature]
type = NSFunctionInitialCondition
variable = 'temperature'
[]
[ht]
type = NSFunctionInitialCondition
variable = 'ht'
[]
[e]
type = NSFunctionInitialCondition
variable = 'e'
[]
[Mach]
type = NSFunctionInitialCondition
variable = 'Mach'
[]
[rho]
type = NSFunctionInitialCondition
fluid_properties = 'fp'
initial_pressure = p_func
initial_temperature = T_func
initial_velocity = 'vx vy vz'
variable = 'rho'
[]
[rhou]
type = NSFunctionInitialCondition
variable = 'rhou'
[]
[rhov]
type = NSFunctionInitialCondition
variable = 'rhov'
[]
[rhow]
type = NSFunctionInitialCondition
variable = 'rhow'
[]
[rho_et]
type = NSFunctionInitialCondition
variable = 'rho_et'
[]
[specific_volume]
type = NSFunctionInitialCondition
variable = 'specific_volume'
[]
[p_2]
type = NSFunctionInitialCondition
variable = 'pressure_2'
variable_type = 'pressure'
[]
[vel_x_2]
type = NSFunctionInitialCondition
variable = 'vel_x_2'
variable_type = 'vel_x'
[]
[vel_y_2]
type = NSFunctionInitialCondition
variable = 'vel_y_2'
variable_type = 'vel_y'
[]
[vel_z_2]
type = NSFunctionInitialCondition
variable = 'vel_z_2'
variable_type = 'vel_z'
[]
[temperature_2]
type = NSFunctionInitialCondition
variable = 'temperature_2'
variable_type = 'temperature'
[]
[ht_2]
type = NSFunctionInitialCondition
variable = 'ht_2'
variable_type = 'ht'
[]
[e_2]
type = NSFunctionInitialCondition
variable = 'e_2'
variable_type = 'e'
[]
[Mach_2]
type = NSFunctionInitialCondition
variable = 'Mach_2'
variable_type = 'Mach'
[]
[rho_2]
type = NSFunctionInitialCondition
variable = 'rho_2'
variable_type = 'rho'
[]
[rhou_2]
type = NSFunctionInitialCondition
variable = 'rhou_2'
variable_type = 'rhou'
[]
[rhov_2]
type = NSFunctionInitialCondition
variable = 'rhov_2'
variable_type = 'rhov'
[]
[rhow_2]
type = NSFunctionInitialCondition
variable = 'rhow_2'
variable_type = 'rhow'
[]
[rho_et_2]
type = NSFunctionInitialCondition
variable = 'rho_et_2'
variable_type = 'rho_et'
[]
[specific_volume_2]
type = NSFunctionInitialCondition
variable = 'specific_volume_2'
variable_type = 'specific_volume'
[]
[]
[Executioner]
type = Steady
[]
[Debug]
show_actions = true
[]
[Outputs]
exodus = true
[]
(test/tests/restart/restart_diffusion/restart_diffusion_test_steady.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Postprocessors]
[./unorm]
type = ElementL2Norm
variable = u
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = steady_out
exodus = true
checkpoint = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/discontinuous-body-forces.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'
[GlobalParams]
two_term_boundary_expansion = true
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 10
ymin = -1
ymax = 1
nx = 100
ny = 9
[]
[subdomain]
type = SubdomainBoundingBoxGenerator
bottom_left = '5 -1 0'
top_right = '10 1 0'
block_id = 1
input = gen
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[FVKernels]
inactive='u_friction_quad v_friction_quad'
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[u_friction_linear]
type = INSFVMomentumFriction
variable = u
linear_coef_name = friction_coefficient
momentum_component = 'x'
block = '1'
[]
[u_friction_quad]
type = INSFVMomentumFriction
variable = u
quadratic_coef_name = friction_coefficient
momentum_component = 'x'
block = '1'
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[v_friction_linear]
type = INSFVMomentumFriction
variable = v
linear_coef_name = friction_coefficient
momentum_component = 'y'
block = '1'
[]
[v_friction_quad]
type = INSFVMomentumFriction
variable = v
quadratic_coef_name = friction_coefficient
momentum_component = 'y'
block = '1'
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = '0'
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = u
function = 0
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = v
function = 0
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = '0'
[]
[]
[Materials]
[friction_coefficient]
type = ADGenericFunctorMaterial
prop_names = 'friction_coefficient'
prop_values = '25'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 200 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_mortar/modular_gap_heat_transfer_mortar_displaced_radiation_conduction_separate.i)
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
[file]
type = FileMeshGenerator
file = 2blk-gap.e
[]
[secondary]
type = LowerDBlockFromSidesetGenerator
sidesets = '101'
new_block_id = 10001
new_block_name = 'secondary_lower'
input = file
[]
[primary]
type = LowerDBlockFromSidesetGenerator
sidesets = '100'
new_block_id = 10000
new_block_name = 'primary_lower'
input = secondary
[]
allow_renumbering = false
[]
[Problem]
kernel_coverage_check = false
material_coverage_check = false
[]
[Variables]
[temp]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[disp_x]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[disp_y]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[lm]
order = FIRST
family = LAGRANGE
block = 'secondary_lower'
[]
[lm_conduction]
order = FIRST
family = LAGRANGE
block = 'secondary_lower'
[]
[]
[Materials]
[left]
type = ADHeatConductionMaterial
block = 1
thermal_conductivity = 0.01
specific_heat = 1
[]
[right]
type = ADHeatConductionMaterial
block = 2
thermal_conductivity = 0.005
specific_heat = 1
[]
[]
[Kernels]
[hc_displaced_block]
type = ADHeatConduction
variable = temp
use_displaced_mesh = true
block = '1'
[]
[hc_undisplaced_block]
type = ADHeatConduction
variable = temp
use_displaced_mesh = false
block = '2'
[]
[disp_x]
type = Diffusion
variable = disp_x
block = '1 2'
[]
[disp_y]
type = Diffusion
variable = disp_y
block = '1 2'
[]
[]
[UserObjects]
[radiation]
type = GapFluxModelRadiation
temperature = temp
boundary = 100
primary_emissivity = 1.0
secondary_emissivity = 1.0
use_displaced_mesh = true
[]
[conduction]
type = GapFluxModelConduction
temperature = temp
boundary = 100
gap_conductivity = 0.02
use_displaced_mesh = true
[]
[]
[Constraints]
[ced_radiation]
type = ModularGapConductanceConstraint
variable = lm
secondary_variable = temp
use_displaced_mesh = true
primary_boundary = 100
primary_subdomain = 10000
secondary_boundary = 101
secondary_subdomain = 10001
gap_flux_models = 'radiation'
[]
[ced_conduction]
type = ModularGapConductanceConstraint
variable = lm_conduction
secondary_variable = temp
use_displaced_mesh = true
primary_boundary = 100
primary_subdomain = 10000
secondary_boundary = 101
secondary_subdomain = 10001
gap_flux_models = 'conduction'
[]
[]
[BCs]
[left]
type = DirichletBC
variable = temp
boundary = 'left'
value = 100
[]
[right]
type = DirichletBC
variable = temp
boundary = 'right'
value = 0
[]
[left_disp_x]
type = DirichletBC
preset = false
variable = disp_x
boundary = 'left'
value = .1
[]
[right_disp_x]
type = DirichletBC
preset = false
variable = disp_x
boundary = 'right'
value = 0
[]
[bottom_disp_y]
type = DirichletBC
preset = false
variable = disp_y
boundary = 'bottom'
value = 0
[]
[]
[Preconditioning]
[fmp]
type = SMP
full = true
solve_type = 'NEWTON'
[]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-11
nl_abs_tol = 1.0e-10
[]
[VectorPostprocessors]
[NodalTemperature]
type = NodalValueSampler
sort_by = id
boundary = '100 101'
variable = 'temp'
[]
[]
[Outputs]
exodus = false
csv = true
[]
(test/tests/multiapps/steffensen/steady_main.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
parallel_type = replicated
uniform_refine = 1
[]
[Variables]
[u]
[]
[]
[AuxVariables]
[v]
[]
[]
[Kernels]
[diff]
type = CoefDiffusion
variable = u
coef = 0.1
[]
[force_u]
type = CoupledForce
variable = u
v = v
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Postprocessors]
[unorm]
type = ElementL2Norm
variable = u
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
nl_abs_tol = 1e-14
fixed_point_algorithm = 'steffensen'
fixed_point_max_its = 30
transformed_variables = 'u'
accept_on_max_fixed_point_iteration = true
[]
[Outputs]
csv = true
exodus = false
[]
[MultiApps]
[sub]
type = FullSolveMultiApp
app_type = MooseTestApp
positions = '0 0 0'
input_files = 'steady_sub.i'
clone_master_mesh = true
transformed_variables = 'v'
[]
[]
[Transfers]
[v_from_sub]
type = MultiAppNearestNodeTransfer
from_multi_app = sub
source_variable = v
variable = v
[]
[u_to_sub]
type = MultiAppNearestNodeTransfer
to_multi_app = sub
source_variable = u
variable = u
[]
[]
(test/tests/misc/check_error/bad_number.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1.2eE
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/mortar/gap-conductance-2d-non-conforming/gap-conductance.i)
[Mesh]
[file]
type = FileMeshGenerator
file = nodal_normals_test_offset_nonmatching_gap.e
[]
[./primary]
input = file
type = LowerDBlockFromSidesetGenerator
sidesets = '2'
new_block_id = '20'
[../]
[./secondary]
input = primary
type = LowerDBlockFromSidesetGenerator
sidesets = '1'
new_block_id = '10'
[../]
[]
[Problem]
kernel_coverage_check = false
[]
[Variables]
[./T]
block = '1 2'
[../]
[./lambda]
block = '10'
[../]
[]
[BCs]
[./neumann]
type = FunctionGradientNeumannBC
exact_solution = exact_soln
variable = T
boundary = '3 4 5 6 7 8'
[../]
[]
[Kernels]
[./conduction]
type = Diffusion
variable = T
block = '1 2'
[../]
[./sink]
type = Reaction
variable = T
block = '1 2'
[../]
[./forcing_function]
type = BodyForce
variable = T
function = forcing_function
block = '1 2'
[../]
[]
[Functions]
[./forcing_function]
type = ParsedFunction
value = '-4 + x^2 + y^2'
[../]
[./exact_soln]
type = ParsedFunction
value = 'x^2 + y^2'
[../]
[]
[Debug]
show_var_residual_norms = 1
[]
[Constraints]
[./mortar]
type = GapHeatConductanceTest
primary_boundary = 2
secondary_boundary = 1
primary_subdomain = 20
secondary_subdomain = 10
variable = lambda
secondary_variable = T
[../]
[]
[Materials]
[constant]
type = ADGenericConstantMaterial
prop_names = 'gap_conductance'
prop_values = '.03'
block = '1 2'
[]
[./ssm]
type = SpatialStatefulMaterial
block = '1 2'
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
solve_type = NEWTON
type = Steady
petsc_options_iname = '-pc_type -snes_linesearch_type'
petsc_options_value = 'lu basic'
[]
[Outputs]
exodus = true
[dofmap]
type = DOFMap
execute_on = 'initial'
[]
[]
(test/tests/materials/material/material_test_dg.i)
[Mesh]
file = sq-2blk.e
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = MONOMIAL
[./InitialCondition]
type = ConstantIC
value = 1
[../]
[../]
[]
[Functions]
active = 'forcing_fn exact_fn'
[./forcing_fn]
type = ParsedFunction
value = (x*x*x)-6.0*x
[../]
[./exact_fn]
type = ParsedGradFunction
value = (x*x*x)
grad_x = 3*x*x
grad_y = 0
[../]
[]
[Kernels]
active = 'diff abs forcing'
[./diff]
type = MatDiffusionTest
variable = u
prop_name = matp
[../]
[./abs]
type = Reaction
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[DGKernels]
active = 'dgdiff'
[./dgdiff]
type = DGDiffusion
variable = u
sigma = 6
epsilon = -1.0
diff = matp
[../]
[]
[BCs]
active = 'all'
[./all]
type = DGMDDBC
variable = u
boundary = '1 2 3 4'
function = exact_fn
prop_name = matp
sigma = 6
epsilon = -1.0
[../]
[]
[Materials]
active = 'mat_1 mat_2'
[./mat_1]
type = MTMaterial
block = 1
value = 1
[../]
[./mat_2]
type = MTMaterial
block = 2
value = 2
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out_dg
exodus = true
[]
(test/tests/mortar/mortar-q-points/test.i)
[Mesh]
[file]
type = FileMeshGenerator
file = nodal_normals_test_offset_nonmatching_gap.e
[]
[./primary]
input = file
type = LowerDBlockFromSidesetGenerator
sidesets = '2'
new_block_id = '20'
[../]
[./secondary]
input = primary
type = LowerDBlockFromSidesetGenerator
sidesets = '1'
new_block_id = '10'
[../]
uniform_refine = 2
[]
[Problem]
kernel_coverage_check = false
[]
[Variables]
[./T]
block = '1 2'
[../]
[]
[Kernels]
[./conduction]
type = Diffusion
variable = T
block = '1 2'
[../]
[./reaction]
type = Reaction
variable = T
block = '1 2'
[../]
[]
[Constraints]
[./mortar]
type = SpatiallyVaryingSource
primary_boundary = 2
secondary_boundary = 1
primary_subdomain = 20
secondary_subdomain = 10
secondary_variable = T
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
solve_type = NEWTON
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/2d-rc.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 2
ymin = -1
ymax = 1
nx = 2
ny = 2
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[u_forcing]
type = INSFVBodyForce
variable = u
functor = forcing_u
momentum_component = 'x'
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[v_forcing]
type = INSFVBodyForce
variable = v
functor = forcing_v
momentum_component = 'y'
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = 'exact_u'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = 'exact_v'
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = u
function = 'exact_u'
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = v
function = 'exact_v'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 'exact_p'
[]
[]
[Functions]
[exact_u]
type = ParsedFunction
value = 'sin((1/2)*y*pi)*cos((1/2)*x*pi)'
[]
[exact_rhou]
type = ParsedFunction
value = 'rho*sin((1/2)*y*pi)*cos((1/2)*x*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_u]
type = ADParsedFunction
value = '(1/2)*pi^2*mu*sin((1/2)*y*pi)*cos((1/2)*x*pi) - 1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi) + (1/2)*pi*rho*sin((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)^2 - pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi) - 1/4*pi*sin((1/4)*x*pi)*sin((3/2)*y*pi)'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_v]
type = ParsedFunction
value = 'sin((1/4)*x*pi)*cos((1/2)*y*pi)'
[]
[exact_rhov]
type = ParsedFunction
value = 'rho*sin((1/4)*x*pi)*cos((1/2)*y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_v]
type = ADParsedFunction
value = '(5/16)*pi^2*mu*sin((1/4)*x*pi)*cos((1/2)*y*pi) - pi*rho*sin((1/4)*x*pi)^2*sin((1/2)*y*pi)*cos((1/2)*y*pi) - 1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*y*pi) + (1/4)*pi*rho*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi) + (3/2)*pi*cos((1/4)*x*pi)*cos((3/2)*y*pi)'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_p]
type = ParsedFunction
value = 'sin((3/2)*y*pi)*cos((1/4)*x*pi)'
[]
[forcing_p]
type = ParsedFunction
value = '-1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi) - 1/2*pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[./L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2v]
type = ElementL2Error
variable = v
function = exact_v
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2p]
type = ElementL2Error
variable = pressure
function = exact_p
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[]
(test/tests/outputs/exodus/exodus_input.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
[./out]
type = Exodus
execute_input_on = final
execute_on = 'initial timestep_end'
[../]
[]
(test/tests/meshgenerators/break_mesh_by_block_generator/hanging_nodes_parallel.i)
[Mesh]
[./msh]
type = GeneratedMeshGenerator
nx = 2
ny = 3
nz = 4
xmin = -2.5
xmax = 2.5
ymin = -2
ymax = 2
zmin = -1.5
zmax = 1.5
dim = 3
[../]
[Partitioner]
type = GridPartitioner
nx = 1
ny = 3
nz = 4
[]
[./subdomain_1]
type = SubdomainBoundingBoxGenerator
input = msh
bottom_left = '-2.5 -2 -1'
top_right = '2.5 0 0.5'
block_id = 1
[]
[./subdomain_2]
type = SubdomainBoundingBoxGenerator
input = subdomain_1
bottom_left = '-2.5 0 -1'
top_right = '2.5 2 0.5'
block_id = 2
[]
[./subdomain_3]
type = SubdomainBoundingBoxGenerator
input = subdomain_2
bottom_left = '-2.5 -2 0.5'
top_right = '1.25 2 1.5'
block_id = 3
[]
[./subdomain_4]
type = SubdomainBoundingBoxGenerator
input = subdomain_3
bottom_left = '1.25 -2 0.5'
top_right = '5 2 1.5'
block_id = 4
[]
[./subdomain_5]
type = SubdomainBoundingBoxGenerator
input = subdomain_4
bottom_left = '-2.5 -2 -1.5'
top_right = '1.25 2 -1'
block_id = 3
[]
[./subdomain_6]
type = SubdomainBoundingBoxGenerator
input = subdomain_5
bottom_left = '1.25 -2 -1.5'
top_right = '2.5 2 -1'
block_id = 4
[]
[./split]
type = BreakMeshByBlockGenerator
input = subdomain_6
[]
[]
[Debug]
pid_aux = true
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/kernels/hfem/array_dirichlet_transform.i)
[Mesh]
[square]
type = GeneratedMeshGenerator
nx = 3
ny = 3
dim = 2
[]
build_all_side_lowerd_mesh = true
[]
[Variables]
[u]
order = THIRD
family = MONOMIAL
block = 0
components = 2
[]
[lambda]
order = CONSTANT
family = MONOMIAL
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
components = 2
[]
[lambdab]
order = CONSTANT
family = MONOMIAL
block = BOUNDARY_SIDE_LOWERD_SUBDOMAIN
components = 2
[]
[]
[AuxVariables]
[v]
order = CONSTANT
family = MONOMIAL
block = 0
initial_condition = '1'
[]
[]
[Kernels]
[diff]
type = ArrayDiffusion
variable = u
block = 0
diffusion_coefficient = dc
[]
[source]
type = ArrayCoupledForce
variable = u
v = v
coef = '1 2'
block = 0
[]
[]
[DGKernels]
[surface]
type = ArrayHFEMDiffusionTest
variable = u
lowerd_variable = lambda
[]
[]
[BCs]
[all]
type = ArrayHFEMDirichletBC
boundary = 'left right top bottom'
variable = u
lowerd_variable = lambdab
[]
[]
[Materials]
[dc]
type = GenericConstantArray
prop_name = dc
prop_value = '1 1'
[]
[]
[Postprocessors]
[intu]
type = ElementIntegralArrayVariablePostprocessor
variable = u
block = 0
[]
[lambdanorm]
type = ElementArrayL2Norm
variable = lambda
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu basic mumps'
[]
[Outputs]
[out]
# we hide lambda because it may flip sign due to element
# renumbering with distributed mesh
type = Exodus
hide = lambda
[]
csv = true
[]
(modules/ray_tracing/test/tests/raybcs/reflect_ray_bc/reflect_ray_bc.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 5
ny = 5
xmax = 5
ymax = 5
[]
[]
[RayBCs]
[kill]
type = KillRayBC
boundary = 'top'
[]
[reflect]
type = ReflectRayBC
boundary = 'top right left bottom'
[]
[]
[UserObjects/lots]
type = LotsOfRaysRayStudy
ray_kernel_coverage_check = false
vertex_to_vertex = true
centroid_to_vertex = true
centroid_to_centroid = false
execute_on = initial
ray_distance = 10
[]
[Postprocessors/total_distance]
type = RayTracingStudyResult
study = lots
result = total_distance
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Outputs]
exodus = false
csv = true
[]
(test/tests/controls/time_periods/aux_scalar_kernels/enable_disable.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Dampers]
[./const_damp]
type = ConstantDamper
damping = 0.9
[../]
[]
[Outputs]
exodus = true
[]
(test/tests/interfacekernels/2d_interface/coupled_value_coupled_flux_with_jump_material.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 2
xmax = 2
ny = 2
ymax = 2
[]
[./subdomain1]
type = SubdomainBoundingBoxGenerator
bottom_left = '0 0 0'
top_right = '1 1 0'
block_id = 1
input = gen
[../]
[./interface]
type = SideSetsBetweenSubdomainsGenerator
input = subdomain1
primary_block = '0'
paired_block = '1'
new_boundary = 'primary0_interface'
[../]
[./break_boundary]
input = interface
type = BreakBoundaryOnSubdomainGenerator
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
block = 0
[../]
[./v]
order = FIRST
family = LAGRANGE
block = 1
[../]
[]
[Kernels]
[./diff_u]
type = CoeffParamDiffusion
variable = u
D = 4
block = 0
[../]
[./diff_v]
type = CoeffParamDiffusion
variable = v
D = 2
block = 1
[../]
[./source_u]
type = BodyForce
variable = u
value = 1
[../]
[]
[InterfaceKernels]
[./interface]
type = PenaltyInterfaceDiffusion
variable = u
neighbor_var = v
boundary = primary0_interface
penalty = 1e6
jump_prop_name = jump
[../]
[]
[Materials]
[./jump]
type = JumpInterfaceMaterial
var = u
neighbor_var = v
boundary = primary0_interface
[../]
[]
[BCs]
[./u]
type = VacuumBC
variable = u
boundary = 'left_to_0 bottom_to_0 right top'
[../]
[./v]
type = VacuumBC
variable = v
boundary = 'left_to_1 bottom_to_1'
[../]
[]
[Postprocessors]
[./u_int]
type = ElementIntegralVariablePostprocessor
variable = u
block = 0
[../]
[./v_int]
type = ElementIntegralVariablePostprocessor
variable = v
block = 1
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
print_linear_residuals = true
[]
(test/tests/preconditioners/pbp/lots_of_variables.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Preconditioning/pbp]
type = PBP
solve_order = 'vars0 vars1 vars2 vars3 vars4 vars5 vars6 vars7 vars8 vars9'
preconditioner = 'AMG AMG AMG AMG AMG AMG AMG AMG AMG AMG'
[]
[Executioner]
type = Steady
solve_type = JFNK
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
[Testing/LotsOfDiffusion/vars]
number = 10
[]
(modules/richards/test/tests/gravity_head_2/gh03.i)
# unsaturated = true
# gravity = false
# supg = true
# transient = false
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
xmin = 0
xmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = 'pwater pgas'
[../]
[./DensityWater]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0E2
[../]
[./DensityGas]
type = RichardsDensityConstBulk
dens0 = 0.5
bulk_mod = 0.5E2
[../]
[./SeffWater]
type = RichardsSeff2waterVG
m = 0.8
al = 1
[../]
[./SeffGas]
type = RichardsSeff2gasVG
m = 0.8
al = 1
[../]
[./RelPermWater]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./RelPermGas]
type = RichardsRelPermPower
simm = 0.0
n = 3
[../]
[./SatWater]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.15
[../]
[./SatGas]
type = RichardsSat
s_res = 0.05
sum_s_res = 0.15
[../]
[./SUPGwater]
type = RichardsSUPGstandard
p_SUPG = 1E-3
[../]
[./SUPGgas]
type = RichardsSUPGstandard
p_SUPG = 1E-3
[../]
[]
[Variables]
[./pwater]
order = FIRST
family = LAGRANGE
[../]
[./pgas]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./water_ic]
type = RandomIC
min = 0.4
max = 0.6
variable = pwater
[../]
[./gas_ic]
type = RandomIC
min = 1.4
max = 1.6
variable = pgas
[../]
[]
[Kernels]
active = 'richardsfwater richardsfgas'
[./richardstwater]
type = RichardsMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFlux
variable = pwater
[../]
[./richardstgas]
type = RichardsMassChange
variable = pgas
[../]
[./richardsfgas]
type = RichardsFlux
variable = pgas
[../]
[]
[AuxVariables]
[./seffgas]
[../]
[./seffwater]
[../]
[]
[AuxKernels]
[./seffgas_kernel]
type = RichardsSeffAux
pressure_vars = 'pwater pgas'
seff_UO = SeffGas
variable = seffgas
[../]
[./seffwater_kernel]
type = RichardsSeffAux
pressure_vars = 'pwater pgas'
seff_UO = SeffWater
variable = seffwater
[../]
[]
[Postprocessors]
[./mwater_init]
type = RichardsMass
variable = pwater
execute_on = timestep_begin
outputs = none
[../]
[./mgas_init]
type = RichardsMass
variable = pgas
execute_on = timestep_begin
outputs = none
[../]
[./mwater_fin]
type = RichardsMass
variable = pwater
execute_on = timestep_end
outputs = none
[../]
[./mgas_fin]
type = RichardsMass
variable = pgas
execute_on = timestep_end
outputs = none
[../]
[./mass_error_water]
type = FunctionValuePostprocessor
function = fcn_mass_error_w
outputs = none # no reason why mass should be conserved
[../]
[./mass_error_gas]
type = FunctionValuePostprocessor
function = fcn_mass_error_g
outputs = none # no reason why mass should be conserved
[../]
[./pw_left]
type = PointValue
point = '0 0 0'
variable = pwater
outputs = none
[../]
[./pw_right]
type = PointValue
point = '1 0 0'
variable = pwater
outputs = none
[../]
[./error_water]
type = FunctionValuePostprocessor
function = fcn_error_water
[../]
[./pg_left]
type = PointValue
point = '0 0 0'
variable = pgas
outputs = none
[../]
[./pg_right]
type = PointValue
point = '1 0 0'
variable = pgas
outputs = none
[../]
[./error_gas]
type = FunctionValuePostprocessor
function = fcn_error_gas
[../]
[]
[Functions]
[./fcn_mass_error_w]
type = ParsedFunction
value = 'abs(0.5*(mi-mf)/(mi+mf))'
vars = 'mi mf'
vals = 'mwater_init mwater_fin'
[../]
[./fcn_mass_error_g]
type = ParsedFunction
value = 'abs(0.5*(mi-mf)/(mi+mf))'
vars = 'mi mf'
vals = 'mgas_init mgas_fin'
[../]
[./fcn_error_water]
type = ParsedFunction
value = 'abs((p0-p1)/p1)'
vars = 'b gdens0 p0 xval p1'
vals = '1E2 -1 pw_left 1 pw_right'
[../]
[./fcn_error_gas]
type = ParsedFunction
value = 'abs((p0-p1)/p1)'
vars = 'b gdens0 p0 xval p1'
vals = '0.5E2 -0.5 pg_left 1 pg_right'
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
density_UO = 'DensityWater DensityGas'
relperm_UO = 'RelPermWater RelPermGas'
SUPG_UO = 'SUPGwater SUPGgas'
sat_UO = 'SatWater SatGas'
seff_UO = 'SeffWater SeffGas'
viscosity = '1E-3 0.5E-3'
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-pc_factor_shift_type'
petsc_options_value = 'nonzero'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = gh03
csv = true
[]
(modules/chemical_reactions/test/tests/equilibrium_const/linear.i)
# Test of EquilibriumConstantAux with three log(K) values.
# The resulting equilibrium constant should be a linear best fit.
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
[]
[AuxVariables]
[./logk]
[../]
[]
[AuxKernels]
[./logk]
type = EquilibriumConstantAux
temperature = temperature
temperature_points = '200 300 400'
logk_points = '1.8 1.5 1.2'
variable = logk
[../]
[]
[Variables]
[./temperature]
[../]
[]
[Kernels]
[./temperature]
type = Diffusion
variable = temperature
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = temperature
value = 150
boundary = left
[../]
[./right]
type = DirichletBC
variable = temperature
value = 400
boundary = right
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_mortar/large_gap_heat_transfer_test_cylinder_mortar_error.i)
rpv_core_gap_size = 0.15
core_outer_radius = 2
rpv_inner_radius = ${fparse 2 + rpv_core_gap_size}
rpv_outer_radius = ${fparse 2.5 + rpv_core_gap_size}
rpv_outer_htc = 10 # W/m^2/K
rpv_outer_Tinf = 300 # K
core_blocks = '1'
rpv_blocks = '3'
[Mesh]
[core_gap_rpv]
type = ConcentricCircleMeshGenerator
num_sectors = 10
radii = '${core_outer_radius} ${rpv_inner_radius} ${rpv_outer_radius}'
rings = '2 1 2'
has_outer_square = false
preserve_volumes = true
portion = full
[]
[rename_core_bdy]
type = SideSetsBetweenSubdomainsGenerator
input = core_gap_rpv
primary_block = 1
paired_block = 2
new_boundary = 'core_outer'
[]
[rename_inner_rpv_bdy]
type = SideSetsBetweenSubdomainsGenerator
input = rename_core_bdy
primary_block = 3
paired_block = 2
new_boundary = 'rpv_inner'
[]
[2d_mesh]
type = BlockDeletionGenerator
input = rename_inner_rpv_bdy
block = 2
[]
[secondary]
type = LowerDBlockFromSidesetGenerator
sidesets = 'rpv_inner'
new_block_id = 10001
new_block_name = 'secondary_lower'
input = 2d_mesh
[]
[primary]
type = LowerDBlockFromSidesetGenerator
sidesets = 'core_outer'
new_block_id = 10000
new_block_name = 'primary_lower'
input = secondary
[]
allow_renumbering = false
[]
[Variables]
[Tsolid]
initial_condition = 500
[]
[lm]
order = FIRST
family = LAGRANGE
block = 'secondary_lower'
[]
[]
[Kernels]
[heat_source]
type = CoupledForce
variable = Tsolid
block = '${core_blocks}'
v = power_density
[]
[heat_conduction]
type = HeatConduction
variable = Tsolid
[]
[]
[BCs]
[RPV_out_BC] # k \nabla T = h (T- T_inf) at RPV outer boundary
type = ConvectiveFluxFunction # (Robin BC)
variable = Tsolid
boundary = 'outer' # outer RPV
coefficient = ${rpv_outer_htc}
T_infinity = ${rpv_outer_Tinf}
[]
[]
[UserObjects]
[radiation]
type = GapFluxModelRadiation
temperature = Tsolid
boundary = 'rpv_inner'
primary_emissivity = 0.8
secondary_emissivity = 0.8
[]
[conduction]
type = GapFluxModelConduction
temperature = Tsolid
boundary = 'rpv_inner'
gap_conductivity = 0.1
[]
[]
[Constraints]
[ced]
type = ModularGapConductanceConstraint
variable = lm
secondary_variable = Tsolid
primary_boundary = 'core_outer'
primary_subdomain = 10000
secondary_boundary = 'rpv_inner'
secondary_subdomain = 10001
gap_flux_models = 'radiation conduction'
gap_geometry_type = 'CYLINDER'
cylinder_axis_point_2 = '0 0 5'
[]
[]
[AuxVariables]
[power_density]
block = '${core_blocks}'
initial_condition = 50e3
[]
[]
[Materials]
[simple_mat]
type = HeatConductionMaterial
thermal_conductivity = 34.6 # W/m/K
[]
[]
[Postprocessors]
[Tcore_avg]
type = ElementAverageValue
variable = Tsolid
block = '${core_blocks}'
[]
[Tcore_max]
type = ElementExtremeValue
value_type = max
variable = Tsolid
block = '${core_blocks}'
[]
[Tcore_min]
type = ElementExtremeValue
value_type = min
variable = Tsolid
block = '${core_blocks}'
[]
[Trpv_avg]
type = ElementAverageValue
variable = Tsolid
block = '${rpv_blocks}'
[]
[Trpv_max]
type = ElementExtremeValue
value_type = max
variable = Tsolid
block = '${rpv_blocks}'
[]
[Trpv_min]
type = ElementExtremeValue
value_type = min
variable = Tsolid
block = '${rpv_blocks}'
[]
[ptot]
type = ElementIntegralVariablePostprocessor
variable = power_density
block = '${core_blocks}'
[]
[rpv_convective_out]
type = ConvectiveHeatTransferSideIntegral
T_solid = Tsolid
boundary = 'outer' # outer RVP
T_fluid = ${rpv_outer_Tinf}
htc = ${rpv_outer_htc}
[]
[heat_balance] # should be equal to 0 upon convergence
type = ParsedPostprocessor
function = '(rpv_convective_out - ptot) / ptot'
pp_names = 'rpv_convective_out ptot'
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[VectorPostprocessors]
[NodalTemperature]
type = NodalValueSampler
sort_by = id
boundary = 'rpv_inner core_outer'
variable = 'Tsolid'
[]
[]
[Executioner]
type = Steady
petsc_options = '-snes_converged_reason -pc_svd_monitor'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package -mat_mffd_err -pc_factor_shift_type '
'-pc_factor_shift_amount'
petsc_options_value = ' lu superlu_dist 1e-5 NONZERO '
'1e-15'
snesmf_reuse_base = false
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
l_max_its = 100
line_search = none
[]
[Outputs]
exodus = false
csv = true
[]
(test/tests/misc/check_error/wrong_moose_object_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
# Test for kernel in BC section
[./left]
type = Diffusion
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-rc-no-slip-extrapolated-outlet-pressure.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 10
ymin = -1
ymax = 1
nx = 100
ny = 20
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[lambda]
family = SCALAR
order = FIRST
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[mean_zero_pressure]
type = FVScalarLagrangeMultiplier
variable = pressure
lambda = lambda
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = '0'
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = u
function = 0
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = v
function = 0
[]
[outlet_u]
type = INSFVMomentumAdvectionOutflowBC
variable = u
u = u
v = v
boundary = 'right'
momentum_component = 'x'
rho = ${rho}
[]
[outlet_v]
type = INSFVMomentumAdvectionOutflowBC
variable = v
u = u
v = v
boundary = 'right'
momentum_component = 'y'
rho = ${rho}
[]
[outlet_p]
type = INSFVMassAdvectionOutflowBC
boundary = 'right'
variable = pressure
u = u
v = v
rho = ${rho}
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 200 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[dof]
type = DOFMap
execute_on = 'initial'
[]
[]
(modules/ray_tracing/test/tests/userobjects/repeatable_ray_study_base/errors.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
nx = 1
[]
[]
[UserObjects/study]
type = RepeatableRayStudyBaseTest
names = 'dummy'
start_points = '0 0 0'
directions = '1 0 0'
ray_kernel_coverage_check = false
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
(test/tests/nodalkernels/multiple-subdomains/test.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 2
[]
[sub]
type = SubdomainBoundingBoxGenerator
bottom_left = '0.5 0 0'
top_right = '1 1 0'
input = 'gen'
block_id = '1'
[]
[]
[Variables]
[u]
block = '0 1'
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[rxn]
type = Reaction
variable = u
[]
[]
[NodalKernels]
[source]
type = UserForcingFunctionNodalKernel
variable = u
block = '0 1'
function = '1'
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/transfers/multiapp_conservative_transfer/secondary_negative_adjuster.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[AuxVariables]
[var]
family = MONOMIAL
order = CONSTANT
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Postprocessors]
[to_postprocessor]
type = ElementIntegralVariablePostprocessor
variable = var
execute_on = 'transfer'
[]
[]
[Problem]
type = FEProblem
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
nl_abs_tol = 1e-12
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/ray_tracing/test/tests/postprocessors/ray_tracing_study_result/ray_tracing_study_result.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
nx = 10
[]
[]
[RayBCs/kill]
type = KillRayBC
boundary = 'left right'
[]
[UserObjects/study]
type = LotsOfRaysRayStudy
ray_kernel_coverage_check = false
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[total_rays_started]
type = RayTracingStudyResult
study = study
result = total_rays_started
[]
[total_processor_crossings]
type = RayTracingStudyResult
study = study
result = total_processor_crossings
[]
[max_processor_crossings]
type = RayTracingStudyResult
study = study
result = max_processor_crossings
[]
[total_distance]
type = RayTracingStudyResult
study = study
result = total_distance
[]
[]
[Outputs]
csv = true
[]
(modules/functional_expansion_tools/test/tests/standard_use/neglect_invalid_enum.i)
[Mesh]
type = GeneratedMesh
dim = 1
xmin = -1
xmax = 1
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diffusion]
type = Diffusion
variable = u
[../]
[]
[Functions]
[./series]
type = FunctionSeries
series_type = Cartesian
x = Legendre
disc = Zernike
orders = '0'
physical_bounds = '-1 1'
[../]
[]
[Executioner]
type = Steady
[]
(test/tests/postprocessors/side_integral/side_integral_fv_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmin = 0
xmax = 4
ymin = 0
ymax = 1
[]
[Variables]
active = 'u'
[./u]
family = MONOMIAL
order = CONSTANT
fv = true
[../]
[]
[FVKernels]
active = 'diff'
[./diff]
type = FVDiffusion
variable = u
coeff = '1'
[../]
[]
[FVBCs]
active = 'left right'
[./left]
type = FVDirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = FVDirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Postprocessors]
[./integral]
type = SideIntegralVariablePostprocessor
boundary = 0
variable = u
[../]
[]
[Outputs]
file_base = fv_out
exodus = true
[]
(test/tests/mortar/periodic-value/periodic.i)
[Mesh]
[file]
type = FileMeshGenerator
file = square.msh
[]
[secondary]
input = file
type = LowerDBlockFromSidesetGenerator
new_block_id = 11
new_block_name = "secondary"
sidesets = '101'
[]
[primary]
input = secondary
type = LowerDBlockFromSidesetGenerator
new_block_id = 12
new_block_name = "primary"
sidesets = '103'
[]
[]
[Variables]
[u]
order = SECOND
block = 'domain'
[]
[lm]
block = 'secondary'
[]
[]
[Kernels]
[diffusion]
type = Diffusion
variable = u
block = 'domain'
[]
[force]
type = BodyForce
variable = u
block = 'domain'
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
value = 1
boundary = 'left'
[]
[]
[Constraints]
[ev]
type = EqualValueConstraint
variable = lm
secondary_variable = u
primary_boundary = 103
secondary_boundary = 101
primary_subdomain = 12
secondary_subdomain = 11
periodic = true
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(test/tests/auxkernels/current_boundary_id/current_boundary_id.i)
#
# This is used to create the mesh but it does not work with --distributed-mesh flag
# and the parallel test bombs.
#
#[Mesh]
# type = MeshGeneratorMesh
#
# [./cartesian]
# type = CartesianMeshGenerator
# dim = 2
# dx = '1 1'
# ix = '10 10'
# dy = '1'
# iy = '10'
# subdomain_id = '1 2'
# [../]
#
# [./interior_bc]
# type = SideSetsBetweenSubdomainsGenerator
# primary_block = 1
# paired_block = 2
# new_boundary = 12
# input = cartesian
# [../]
#[]
[Mesh]
type = FileMesh
file = current_boundary_id_in.e
[]
[Problem]
kernel_coverage_check = false
[]
[Variables]
[./u]
[../]
[]
[Executioner]
type = Steady
[]
[AuxVariables]
[./id1]
family = MONOMIAL
order = CONSTANT
[]
[./id2]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[./id1]
type = BIDAux
variable = id1
boundary = 'top'
[../]
[./id2]
type = BIDAux
variable = id2
boundary = '12'
[../]
[]
[Outputs]
exodus = true
[]
(test/tests/postprocessors/point_value/point_value.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 2
[]
[./subdomain]
input = gen
type = ElementSubdomainIDGenerator
element_ids = '0 1 2 3'
subdomain_ids = '1 2 3 4'
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Postprocessors]
[./value]
type = PointValue
variable = u
point = '0.371 .41 0'
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
csv = true
[]
(modules/thermal_hydraulics/test/tests/materials/ad_convection_heat_flux_hs/ad_convection_heat_flux_hs.i)
# Gold value should be the following:
# q_wall = kappa * htc_wall * (T_wall - T)
# = 0.5 * 100 * (500 - 400)
# = 5000
[GlobalParams]
execute_on = 'initial'
[]
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
[]
[Materials]
[props]
type = ADGenericConstantMaterial
prop_names = 'T T_wall htc_wall kappa'
prop_values = '400 500 100 0.5'
[]
[q_wall_mat]
type = ADConvectionHeatFluxHSMaterial
q_wall = q_wall_prop
T = T
T_wall = T_wall
htc_wall = htc_wall
kappa = kappa
[]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Postprocessors]
[q_wall_pp]
type = ADElementAverageMaterialProperty
mat_prop = q_wall_prop
[]
[]
[Outputs]
csv = true
[]
(modules/geochemistry/test/tests/time_dependent_reactions/except4.i)
#Exception: cannot remove fixed activity of a species that does not have an activity or fugacity constraint
[TimeDependentReactionSolver]
model_definition = definition
geochemistry_reactor_name = reactor
charge_balance_species = "Cl-"
constraint_species = "H2O H+ Na+ K+ Ca++ Mg++ Al+++ SiO2(aq) Cl- SO4-- HCO3-"
constraint_value = " 1.0 1E-5 1E-5 1E-5 1E-5 1E-5 1E-5 1E-5 1E-5 1E-5 1E-5"
constraint_meaning = "kg_solvent_water activity bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition"
constraint_unit = "kg dimensionless moles moles moles moles moles moles moles moles moles"
remove_fixed_activity_name = "Na+"
remove_fixed_activity_time = "0"
[]
[Executioner]
type = Steady
[]
[UserObjects]
[definition]
type = GeochemicalModelDefinition
database_file = "../../../database/moose_geochemdb.json"
basis_species = "H2O H+ Na+ K+ Ca++ Mg++ Al+++ SiO2(aq) Cl- SO4-- HCO3-"
[]
[]
(modules/phase_field/test/tests/initial_conditions/MultiBoundingBoxIC2D.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
[]
[Variables]
[./c1]
order = FIRST
family = LAGRANGE
[../]
[./c2]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./c1]
type = MultiBoundingBoxIC
corners = '0.1 0.4 0 0.8 0.5 0 0.3 0.7 0'
opposite_corners = '0.2 0.6 0 0.6 0.9 0 0.4 0.5 0'
inside = '1.0'
outside = 0.1
variable = c1
[../]
[./c2]
type = MultiBoundingBoxIC
corners = '0.1 0.4 0 0.8 0.5 0 0.3 0.6 0'
opposite_corners = '0.2 0.6 0 0.4 0.9 0 0.5 0.8 0'
inside = '1.0 2.0 3.0'
outside = 0.1
variable = c2
[../]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
kernel_coverage_check = false
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/heat_conduction_patch/heat_conduction_patch_rz.i)
#
# This problem is taken from the Abaqus verification manual:
# "1.5.8 Patch test for heat transfer elements"
#
# The temperature on the exterior nodes is -2e5+200x+100y.
#
# This gives a constant flux at all Gauss points.
#
# In addition, the temperature at all nodes follows the same formula.
#
# Node x y Temperature
# 1 1e3 0 0
# 2 1.00024e3 0 48
# 3 1.00018e3 3e-2 39
# 4 1.00004e3 2e-2 10
# 5 1.00008e3 8e-2 24
# 6 1e3 1.2e-1 12
# 7 1.00016e3 8e-2 40
# 8 1.00024e3 1.2e-1 60
[Problem]
coord_type = RZ
[]
[Mesh]#Comment
file = heat_conduction_patch_rz.e
[] # Mesh
[Functions]
[./temps]
type = ParsedFunction
value='-2e5+200*x+100*y'
[../]
[] # Functions
[Variables]
[./temp]
order = FIRST
family = LAGRANGE
[../]
[] # Variables
[Kernels]
[./heat_r]
type = HeatConduction
variable = temp
[../]
[] # Kernels
[BCs]
[./temps]
type = FunctionDirichletBC
variable = temp
boundary = 10
function = temps
[../]
[] # BCs
[Materials]
[./heat]
type = HeatConductionMaterial
block = 1
specific_heat = 0.116
thermal_conductivity = 4.85e-4
[../]
[] # Materials
[Executioner]
type = Steady
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -ksp_gmres_restart'
petsc_options_value = 'lu 101'
line_search = 'none'
nl_abs_tol = 1e-11
nl_rel_tol = 1e-10
l_max_its = 20
[] # Executioner
[Outputs]
exodus = true
[] # Outputs
(modules/porous_flow/test/tests/gravity/grav01c.i)
# Checking that gravity head is established
# 1phase, vanGenuchten, constant fluid-bulk, constant viscosity, constant permeability, Corey relative perm
# unsaturated
# For better agreement with the analytical solution (ana_pp), just increase nx
[Mesh]
type = GeneratedMesh
dim = 1
nx = 100
xmin = -1
xmax = 0
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Variables]
[pp]
[InitialCondition]
type = RandomIC
min = -1
max = 1
[]
[]
[]
[Kernels]
[flux0]
type = PorousFlowAdvectiveFlux
fluid_component = 0
variable = pp
gravity = '-1 0 0'
[]
[]
[Functions]
[ana_pp]
type = ParsedFunction
vars = 'g B p0 rho0'
vals = '1 2 -1 1'
value = '-B*log(exp(-p0/B)+g*rho0*x/B)' # expected pp at base
[]
[]
[BCs]
[z]
type = DirichletBC
variable = pp
boundary = right
value = -1
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureVG
m = 0.5
alpha = 1
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 2
density0 = 1
viscosity = 1
thermal_expansion = 0
[]
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pp
capillary_pressure = pc
[]
[massfrac]
type = PorousFlowMassFraction
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1 0 0 0 2 0 0 0 3'
[]
[relperm]
type = PorousFlowRelativePermeabilityCorey
n = 1
phase = 0
[]
[]
[Postprocessors]
[pp_base]
type = PointValue
variable = pp
point = '-1 0 0'
[]
[pp_analytical]
type = FunctionValuePostprocessor
function = ana_pp
point = '-1 0 0'
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = grav01c
exodus = true
[csv]
type = CSV
[]
[]
(modules/tensor_mechanics/test/tests/lagrangian/total/stabilization/cook_small.i)
[GlobalParams]
displacements = 'disp_x disp_y'
large_kinematics = false
stabilize_strain = true
[]
[Mesh]
type = FileMesh
file = cook_mesh.exo
dim = 2
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[]
[Kernels]
[sdx]
type = TotalLagrangianStressDivergence
variable = disp_x
component = 0
[]
[sdy]
type = TotalLagrangianStressDivergence
variable = disp_y
component = 1
[]
[]
[AuxVariables]
[strain_xx]
order = CONSTANT
family = MONOMIAL
[]
[strain_yy]
order = CONSTANT
family = MONOMIAL
[]
[strain_zz]
order = CONSTANT
family = MONOMIAL
[]
[strain_xy]
order = CONSTANT
family = MONOMIAL
[]
[strain_xz]
order = CONSTANT
family = MONOMIAL
[]
[strain_yz]
order = CONSTANT
family = MONOMIAL
[]
[stress_xx]
order = CONSTANT
family = MONOMIAL
[]
[stress_yy]
order = CONSTANT
family = MONOMIAL
[]
[stress_zz]
order = CONSTANT
family = MONOMIAL
[]
[stress_xy]
order = CONSTANT
family = MONOMIAL
[]
[stress_yz]
order = CONSTANT
family = MONOMIAL
[]
[stress_xz]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[stress_xx]
type = RankTwoAux
rank_two_tensor = pk1_stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[]
[stress_yy]
type = RankTwoAux
rank_two_tensor = pk1_stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[]
[stress_zz]
type = RankTwoAux
rank_two_tensor = pk1_stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[]
[stress_xy]
type = RankTwoAux
rank_two_tensor = pk1_stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[]
[stress_xz]
type = RankTwoAux
rank_two_tensor = pk1_stress
variable = stress_xz
index_i = 0
index_j = 2
execute_on = timestep_end
[]
[stress_yz]
type = RankTwoAux
rank_two_tensor = pk1_stress
variable = stress_yz
index_i = 1
index_j = 2
execute_on = timestep_end
[]
[strain_xx]
type = RankTwoAux
rank_two_tensor = mechanical_strain
variable = strain_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[]
[strain_yy]
type = RankTwoAux
rank_two_tensor = mechanical_strain
variable = strain_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[]
[strain_zz]
type = RankTwoAux
rank_two_tensor = mechanical_strain
variable = strain_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[]
[strain_xy]
type = RankTwoAux
rank_two_tensor = mechanical_strain
variable = strain_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[]
[strain_xz]
type = RankTwoAux
rank_two_tensor = mechanical_strain
variable = strain_xz
index_i = 0
index_j = 2
execute_on = timestep_end
[]
[strain_yz]
type = RankTwoAux
rank_two_tensor = mechanical_strain
variable = strain_yz
index_i = 1
index_j = 2
execute_on = timestep_end
[]
[]
[BCs]
[fixed_x]
type = DirichletBC
preset = true
variable = disp_x
boundary = canti
value = 0.0
[]
[fixed_y]
type = DirichletBC
preset = true
variable = disp_y
boundary = canti
value = 0.0
[]
[pull]
type = NeumannBC
variable = disp_y
boundary = loading
value = 10.0
[]
[]
[Materials]
[elastic_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 250.0
poissons_ratio = 0.4999999
[]
[compute_stress]
type = ComputeLagrangianLinearElasticStress
[]
[compute_strain]
type = ComputeLagrangianStrain
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = 'newton'
line_search = 'none'
petsc_options_iname = -pc_type
petsc_options_value = lu
nl_abs_tol = 1e-10
nl_rel_tol = 1e-6
l_tol = 1e-10
[]
[Postprocessors]
[value]
type = PointValue
variable = disp_y
point = '48 60 0'
use_displaced_mesh = false
[]
[]
[Outputs]
exodus = false
csv = true
[]
(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/heated/2d-rc-heated-boussinesq.i)
mu=1
rho=1
k=1e-3
cp=1
v_inlet=1
T_inlet=200
advected_interp_method='average'
velocity_interp_method='rc'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 2
ymin = 0
ymax = 10
nx = 20
ny = 100
[]
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = PINSFVRhieChowInterpolator
u = superficial_vel_x
v = superficial_vel_y
pressure = pressure
porosity = porosity
[]
[]
[Variables]
[superficial_vel_x]
type = PINSFVSuperficialVelocityVariable
initial_condition = 1e-6
[]
[superficial_vel_y]
type = PINSFVSuperficialVelocityVariable
initial_condition = ${v_inlet}
[]
[pressure]
type = INSFVPressureVariable
[]
[T_fluid]
type = INSFVEnergyVariable
[]
[]
[AuxVariables]
[T_solid]
family = 'MONOMIAL'
order = 'CONSTANT'
fv = true
initial_condition = 100
[]
[porosity]
family = MONOMIAL
order = CONSTANT
fv = true
initial_condition = 0.4
[]
[]
[FVKernels]
[mass]
type = PINSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = PINSFVMomentumAdvection
variable = superficial_vel_x
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
porosity = porosity
momentum_component = 'x'
[]
[u_viscosity]
type = PINSFVMomentumDiffusion
variable = superficial_vel_x
mu = ${mu}
porosity = porosity
momentum_component = 'x'
[]
[u_pressure]
type = PINSFVMomentumPressure
variable = superficial_vel_x
momentum_component = 'x'
pressure = pressure
porosity = porosity
[]
[u_gravity]
type = PINSFVMomentumGravity
variable = superficial_vel_x
rho = ${rho}
gravity = '0 -9.81 0'
momentum_component = 'x'
porosity = porosity
[]
[u_boussinesq]
type = PINSFVMomentumBoussinesq
variable = superficial_vel_x
T_fluid = 'T_fluid'
rho = ${rho}
ref_temperature = 150
gravity = '0 -9.81 0'
momentum_component = 'x'
alpha_name = 'alpha_b'
porosity = porosity
[]
[v_advection]
type = PINSFVMomentumAdvection
variable = superficial_vel_y
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
porosity = porosity
momentum_component = 'y'
[]
[v_viscosity]
type = PINSFVMomentumDiffusion
variable = superficial_vel_y
mu = ${mu}
porosity = porosity
momentum_component = 'y'
[]
[v_pressure]
type = PINSFVMomentumPressure
variable = superficial_vel_y
momentum_component = 'y'
pressure = pressure
porosity = porosity
[]
[v_gravity]
type = PINSFVMomentumGravity
variable = superficial_vel_y
rho = ${rho}
gravity = '-0 -9.81 0'
momentum_component = 'y'
porosity = porosity
[]
[v_boussinesq]
type = PINSFVMomentumBoussinesq
variable = superficial_vel_y
T_fluid = 'T_fluid'
rho = ${rho}
ref_temperature = 150
gravity = '0 -9.81 0'
momentum_component = 'y'
alpha_name = 'alpha_b'
porosity = porosity
[]
[energy_advection]
type = PINSFVEnergyAdvection
variable = T_fluid
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
[]
[energy_diffusion]
type = PINSFVEnergyDiffusion
k = ${k}
variable = T_fluid
porosity = porosity
[]
[energy_convection]
type = PINSFVEnergyAmbientConvection
variable = T_fluid
is_solid = false
T_fluid = T_fluid
T_solid = T_solid
h_solid_fluid = 'h_cv'
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = superficial_vel_x
function = 0
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = superficial_vel_y
function = ${v_inlet}
[]
[inlet-T]
type = FVNeumannBC
variable = T_fluid
value = ${fparse v_inlet * rho * cp * T_inlet}
boundary = 'bottom'
[]
[no-slip-u]
type = INSFVNoSlipWallBC
boundary = 'right'
variable = superficial_vel_x
function = 0
[]
[no-slip-v]
type = INSFVNoSlipWallBC
boundary = 'right'
variable = superficial_vel_y
function = 0
[]
[symmetry-u]
type = PINSFVSymmetryVelocityBC
boundary = 'left'
variable = superficial_vel_x
u = superficial_vel_x
v = superficial_vel_y
mu = ${mu}
momentum_component = 'x'
[]
[symmetry-v]
type = PINSFVSymmetryVelocityBC
boundary = 'left'
variable = superficial_vel_y
u = superficial_vel_x
v = superficial_vel_y
mu = ${mu}
momentum_component = 'y'
[]
[symmetry-p]
type = INSFVSymmetryPressureBC
boundary = 'left'
variable = pressure
[]
[outlet-p]
type = INSFVOutletPressureBC
boundary = 'top'
variable = pressure
function = 0
[]
[]
[Materials]
[constants]
type = ADGenericFunctorMaterial
prop_names = 'h_cv alpha_b'
prop_values = '1e-3 8e-4'
[]
[functor_constants]
type = ADGenericFunctorMaterial
prop_names = 'cp'
prop_values = '${cp}'
[]
[ins_fv]
type = INSFVEnthalpyMaterial
rho = ${rho}
temperature = 'T_fluid'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
# Some basic Postprocessors to examine the solution
[Postprocessors]
[inlet-p]
type = SideAverageValue
variable = pressure
boundary = 'top'
[]
[outlet-v]
type = SideAverageValue
variable = superficial_vel_y
boundary = 'top'
[]
[outlet-temp]
type = SideAverageValue
variable = T_fluid
boundary = 'top'
[]
[]
[Outputs]
exodus = true
csv = false
[]
(examples/ex04_bcs/dirichlet_bc.i)
[Mesh]
file = square.e
uniform_refine = 4
[]
[Variables]
[./convected]
order = FIRST
family = LAGRANGE
[../]
[./diffused]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff_convected]
type = Diffusion
variable = convected
[../]
[./conv]
type = ExampleConvection
variable = convected
some_variable = diffused
[../]
[./diff_diffused]
type = Diffusion
variable = diffused
[../]
[]
[BCs]
active = 'left_convected right_convected_dirichlet left_diffused right_diffused'
[./left_convected]
type = DirichletBC
variable = convected
boundary = 'left'
value = 0
[../]
[./right_convected_dirichlet]
type = CoupledDirichletBC
variable = convected
boundary = 'right'
alpha = 2
some_var = diffused
[../]
# Note: This BC is not active in this input file
[./right_convected_neumann]
type = CoupledNeumannBC
variable = convected
boundary = 'right'
alpha = 2
some_var = diffused
[../]
[./left_diffused]
type = DirichletBC
variable = diffused
boundary = 'left'
value = 0
[../]
[./right_diffused]
type = DirichletBC
variable = diffused
boundary = 'right'
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(test/tests/fvkernels/mms/grad-reconstruction/mat-rz.i)
a=1.1
diff=1.1
[Mesh]
[gen_mesh]
type = GeneratedMeshGenerator
dim = 2
xmin = 2
xmax = 3
ymin = 0
ymax = 1
nx = 2
ny = 2
[]
[]
[Problem]
coord_type = 'RZ'
[]
[Variables]
[v]
family = MONOMIAL
order = CONSTANT
fv = true
initial_condition = 1
[]
[]
[FVKernels]
[advection]
type = FVElementalAdvection
variable = v
velocity = '${a} ${a} 0'
advected_quantity = 'mat_u'
grad_advected_quantity = 'mat_grad_u'
[]
[reaction]
type = FVReaction
variable = v
[]
[diff_v]
type = FVDiffusion
variable = v
coeff = ${diff}
[]
[body_v]
type = FVBodyForce
variable = v
function = 'forcing'
[]
[]
[FVBCs]
[diri]
type = FVFunctionDirichletBC
boundary = 'left right top bottom'
function = 'exact'
variable = v
[]
[]
[Materials]
[mat]
type = ADCoupledGradientMaterial
mat_prop = 'mat_u'
grad_mat_prop = 'mat_grad_u'
u = v
[]
[]
[Functions]
[exact]
type = ParsedFunction
value = 'sin(x)*cos(y)'
[]
[forcing]
type = ParsedFunction
value = '-a*sin(x)*sin(y) + diff*sin(x)*cos(y) + sin(x)*cos(y) + (x*a*cos(x)*cos(y) + a*sin(x)*cos(y))/x - (-x*diff*sin(x)*cos(y) + diff*cos(x)*cos(y))/x'
vars = 'a diff'
vals = '${a} ${diff}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_shift_type -sub_pc_type'
petsc_options_value = 'asm NONZERO lu'
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[error]
type = ElementL2Error
variable = v
function = exact
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(test/tests/materials/derivative_material_interface/ad_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
[]
[Materials]
[./provider]
type = ADDerivativeMaterialInterfaceTestProvider
block = 0
outputs = exodus
output_properties = 'dprop/db dprop/da d^2prop/dadb d^2prop/dadc d^3prop/dadbdc'
[../]
[./client]
type = ADDerivativeMaterialInterfaceTestClient
block = 0
[../]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Debug]
show_material_props = true
[]
[Outputs]
exodus = true
[]
(test/tests/multiapps/picard/steady_picard_sub.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./v]
[../]
[]
[AuxVariables]
[./u]
[../]
[]
[Kernels]
[./diff_v]
type = Diffusion
variable = v
[../]
[./force_v]
type = CoupledForce
variable = v
v = u
[../]
[]
[BCs]
[./left_v]
type = DirichletBC
variable = v
boundary = left
value = 1
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = right
value = 0
[../]
[]
[Postprocessors]
[./vnorm]
type = ElementL2Norm
variable = v
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
nl_abs_tol = 1e-14
[]
[Outputs]
exodus = true
[]
(test/tests/postprocessors/element_vec_l2_error_pps/element_vec_l2_error.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
[]
[Variables]
active = 'u v'
[./u]
order = FIRST
family = LAGRANGE
[../]
[./v]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
active = 'bc_u bc_v f_u f_v'
# A ParsedFunction allows us to supply analytic expressions
# directly in the input file
[./bc_u]
type = ParsedFunction
value = sin(alpha*pi*x)
vars = 'alpha'
vals = '2'
[../]
[./bc_v]
type = ParsedFunction
value = sin(alpha*pi*y)
vars = 'alpha'
vals = '2'
[../]
[./f_u]
type = ParsedFunction
value = alpha*alpha*pi*pi*sin(alpha*pi*x)
vars = 'alpha'
vals = '2'
[../]
[./f_v]
type = ParsedFunction
value = alpha*alpha*pi*pi*sin(alpha*pi*y)
vars = 'alpha'
vals = '2'
[../]
[]
[Kernels]
active = 'diff_u diff_v forcing_u forcing_v'
[./diff_u]
type = Diffusion
variable = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
# This Kernel can take a function name to use
[./forcing_u]
type = BodyForce
variable = u
function = f_u
[../]
[./forcing_v]
type = BodyForce
variable = v
function = f_v
[../]
[]
[BCs]
active = 'all_u all_v'
# The BC can take a function name to use
[./all_u]
type = FunctionDirichletBC
variable = u
boundary = 'bottom right top left'
function = bc_u
[../]
[./all_v]
type = FunctionDirichletBC
variable = v
boundary = 'bottom right top left'
function = bc_v
[../]
[]
[Executioner]
type = Steady
[./Adaptivity]
refine_fraction = 1.0
coarsen_fraction = 0.0
max_h_level = 10
steps = 3
[../]
[]
[Postprocessors]
[./dofs]
type = NumDOFs
execute_on = 'initial timestep_end'
[../]
[./integral]
type = ElementVectorL2Error
var_x = u
var_y = v
function_x = bc_u
function_y = bc_v
execute_on = 'initial timestep_end'
[../]
[]
[Outputs]
file_base = out
exodus = false
csv = true
[]
(test/tests/meshgenerators/combiner_generator/combiner_multi_input_translate.i)
[Mesh]
[gen1]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[gen2]
type = GeneratedMeshGenerator
dim = 2
nx = 12
ny = 12
[]
[gen3]
type = GeneratedMeshGenerator
dim = 2
nx = 14
ny = 14
[]
[cmbn]
type = CombinerGenerator
inputs = 'gen1 gen2 gen3'
positions = '1 0 0 2 2 2 3 0 0'
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/functional_expansion_tools/test/tests/errors/bc_value_penalty_bad_function.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Variables]
[./v]
[../]
[]
[BCs]
[./this_could_be_bad]
type = FXValuePenaltyBC
boundary = right
penalty = 1.0
function = const
variable = v
[../]
[]
[Functions]
[./const]
type = ConstantFunction
value = -1
[../]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
(test/tests/mesh_modifiers/add_side_sets_from_bounding_box/multiple_boundary_ids_3d.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
nx = 10
ny = 10
nz = 10
[]
[createNewSidesetOne]
type = SideSetsFromBoundingBoxGenerator
input = gen
block_id = 0
boundary_id_old = 'left bottom front'
boundary_id_new = 10
bottom_left = '-0.1 -0.1 -0.1'
top_right = '0.1 0.2 0.3'
[]
[createNewSidesetTwo]
type = SideSetsFromBoundingBoxGenerator
input = createNewSidesetOne
block_id = 0
boundary_id_old = 'right top back'
boundary_id_new = 11
bottom_left = '0.6 0.7 0.8'
top_right = '1.1 1.1 1.1'
[]
[createNewSidesetThree]
type = SideSetsFromBoundingBoxGenerator
input = createNewSidesetTwo
block_id = 0
boundary_id_old = 'left top back'
boundary_id_new = 12
bottom_left = '-0.1 0.9 0.9'
top_right = '0.1 1.1 1.1'
[]
[createNewSidesetFour]
type = SideSetsFromBoundingBoxGenerator
input = createNewSidesetThree
block_id = 0
boundary_id_old = 'front'
boundary_id_new = 13
bottom_left = '0.4 0.4 0.9'
top_right = '0.6 0.6 1.1'
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[firstBC]
type = DirichletBC
variable = u
boundary = 10
value = 1
[]
[secondBC]
type = DirichletBC
variable = u
boundary = 11
value = 0
[]
[thirdBC]
type = DirichletBC
variable = u
boundary = 12
value = 0
[]
[fourthBC]
type = DirichletBC
variable = u
boundary = 13
value = 0.5
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/cylindrical/2d-average-with-temp.i)
mu=1.1
rho=1.1
k=1.1
cp=1.1
advected_interp_method='average'
velocity_interp_method='average'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
[]
[]
[Problem]
fv_bcs_integrity_check = true
coord_type = 'RZ'
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
two_term_boundary_expansion = false
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
two_term_boundary_expansion = false
[]
[pressure]
type = INSFVPressureVariable
two_term_boundary_expansion = false
[]
[temperature]
type = INSFVEnergyVariable
two_term_boundary_expansion = false
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[u_forcing]
type = INSFVBodyForce
variable = u
functor = forcing_u
momentum_component = 'x'
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[v_forcing]
type = INSFVBodyForce
variable = v
functor = forcing_v
momentum_component = 'y'
[]
[temp_conduction]
type = FVDiffusion
coeff = 'k'
variable = temperature
[]
[temp_advection]
type = INSFVEnergyAdvection
variable = temperature
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
[]
[temp_forcing]
type = FVBodyForce
variable = temperature
function = forcing_t
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = u
function = 'exact_u'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = v
function = 'exact_v'
[]
[no-slip-wall-u]
type = INSFVNoSlipWallBC
boundary = 'right'
variable = u
function = 'exact_u'
[]
[no-slip-wall-v]
type = INSFVNoSlipWallBC
boundary = 'right'
variable = v
function = 'exact_v'
[]
[outlet-p]
type = INSFVOutletPressureBC
boundary = 'top'
variable = pressure
function = 'exact_p'
[]
[axis-u]
type = INSFVSymmetryVelocityBC
boundary = 'left'
variable = u
u = u
v = v
mu = ${mu}
momentum_component = x
[]
[axis-v]
type = INSFVSymmetryVelocityBC
boundary = 'left'
variable = v
u = u
v = v
mu = ${mu}
momentum_component = y
[]
[axis-p]
type = INSFVSymmetryPressureBC
boundary = 'left'
variable = pressure
[]
[axis-inlet-wall-t]
type = FVFunctionDirichletBC
boundary = 'left bottom right'
variable = temperature
function = 'exact_t'
[]
[]
[Materials]
[const_functor]
type = ADGenericFunctorMaterial
prop_names = 'cp k'
prop_values = '${cp} ${k}'
[]
[ins_fv]
type = INSFVEnthalpyMaterial
temperature = 'temperature'
rho = ${rho}
[]
[]
[Functions]
[exact_u]
type = ParsedFunction
value = 'sin(x*pi)^2*sin((1/2)*y*pi)'
[]
[exact_rhou]
type = ParsedFunction
value = 'rho*sin(x*pi)^2*sin((1/2)*y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_u]
type = ADParsedFunction
value = '(1/4)*pi^2*mu*sin(x*pi)^2*sin((1/2)*y*pi) - pi*sin(x*pi)*cos((1/2)*y*pi) + (4*x*pi*rho*sin(x*pi)^3*sin((1/2)*y*pi)^2*cos(x*pi) + rho*sin(x*pi)^4*sin((1/2)*y*pi)^2)/x + (-x*pi*rho*sin(x*pi)^2*sin((1/2)*y*pi)*sin(y*pi)*cos(x*pi) + (1/2)*x*pi*rho*sin(x*pi)^2*cos(x*pi)*cos((1/2)*y*pi)*cos(y*pi))/x - (-2*x*pi^2*mu*sin(x*pi)^2*sin((1/2)*y*pi) + 2*x*pi^2*mu*sin((1/2)*y*pi)*cos(x*pi)^2 + 2*pi*mu*sin(x*pi)*sin((1/2)*y*pi)*cos(x*pi))/x'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_v]
type = ParsedFunction
value = 'cos(x*pi)*cos(y*pi)'
[]
[exact_rhov]
type = ParsedFunction
value = 'rho*cos(x*pi)*cos(y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_v]
type = ADParsedFunction
value = 'pi^2*mu*cos(x*pi)*cos(y*pi) - 2*pi*rho*sin(y*pi)*cos(x*pi)^2*cos(y*pi) - 1/2*pi*sin((1/2)*y*pi)*cos(x*pi) - (-x*pi^2*mu*cos(x*pi)*cos(y*pi) - pi*mu*sin(x*pi)*cos(y*pi))/x + (-x*pi*rho*sin(x*pi)^3*sin((1/2)*y*pi)*cos(y*pi) + 2*x*pi*rho*sin(x*pi)*sin((1/2)*y*pi)*cos(x*pi)^2*cos(y*pi) + rho*sin(x*pi)^2*sin((1/2)*y*pi)*cos(x*pi)*cos(y*pi))/x'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_p]
type = ParsedFunction
value = 'cos(x*pi)*cos((1/2)*y*pi)'
[]
[forcing_p]
type = ParsedFunction
value = '-pi*rho*sin(y*pi)*cos(x*pi) + (2*x*pi*rho*sin(x*pi)*sin((1/2)*y*pi)*cos(x*pi) + rho*sin(x*pi)^2*sin((1/2)*y*pi))/x'
vars = 'rho'
vals = '${rho}'
[]
[exact_t]
type = ParsedFunction
value = 'sin(x*pi)*sin((1/2)*y*pi)'
[]
[forcing_t]
type = ParsedFunction
value = '(1/4)*pi^2*k*sin(x*pi)*sin((1/2)*y*pi) - (-x*pi^2*k*sin(x*pi)*sin((1/2)*y*pi) + pi*k*sin((1/2)*y*pi)*cos(x*pi))/x + (3*x*pi*cp*rho*sin(x*pi)^2*sin((1/2)*y*pi)^2*cos(x*pi) + cp*rho*sin(x*pi)^3*sin((1/2)*y*pi)^2)/x + (-x*pi*cp*rho*sin(x*pi)*sin((1/2)*y*pi)*sin(y*pi)*cos(x*pi) + (1/2)*x*pi*cp*rho*sin(x*pi)*cos(x*pi)*cos((1/2)*y*pi)*cos(y*pi))/x'
vars = 'k rho cp'
vals = '${k} ${rho} ${cp}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
[]
[Outputs]
exodus = true
csv = true
[dof]
type = DOFMap
execute_on = 'initial'
[]
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[./L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2v]
type = ElementL2Error
variable = v
function = exact_v
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2p]
variable = pressure
function = exact_p
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2t]
variable = temperature
function = exact_t
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[]
(test/tests/materials/discrete/recompute_no_calc.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 1
[]
[./left_domain]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '0 0 0'
top_right = '0.5 1 0'
block_id = 10
[../]
[]
[Variables]
[./u]
initial_condition = 2
[../]
[]
[Kernels]
[./diff]
type = MatDiffusionTest
variable = u
prop_name = 'p'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 2
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 3
[../]
[]
[Materials]
[./recompute_props]
type = RecomputeMaterial
block = '0'
f_name = 'f'
f_prime_name = 'f_prime'
p_name = 'p'
outputs = all
output_properties = 'f f_prime p'
compute = false
[../]
[./newton]
type = NewtonMaterial
block = 0
outputs = all
f_name = 'f'
f_prime_name = 'f_prime'
p_name = 'p'
material = recompute_props
max_iterations = 0
[../]
[./left]
type = GenericConstantMaterial
prop_names = 'f f_prime p'
prop_values = '1 0.5 1.2345'
block = 10
outputs = all
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
print_linear_residuals = true
perf_graph = true
[]
(test/tests/restrictable/boundary_api_test/boundary_restrictable.i)
[Mesh]
type = FileMesh
file = rectangle.e
dim = 2
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = BndTestDirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Materials]
[./mat0]
type = GenericConstantMaterial
boundary = 1
prop_names = 'a'
prop_values = '1'
[../]
[./mat1]
type = GenericConstantMaterial
boundary = 2
prop_names = 'a b'
prop_values = '10 20'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/interfacekernels/1d_interface/coupled_value_coupled_flux.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 10
xmax = 2
[]
[./subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '1.0 0 0'
block_id = 1
top_right = '2.0 1.0 0'
[../]
[./interface]
input = subdomain1
type = SideSetsBetweenSubdomainsGenerator
primary_block = '0'
paired_block = '1'
new_boundary = 'primary0_interface'
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
block = '0'
[../]
[./v]
order = FIRST
family = LAGRANGE
block = '1'
[../]
[]
[Kernels]
[./diff_u]
type = CoeffParamDiffusion
variable = u
D = 4
block = 0
[../]
[./diff_v]
type = CoeffParamDiffusion
variable = v
D = 2
block = 1
[../]
[]
[InterfaceKernels]
active = 'interface'
[./interface]
type = InterfaceDiffusion
variable = u
neighbor_var = v
boundary = primary0_interface
D = 'D'
D_neighbor = 'D'
[../]
[./penalty_interface]
type = PenaltyInterfaceDiffusion
variable = u
neighbor_var = v
boundary = primary0_interface
penalty = 1e6
[../]
[]
[BCs]
active = 'left right middle'
[./left]
type = DirichletBC
variable = u
boundary = 'left'
value = 1
[../]
[./right]
type = DirichletBC
variable = v
boundary = 'right'
value = 0
[../]
[./middle]
type = MatchedValueBC
variable = v
boundary = 'primary0_interface'
v = u
[../]
[]
[Materials]
[./stateful]
type = StatefulMaterial
initial_diffusivity = 1
boundary = primary0_interface
[../]
[./block0]
type = GenericConstantMaterial
block = '0'
prop_names = 'D'
prop_values = '4'
[../]
[./block1]
type = GenericConstantMaterial
block = '1'
prop_names = 'D'
prop_values = '2'
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
print_linear_residuals = true
[]
[Debug]
show_var_residual_norms = true
[]
(test/tests/kernels/ad_mat_diffusion/ad_2d_steady_state.i)
# This test solves a 2D steady state heat equation
# The error is found by comparing to the analytical solution
# Note that the thermal conductivity, specific heat, and density in this problem
# Are set to 1, and need to be changed to the constants of the material being
# Analyzed
[Mesh]
type = GeneratedMesh
dim = 2
nx = 30
ny = 30
xmax = 2
ymax = 2
[]
[Variables]
[./T]
[../]
[]
[Kernels]
[./HeatDiff]
type = ADMatDiffusion
variable = T
diffusivity = diffusivity
[../]
[]
[BCs]
[./zero]
type = DirichletBC
variable = T
boundary = 'left right bottom'
value = 0
[../]
[./top]
type = ADFunctionDirichletBC
variable = T
boundary = top
function = '10*sin(pi*x*0.5)'
[../]
[]
[Materials]
[./k]
type = ADGenericConstantMaterial
prop_names = diffusivity
prop_values = 1
[../]
[]
[Postprocessors]
[./nodal_error]
type = NodalL2Error
function = '10/(sinh(pi))*sin(pi*x*0.5)*sinh(pi*y*0.5)'
variable = T
outputs = console
[../]
[./elemental_error]
type = ElementL2Error
function = '10/(sinh(pi))*sin(pi*x*0.5)*sinh(pi*y*0.5)'
variable = T
outputs = console
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/actions/get_actions/test_get_actions.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
uniform_refine = 4
[]
[TestGetActions]
[]
[Variables]
[./convected]
[../]
[./diffused]
[../]
[]
[Kernels]
# intentionally give a name the same as material names
[./mat1]
type = Diffusion
variable = convected
[../]
[./diff_u]
type = Diffusion
variable = diffused
[../]
[]
[BCs]
active = 'left_convected right_convected left_diffused right_diffused'
[./left_convected]
type = DirichletBC
variable = convected
boundary = '1'
value = 0
[../]
[./right_convected]
type = DirichletBC
variable = convected
boundary = '2'
value = 1
[../]
[./left_diffused]
type = DirichletBC
variable = diffused
boundary = '1'
value = 0
[../]
[./right_diffused]
type = DirichletBC
variable = diffused
boundary = '2'
value = 1
[../]
[]
[Materials]
[./mat4]
type = RandomMaterial
block = 0
[../]
[./mat3]
type = MTMaterial
block = 0
[../]
[./mat1]
type = GenericConstantMaterial
prop_names = prop1
prop_values = 1.0
block = 0
[../]
[./mat2]
type = CoupledMaterial
mat_prop = prop2
coupled_mat_prop = prop1
block = 0
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
execute_on = 'timestep_end'
[]
(test/tests/globalparams/global_param/global_param_test.i)
[GlobalParams]
variable = u
dim = 2
[]
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
# dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
# variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
# variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
# variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/chemical_reactions/test/tests/equilibrium_const/maier_kelly.i)
# Test of EquilibriumConstantAux with eight log10(Keq) values.
# The resulting equilibrium constant should be a Maier-Kelly best fit.
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
[]
[AuxVariables]
[./logk]
[../]
[]
[AuxKernels]
[./logk]
type = EquilibriumConstantAux
temperature = temperature
temperature_points = '273.16 298.15 333.15 373.15 423.15 473.15 523.15 573.15'
logk_points = '-6.5804 -6.3447 -6.2684 -6.3882 -6.7235 -7.1969 -7.7868 -8.5280'
variable = logk
[../]
[]
[Variables]
[./temperature]
[../]
[]
[Kernels]
[./temperature]
type = Diffusion
variable = temperature
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = temperature
value = 300
boundary = left
[../]
[./right]
type = DirichletBC
variable = temperature
value = 573.15
boundary = right
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/mesh/named_entities/name_on_the_fly.i)
[Mesh]
file = three_block.e
# These names will be applied on the fly to the
# mesh so that they can be used in the input file
# In addition they will show up in the output file
block_id = '1 2 3'
block_name = 'wood steel copper'
boundary_id = '1 2'
boundary_name = 'left right'
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[../]
[]
[Materials]
active = empty
[./empty]
type = MTMaterial
block = 'wood steel copper'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/parser/active_inactive/top_level.i)
#############################################################
# This input file demonstrates the use of inactive at the
# top level.
##############################################################
inactive = 'Executioner' # This will produce an error about missing Executioner
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
active = 'u'
[./u]
[../]
[]
[AuxVariables]
inactive = 'aux1 aux3'
# The parameters in the inactive sections can be invalid because
# they are never parsed.
[./aux1]
type = DoesntExist
flintstones = 'fred wilma'
[../]
[./aux2]
[../]
[./aux3]
order = TENZILLION
[../]
[./aux4]
[../]
[]
[AuxKernels]
active = 'aux2 aux4'
# You can use active or inactive depending on whatever is easier
[./aux1]
type = ConstantAux
value = 1
variable = aux1
[../]
[./aux2]
type = ConstantAux
value = 2
variable = aux2
[../]
[./aux3]
type = ConstantAux
value = 3
variable = aux3
[../]
[./aux4]
type = ConstantAux
value = 4
variable = aux4
[../]
[]
[Kernels]
inactive = ''
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
inactive = ''
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
inactive = Adaptivity
[./Adaptivity]
[../]
[]
# No output so we can override several parameters and test them concurrently
(modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/ad_rz_cone_by_parts_traction_steady_stabilized.i)
[GlobalParams]
order = FIRST
integrate_p_by_parts = true
viscous_form = 'traction'
[]
[Mesh]
file = '2d_cone.msh'
[]
[Problem]
coord_type = RZ
[]
[AuxVariables]
[vel_x]
[]
[vel_y]
[]
[]
[AuxKernels]
[vel_x]
type = VectorVariableComponentAux
variable = vel_x
vector_variable = velocity
component = 'x'
[]
[vel_y]
type = VectorVariableComponentAux
variable = vel_y
vector_variable = velocity
component = 'y'
[]
[]
[Variables]
[./velocity]
family = LAGRANGE_VEC
[../]
[./p]
[../]
[]
# Need to set a non-zero initial condition because we have a velocity norm in
# the denominator for the tau coefficient of the stabilization term
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[mass_pspg]
type = INSADMassPSPG
variable = p
[]
[momentum_advection]
type = INSADMomentumAdvection
variable = velocity
[]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
[../]
[momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[]
[]
[BCs]
[inlet]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom'
function_x = 0
function_y = 'inlet_func'
[../]
[wall]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'right'
function_x = 0
function_y = 0
[]
[axis]
type = ADVectorFunctionDirichletBC
variable = velocity
boundary = 'left'
set_y_comp = false
function_x = 0
[]
[]
[Functions]
[./inlet_func]
type = ParsedFunction
value = '-4 * x^2 + 1'
[../]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[ins_mat]
type = INSADTauMaterial
velocity = velocity
pressure = p
[]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = 'bjacobi ilu 4'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
csv = true
console = true
[./out]
type = Exodus
[../]
[]
[Postprocessors]
[./flow_in]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'bottom'
execute_on = 'timestep_end'
[../]
[./flow_out]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'top'
execute_on = 'timestep_end'
[../]
[]
(modules/porous_flow/examples/co2_intercomparison/1Dradial/properties.i)
# Liquid and gas properties for code intercomparison problem 3
#
# From Pruess et al, Code intercomparison builds confidence in
# numerical simulation models for geologic disposal of CO2, Energy 29 (2004)
#
# This test simply calculates density and viscosity of each phase for
# various pressures and salinities, as well as mass fractions of CO2 in the
# liquid phase and H2O in the gas phase.
#
# Four versions of this are run:
# 1) No CO2, 0 salt mass fraction (pure water)
# 2) Enough CO2 to form gas phase, 0 salt mass fraction (pure water)
# 3) No CO2, 0.15 salt mass fraction
# 4) Enough CO2 to form gas phase, 0.15 salt mass fraction
#
# These results compare well with detailed results presented in Pruess et al,
# Intercomparison of numerical simulation codes for geologic disposal of CO2,
# LBNL-51813 (2002)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
xmax = 4
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[AuxVariables]
[density_liquid]
order = CONSTANT
family = MONOMIAL
[]
[density_gas]
order = CONSTANT
family = MONOMIAL
[]
[viscosity_liquid]
order = CONSTANT
family = MONOMIAL
[]
[viscosity_gas]
order = CONSTANT
family = MONOMIAL
[]
[x1]
order = CONSTANT
family = MONOMIAL
[]
[y0]
order = CONSTANT
family = MONOMIAL
[]
[xnacl]
initial_condition = 0.0
[]
[]
[AuxKernels]
[density_liquid]
type = PorousFlowPropertyAux
variable = density_liquid
property = density
phase = 0
execute_on = timestep_end
[]
[density_gas]
type = PorousFlowPropertyAux
variable = density_gas
property = density
phase = 1
execute_on = timestep_end
[]
[viscosity_liquid]
type = PorousFlowPropertyAux
variable = viscosity_liquid
property = viscosity
phase = 0
execute_on = timestep_end
[]
[viscosity_gas]
type = PorousFlowPropertyAux
variable = viscosity_gas
property = viscosity
phase = 1
execute_on = timestep_end
[]
[x1]
type = PorousFlowPropertyAux
variable = x1
property = mass_fraction
phase = 0
fluid_component = 1
execute_on = timestep_end
[]
[y0]
type = PorousFlowPropertyAux
variable = y0
property = mass_fraction
phase = 1
fluid_component = 0
execute_on = timestep_end
[]
[]
[Variables]
[pgas]
order = CONSTANT
family = MONOMIAL
[]
[zi]
initial_condition = 0.0
[]
[]
[Functions]
[pic]
type = ParsedFunction
value = 'if(x<1,12e6,if(x<2,16e6,if(x<3,20e6,24e6)))'
[]
[]
[ICs]
[pic]
type = FunctionIC
function = pic
variable = pgas
[]
[]
[Kernels]
[diffusionp]
type = NullKernel
variable = pgas
[]
[diffusionz]
type = NullKernel
variable = zi
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pgas zi'
number_fluid_phases = 2
number_fluid_components = 2
[]
[pc]
type = PorousFlowCapillaryPressureConst
pc = 0
[]
[fs]
type = PorousFlowBrineCO2
brine_fp = brine
co2_fp = co2
capillary_pressure = pc
[]
[]
[Modules]
[FluidProperties]
[co2]
type = CO2FluidProperties
[]
[brine]
type = BrineFluidProperties
[]
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
temperature = 45
[]
[brineco2]
type = PorousFlowFluidState
gas_porepressure = pgas
z = zi
temperature_unit = Celsius
xnacl = xnacl
capillary_pressure = pc
fluid_state = fs
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -sub_pc_factor_shift_type -pc_asm_overlap'
petsc_options_value = 'gmres asm lu NONZERO 2 '
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
perf_graph = true
csv = true
execute_on = timestep_end
file_base = properties_water
[]
[VectorPostprocessors]
[vpp]
type = ElementValueSampler
variable = 'pgas density_liquid density_gas viscosity_liquid viscosity_gas x1 y0'
sort_by = x
[]
[]
(test/tests/outputs/oversample/ex02_adapt.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
nz = 0
zmax = 0
elem_type = QUAD9
[]
[Variables]
[./diffused]
order = SECOND
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = diffused
[../]
[]
[DiracKernels]
[./foo]
variable = diffused
type = ConstantPointSource
value = 1
point = '0.3 0.3 0.0'
[../]
[]
[BCs]
[./all]
type = DirichletBC
variable = diffused
boundary = 'bottom left right top'
value = 0.0
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
[]
[Adaptivity]
max_h_level = 2
initial_steps = 2
marker = marker
steps = 2
initial_marker = marker
[./Indicators]
[./indicator]
type = GradientJumpIndicator
variable = diffused
[../]
[../]
[./Markers]
[./marker]
type = ErrorFractionMarker
indicator = indicator
refine = 0.5
[../]
[../]
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[./os2]
type = Exodus
refinements = 2
[../]
[./os4]
type = Exodus
refinements = 4
[../]
[]
(test/tests/misc/check_error/check_dynamic_name_boundary_mismatch.i)
[Mesh]
file = three_block.e
# These names will be applied on the fly to the
# mesh so they can be used in the input file
# In addition they will show up in the input file
block_id = '1 2 3'
block_name = 'wood steel copper'
boundary_id = '1'
boundary_name = 'left right'
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[../]
[]
[Materials]
active = empty
[./empty]
type = MTMaterial
block = 'wood steel copper'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(modules/phase_field/test/tests/initial_conditions/MultiBoundingBoxIC3D.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 10
ny = 10
nz = 10
[]
[Variables]
[./c1]
order = FIRST
family = LAGRANGE
[../]
[./c2]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./c1]
type = MultiBoundingBoxIC
corners = '0.1 0.0 0.1 0.8 0.5 0.0 0.0 1.0 0.4'
opposite_corners = '0.5 0.5 0.6 0.2 0.9 0.4 0.4 0.6 1.0'
inside = '1.0'
outside = 0.1
variable = c1
[../]
[./c2]
type = MultiBoundingBoxIC
corners = '0.1 0.0 0.1 0.8 0.5 0.0 0.3 0.2 0.4'
opposite_corners = '0.8 0.5 0.6 0.2 0.9 0.4 0.7 0.9 1.0'
inside = '1.0 2.0 3.0'
outside = 0.1
variable = c2
[../]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
kernel_coverage_check = false
[]
[Outputs]
exodus = true
[]
(modules/thermal_hydraulics/test/tests/functions/piecewise_function/piecewise_function.i)
# This test tests the PiecewiseFunction, which pieces functions together.
# Piecing together the 2 CosineTransitionFunction functions should yield the
# CosineHumpFunction function. This test samples the PiecewiseFunction and the
# CosineHumpFunction and compares the samples using the
# VectorPostprocessorComparison post-processor.
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Functions]
[function_left]
type = CosineTransitionFunction
axis = y
transition_center = 2
transition_width = 2
function1 = 5
function2 = 20
[]
[function_right]
type = CosineTransitionFunction
axis = y
transition_center = 4
transition_width = 2
function1 = 20
function2 = 5
[]
[function_end]
type = ConstantFunction
value = 5
[]
[function_piecewise]
type = PiecewiseFunction
axis = y
axis_coordinates = '3 5'
functions = 'function_left function_right function_end'
[]
[function_gold]
type = CosineHumpFunction
axis = y
hump_center_position = 3
hump_width = 4
hump_begin_value = 5
hump_center_value = 20
[]
[]
[VectorPostprocessors]
[piecewise_function_vpp]
type = LineFunctionSampler
functions = 'function_piecewise function_gold'
sort_by = y
start_point = '0 0 0'
end_point = '0 6 0'
num_points = 20
execute_on = 'initial'
[]
[]
[Postprocessors]
[matches_gold]
type = VectorPostprocessorComparison
comparison_type = equals
vectorpostprocessor_a = piecewise_function_vpp
vectorpostprocessor_b = piecewise_function_vpp
vector_name_a = function_piecewise
vector_name_b = function_gold
execute_on = 'initial'
[]
[]
[Outputs]
csv = true
show = 'matches_gold'
execute_on = 'initial'
[]
(test/tests/misc/check_error/function_file_test12.i)
# Test for usage of missing function
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = ic_function
[../]
[../]
[]
[Functions]
[./ic_function]
type = PiecewiseLinear
data_file = piecewise_linear_columns_more_data.csv
format = columns
xy_in_file_only = false
y_index_in_file = 3 #Will generate error because data does not contain 4 columns
scale_factor = 1.0
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/outputs/format/output_test_sln.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
nz = 0
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
solution_history = true
[]
(modules/thermal_hydraulics/test/tests/materials/wall_heat_transfer_coefficient_3eqn_dittus_boelter/test.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
allow_renumbering = false
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[AuxVariables]
[Hw]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[Hw_ak]
type = MaterialRealAux
variable = Hw
property = Hw
[]
[]
[Materials]
[props]
type = GenericConstantMaterial
prop_names = 'rho vel D_h k mu cp T T_wall'
prop_values = '1000 0.1 0.1 0.001 0.1 12 300 310'
[]
[Hw_material]
type = WallHeatTransferCoefficient3EqnDittusBoelterMaterial
rho = rho
vel = vel
D_h = D_h
k = k
mu = mu
cp = cp
T = T
T_wall = T_wall
[]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[Hw]
type = ElementalVariableValue
elementid = 0
variable = Hw
[]
[]
[Outputs]
csv = true
execute_on = timestep_end
[]
(test/tests/kernels/jxw_grad_test_dep_on_displacements/jxw-spherical.i)
[GlobalParams]
displacements = 'disp_r'
order = SECOND
[]
[Mesh]
type = GeneratedMesh
dim = 1
nx = 3
elem_type = EDGE3
[]
[Problem]
coord_type = RSPHERICAL
[]
[Variables]
[./disp_r]
[../]
[./u]
order = FIRST
[../]
[]
[Kernels]
[./disp_r]
type = Diffusion
variable = disp_r
[../]
[./u]
type = ADDiffusion
variable = u
use_displaced_mesh = true
[../]
[]
[BCs]
# BCs cannot be preset due to Jacobian tests
[./u_left]
type = DirichletBC
preset = false
value = 0
boundary = 'left'
variable = u
[../]
[./u_right]
type = DirichletBC
preset = false
value = 1
boundary = 'right'
variable = u
[../]
[./disp_r_left]
type = DirichletBC
preset = false
value = 0
boundary = 'left'
variable = disp_r
[../]
[./disp_r_right]
type = DirichletBC
preset = false
value = 1
boundary = 'right'
variable = disp_r
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
[./dofmap]
type = DOFMap
execute_on = 'initial'
[../]
exodus = true
[]
[ICs]
[./disp_r]
type = RandomIC
variable = disp_r
min = 0.01
max = 0.09
[../]
[./u]
type = RandomIC
variable = u
min = 0.1
max = 0.9
[../]
[]
(modules/stochastic_tools/examples/surrogates/polynomial_regression/sub.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 100
xmax = 1
elem_type = EDGE3
[]
[Variables]
[T]
order = SECOND
family = LAGRANGE
[]
[]
[Kernels]
[diffusion]
type = MatDiffusion
variable = T
diffusivity = k
[]
[source]
type = BodyForce
variable = T
value = 1.0
[]
[]
[Materials]
[conductivity]
type = GenericConstantMaterial
prop_names = k
prop_values = 2.0
[]
[]
[BCs]
[right]
type = DirichletBC
variable = T
boundary = right
value = 300
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Postprocessors]
[max]
type = NodalExtremeValue
variable = T
value_type = max
[]
[]
[Outputs]
[]
(examples/ex10_aux/ex10.i)
[Mesh]
file = car.e
[]
[Variables]
[diffused]
order = FIRST
family = LAGRANGE
[]
[]
# Here is the AuxVariables section where we declare the variables that
# will hold the AuxKernel calcuations. The declaration syntax is very
# similar to that of the regular variables section
[AuxVariables]
[nodal_aux]
order = FIRST
family = LAGRANGE
[]
[element_aux]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = diffused
[]
[]
# Here is the AuxKernels section where we enable the AuxKernels, link
# them to our AuxVariables, set coupling parameters, and set input parameters
[AuxKernels]
[nodal_example]
type = ExampleAux
variable = nodal_aux
value = 3.0
coupled = diffused
[]
[element_example]
type = ExampleAux
variable = element_aux
value = 4.0
coupled = diffused
[]
[]
[BCs]
[bottom]
type = DirichletBC
variable = diffused
boundary = 'bottom'
value = 0
[]
[top]
type = DirichletBC
variable = diffused
boundary = 'top'
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/1d-average.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='average'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
xmin = 0
xmax = 1
nx = 2
[]
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
pressure = pressure
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
two_term_boundary_expansion = false
[]
[pressure]
type = INSFVPressureVariable
two_term_boundary_expansion = false
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[u_forcing]
type = INSFVBodyForce
variable = u
functor = forcing_u
momentum_component = 'x'
[]
[]
[FVBCs]
[inlet_u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = 'exact_u'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 'exact_p'
[]
[]
[Functions]
[exact_u]
type = ParsedFunction
value = 'sin((1/2)*x*pi)'
[]
[exact_rhou]
type = ParsedFunction
value = 'rho*sin((1/2)*x*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_u]
type = ADParsedFunction
value = '(1/4)*pi^2*mu*sin((1/2)*x*pi) + pi*rho*sin((1/2)*x*pi)*cos((1/2)*x*pi) - 1/2*pi*sin((1/2)*x*pi)'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_p]
type = ParsedFunction
value = 'cos((1/2)*x*pi)'
[]
[forcing_p]
type = ParsedFunction
value = '(1/2)*pi*rho*cos((1/2)*x*pi)'
vars = 'rho'
vals = '${rho}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[./L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2p]
variable = pressure
function = exact_p
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[]
(test/tests/transfers/multiapp_nearest_node_transfer/target_boundary_sub.i)
[Mesh]
[drmg]
type = DistributedRectilinearMeshGenerator
dim = 2
nx = 30
ny = 30
elem_type = QUAD4
partition = square
[]
[]
[Variables]
[u][]
[]
[AuxVariables]
[source][]
[]
[Kernels]
[conduction]
type = Diffusion
variable = u
[]
[]
[BCs]
[flux]
type = CoupledVarNeumannBC
variable = u
boundary = 'right'
v = source
[]
[bdr]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-6
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/pins/mms/porosity_change/pressure-interpolation-corrected-action.i)
mu=1.1
rho=1.1
darcy=1.1
forch=1.1
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 2
ymin = -1
ymax = 1
nx = 2
ny = 2
[]
[]
[AuxVariables]
[eps_out]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[eps_out]
type = ADFunctorElementalAux
variable = eps_out
functor = porosity
execute_on = 'timestep_end'
[]
[]
[Modules]
[NavierStokesFV]
compressibility = 'incompressible'
porous_medium_treatment = true
porosity = porosity
porosity_smoothing_layers = 2
friction_types = 'darcy forchheimer'
friction_coeffs = 'Darcy_coefficient Forchheimer_coefficient'
use_friction_correction = true
consistent_scaling = 1.0
density = 'rho'
dynamic_viscosity = 'mu'
initial_velocity = '1 1 0'
initial_pressure = 0.0
inlet_boundaries = 'left top bottom'
momentum_inlet_types = 'fixed-velocity fixed-velocity fixed-velocity'
momentum_inlet_function = 'exact_u exact_v exact_u exact_v exact_u exact_v'
outlet_boundaries = 'right'
momentum_outlet_types = 'fixed-pressure'
pressure_function = 'exact_p'
[]
[]
[FVKernels]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[u_forcing]
type = INSFVBodyForce
variable = superficial_vel_x
functor = forcing_u
momentum_component = 'x'
rhie_chow_user_object = 'pins_rhie_chow_interpolator'
[]
[v_forcing]
type = INSFVBodyForce
variable = superficial_vel_y
functor = forcing_v
momentum_component = 'y'
rhie_chow_user_object = 'pins_rhie_chow_interpolator'
[]
[]
[Materials]
[darcy]
type = ADGenericVectorFunctorMaterial
prop_names = 'Darcy_coefficient Forchheimer_coefficient'
prop_values = '${darcy} ${darcy} ${darcy} ${forch} ${forch} ${forch}'
[]
[constants]
type = ADGenericFunctorMaterial
prop_names = 'rho mu'
prop_values = '${rho} ${mu}'
[]
[]
[Functions]
[porosity]
type = ADParsedFunction
value = '.5 + .1 * sin(pi * x / 4) * cos(pi * y / 4)'
[]
[exact_u]
type = ParsedFunction
value = 'sin((1/2)*y*pi)*cos((1/2)*x*pi)'
[]
[forcing_u]
type = ADParsedFunction
value = '-mu*(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)*(-1/4*pi^2*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) + 0.025*pi^2*sin((1/4)*x*pi)*sin((1/4)*y*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2 + 0.00625*pi^2*sin((1/4)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*x*pi)*cos((1/4)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2 + 0.00125*pi^2*sin((1/4)*x*pi)^2*sin((1/4)*y*pi)^2*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^3) - mu*(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)*(-1/4*pi^2*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) + 0.00625*pi^2*sin((1/4)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*x*pi)*cos((1/4)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2 + 0.025*pi^2*sin((1/2)*x*pi)*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/4)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2 + 0.00125*pi^2*sin((1/2)*y*pi)*cos((1/4)*x*pi)^2*cos((1/2)*x*pi)*cos((1/4)*y*pi)^2/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^3) - 0.025*pi*mu*(-1/2*pi*sin((1/2)*x*pi)*sin((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) - 0.025*pi*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/4)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2)*cos((1/4)*x*pi)*cos((1/4)*y*pi) + 0.025*pi*mu*((1/2)*pi*cos((1/2)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) + 0.025*pi*sin((1/4)*x*pi)*sin((1/4)*y*pi)*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2)*sin((1/4)*x*pi)*sin((1/4)*y*pi) + rho*(darcy + forch)*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) - 1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) + (1/2)*pi*rho*sin((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)^2/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) - pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) + 0.025*pi*rho*sin((1/4)*x*pi)^2*sin((1/4)*y*pi)*sin((1/2)*y*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2 - 0.025*pi*rho*sin((1/2)*y*pi)^2*cos((1/4)*x*pi)*cos((1/2)*x*pi)^2*cos((1/4)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2 - 1/4*pi*(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)*sin((1/4)*x*pi)*sin((3/2)*y*pi)'
vars = 'mu rho darcy forch'
vals = '${mu} ${rho} ${darcy} ${forch}'
[]
[exact_v]
type = ParsedFunction
value = 'sin((1/4)*x*pi)*cos((1/2)*y*pi)'
[]
[forcing_v]
type = ADParsedFunction
value = '-mu*(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)*(-1/4*pi^2*sin((1/4)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) - 0.025*pi^2*sin((1/4)*x*pi)^2*sin((1/4)*y*pi)*sin((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2 + 0.00625*pi^2*sin((1/4)*x*pi)^2*cos((1/4)*y*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2 + 0.00125*pi^2*sin((1/4)*x*pi)^3*sin((1/4)*y*pi)^2*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^3) - mu*(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)*(-1/16*pi^2*sin((1/4)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) + 0.00625*pi^2*sin((1/4)*x*pi)^2*cos((1/4)*y*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2 - 0.0125*pi^2*cos((1/4)*x*pi)^2*cos((1/4)*y*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2 + 0.00125*pi^2*sin((1/4)*x*pi)*cos((1/4)*x*pi)^2*cos((1/4)*y*pi)^2*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^3) + 0.025*pi*mu*(-1/2*pi*sin((1/4)*x*pi)*sin((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) + 0.025*pi*sin((1/4)*x*pi)^2*sin((1/4)*y*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2)*sin((1/4)*x*pi)*sin((1/4)*y*pi) - 0.025*pi*mu*((1/4)*pi*cos((1/4)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) - 0.025*pi*sin((1/4)*x*pi)*cos((1/4)*x*pi)*cos((1/4)*y*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2)*cos((1/4)*x*pi)*cos((1/4)*y*pi) + rho*(darcy + forch)*sin((1/4)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) - pi*rho*sin((1/4)*x*pi)^2*sin((1/2)*y*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) - 1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) + (1/4)*pi*rho*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) + 0.025*pi*rho*sin((1/4)*x*pi)^3*sin((1/4)*y*pi)*cos((1/2)*y*pi)^2/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2 - 0.025*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/4)*y*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2 + (3/2)*pi*(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)*cos((1/4)*x*pi)*cos((3/2)*y*pi)'
vars = 'mu rho darcy forch'
vals = '${mu} ${rho} ${darcy} ${forch}'
[]
[exact_p]
type = ParsedFunction
value = 'sin((3/2)*y*pi)*cos((1/4)*x*pi)'
[]
[forcing_p]
type = ParsedFunction
value = '-1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi) - 1/2*pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = false
csv = true
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2u]
type = ElementL2Error
variable = superficial_vel_x
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2v]
type = ElementL2Error
variable = superficial_vel_y
function = exact_v
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2p]
type = ElementL2Error
variable = pressure
function = exact_p
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(modules/fluid_properties/test/tests/functions/saturation_pressure_function/saturation_pressure_function.i)
# TestTwoPhaseFluidProperties has the following saturation pressure function:
# p_sat(p) = 3 T
# Thus for T = 5, p_sat should be 15.
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
[]
[Modules]
[./FluidProperties]
[./fp_liquid]
type = IdealGasFluidProperties
[../]
[./fp_vapor]
type = IdealGasFluidProperties
[../]
[./fp_2phase]
type = TestTwoPhaseFluidProperties
fp_liquid = fp_liquid
fp_vapor = fp_vapor
[../]
[]
[]
[Functions]
[./T]
type = ConstantFunction
value = 5
[../]
[./p_sat]
type = SaturationPressureFunction
T = T
fp_2phase = fp_2phase
[../]
[]
[Postprocessors]
[./p_sat_pp]
type = FunctionValuePostprocessor
function = p_sat
execute_on = 'INITIAL'
[../]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
[]
(modules/richards/test/tests/gravity_head_2/gh04.i)
# unsaturated = true
# gravity = true
# supg = true
# transient = false
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
xmin = 0
xmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = 'pwater pgas'
[../]
[./DensityWater]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0E2
[../]
[./DensityGas]
type = RichardsDensityConstBulk
dens0 = 0.5
bulk_mod = 0.5E2
[../]
[./SeffWater]
type = RichardsSeff2waterVG
m = 0.8
al = 1
[../]
[./SeffGas]
type = RichardsSeff2gasVG
m = 0.8
al = 1
[../]
[./RelPermWater]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./RelPermGas]
type = RichardsRelPermPower
simm = 0.0
n = 3
[../]
[./SatWater]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.15
[../]
[./SatGas]
type = RichardsSat
s_res = 0.05
sum_s_res = 0.15
[../]
[./SUPGwater]
type = RichardsSUPGstandard
p_SUPG = 1E-3
[../]
[./SUPGgas]
type = RichardsSUPGstandard
p_SUPG = 1E-3
[../]
[]
[Variables]
[./pwater]
order = FIRST
family = LAGRANGE
[../]
[./pgas]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
# get nonconvergence if initial condition is too crazy
[./water_ic]
type = FunctionIC
function = '1-x/2'
variable = pwater
[../]
[./gas_ic]
type = FunctionIC
function = '4-x/5'
variable = pgas
[../]
[]
[Kernels]
active = 'richardsfwater richardsfgas'
[./richardstwater]
type = RichardsMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFlux
variable = pwater
[../]
[./richardstgas]
type = RichardsMassChange
variable = pgas
[../]
[./richardsfgas]
type = RichardsFlux
variable = pgas
[../]
[]
[AuxVariables]
[./seffgas]
[../]
[./seffwater]
[../]
[]
[AuxKernels]
[./seffgas_kernel]
type = RichardsSeffAux
pressure_vars = 'pwater pgas'
seff_UO = SeffGas
variable = seffgas
[../]
[./seffwater_kernel]
type = RichardsSeffAux
pressure_vars = 'pwater pgas'
seff_UO = SeffWater
variable = seffwater
[../]
[]
[Postprocessors]
[./pw_left]
type = PointValue
point = '0 0 0'
variable = pwater
outputs = none
[../]
[./pw_right]
type = PointValue
point = '1 0 0'
variable = pwater
outputs = none
[../]
[./error_water]
type = FunctionValuePostprocessor
function = fcn_error_water
[../]
[./pg_left]
type = PointValue
point = '0 0 0'
variable = pgas
outputs = none
[../]
[./pg_right]
type = PointValue
point = '1 0 0'
variable = pgas
outputs = none
[../]
[./error_gas]
type = FunctionValuePostprocessor
function = fcn_error_gas
[../]
[]
[Functions]
[./fcn_error_water]
type = ParsedFunction
value = 'abs((-b*log(-(gdens0*xval+(-b*exp(-p0/b)))/b)-p1)/p1)'
vars = 'b gdens0 p0 xval p1'
vals = '1E2 -1 pw_left 1 pw_right'
[../]
[./fcn_error_gas]
type = ParsedFunction
value = 'abs((-b*log(-(gdens0*xval+(-b*exp(-p0/b)))/b)-p1)/p1)'
vars = 'b gdens0 p0 xval p1'
vals = '0.5E2 -0.5 pg_left 1 pg_right'
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
density_UO = 'DensityWater DensityGas'
relperm_UO = 'RelPermWater RelPermGas'
SUPG_UO = 'SUPGwater SUPGgas'
sat_UO = 'SatWater SatGas'
seff_UO = 'SeffWater SeffGas'
viscosity = '1E-3 0.5E-3'
gravity = '-1 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -sub_pc_factor_shift_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'gmres asm lu NONZERO 1E-10 1E-10 10000'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = gh04
csv = true
[]
(test/tests/dgkernels/3d_diffusion_dg/3d_diffusion_dg_test.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 5
ny = 5
nz = 5
xmin = 0
xmax = 1
ymin = 0
ymax = 1
zmin = 0
zmax = 1
elem_type = HEX8
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = MONOMIAL
[./InitialCondition]
type = ConstantIC
value = 0.5
[../]
[../]
[]
[Functions]
active = 'forcing_fn exact_fn'
[./forcing_fn]
type = ParsedFunction
value = 2*pow(e,-x-(y*y))*(1-2*y*y)
[../]
[./exact_fn]
type = ParsedGradFunction
value = pow(e,-x-(y*y))
grad_x = -pow(e,-x-(y*y))
grad_y = -2*y*pow(e,-x-(y*y))
[../]
[]
[Kernels]
active = 'diff abs forcing'
[./diff]
type = Diffusion
variable = u
[../]
[./abs] # u * v
type = Reaction
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[DGKernels]
active = 'dg_diff'
[./dg_diff]
type = DGDiffusion
variable = u
epsilon = -1
sigma = 6
[../]
[]
[BCs]
active = 'all'
[./all]
type = DGFunctionDiffusionDirichletBC
variable = u
boundary = '0 1 2 3 4 5'
function = exact_fn
epsilon = -1
sigma = 6
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Postprocessors]
active = 'h dofs l2_err'
[./h]
type = AverageElementSize
execute_on = 'initial timestep_end'
[../]
[./dofs]
type = NumDOFs
execute_on = 'initial timestep_end'
[../]
[./l2_err]
type = ElementL2Error
variable = u
function = exact_fn
execute_on = 'initial timestep_end'
[../]
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/meshgenerators/transform_generator/rotate_and_scale.i)
[Mesh]
[./fmg]
type = FileMeshGenerator
file = cylinder.e
[]
[./rotate]
type = TransformGenerator
input = fmg
transform = ROTATE
vector_value = '0 90 0'
[]
[./scale]
type = TransformGenerator
input = rotate
transform = SCALE
vector_value ='1e2 1e2 1e2'
[]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/materials/functor_properties/ad_conversion/1d_dirichlet.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 10
xmax = 2
[]
[Variables]
[v]
type = MooseVariableFVReal
[]
[]
[AuxVariables]
[sink]
type = MooseVariableFVReal
[]
[]
[ICs]
[sink]
type = FunctionIC
variable = sink
function = 'x^3'
[]
[]
[FVKernels]
[diff]
type = FVDiffusion
variable = v
coeff = 1
[]
[sink]
type = FVFunctorElementalKernel
variable = v
functor_name = 'ad_sink'
[]
[]
[FVBCs]
[bounds]
type = FVDirichletBC
variable = v
boundary = 'left right'
value = 0
[]
[]
[Materials]
[converter_to_regular]
type = FunctorADConverter
ad_props_in = 'sink'
reg_props_out = 'regular_sink_0'
[]
# Just to change the name
[functor]
type = GenericFunctorMaterial
prop_names = 'regular_sink_1'
prop_values = 'regular_sink_0'
[]
[converter_to_ad]
type = FunctorADConverter
reg_props_in = 'regular_sink_1'
ad_props_out = 'ad_sink'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/pins/mms/porosity_change/pressure-interpolation-corrected.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'
darcy=1.1
forch=1.1
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 2
ymin = -1
ymax = 1
nx = 2
ny = 2
[]
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
Darcy_name = 'Darcy_coefficient'
Forchheimer_name = 'Forchheimer_coefficient'
porosity = porosity
[]
[UserObjects]
[rc]
type = PINSFVRhieChowInterpolator
u = u
v = v
porosity = porosity
pressure = pressure
smoothing_layers = 2
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[Variables]
[u]
type = PINSFVSuperficialVelocityVariable
initial_condition = 1
[]
[v]
type = PINSFVSuperficialVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[AuxVariables]
[eps_out]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[eps_out]
type = ADFunctorElementalAux
variable = eps_out
functor = porosity
execute_on = 'timestep_end'
[]
[]
[FVKernels]
[mass]
type = PINSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[u_advection]
type = PINSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = PINSFVMomentumDiffusion
variable = u
mu = ${mu}
porosity = porosity
momentum_component = 'x'
[]
[u_pressure]
type = PINSFVMomentumPressure
variable = u
pressure = pressure
porosity = porosity
momentum_component = 'x'
[]
[u_drag]
type = PINSFVMomentumFriction
variable = u
momentum_component = 'x'
porosity = porosity
rho = ${rho}
[]
[u_correction]
type = PINSFVMomentumFrictionCorrection
variable = u
momentum_component = 'x'
porosity = porosity
rho = ${rho}
[]
[u_forcing]
type = INSFVBodyForce
variable = u
functor = forcing_u
momentum_component = 'x'
[]
[v_advection]
type = PINSFVMomentumAdvection
variable = v
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = PINSFVMomentumDiffusion
variable = v
mu = ${mu}
porosity = porosity
momentum_component = 'y'
[]
[v_pressure]
type = PINSFVMomentumPressure
variable = v
pressure = pressure
porosity = porosity
momentum_component = 'y'
[]
[v_drag]
type = PINSFVMomentumFriction
variable = v
momentum_component = 'y'
porosity = porosity
rho = ${rho}
[]
[v_correction]
type = PINSFVMomentumFrictionCorrection
variable = v
momentum_component = 'y'
porosity = porosity
rho = ${rho}
[]
[v_forcing]
type = INSFVBodyForce
variable = v
functor = forcing_v
momentum_component = 'y'
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = 'exact_u'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = 'exact_v'
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = u
function = 'exact_u'
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = v
function = 'exact_v'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 'exact_p'
[]
[]
[Materials]
[darcy]
type = ADGenericVectorFunctorMaterial
prop_names = 'Darcy_coefficient Forchheimer_coefficient'
prop_values = '${darcy} ${darcy} ${darcy} ${forch} ${forch} ${forch}'
[]
[]
[Functions]
[porosity]
type = ADParsedFunction
value = '.5 + .1 * sin(pi * x / 4) * cos(pi * y / 4)'
[]
[exact_u]
type = ParsedFunction
value = 'sin((1/2)*y*pi)*cos((1/2)*x*pi)'
[]
[forcing_u]
type = ADParsedFunction
value = '-mu*(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)*(-1/4*pi^2*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) + 0.025*pi^2*sin((1/4)*x*pi)*sin((1/4)*y*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2 + 0.00625*pi^2*sin((1/4)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*x*pi)*cos((1/4)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2 + 0.00125*pi^2*sin((1/4)*x*pi)^2*sin((1/4)*y*pi)^2*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^3) - mu*(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)*(-1/4*pi^2*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) + 0.00625*pi^2*sin((1/4)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*x*pi)*cos((1/4)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2 + 0.025*pi^2*sin((1/2)*x*pi)*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/4)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2 + 0.00125*pi^2*sin((1/2)*y*pi)*cos((1/4)*x*pi)^2*cos((1/2)*x*pi)*cos((1/4)*y*pi)^2/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^3) - 0.025*pi*mu*(-1/2*pi*sin((1/2)*x*pi)*sin((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) - 0.025*pi*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/4)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2)*cos((1/4)*x*pi)*cos((1/4)*y*pi) + 0.025*pi*mu*((1/2)*pi*cos((1/2)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) + 0.025*pi*sin((1/4)*x*pi)*sin((1/4)*y*pi)*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2)*sin((1/4)*x*pi)*sin((1/4)*y*pi) + rho*(darcy + forch)*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) - 1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) + (1/2)*pi*rho*sin((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)^2/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) - pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) + 0.025*pi*rho*sin((1/4)*x*pi)^2*sin((1/4)*y*pi)*sin((1/2)*y*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2 - 0.025*pi*rho*sin((1/2)*y*pi)^2*cos((1/4)*x*pi)*cos((1/2)*x*pi)^2*cos((1/4)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2 - 1/4*pi*(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)*sin((1/4)*x*pi)*sin((3/2)*y*pi)'
vars = 'mu rho darcy forch'
vals = '${mu} ${rho} ${darcy} ${forch}'
[]
[exact_v]
type = ParsedFunction
value = 'sin((1/4)*x*pi)*cos((1/2)*y*pi)'
[]
[forcing_v]
type = ADParsedFunction
value = '-mu*(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)*(-1/4*pi^2*sin((1/4)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) - 0.025*pi^2*sin((1/4)*x*pi)^2*sin((1/4)*y*pi)*sin((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2 + 0.00625*pi^2*sin((1/4)*x*pi)^2*cos((1/4)*y*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2 + 0.00125*pi^2*sin((1/4)*x*pi)^3*sin((1/4)*y*pi)^2*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^3) - mu*(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)*(-1/16*pi^2*sin((1/4)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) + 0.00625*pi^2*sin((1/4)*x*pi)^2*cos((1/4)*y*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2 - 0.0125*pi^2*cos((1/4)*x*pi)^2*cos((1/4)*y*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2 + 0.00125*pi^2*sin((1/4)*x*pi)*cos((1/4)*x*pi)^2*cos((1/4)*y*pi)^2*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^3) + 0.025*pi*mu*(-1/2*pi*sin((1/4)*x*pi)*sin((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) + 0.025*pi*sin((1/4)*x*pi)^2*sin((1/4)*y*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2)*sin((1/4)*x*pi)*sin((1/4)*y*pi) - 0.025*pi*mu*((1/4)*pi*cos((1/4)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) - 0.025*pi*sin((1/4)*x*pi)*cos((1/4)*x*pi)*cos((1/4)*y*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2)*cos((1/4)*x*pi)*cos((1/4)*y*pi) + rho*(darcy + forch)*sin((1/4)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) - pi*rho*sin((1/4)*x*pi)^2*sin((1/2)*y*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) - 1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) + (1/4)*pi*rho*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) + 0.025*pi*rho*sin((1/4)*x*pi)^3*sin((1/4)*y*pi)*cos((1/2)*y*pi)^2/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2 - 0.025*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/4)*y*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)^2 + (3/2)*pi*(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)*cos((1/4)*x*pi)*cos((3/2)*y*pi)'
vars = 'mu rho darcy forch'
vals = '${mu} ${rho} ${darcy} ${forch}'
[]
[exact_p]
type = ParsedFunction
value = 'sin((3/2)*y*pi)*cos((1/4)*x*pi)'
[]
[forcing_p]
type = ParsedFunction
value = '-1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi) - 1/2*pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = false
csv = true
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2v]
type = ElementL2Error
variable = v
function = exact_v
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2p]
type = ElementL2Error
variable = pressure
function = exact_p
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/multiapp-scalar-transport/scalar-transport.i)
diff=1e-3
advected_interp_method='average'
velocity_interp_method='rc'
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
active = 'rc'
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
a_u = ax
a_v = ay
[]
[rc_bad]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 10
ymin = -1
ymax = 1
nx = 100
ny = 20
[]
[]
[Variables]
[scalar]
type = INSFVScalarFieldVariable
[]
[]
[AuxVariables]
[ax]
type = MooseVariableFVReal
[]
[ay]
type = MooseVariableFVReal
[]
[u]
type = INSFVVelocityVariable
[]
[v]
type = INSFVVelocityVariable
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[FVKernels]
[scalar_advection]
type = INSFVScalarFieldAdvection
variable = scalar
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
[]
[scalar_diffusion]
type = FVDiffusion
coeff = ${diff}
variable = scalar
[]
[scalar_src]
type = FVBodyForce
variable = scalar
value = 0.1
[]
[]
[FVBCs]
[inlet_scalar]
type = FVDirichletBC
boundary = 'left'
variable = scalar
value = 1
[]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = 0
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 0
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/ad_rz_cone_no_parts_steady_nobcbc.i)
[GlobalParams]
integrate_p_by_parts = false
[]
[Mesh]
file = '2d_cone.msh'
[]
[Problem]
coord_type = RZ
[]
[AuxVariables]
[vel_x]
order = SECOND
[]
[vel_y]
order = SECOND
[]
[]
[AuxKernels]
[vel_x]
type = VectorVariableComponentAux
variable = vel_x
vector_variable = velocity
component = 'x'
[]
[vel_y]
type = VectorVariableComponentAux
variable = vel_y
vector_variable = velocity
component = 'y'
[]
[]
[Variables]
[./velocity]
order = SECOND
family = LAGRANGE_VEC
[../]
[./p]
[../]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[momentum_advection]
type = INSADMomentumAdvection
variable = velocity
[]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
[../]
[]
[BCs]
[p_corner]
type = DirichletBC
boundary = top_right
value = 0
variable = p
[]
[inlet]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom'
function_x = 0
function_y = 'inlet_func'
[../]
[wall]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'right'
function_x = 0
function_y = 0
[]
[axis]
type = ADVectorFunctionDirichletBC
variable = velocity
boundary = 'left'
set_y_comp = false
function_x = 0
[]
[outlet]
type = INSADMomentumNoBCBC
variable = velocity
pressure = p
boundary = 'top'
[]
[]
[Functions]
[./inlet_func]
type = ParsedFunction
value = '-4 * x^2 + 1'
[../]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[ins_mat]
type = INSADMaterial
velocity = velocity
pressure = p
[]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = 'bjacobi ilu 4'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
csv = true
console = true
[./out]
type = Exodus
[../]
[]
[Postprocessors]
[./flow_in]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'bottom'
execute_on = 'timestep_end'
[../]
[./flow_out]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'top'
execute_on = 'timestep_end'
[../]
[]
(test/tests/kernels/adv_diff_reaction/adv_diff_reaction_test.i)
[Mesh]
dim = 2
file = Mesh24.e
[]
[Variables]
active = 'phi'
[./phi]
order = SECOND
family = LAGRANGE
[../]
[]
[Kernels]
active = 'advection diffusion source'
[./advection]
type = Advection0
variable = phi
Au = 10.
Bu = -6.
Cu = 5.
Av = 10.
Bv = 8.
Cv = -1.
[../]
[./diffusion]
type = Diffusion0
variable = phi
Ak = 10.
Bk = 0.1
Ck = 0.1
[../]
[./source]
type = ForcingFunctionXYZ0
variable = phi
omega0 = 2.
A0 = 1.
B0 = 1.2
C0 = 0.8
Au = 10.
Bu = -6.
Cu = 5.
Av = 10.
Bv = 8.
Cv = -1.
Ak = 10.
Bk = 0.1
Ck = 0.1
[../]
[]
[BCs]
active = 'btm_sca rgt_sca top_sca lft_sca'
[./btm_sca]
type = DirichletBCfuncXYZ0
variable = phi
boundary = 1
omega0 = 2.
A0 = 1.
B0 = 1.2
C0 = 0.8
[../]
[./rgt_sca]
type = DirichletBCfuncXYZ0
variable = phi
boundary = 2
omega0 = 2.
A0 = 1.
B0 = 1.2
C0 = 0.8
[../]
[./top_sca]
type = DirichletBCfuncXYZ0
variable = phi
boundary = 3
omega0 = 2.
A0 = 1.
B0 = 1.2
C0 = 0.8
[../]
[./lft_sca]
type = DirichletBCfuncXYZ0
variable = phi
boundary = 4
omega0 = 2.
A0 = 1.
B0 = 1.2
C0 = 0.8
[../]
[]
[Executioner]
type = Steady
nl_rel_tol = 1.e-10
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_levels -pc_factor_mat_ordering_type'
petsc_options_value = 'ilu 20 rcm'
[]
[Outputs]
exodus = true
[]
(test/tests/controls/restrict_exec_flag/exec_flag_error.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
[]
[MultiApps]
[sub]
type = FullSolveMultiApp
positions = '0 0 0'
input_files = sub.i
[]
[]
[Controls]
[test]
type = TestControl
test_type = 'execflag_error'
[]
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_mortar_action/modular_gap_heat_transfer_mortar_displaced_radiation_conduction_action_lowerd_exists.i)
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
[file]
type = FileMeshGenerator
file = 2blk-gap.e
[]
[secondary]
type = LowerDBlockFromSidesetGenerator
sidesets = '101'
new_block_id = 10001
new_block_name = 'secondary_lower'
input = file
[]
[primary]
type = LowerDBlockFromSidesetGenerator
sidesets = '100'
new_block_id = 10000
new_block_name = 'primary_lower'
input = secondary
[]
allow_renumbering = false
[]
[Problem]
kernel_coverage_check = false
material_coverage_check = false
[]
[Variables]
[temp]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[disp_x]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[disp_y]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[]
[Materials]
[left]
type = ADHeatConductionMaterial
block = 1
thermal_conductivity = 0.01
specific_heat = 1
[]
[right]
type = ADHeatConductionMaterial
block = 2
thermal_conductivity = 0.005
specific_heat = 1
[]
[]
[Kernels]
[hc_displaced_block]
type = ADHeatConduction
variable = temp
use_displaced_mesh = true
block = '1'
[]
[hc_undisplaced_block]
type = ADHeatConduction
variable = temp
use_displaced_mesh = false
block = '2'
[]
[disp_x]
type = Diffusion
variable = disp_x
block = '1 2'
[]
[disp_y]
type = Diffusion
variable = disp_y
block = '1 2'
[]
[]
[MortarGapHeatTransfer]
[mortar_heat_transfer]
temperature = temp
primary_emissivity = 1.0
secondary_emissivity = 1.0
boundary = 100
use_displaced_mesh = true
gap_conductivity = 0.02
primary_boundary = 100
secondary_boundary = 101
# We already have mortar lower-dimensional domains and do not need the action
# to create them for us. It will reuse those and define variables and constraints on
# the existing appended meshes.
primary_subdomain = 'primary_lower'
secondary_subdomain = 'secondary_lower'
gap_flux_options = 'CONDUCTION RADIATION'
[]
[]
[BCs]
[left]
type = DirichletBC
variable = temp
boundary = 'left'
value = 100
[]
[right]
type = DirichletBC
variable = temp
boundary = 'right'
value = 0
[]
[left_disp_x]
type = DirichletBC
preset = false
variable = disp_x
boundary = 'left'
value = .1
[]
[right_disp_x]
type = DirichletBC
preset = false
variable = disp_x
boundary = 'right'
value = 0
[]
[bottom_disp_y]
type = DirichletBC
preset = false
variable = disp_y
boundary = 'bottom'
value = 0
[]
[]
[Preconditioning]
[fmp]
type = SMP
full = true
solve_type = 'NEWTON'
[]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-11
nl_abs_tol = 1.0e-10
[]
[VectorPostprocessors]
[NodalTemperature]
type = NodalValueSampler
sort_by = id
boundary = '100 101'
variable = 'temp'
[]
[]
[Outputs]
csv = true
[exodus]
type = Exodus
show = 'temp'
[]
[]
(test/tests/functions/solution_function/solution_function_exodus_interp_test.i)
[Mesh]
file = cubesource.e
# This test uses SolutionUserObject which doesn't work with DistributedMesh.
parallel_type = replicated
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
initial_condition = 0.0
[../]
[]
[AuxVariables]
[./nn]
order = FIRST
family = LAGRANGE
[../]
# [./ne]
# order = FIRST
# family = LAGRANGE
# [../]
[./en]
order = CONSTANT
family = MONOMIAL
[../]
# [./ee]
# order = CONSTANT
# family = MONOMIAL
# [../]
[]
[Functions]
[./sourcen]
type = SolutionFunction
solution = cube_soln
[../]
# [./sourcee]
# type = SolutionFunction
# file_type = exodusII
# mesh = cubesource.e
# variable = source_element
# [../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./nn]
type = FunctionAux
variable = nn
function = sourcen
[../]
# [./ne]
# type = FunctionAux
# variable = ne
# function = sourcee
# [../]
[./en]
type = FunctionAux
variable = en
function = sourcen
[../]
# [./ee]
# type = FunctionAux
# variable = ee
# function = sourcee
# [../]
[]
[BCs]
[./stuff]
type = DirichletBC
variable = u
boundary = '1 2'
value = 0.0
[../]
[]
[UserObjects]
[./cube_soln]
type = SolutionUserObject
mesh = cubesource.e
system_variables = source_nodal
[../]
[]
#[Executioner]
# type = Steady
# petsc_options = '-snes'
# l_max_its = 800
# nl_rel_tol = 1e-10
#[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
l_max_its = 800
nl_rel_tol = 1e-10
num_steps = 50
end_time = 5
dt = 0.5
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(test/tests/misc/check_error/dot_integrity_check.i)
# Test that coupling a time derivative of a variable (DotCouplingKernel) and using a Steady executioner
# errors out
[Mesh]
type = GeneratedMesh
dim = 2
[]
[Variables]
[./v]
[../]
[./u]
[../]
[]
[Kernels]
[./diff_v]
type = CoefDiffusion
variable = u
coef = 0.5
[../]
[./conv_v]
type = DotCouplingKernel
variable = v
v = u
[../]
[]
[Executioner]
type = Steady
[]
(modules/porous_flow/test/tests/poroperm/PermTensorFromVar02.i)
# Testing permeability calculated from scalar and tensor
# Trivial test, checking calculated permeability is correct
# when scalar is a FunctionAux.
# k = k_anisotropy * perm
[Mesh]
type = GeneratedMesh
dim = 1
nx = 3
xmin = 0
xmax = 3
[]
[GlobalParams]
block = 0
PorousFlowDictator = dictator
[]
[Variables]
[pp]
[InitialCondition]
type = ConstantIC
value = 0
[]
[]
[]
[Kernels]
[flux]
type = PorousFlowAdvectiveFlux
gravity = '0 0 0'
variable = pp
[]
[]
[BCs]
[ptop]
type = DirichletBC
variable = pp
boundary = right
value = 0
[]
[pbase]
type = DirichletBC
variable = pp
boundary = left
value = 1
[]
[]
[Functions]
[perm_fn]
type = ParsedFunction
value = '2*(x+1)'
[]
[]
[AuxVariables]
[perm_var]
order = CONSTANT
family = MONOMIAL
[]
[perm_x]
order = CONSTANT
family = MONOMIAL
[]
[perm_y]
order = CONSTANT
family = MONOMIAL
[]
[perm_z]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[perm_var]
type = FunctionAux
function = perm_fn
variable = perm_var
[]
[perm_x]
type = PorousFlowPropertyAux
property = permeability
variable = perm_x
row = 0
column = 0
[]
[perm_y]
type = PorousFlowPropertyAux
property = permeability
variable = perm_y
row = 1
column = 1
[]
[perm_z]
type = PorousFlowPropertyAux
property = permeability
variable = perm_z
row = 2
column = 2
[]
[]
[Postprocessors]
[perm_x_left]
type = PointValue
variable = perm_x
point = '0.5 0 0'
[]
[perm_y_left]
type = PointValue
variable = perm_y
point = '0.5 0 0'
[]
[perm_z_left]
type = PointValue
variable = perm_z
point = '0.5 0 0'
[]
[perm_x_right]
type = PointValue
variable = perm_x
point = '2.5 0 0'
[]
[perm_y_right]
type = PointValue
variable = perm_y
point = '2.5 0 0'
[]
[perm_z_right]
type = PointValue
variable = perm_z
point = '2.5 0 0'
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureVG
# unimportant in this fully-saturated test
m = 0.8
alpha = 1e-4
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
[]
[]
[]
[Materials]
[permeability]
type = PorousFlowPermeabilityTensorFromVar
k_anisotropy = '1 0 0 0 2 0 0 0 0.1'
perm = perm_var
[]
[temperature]
type = PorousFlowTemperature
[]
[massfrac]
type = PorousFlowMassFraction
[]
[eff_fluid_pressure]
type = PorousFlowEffectiveFluidPressure
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pp
capillary_pressure = pc
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[porosity]
type = PorousFlowPorosity
porosity_zero = 0.1
[]
[relperm]
type = PorousFlowRelativePermeabilityCorey
n = 0 # unimportant in this fully-saturated situation
phase = 0
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
[]
[]
[Executioner]
solve_type = Newton
type = Steady
l_tol = 1E-5
nl_abs_tol = 1E-3
nl_rel_tol = 1E-8
l_max_its = 200
nl_max_its = 400
petsc_options_iname = '-pc_type -pc_asm_overlap -sub_pc_type -ksp_type -ksp_gmres_restart'
petsc_options_value = ' asm 2 lu gmres 200'
[]
[Outputs]
csv = true
execute_on = 'timestep_end'
[]
(test/tests/transfers/multiapp_nearest_node_transfer/source_boundary_master.i)
[Mesh]
[drmg]
type = DistributedRectilinearMeshGenerator
dim = 2
nx = 30
ny = 30
xmax = 2
elem_type = QUAD4
partition = square
[]
[]
[Variables]
[u][]
[]
[AuxVariables]
[from_sub][]
[]
[Kernels]
[conduction]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 1
[]
[right]
type = DirichletBC
variable = u
boundary = 'right'
value = 10
[]
[]
[MultiApps]
[sub]
type = FullSolveMultiApp
app_type = MooseTestApp
input_files = 'source_boundary_sub.i'
positions = '-1.0 0.0 0.0
2. 0.0 0.0'
output_in_position = true
cli_args='BCs/right/value="1" BCs/right/value="10"'
[]
[]
[Transfers]
[source_boundary]
type = MultiAppNearestNodeTransfer
source_variable = u
from_multi_app = sub
variable = from_sub
source_boundary = 'right'
[]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-6
[]
[Outputs]
exodus = true
[]
(test/tests/kernels/vector_fe/lagrange_vec_1d.i)
# This example reproduces the libmesh vector_fe example 1 results
[Mesh]
type = GeneratedMesh
dim = 1
nx = 15
xmin = -1
elem_type = EDGE3
[]
[Variables]
[./u]
family = LAGRANGE_VEC
order = SECOND
[../]
[]
[Kernels]
[./diff]
type = VectorDiffusion
variable = u
[../]
[./body_force]
type = VectorBodyForce
variable = u
function_x = 'ffx'
[../]
[]
[BCs]
[./bnd]
type = VectorFunctionDirichletBC
variable = u
function_x = 'x_exact_sln'
boundary = 'left right'
[../]
[]
[Functions]
[./x_exact_sln]
type = ParsedFunction
value = 'cos(.5*pi*x)'
[../]
[./ffx]
type = ParsedFunction
value = '.25*pi*pi*cos(.5*pi*x)'
[../]
[]
[Preconditioning]
[./pre]
type = SMP
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/format/output_test_xdr.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
nz = 0
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
xdr = true
[]
(test/tests/markers/error_fraction_marker/error_fraction_marker_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
nz = 10
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
[]
[]
[Functions]
[solution]
type = ParsedFunction
value = (exp(x)-1)/(exp(1)-1)
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[conv]
type = Convection
variable = u
velocity = '1 0 0'
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Adaptivity]
[Indicators]
[error]
type = AnalyticalIndicator
variable = u
function = solution
[]
[]
[Markers]
[marker]
type = ErrorFractionMarker
coarsen = 0.1
indicator = error
refine = 0.3
[]
[]
[]
[Outputs]
exodus = true
[]
(test/tests/transfers/multiapp_conservative_transfer/sub_nearest_point.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0.01 # to make sure the meshes don't align
xmax = 0.49 # to make sure the meshes don't align
ymax = 1
nx = 10
ny = 10
[]
[block1]
input = gen
type = SubdomainBoundingBoxGenerator
block_id = 1
bottom_left = '0.2 0.2 0'
top_right = '0.3 0.8 0'
[]
[]
[Variables]
[sink]
family = MONOMIAL
order = CONSTANT
[]
[]
[Functions]
[sink_func]
type = ParsedFunction
value = '5e2*x*(0.5-x)+5e1'
[]
[]
[Kernels]
[reaction]
type = Reaction
variable = sink
[]
[coupledforce]
type = BodyForce
variable = sink
function = sink_func
[]
[]
[AuxVariables]
[from_master]
block = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Postprocessors]
[sink]
type = ElementIntegralVariablePostprocessor
block = 1
variable = sink
[]
[from_master_pp]
type = ElementIntegralVariablePostprocessor
block = 1
variable = from_master
execute_on = 'transfer'
[]
[]
[Outputs]
exodus = true
[console]
type = Console
execute_on = 'timestep_end timestep_begin'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/boussinesq/boussinesq.i)
mu = 1
rho = 1
k = 1
cp = 1
alpha = 1
velocity_interp_method = 'rc'
advected_interp_method = 'upwind'
rayleigh=1e3
hot_temp=${rayleigh}
temp_ref=${fparse hot_temp / 2.}
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 32
ny = 32
[]
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
[]
[vel_y]
type = INSFVVelocityVariable
[]
[pressure]
type = INSFVPressureVariable
[]
[T_fluid]
type = INSFVEnergyVariable
scaling = 1e-4
[]
[lambda]
family = SCALAR
order = FIRST
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[mean_zero_pressure]
type = FVScalarLagrangeMultiplier
variable = pressure
lambda = lambda
[]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
[]
[u_buoyancy]
type = INSFVMomentumBoussinesq
variable = vel_x
T_fluid = T_fluid
gravity = '0 -1 0'
rho = ${rho}
ref_temperature = ${temp_ref}
momentum_component = 'x'
[]
[u_gravity]
type = INSFVMomentumGravity
variable = vel_x
gravity = '0 -1 0'
rho = ${rho}
momentum_component = 'x'
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
[]
[v_buoyancy]
type = INSFVMomentumBoussinesq
variable = vel_y
T_fluid = T_fluid
gravity = '0 -1 0'
rho = ${rho}
ref_temperature = ${temp_ref}
momentum_component = 'y'
[]
[v_gravity]
type = INSFVMomentumGravity
variable = vel_y
gravity = '0 -1 0'
rho = ${rho}
momentum_component = 'y'
[]
[temp_conduction]
type = FVDiffusion
coeff = 'k'
variable = T_fluid
[]
[temp_advection]
type = INSFVEnergyAdvection
variable = T_fluid
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
[]
[]
[FVBCs]
[top_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'top'
function = 'lid_function'
[]
[no_slip_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'left right bottom'
function = 0
[]
[no_slip_y]
type = INSFVNoSlipWallBC
variable = vel_y
boundary = 'left right top bottom'
function = 0
[]
[T_hot]
type = FVDirichletBC
variable = T_fluid
boundary = left
value = ${hot_temp}
[]
[T_cold]
type = FVDirichletBC
variable = T_fluid
boundary = right
value = 0
[]
[]
[Materials]
[const_functor]
type = ADGenericFunctorMaterial
prop_names = 'alpha_b cp k'
prop_values = '${alpha} ${cp} ${k}'
[]
[ins_fv]
type = INSFVEnthalpyMaterial
temperature = 'T_fluid'
rho = ${rho}
[]
[]
[Functions]
[lid_function]
type = ParsedFunction
value = '4*x*(1-x)'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 300 lu NONZERO'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(test/tests/kernels/hfem/robin_displaced.i)
[Mesh]
[square]
type = CartesianMeshGenerator
dx = '0.3125 0.3125 0.3125'
dy = '0.3333333333333 0.3333333333333 0.3333333333333'
dim = 2
[]
displacements = 'x_disp y_disp'
build_all_side_lowerd_mesh = true
[]
[Variables]
[u]
order = THIRD
family = MONOMIAL
block = 0
components = 2
[]
[lambda]
order = CONSTANT
family = MONOMIAL
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
components = 2
[]
[]
[AuxVariables]
[v]
order = CONSTANT
family = MONOMIAL
block = 0
initial_condition = '1'
[]
[x_disp]
block = 0
[]
[y_disp]
block = 0
initial_condition = 0
[]
[]
[AuxKernels]
[x_disp]
type = ParsedAux
variable = x_disp
use_xyzt = true
function = 'x/15'
[]
[]
[Kernels]
[diff]
type = ArrayDiffusion
variable = u
block = 0
diffusion_coefficient = dc
use_displaced_mesh = true
[]
[source]
type = ArrayCoupledForce
variable = u
v = v
coef = '1 2'
block = 0
use_displaced_mesh = true
[]
[]
[DGKernels]
[surface]
type = ArrayHFEMDiffusion
variable = u
lowerd_variable = lambda
use_displaced_mesh = true
[]
[]
[BCs]
[all]
type = ArrayVacuumBC
boundary = 'left right top bottom'
variable = u
use_displaced_mesh = true
[]
[]
[Materials]
[dc]
type = GenericConstantArray
prop_name = dc
prop_value = '1 1'
[]
[]
[Postprocessors]
[intu]
type = ElementIntegralArrayVariablePostprocessor
variable = u
block = 0
use_displaced_mesh = true
[]
[lambdanorm]
type = ElementArrayL2Norm
variable = lambda
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
use_displaced_mesh = true
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu basic mumps'
[]
[Outputs]
[out]
# we hide lambda because it may flip sign due to element
# renumbering with distributed mesh
type = Exodus
hide = lambda
[]
csv = true
[]
(modules/level_set/test/tests/transfers/copy_solution/sub.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Executioner]
type = Steady
[]
[Problem]
kernel_coverage_check = false
[]
[Outputs]
exodus = true
[]
(test/tests/meshgenerators/sidesets_from_normals_generator/sidesets_cylinder_normals.i)
[Mesh]
[./fmg]
type = FileMeshGenerator
file = cylinder.e
#parallel_type = replicated
[]
[./sidesets]
type = SideSetsFromNormalsGenerator
input = fmg
normals = '0 0 1
0 1 0
0 0 -1'
fixed_normal = false
new_boundary = 'top side bottom'
[]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = u
boundary = bottom
value = 0
[../]
[./top]
type = DirichletBC
variable = u
boundary = top
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/tag/2d_diffusion_matrix_tag_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./tag_variable]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
extra_matrix_tags = 'mat_tag1 mat_tag2'
[../]
[./diff1]
type = Diffusion
variable = u
extra_matrix_tags = 'mat_tag2'
vector_tags = vec_tag1
[../]
[./diff2]
type = Diffusion
variable = u
vector_tags = vec_tag1
[../]
[./diff3]
type = Diffusion
variable = u
vector_tags = vec_tag1
[../]
[]
[AuxKernels]
[./TagMatrixAux]
type = TagMatrixAux
variable = tag_variable
v = u
matrix_tag = mat_tag2
execute_on = timestep_end
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
extra_matrix_tags = mat_tag1
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
extra_matrix_tags = mat_tag1
[../]
[]
[Problem]
type = TagTestProblem
test_tag_vectors = 'nontime residual'
test_tag_matrices = 'mat_tag1 mat_tag2'
extra_tag_matrices = 'mat_tag1 mat_tag2'
extra_tag_vectors = 'vec_tag1'
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
file_base = matrix_tag_test_out
exodus = true
[]
(test/tests/transfers/multiapp_conservative_transfer/primary_skipped_adjuster.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[AuxVariables]
[var]
family = MONOMIAL
order = THIRD
[]
[]
[ICs]
[var_ic]
type = FunctionIC
variable = var
function = '-exp(x * y)'
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[MultiApps]
[sub]
type = FullSolveMultiApp
input_files = secondary_negative_adjuster.i
execute_on = timestep_begin
[]
[]
[Postprocessors]
[from_postprocessor]
type = ElementIntegralVariablePostprocessor
variable = var
[]
[]
[Transfers]
[to_sub]
type = MultiAppMeshFunctionTransfer
source_variable = var
variable = var
to_multi_app = sub
from_postprocessors_to_be_preserved = 'from_postprocessor'
to_postprocessors_to_be_preserved = 'to_postprocessor'
allow_skipped_adjustment = true
[]
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/radiation_transfer_action/radiative_transfer_no_action.i)
[Problem]
kernel_coverage_check = false
[]
[Mesh]
type = MeshGeneratorMesh
[./cmg]
type = CartesianMeshGenerator
dim = 2
dx = '1 1.3 1.9'
ix = '3 3 3'
dy = '2 1.2 0.9'
iy = '3 3 3'
subdomain_id = '0 1 0
4 5 2
0 3 0'
[../]
[./inner_bottom]
type = SideSetsBetweenSubdomainsGenerator
input = cmg
primary_block = 1
paired_block = 5
new_boundary = 'inner_bottom'
[../]
[./inner_left]
type = SideSetsBetweenSubdomainsGenerator
input = inner_bottom
primary_block = 4
paired_block = 5
new_boundary = 'inner_left'
[../]
[./inner_right]
type = SideSetsBetweenSubdomainsGenerator
input = inner_left
primary_block = 2
paired_block = 5
new_boundary = 'inner_right'
[../]
[./inner_top]
type = SideSetsBetweenSubdomainsGenerator
input = inner_right
primary_block = 3
paired_block = 5
new_boundary = 'inner_top'
[../]
[./rename]
type = RenameBlockGenerator
old_block = '1 2 3 4'
new_block = '0 0 0 0'
input = inner_top
[../]
[./split_inner_bottom]
type = PatchSidesetGenerator
boundary = 4
n_patches = 2
partitioner = centroid
centroid_partitioner_direction = x
input = rename
[../]
[./split_inner_left]
type = PatchSidesetGenerator
boundary = 5
n_patches = 2
partitioner = centroid
centroid_partitioner_direction = y
input = split_inner_bottom
[../]
[./split_inner_right]
type = PatchSidesetGenerator
boundary = 6
n_patches = 2
partitioner = centroid
centroid_partitioner_direction = y
input = split_inner_left
[../]
[./split_inner_top]
type = PatchSidesetGenerator
boundary = 7
n_patches = 3
partitioner = centroid
centroid_partitioner_direction = x
input = split_inner_right
[../]
[]
[Variables]
[./temperature]
block = 0
[../]
[]
[Kernels]
[./heat_conduction]
type = HeatConduction
variable = temperature
block = 0
diffusion_coefficient = 5
[../]
[]
[UserObjects]
[./gray_lambert]
type = ViewFactorObjectSurfaceRadiation
boundary = 'inner_bottom_0 inner_bottom_1
inner_left_0 inner_left_1
inner_right_0 inner_right_1
inner_top_0 inner_top_1 inner_top_2'
fixed_temperature_boundary = 'inner_bottom_0 inner_bottom_1'
fixed_boundary_temperatures = '1200 1200'
adiabatic_boundary = 'inner_top_0 inner_top_1 inner_top_2'
emissivity = '0.9 0.9
0.8 0.8
0.4 0.4
1 1 1'
temperature = temperature
view_factor_object_name = view_factor
execute_on = 'LINEAR TIMESTEP_END'
[../]
[./view_factor]
type = UnobstructedPlanarViewFactor
boundary = 'inner_bottom_0 inner_bottom_1
inner_left_0 inner_left_1
inner_right_0 inner_right_1
inner_top_0 inner_top_1 inner_top_2'
normalize_view_factor = true
execute_on = 'INITIAL'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = temperature
boundary = left
value = 600
[../]
[./right]
type = DirichletBC
variable = temperature
boundary = right
value = 300
[../]
[./radiation]
type = GrayLambertNeumannBC
variable = temperature
surface_radiation_object_name = gray_lambert
boundary = 'inner_left_0 inner_left_1
inner_right_0 inner_right_1'
[../]
[]
[Postprocessors]
[./average_T_inner_right]
type = SideAverageValue
variable = temperature
boundary = inner_right
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/porous_flow/test/tests/fluids/simple_fluid.i)
# Test the properties calculated by the simple fluid Material
# Pressure 10 MPa
# Temperature = 300 K (temperature unit = K)
# Density should equal 1500*exp(1E7/1E9-2E-4*300)=1426.844 kg/m^3
# Viscosity should equal 1.1E-3 Pa.s
# Energy density should equal 4000 * 300 = 1.2E6 J/kg
# Specific enthalpy should equal 4000 * 300 + 10e6 / 1426.844 = 1.207008E6 J/kg
[Modules]
[FluidProperties]
[the_simple_fluid]
type = SimpleFluidProperties
thermal_expansion = 2.0E-4
cv = 4000.0
cp = 5000.0
bulk_modulus = 1.0E9
thermal_conductivity = 1.0
viscosity = 1.1E-3
density0 = 1500.0
[]
[]
[]
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp T'
number_fluid_phases = 1
number_fluid_components = 1
[]
[]
[Variables]
[pp]
initial_condition = 10e6
[]
[T]
initial_condition = 300.0
[]
[]
[Kernels]
[dummy_p]
type = Diffusion
variable = pp
[]
[dummy_T]
type = Diffusion
variable = T
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
temperature = T
[]
[ppss]
type = PorousFlow1PhaseFullySaturated
porepressure = pp
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
temperature_unit = Kelvin
fp = the_simple_fluid
phase = 0
[]
[]
[Postprocessors]
[pressure]
type = ElementIntegralVariablePostprocessor
variable = pp
[]
[temperature]
type = ElementIntegralVariablePostprocessor
variable = T
[]
[density]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_fluid_phase_density_qp0'
[]
[viscosity]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_viscosity_qp0'
[]
[internal_energy]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_fluid_phase_internal_energy_qp0'
[]
[enthalpy]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_fluid_phase_enthalpy_qp0'
[]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = simple_fluid
csv = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/rz_cone_no_parts_steady_nobcbc.i)
# This input file tests several different things:
# .) The axisymmetric (RZ) form of the governing equations.
# .) An open boundary.
# .) Not integrating the pressure by parts, thereby requiring a pressure pin.
# .) Natural boundary condition at the outlet.
[GlobalParams]
integrate_p_by_parts = false
laplace = true
gravity = '0 0 0'
[]
[Mesh]
file = '2d_cone.msh'
[]
[Problem]
coord_type = RZ
[]
[Preconditioning]
[./SMP_PJFNK]
type = SMP
full = true
solve_type = Newton
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = 'bjacobi ilu 4'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
csv = true
console = true
[./out]
type = Exodus
[../]
[]
[Variables]
[./vel_x]
# Velocity in radial (r) direction
family = LAGRANGE
order = SECOND
[../]
[./vel_y]
# Velocity in axial (z) direction
family = LAGRANGE
order = SECOND
[../]
[./p]
family = LAGRANGE
order = FIRST
[../]
[]
[BCs]
[./p_corner]
# This is required, because pressure term is *not* integrated by parts.
type = DirichletBC
boundary = top_right
value = 0
variable = p
[../]
[./u_in]
type = DirichletBC
boundary = bottom
variable = vel_x
value = 0
[../]
[./v_in]
type = FunctionDirichletBC
boundary = bottom
variable = vel_y
function = 'inlet_func'
[../]
[./u_axis_and_walls]
type = DirichletBC
boundary = 'left right'
variable = vel_x
value = 0
[../]
[./v_no_slip]
type = DirichletBC
boundary = 'right'
variable = vel_y
value = 0
[../]
[./u_out]
type = INSMomentumNoBCBCLaplaceForm
boundary = top
variable = vel_x
u = vel_x
v = vel_y
pressure = p
component = 0
[../]
[./v_out]
type = INSMomentumNoBCBCLaplaceForm
boundary = top
variable = vel_y
u = vel_x
v = vel_y
pressure = p
component = 1
[../]
[]
[Kernels]
[./mass]
type = INSMassRZ
variable = p
u = vel_x
v = vel_y
pressure = p
[../]
[./x_momentum_space]
type = INSMomentumLaplaceFormRZ
variable = vel_x
u = vel_x
v = vel_y
pressure = p
component = 0
[../]
[./y_momentum_space]
type = INSMomentumLaplaceFormRZ
variable = vel_y
u = vel_x
v = vel_y
pressure = p
component = 1
[../]
[]
[Materials]
[./const]
type = GenericConstantMaterial
block = 'volume'
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[]
[Functions]
[./inlet_func]
type = ParsedFunction
value = '-4 * x^2 + 1'
[../]
[]
[Postprocessors]
[./flow_in]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'bottom'
execute_on = 'timestep_end'
[../]
[./flow_out]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'top'
execute_on = 'timestep_end'
[../]
[]
(test/tests/misc/check_mesh_meta_data/check_mesh_meta_data_test.i)
[Mesh]
[square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[]
[normal]
type = AllSideSetsByNormalsGenerator
input = square
[]
[]
[Debug]
show_mesh_meta_data = true
[]
[CheckMeshMetaData]
mesh_generator_name = normal
mesh_meta_data_name = boundary_normals
[]
[Problem]
solve = false
kernel_coverage_check = false
[]
[Executioner]
type = Steady
[]
(test/tests/parser/active_inactive/active_inactive.i)
#############################################################
# This input file demonstrates the use of the active/inactive
# block level parameters that can be used to toggle individual
# blocks on/off for every block in a MOOSE-based input file.
#
# "active" and "inactive" cannot be used within the same block
##############################################################
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
active = 'u'
[./u]
[../]
[]
[AuxVariables]
inactive = 'aux1 aux3'
# The parameters in the inactive sections can be invalid because
# they are never parsed.
[./aux1]
type = DoesntExist
flintstones = 'fred wilma'
[../]
[./aux2]
[../]
[./aux3]
order = TENZILLION
[../]
[./aux4]
[../]
[]
[AuxKernels]
active = 'aux2 aux4'
# You can use active or inactive depending on whatever is easier
[./aux1]
type = ConstantAux
value = 1
variable = aux1
[../]
[./aux2]
type = ConstantAux
value = 2
variable = aux2
[../]
[./aux3]
type = ConstantAux
value = 3
variable = aux3
[../]
[./aux4]
type = ConstantAux
value = 4
variable = aux4
[../]
[]
[Kernels]
inactive = ''
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
inactive = ''
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
inactive = Adaptivity
[./Adaptivity]
[../]
[]
# No output so we can override several parameters and test them concurrently
(test/tests/userobjects/shape_element_user_object/shape_side_uo_jac_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
parallel_type = replicated
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[./pot]
[../]
[]
[Kernels]
[]
[BCs]
[./left_pot]
boundary = left
type = ExampleShapeSideIntegratedBC
variable = pot
num_user_object = num_user_object
denom_user_object = denom_user_object
v = u
Vb = 1
[../]
[]
[UserObjects]
[./num_user_object]
type = NumShapeSideUserObject
u = u
boundary = left
execute_on = 'linear nonlinear'
[../]
[./denom_user_object]
type = DenomShapeSideUserObject
u = u
boundary = left
execute_on = 'linear nonlinear'
[../]
[]
[Problem]
type = FEProblem
kernel_coverage_check = false
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
petsc_options = '-snes_test_display'
petsc_options_iname = '-snes_type'
petsc_options_value = 'test'
[]
[Outputs]
exodus = true
perf_graph = true
[]
[ICs]
[./u]
type = RandomIC
variable = u
[../]
[./pot]
type = RandomIC
variable = pot
[../]
[]
(test/tests/tag/tag_neumann.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 10
construct_side_list_from_node_list = true
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
extra_matrix_tags = 'mat_tag1 mat_tag2'
extra_vector_tags = 'vec_tag1'
[../]
[]
[AuxVariables]
[./tag_variable1]
order = FIRST
family = LAGRANGE
[../]
[./tag_variable2]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./TagVectorAux1]
type = TagVectorAux
variable = tag_variable1
v = u
vector_tag = vec_tag2
execute_on = timestep_end
[../]
[./TagVectorAux2]
type = TagMatrixAux
variable = tag_variable2
v = u
matrix_tag = mat_tag2
execute_on = timestep_end
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
extra_matrix_tags = 'mat_tag1 mat_tag2'
extra_vector_tags = 'vec_tag1'
[../]
[./right]
type = NeumannBC
variable = u
boundary = right
value = 2
extra_vector_tags = 'vec_tag1 vec_tag2'
[../]
[]
[Problem]
type = TagTestProblem
test_tag_vectors = 'nontime residual vec_tag1 vec_tag2'
test_tag_matrices = 'mat_tag1 mat_tag2'
extra_tag_matrices = 'mat_tag1 mat_tag2'
extra_tag_vectors = 'vec_tag1 vec_tag2'
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/missing_function_test.i)
# Test for usage of missing function
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = missing_function #should generate error
[../]
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/bcs/1d_neumann/from_cubit.i)
[Mesh]
file = 1d_line.e
construct_side_list_from_node_list = true
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = NeumannBC
variable = u
boundary = 2
value = 2
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/incomplete_kernel_variable_coverage_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[./v]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff body_force'
[./diff]
type = Diffusion
variable = u
[../]
[./body_force]
type = BodyForce
variable = u
value = 10
[../]
[]
[BCs]
active = 'right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/userobjects/nearest_point_layered_side_average/nearest_point_layered_side_average.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 40
ny = 10
nz = 10
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./np_layered_average]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./np_layered_average]
type = SpatialUserObjectAux
variable = np_layered_average
execute_on = timestep_end
user_object = npla
boundary = 'bottom top'
[../]
[]
[UserObjects]
[./npla]
type = NearestPointLayeredSideAverage
direction = x
points='0.25 0 0.25 0.75 0 0.25 0.25 0 0.75 0.75 0 0.75'
num_layers = 10
variable = u
execute_on = linear
boundary = 'bottom top'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./one]
type = DirichletBC
variable = u
boundary = 'right back top'
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/ray_tracing/test/tests/userobjects/ray_tracing_study/kernel_change_ray/kernel_change_ray.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 5
ny = 5
xmax = 5
ymax = 5
[]
[]
[Variables/phase]
[InitialCondition]
type = FunctionIC
variable = field
function = '(x > 2.99) * 1.0'
[]
[]
[RayBCs/kill]
type = KillRayBC
boundary = 'top right bottom left'
[]
[RayKernels/test]
type = RefractionRayKernelTest
field = phase
[]
[UserObjects/lots]
type = LotsOfRaysRayStudy
vertex_to_vertex = true
centroid_to_vertex = true
centroid_to_centroid = false
execute_on = initial
[]
[Postprocessors/total_distance]
type = RayTracingStudyResult
study = lots
result = total_distance
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Outputs]
exodus = false
csv = true
[]
(test/tests/geomsearch/2d_penetration_locator/2d_triangle.i)
[Mesh]
file = nonmatching_tri.e
dim = 2
construct_side_list_from_node_list = true
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./gap_distance]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = leftleft
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = rightright
value = 1
[../]
[]
[AuxKernels]
[./distance]
type = PenetrationAux
variable = gap_distance
boundary = leftright
paired_boundary = rightleft
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/indicators/analytical_indicator/analytical_indicator_fv.i)
[Mesh]
[mesh]
type = GeneratedMeshGenerator
dim = 2
nx = 20
ny = 1
[]
[]
[Variables]
[u]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[]
[Functions]
[solution]
type = ParsedFunction
value = (exp(x)-1)/(exp(1)-1)
[]
[]
[FVKernels]
[diff]
type = FVDiffusion
variable = u
coeff = coeff
[]
[conv]
type = FVAdvection
variable = u
velocity = '1 0 0'
[]
[]
[FVBCs]
[left]
type = FVDirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = FVDirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Materials]
[diff]
type = ADGenericFunctorMaterial
prop_names = 'coeff'
prop_values = '1'
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Adaptivity]
[Indicators]
[error]
type = AnalyticalIndicator
variable = u
function = solution
[]
[]
[]
[Outputs]
exodus = true
[]
(test/tests/mesh/adapt/initial_adaptivity_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 2
ny = 2
elem_type = QUAD9
[]
[Functions]
[./exact_fn]
type = ParsedFunction
value = x*x+y*y
[../]
[./ffn]
type = ParsedFunction
value = -4
[../]
[]
[Variables]
[./u]
order = SECOND
family = LAGRANGE
[./InitialCondition]
type = BoundingBoxIC
x1 = -2
y1 = -2
x2 = 0
y2 = 2
inside = 1
outside = 0
[../]
[../]
[]
[Kernels]
[./udiff]
type = Diffusion
variable = u
[../]
[./forcing_fn]
type = BodyForce
variable = u
function = ffn
[../]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
boundary = '0 1 2 3'
function = exact_fn
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[./Adaptivity]
initial_adaptivity = 5
refine_fraction = 0.2
coarsen_fraction = 0.3
max_h_level = 4
[../]
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/missing_mesh_test.i)
# Test for missing input mesh
[Mesh]
file = foo.e
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/userobjects/nearest_point_layered_integral/points_from_uo.i)
[Mesh]
type = GeneratedMesh
dim = 3
xmax = 1.5
ymax = 1.5
zmax = 1.2
nx = 10
ny = 10
nz = 10
[]
[Variables]
[u]
[]
[]
[AuxVariables]
[np_layered_integral]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[AuxKernels]
[np_layered_integral]
type = SpatialUserObjectAux
variable = np_layered_integral
execute_on = timestep_end
user_object = npla
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[one]
type = DirichletBC
variable = u
boundary = 'right back top'
value = 1
[]
[]
[UserObjects]
[npla]
type = NearestPointLayeredIntegral
direction = y
num_layers = 3
variable = u
points = '0.375 0.0 0.3
1.125 0.0 0.3
0.375 0.0 0.9
1.125 0.0 0.9'
[]
[]
[VectorPostprocessors]
# getting the points from the user object itself is here exactly equivalent to the points
# provided in the 'spatial_manually_provided' vector postprocessor
[spatial_from_uo]
type = SpatialUserObjectVectorPostprocessor
userobject = npla
[]
[spatial_manually_provided]
type = SpatialUserObjectVectorPostprocessor
userobject = npla
points = '0.375 0.25 0.3
0.375 0.75 0.3
0.375 1.25 0.3
1.125 0.25 0.3
1.125 0.75 0.3
1.125 1.25 0.3
0.375 0.25 0.9
0.375 0.75 0.9
0.375 1.25 0.9
1.125 0.25 0.9
1.125 0.75 0.9
1.125 1.25 0.9'
[]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
csv = true
execute_on = 'final'
[]
(test/tests/postprocessors/interface_diffusive_flux/interface_diffusive_flux.i)
postprocessor_type = InterfaceDiffusiveFluxAverage
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 6
xmax = 3
ny = 9
ymax = 3
elem_type = QUAD4
[]
[subdomain_id]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '0 0 0'
top_right = '2 1 0'
block_id = 1
[]
[interface]
input = subdomain_id
type = SideSetsBetweenSubdomainsGenerator
primary_block = '0'
paired_block = '1'
new_boundary = 'interface'
[]
[]
[Functions]
[fn_exact]
type = ParsedFunction
value = 'x*x+y*y'
[]
[]
[Variables]
[u]
block = 0
[]
[v]
block = 1
[]
[]
[Kernels]
[diff_u]
type = Diffusion
variable = u
[]
[body_u]
type = BodyForce
variable = u
function = 1
[]
[diff_v]
type = Diffusion
variable = v
[]
[body_v]
type = BodyForce
variable = v
function = -1
[]
[]
# Not a diffusion interface but can test the postprocessor anyway
[InterfaceKernels]
[reaction]
type = InterfaceReaction
kb = 1
kf = 2
variable = u
neighbor_var = v
boundary = 'interface'
[]
[]
[BCs]
[all]
type = FunctionDirichletBC
variable = u
boundary = '0 1 2 3'
function = fn_exact
[]
[]
[Postprocessors]
[diffusive_flux]
type = ${postprocessor_type}
variable = u
neighbor_variable = v
diffusivity = 1
execute_on = TIMESTEP_END
boundary = 'interface'
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
file_base = ${raw ${postprocessor_type} _fe}
exodus = true
[]
(test/tests/materials/material/material_check_test.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 4
ny = 4
[]
[./block_1]
input = gen
type = SubdomainBoundingBoxGenerator
top_right = '0.5 0.5 0'
bottom_left = '0 0 0'
block_id = 1
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./mat]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./mat]
type = MaterialRealAux
variable = mat
property = prop
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 3
[../]
[]
[Materials]
[./mat]
type = GenericConstantMaterial
block = 1
prop_names = prop
prop_values = 1
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
[]
[Outputs]
file_base = out
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[]
(test/tests/auxkernels/nodal_aux_var/nodal_aux_var_test.i)
###########################################################
# This is a simple test of the AuxKernel System.
# Several explicit calculations are being done
# using spatial variables.
# This simulation demonstrates coupling, and dependency
# resolution. For simplicity all AuxVariables in this
# simulation are constant.
#
# @Requirement F5.30
###########################################################
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
active = 'one five coupled'
[./one]
order = FIRST
family = LAGRANGE
[../]
[./five]
order = FIRST
family = LAGRANGE
[../]
[./coupled]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff force'
[./diff]
type = Diffusion
variable = u
[../]
#Coupling of nonlinear to Aux
[./force]
type = CoupledForce
variable = u
v = one
[../]
[]
# AuxKernel System
[AuxKernels]
#Simple Aux Kernel
[./constant]
variable = one
type = ConstantAux
value = 1
[../]
#Shows coupling of Aux to nonlinear
[./coupled]
variable = coupled
type = CoupledAux
value = 2
coupled = u
[../]
[./five]
type = ConstantAux
variable = five
boundary = '3 1'
value = 5
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_mortar/modular_gap_heat_transfer_mortar_displaced.i)
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
[file]
type = FileMeshGenerator
file = 2blk-gap.e
[]
[secondary]
type = LowerDBlockFromSidesetGenerator
sidesets = '101'
new_block_id = 10001
new_block_name = 'secondary_lower'
input = file
[]
[primary]
type = LowerDBlockFromSidesetGenerator
sidesets = '100'
new_block_id = 10000
new_block_name = 'primary_lower'
input = secondary
[]
[]
[Problem]
kernel_coverage_check = false
material_coverage_check = false
[]
[Variables]
[./temp]
order = FIRST
family = LAGRANGE
block = '1 2'
[../]
[./disp_x]
order = FIRST
family = LAGRANGE
block = '1 2'
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
block = '1 2'
[../]
[./lm]
order = FIRST
family = LAGRANGE
block = 'secondary_lower'
[../]
[]
[Materials]
[./left]
type = ADHeatConductionMaterial
block = 1
thermal_conductivity = 1000
specific_heat = 1
[../]
[./right]
type = ADHeatConductionMaterial
block = 2
thermal_conductivity = 500
specific_heat = 1
[../]
[]
[Kernels]
[./hc_displaced_block]
type = ADHeatConduction
variable = temp
use_displaced_mesh = true
block = '1'
[../]
[./hc_undisplaced_block]
type = ADHeatConduction
variable = temp
use_displaced_mesh = false
block = '2'
[../]
[disp_x]
type = Diffusion
variable = disp_x
block = '1 2'
[]
[disp_y]
type = Diffusion
variable = disp_y
block = '1 2'
[]
[]
[UserObjects]
[simple]
type = GapFluxModelSimple
k = 100
temperature = temp
boundary = 100
[]
[]
[Constraints]
[ced]
type = ModularGapConductanceConstraint
variable = lm
secondary_variable = temp
use_displaced_mesh = true
primary_boundary = 100
primary_subdomain = 10000
secondary_boundary = 101
secondary_subdomain = 10001
gap_flux_models = simple
[]
[]
[BCs]
[./left]
type = DirichletBC
variable = temp
boundary = 'left'
value = 1
[../]
[./right]
type = DirichletBC
variable = temp
boundary = 'right'
value = 0
[../]
[left_disp_x]
type = DirichletBC
preset = false
variable = disp_x
boundary = 'left'
value = .1
[]
[right_disp_x]
type = DirichletBC
preset = false
variable = disp_x
boundary = 'right'
value = 0
[]
[bottom_disp_y]
type = DirichletBC
preset = false
variable = disp_y
boundary = 'bottom'
value = 0
[]
[]
[Preconditioning]
[./fmp]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-11
[]
[Outputs]
exodus = true
show = 'temp disp_x disp_y'
[dof]
type = DOFMap
execute_on = 'initial'
[]
[]
(modules/functional_expansion_tools/test/tests/errors/invalid_bounds_length.i)
[Mesh]
type = GeneratedMesh
dim = 3
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diffusion]
type = Diffusion
variable = u
[../]
[]
[Functions]
[./series]
type = FunctionSeries
series_type = Cartesian
x = Legendre
orders = '0'
physical_bounds = '-1 1 0 3'
[../]
[]
[Executioner]
type = Steady
[]
(test/tests/misc/should_execute/should_execute.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/auxkernels/vector_variable_nodal/vector_variable_nodal.i)
[Mesh]
type = GeneratedMesh
dim = 3
xmin = -1
xmax = 1
ymin = -1
ymax = 1
zmin = -1
zmax = 1
nx = 2
ny = 2
nz = 2
[../]
[Variables]
[./u]
family = LAGRANGE_VEC
order = first
[../]
[]
[Kernels]
[./none]
type = VectorDiffusion
variable = u
[../]
[]
[BCs]
[./left]
type = VectorDirichletBC
variable = u
boundary = left
values = '0 0 0'
[../]
[./right]
type = VectorDirichletBC
variable = u
boundary = right
values = '1 2 3'
[../]
[]
[AuxVariables]
[./u_mag]
[../]
[]
[AuxKernels]
[./calc_u_mag]
type = VectorVariableMagnitudeAux
variable = u_mag # the auxvariable to compute
vector_variable = u # vector variable to compute from
execute_on = 'initial timestep_end'
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/uo_vector_pps_name_collision_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 5
ny = 5
elem_type = QUAD4
[]
[UserObjects]
[./ud]
type = MTUserObject
scalar = 2
vector = '9 7 5'
[../]
[]
[Functions]
[./forcing_fn]
type = ParsedFunction
value = -2
[../]
[./exact_fn]
type = ParsedFunction
value = x*x
[../]
[]
[Variables]
[./u]
family = LAGRANGE
order = FIRST
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./ffn]
type = UserObjectKernel
variable = u
user_object = ud
[]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
function = exact_fn
boundary = '0 1 2 3'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[VectorPostprocessors]
[./ud]
type = ConstantVectorPostprocessor
value = 1
[]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = out
exodus = true
[]
(test/tests/reporters/extra_id_integral/extra_id_integral.i)
[Mesh]
[fmg]
type = FileMeshGenerator
file = 'extra_id_integral.e'
use_for_exodus_restart = true
exodus_extra_element_integers = 'pin_id assembly_id'
[]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[AuxVariables]
[value1]
order = FIRST
initial_from_file_var = value1
[]
[value2]
order = FIRST
initial_from_file_var = value2
[]
[]
[Reporters]
[extra_id_integral]
type = ExtraIDIntegralReporter
variable = 'value1'
id_name = 'assembly_id'
[]
[]
[Outputs/out]
type = JSON
execute_on = FINAL
execute_system_information_on = NONE
[]
(modules/stochastic_tools/test/tests/surrogates/pod_rb/internal/sub.i)
[Problem]
type = FEProblem
extra_tag_vectors = 'diff react bodyf'
[]
[Mesh]
type = GeneratedMesh
dim = 1
nx = 15
xmax = 10
[]
[Variables]
[u]
[]
[]
[Kernels]
[diffusion]
type = MatDiffusion
variable = u
diffusivity = k
extra_vector_tags = 'diff'
[]
[reaction]
type = MaterialReaction
variable = u
coefficient = alpha
extra_vector_tags = 'react'
[]
[source]
type = BodyForce
variable = u
value = 1.0
extra_vector_tags = 'bodyf'
[]
[]
[Materials]
[k]
type = GenericConstantMaterial
prop_names = k
prop_values = 1.0
[]
[alpha]
type = GenericConstantMaterial
prop_names = alpha
prop_values = 1.0
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 0
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Controls]
[stochastic]
type = SamplerReceiver
[]
[]
[Outputs]
[]
(modules/navier_stokes/test/tests/finite_volume/pins/mms/1d-rc.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'
[Mesh]
[mesh]
type = CartesianMeshGenerator
dim = 1
dx = '1 1'
ix = '5 5'
subdomain_id = '1 2'
[]
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = PINSFVRhieChowInterpolator
u = u
pressure = pressure
porosity = porosity
[]
[]
[Variables]
[u]
type = PINSFVSuperficialVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[AuxVariables]
[porosity]
family = MONOMIAL
order = CONSTANT
fv = true
initial_condition = 0.8
[]
[]
[Problem]
error_on_jacobian_nonzero_reallocation = true
[]
[Functions]
[exact_u]
type = ParsedFunction
value = 'cos((1/2)*x*pi)'
[]
[forcing_u]
type = ADParsedFunction
value = '0.25*pi^2*mu*cos((1/2)*x*pi) - 1.25*pi*rho*sin((1/2)*x*pi)*cos((1/2)*x*pi) + 0.8*cos(x)'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_p]
type = ParsedFunction
value = 'sin(x)'
[]
[forcing_p]
type = ParsedFunction
value = '-1/2*pi*rho*sin((1/2)*x*pi)'
vars = 'rho'
vals = '${rho}'
[]
[]
[FVKernels]
[mass]
type = PINSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[u_advection]
type = PINSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
porosity = porosity
momentum_component = 'x'
[]
[u_viscosity]
type = PINSFVMomentumDiffusion
variable = u
mu = ${mu}
porosity = porosity
momentum_component = 'x'
[]
[u_pressure]
type = PINSFVMomentumPressureFlux
variable = u
pressure = pressure
porosity = porosity
momentum_component = 'x'
[]
[u_forcing]
type = INSFVBodyForce
variable = u
functor = forcing_u
momentum_component = 'x'
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = 'exact_u'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 'exact_p'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
[]
[Postprocessors]
[inlet_p]
type = SideAverageValue
variable = 'pressure'
boundary = 'left'
[]
[outlet-u]
type = SideIntegralVariablePostprocessor
variable = u
boundary = 'right'
[]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2p]
variable = pressure
function = exact_p
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
[Outputs]
exodus = true
csv = true
[]
(test/tests/misc/check_error/double_restrict_uo.i)
[Mesh]
file = sq-2blk.e
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
block = 1
[../]
[./v]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[BCs]
[./left_u]
type = DirichletBC
variable = u
boundary = 6
value = 0
[../]
[./right_u]
type = NeumannBC
variable = u
boundary = 8
value = 4
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = 6
value = 1
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = 3
value = 6
[../]
[]
[Postprocessors]
# This test demonstrates that you can have a block restricted NodalPostprocessor
[./restricted_max]
type = NodalExtremeValue
variable = v
block = 1 # Block restricted
boundary = 1 # Boundary restricted
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(examples/ex15_actions/ex15.i)
[Mesh]
file = square.e
uniform_refine = 4
[]
[Variables]
[./convected]
order = FIRST
family = LAGRANGE
[../]
[./diffused]
order = FIRST
family = LAGRANGE
[../]
[]
#This is our new custom Convection Diffusion "Meta" block
#that adds multiple kernels into our simulation
#Convection and Diffusion kernels on the first variable
#Diffusion kernel on the second variable
#The Convection kernel is coupled to the Diffusion kernel on the second variable
[ConvectionDiffusion]
variables = 'convected diffused'
[]
[BCs]
[./left_convected]
type = DirichletBC
variable = convected
boundary = 'left'
value = 0
[../]
[./right_convected]
type = DirichletBC
variable = convected
boundary = 'right'
value = 1
some_var = diffused
[../]
[./left_diffused]
type = DirichletBC
variable = diffused
boundary = 'left'
value = 0
[../]
[./right_diffused]
type = DirichletBC
variable = diffused
boundary = 'right'
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(examples/ex01_inputfile/diffusion_pathological.i)
[Mesh]
file = square.e
uniform_refine = 4
[]
# Note: This output block is out of its normal place (should be at the bottom)
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
# Note: The executioner is out of its normal place (should be just about the output block)
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Variables]
active = 'diffused' # Note the active list here
[./diffused]
order = FIRST
family = LAGRANGE
[../]
# This variable is not active in the list above
# therefore it is not used in the simulation
[./convected]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = diffused
[../]
[]
# This example applies DirichletBCs to all four sides of our square domain
[BCs]
[./left]
type = DirichletBC
variable = diffused
boundary = '1'
value = 0
[../]
[./right]
type = DirichletBC
variable = diffused
boundary = '2'
value = 1
[../]
[]
(test/tests/misc/check_error/coupling_itself.i)
[Mesh]
type = GeneratedMesh
dim = 2
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./coupled]
type = CoupledForce
variable = u
v = u
[../]
[]
[Executioner]
type = Steady
[]
(test/tests/materials/material/material_test.i)
###########################################################
# This is a simple test of the Material System. A
# user-defined Material (MTMaterial) is providing a
# Real property named "matp" that varies spatially
# throughout the domain. This property is used as a
# coefficient by MatDiffusionTest. It is also output
# by MaterialRealAux for visualization purposes.
#
# @Requirement F4.10
###########################################################
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 4
ny = 4
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./mat]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = MatDiffusionTest
variable = u
prop_name = matp
[../]
[]
[AuxKernels]
[./mat]
type = MaterialRealAux
variable = mat
property = matp
execute_on = timestep_end
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[./right]
type = MTBC
variable = u
boundary = 1
grad = 8
prop_name = matp
[../]
[]
# Materials System
[Materials]
[./mat]
type = MTMaterial
block = 0
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[]
(test/tests/mesh/face_info/face_info_two_region_quads.i)
[Mesh]
[./generated]
type = CartesianMeshGenerator
dim = 2
dx = '1 1'
dy = '1 1'
subdomain_id = '1 2 2 2'
[../]
[]
[Problem]
kernel_coverage_check = false
[]
[Variables]
[./u]
family = MONOMIAL
order = CONSTANT
block = 1
[../]
[./v]
family = MONOMIAL
order = CONSTANT
block = 2
[../]
[./w]
family = MONOMIAL
order = CONSTANT
[../]
[_trigger_fv_on]
fv = true
family = MONOMIAL
order = CONSTANT
[]
[]
[VectorPostprocessors]
[./face_info_1]
type = TestFaceInfo
vars = 'u'
[../]
[./face_info_2]
type = TestFaceInfo
vars = 'v'
[../]
[./face_info_3]
type = TestFaceInfo
vars = 'w'
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
[]
(modules/combined/examples/effective_properties/effective_th_cond.i)
# This example calculates the effective thermal conductivity across a microstructure
# with circular second phase precipitates. Two methods are used to calculate the effective thermal conductivity,
# the direct method that applies a temperature to one side and a heat flux to the other,
# and the AEH method.
[Mesh] #Sets mesh size to 10 microns by 10 microns
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 100
ny = 100
xmax = 10
ymax = 10
[]
[./new_nodeset]
input = gen
type = ExtraNodesetGenerator
coord = '5 5'
new_boundary = 100
[../]
[]
[Variables] #Adds variables needed for two ways of calculating effective thermal cond.
[./T] #Temperature used for the direct calculation
initial_condition = 800
[../]
[./Tx_AEH] #Temperature used for the x-component of the AEH solve
initial_condition = 800
scaling = 1.0e4 #Scales residual to improve convergence
[../]
[./Ty_AEH] #Temperature used for the y-component of the AEH solve
initial_condition = 800
scaling = 1.0e4 #Scales residual to improve convergence
[../]
[]
[AuxVariables] #Creates second constant phase
[./phase2]
[../]
[]
[ICs] #Sets the IC for the second constant phase
[./phase2_IC] #Creates circles with smooth interfaces at random locations
variable = phase2
type = MultiSmoothCircleIC
int_width = 0.3
numbub = 20
bubspac = 1.5
radius = 0.5
outvalue = 0
invalue = 1
block = 0
[../]
[]
[Kernels]
[./HtCond] #Kernel for direct calculation of thermal cond
type = HeatConduction
variable = T
[../]
[./heat_x] #All other kernels are for AEH approach to calculate thermal cond.
type = HeatConduction
variable = Tx_AEH
[../]
[./heat_rhs_x]
type = HomogenizedHeatConduction
variable = Tx_AEH
component = 0
[../]
[./heat_y]
type = HeatConduction
variable = Ty_AEH
[../]
[./heat_rhs_y]
type = HomogenizedHeatConduction
variable = Ty_AEH
component = 1
[../]
[]
[BCs]
[./Periodic]
[./all]
auto_direction = 'x y'
variable = 'Tx_AEH Ty_AEH'
[../]
[../]
[./left_T] #Fix temperature on the left side
type = DirichletBC
variable = T
boundary = left
value = 800
[../]
[./right_flux] #Set heat flux on the right side
type = NeumannBC
variable = T
boundary = right
value = 5e-6
[../]
[./fix_x] #Fix Tx_AEH at a single point
type = DirichletBC
variable = Tx_AEH
value = 800
boundary = 100
[../]
[./fix_y] #Fix Ty_AEH at a single point
type = DirichletBC
variable = Ty_AEH
value = 800
boundary = 100
[../]
[]
[Materials]
[./thcond] #The equation defining the thermal conductivity is defined here, using two ifs
# The k in the bulk is k_b, in the precipitate k_p2, and across the interaface k_int
type = ParsedMaterial
block = 0
constant_names = 'length_scale k_b k_p2 k_int'
constant_expressions = '1e-6 5 1 0.1'
function = 'sk_b:= length_scale*k_b; sk_p2:= length_scale*k_p2; sk_int:= k_int*length_scale; if(phase2>0.1,if(phase2>0.95,sk_p2,sk_int),sk_b)'
outputs = exodus
f_name = thermal_conductivity
args = phase2
[../]
[]
[Postprocessors]
[./right_T]
type = SideAverageValue
variable = T
boundary = right
[../]
[./k_x_direct] #Effective thermal conductivity from direct method
# This value is lower than the AEH value because it is impacted by second phase
# on the right boundary
type = ThermalConductivity
variable = T
flux = 5e-6
length_scale = 1e-06
T_hot = 800
dx = 10
boundary = right
[../]
[./k_x_AEH] #Effective thermal conductivity in x-direction from AEH
type = HomogenizedThermalConductivity
variable = Tx_AEH
temp_x = Tx_AEH
temp_y = Ty_AEH
component = 0
scale_factor = 1e6 #Scale due to length scale of problem
[../]
[./k_y_AEH] #Effective thermal conductivity in x-direction from AEH
type = HomogenizedThermalConductivity
variable = Ty_AEH
temp_x = Tx_AEH
temp_y = Ty_AEH
component = 1
scale_factor = 1e6 #Scale due to length scale of problem
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
off_diag_row = 'Tx_AEH Ty_AEH'
off_diag_column = 'Ty_AEH Tx_AEH'
[../]
[]
[Executioner]
type = Steady
l_max_its = 15
solve_type = NEWTON
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart -pc_hypre_boomeramg_strong_threshold'
petsc_options_value = 'hypre boomeramg 31 0.7'
l_tol = 1e-04
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
csv = true
[]
(test/tests/variables/coupled_scalar/coupled_scalar_from_ic.i)
# This makes sure that aux kernels using coupled scalar variables that are
# executed on initial will use the initial condition set on the scalar variable
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[AuxVariables]
[./aux_scalar]
order = FIRST
family = SCALAR
[../]
[./coupled]
[../]
[]
[ICs]
[./aux_scalar_ic]
type = ScalarConstantIC
variable = aux_scalar
value = 123
[../]
[]
[AuxKernels]
[./coupled]
type = CoupledScalarAux
variable = coupled
coupled = aux_scalar
execute_on = 'initial linear'
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 1
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/test_harness/jsondiff.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Reporters]
[test]
type = TestDeclareReporter
[]
[]
[Outputs]
json = true
[]
(test/tests/postprocessors/num_vars/num_vars.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 10
ny = 10
elem_type = QUAD9
[]
[Functions]
[./forcing_fnu]
type = ParsedFunction
value = -6*(x+y)+x*x+y*y
[../]
[./forcing_fnv]
type = ParsedFunction
value = -4+x*x*x-x+y*y*y-y
[../]
[./bc_fnut]
type = ParsedFunction
value = 3*y*y-1
[../]
[./bc_fnub]
type = ParsedFunction
value = -3*y*y+1
[../]
[./bc_fnul]
type = ParsedFunction
value = -3*x*x+1
[../]
[./bc_fnur]
type = ParsedFunction
value = 3*x*x-1
[../]
[./slnu]
type = ParsedGradFunction
value = x*x*x-x+y*y*y-y
grad_x = 3*x*x-1
grad_y = 3*y*y-1
[../]
[./slnv]
type = ParsedGradFunction
value = x*x+y*y
grad_x = 2*x
grad_y = 2*y
[../]
[]
[Variables]
[./u]
order = THIRD
family = HIERARCHIC
[../]
[./v]
order = SECOND
family = LAGRANGE
[../]
[]
[Kernels]
[./diff1]
type = Diffusion
variable = u
[../]
[./diff2]
type = Diffusion
variable = v
[../]
[./forceu]
type = BodyForce
variable = u
function = forcing_fnu
[../]
[./forcev]
type = BodyForce
variable = v
function = forcing_fnv
[../]
[]
[BCs]
# active = 'bc_u bc_v'
# [./bc_u]
# type = FunctionDirichletBC
# variable = u
# function = slnu
# boundary = 'top left right bottom'
# [../]
[./bc_ut]
type = FunctionDirichletBC
variable = u
boundary = top
function = bc_fnut
[../]
[./bc_ub]
type = FunctionDirichletBC
variable = u
boundary = bottom
function = bc_fnub
[../]
[./bc_ul]
type = FunctionDirichletBC
variable = u
boundary = left
function = bc_fnul
[../]
[./bc_ur]
type = FunctionDirichletBC
variable = u
boundary = right
function = bc_fnur
[../]
[./bc_v]
type = FunctionDirichletBC
variable = v
function = slnv
boundary = 'top left right bottom'
[../]
[]
[Preconditioning]
[./prec]
type = SMP
full = true
[../]
[]
[Postprocessors]
active = 'num_vars'
[./dofs]
type = NumDOFs
[../]
[./h]
type = AverageElementSize
[../]
[./L2u]
type = ElementL2Error
variable = u
function = slnu
[../]
[./L2v]
type = ElementL2Error
variable = v
function = slnv
[../]
[./H1error]
type = ElementH1Error
variable = u
function = solution
[../]
[./H1Semierror]
type = ElementH1SemiError
variable = u
function = solution
[../]
[./num_vars]
type = NumVars
system = 'NL'
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
nl_rel_tol = 1e-15
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
csv = true
[]
(modules/phase_field/test/tests/initial_conditions/RampIC.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 30
xmax = 13
xmin = -5
elem_type = EDGE
[]
[Variables]
[./c]
order = FIRST
family = LAGRANGE
scaling = 1e1
[./InitialCondition]
type = RampIC
variable = c
value_left = -0.2
value_right = 1.3
[../]
[../]
[]
[Problem]
type = FEProblem
solve = false
kernel_coverage_check = false
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(test/tests/kernels/hfem/variable_robin.i)
[Mesh]
[square]
type = GeneratedMeshGenerator
nx = 3
ny = 3
dim = 2
[]
build_all_side_lowerd_mesh = true
[]
[Variables]
[u]
order = THIRD
family = MONOMIAL
block = 0
components = 2
[]
[uhat]
order = CONSTANT
family = MONOMIAL
block = BOUNDARY_SIDE_LOWERD_SUBDOMAIN
components = 2
[]
[lambda]
order = CONSTANT
family = MONOMIAL
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
components = 2
[]
[lambdab]
order = CONSTANT
family = MONOMIAL
block = BOUNDARY_SIDE_LOWERD_SUBDOMAIN
components = 2
[]
[]
[AuxVariables]
[v]
order = CONSTANT
family = MONOMIAL
block = 0
initial_condition = '1'
[]
[]
[Kernels]
[diff]
type = ArrayDiffusion
variable = u
block = 0
diffusion_coefficient = dc
[]
[source]
type = ArrayCoupledForce
variable = u
v = v
coef = '1 2'
block = 0
[]
[uhat_reaction]
type = ArrayReaction
variable = uhat
block = BOUNDARY_SIDE_LOWERD_SUBDOMAIN
reaction_coefficient = rc
[]
[uhat_coupled]
type = ArrayCoupledForce
variable = uhat
block = BOUNDARY_SIDE_LOWERD_SUBDOMAIN
v = lambdab
is_v_array = true
coef = '1 1'
[]
[]
[DGKernels]
[surface]
type = ArrayHFEMDiffusion
variable = u
lowerd_variable = lambda
[]
[]
[BCs]
[all]
type = ArrayHFEMDirichletBC
boundary = 'left right top bottom'
variable = u
lowerd_variable = lambdab
uhat = uhat
[]
[]
[Materials]
[dc]
type = GenericConstantArray
prop_name = dc
prop_value = '1 1'
[]
[rc]
type = GenericConstantArray
block = BOUNDARY_SIDE_LOWERD_SUBDOMAIN
prop_name = rc
prop_value = '0.5 0.5'
[]
[]
[Postprocessors]
[intu]
type = ElementIntegralArrayVariablePostprocessor
variable = u
block = 0
[]
[lambdanorm]
type = ElementArrayL2Norm
variable = lambda
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu basic mumps'
[]
[Outputs]
[out]
# we hide lambda because it may flip sign due to element
# renumbering with distributed mesh
type = Exodus
hide = lambda
[]
csv = true
[]
(test/tests/misc/no_exodiff_map/no_exodiff_map.i)
[Mesh]
type = FileMesh
file = double_square.e
parallel_type = replicated
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left1]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[./right1]
type = DirichletBC
variable = u
boundary = 2
value = 2
[../]
[./left2]
type = DirichletBC
variable = u
boundary = 3
value = 3
[../]
[./right2]
type = DirichletBC
variable = u
boundary = 4
value = 4
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/fviks/continuity/test.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 20
xmax = 2
[]
[subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '1.0 0 0'
block_id = 1
top_right = '2.0 1.0 0'
[]
[interface_primary_side]
input = subdomain1
type = SideSetsBetweenSubdomainsGenerator
primary_block = '0'
paired_block = '1'
new_boundary = 'primary_interface'
[]
[]
[GlobalParams]
# retain behavior at time of test creation
two_term_boundary_expansion = false
[]
[Variables]
[u]
type = MooseVariableFVReal
block = 0
initial_condition = 0.5
[]
[v]
type = MooseVariableFVReal
block = 1
initial_condition = 0.5
[]
[lambda]
type = MooseVariableScalar
[]
[]
[Problem]
kernel_coverage_check = false
[]
[FVKernels]
[diff_left]
type = FVDiffusion
variable = u
coeff = 'left'
block = 0
[]
[diff_right]
type = FVDiffusion
variable = v
coeff = 'right'
block = 1
[]
[]
[FVInterfaceKernels]
[interface]
type = FVTwoVarContinuityConstraint
variable1 = u
variable2 = v
boundary = 'primary_interface'
subdomain1 = '0'
subdomain2 = '1'
lambda = 'lambda'
[]
[]
[FVBCs]
[left]
type = FVDirichletBC
variable = u
boundary = 'left'
value = 1
[]
[v_left]
type = FVDirichletBC
variable = v
boundary = 'right'
value = 0
[]
[]
[Materials]
[block0]
type = ADGenericFunctorMaterial
block = '0'
prop_names = 'left'
prop_values = '1'
[]
[block1]
type = ADGenericFunctorMaterial
block = '1'
prop_names = 'right'
prop_values = '1'
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm lu NONZERO'
[]
[Outputs]
exodus = true
[]
(test/tests/fvkernels/mms/advective-outflow/limited-advection.i)
a=1.1
[Mesh]
[./gen_mesh]
type = GeneratedMeshGenerator
dim = 1
xmin = 0.1
xmax = 1.1
nx = 2
[../]
[]
[ICs]
[u]
type = FunctionIC
variable = u
function = exact
[]
[]
[Variables]
[./u]
two_term_boundary_expansion = true
type = MooseVariableFVReal
[../]
[]
[FVKernels]
[./advection_u]
type = FVLimitedAdvection
variable = u
velocity = '${a} 0 0'
boundaries_to_force = 'right'
limiter = 'vanLeer'
[../]
[body_u]
type = FVBodyForce
variable = u
function = 'forcing'
[]
[]
[FVBCs]
[left_u]
type = FVFunctionNeumannBC
boundary = 'left'
function = 'advection'
variable = u
[]
[]
[Functions]
[exact]
type = ParsedFunction
value = 'cos(x)'
[]
[advection]
type = ParsedFunction
value = '${a} * cos(x)'
[]
[forcing]
type = ParsedFunction
value = '-${a} * sin(x)'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
nl_abs_tol = 1e-13
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[./L2u]
type = ElementL2Error
variable = u
function = exact
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/rz_cone_no_parts_steady_stabilized_second_order.i)
# This input file tests several different things:
# .) The axisymmetric (RZ) form of the governing equations.
# .) An open boundary.
# .) Not integrating the pressure by parts, thereby requiring a pressure pin.
# .) Natural boundary condition at the outlet.
[GlobalParams]
integrate_p_by_parts = false
laplace = true
gravity = '0 0 0'
supg = true
pspg = true
order = SECOND
[]
[Mesh]
file = '2d_cone.msh'
[]
[Problem]
coord_type = RZ
[]
[Preconditioning]
[./SMP_PJFNK]
type = SMP
full = true
solve_type = Newton
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = 'bjacobi ilu 4'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
csv = true
console = true
[./out]
type = Exodus
[../]
[]
[Variables]
[./vel_x]
# Velocity in radial (r) direction
[../]
[./vel_y]
# Velocity in axial (z) direction
[../]
[./p]
order = FIRST
[../]
[]
[BCs]
[./p_corner]
# This is required, because pressure term is *not* integrated by parts.
type = DirichletBC
boundary = top_right
value = 0
variable = p
[../]
[./u_in]
type = DirichletBC
boundary = bottom
variable = vel_x
value = 0
[../]
[./v_in]
type = FunctionDirichletBC
boundary = bottom
variable = vel_y
function = 'inlet_func'
[../]
[./u_axis_and_walls]
type = DirichletBC
boundary = 'left right'
variable = vel_x
value = 0
[../]
[./v_no_slip]
type = DirichletBC
boundary = 'right'
variable = vel_y
value = 0
[../]
[]
[Kernels]
[./mass]
type = INSMassRZ
variable = p
u = vel_x
v = vel_y
pressure = p
[../]
[./x_momentum_space]
type = INSMomentumLaplaceFormRZ
variable = vel_x
u = vel_x
v = vel_y
pressure = p
component = 0
[../]
[./y_momentum_space]
type = INSMomentumLaplaceFormRZ
variable = vel_y
u = vel_x
v = vel_y
pressure = p
component = 1
[../]
[]
[Materials]
[./const]
type = GenericConstantMaterial
block = 'volume'
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[]
[Functions]
[./inlet_func]
type = ParsedFunction
value = '-4 * x^2 + 1'
[../]
[]
[Postprocessors]
[./flow_in]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'bottom'
execute_on = 'timestep_end'
[../]
[./flow_out]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'top'
execute_on = 'timestep_end'
[../]
[]
(test/tests/materials/interface_material/interface_value_material_split_mesh.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 2
xmax = 2
ny = 2
ymax = 2
elem_type = QUAD4
[]
[./subdomain_id]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '1 0 0'
top_right = '2 2 0'
block_id = 1
[../]
[./split]
type = BreakMeshByBlockGenerator
input = subdomain_id
[../]
[]
[Variables]
[./u]
block = 0
[../]
[./v]
block = 1
[../]
[]
[Kernels]
[./diff]
type = MatDiffusion
variable = u
diffusivity = 'diffusivity'
block = 0
[../]
[./diff_v]
type = MatDiffusion
variable = v
diffusivity = 'diffusivity'
block = 1
[../]
[]
[InterfaceKernels]
[tied]
type = PenaltyInterfaceDiffusion
variable = u
neighbor_var = v
jump_prop_name = "average_jump"
penalty = 1e6
boundary = 'interface'
[]
[]
[BCs]
[u_left]
type = DirichletBC
boundary = 'left'
variable = u
value = 1
[]
[v_right]
type = DirichletBC
boundary = 'right'
variable = v
value = 0
[]
[]
[Materials]
[./stateful1]
type = StatefulMaterial
block = 0
initial_diffusivity = 1
# outputs = all
[../]
[./stateful2]
type = StatefulMaterial
block = 1
initial_diffusivity = 2
# outputs = all
[../]
[./interface_material_avg]
type = InterfaceValueMaterial
mat_prop_primary = diffusivity
mat_prop_secondary = diffusivity
var_primary = diffusivity_var
var_secondary = diffusivity_var
mat_prop_out_basename = diff
boundary = interface
interface_value_type = average
mat_prop_var_out_basename = diff_var
nl_var_primary = u
nl_var_secondary = v
[../]
[./interface_material_jump_primary_minus_secondary]
type = InterfaceValueMaterial
mat_prop_primary = diffusivity
mat_prop_secondary = diffusivity
var_primary = diffusivity_var
var_secondary = diffusivity_var
mat_prop_out_basename = diff
boundary = interface
interface_value_type = jump_primary_minus_secondary
mat_prop_var_out_basename = diff_var
nl_var_primary = u
nl_var_secondary = v
[../]
[./interface_material_jump_secondary_minus_primary]
type = InterfaceValueMaterial
mat_prop_primary = diffusivity
mat_prop_secondary = diffusivity
var_primary = diffusivity_var
var_secondary = diffusivity_var
mat_prop_out_basename = diff
boundary = interface
interface_value_type = jump_secondary_minus_primary
mat_prop_var_out_basename = diff_var
nl_var_primary = u
nl_var_secondary = v
[../]
[./interface_material_jump_abs]
type = InterfaceValueMaterial
mat_prop_primary = diffusivity
mat_prop_secondary = diffusivity
var_primary = diffusivity_var
var_secondary = diffusivity_var
mat_prop_out_basename = diff
boundary = interface
interface_value_type = jump_abs
mat_prop_var_out_basename = diff_var
nl_var_primary = u
nl_var_secondary = v
[../]
[./interface_material_primary]
type = InterfaceValueMaterial
mat_prop_primary = diffusivity
mat_prop_secondary = diffusivity
var_primary = diffusivity_var
var_secondary = diffusivity_var
mat_prop_out_basename = diff
boundary = interface
interface_value_type = primary
mat_prop_var_out_basename = diff_var
nl_var_primary = u
nl_var_secondary = v
[../]
[./interface_material_secondary]
type = InterfaceValueMaterial
mat_prop_primary = diffusivity
mat_prop_secondary = diffusivity
var_primary = diffusivity_var
var_secondary = diffusivity_var
mat_prop_out_basename = diff
mat_prop_var_out_basename = diff_var
boundary = interface
interface_value_type = secondary
nl_var_primary = u
nl_var_secondary = v
[../]
[]
[AuxKernels]
[./interface_material_avg]
type = MaterialRealAux
property = diff_average
variable = diffusivity_average
boundary = interface
[]
[./interface_material_jump_primary_minus_secondary]
type = MaterialRealAux
property = diff_jump_primary_minus_secondary
variable = diffusivity_jump_primary_minus_secondary
boundary = interface
[]
[./interface_material_jump_secondary_minus_primary]
type = MaterialRealAux
property = diff_jump_secondary_minus_primary
variable = diffusivity_jump_secondary_minus_primary
boundary = interface
[]
[./interface_material_jump_abs]
type = MaterialRealAux
property = diff_jump_abs
variable = diffusivity_jump_abs
boundary = interface
[]
[./interface_material_primary]
type = MaterialRealAux
property = diff_primary
variable = diffusivity_primary
boundary = interface
[]
[./interface_material_secondary]
type = MaterialRealAux
property = diff_secondary
variable = diffusivity_secondary
boundary = interface
[]
[diffusivity_var]
type = MaterialRealAux
property = diffusivity
variable = diffusivity_var
[]
[]
[AuxVariables]
[diffusivity_var]
family = MONOMIAL
order = CONSTANT
[]
[./diffusivity_average]
family = MONOMIAL
order = CONSTANT
[]
[./diffusivity_jump_primary_minus_secondary]
family = MONOMIAL
order = CONSTANT
[]
[./diffusivity_jump_secondary_minus_primary]
family = MONOMIAL
order = CONSTANT
[]
[./diffusivity_jump_abs]
family = MONOMIAL
order = CONSTANT
[]
[./diffusivity_primary]
family = MONOMIAL
order = CONSTANT
[]
[./diffusivity_secondary]
family = MONOMIAL
order = CONSTANT
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/linear_interp_not_increasing.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
nz = 0
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[]
[Materials]
[./linear_interp]
type = LinearInterpolationMaterial
prop_name = 'diffusivity'
independent_vals = '0 0.2 0.2 0.4 0.6 0.8 1.0'
dependent_vals = '16 8 4 2 1 0.5 1'
# Note the following line gets enabled by the tester
#use_poly_fit = true
block = 0
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
gmv = true
[]
(modules/fluid_properties/test/tests/brine/brine_tabulated.i)
# Test BrineFluidProperties calculations of density, viscosity and thermal
# conductivity with a TabulatedFluidProperties water.
#
# Experimental density values from Pitzer et al, "Thermodynamic properties
# of aqueous sodium chloride solution", Journal of Physical and Chemical
# Reference Data, 13, 1-102 (1984)
#
# Experimental viscosity values from Phillips et al, "Viscosity of NaCl and
# other solutions up to 350C and 50MPa pressures", LBL-11586 (1980)
#
# Thermal conductivity values from Ozbek and Phillips, "Thermal conductivity of
# aqueous NaCl solutions from 20C to 330C", LBL-9086 (1980)
#
# --------------------------------------------------------------
# Pressure (Mpa) | 20 | 20 | 40
# Temperature (C) | 50 | 200 | 200
# NaCl molality (mol/kg) | 2 | 2 | 5
# NaCl mass fraction (kg/kg) | 0.1047 | 0.1047 | 0.2261
# --------------------------------------------------------------
# Expected values
# --------------------------------------------------------------
# Density (kg/m^3) | 1068.52 | 959.27 | 1065.58
# Viscosity (1e-6Pa.s) | 679.8 | 180.0 | 263.1
# Thermal conductivity (W/m/K) | 0.630 | 0.649 | 0.633
# --------------------------------------------------------------
# Calculated values
# --------------------------------------------------------------
# Density (kg/m^3) | 1067.18 | 958.68 | 1065.46
# Viscosity (1e-6 Pa.s) | 681.1 | 181.98 | 266.1
# Thermal conductivity (W/m/K) | 0.637 | 0.662 | 0.658
# --------------------------------------------------------------
#
# All results are within expected accuracy
[Mesh]
type = GeneratedMesh
dim = 2
nx = 3
ny = 1
xmax = 3
# This test uses ElementalVariableValue postprocessors on specific
# elements, so element numbering needs to stay unchanged
allow_renumbering = false
[]
[Variables]
[./dummy]
[../]
[]
[AuxVariables]
[./pressure]
family = MONOMIAL
order = CONSTANT
[../]
[./temperature]
family = MONOMIAL
order = CONSTANT
[../]
[./xnacl]
family = MONOMIAL
order = CONSTANT
[../]
[./density]
family = MONOMIAL
order = CONSTANT
[../]
[./enthalpy]
family = MONOMIAL
order = CONSTANT
[../]
[./internal_energy]
family = MONOMIAL
order = CONSTANT
[../]
[]
[Functions]
[./pic]
type = ParsedFunction
value = 'if(x<2,20e6, 40e6)'
[../]
[./tic]
type = ParsedFunction
value = 'if(x<1, 323.15, 473.15)'
[../]
[./xic]
type = ParsedFunction
value = 'if(x<2,0.1047, 0.2261)'
[../]
[]
[ICs]
[./p_ic]
type = FunctionIC
function = pic
variable = pressure
[../]
[./t_ic]
type = FunctionIC
function = tic
variable = temperature
[../]
[./x_ic]
type = FunctionIC
function = xic
variable = xnacl
[../]
[]
[AuxKernels]
[./density]
type = MaterialRealAux
variable = density
property = density
[../]
[./enthalpy]
type = MaterialRealAux
variable = enthalpy
property = enthalpy
[../]
[./internal_energy]
type = MaterialRealAux
variable = internal_energy
property = e
[../]
[]
[Modules]
[./FluidProperties]
[./water]
type = Water97FluidProperties
[../]
[./water_tab]
type = TabulatedFluidProperties
fp = water
save_file = false
[../]
[./brine]
type = BrineFluidProperties
water_fp = water_tab
[../]
[../]
[]
[Materials]
[./fp_mat]
type = MultiComponentFluidPropertiesMaterialPT
pressure = pressure
temperature = temperature
xmass = xnacl
fp = brine
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = dummy
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Postprocessors]
[./density0]
type = ElementalVariableValue
variable = density
elementid = 0
[../]
[./density1]
type = ElementalVariableValue
variable = density
elementid = 1
[../]
[./density2]
type = ElementalVariableValue
variable = density
elementid = 2
[../]
[./enthalpy0]
type = ElementalVariableValue
variable = enthalpy
elementid = 0
[../]
[./enthalpy1]
type = ElementalVariableValue
variable = enthalpy
elementid = 1
[../]
[./enthalpy2]
type = ElementalVariableValue
variable = enthalpy
elementid = 2
[../]
[./e0]
type = ElementalVariableValue
variable = internal_energy
elementid = 0
[../]
[./e1]
type = ElementalVariableValue
variable = internal_energy
elementid = 1
[../]
[./e2]
type = ElementalVariableValue
variable = internal_energy
elementid = 2
[../]
[]
[Outputs]
csv = true
file_base = brine_out
[]
(test/tests/multiapps/full_solve_multiapp/master.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
perf_graph = true
[]
[MultiApps]
[full_solve]
type = FullSolveMultiApp
# not setting app_type to use the same app type of master, i.e. MooseTestApp
execute_on = initial
positions = '0 0 0'
input_files = sub.i
[]
[]
(test/tests/ics/lagrange_ic/3d_second_order.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 5
ny = 5
nz = 5
elem_type = HEX27
[]
[Variables]
[./u]
order = SECOND
[../]
[]
[Functions]
[./afunc]
type = ParsedFunction
value = x^2
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
[ICs]
[./func_ic]
function = afunc
variable = u
type = FunctionIC
[../]
[]
(test/tests/auxkernels/solution_aux/solution_aux.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
# This test uses SolutionUserObject which doesn't work with DistributedMesh.
parallel_type = replicated
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./u_aux]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./initial_cond_aux]
type = SolutionAux
solution = xda_soln
execute_on = initial
variable = u_aux
[../]
[]
[UserObjects]
[./xda_soln]
type = SolutionUserObject
mesh = build_out_0001_mesh.xda
es = build_out_0001.xda
system_variables = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
nl_rel_tol = 1e-10
[]
[Outputs]
exodus = true
[./xda]
type = XDA
[../]
[]
(modules/heat_conduction/test/tests/code_verification/cartesian_test_no1.i)
# Problem I.1
#
# An infinite plate with constant thermal conductivity k and
# internal heat generation q. It is exposed on each boundary
# to a constant temperature: u(0) = ui and u(L) = uo.
#
# REFERENCE:
# A. Toptan, et al. (Mar.2020). Tech. rep. CASL-U-2020-1939-000, SAND2020-3887 R. DOI:10.2172/1614683.
[Mesh]
[./geom]
type = GeneratedMeshGenerator
dim = 1
elem_type = EDGE2
nx = 1
[../]
[]
[Variables]
[./u]
order = FIRST
[../]
[]
[Functions]
[./exact]
type = ParsedFunction
vars = 'q L k ui uo'
vals = '1200 1 12 100 0'
value = 'ui + (uo-ui)*x/L + (q/k) * x * (L-x) / 2'
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = u
[../]
[./heatsource]
type = HeatSource
function = 1200
variable = u
[../]
[]
[BCs]
[./ui]
type = DirichletBC
boundary = left
variable = u
value = 100
[../]
[./uo]
type = DirichletBC
boundary = right
variable = u
value = 0
[../]
[]
[Materials]
[./property]
type = GenericConstantMaterial
prop_names = 'density specific_heat thermal_conductivity'
prop_values = '1.0 1.0 12.0'
[../]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[./error]
type = ElementL2Error
function = exact
variable = u
[../]
[./h]
type = AverageElementSize
[]
[]
[Outputs]
csv = true
[]
(modules/porous_flow/test/tests/gravity/fully_saturated_grav01c.i)
# Checking that gravity head is established
# 1phase, 2-component, constant fluid-bulk, constant viscosity, constant permeability
# fully saturated with fully-saturated Kernel
# For better agreement with the analytical solution (ana_pp), just increase nx
# NOTE: the numerics described by this input file is quite delicate. Firstly, the steady-state solution does not depend on the mass-fraction distribution, so the mass-fraction variable can assume any values (with the constraint that its integral is the same as the initial condition). Secondly, because the PorousFlowFullySaturatedDarcyFlow does no upwinding, the steady-state porepressure distribution can contain non-physical oscillations. The solver choice and mesh choice used below mean the result is as expected, but changing these can produce different results.
[Mesh]
type = GeneratedMesh
dim = 1
nx = 100
xmin = -1
xmax = 0
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Variables]
[pp]
[InitialCondition]
type = RandomIC
min = 0
max = 1
[]
[]
[frac]
[InitialCondition]
type = RandomIC
min = 0
max = 1
[]
[]
[]
[Kernels]
[flux1]
type = PorousFlowFullySaturatedDarcyFlow
variable = pp
fluid_component = 0
gravity = '-1 0 0'
[]
[flux0]
type = PorousFlowFullySaturatedDarcyFlow
variable = frac
fluid_component = 1
gravity = '-1 0 0'
[]
[]
[Functions]
[ana_pp]
type = ParsedFunction
vars = 'g B p0 rho0'
vals = '1 1.2 0 1'
value = '-B*log(exp(-p0/B)+g*rho0*x/B)' # expected pp at base
[]
[]
[BCs]
[z]
type = DirichletBC
variable = pp
boundary = right
value = 0
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp frac'
number_fluid_phases = 1
number_fluid_components = 2
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 1.2
density0 = 1
viscosity = 1
thermal_expansion = 0
[]
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow1PhaseFullySaturated
porepressure = pp
[]
[massfrac]
type = PorousFlowMassFraction
mass_fraction_vars = frac
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1 0 0 0 2 0 0 0 3'
[]
[]
[Postprocessors]
[pp_base]
type = PointValue
variable = pp
point = '-1 0 0'
[]
[pp_analytical]
type = FunctionValuePostprocessor
function = ana_pp
point = '-1 0 0'
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = Newton
nl_rel_tol = 1E-12
petsc_options_iname = '-pc_factor_shift_type'
petsc_options_value = 'NONZERO'
[]
[Outputs]
execute_on = 'timestep_end'
file_base = fully_saturated_grav01c
[csv]
type = CSV
[]
[]
(modules/navier_stokes/test/tests/finite_element/ins/coupled-force/steady.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
nx = 16
ny = 16
[]
[./corner_node]
type = ExtraNodesetGenerator
new_boundary = 'pinned_node'
nodes = '0'
input = gen
[../]
[]
[Variables]
[./velocity]
family = LAGRANGE_VEC
[../]
[./p]
[../]
[u]
family = LAGRANGE_VEC
[]
[]
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[./mass_pspg]
type = INSADMassPSPG
variable = p
[../]
[./momentum_convection]
type = INSADMomentumAdvection
variable = velocity
[../]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
integrate_p_by_parts = true
[../]
[momentum_coupled_force]
type = INSADMomentumCoupledForce
variable = velocity
coupled_vector_var = u
[]
[./momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[../]
[u_diff]
type = VectorDiffusion
variable = u
[]
[]
[BCs]
[./no_slip]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom right left top'
[../]
[./pressure_pin]
type = DirichletBC
variable = p
boundary = 'pinned_node'
value = 0
[../]
[u_left]
type = VectorFunctionDirichletBC
variable = u
boundary = 'left'
function_x = 1
function_y = 1
[]
[u_right]
type = VectorFunctionDirichletBC
variable = u
boundary = 'right'
function_x = -1
function_y = -1
[]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[ins_mat]
type = INSADTauMaterial
velocity = velocity
pressure = p
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_levels -ksp_gmres_restart'
petsc_options_value = 'asm 6 200'
line_search = 'none'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
exodus = true
[]
(modules/phase_field/test/tests/ExpressionBuilderCoupledVectorTest/testCoupledVector.i)
[Mesh]
type = GeneratedMesh
dim = 2 # Problem dimension
nx = 10
ny = 10
[]
[GlobalParams]
op_num = 2 # Number of grains
var_name_base = gr # Base name of grains
[]
[AuxVariables]
[./gr0]
[./InitialCondition]
type = FunctionIC
function = x
[../]
[../]
[./gr1]
[./InitialCondition]
type = FunctionIC
function = y
[../]
[../]
[]
[Materials]
[./Tester]
type = EBCoupledVarTest
outputs = exodus
[../]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[../]
[Outputs]
exodus = true
execute_on = 'INITIAL TIMESTEP_END'
[]
(modules/fluid_properties/test/tests/interfaces/nan_interface/nan_interface.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./test_kernel]
type = NaNInterfaceTestKernel
variable = u
nan_interface_test_fp = fp
[../]
[]
[Modules]
[./FluidProperties]
[./fp]
type = NaNInterfaceTestFluidProperties
[../]
[]
[]
[Executioner]
type = Steady
[]
(modules/ray_tracing/test/tests/raybcs/dependencies/ray_bc_dependencies.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
[]
[]
[UserObjects/study]
type = RepeatableRayStudy
start_points = '0 0 0'
directions = '1 0 0'
names = ray
ray_data_names = data
initial_ray_data = 1
ray_kernel_coverage_check = false
[]
[RayBCs]
[add_1]
type = ChangeRayRayBCTest
boundary = right
data_name = data
add_value = 1
depends_on = add_10
[]
[scale_5]
type = ChangeRayRayBCTest
data_name = data
boundary = right
scale_value = 5
depends_on = scale_9
[]
[add_10]
type = ChangeRayRayBCTest
data_name = data
boundary = right
add_value = 10
[]
[scale_9]
type = ChangeRayRayBCTest
data_name = data
boundary = right
scale_value = 9
depends_on = add_1
[]
[kill]
type = KillRayBC
boundary = right
[]
[]
[Postprocessors/value]
type = RayDataValue
study = study
ray_name = ray
data_name = data
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
[]
(tutorials/tutorial01_app_development/step08_test_harness/problems/pressure_diffusion.i)
[Mesh]
type = GeneratedMesh # Can generate simple lines, rectangles and rectangular prisms
dim = 2 # Dimension of the mesh
nx = 100 # Number of elements in the x direction
ny = 10 # Number of elements in the y direction
xmax = 0.304 # Length of test chamber
ymax = 0.0257 # Test chamber radius
[]
[Problem]
type = FEProblem # This is the "normal" type of Finite Element Problem in MOOSE
coord_type = RZ # Axisymmetric RZ
rz_coord_axis = X # Which axis the symmetry is around
[]
[Variables]
[pressure]
# Adds a Linear Lagrange variable by default
[]
[]
[Kernels]
[diffusion]
type = DarcyPressure # Zero-gravity, divergence-free form of Darcy's law
variable = pressure # Operate on the "pressure" variable from above
permeability = 0.8451e-09 # (m^2) assumed permeability of the porous medium
[]
[]
[BCs]
[inlet]
type = ADDirichletBC # Simple u=value BC
variable = pressure # Variable to be set
boundary = left # Name of a sideset in the mesh
value = 4000 # (Pa) From Figure 2 from paper. First data point for 1mm spheres.
[]
[outlet]
type = ADDirichletBC
variable = pressure
boundary = right
value = 0 # (Pa) Gives the correct pressure drop from Figure 2 for 1mm spheres
[]
[]
[Executioner]
type = Steady # Steady state problem
solve_type = NEWTON # Perform a Newton solve
# Set PETSc parameters to optimize solver efficiency
petsc_options_iname = '-pc_type -pc_hypre_type' # PETSc option pairs with values below
petsc_options_value = ' hypre boomeramg'
[]
[Outputs]
exodus = true # Output Exodus format
[]
(test/tests/vectorpostprocessors/intersection_points_along_line/1d.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 10
# Ray tracing code is not yet compatible with DistributedMesh
parallel_type = replicated
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[VectorPostprocessors]
[./intersections]
type = IntersectionPointsAlongLine
start = '0.05 0 0'
end = '0.405 0 0'
[../]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Outputs]
csv = true
[]
(modules/navier_stokes/test/tests/finite_volume/cns/mms/1d/hllc-mms.i)
[GlobalParams]
fp = fp
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
xmin = .1
xmax = 1
nx = 2
[]
[]
[Variables]
[rho]
type = MooseVariableFVReal
[]
[rho_u]
type = MooseVariableFVReal
[]
[rho_et]
type = MooseVariableFVReal
[]
[]
[ICs]
[rho]
type = FunctionIC
variable = rho
function = 'cos(1.1*x)'
[]
[rho_u]
type = FunctionIC
variable = rho_u
function = '2*sin(1.1*x)'
[]
[rho_et]
type = FunctionIC
variable = rho_et
function = '3*cos(1.1*x)'
[]
[]
[FVKernels]
[mass_advection]
type = CNSFVMassHLLC
variable = rho
[]
[fake_diffusivity]
type = FVDiffusion
variable = rho
coeff = 1
[]
[mass_fn]
type = FVBodyForce
variable = rho
function = 'forcing_rho'
[]
[momentum_advection]
type = CNSFVMomentumHLLC
variable = rho_u
momentum_component = x
[]
[viscosity]
type = FVDiffusion
variable = rho_u
coeff = 1
[]
[momentum_fn]
type = FVBodyForce
variable = rho_u
function = 'forcing_rho_u'
[]
[fluid_energy_advection]
type = CNSFVFluidEnergyHLLC
variable = rho_et
[]
[fake_conduction]
type = FVDiffusion
variable = rho_et
coeff = 1
[]
[energy_fn]
type = FVBodyForce
variable = rho_et
function = 'forcing_rho_et'
[]
[]
[FVBCs]
[rho]
type = FVFunctionDirichletBC
boundary = 'left right'
variable = rho
function = 'exact_rho'
[]
[rho_u]
type = FVFunctionDirichletBC
boundary = 'left right'
variable = rho_u
function = 'exact_rho_u'
[]
[rho_et]
type = FVFunctionDirichletBC
boundary = 'left right'
variable = rho_et
function = 'exact_rho_et'
[]
[]
[Materials]
[var_mat]
type = ConservedVarValuesMaterial
rho = rho
rhou = rho_u
rho_et = rho_et
[]
[]
[Modules]
[FluidProperties]
[fp]
type = TestConservedVarFluidProperties
[]
[]
[]
[Functions]
[exact_rho]
type = ParsedFunction
value = 'cos(x)'
[]
[forcing_rho]
type = ParsedFunction
value = '3*cos(x)'
[]
[exact_rho_u]
type = ParsedFunction
value = '2*sin(x)'
[]
[forcing_rho_u]
type = ParsedFunction
value = '4*sin(x)^3/cos(x)^2 + 9*sin(x)'
[]
[exact_rho_et]
type = ParsedFunction
value = '3*cos(x)'
[]
[forcing_rho_et]
type = ParsedFunction
value = '11*cos(x)'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2rho]
type = ElementL2Error
variable = rho
function = exact_rho
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2rho_u]
variable = rho_u
function = exact_rho_u
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2rho_et]
variable = rho_et
function = exact_rho_et
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(test/tests/outputs/dofmap/simple.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[AuxVariables]
[./w]
[../]
[]
[Kernels]
[./diffu]
type = Diffusion
variable = u
[../]
[./diffv]
type = Diffusion
variable = v
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
dofmap = true
[]
(test/tests/postprocessors/nodal_sum/nodal_sum_block_non_unique.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 2
[]
[./left]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '0 0 0'
top_right = '0.5 1 0'
block_id = 100
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Postprocessors]
[./nodal_sum]
type = NodalSum
variable = u
execute_on = 'initial timestep_end'
block = '0 100'
unique_node_execute = false
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
csv = true
[]
(test/tests/mesh_modifiers/add_side_sets_from_bounding_box/error_no_side_sets_found.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[createNewSidesetOne]
type = SideSetsFromBoundingBoxGenerator
input = gen
block_id = 0
boundary_id_old = 'right'
boundary_id_new = 11
bottom_left = '-0.1 -0.1 0'
top_right = '0.9 0.9 0'
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[leftBC]
type = DirichletBC
variable = u
boundary = 'left'
value = 1
[]
[rightBC]
type = DirichletBC
variable = u
boundary = 11
value = 0
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/fluid_properties/test/tests/ideal_gas/test2.i)
# Test IdealGasFluidPropertiesFluidProperties using pressure and temperature
# Use values for Oxygen at 1 MPa and 350 K from NIST chemistry webook
#
# Input values:
# Cv = 669.8e J/kg/K
# Cp = 938.75 J/kg/K
# M = 31.9988e-3 kg/mol
#
# Expected output:
# density = 10.99591793 kg/m^3
# internal energy = 234.43e3 J/kg
# enthalpy = 328.5625e3 J/kg
# speed of sound = 357.0151605 m/s
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
[]
[Variables]
[./dummy]
[../]
[]
[AuxVariables]
[./pressure]
family = MONOMIAL
order = CONSTANT
initial_condition = 1e6
[../]
[./temperature]
family = MONOMIAL
order = CONSTANT
initial_condition = 350
[../]
[./density]
family = MONOMIAL
order = CONSTANT
[../]
[./viscosity]
family = MONOMIAL
order = CONSTANT
[../]
[./cp]
family = MONOMIAL
order = CONSTANT
[../]
[./cv]
family = MONOMIAL
order = CONSTANT
[../]
[./internal_energy]
family = MONOMIAL
order = CONSTANT
[../]
[./enthalpy]
family = MONOMIAL
order = CONSTANT
[../]
[./entropy]
family = MONOMIAL
order = CONSTANT
[../]
[./thermal_cond]
family = MONOMIAL
order = CONSTANT
[../]
[./c]
family = MONOMIAL
order = CONSTANT
[../]
[]
[AuxKernels]
[./density]
type = MaterialRealAux
variable = density
property = density
[../]
[./viscosity]
type = MaterialRealAux
variable = viscosity
property = viscosity
[../]
[./cp]
type = MaterialRealAux
variable = cp
property = cp
[../]
[./cv]
type = MaterialRealAux
variable = cv
property = cv
[../]
[./e]
type = MaterialRealAux
variable = internal_energy
property = e
[../]
[./enthalpy]
type = MaterialRealAux
variable = enthalpy
property = h
[../]
[./entropy]
type = MaterialRealAux
variable = entropy
property = s
[../]
[./thermal_cond]
type = MaterialRealAux
variable = thermal_cond
property = k
[../]
[./c]
type = MaterialRealAux
variable = c
property = c
[../]
[]
[Modules]
[./FluidProperties]
[./idealgas]
type = IdealGasFluidProperties
gamma = 1.401537772469394
molar_mass = 0.0319988
[../]
[]
[]
[Materials]
[./fp_mat]
type = FluidPropertiesMaterialPT
pressure = pressure
temperature = temperature
fp = idealgas
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = dummy
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(modules/combined/test/tests/restart-transient-from-ss-with-stateful/sub_ss.i)
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
nx = 8
ny = 8
xmin = -82.627
xmax = 82.627
ymin = -82.627
ymax = 82.627
dim = 2
[]
[./extra_nodes_x]
type = ExtraNodesetGenerator
input = 'gen'
new_boundary = 'no_x'
coord = '0 82.627 0'
[../]
[./extra_nodes_y]
type = ExtraNodesetGenerator
input = 'extra_nodes_x'
new_boundary = 'no_y'
coord = '-82.627 0 0'
[../]
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
[]
[AuxVariables]
[./temp]
[../]
[]
[Modules/TensorMechanics/Master]
# FINITE strain when strain is large, i.e., visible movement.
# SMALL strain when things are stressed, but may not move.
[./fuel]
add_variables = true
strain = FINITE
temperature = temp
eigenstrain_names = 'thermal_eigenstrain'
generate_output = 'vonmises_stress stress_xx stress_yy hydrostatic_stress max_principal_stress strain_xy elastic_strain_xx stress_xy'
extra_vector_tags = 'ref'
use_finite_deform_jacobian = true
incremental = true
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 'no_x'
value = 0.0
preset = true
[../]
[./no_y]
type = DirichletBC
preset = true
variable = disp_y
boundary = 'no_y'
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 3e10 # Pa
poissons_ratio = 0.33 # unitless
[../]
[./thermal_strains]
type = ComputeThermalExpansionEigenstrain
temperature = temp
thermal_expansion_coeff = 2e-6 # 1/K
stress_free_temperature = 500 # K
eigenstrain_name = 'thermal_eigenstrain'
[../]
[./stress_finite] # goes with FINITE strain formulation
type = ComputeFiniteStrainElasticStress
[../]
[]
[Postprocessors]
[./avg_temp]
type = ElementAverageValue
variable = temp
[../]
[./disp_x_max_element]
type = ElementExtremeValue
value_type = max
variable = disp_x
execute_on = 'initial timestep_end'
[../]
[./disp_y_max_element]
type = ElementExtremeValue
value_type = max
variable = disp_y
execute_on = 'initial timestep_end'
[../]
[./disp_x_max_nodal]
type = NodalExtremeValue
value_type = max
variable = disp_x
execute_on = 'initial timestep_end'
[../]
[./disp_y_max_nodal]
type = NodalExtremeValue
value_type = max
variable = disp_y
execute_on = 'initial timestep_end'
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart'
petsc_options_value = 'hypre boomeramg 300'
line_search = 'none'
l_tol = 1e-02
nl_rel_tol = 5e-04
nl_abs_tol = 1e-2
l_max_its = 50
nl_max_its = 25
[]
[Outputs]
exodus = true
print_linear_residuals = false
perf_graph = true
[]
(test/tests/kernels/jxw_grad_test_dep_on_displacements/not-handling-jxw.i)
[GlobalParams]
displacements = 'disp_x disp_y'
order = SECOND
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
elem_type = QUAD9
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./u]
order = FIRST
[../]
[./v]
[../]
[]
[Kernels]
[./disp_x]
type = Diffusion
variable = disp_x
[../]
[./disp_y]
type = Diffusion
variable = disp_y
[../]
[./u]
type = ADDiffusion
variable = u
use_displaced_mesh = true
[../]
[./v]
type = ADDiffusion
variable = v
use_displaced_mesh = true
[../]
[]
[BCs]
# BCs cannot be preset due to Jacobian test
[./u_left]
type = DirichletBC
preset = false
value = 0
boundary = 'left'
variable = u
[../]
[./u_right]
type = DirichletBC
preset = false
value = 1
boundary = 'right'
variable = u
[../]
[./v_left]
type = DirichletBC
preset = false
value = 0
boundary = 'left'
variable = v
[../]
[./v_right]
type = DirichletBC
preset = false
value = 1
boundary = 'right'
variable = v
[../]
[./disp_x_left]
type = DirichletBC
preset = false
value = 0
boundary = 'left'
variable = disp_x
[../]
[./disp_x_right]
type = DirichletBC
preset = false
value = 1
boundary = 'right'
variable = disp_x
[../]
[./disp_y_left]
type = DirichletBC
preset = false
value = 0
boundary = 'bottom'
variable = disp_y
[../]
[./disp_y_right]
type = DirichletBC
preset = false
value = 1
boundary = 'top'
variable = disp_y
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
[./dofmap]
type = DOFMap
execute_on = 'initial'
[../]
exodus = true
[]
[ICs]
[./disp_x]
type = RandomIC
variable = disp_x
min = 0.01
max = 0.09
[../]
[./disp_y]
type = RandomIC
variable = disp_y
min = 0.01
max = 0.09
[../]
[./u]
type = RandomIC
variable = u
min = 0.1
max = 0.9
[../]
[./v]
type = RandomIC
variable = v
min = 0.1
max = 0.9
[../]
[]
(test/tests/outputs/tecplot/tecplot.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
tecplot = true
[]
(tutorials/tutorial01_app_development/step10_auxkernels/test/tests/kernels/darcy_pressure/darcy_pressure_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[pressure]
[]
[]
[Kernels]
[diffusion]
type = DarcyPressure
variable = pressure
[]
[]
[Materials]
[column]
type = PackedColumn
[]
[]
[BCs]
[left]
type = ADDirichletBC
variable = pressure
boundary = left
value = 0
[]
[right]
type = ADDirichletBC
variable = pressure
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/materials/functor_properties/vector-magnitude/vector-test.i)
# This example reproduces the libmesh vector_fe example 1 results
[Mesh]
type = GeneratedMesh
dim = 2
nx = 15
ny = 15
xmin = -1
ymin = -1
[]
[Variables]
[u]
family = LAGRANGE_VEC
[]
[]
[AuxVariables]
[mag]
order = FIRST
family = MONOMIAL
[]
[]
[AuxKernels]
[mag]
type = ADFunctorElementalAux
variable = mag
functor = mat_mag
[]
[]
[Kernels]
[diff]
type = VectorDiffusion
variable = u
[]
[body_force]
type = VectorBodyForce
variable = u
function_x = 'ffx'
function_y = 'ffy'
[]
[]
[BCs]
[bnd]
type = VectorFunctionDirichletBC
variable = u
function_x = 'x_exact_sln'
function_y = 'y_exact_sln'
function_z = '0'
boundary = 'left right top bottom'
[]
[]
[Functions]
[x_exact_sln]
type = ParsedFunction
value = 'cos(.5*pi*x)*sin(.5*pi*y)'
[]
[y_exact_sln]
type = ParsedFunction
value = 'sin(.5*pi*x)*cos(.5*pi*y)'
[]
[ffx]
type = ParsedFunction
value = '.5*pi*pi*cos(.5*pi*x)*sin(.5*pi*y)'
[]
[ffy]
type = ParsedFunction
value = '.5*pi*pi*sin(.5*pi*x)*cos(.5*pi*y)'
[]
[]
[Materials]
[functor]
type = ADVectorMagnitudeFunctorMaterial
vector_functor = u
vector_magnitude_name = mat_mag
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/rz_cone_by_parts_steady.i)
# This input file tests several different things:
# .) The axisymmetric (RZ) form of the governing equations.
# .) An open boundary.
# .) Not integrating the pressure by parts, thereby requiring a pressure pin.
# .) Natural boundary condition at the outlet.
[GlobalParams]
integrate_p_by_parts = true
laplace = true
gravity = '0 0 0'
[]
[Mesh]
file = '2d_cone.msh'
[]
[Problem]
coord_type = RZ
[]
[Preconditioning]
[./SMP_PJFNK]
type = SMP
full = true
solve_type = Newton
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = 'bjacobi ilu 4'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
csv = true
console = true
[./out]
type = Exodus
[../]
[]
[Variables]
[./vel_x]
# Velocity in radial (r) direction
family = LAGRANGE
order = SECOND
[../]
[./vel_y]
# Velocity in axial (z) direction
family = LAGRANGE
order = SECOND
[../]
[./p]
family = LAGRANGE
order = FIRST
[../]
[]
[BCs]
[./u_in]
type = DirichletBC
boundary = bottom
variable = vel_x
value = 0
[../]
[./v_in]
type = FunctionDirichletBC
boundary = bottom
variable = vel_y
function = 'inlet_func'
[../]
[./u_axis_and_walls]
type = DirichletBC
boundary = 'left right'
variable = vel_x
value = 0
[../]
[./v_no_slip]
type = DirichletBC
boundary = 'right'
variable = vel_y
value = 0
[../]
[]
[Kernels]
[./mass]
type = INSMassRZ
variable = p
u = vel_x
v = vel_y
pressure = p
[../]
[./x_momentum_space]
type = INSMomentumLaplaceFormRZ
variable = vel_x
u = vel_x
v = vel_y
pressure = p
component = 0
[../]
[./y_momentum_space]
type = INSMomentumLaplaceFormRZ
variable = vel_y
u = vel_x
v = vel_y
pressure = p
component = 1
[../]
[]
[Materials]
[./const]
type = GenericConstantMaterial
block = 'volume'
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[]
[Functions]
[./inlet_func]
type = ParsedFunction
value = '-4 * x^2 + 1'
[../]
[]
[Postprocessors]
[./flow_in]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'bottom'
execute_on = 'timestep_end'
[../]
[./flow_out]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'top'
execute_on = 'timestep_end'
[../]
[]
(test/tests/postprocessors/change_over_fixed_point/change_over_fixed_point.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 5
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = PostprocessorDirichletBC
variable = u
boundary = right
postprocessor = 'num_coupling'
[]
[]
[Executioner]
type = Steady
fixed_point_min_its = 10
fixed_point_max_its = 10
[]
[Postprocessors]
[num_coupling]
type = NumFixedPointIterations
execute_on = 'initial timestep_begin timestep_end'
[]
[norm]
type = ElementL2Norm
variable = u
execute_on = 'initial timestep_begin timestep_end'
[]
[change_over_fixed_point]
type = ChangeOverFixedPointPostprocessor
postprocessor = norm
change_with_respect_to_initial = false
execute_on = 'initial timestep_end'
[]
[]
[Outputs]
file_base = 'change_over_fixed_point_previous'
csv = true
[]
(test/tests/misc/check_error/missing_req_par_mesh_block_test.i)
#
# Tests elemental PPS running on multiple block
#
[Mesh]
type = StripeMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 3
ny = 3
elem_type = QUAD4
[]
[Functions]
[./forcing_fn]
type = ParsedFunction
value = x
[../]
[]
[Variables]
[./u]
family = MONOMIAL
order = CONSTANT
[../]
[]
[Kernels]
[./uv]
type = Reaction
variable = u
[../]
[./fv]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[Postprocessors]
[./avg_1_2]
type = ElementAverageValue
variable = u
block = '0 1'
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(modules/porous_flow/test/tests/fluids/simple_fluid_yr.i)
# Test the properties calculated by the simple fluid Material
# Time unit is chosen to be years
# Pressure 10 MPa
# Temperature = 300 K (temperature unit = K)
# Density should equal 1500*exp(1E7/1E9-2E-4*300)=1426.844 kg/m^3
# Viscosity should equal 3.49E-11 Pa.yr
# Energy density should equal 4000 * 300 = 1.2E6 J/kg
# Specific enthalpy should equal 4000 * 300 + 10e6 / 1426.844 = 1.207008E6 J/kg
[Modules]
[FluidProperties]
[the_simple_fluid]
type = SimpleFluidProperties
thermal_expansion = 2.0E-4
cv = 4000.0
cp = 5000.0
bulk_modulus = 1.0E9
thermal_conductivity = 1.0
viscosity = 1.1E-3
density0 = 1500.0
[]
[]
[]
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp T'
number_fluid_phases = 1
number_fluid_components = 1
[]
[]
[Variables]
[pp]
initial_condition = 10E6
[]
[T]
initial_condition = 300.0
[]
[]
[Kernels]
[dummy_p]
type = Diffusion
variable = pp
[]
[dummy_T]
type = Diffusion
variable = T
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
temperature = T
[]
[ppss]
type = PorousFlow1PhaseFullySaturated
porepressure = pp
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
temperature_unit = Kelvin
time_unit = years
fp = the_simple_fluid
phase = 0
[]
[]
[Postprocessors]
[pressure]
type = ElementIntegralVariablePostprocessor
variable = pp
[]
[temperature]
type = ElementIntegralVariablePostprocessor
variable = T
[]
[density]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_fluid_phase_density_qp0'
[]
[viscosity]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_viscosity_qp0'
[]
[internal_energy]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_fluid_phase_internal_energy_qp0'
[]
[enthalpy]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_fluid_phase_enthalpy_qp0'
[]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
csv = true
[]
(test/tests/preconditioners/pbp/pbp_adapt_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 2
ny = 2
elem_type = QUAD4
[]
[Variables]
active = 'u v'
[./u]
order = FIRST
family = LAGRANGE
[../]
[./v]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
[./forcing_fn]
type = ParsedFunction
value = -4
[../]
[./exact_fn]
type = ParsedFunction
value = ((x*x)+(y*y))
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = forcing_fn
[../]
[./conv_v]
type = CoupledForce
variable = v
v = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
boundary = '0 1 2 3'
function = exact_fn
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = 1
value = 0
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = 2
value = 0
[../]
[]
[Postprocessors]
[./l2_err]
type = ElementL2Error
variable = u
function = exact_fn
[../]
[]
[Preconditioning]
[./PBP]
type = PBP
solve_order = 'u v'
preconditioner = 'AMG ASM'
off_diag_row = 'v'
off_diag_column = 'u'
[../]
[]
[Executioner]
type = Steady
solve_type = JFNK
[./Adaptivity]
steps = 3
coarsen_fraction = 0.1
refine_fraction = 0.2
max_h_level = 5
[../]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = out_pbp_adapt
print_mesh_changed_info = true
exodus = true
[]
(modules/tensor_mechanics/test/tests/gravity/ad_gravity_test.i)
#
# Gravity Test
#
# This test is designed to apply a gravity body force.
#
# The mesh is composed of one block with a single element.
# The bottom is fixed in all three directions. Poisson's ratio
# is zero and the density is 20/9.81
# which makes it trivial to check displacements.
#
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
type = GeneratedMesh
dim = 3
[]
[Modules/TensorMechanics/Master]
[all]
add_variables = true
use_automatic_differentiation = true
[]
[]
[Kernels]
[gravity_y]
type = ADGravity
variable = disp_y
value = -9.81
[]
[]
[BCs]
[no_x]
type = DirichletBC
variable = disp_x
boundary = bottom
value = 0.0
[]
[no_y]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[]
[no_z]
type = DirichletBC
variable = disp_z
boundary = bottom
value = 0.0
[]
[]
[Materials]
[Elasticity_tensor]
type = ADComputeElasticityTensor
fill_method = symmetric_isotropic
C_ijkl = '0 0.5e6'
[]
[stress]
type = ADComputeLinearElasticStress
[]
[density]
type = ADGenericConstantMaterial
prop_names = density
prop_values = 2.0387
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
nl_abs_tol = 1e-10
l_max_its = 20
[]
[Outputs]
[out]
type = Exodus
elemental_as_nodal = true
[]
[]
(modules/chemical_reactions/test/tests/jacobian/coupled_convreact.i)
# Test the Jacobian terms for the CoupledConvectionReactionSub Kernel
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
[./a]
order = FIRST
family = LAGRANGE
[../]
[./b]
order = FIRST
family = LAGRANGE
[../]
[./pressure]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./pressure]
type = RandomIC
variable = pressure
min = 1
max = 5
[../]
[./a]
type = RandomIC
variable = a
max = 1
min = 0
[../]
[./b]
type = RandomIC
variable = b
max = 1
min = 0
[../]
[]
[Kernels]
[./diff]
type = DarcyFluxPressure
variable = pressure
[../]
[./diff_b]
type = Diffusion
variable = b
[../]
[./a1conv]
type = CoupledConvectionReactionSub
variable = a
v = b
log_k = 2
weight = 1
sto_v = 2.5
sto_u = 2
p = pressure
[../]
[]
[Materials]
[./porous]
type = GenericConstantMaterial
prop_names = 'diffusivity conductivity porosity'
prop_values = '1e-4 1e-4 0.2'
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
perf_graph = true
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
(modules/navier_stokes/test/tests/postprocessors/flow_rates/conservation_INSFE.i)
[Mesh]
second_order = true
inactive = 'mesh internal_boundary_bot internal_boundary_top'
[mesh]
type = CartesianMeshGenerator
dim = 2
dx = '1'
dy = '1 1 1'
ix = '5'
iy = '5 5 5'
subdomain_id = '1
2
3'
[]
[internal_boundary_bot]
type = SideSetsBetweenSubdomainsGenerator
input = mesh
new_boundary = 'internal_bot'
primary_block = 1
paired_block = 2
[]
[internal_boundary_top]
type = SideSetsBetweenSubdomainsGenerator
input = internal_boundary_bot
new_boundary = 'internal_top'
primary_block = 2
paired_block = 3
[]
[diverging_mesh]
type = FileMeshGenerator
file = 'expansion_quad.e'
[]
[]
[Modules]
[IncompressibleNavierStokes]
equation_type = steady-state
# no slip BCs
velocity_boundary = 'bottom right left'
velocity_function = '0 1 0 0 0 0'
pressure_boundary = 'top'
pressure_function = '1'
density_name = rho
dynamic_viscosity_name = mu
integrate_p_by_parts = false
order = SECOND
[]
[]
[Materials]
[const]
type = GenericConstantMaterial
block = '1 2 3'
prop_names = 'rho mu'
prop_values = '1 1'
[]
[ADconst]
type = ADGenericFunctorMaterial
block = '1 2 3'
prop_names = 'rho_ad'
prop_values = '1'
[]
[]
[Preconditioning]
[SMP_PJFNK]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-ksp_gmres_restart -pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = '300 bjacobi ilu 4'
line_search = none
nl_rel_tol = 1e-12
nl_max_its = 6
l_tol = 1e-6
l_max_its = 300
[]
[Postprocessors]
[inlet_mass_constant]
type = VolumetricFlowRate
boundary = bottom
vel_x = vel_x
vel_y = vel_y
advected_variable = 1
[]
[inlet_mass_matprop]
type = VolumetricFlowRate
boundary = bottom
vel_x = vel_x
vel_y = vel_y
advected_mat_prop = 'rho_ad'
[]
[mid1_mass]
type = VolumetricFlowRate
boundary = internal_bot
vel_x = vel_x
vel_y = vel_y
[]
[other_mid1_mass]
type = VolumetricFlowRate
boundary = internal_bot
vel_x = vel_x
vel_y = vel_y
advected_mat_prop = 'rho_ad'
[]
[mid2_mass]
type = VolumetricFlowRate
boundary = internal_top
vel_x = vel_x
vel_y = vel_y
[]
[outlet_mass]
type = VolumetricFlowRate
boundary = top
vel_x = vel_x
vel_y = vel_y
[]
[inlet_momentum_x]
type = VolumetricFlowRate
boundary = bottom
vel_x = vel_x
vel_y = vel_y
advected_variable = vel_x
[]
[mid1_momentum_x]
type = VolumetricFlowRate
boundary = internal_bot
vel_x = vel_x
vel_y = vel_y
advected_variable = vel_x
[]
[mid2_momentum_x]
type = VolumetricFlowRate
boundary = internal_top
vel_x = vel_x
vel_y = vel_y
advected_variable = vel_x
[]
[outlet_momentum_x]
type = VolumetricFlowRate
boundary = top
vel_x = vel_x
vel_y = vel_y
advected_variable = vel_x
[]
[inlet_momentum_y]
type = VolumetricFlowRate
boundary = bottom
vel_x = vel_x
vel_y = vel_y
advected_variable = vel_y
[]
[mid1_momentum_y]
type = VolumetricFlowRate
boundary = internal_bot
vel_x = vel_x
vel_y = vel_y
advected_variable = vel_y
[]
[mid2_momentum_y]
type = VolumetricFlowRate
boundary = internal_top
vel_x = vel_x
vel_y = vel_y
advected_variable = vel_y
[]
[outlet_momentum_y]
type = VolumetricFlowRate
boundary = top
vel_x = vel_x
vel_y = vel_y
advected_variable = vel_y
[]
[]
[Outputs]
exodus = false
csv = true
inactive = 'console_mass console_momentum_x console_momentum_y'
[console_mass]
type = Console
start_step = 1
show = 'inlet_mass_variable inlet_mass_constant inlet_mass_matprop mid1_mass mid2_mass outlet_mass'
[]
[console_momentum_x]
type = Console
start_step = 1
show = 'inlet_momentum_x mid1_momentum_x mid2_momentum_x outlet_momentum_x'
[]
[console_momentum_y]
type = Console
start_step = 1
show = 'inlet_momentum_y mid1_momentum_y mid2_momentum_y outlet_momentum_y'
[]
[]
(test/tests/auxkernels/element_aux_var/elemental_sort_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./one]
order = CONSTANT
family = MONOMIAL
initial_condition = 0
[../]
[./two]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
# Intentionally out of order to test sorting capabiilties
active = 'one two'
[./two]
variable = two
type = CoupledAux
value = 2
operator = '/'
coupled = one
[../]
[./one]
variable = one
type = ConstantAux
value = 1
[../]
[./five]
type = ConstantAux
variable = five
boundary = '3 1'
value = 5
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[]
(test/tests/samplers/base/threads.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
ny = 1
[]
[Variables]
[u]
[]
[]
[Samplers]
[sample]
type = TestSampler
execute_on = 'initial'
[]
[]
[Postprocessors]
[test]
type = SamplerTester
sampler = sample
test_type = THREAD
[]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
kernel_coverage_check = false
[]
[Outputs]
[]
(test/tests/auxkernels/hardware_id_aux/hardware_id_aux.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./hardware_id]
family = MONOMIAL
order = CONSTANT
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./hardware_id]
type = HardwareIDAux
variable = hardware_id
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/position/position.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
[./out]
type = Exodus
position = '1 1 0'
[../]
[]
(test/tests/controls/moose_base_naming_access/base_object_param.i)
[Mesh]
type = GeneratedMesh
dim = 2
elem_type = QUAD4
# use odd numbers so points do not fall on element boundaries
nx = 31
ny = 31
[]
[Variables]
[./diffused]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = diffused
[../]
[]
[DiracKernels]
[./test_object]
type = MaterialPointSource
point = '0.5 0.5 0'
variable = diffused
[../]
[]
[BCs]
[./bottom_diffused]
type = DirichletBC
variable = diffused
boundary = 'bottom'
value = 2
[../]
[./top_diffused]
type = DirichletBC
variable = diffused
boundary = 'top'
value = 0
[../]
[]
[Materials]
[./mat]
type = GenericConstantMaterial
prop_names = 'matp'
prop_values = '1'
block = 0
[../]
[]
[Postprocessors]
[./test_object]
type = FunctionValuePostprocessor
function = '2*(x+y)'
point = '0.5 0.5 0'
[../]
[./other_point_test_object]
type = FunctionValuePostprocessor
function = '3*(x+y)'
point = '0.5 0.5 0'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
[Controls]
[./point_control]
type = TestControl
test_type = 'point'
parameter = 'DiracKernel::test_object/point'
execute_on = 'initial'
[../]
[]
(test/tests/mesh_modifiers/smooth_mesh/mesh_smoother.i)
[Mesh]
[file]
type = FileMeshGenerator
file = concentric_circle_mesh_in.e
[]
[smooth]
type = SmoothMeshGenerator
input = file
iterations = 5
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/misc/save_in/dg_save_in_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 9
ny = 9
elem_type = QUAD4
[]
[Variables]
[./u]
order = FIRST
family = MONOMIAL
[./InitialCondition]
type = ConstantIC
value = 1
[../]
[../]
[]
[AuxVariables]
[./tot_resid]
order = FIRST
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
save_in = 'tot_resid'
[../]
[./forcing]
type = BodyForce
variable = u
function = 1
save_in = 'tot_resid'
[../]
[]
[DGKernels]
[./dg_diff]
type = DGDiffusion
variable = u
epsilon = -1
sigma = 6
save_in = 'tot_resid'
[../]
[]
[BCs]
[./robin]
type = RobinBC
boundary = 'left right top bottom'
variable = u
save_in = 'tot_resid'
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
nl_rel_tol = 1e-10
[]
[Outputs]
exodus = true
[]
(test/tests/samplers/distribute/distribute.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[Samplers]
[sampler]
type = TestSampler
num_rows = 10000000
num_cols = 1
[]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[total]
type = MemoryUsage
mem_units = 'bytes'
execute_on = 'INITIAL TIMESTEP_END'
[]
[per_proc]
type = MemoryUsage
value_type = "average"
mem_units = 'bytes'
execute_on = 'INITIAL TIMESTEP_END'
[]
[max_proc]
type = MemoryUsage
value_type = "max_process"
mem_units = 'bytes'
execute_on = 'INITIAL TIMESTEP_END'
[]
[test]
type = SamplerTester
sampler = sampler
test_type = 'getLocalSamples'
[]
[]
[Outputs]
csv = true
perf_graph = true
[]
(modules/phase_field/test/tests/solution_rasterizer/raster.i)
[Mesh]
type = GeneratedMesh
dim = 3
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[Executioner]
type = Steady
[]
[UserObjects]
[./soln]
type = SolutionRasterizer
system_variables = 'c'
mesh = diffuse_out.e
execute_on = timestep_begin
variable = c
xyz_input = in.xyz
xyz_output = out.xyz
# raster_mode = MAP
raster_mode = FILTER
threshold = 0.5
[../]
[]
(test/tests/outputs/postprocessor/postprocessor.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[AuxVariables]
[./aux0]
order = SECOND
family = SCALAR
[../]
[./aux1]
family = SCALAR
initial_condition = 5
[../]
[./aux2]
family = SCALAR
initial_condition = 10
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./diff_v]
type = CoefDiffusion
variable = v
coef = 2
[../]
[]
[BCs]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[./left_u]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = right
value = 3
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = left
value = 2
[../]
[]
[Postprocessors]
[./num_vars]
type = NumVars
system = 'ALL'
outputs = 'exodus2 console'
[../]
[./num_aux]
type = NumVars
system = 'AUX'
outputs = 'exodus'
[../]
[./num_nonlinear]
type = NumVars
system = 'NL'
outputs = 'all'
[../]
[./num_dofs]
type = NumDOFs
outputs = 'none'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
[./exodus]
type = Exodus
[../]
[./exodus2]
type = Exodus
[../]
[]
[ICs]
[./aux0_IC]
variable = aux0
values = '12 13'
type = ScalarComponentIC
[../]
[]
(test/tests/coord_type/coord_type_rz_integrated.i)
[Mesh]
type = GeneratedMesh
nx = 10
xmax = 1
ny = 10
ymax = 1
dim = 2
allow_renumbering = false
[]
[Problem]
type = FEProblem
coord_type = RZ
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
[./out]
type = Exodus
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[]
[DGKernels]
[./dg_diff]
type = DGDiffusion
variable = u
epsilon = -1
sigma = 6
[../]
[]
[Variables]
[./u]
order = FIRST
family = MONOMIAL
[../]
[]
[BCs]
[./source]
type = DGFunctionDiffusionDirichletBC
variable = u
boundary = 'right'
function = exact_fn
epsilon = -1
sigma = 6
[../]
[./vacuum]
boundary = 'top'
type = VacuumBC
variable = u
[../]
[]
[Functions]
[./exact_fn]
type = ConstantFunction
value = 1
[../]
[]
[ICs]
[./u]
type = ConstantIC
value = 1
variable = u
[../]
[]
(test/tests/misc/check_error/function_file_test6.i)
# Test for usage of missing function
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = ic_function
[../]
[../]
[]
[Functions]
[./ic_function]
type = PiecewiseLinear
x = '1'
y = '2'
xy_data = '1 2'
scale_factor = 1.0
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/interfacekernels/2d_interface/coupled_value_coupled_flux.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 2
xmax = 2
ny = 2
ymax = 2
[]
[./subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '0 0 0'
top_right = '1 1 0'
block_id = 1
[../]
[./interface]
type = SideSetsBetweenSubdomainsGenerator
input = subdomain1
primary_block = '0'
paired_block = '1'
new_boundary = 'primary0_interface'
[../]
[./break_boundary]
input = interface
type = BreakBoundaryOnSubdomainGenerator
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
block = 0
[../]
[./v]
order = FIRST
family = LAGRANGE
block = 1
[../]
[]
[Kernels]
[./diff_u]
type = CoeffParamDiffusion
variable = u
D = 4
block = 0
[../]
[./diff_v]
type = CoeffParamDiffusion
variable = v
D = 2
block = 1
[../]
[./source_u]
type = BodyForce
variable = u
value = 1
[../]
[]
[InterfaceKernels]
[./interface]
type = PenaltyInterfaceDiffusion
variable = u
neighbor_var = v
boundary = primary0_interface
penalty = 1e6
[../]
[]
[BCs]
[./u]
type = VacuumBC
variable = u
boundary = 'left_to_0 bottom_to_0 right top'
[../]
[./v]
type = VacuumBC
variable = v
boundary = 'left_to_1 bottom_to_1'
[../]
[]
[Postprocessors]
[./u_int]
type = ElementIntegralVariablePostprocessor
variable = u
block = 0
[../]
[./v_int]
type = ElementIntegralVariablePostprocessor
variable = v
block = 1
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
print_linear_residuals = true
[]
(modules/richards/test/tests/gravity_head_1/gh01.i)
# unsaturated = false
# gravity = false
# supg = false
# transient = false
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
xmin = -1
xmax = 1
[]
[BCs]
[./left]
type = DirichletBC
boundary = left
value = 1
variable = pressure
[../]
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0E3
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGnone]
type = RichardsSUPGnone
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = RandomIC
block = 0
min = 0
max = 1
[../]
[../]
[]
[Kernels]
active = 'richardsf'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
richardsVarNames_UO = PPNames
variable = pressure
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGnone
sat_UO = Saturation
seff_UO = SeffVG
viscosity = 1E-3
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = gh01
exodus = true
[]
(modules/phase_field/test/tests/feature_flood_test/parallel_feature_count.i)
[Mesh]
type = ImageMesh
dim = 2
file = spiral_16x16.png
scale_to_one = false
[]
[Variables]
[./u]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxVariables]
[./feature]
order = CONSTANT
family = MONOMIAL
[../]
[./proc_id]
order = CONSTANT
family = MONOMIAL
[../]
[./feature_ghost]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./nodal_flood_aux]
type = FeatureFloodCountAux
variable = feature
flood_counter = flood_count_pp
execute_on = 'initial timestep_end'
[../]
[./proc_id]
type = ProcessorIDAux
variable = proc_id
execute_on = 'initial timestep_end'
[../]
[./ghost]
type = FeatureFloodCountAux
variable = feature_ghost
field_display = GHOSTED_ENTITIES
flood_counter = flood_count_pp
execute_on = 'initial timestep_end'
[../]
[]
[Functions]
[./tif]
type = ImageFunction
component = 0
[../]
[]
[ICs]
[./u_ic]
type = FunctionIC
function = tif
variable = u
[../]
[]
[Postprocessors]
[./flood_count_pp]
type = FeatureFloodCount
variable = u
threshold = 1.0
execute_on = 'initial timestep_end'
[../]
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
[]
(test/tests/vectorpostprocessors/csv_reader/transfer/sub.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./aux]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/kernels/ad_mat_diffusion/2d_steady_state.i)
# This test solves a 2D steady state heat equation
# The error is found by comparing to the analytical solution
# Note that the thermal conductivity, specific heat, and density in this problem
# Are set to 1, and need to be changed to the constants of the material being
# Analyzed
[Mesh]
type = GeneratedMesh
dim = 2
nx = 30
ny = 30
xmax = 2
ymax = 2
[]
[Variables]
[./T]
[../]
[]
[Kernels]
[./diff]
type = MatDiffusion
variable = T
diffusivity = 1
[../]
[]
[BCs]
[./zero]
type = DirichletBC
variable = T
boundary = 'left right bottom'
value = 0
[../]
[./top]
type = FunctionDirichletBC
variable = T
boundary = top
function = '10*sin(pi*x*0.5)'
[../]
[]
[Postprocessors]
[./nodal_error]
type = NodalL2Error
function = '10/(sinh(pi))*sin(pi*x*0.5)*sinh(pi*y*0.5)'
variable = T
outputs = console
[../]
[./elemental_error]
type = ElementL2Error
function = '10/(sinh(pi))*sin(pi*x*0.5)*sinh(pi*y*0.5)'
variable = T
outputs = console
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/fvkernels/block-restriction/1d.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 20
xmax = 2
[]
[./subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '1.0 0 0'
block_id = 1
top_right = '2.0 1.0 0'
[../]
[./left_right]
input = subdomain1
type = SideSetsBetweenSubdomainsGenerator
primary_block = '0'
paired_block = '1'
new_boundary = 'left_right'
[../]
[./right_left]
input = left_right
type = SideSetsBetweenSubdomainsGenerator
primary_block = '1'
paired_block = '0'
new_boundary = 'right_left'
[../]
[]
[Variables]
[left]
family = MONOMIAL
order = CONSTANT
fv = true
block = 0
[]
[right]
family = MONOMIAL
order = CONSTANT
fv = true
block = 1
[]
[]
[FVKernels]
[left]
type = FVDiffusion
variable = left
coeff = coeff_left
block = 0
[]
[right]
type = FVDiffusion
variable = right
coeff = coeff_right
block = 1
[]
[]
[FVBCs]
[left]
type = FVDirichletBC
variable = left
boundary = left
value = 0
[]
[left_right]
type = FVDirichletBC
variable = left
boundary = left_right
value = 1
[]
[right_left]
type = FVDirichletBC
variable = right
boundary = right_left
value = 0
[]
[right]
type = FVDirichletBC
variable = right
boundary = right
value = 1
[]
[]
[Materials]
[left]
type = ADGenericFunctorMaterial
prop_names = 'coeff_left'
prop_values = '1'
block = 0
[]
[right]
type = ADGenericFunctorMaterial
prop_names = 'coeff_right'
prop_values = '1'
block = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
[]
[Outputs]
exodus = true
[]
(modules/richards/test/tests/gravity_head_2/gh_fu_02.i)
# unsaturated = true
# gravity = true
# supg = false
# transient = false
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
xmin = 0
xmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = 'DensityWater DensityGas'
relperm_UO = 'RelPermWater RelPermGas'
SUPG_UO = 'SUPGwater SUPGgas'
sat_UO = 'SatWater SatGas'
seff_UO = 'SeffWater SeffGas'
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = 'pwater pgas'
[../]
[./DensityWater]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0E2
[../]
[./DensityGas]
type = RichardsDensityConstBulk
dens0 = 0.5
bulk_mod = 0.5E2
[../]
[./SeffWater]
type = RichardsSeff2waterVG
m = 0.8
al = 1
[../]
[./SeffGas]
type = RichardsSeff2gasVG
m = 0.8
al = 1
[../]
[./RelPermWater]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./RelPermGas]
type = RichardsRelPermPower
simm = 0.0
n = 3
[../]
[./SatWater]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.15
[../]
[./SatGas]
type = RichardsSat
s_res = 0.05
sum_s_res = 0.15
[../]
[./SUPGwater]
type = RichardsSUPGnone
[../]
[./SUPGgas]
type = RichardsSUPGnone
[../]
[]
[Variables]
[./pwater]
order = FIRST
family = LAGRANGE
[../]
[./pgas]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
# get nonconvergence if initial condition is too crazy
[./water_ic]
type = FunctionIC
function = pwater_initial
variable = pwater
[../]
[./gas_ic]
type = FunctionIC
function = pgas_initial
variable = pgas
[../]
[]
[Kernels]
active = 'richardsfwater richardsfgas'
[./richardstwater]
type = RichardsMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFullyUpwindFlux
variable = pwater
[../]
[./richardstgas]
type = RichardsMassChange
variable = pgas
[../]
[./richardsfgas]
type = RichardsFullyUpwindFlux
variable = pgas
[../]
[]
[AuxVariables]
[./seffgas]
[../]
[./seffwater]
[../]
[]
[AuxKernels]
[./seffgas_kernel]
type = RichardsSeffAux
pressure_vars = 'pwater pgas'
seff_UO = SeffGas
variable = seffgas
[../]
[./seffwater_kernel]
type = RichardsSeffAux
pressure_vars = 'pwater pgas'
seff_UO = SeffWater
variable = seffwater
[../]
[]
[Postprocessors]
[./mwater_init]
type = RichardsMass
variable = pwater
execute_on = timestep_begin
outputs = none
[../]
[./mgas_init]
type = RichardsMass
variable = pgas
execute_on = timestep_begin
outputs = none
[../]
[./mwater_fin]
type = RichardsMass
variable = pwater
execute_on = timestep_end
outputs = none
[../]
[./mgas_fin]
type = RichardsMass
variable = pgas
execute_on = timestep_end
outputs = none
[../]
[./mass_error_water]
type = FunctionValuePostprocessor
function = fcn_mass_error_w
outputs = none # no reason why mass should be conserved
[../]
[./mass_error_gas]
type = FunctionValuePostprocessor
function = fcn_mass_error_g
outputs = none # no reason why mass should be conserved
[../]
[./pw_left]
type = PointValue
point = '0 0 0'
variable = pwater
outputs = none
[../]
[./pw_right]
type = PointValue
point = '1 0 0'
variable = pwater
outputs = none
[../]
[./error_water]
type = FunctionValuePostprocessor
function = fcn_error_water
[../]
[./pg_left]
type = PointValue
point = '0 0 0'
variable = pgas
outputs = none
[../]
[./pg_right]
type = PointValue
point = '1 0 0'
variable = pgas
outputs = none
[../]
[./error_gas]
type = FunctionValuePostprocessor
function = fcn_error_gas
[../]
[]
[Functions]
[./pwater_initial]
type = ParsedFunction
value = 1-x/2
[../]
[./pgas_initial]
type = ParsedFunction
value = 2-x/5
[../]
[./fcn_mass_error_w]
type = ParsedFunction
value = 'abs(0.5*(mi-mf)/(mi+mf))'
vars = 'mi mf'
vals = 'mwater_init mwater_fin'
[../]
[./fcn_mass_error_g]
type = ParsedFunction
value = 'abs(0.5*(mi-mf)/(mi+mf))'
vars = 'mi mf'
vals = 'mgas_init mgas_fin'
[../]
[./fcn_error_water]
type = ParsedFunction
value = 'abs((-b*log(-(gdens0*xval+(-b*exp(-p0/b)))/b)-p1)/p1)'
vars = 'b gdens0 p0 xval p1'
vals = '1E2 -1 pw_left 1 pw_right'
[../]
[./fcn_error_gas]
type = ParsedFunction
value = 'abs((-b*log(-(gdens0*xval+(-b*exp(-p0/b)))/b)-p1)/p1)'
vars = 'b gdens0 p0 xval p1'
vals = '0.5E2 -0.5 pg_left 1 pg_right'
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
viscosity = '1E-3 0.5E-3'
gravity = '-1 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -sub_pc_factor_shift_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'gmres asm lu NONZERO 1E-10 1E-10 10000'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = gh_fu_02
csv = true
[]
(test/tests/meshgenerators/combiner_generator/combiner_multi_input.i)
[Mesh]
[gen1]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
xmin=0
xmax=1
ymin=0
ymax=1
[]
[gen2]
type = GeneratedMeshGenerator
dim = 2
nx = 12
ny = 12
xmin=2
xmax=3
ymin=2
ymax=3
[]
[gen3]
type = GeneratedMeshGenerator
dim = 2
nx = 14
ny = 14
xmin=3.5
xmax=5
ymin=3
ymax=4
[]
[cmbn]
type = CombinerGenerator
inputs = 'gen1 gen2 gen3'
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/porous_flow/test/tests/gravity/grav02b.i)
# Checking that gravity head is established in the steady-state situation when 0<saturation<1 (note the strictly less-than).
# 2phase (PP), 2components, vanGenuchten, constant fluid bulk-moduli for each phase, constant viscosity, constant permeability, Corey relative perm
# For better agreement with the analytical solution (ana_pp), just increase nx
[Mesh]
type = GeneratedMesh
dim = 1
nx = 10
xmin = -1
xmax = 0
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Variables]
[ppwater]
initial_condition = -1.0
[]
[ppgas]
initial_condition = 0
[]
[]
[AuxVariables]
[massfrac_ph0_sp0]
initial_condition = 1
[]
[massfrac_ph1_sp0]
initial_condition = 0
[]
[]
[Kernels]
[flux0]
type = PorousFlowAdvectiveFlux
fluid_component = 0
variable = ppwater
gravity = '-1 0 0'
[]
[flux1]
type = PorousFlowAdvectiveFlux
fluid_component = 1
variable = ppgas
gravity = '-1 0 0'
[]
[]
[BCs]
[ppwater]
type = DirichletBC
boundary = right
variable = ppwater
value = -1
[]
[ppgas]
type = DirichletBC
boundary = right
variable = ppgas
value = 0
[]
[]
[Functions]
[ana_ppwater]
type = ParsedFunction
vars = 'g B p0 rho0'
vals = '1 2 pp_water_top 1'
value = '-B*log(exp(-p0/B)+g*rho0*x/B)' # expected pp at base
[]
[ana_ppgas]
type = ParsedFunction
vars = 'g B p0 rho0'
vals = '1 1 pp_gas_top 0.1'
value = '-B*log(exp(-p0/B)+g*rho0*x/B)' # expected pp at base
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'ppwater ppgas'
number_fluid_phases = 2
number_fluid_components = 2
[]
[pc]
type = PorousFlowCapillaryPressureVG
m = 0.5
alpha = 1
[]
[]
[Modules]
[FluidProperties]
[simple_fluid0]
type = SimpleFluidProperties
bulk_modulus = 2
density0 = 1
viscosity = 1
thermal_expansion = 0
[]
[simple_fluid1]
type = SimpleFluidProperties
bulk_modulus = 1
density0 = 0.1
viscosity = 0.5
thermal_expansion = 0
[]
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow2PhasePP
phase0_porepressure = ppwater
phase1_porepressure = ppgas
capillary_pressure = pc
[]
[massfrac]
type = PorousFlowMassFraction
mass_fraction_vars = 'massfrac_ph0_sp0 massfrac_ph1_sp0'
[]
[simple_fluid0]
type = PorousFlowSingleComponentFluid
fp = simple_fluid0
phase = 0
[]
[simple_fluid1]
type = PorousFlowSingleComponentFluid
fp = simple_fluid1
phase = 1
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1 0 0 0 2 0 0 0 3'
[]
[relperm_water]
type = PorousFlowRelativePermeabilityCorey
n = 1
phase = 0
[]
[relperm_gas]
type = PorousFlowRelativePermeabilityCorey
n = 1
phase = 1
[]
[]
[Postprocessors]
[pp_water_top]
type = PointValue
variable = ppwater
point = '0 0 0'
[]
[pp_water_base]
type = PointValue
variable = ppwater
point = '-1 0 0'
[]
[pp_water_analytical]
type = FunctionValuePostprocessor
function = ana_ppwater
point = '-1 0 0'
[]
[pp_gas_top]
type = PointValue
variable = ppgas
point = '0 0 0'
[]
[pp_gas_base]
type = PointValue
variable = ppgas
point = '-1 0 0'
[]
[pp_gas_analytical]
type = FunctionValuePostprocessor
function = ana_ppgas
point = '-1 0 0'
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
file_base = grav02b
[csv]
type = CSV
[]
exodus = false
[]
(test/tests/mortar/continuity-2d-non-conforming/soln-continuity.i)
[Mesh]
second_order = true
[file]
type = FileMeshGenerator
file = nodal_normals_test_offset_nonmatching_gap.e
[]
[./primary]
input = file
type = LowerDBlockFromSidesetGenerator
sidesets = '2'
new_block_id = '20'
[../]
[./secondary]
input = primary
type = LowerDBlockFromSidesetGenerator
sidesets = '1'
new_block_id = '10'
[../]
[]
[Problem]
kernel_coverage_check = false
[]
[Variables]
[./T]
block = '1 2'
order = SECOND
[../]
[./lambda]
block = '10'
[../]
[]
[BCs]
[./neumann]
type = FunctionGradientNeumannBC
exact_solution = exact_soln
variable = T
boundary = '3 4 5 6 7 8'
[../]
[]
[Kernels]
[./conduction]
type = Diffusion
variable = T
block = '1 2'
[../]
[./sink]
type = Reaction
variable = T
block = '1 2'
[../]
[./forcing_function]
type = BodyForce
variable = T
function = forcing_function
block = '1 2'
[../]
[]
[Functions]
[./forcing_function]
type = ParsedFunction
value = '-4 + x^2 + y^2'
[../]
[./exact_soln]
type = ParsedFunction
value = 'x^2 + y^2'
[../]
[]
[Debug]
show_var_residual_norms = 1
[]
[Constraints]
[./mortar]
type = EqualValueConstraint
primary_boundary = 2
secondary_boundary = 1
primary_subdomain = 20
secondary_subdomain = 10
variable = lambda
secondary_variable = T
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
solve_type = NEWTON
type = Steady
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_shift_type -pc_factor_shift_amount'
petsc_options_value = 'lu basic NONZERO 1e-15'
[]
[Outputs]
exodus = true
[dofmap]
type = DOFMap
execute_on = 'initial'
[]
[]
(modules/richards/test/tests/gravity_head_1/gh_fu_04.i)
# unsaturated = true
# gravity = true
# supg = false
# transient = false
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
xmin = -1
xmax = 1
[]
[BCs]
[./left]
type = DirichletBC
boundary = left
value = -1
variable = pressure
[../]
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGnone
sat_UO = Saturation
seff_UO = SeffVG
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0E3
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGnone]
type = RichardsSUPGnone
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = RandomIC
block = 0
min = -1
max = 0
[../]
[../]
[]
[Kernels]
active = 'richardsf'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFullyUpwindFlux
variable = pressure
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
viscosity = 1E-3
gravity = '-1 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = gh_fu_04
exodus = true
[]
(modules/ray_tracing/test/tests/actions/add_raybc_action/add_raybc_action.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
[]
[]
[UserObjects]
active = ''
[study]
type = RepeatableRayStudy
start_points = '0 0 0'
directions = '1 0 0'
names = 'ray'
ray_kernel_coverage_check = false
[]
[another_study]
type = RepeatableRayStudy
start_points = '0 0 0'
directions = '1 0 0'
names = 'ray'
ray_kernel_coverage_check = false
[]
[not_a_study]
type = VerifyElementUniqueID
[]
[]
[RayBCs]
active = ''
[missing_study_by_name]
type = NullRayBC
boundary = top
study = dummy
[]
[not_a_study]
type = NullRayBC
boundary = top
study = not_a_study
[]
[multiple_studies]
type = NullRayBC
boundary = top
[]
[missing_study]
type = NullRayBC
boundary = top
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
(test/tests/tag/2d_diffusion_tag_matrix.i)
[Mesh]
[square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[]
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
[]
[]
[AuxVariables]
[tag_variable1]
order = FIRST
family = LAGRANGE
[]
[tag_variable2]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
extra_matrix_tags = 'mat_tag1 mat_tag2'
[]
[]
[AuxKernels]
[TagMatrixAux1]
type = TagMatrixAux
variable = tag_variable1
v = u
matrix_tag = mat_tag1
[]
[TagMatrixAux2]
type = TagMatrixAux
variable = tag_variable2
v = u
matrix_tag = mat_tag2
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 3
value = 0
extra_matrix_tags = mat_tag1
[]
[right]
type = DirichletBC
variable = u
boundary = 1
value = 1
extra_matrix_tags = mat_tag2
[]
[]
[Problem]
type = FEProblem
extra_tag_matrices = 'mat_tag1 mat_tag2'
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
file_base = tag_matrix_out
exodus = true
[]
(test/tests/restart/restart_steady_from_transient/steady_from_transient_restart.i)
[Mesh]
[fmg]
type = FileMeshGenerator
file = transient_out_cp/LATEST
[]
parallel_type = replicated
[]
[Functions]
[./exact_fn]
type = ParsedFunction
value = ((x*x)+(y*y))
[../]
[./forcing_fn]
type = ParsedFunction
value = -4
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
boundary = '0 1 2 3'
function = exact_fn
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
[Problem]
restart_file_base = transient_out_cp/LATEST
[]
(test/tests/vectorpostprocessors/line_value_sampler/line_value_sampler.i)
###########################################################
# This is a simple test of the Vector Postprocessor
# System. A LineValueSampler is placed inside of a 2D
# domain to sample solution points uniformly along a line.
#
# @Requirement F6.30
###########################################################
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = left
value = 1
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = right
value = 0
[../]
[]
[Postprocessors]
[./u_avg]
type = ElementAverageValue
variable = u
execute_on = 'initial timestep_end'
[../]
[]
# Vector Postprocessor System
[VectorPostprocessors]
[./line_sample]
type = LineValueSampler
variable = 'u v'
start_point = '0 0.5 0'
end_point = '1 0.5 0'
num_points = 11
sort_by = id
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
csv = true
[]
(test/tests/mesh_modifiers/add_side_sets_from_bounding_box/overlapping_sidesets.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
nx = 10
ny = 10
nz = 10
[]
[createNewSidesetOne]
type = SideSetsFromBoundingBoxGenerator
input = gen
block_id = 0
boundary_id_old = 'bottom back left'
boundary_id_new = 10
bottom_left = '-1.1 -1.1 -1.1'
top_right = '1.1 1.1 1.1'
boundary_id_overlap = true
[]
[createNewSidesetTwo]
type = SideSetsFromBoundingBoxGenerator
input = createNewSidesetOne
block_id = 0
boundary_id_old = 'right bottom'
boundary_id_new = 11
bottom_left = '-1.1 -1.1 -1.1'
top_right = '1.1 1.1 1.1'
boundary_id_overlap = true
[]
[createNewSidesetThree]
type = SideSetsFromBoundingBoxGenerator
input = createNewSidesetTwo
block_id = 0
boundary_id_old = 'top front'
boundary_id_new = 12
bottom_left = '-1.1 -1.1 -1.1'
top_right = '1.1 1.1 1.1'
boundary_id_overlap = true
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[BCone]
type = DirichletBC
variable = u
boundary = 10
value = 1
[]
[BCtwo]
type = DirichletBC
variable = u
boundary = 11
value = 1
[]
[BCthree]
type = DirichletBC
variable = u
boundary = 12
value = 0
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/fvkernels/mms/skewness-correction/adv-diff-react/skewed.i)
a=1.1
diff=1.1
[Mesh]
[gen_mesh]
type = FileMeshGenerator
file = skewed.msh
[]
[]
[Variables]
[v]
initial_condition = 1
type = MooseVariableFVReal
face_interp_method = 'skewness-corrected'
cache_face_gradients = false
cache_face_values = true
[]
[]
[FVKernels]
[diff_v]
type = FVDiffusion
variable = v
coeff = ${diff}
[]
[advection]
type = FVAdvection
variable = v
velocity = '${a} ${fparse 2*a} 0'
advected_interp_method = 'average'
[]
[reaction]
type = FVReaction
variable = v
[]
[body_v]
type = FVBodyForce
variable = v
function = 'forcing'
[]
[]
[FVBCs]
[exact]
type = FVFunctionDirichletBC
boundary = 'left right top bottom'
function = 'exact'
variable = v
[]
[]
[Functions]
[exact]
type = ParsedFunction
value = 'sin(x)*cos(y)'
[]
[forcing]
type = ParsedFunction
value = '-2*a*sin(x)*sin(y) + a*cos(x)*cos(y) + 2*diff*sin(x)*cos(y) + sin(x)*cos(y)'
vars = 'a diff'
vals = '${a} ${diff}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
csv = true
[]
[Postprocessors]
[./error]
type = ElementL2Error
variable = v
function = exact
outputs = 'console csv'
[../]
[h]
type = AverageElementSize
outputs = 'console csv'
[]
[]
(test/tests/fvkernels/fv_simple_diffusion/3d_dirichlet.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 2
ny = 2
nz = 2
[]
[Variables]
[v]
family = MONOMIAL
order = CONSTANT
fv = true
[]
[]
[FVKernels]
[diff]
type = FVDiffusion
variable = v
coeff = coeff
[]
[]
[FVBCs]
[left]
type = FVDirichletBC
variable = v
boundary = left
value = 7
[]
[right]
type = FVDirichletBC
variable = v
boundary = right
value = 42
[]
[]
[Materials]
[diff]
type = ADGenericFunctorMaterial
prop_names = 'coeff'
prop_values = '1'
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/ray_tracing/test/tests/traceray/internal_sidesets/internal_sidesets_3d.i)
[Mesh]
[cmg]
type = CartesianMeshGenerator
dim = 3
dx = '2 2 2'
dy = '2 2 2'
dz = '2 2 2'
ix = '2 2 2'
iy = '2 2 2'
iz = '2 2 2'
subdomain_id = '0 0 0
0 1 0
0 0 0
0 2 0
3 7 4
0 5 0
0 0 0
0 6 0
0 0 0'
[]
[interior_back]
type = SideSetsBetweenSubdomainsGenerator
input = cmg
primary_block = 7
paired_block = 1
new_boundary = 'interior_back'
[]
[interior_bottom]
type = SideSetsBetweenSubdomainsGenerator
input = interior_back
primary_block = 7
paired_block = 2
new_boundary = 'interior_bottom'
[]
[interior_left]
type = SideSetsBetweenSubdomainsGenerator
input = interior_bottom
primary_block = 7
paired_block = 3
new_boundary = 'interior_left'
[]
[interior_right]
type = SideSetsBetweenSubdomainsGenerator
input = interior_left
primary_block = 7
paired_block = 4
new_boundary = 'interior_right'
[]
[interior_top]
type = SideSetsBetweenSubdomainsGenerator
input = interior_right
primary_block = 7
paired_block = 5
new_boundary = 'interior_top'
[]
[interior_front]
type = SideSetsBetweenSubdomainsGenerator
input = interior_top
primary_block = 7
paired_block = 6
new_boundary = 'interior_front'
[]
[]
[RayBCs]
active = 'kill_internal'
# active = 'kill_external reflect_internal'
# for testing internal kill
[kill_internal]
type = KillRayBC
boundary = 'interior_top interior_right interior_bottom interior_left interior_front interior_back'
[]
# for testing internal reflect
[kill_external]
type = KillRayBC
boundary = 'top right bottom left front back'
[]
[reflect_internal]
type = ReflectRayBC
boundary = 'interior_top interior_right interior_bottom interior_left interior_front interior_back'
[]
[]
[UserObjects/study]
type = RepeatableRayStudy
start_points = '0 0 0
2 2 2
6 6 6
4 4 4
0 2.5 2.5
3 3 6
2.5 0 0
3 3 3
2.5 2.5 2.5'
directions = '1 1 1
1 1 1
-1 -1 -1
-1 -1 -1
1 0.1 0
0 0 -1
0 1 1
1 1 1
0.5 1.5 1.5'
names = 'to_bottom_left_corner
at_bottom_left_corner
to_top_right_corner
at_top_right_corner
centroid_offset
top_down
left_to_edge
inside_to_corner
inside_offset'
execute_on = initial
ray_distance = 10
ray_kernel_coverage_check = false
use_internal_sidesets = true
[]
[Postprocessors/total_distance]
type = RayTracingStudyResult
study = study
result = total_distance
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Outputs]
exodus = false
csv = true
[]
(test/tests/controls/moose_base_naming_access/base_param.i)
[Mesh]
type = GeneratedMesh
dim = 2
elem_type = QUAD4
# use odd numbers so points do not fall on element boundaries
nx = 31
ny = 31
[]
[Variables]
[./diffused]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = diffused
[../]
[]
[DiracKernels]
[./test_object]
type = MaterialPointSource
point = '0.5 0.5 0'
variable = diffused
[../]
[]
[BCs]
[./bottom_diffused]
type = DirichletBC
variable = diffused
boundary = 'bottom'
value = 2
[../]
[./top_diffused]
type = DirichletBC
variable = diffused
boundary = 'top'
value = 0
[../]
[]
[Materials]
[./mat]
type = GenericConstantMaterial
prop_names = 'matp'
prop_values = '1'
block = 0
[../]
[]
[Postprocessors]
[./test_object]
type = FunctionValuePostprocessor
function = '2*(x+y)'
point = '0.5 0.5 0'
[../]
[./other_point_test_object]
type = FunctionValuePostprocessor
function = '3*(x+y)'
point = '0.5 0.5 0'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
[Controls]
[./point_control]
type = TestControl
test_type = 'point'
parameter = 'Postprocessor::*/point'
execute_on = 'initial'
[../]
[]
(test/tests/mesh_modifiers/transform/rotate_and_scale.i)
[Mesh]
[file]
type = FileMeshGenerator
file = cylinder.e
[]
[rotate]
type = TransformGenerator
input = file
transform = ROTATE
vector_value = '0 90 0'
[]
[scale]
type = TransformGenerator
input = rotate
transform = SCALE
vector_value = '1e2 1e2 1e2'
[]
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(modules/reactor/test/tests/meshgenerators/subdomain_extra_element_id_generator/subdomain_elem_ids_test.i)
[Mesh]
[gmg]
type = CartesianMeshGenerator
dim = 2
dx = 1
ix = 10
dy = '0.2 0.2 0.2 0.2 0.2'
iy = '2 2 2 2 2'
subdomain_id = '0 1 2 3 4'
[]
[give_subdomain_name]
type = RenameBlockGenerator
input = gmg
old_block = '1 3'
new_block = 'sub1 sub3'
[]
[subdomain_ids]
type = SubdomainExtraElementIDGenerator
input = give_subdomain_name
subdomains = '0 sub1 2 sub3'
extra_element_id_names = 'test_id1 test_id2 test_id3'
extra_element_ids = '
1 3 5 4;
2 9 10 11;
0 8 1 2
'
default_extra_element_ids = '-1 0 0'
[]
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[AuxVariables]
[test_id1]
family = MONOMIAL
order = CONSTANT
[]
[test_id2]
family = MONOMIAL
order = CONSTANT
[]
[test_id3]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[test_id1]
type = ExtraElementIDAux
variable = test_id1
extra_id_name = test_id1
[]
[test_id2]
type = ExtraElementIDAux
variable = test_id2
extra_id_name = test_id2
[]
[test_id3]
type = ExtraElementIDAux
variable = test_id3
extra_id_name = test_id3
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/lagrangian/updated/stabilization/cook_large.i)
[GlobalParams]
displacements = 'disp_x disp_y'
large_kinematics = true
stabilize_strain = true
[]
[Mesh]
type = FileMesh
file = cook_mesh.exo
dim = 2
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[]
[Kernels]
[sdx]
type = UpdatedLagrangianStressDivergence
variable = disp_x
component = 0
use_displaced_mesh = true
[]
[sdy]
type = UpdatedLagrangianStressDivergence
variable = disp_y
component = 1
use_displaced_mesh = true
[]
[]
[AuxVariables]
[strain_xx]
order = CONSTANT
family = MONOMIAL
[]
[strain_yy]
order = CONSTANT
family = MONOMIAL
[]
[strain_zz]
order = CONSTANT
family = MONOMIAL
[]
[strain_xy]
order = CONSTANT
family = MONOMIAL
[]
[strain_xz]
order = CONSTANT
family = MONOMIAL
[]
[strain_yz]
order = CONSTANT
family = MONOMIAL
[]
[stress_xx]
order = CONSTANT
family = MONOMIAL
[]
[stress_yy]
order = CONSTANT
family = MONOMIAL
[]
[stress_zz]
order = CONSTANT
family = MONOMIAL
[]
[stress_xy]
order = CONSTANT
family = MONOMIAL
[]
[stress_yz]
order = CONSTANT
family = MONOMIAL
[]
[stress_xz]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[stress_xx]
type = RankTwoAux
rank_two_tensor = cauchy_stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[]
[stress_yy]
type = RankTwoAux
rank_two_tensor = cauchy_stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[]
[stress_zz]
type = RankTwoAux
rank_two_tensor = cauchy_stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[]
[stress_xy]
type = RankTwoAux
rank_two_tensor = cauchy_stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[]
[stress_xz]
type = RankTwoAux
rank_two_tensor = cauchy_stress
variable = stress_xz
index_i = 0
index_j = 2
execute_on = timestep_end
[]
[stress_yz]
type = RankTwoAux
rank_two_tensor = cauchy_stress
variable = stress_yz
index_i = 1
index_j = 2
execute_on = timestep_end
[]
[strain_xx]
type = RankTwoAux
rank_two_tensor = mechanical_strain
variable = strain_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[]
[strain_yy]
type = RankTwoAux
rank_two_tensor = mechanical_strain
variable = strain_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[]
[strain_zz]
type = RankTwoAux
rank_two_tensor = mechanical_strain
variable = strain_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[]
[strain_xy]
type = RankTwoAux
rank_two_tensor = mechanical_strain
variable = strain_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[]
[strain_xz]
type = RankTwoAux
rank_two_tensor = mechanical_strain
variable = strain_xz
index_i = 0
index_j = 2
execute_on = timestep_end
[]
[strain_yz]
type = RankTwoAux
rank_two_tensor = mechanical_strain
variable = strain_yz
index_i = 1
index_j = 2
execute_on = timestep_end
[]
[]
[BCs]
[fixed_x]
type = DirichletBC
preset = true
variable = disp_x
boundary = canti
value = 0.0
[]
[fixed_y]
type = DirichletBC
preset = true
variable = disp_y
boundary = canti
value = 0.0
[]
[pull]
type = NeumannBC
variable = disp_y
boundary = loading
value = 0.1
[]
[]
[Materials]
[compute_stress]
type = ComputeNeoHookeanStress
lambda = 416666611.0991259
mu = 8300.33333888888926
[]
[compute_strain]
type = ComputeLagrangianStrain
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = 'newton'
line_search = 'none'
petsc_options_iname = -pc_type
petsc_options_value = lu
nl_max_its = 500
nl_abs_tol = 1e-5
nl_rel_tol = 1e-6
[]
[Postprocessors]
[value]
type = PointValue
variable = disp_y
point = '48 60 0'
use_displaced_mesh = false
[]
[]
[Outputs]
exodus = false
csv = true
[]
(tutorials/darcy_thermo_mech/step04_velocity_aux/problems/step4.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 100
ny = 10
xmax = 0.304 # Length of test chamber
ymax = 0.0257 # Test chamber radius
[]
[Variables/pressure]
[]
[AuxVariables]
[velocity]
order = CONSTANT
family = MONOMIAL_VEC
[]
[]
[Kernels]
[darcy_pressure]
type = DarcyPressure
variable = pressure
[]
[]
[AuxKernels]
[velocity]
type = DarcyVelocity
variable = velocity
execute_on = timestep_end
pressure = pressure
[]
[]
[BCs]
[inlet]
type = DirichletBC
variable = pressure
boundary = left
value = 4000 # (Pa) From Figure 2 from paper. First data point for 1mm spheres.
[]
[outlet]
type = DirichletBC
variable = pressure
boundary = right
value = 0 # (Pa) Gives the correct pressure drop from Figure 2 for 1mm spheres
[]
[]
[Materials]
[column]
type = PackedColumn
radius = 1
[]
[]
[Problem]
type = FEProblem
coord_type = RZ
rz_coord_axis = X
[]
[Executioner]
type = Steady
solve_type = PJFNK
#nl_rel_tol = 1e-12
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/error/none_reserved.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[./none]
type = Exodus
[../]
[]
(test/tests/ics/constant_ic/constant_ic_test.i)
###########################################################
# This is a simple test demonstrating the use of the
# user-defined initial condition system.
#
# @Requirement F3.20
# @Requirement F5.20
###########################################################
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
# Initial Condition on Nonlinear variable
[./InitialCondition]
type = ConstantIC
value = 6.2
[../]
[../]
[]
[AuxVariables]
active = 'u_aux'
[./u_aux]
order = FIRST
family = LAGRANGE
# Initial Condition on Auxiliary variable
[./InitialCondition]
type = ConstantIC
value = 9.3
[../]
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
nl_rel_tol = 1e-10
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/multiapps/initial_failure/sub.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Problem]
type = FailingProblem
# time_step is set to two if there is no AMR by Steady at the end of its execute.
fail_step = 1
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/csv/csv.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[AuxVariables]
[./aux0]
order = SECOND
family = SCALAR
[../]
[./aux1]
family = SCALAR
initial_condition = 5
[../]
[./aux2]
family = SCALAR
initial_condition = 10
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./diff_v]
type = CoefDiffusion
variable = v
coef = 2
[../]
[]
[BCs]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[./left_u]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = right
value = 3
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = left
value = 2
[../]
[]
[Postprocessors]
[./num_vars]
type = NumVars
system = 'NL'
[../]
[./num_aux]
type = NumVars
system = 'AUX'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
csv = true
[]
[ICs]
[./aux0_IC]
variable = aux0
values = '12 13'
type = ScalarComponentIC
[../]
[]
(test/tests/bcs/ad_bc_preset_nodal/bc_function_preset.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
nz = 0
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
[./left]
type = ParsedFunction
value = 'y'
[../]
[./right]
type = ParsedFunction
value = '1+y'
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = ADDiffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = ADFunctionDirichletBC
variable = u
boundary = 3
function = left
[../]
[./right]
type = ADFunctionDirichletBC
variable = u
boundary = 1
function = right
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = bc_func_out
exodus = true
[]
(test/tests/vectorpostprocessors/late_declaration_vector_postprocessor/late_declaration_vector_postprocessor.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[VectorPostprocessors]
[./constant]
type = LateDeclarationVectorPostprocessor
value = '1.5 2.7'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'initial timestep_end'
csv = true
[]
(test/tests/meshgenerators/plane_id_mesh_generator/plane_id_pin3d.i)
[Mesh]
[pin2d]
type = ConcentricCircleMeshGenerator
num_sectors = 2
radii = '0.4 0.5'
rings = '1 1 1'
has_outer_square = on
pitch = 1.26
preserve_volumes = yes
smoothing_max_it = 3
[]
[pin3d]
type = FancyExtruderGenerator
input = 'pin2d'
heights = '5.0 5.0 5.0'
direction = '0 0 1'
num_layers = '2 2 2'
[]
[pin3d_id]
type = PlaneIDMeshGenerator
input = 'pin3d'
plane_coordinates = '0.0 5.0 10.0 15.0'
num_ids_per_plane = ' 1 2 1'
plane_axis = 'z'
id_name = 'plane_id'
[]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[AuxVariables]
[plane_id]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[set_plane_id]
type = ExtraElementIDAux
variable = plane_id
extra_id_name = plane_id
[]
[]
[Outputs]
exodus = true
execute_on = timestep_end
[]
(test/tests/kernels/ad_max_dofs_per_elem_error/ad_max_dofs_per_elem.i)
[Mesh]
type = GeneratedMesh
elem_type = HEX27
dim = 3
[]
[Variables]
[u]
order = SECOND
[]
[v]
order = SECOND
[]
[]
[Kernels]
[u_diff]
type = ADDiffusion
variable = u
[]
[v_diff]
type = ADDiffusion
variable = v
[]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
[]
(test/tests/auxkernels/element_aux_var/element_aux_var_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
[]
[]
[AuxVariables]
[one]
order = CONSTANT
family = MONOMIAL
[]
[five]
order = FIRST
family = LAGRANGE
[]
[three]
order = CONSTANT
family = MONOMIAL
[]
[coupled_nine]
order = CONSTANT
family = MONOMIAL
[]
[coupled_fifteen]
order = CONSTANT
family = MONOMIAL
[]
[coupled]
order = CONSTANT
family = MONOMIAL
[]
[coupled_nl]
order = CONSTANT
family = MONOMIAL
[]
[coupled_grad_nl]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
# Coupling of nonlinear to Aux
[diff]
type = Diffusion
variable = u
[]
[force]
type = CoupledForce
variable = u
v = one
[]
[]
[AuxKernels]
# Simple Aux Kernel
# Shows coupling of Element to Nodal
# Shows coupling of Element to non-linear
# Shows coupling of Element to non-linear grad
[constant]
variable = one
type = ConstantAux
value = 1
[]
[coupled_nine]
variable = coupled_nine
type = CoupledAux
value = 3
operator = *
coupled = three
[]
[coupled_three]
variable = three
type = CoupledAux
value = 2
operator = +
coupled = one
[]
[coupled_fifteen]
variable = coupled_fifteen
type = CoupledAux
value = 5
operator = *
coupled = three
[]
[coupled]
variable = coupled
type = CoupledAux
value = 2
coupled = five
[]
[coupled_nl]
variable = coupled_nl
type = CoupledAux
value = 2
coupled = u
[]
[coupled_grad_nl]
variable = coupled_grad_nl
type = CoupledGradAux
grad = '2 0 0'
coupled = u
[]
[five]
type = ConstantAux
variable = five
boundary = '3 1'
value = 5
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
[exodus]
type = Exodus
elemental_as_nodal = true
[]
[]
(modules/porous_flow/test/tests/flux_limited_TVD_pflow/except02.i)
# Exception test: fluid_component number too big
[Mesh]
type = GeneratedMesh
dim = 1
[]
[GlobalParams]
gravity = '1 2 3'
PorousFlowDictator = dictator
[]
[Variables]
[pp]
[]
[tracer]
[]
[]
[Modules]
[FluidProperties]
[the_simple_fluid]
type = SimpleFluidProperties
[]
[]
[]
[PorousFlowUnsaturated]
porepressure = pp
mass_fraction_vars = tracer
fp = the_simple_fluid
[]
[UserObjects]
[advective_flux_calculator]
type = PorousFlowAdvectiveFluxCalculatorSaturatedMultiComponent
fluid_component = 2
[]
[]
[Materials]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1 0 0 0 2 0 0 0 3'
[]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
(test/tests/postprocessors/geometry/3d_geometry.i)
radius = 0.5
inner_box_length = 2.2
outer_box_length = 3
depth = 0.4
sides = 28
alpha = ${fparse 2 * pi / ${sides}}
perimeter_correction = ${fparse ${alpha} / 2 / sin(alpha / 2)}
area_correction = ${fparse alpha / sin(alpha)}
[Mesh]
file = 3d.e
construct_side_list_from_node_list = true
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[./circle_side_area]
type = AreaPostprocessor
boundary = circle_side
[../]
[./inside_side_area]
type = AreaPostprocessor
boundary = inside_side
[../]
[./outside_side_area]
type = AreaPostprocessor
boundary = outside_side
[../]
[./circle_volume]
type = VolumePostprocessor
block = circle
[../]
[./inside_volume]
type = VolumePostprocessor
block = inside
[../]
[./outside_volume]
type = VolumePostprocessor
block = outside
[../]
[./total_volume]
type = VolumePostprocessor
block = 'circle inside outside'
[../]
[./circle_side_area_exact]
type = FunctionValuePostprocessor
function = 'circle_side_area_exact'
[../]
[./inside_side_area_exact]
type = FunctionValuePostprocessor
function = 'inside_side_area_exact'
[../]
[./outside_side_area_exact]
type = FunctionValuePostprocessor
function = 'outside_side_area_exact'
[../]
[./circle_volume_exact]
type = FunctionValuePostprocessor
function = 'circle_volume_exact'
[../]
[./inside_volume_exact]
type = FunctionValuePostprocessor
function = 'inside_volume_exact'
[../]
[./outside_volume_exact]
type = FunctionValuePostprocessor
function = 'outside_volume_exact'
[../]
[./total_volume_exact]
type = FunctionValuePostprocessor
function = 'total_volume_exact'
[../]
[]
[Functions]
[./circle_side_area_exact]
type = ParsedFunction
value = '2 * pi * ${radius} / ${perimeter_correction} * ${depth}'
[../]
[./inside_side_area_exact]
type = ParsedFunction
value = '${inner_box_length} * ${depth} * 4'
[../]
[./outside_side_area_exact]
type = ParsedFunction
value = '${outer_box_length} * ${depth} * 4'
[../]
[./circle_volume_exact]
type = ParsedFunction
value = 'pi * ${radius}^2 * ${depth} / ${area_correction}'
[../]
[./inside_volume_exact]
type = ParsedFunction
value = '${inner_box_length}^2 * ${depth} - pi * ${radius}^2 * ${depth} / ${area_correction}'
[../]
[./outside_volume_exact]
type = ParsedFunction
value = '${outer_box_length}^2 * ${depth} - ${inner_box_length}^2 * ${depth}'
[../]
[./total_volume_exact]
type = ParsedFunction
value = '${outer_box_length}^2 * ${depth}'
[../]
[]
[Outputs]
csv = true
[]
(test/tests/vectorpostprocessors/distributed/input.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[VectorPostprocessors/test]
type = TestDistributedVectorPostprocessor
parallel_type = replicated
[]
[Outputs]
[out]
type = CSV
execute_on = TIMESTEP_END
[]
[]
(test/tests/bcs/nodal_normals/circle_quads.i)
[Mesh]
file = circle-quads.e
[]
[Functions]
[./all_bc_fn]
type = ParsedFunction
value = x*x+y*y
[../]
[./f_fn]
type = ParsedFunction
value = -4
[../]
[./analytical_normal_x]
type = ParsedFunction
value = x
[../]
[./analytical_normal_y]
type = ParsedFunction
value = y
[../]
[]
[NodalNormals]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = f_fn
[../]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
boundary = '1'
function = 'all_bc_fn'
[../]
[]
[Postprocessors]
[./nx_pps]
type = NodalL2Error
variable = nodal_normal_x
boundary = '1'
function = analytical_normal_x
[../]
[./ny_pps]
type = NodalL2Error
variable = nodal_normal_y
boundary = '1'
function = analytical_normal_y
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
nl_rel_tol = 1e-13
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(test/tests/dirackernels/point_caching/point_caching_error.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
elem_type = QUAD4
uniform_refine = 4
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[DiracKernels]
active = 'point_source'
[./point_source]
type = BadCachingPointSource
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/fvkernels/fv_simple_diffusion/fv_only.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
[]
[Variables]
[v]
family = MONOMIAL
order = CONSTANT
fv = true
[]
[]
[FVKernels]
[diff]
type = FVDiffusion
variable = v
coeff = coeff
[]
[]
[FVBCs]
[left]
type = FVDirichletBC
variable = v
boundary = left
value = 7
[]
[right]
type = FVDirichletBC
variable = v
boundary = right
value = 42
[]
[]
[Materials]
[diff]
type = ADGenericFunctorMaterial
prop_names = 'coeff'
prop_values = '1'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/postprocessors/side_integral/side_integral_functor.i)
[Mesh]
inactive = 'refine'
# U-shaped domains to have internal boundaries in
# a variety of directions
[cmg]
type = CartesianMeshGenerator
dim = 2
dx = '1 1 1'
dy = '3 1'
ix = '4 5 3'
iy = '12 4'
subdomain_id = '1 2 1
1 1 1'
[]
[internal_boundary_dir1]
type = SideSetsBetweenSubdomainsGenerator
input = cmg
primary_block = 1
paired_block = 2
new_boundary = 'inside_1'
[]
[internal_boundary_dir2]
type = SideSetsBetweenSubdomainsGenerator
input = internal_boundary_dir1
primary_block = 2
paired_block = 1
new_boundary = 'inside_2'
[]
[refine]
type = RefineBlockGenerator
input = internal_boundary_dir2
block = '1 2'
refinement = '2 1'
[]
[]
[Variables]
[u]
type = MooseVariableFVReal
block = 1
[]
[]
[AuxVariables]
[v1]
type = MooseVariableFVReal
block = 1
[InitialCondition]
type = FunctionIC
function = 'x + y'
[]
[]
[v2]
type = MooseVariableFVReal
block = 2
[InitialCondition]
type = FunctionIC
function = '2*x*x - y'
[]
[]
[]
[Functions]
[f1]
type = ADParsedFunction
value = 'exp(x - y)'
[]
[]
[Materials]
[m1]
type = ADGenericFunctorMaterial
prop_names = 'm1'
prop_values = 'f1'
[]
[m2]
type = ADPiecewiseByBlockFunctorMaterial
prop_name = 'm2'
subdomain_to_prop_value = '1 12
2 4'
[]
[]
[FVKernels]
[diff]
type = FVDiffusion
variable = u
coeff = '1'
[]
[]
[FVBCs]
[left]
type = FVDirichletBC
variable = u
boundary = 3
value = 0
[]
[right]
type = FVDirichletBC
variable = u
boundary = 1
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Postprocessors]
# Mesh external boundaries integration
[ext_u]
type = ADSideIntegralFunctorPostprocessor
boundary = 'left top right'
functor = u
restrict_to_functors_domain = true
[]
[ext_v1]
type = ADSideIntegralFunctorPostprocessor
boundary = 'left right'
functor = v1
[]
[ext_v2]
type = ADSideIntegralFunctorPostprocessor
boundary = 'top'
functor = v2
restrict_to_functors_domain = true
[]
[ext_f1]
type = ADSideIntegralFunctorPostprocessor
boundary = 'left top right'
functor = f1
prefactor = f1
[]
[ext_m1]
type = ADSideIntegralFunctorPostprocessor
boundary = 'left top right'
functor = m1
restrict_to_functors_domain = true
[]
[ext_m2]
type = ADSideIntegralFunctorPostprocessor
boundary = 'left top right'
functor = m2
restrict_to_functors_domain = true
[]
# Internal to the mesh, but a side to the variables
# With orientation of normal 1->2
[int_s1_u]
type = ADSideIntegralFunctorPostprocessor
boundary = inside_1
functor = u
[]
[int_s1_v1]
type = ADSideIntegralFunctorPostprocessor
boundary = inside_1
functor = v1
[]
[int_s1_f1]
type = ADSideIntegralFunctorPostprocessor
boundary = inside_1
functor = f1
[]
[int_s1_m1]
type = ADSideIntegralFunctorPostprocessor
boundary = inside_1
functor = m1
[]
[int_s1_m2]
type = ADSideIntegralFunctorPostprocessor
boundary = inside_1
functor = m2
[]
# With orientation of normal 2->1
[int_s2_v2]
type = ADSideIntegralFunctorPostprocessor
boundary = inside_2
functor = v2
[]
[int_s2_f1]
type = ADSideIntegralFunctorPostprocessor
boundary = inside_2
functor = f1
[]
[int_s2_m1]
type = ADSideIntegralFunctorPostprocessor
boundary = inside_2
functor = m1
[]
[int_s2_m2]
type = ADSideIntegralFunctorPostprocessor
boundary = inside_2
functor = m2
[]
[]
[Outputs]
csv = true
exodus = true
[]
[Problem]
kernel_coverage_check = false
[]
(modules/porous_flow/test/tests/gravity/fully_saturated_upwinded_nodens_grav01c_action.i)
# Checking that gravity head is established
# 1phase, 2-component, constant fluid-bulk, constant viscosity, constant permeability
# fully saturated with fully-saturated Kernel with upwinding
# For better agreement with the analytical solution (ana_pp), just increase nx
# This is the Action version of fully_saturated_upwinded_grav01c.i but with multiply_by_density=false
# NOTE: this test is numerically delicate because the steady-state configuration is independent of the mass fraction, so the frac variable can assume any value as long as mass-fraction is conserved
[Mesh]
type = GeneratedMesh
dim = 1
nx = 100
xmin = -1
xmax = 0
[]
[Variables]
[pp]
[InitialCondition]
type = RandomIC
min = 0
max = 1
[]
[]
[frac]
[InitialCondition]
type = RandomIC
min = 0
max = 1
[]
[]
[]
[PorousFlowFullySaturated]
porepressure = pp
mass_fraction_vars = frac
fp = simple_fluid
gravity = '-1 0 0'
multiply_by_density = false
[]
[Functions]
[ana_pp]
type = ParsedFunction
vars = 'g B p0 rho0'
vals = '1 1.2 0 1'
value = '-B*log(exp(-p0/B)+g*rho0*x/B)' # expected pp at base
[]
[]
[BCs]
[z]
type = DirichletBC
variable = pp
boundary = right
value = 0
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 1.2
density0 = 1
viscosity = 1
thermal_expansion = 0
[]
[]
[]
[Materials]
[permeability]
type = PorousFlowPermeabilityConst
PorousFlowDictator = dictator
permeability = '1 0 0 0 2 0 0 0 3'
[]
[]
[Postprocessors]
[pp_base]
type = PointValue
variable = pp
point = '-1 0 0'
[]
[pp_analytical]
type = FunctionValuePostprocessor
function = ana_pp
point = '-1 0 0'
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = Newton
nl_rel_tol = 1E-12
petsc_options_iname = '-pc_factor_shift_type'
petsc_options_value = 'NONZERO'
nl_max_its = 100
[]
[Outputs]
csv = true
[]
(test/tests/functions/parsed/function.i)
[Mesh]
type = GeneratedMesh
dim = 1
xmin = -1
xmax = 1
nx = 20
[]
[AuxVariables]
[f]
[]
[]
[AuxKernels]
[function_aux]
type = FunctionAux
variable = f
function = fn
execute_on = initial
[../]
[]
[Functions]
[sin_fn]
type = ParsedFunction
value = sin(x)
[]
[cos_fn]
type = ParsedFunction
value = cos(x)
[]
[fn]
type = ParsedFunction
value = 's/c'
vars = 's c'
vals = 'sin_fn cos_fn'
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
show = f
exodus = true
[]
(test/tests/misc/check_error/missing_req_par_moose_obj_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
# Test missing required param (type in this case)
[./diff]
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/mesh_modifiers/mesh_extruder/extruder_quad.i)
[Mesh]
[file]
type = FileMeshGenerator
file = chimney_quad.e
[]
[extrude]
type = MeshExtruderGenerator
input = file
num_layers = 20
extrusion_vector = '0 1e-2 0'
bottom_sideset = 'new_bottom'
top_sideset = 'new_top'
[]
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[bottom]
type = DirichletBC
variable = u
boundary = 'new_bottom'
value = 0
[]
[top]
type = DirichletBC
variable = u
boundary = 'new_top'
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out_quad
exodus = true
[]
(test/tests/bcs/nodal_normals/cylinder_hexes_1st_2nd.i)
# First order normals on second order mesh
[Mesh]
file = cylinder-hexes-2nd.e
[]
[Functions]
[./all_bc_fn]
type = ParsedFunction
value = x*x+y*y
[../]
[./f_fn]
type = ParsedFunction
value = -4
[../]
[]
[NodalNormals]
boundary = '1'
corner_boundary = 100
order = FIRST
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = f_fn
[../]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
boundary = '1'
function = 'all_bc_fn'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
nl_rel_tol = 1e-13
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(test/tests/vectorpostprocessors/elements_along_line/1d.i)
[Mesh]
type = GeneratedMesh
parallel_type = replicated # Until RayTracing.C is fixed
dim = 1
nx = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[VectorPostprocessors]
[./elems]
type = ElementsAlongLine
start = '0.05 0 0'
end = '0.405 0 0'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
csv = true
[]
(test/tests/postprocessors/element_variable_value/elemental_variable_value_fv.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 1
ymax = 0.1
[]
[Variables]
[./u]
family = MONOMIAL
order = CONSTANT
fv = true
[../]
[]
[FVKernels]
[./diff]
type = FVDiffusion
variable = u
coeff = 0.1
[../]
[]
[FVBCs]
[./left]
type = FVDirichletBC
variable = u
boundary = left
value = 1
[../]
[./right]
type = FVDirichletBC
variable = u
boundary = right
value = 10
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Postprocessors]
[./elem_left]
type = ElementalVariableValue
variable = u
elementid = 0
[]
[./elem_right]
type = ElementalVariableValue
variable = u
elementid = 9
[]
[]
[Outputs]
csv = true
[]
(test/tests/preconditioners/vcp/vcp_test.i)
[Mesh]
[original_file_mesh]
type = FileMeshGenerator
file = non_conform_2blocks.e
[]
[secondary_side]
input = original_file_mesh
type = LowerDBlockFromSidesetGenerator
sidesets = '10'
new_block_id = '100'
new_block_name = 'secondary_side'
[]
[primary_side]
input = secondary_side
type = LowerDBlockFromSidesetGenerator
sidesets = '20'
new_block_id = '200'
new_block_name = 'primary_side'
[]
[]
[Functions]
[exact_sln]
type = ParsedFunction
value = sin(2*pi*x)*sin(2*pi*y)
[]
[ffn]
type = ParsedFunction
value = 8*pi*pi*sin(2*pi*x)*sin(2*pi*y)
[]
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[lm]
order = FIRST
family = LAGRANGE
block = secondary_side
use_dual = true
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[ffn]
type = BodyForce
variable = u
function = ffn
[]
[]
[Constraints]
[ced]
type = EqualValueConstraint
variable = lm
secondary_variable = u
primary_boundary = 20
primary_subdomain = 200
secondary_boundary = 10
secondary_subdomain = 100
[]
[]
[BCs]
[all]
type = DirichletBC
variable = u
boundary = '30 40'
value = 0.0
[]
[neumann]
type = FunctionGradientNeumannBC
exact_solution = exact_sln
variable = u
boundary = '50 60'
[]
[]
[Postprocessors]
[l2_error]
type = ElementL2Error
variable = u
function = exact_sln
block = '1 2'
execute_on = 'initial timestep_end'
[]
[]
[Preconditioning]
[vcp]
type = VCP
full = true
lm_variable = 'lm'
primary_variable = 'u'
preconditioner = 'AMG'
is_lm_coupling_diagonal = true
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options = '-snes_converged_reason -ksp_converged_reason -snes_view'
l_max_its = 100
nl_rel_tol = 1e-6
[]
[Outputs]
csv = true
[]
(test/tests/kernels/material_derivatives/material_derivatives_test.i)
###########################################################
# This is a test of the material derivatives test kernel.
###########################################################
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[./v]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
[./u_IC_fn]
type = ParsedFunction
value = 'x'
[../]
[./v_IC_fn]
type = ParsedFunction
value = 'sin(x)'
[../]
[]
[ICs]
[./u_IC]
type = FunctionIC
variable = u
function = u_IC_fn
[../]
[./v_IC]
type = FunctionIC
variable = v
function = v_IC_fn
[../]
[]
[Kernels]
[./test_kernel]
type = MaterialDerivativeTestKernel
variable = u
args = 'u v'
material_property = material_derivative_test_property
[../]
# add a dummy kernel for v to prevent singular Jacobian
[./dummy_kernel]
type = Diffusion
variable = v
[../]
[]
[Materials]
[./material_derivative_test_material]
type = MaterialDerivativeTestMaterial
var1 = u
var2 = v
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
solve_type = newton
petsc_options_iname = '-snes_type -snes_test_err'
petsc_options_value = 'test 1e-10'
[../]
[]
[Executioner]
type = Steady
[]
(test/tests/vectorpostprocessors/point_value_sampler/point_value_sampler_fv.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
family = MONOMIAL
order = CONSTANT
fv = true
[../]
[./v]
family = MONOMIAL
order = CONSTANT
fv = true
[../]
[]
[FVKernels]
[./diff]
type = FVDiffusion
variable = u
coeff = 1
[../]
[./diff_v]
type = FVDiffusion
variable = v
coeff = 1
[../]
[]
[FVBCs]
[./left]
type = FVDirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = FVDirichletBC
variable = u
boundary = right
value = 1
[../]
[./left_v]
type = FVDirichletBC
variable = v
boundary = left
value = 1
[../]
[./right_v]
type = FVDirichletBC
variable = v
boundary = right
value = 0
[../]
[]
[VectorPostprocessors]
[./point_sample]
type = PointValueSampler
warn_discontinuous_face_values = false
variable = 'u v'
points = '0.09 0.09 0 0.23 0.4 0 0.78 0.2 0'
sort_by = x
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
csv = true
[]
(test/tests/fvkernels/orthogonal-diffusion/orthogonal-diffusion.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 32
ny = 32
[]
[]
[Variables]
[u]
type = MooseVariableFVReal
[]
[]
[FVKernels]
[diff]
type = FVOrthogonalDiffusion
variable = u
coeff = 1
[]
[]
[FVBCs]
[left]
type = FVOrthogonalBoundaryDiffusion
boundary = 'top'
variable = u
function = 0
coeff = 1
[]
[right]
type = FVOrthogonalBoundaryDiffusion
boundary = 'bottom'
variable = u
function = 1
coeff = 1
[]
[]
[Executioner]
solve_type = NEWTON
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/variables/fe_hermite/hermite-3-1d.i)
###########################################################
# This is a simple test demonstrating the use of the
# Hermite variable type.
#
# @Requirement F3.10
###########################################################
[Mesh]
type = GeneratedMesh
dim = 1
xmin = -1
xmax = 1
nx = 5
elem_type = EDGE3
[]
[Functions]
[./bc_fnl]
type = ParsedFunction
value = -3*x*x
[../]
[./bc_fnr]
type = ParsedFunction
value = 3*x*x
[../]
[./forcing_fn]
type = ParsedFunction
value = -6*x+(x*x*x)
[../]
[./solution]
type = ParsedGradFunction
value = x*x*x
grad_x = 3*x*x
[../]
[]
# Hermite Variable type
[Variables]
[./u]
order = THIRD
family = HERMITE
[../]
[]
[Kernels]
active = 'diff forcing reaction'
[./diff]
type = Diffusion
variable = u
[../]
[./reaction]
type = Reaction
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
[./bc_left]
type = FunctionNeumannBC
variable = u
boundary = 'left'
function = bc_fnl
[../]
[./bc_right]
type = FunctionNeumannBC
variable = u
boundary = 'right'
function = bc_fnr
[../]
[]
[Postprocessors]
[./dofs]
type = NumDOFs
[../]
[./h]
type = AverageElementSize
[../]
[./L2error]
type = ElementL2Error
variable = u
function = solution
[../]
[./H1error]
type = ElementH1Error
variable = u
function = solution
[../]
[./H1Semierror]
type = ElementH1SemiError
variable = u
function = solution
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
csv = true
[]
(modules/reactor/test/tests/meshgenerators/tri_pin_hex_assemby_generator/tri_pin.i)
[Mesh]
[assm_up]
type = TriPinHexAssemblyGenerator
ring_radii = '7 8;5 6; '
ring_intervals = '2 1;1 1; '
ring_block_ids = '200 400 600;700 800; '
background_block_ids = '30 40'
num_sectors_per_side = 6
background_intervals = 2
hexagon_size = ${fparse 40.0/sqrt(3.0)}
ring_offset = 0.6
external_boundary_id = 200
external_boundary_name = 'surface'
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[AuxVariables]
[pin_id]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[set_pin_id]
type = ExtraElementIDAux
variable = pin_id
extra_id_name = pin_id
[]
[]
[Outputs]
exodus = true
execute_on = timestep_end
[]
(modules/richards/test/tests/jacobian_1/jn01.i)
# unsaturated = false
# gravity = false
# supg = false
# transient = false
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = -1
xmax = 1
ymin = -1
ymax = 1
zmin = -1
zmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0 # notice small quantity, so the PETSc constant state works
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1 # notice small quantity, so the PETSc constant state works
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.2
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGnone]
type = RichardsSUPGnone
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = RandomIC
block = 0
min = 0
max = 1
[../]
[../]
[]
[Kernels]
active = 'richardsf'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
richardsVarNames_UO = PPNames
variable = pressure
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGnone
sat_UO = Saturation
seff_UO = SeffVG
viscosity = 1E-3
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -snes_type'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000 test'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = jn01
exodus = false
[]
(test/tests/auxkernels/element_aux_var/block_global_depend_elem_aux.i)
[Mesh]
file = rectangle.e
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./coupled_left]
order = CONSTANT
family = MONOMIAL
block = 1
[../]
[./coupled_right]
order = CONSTANT
family = MONOMIAL
block = 2
[../]
[./two]
order = CONSTANT
family = MONOMIAL
initial_condition = 0
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./body_force]
type = BodyForce
variable = u
block = 1
value = 10
[../]
[]
[AuxKernels]
[./coupled_left]
variable = coupled_left
type = CoupledAux
value = 8
operator = /
coupled = two
[../]
[./coupled_right]
variable = coupled_right
type = CoupledAux
value = 8
operator = /
coupled = two
[../]
[./two]
type = ConstantAux
variable = two
value = 2
[../]
[]
[BCs]
active = 'right'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/auxkernels/solution_aux/aux_nonlinear_solution_adapt.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./u_aux]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./aux_kernel]
type = FunctionAux
function = x*y
variable = u_aux
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
nl_rel_tol = 1e-10
[]
[Adaptivity]
marker = error_frac
steps = 3
[./Indicators]
[./jump_indicator]
type = GradientJumpIndicator
variable = u
[../]
[../]
[./Markers]
[./error_frac]
type = ErrorFractionMarker
indicator = jump_indicator
refine = 0.7
[../]
[../]
[]
[Outputs]
xda = true
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_mortar/large_gap_heat_transfer_test_rz_cylinder_mortar.i)
rpv_core_gap_size = 0.2
core_outer_radius = 2
rpv_inner_radius = '${fparse 2 + rpv_core_gap_size}'
rpv_outer_radius = '${fparse 2.5 + rpv_core_gap_size}'
rpv_width = '${fparse rpv_outer_radius - rpv_inner_radius}'
rpv_outer_htc = 10 # W/m^2/K
rpv_outer_Tinf = 300 # K
core_blocks = '1'
rpv_blocks = '3'
[Mesh]
[gmg]
type = CartesianMeshGenerator
dim = 2
dx = '${core_outer_radius} ${rpv_core_gap_size} ${rpv_width}'
ix = '400 1 100'
dy = 1
iy = '5'
[]
[set_block_id1]
type = SubdomainBoundingBoxGenerator
input = gmg
bottom_left = '0 0 0'
top_right = '${core_outer_radius} 1 0'
block_id = 1
location = INSIDE
[]
[rename_core_bdy]
type = SideSetsBetweenSubdomainsGenerator
input = set_block_id1
primary_block = 1
paired_block = 0
new_boundary = 'core_outer'
[]
[set_block_id3]
type = SubdomainBoundingBoxGenerator
input = rename_core_bdy
bottom_left = '${rpv_inner_radius} 0 0'
top_right = '${rpv_outer_radius} 1 0'
block_id = 3
location = INSIDE
[]
[rename_inner_rpv_bdy]
type = SideSetsBetweenSubdomainsGenerator
input = set_block_id3
primary_block = 3
paired_block = 0
new_boundary = 'rpv_inner'
[]
# comment out for test without gap
[2d_mesh]
type = BlockDeletionGenerator
input = rename_inner_rpv_bdy
block = 0
[]
[secondary]
type = LowerDBlockFromSidesetGenerator
sidesets = 'rpv_inner'
new_block_id = 10001
new_block_name = 'secondary_lower'
input = 2d_mesh
[]
[primary]
type = LowerDBlockFromSidesetGenerator
sidesets = 'core_outer'
new_block_id = 10000
new_block_name = 'primary_lower'
input = secondary
[]
allow_renumbering = false
[]
[Problem]
coord_type = RZ
[]
[Variables]
[Tsolid]
initial_condition = 500
[]
[lm]
order = FIRST
family = LAGRANGE
block = 'secondary_lower'
[]
[]
[Kernels]
[heat_source]
type = CoupledForce
variable = Tsolid
block = '${core_blocks}'
v = power_density
[]
[heat_conduction]
type = HeatConduction
variable = Tsolid
[]
[]
[BCs]
[RPV_out_BC] # k \nabla T = h (T- T_inf) at RPV outer boundary
type = ConvectiveFluxFunction # (Robin BC)
variable = Tsolid
boundary = 'right' # outer RPV
coefficient = ${rpv_outer_htc}
T_infinity = ${rpv_outer_Tinf}
[]
[]
[UserObjects]
[radiation]
type = GapFluxModelRadiation
temperature = Tsolid
boundary = 'rpv_inner'
primary_emissivity = 0.8
secondary_emissivity = 0.8
[]
[conduction]
type = GapFluxModelConduction
temperature = Tsolid
boundary = 'rpv_inner'
gap_conductivity = 0.1
[]
[]
[Constraints]
[ced]
type = ModularGapConductanceConstraint
variable = lm
secondary_variable = Tsolid
primary_boundary = 'core_outer'
primary_subdomain = 10000
secondary_boundary = 'rpv_inner'
secondary_subdomain = 10001
gap_flux_models = 'radiation conduction'
gap_geometry_type = 'CYLINDER'
[]
[]
[AuxVariables]
[power_density]
block = '${core_blocks}'
initial_condition = 50e3
[]
[]
[Materials]
[simple_mat]
type = HeatConductionMaterial
thermal_conductivity = 34.6 # W/m/K
[]
[]
[Postprocessors]
[Tcore_avg]
type = ElementAverageValue
variable = Tsolid
block = '${core_blocks}'
[]
[Tcore_max]
type = ElementExtremeValue
value_type = max
variable = Tsolid
block = '${core_blocks}'
[]
[Tcore_min]
type = ElementExtremeValue
value_type = min
variable = Tsolid
block = '${core_blocks}'
[]
[Trpv_avg]
type = ElementAverageValue
variable = Tsolid
block = '${rpv_blocks}'
[]
[Trpv_max]
type = ElementExtremeValue
value_type = max
variable = Tsolid
block = '${rpv_blocks}'
[]
[Trpv_min]
type = ElementExtremeValue
value_type = min
variable = Tsolid
block = '${rpv_blocks}'
[]
[ptot]
type = ElementIntegralVariablePostprocessor
variable = power_density
block = '${core_blocks}'
[]
[rpv_convective_out]
type = ConvectiveHeatTransferSideIntegral
T_solid = Tsolid
boundary = 'right' # outer RVP
T_fluid = ${rpv_outer_Tinf}
htc = ${rpv_outer_htc}
[]
[heat_balance] # should be equal to 0 upon convergence
type = ParsedPostprocessor
function = '(rpv_convective_out - ptot) / ptot'
pp_names = 'rpv_convective_out ptot'
[]
[flux_from_core] # converges to ptot as the mesh is refined
type = SideDiffusiveFluxIntegral
variable = Tsolid
boundary = core_outer
diffusivity = thermal_conductivity
[]
[flux_into_rpv] # converges to rpv_convective_out as the mesh is refined
type = SideDiffusiveFluxIntegral
variable = Tsolid
boundary = rpv_inner
diffusivity = thermal_conductivity
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[VectorPostprocessors]
[NodalTemperature]
type = NodalValueSampler
sort_by = id
boundary = 'rpv_inner core_outer'
variable = Tsolid
[]
[]
[Executioner]
type = Steady
petsc_options = '-snes_converged_reason -pc_svd_monitor'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package -mat_mffd_err -pc_factor_shift_type '
'-pc_factor_shift_amount'
petsc_options_value = ' lu superlu_dist 1e-5 NONZERO '
'1e-15'
snesmf_reuse_base = false
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
l_max_its = 100
line_search = none
[]
[Outputs]
exodus = false
csv = true
[]
(modules/tensor_mechanics/test/tests/ad_isotropic_elasticity_tensor/lambda_shear_modulus_test.i)
[Mesh]
type = GeneratedMesh
dim = 3
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[AuxVariables]
[./stress_11]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
add_variables = true
use_automatic_differentiation = true
[../]
[]
[AuxKernels]
[./stress_11]
type = ADRankTwoAux
variable = stress_11
rank_two_tensor = stress
index_j = 1
index_i = 1
[../]
[]
[BCs]
[./bottom]
type = ADDirichletBC
variable = disp_y
boundary = bottom
value = 0
[../]
[./left]
type = ADDirichletBC
variable = disp_x
boundary = left
value = 0
[../]
[./back]
type = ADDirichletBC
variable = disp_z
boundary = back
value = 0
[../]
[./top]
type = ADDirichletBC
variable = disp_y
boundary = top
value = 0.001
[../]
[]
[Materials]
[./stress]
type = ADComputeLinearElasticStress
[../]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
lambda = 113636
shear_modulus = 454545
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
l_max_its = 20
nl_max_its = 10
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(test/tests/dirackernels/block_restriction/skip.i)
[Mesh]
[square]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[left]
type = SubdomainBoundingBoxGenerator
input = square
block_id = 1
bottom_left = '0 0 0'
top_right = '0.5 1 0'
[]
[right]
type = SubdomainBoundingBoxGenerator
input = left
block_id = 2
bottom_left = '0.5 0 0'
top_right = '1 1 0'
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[VectorPostprocessors]
[source]
type = CSVReader
csv_file = point_value_file.csv
[]
[]
[DiracKernels]
[point_source]
type = ReporterPointSource
variable = u
block = 1
value_name = source/value
x_coord_name = source/x
y_coord_name = source/y
z_coord_name = source/z
# The VPP contains the following information
# x,y,z,value
# 0.25,0.25,0.0,1
# 0.50,0.50,0.0,2
# 0.75,0.75,0.0,3
# The first point is in block 1.
# The second point is on the interface between blocks 1 and 2.
# The third point is in block 2.
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/fvkernels/fv_euler/fv_euler.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 20
[]
[]
[Variables]
# we have to impose non-zero initial conditions in order to avoid an initially
# singular matrix
[fv_vel]
order = CONSTANT
family = MONOMIAL
fv = true
initial_condition = 2
[]
[fv_rho]
order = CONSTANT
family = MONOMIAL
fv = true
initial_condition = 2
[]
[]
[FVKernels]
# del * rho * velocity * velocity
[adv_rho_u]
type = FVMatAdvection
variable = fv_vel
vel = 'fv_velocity'
advected_quantity = 'rho_u'
[]
# del * rho * velocity
[adv_rho]
type = FVMatAdvection
variable = fv_rho
vel = 'fv_velocity'
[]
[]
[FVBCs]
[left_vel]
type = FVDirichletBC
variable = fv_vel
value = 1
boundary = 'left'
[]
[left_rho]
type = FVDirichletBC
variable = fv_rho
value = 1
boundary = 'left'
[]
# del * rho * velocity * velocity
[right_vel]
type = FVMatAdvectionOutflowBC
variable = fv_vel
vel = 'fv_velocity'
advected_quantity = 'rho_u'
boundary = 'right'
[]
# del * rho * velocity
[adv_rho]
type = FVMatAdvectionOutflowBC
variable = fv_rho
vel = 'fv_velocity'
boundary = 'right'
[]
[]
[Materials]
[euler_material]
type = ADCoupledVelocityMaterial
vel_x = fv_vel
rho = fv_rho
velocity = 'fv_velocity'
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
line_search = 'none'
[]
[Outputs]
[out]
type = Exodus
execute_on = 'final'
[]
[]
(test/tests/vectorpostprocessors/material_vector_postprocessor/block-restrict-err.i)
# check that the simulation terminates with an error when you try to use this
# on an element that isn't available/computed on a particular block.
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Materials]
[./mat]
type = GenericConstantMaterial
prop_names = 'prop1 prop2 prop3'
prop_values = '1 2 42'
[../]
[]
[VectorPostprocessors]
[./vpp]
type = MaterialVectorPostprocessor
material = 'mat'
elem_ids = '2112'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'initial timestep_end'
csv = true
[]
(test/tests/constraints/nodal_constraint/nodal_constraint_test.i)
[Mesh]
file = 2-lines.e
[]
[Variables]
[./u]
family = LAGRANGE
order = FIRST
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = 4
value = 3
[../]
[]
[Constraints]
[./c1]
type = EqualValueNodalConstraint
variable = u
primary = 0
secondary = 4
penalty = 100000
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(modules/level_set/test/tests/functions/olsson_plane/olsson_plane.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmax = 1
ymax = 1
nx = 100
ny = 100
elem_type = QUAD9
[]
[AuxVariables/phi]
family = LAGRANGE
order = FIRST
[]
[Functions/phi_exact]
type = LevelSetOlssonPlane
epsilon = 0.04
point = '0.5 0.5 0'
normal = '0 1 0'
[]
[ICs/phi_ic]
type = FunctionIC
function = phi_exact
variable = phi
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/transfers/multiapp_conservative_transfer/master_conservative_transfer.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[MultiApps]
[./sub]
type = FullSolveMultiApp
input_files = sub_conservative_transfer.i
execute_on = timestep_end
[../]
[]
[Postprocessors]
[./from_postprocessor]
type = ElementIntegralVariablePostprocessor
variable = u
[../]
[]
[Transfers]
[./to_sub]
type = MultiAppMeshFunctionTransfer
source_variable = u
variable = aux_u
to_multi_app = sub
from_postprocessors_to_be_preserved = 'from_postprocessor'
to_postprocessors_to_be_preserved = 'to_postprocessor'
[../]
[]
[Outputs]
exodus = true
[./console]
type = Console
execute_postprocessors_on = 'INITIAL nonlinear TIMESTEP_END'
[../]
[]
(modules/phase_field/test/tests/free_energy_material/RegularSolutionFreeEnergy_const_T.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 10
xmax = 1
[]
[Variables]
[./c]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = x
[../]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = c
[../]
[]
[BCs]
[./left]
type = FunctionDirichletBC
variable = c
boundary = left
function = x
[../]
[./right]
type = FunctionDirichletBC
variable = c
boundary = right
function = x
[../]
[]
[Materials]
[./free_energy]
type = RegularSolutionFreeEnergy
f_name = F
c = c
outputs = out
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
l_max_its = 1
nl_max_its = 1
nl_abs_tol = 1
[]
[Outputs]
execute_on = 'timestep_end'
[./out]
type = Exodus
execute_on = timestep_end
[../]
[]
(modules/heat_conduction/test/tests/heat_conduction/2d_quadrature_gap_heat_transfer/second_order.i)
[Mesh]
file = nonmatching.e
second_order = true
[]
[Variables]
[./temp]
order = SECOND
[../]
[]
[Kernels]
[./hc]
type = HeatConduction
variable = temp
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = temp
boundary = leftleft
value = 1000
[../]
[./right]
type = DirichletBC
variable = temp
boundary = rightright
value = 400
[../]
[]
[ThermalContact]
[./left_to_right]
emissivity_primary = 0
emissivity_secondary = 0
secondary = leftright
quadrature = true
primary = rightleft
variable = temp
type = GapHeatTransfer
order = SECOND
[../]
[]
[Materials]
[./hcm]
type = HeatConductionMaterial
block = 'left right'
specific_heat = 1
thermal_conductivity = 1
[../]
[]
[Postprocessors]
[./left]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = leftright
diffusivity = thermal_conductivity
[../]
[./right]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = rightleft
diffusivity = thermal_conductivity
[../]
[]
[Executioner]
type = Steady
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/ray_tracing/test/tests/raykernels/line_source_ray_kernel/simple_diffusion_line_source.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
xmax = 5
ymax = 5
[]
[]
[Variables/u]
[]
[Kernels/diff]
type = Diffusion
variable = u
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
[UserObjects/study]
type = RepeatableRayStudy
names = 'line_source_ray'
start_points = '1 1 0'
end_points = '5 2 0'
execute_on = PRE_KERNELS # must be set for line sources!
[]
[RayKernels/line_source]
type = LineSourceRayKernel
variable = u
value = 5
[]
# This isn't used in the test but can be enabled
# for pretty pictures as is used in an example!
[Adaptivity]
steps = 0 # 5
marker = marker
initial_marker = marker
max_h_level = 5
[Indicators/indicator]
type = GradientJumpIndicator
variable = u
[]
[Markers/marker]
type = ErrorFractionMarker
indicator = indicator
coarsen = 0.1
refine = 0.5
[]
[]
(modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/ad_rz_cone_no_parts_steady_stabilized_second_order.i)
[GlobalParams]
order = SECOND
integrate_p_by_parts = false
[]
[Mesh]
file = '2d_cone.msh'
[]
[Problem]
coord_type = RZ
[]
[AuxVariables]
[vel_x]
[]
[vel_y]
[]
[]
[AuxKernels]
[vel_x]
type = VectorVariableComponentAux
variable = vel_x
vector_variable = velocity
component = 'x'
[]
[vel_y]
type = VectorVariableComponentAux
variable = vel_y
vector_variable = velocity
component = 'y'
[]
[]
[Variables]
[./velocity]
family = LAGRANGE_VEC
[../]
[./p]
order = FIRST
[../]
[]
# Need to set a non-zero initial condition because we have a velocity norm in
# the denominator for the tau coefficient of the stabilization term
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[mass_pspg]
type = INSADMassPSPG
variable = p
[]
[momentum_advection]
type = INSADMomentumAdvection
variable = velocity
[]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
[../]
[momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[]
[]
[BCs]
[p_corner]
type = DirichletBC
boundary = top_right
value = 0
variable = p
[]
[inlet]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom'
function_x = 0
function_y = 'inlet_func'
[../]
[wall]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'right'
function_x = 0
function_y = 0
[]
[axis]
type = ADVectorFunctionDirichletBC
variable = velocity
boundary = 'left'
set_y_comp = false
function_x = 0
[]
[]
[Functions]
[./inlet_func]
type = ParsedFunction
value = '-4 * x^2 + 1'
[../]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[ins_mat]
type = INSADTauMaterial
velocity = velocity
pressure = p
[]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = 'bjacobi ilu 4'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
csv = true
console = true
[./out]
type = Exodus
[../]
[]
[Postprocessors]
[./flow_in]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'bottom'
execute_on = 'timestep_end'
[../]
[./flow_out]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'top'
execute_on = 'timestep_end'
[../]
[]
(modules/porous_flow/test/tests/relperm/corey3.i)
# Test Corey relative permeability curve by varying saturation over the mesh
# Residual saturation of phase 0: s0r = 0.2
# Residual saturation of phase 1: s1r = 0.3
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Variables]
[p0]
initial_condition = 1e6
[]
[s1]
family = LAGRANGE
order = FIRST
[]
[]
[AuxVariables]
[s0aux]
family = MONOMIAL
order = CONSTANT
[]
[s1aux]
family = MONOMIAL
order = CONSTANT
[]
[kr0aux]
family = MONOMIAL
order = CONSTANT
[]
[kr1aux]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[s0]
type = PorousFlowPropertyAux
property = saturation
phase = 0
variable = s0aux
[]
[s1]
type = PorousFlowPropertyAux
property = saturation
phase = 1
variable = s1aux
[]
[kr0]
type = PorousFlowPropertyAux
property = relperm
phase = 0
variable = kr0aux
[]
[kr1]
type = PorousFlowPropertyAux
property = relperm
phase = 1
variable = kr1aux
[]
[]
[Functions]
[s1]
type = ParsedFunction
value = x
[]
[]
[ICs]
[s1]
type = FunctionIC
variable = s1
function = s1
[]
[]
[Kernels]
[p0]
type = Diffusion
variable = p0
[]
[s1]
type = Diffusion
variable = s1
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'p0 s1'
number_fluid_phases = 2
number_fluid_components = 2
[]
[pc]
type = PorousFlowCapillaryPressureConst
pc = 0
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow2PhasePS
phase0_porepressure = p0
phase1_saturation = s1
capillary_pressure = pc
[]
[kr0]
type = PorousFlowRelativePermeabilityCorey
phase = 0
n = 2
s_res = 0.2
sum_s_res = 0.5
[]
[kr1]
type = PorousFlowRelativePermeabilityCorey
phase = 1
n = 2
s_res = 0.3
sum_s_res = 0.5
[]
[]
[VectorPostprocessors]
[vpp]
type = LineValueSampler
warn_discontinuous_face_values = false
variable = 's0aux s1aux kr0aux kr1aux'
start_point = '0 0 0'
end_point = '1 0 0'
num_points = 20
sort_by = id
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
nl_abs_tol = 1e-8
[]
[BCs]
[sleft]
type = DirichletBC
variable = s1
value = 0
boundary = left
[]
[sright]
type = DirichletBC
variable = s1
value = 1
boundary = right
[]
[]
[Outputs]
csv = true
execute_on = timestep_end
[]
(test/tests/fviks/one-var-diffusion/no-ik.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 10
xmax = 2
[]
[subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '1.0 0 0'
block_id = 1
top_right = '2.0 1.0 0'
[]
[]
[Variables]
[u]
type = MooseVariableFVReal
[]
[]
[FVKernels]
[diff]
type = FVDiffusion
variable = u
coeff = 'coeff'
[]
[]
[FVBCs]
[left]
type = FVDirichletBC
variable = u
boundary = 'left'
value = 1
[]
[right]
type = FVDirichletBC
variable = u
boundary = 'right'
value = 0
[]
[]
[Materials]
[block0]
type = ADGenericFunctorMaterial
block = '0'
prop_names = 'coeff'
prop_values = '4'
[]
[block1]
type = ADGenericFunctorMaterial
block = '1'
prop_names = 'coeff'
prop_values = '2'
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
csv = true
[]
[Functions]
[exact_u]
type = ParsedFunction
value = 'if(x<1, 1 - x/3, 4/3 - 2*x/3)'
[]
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(test/tests/misc/check_error/function_file_test17.i)
# Test for usage of missing function
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = ic_function
[../]
[../]
[]
[Functions]
[./ic_function]
type = PiecewiseLinear
data_file = piecewise_linear_rows_more_data.csv
xy_in_file_only = false
x_index_in_file = 0
y_index_in_file = 0 # will generate an error because x and y index are equal
scale_factor = 1.0
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/kernels/hfem/lower-d-volumes.i)
[Mesh]
[square]
type = GeneratedMeshGenerator
nx = 3
ny = 3
dim = 2
[]
build_all_side_lowerd_mesh = true
[]
[Variables]
[u]
order = THIRD
family = MONOMIAL
block = 0
[]
[uhat]
order = CONSTANT
family = MONOMIAL
block = BOUNDARY_SIDE_LOWERD_SUBDOMAIN
[]
[lambda]
order = CONSTANT
family = MONOMIAL
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
[]
[lambdab]
order = CONSTANT
family = MONOMIAL
block = BOUNDARY_SIDE_LOWERD_SUBDOMAIN
[]
[]
[AuxVariables]
[v]
order = CONSTANT
family = MONOMIAL
block = 0
initial_condition = '1'
[]
[]
[Kernels]
[diff]
type = MatDiffusion
variable = u
diffusivity = '1'
block = 0
[]
[source]
type = CoupledForce
variable = u
v = v
coef = '1'
block = 0
[]
[reaction]
type = Reaction
variable = uhat
rate = '1'
block = BOUNDARY_SIDE_LOWERD_SUBDOMAIN
[]
[uhat_coupled]
type = CoupledForce
variable = uhat
block = BOUNDARY_SIDE_LOWERD_SUBDOMAIN
v = lambdab
coef = '1'
[]
[]
[DGKernels]
[surface]
type = TestLowerDVolumes
variable = u
lowerd_variable = lambda
l = 1
n = 3
[]
[]
[BCs]
[all]
type = HFEMDirichletBC
boundary = 'left right top bottom'
variable = u
lowerd_variable = lambdab
uhat = uhat
[]
[]
[Postprocessors]
[intu]
type = ElementIntegralVariablePostprocessor
variable = u
block = 0
[]
[lambdanorm]
type = ElementL2Norm
variable = lambda
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu basic mumps'
[]
[Outputs]
[out]
# we hide lambda because it may flip sign due to element
# renumbering with distributed mesh
type = Exodus
hide = lambda
[]
csv = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-rc-friction-action.i)
mu=1.1
rho=1.1
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 5
ymin = -1
ymax = 1
nx = 50
ny = 10
[]
[]
[Modules]
[NavierStokesFV]
compressibility = 'incompressible'
density = 'rho'
dynamic_viscosity = 'mu'
initial_velocity = '1 1 0'
initial_pressure = 0.0
inlet_boundaries = 'left'
momentum_inlet_types = 'fixed-velocity'
momentum_inlet_function = '1 0'
wall_boundaries = 'top bottom'
momentum_wall_types = 'noslip noslip'
outlet_boundaries = 'right'
momentum_outlet_types = 'fixed-pressure'
pressure_function = '0'
friction_types = 'darcy'
friction_coeffs = '25'
[]
[]
[Materials]
[const]
type = ADGenericFunctorMaterial
prop_names = 'rho mu'
prop_values = '${rho} ${mu}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 200 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(test/tests/materials/functor_properties/gradients/functor-gradients.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 4
xmax = 2
[]
[Variables]
[u]
type = MooseVariableFVReal
[]
[]
[AuxVariables]
[sink]
type = MooseVariableFVReal
[]
[diffusive_flux_x]
type = MooseVariableFVReal
[]
[diffusive_flux_y]
type = MooseVariableFVReal
[]
[diffusive_flux_magnitude]
type = MooseVariableFVReal
[]
[]
[ICs]
[sink]
type = FunctionIC
variable = sink
function = 'x^3'
[]
[]
[FVKernels]
[diff]
type = FVDiffusion
variable = u
coeff = 1.1
[]
[sink]
type = FVFunctorElementalKernel
variable = u
functor_name = 'sink_mat'
[]
[]
[FVBCs]
[bounds]
type = FVDirichletBC
variable = u
boundary = 'left right top bottom'
value = 0
[]
[]
[Materials]
[functor_properties]
type = ADGenericFunctorMaterial
prop_names = 'sink_mat diffusive_coef'
prop_values = 'sink 4.5'
[]
[gradient_of_u]
type = ADGenericFunctorGradientMaterial
prop_names = 'grad_u'
prop_values = 'u'
[]
[]
# Compute the diffusive flux magnitude
[AuxKernels]
[diffusive_flux_x]
type = ADFunctorVectorElementalAux
variable = 'diffusive_flux_x'
functor = 'grad_u'
factor = 'diffusive_coef'
component = 0
[]
[diffusive_flux_y]
type = ADFunctorVectorElementalAux
variable = 'diffusive_flux_y'
functor = 'grad_u'
factor = 'diffusive_coef'
component = 1
[]
[diffusive_flux_magnitude]
type = VectorMagnitudeAux
variable = 'diffusive_flux_magnitude'
x = 'diffusive_flux_x'
y = 'diffusive_flux_y'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(examples/ex19_dampers/ex19.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0.0
xmax = 1.0
nx = 10
ymin = 0.0
ymax = 1.0
ny = 10
[]
[Variables]
[./diffusion]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = diffusion
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = diffusion
boundary = 3
value = 3
[../]
[./right]
type = DirichletBC
variable = diffusion
boundary = 1
value = 1
[../]
[]
[Dampers]
# Use a constant damping parameter
[./diffusion_damp]
type = ConstantDamper
variable = diffusion
damping = 0.9
[../]
[]
[Executioner]
type = Steady
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/verify_against_analytical/ad_2d_steady_state.i)
# This test solves a 2D steady state heat equation
# The error is found by comparing to the analytical solution
# Note that the thermal conductivity, specific heat, and density in this problem
# Are set to 1, and need to be changed to the constants of the material being
# Analyzed
[Mesh]
type = GeneratedMesh
dim = 2
nx = 30
ny = 30
xmax = 2
ymax = 2
[]
[Variables]
[./T]
[../]
[]
[Kernels]
[./HeatDiff]
type = ADHeatConduction
variable = T
[../]
[]
[BCs]
[./zero]
type = DirichletBC
variable = T
boundary = 'right bottom left'
value = 0
[../]
[./top]
type = ADFunctionDirichletBC
variable = T
boundary = top
function = '10*sin(pi*x*0.5)'
[../]
[]
[Materials]
[./properties]
type = ADGenericConstantMaterial
prop_names = 'thermal_conductivity specific_heat density'
prop_values = '1 1 1'
[../]
[]
[Postprocessors]
[./nodal_error]
type = NodalL2Error
function = '10/(sinh(pi))*sin(pi*x*0.5)*sinh(pi*y*0.5)'
variable = T
[../]
[./elemental_error]
type = ElementL2Error
function = '10/(sinh(pi))*sin(pi*x*0.5)*sinh(pi*y*0.5)'
variable = T
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/postprocessors/element_h1_error_pps/element_h1_error_pp_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 3
ny = 3
xmin = 0
xmax = 2
ymin = 0
ymax = 2
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
active = 'forcing_func u_func'
[./forcing_func]
type = ParsedFunction
#value = alpha*alpha*pi*pi*(y*y*sin(alpha*pi*x*y)+y*y*sin(alpha*pi*x*y))
value = alpha*alpha*pi*pi*sin(alpha*pi*x)
vars = 'alpha'
vals = '4'
[../]
[./u_func]
type = ParsedGradFunction
#value = sin(alpha*pi*x*y)
#grad_x = alpha*pi*y*cos(alpha*pi*x*y)
#grad_y = alpha*pi*x*cos(alpha*pi*x*y)
value = sin(alpha*pi*x)
grad_x = alpha*pi*cos(alpha*pi*x)
vars = 'alpha'
vals = '4'
[../]
[]
[Kernels]
active = 'diff forcing'
[./diff]
type = Diffusion
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_func
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = '1'
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = '3'
value = 0
[../]
[]
[Executioner]
type = Steady
[./Adaptivity]
refine_fraction = 1.0
coarsen_fraction = 0.0
max_h_level = 10
steps = 4
[../]
[]
[Postprocessors]
[./dofs]
type = NumDOFs
execute_on = 'initial timestep_end'
[../]
[./h1_error]
type = ElementH1Error
variable = u
function = u_func
execute_on = 'initial timestep_end'
[../]
[./h1_semi]
type = ElementH1SemiError
variable = u
function = u_func
execute_on = 'initial timestep_end'
[../]
[./l2_error]
type = ElementL2Error
variable = u
function = u_func
execute_on = 'initial timestep_end'
[../]
[]
[Outputs]
file_base = out
exodus = false
csv = true
[]
(test/tests/outputs/oversample/oversample.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
[./out]
type = Exodus
refinements = 2
position = '1 1 0'
[../]
[]
(test/tests/meshgenerators/mesh_extruder_generator/extrude_quad.i)
[Mesh]
[./fmg]
type = FileMeshGenerator
file = chimney_quad.e
[]
[./extrude]
type = MeshExtruderGenerator
input = fmg
num_layers = 20
extrusion_vector = '0 1e-2 0'
bottom_sideset = 'new_bottom'
top_sideset = 'new_top'
[]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = u
boundary = 'new_bottom'
value = 0
[../]
[./top]
type = DirichletBC
variable = u
boundary = 'new_top'
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out_quad
exodus = true
[]
(modules/heat_conduction/test/tests/radiation_transfer_action/radiative_transfer_action.i)
[Problem]
kernel_coverage_check = false
[]
[Mesh]
type = MeshGeneratorMesh
[./cmg]
type = CartesianMeshGenerator
dim = 2
dx = '1 1.3 1.9'
ix = '3 3 3'
dy = '2 1.2 0.9'
iy = '3 3 3'
subdomain_id = '0 1 0
4 5 2
0 3 0'
[../]
[./inner_bottom]
type = SideSetsBetweenSubdomainsGenerator
input = cmg
primary_block = 1
paired_block = 5
new_boundary = 'inner_bottom'
[../]
[./inner_left]
type = SideSetsBetweenSubdomainsGenerator
input = inner_bottom
primary_block = 4
paired_block = 5
new_boundary = 'inner_left'
[../]
[./inner_right]
type = SideSetsBetweenSubdomainsGenerator
input = inner_left
primary_block = 2
paired_block = 5
new_boundary = 'inner_right'
[../]
[./inner_top]
type = SideSetsBetweenSubdomainsGenerator
input = inner_right
primary_block = 3
paired_block = 5
new_boundary = 'inner_top'
[../]
[./rename]
type = RenameBlockGenerator
old_block = '1 2 3 4'
new_block = '0 0 0 0'
input = inner_top
[../]
[]
[Variables]
[./temperature]
block = 0
[../]
[]
[Kernels]
[./heat_conduction]
type = HeatConduction
variable = temperature
block = 0
diffusion_coefficient = 5
[../]
[]
[GrayDiffuseRadiation]
[./cavity]
boundary = '4 5 6 7'
emissivity = '0.9 0.8 0.4 1'
n_patches = '2 2 2 3'
partitioners = 'centroid centroid centroid centroid'
centroid_partitioner_directions = 'x y y x'
temperature = temperature
adiabatic_boundary = '7'
fixed_temperature_boundary = '4'
fixed_boundary_temperatures = '1200'
view_factor_calculator = analytical
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = temperature
boundary = left
value = 600
[../]
[./right]
type = DirichletBC
variable = temperature
boundary = right
value = 300
[../]
[]
[Postprocessors]
[./average_T_inner_right]
type = SideAverageValue
variable = temperature
boundary = inner_right
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/lid-driven/lid-driven-action.i)
mu=.01
rho=1
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = .1
ymin = 0
ymax = .1
nx = 20
ny = 20
[]
[]
[Modules]
[NavierStokesFV]
compressibility = 'incompressible'
density = ${rho}
dynamic_viscosity = ${mu}
initial_pressure = 0.0
inlet_boundaries = 'top'
momentum_inlet_types = 'fixed-velocity'
momentum_inlet_function = '1 0'
wall_boundaries = 'left right bottom'
momentum_wall_types = 'noslip noslip noslip'
pin_pressure = true
pinned_pressure_type = average
pinned_pressure_value = 0
[]
[]
[AuxVariables]
[U]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[]
[AuxKernels]
[mag]
type = VectorMagnitudeAux
variable = U
x = vel_x
y = vel_y
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/check_syntax_ok.i)
[Mesh]
file = 2-lines.e
construct_side_list_from_node_list = true
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
block = '1 2'
[../]
[./lm]
order = FIRST
family = SCALAR
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[ScalarKernels]
[./ced]
type = NodalEqualValueConstraint
variable = lm
var = u
boundary = '100 101'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = '1'
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = '2'
value = 3
[../]
[./evc1]
type = OneDEqualValueConstraintBC
variable = u
boundary = '100'
lambda = lm
component = 0
vg = 1
[../]
[./evc2]
type = OneDEqualValueConstraintBC
variable = u
boundary = '101'
lambda = lm
component = 0
vg = -1
[../]
[]
[Preconditioning]
[./fmp]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
execute_on = 'timestep_end'
[]
(test/tests/postprocessors/variable_residual_norm/variable_residual.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
xmin = -1
xmax = 1
ymin = 0
ymax = 1
elem_type = QUAD4
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[Functions]
[./leg1]
type = ParsedFunction
value = 'x'
[../]
[./leg2]
type = ParsedFunction
value = '0.5*(3.0*x*x-1.0)'
[../]
[]
[BCs]
[./left_u]
type = DirichletBC
variable = u
preset = false
boundary = 1
value = 0
[../]
[./right_u]
type = DirichletBC
variable = u
preset = false
boundary = 2
value = 1
[../]
[./left_v]
type = DirichletBC
variable = v
preset = false
boundary = 1
value = 200
[../]
[./right_v]
type = DirichletBC
variable = v
preset = false
boundary = 2
value = 100
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
# this is large on purpose so we don't reduce the variable residual to machine zero
# and so that we can compare to larger numbers. This also means this test can run only
# in serial, since parallel runs yield different convergence history.
nl_rel_tol = 1e-4
[]
[Postprocessors]
[./u_res_l2]
type = VariableResidual
variable = u
[../]
[./v_res_l2]
type = VariableResidual
variable = v
[../]
[]
[Outputs]
csv = true
[./console]
type = Console
# turn this on, so we can visually compare the postprocessor value with what is computed by the Console object
all_variable_norms = true
[../]
[]
(test/tests/dirackernels/point_caching/point_caching_adaptive_refinement.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
elem_type = QUAD4
uniform_refine = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[DiracKernels]
active = 'point_source'
[./point_source]
type = CachingPointSource
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Adaptivity]
steps = 3
marker = 'combo'
[./Markers]
[./combo]
# In a real problem you would want to mark based on an error
# indicator, but we want this test to run consistently in
# parallel, so we just mark elements within a box for
# refinement. The boxes here are based on the 8x8
# uniformly-refined initial grid.
type = ComboMarker
markers = 'box1 box2 box3'
[../]
[./box1]
type = BoxMarker
bottom_left = '0.125 0.625 0'
top_right = '0.375 0.875 0'
inside = refine
outside = dont_mark
[../]
[./box2]
type = BoxMarker
bottom_left = '0.625 0.625 0'
top_right = '0.875 0.875 0'
inside = refine
outside = dont_mark
[../]
[./box3]
type = BoxMarker
bottom_left = '0.625 0.125 0'
top_right = '0.875 0.375 0'
inside = refine
outside = dont_mark
[../]
[../]
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(test/tests/functions/solution_function/solution_function_grad_p2.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
parallel_type = replicated
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./test_variable_x]
order = FIRST
family = LAGRANGE
[../]
[./test_variable_y]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./test_variable_x_aux]
type = FunctionDerivativeAux
variable = test_variable_x
component = x
function = solution_function
[../]
[./test_variable_y_aux]
type = FunctionDerivativeAux
variable = test_variable_y
component = y
function = solution_function
[../]
[]
[UserObjects]
[./ex_soln]
type = SolutionUserObject
system_variables = test_variable
mesh = solution_function_grad_p1.e
[../]
[]
[Functions]
[./solution_function]
type = SolutionFunction
solution = ex_soln
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-10
[]
[Outputs]
file_base = solution_function_grad_p2
exodus = true
[]
(modules/functional_expansion_tools/test/tests/errors/aux_bad_function.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[AuxVariables]
[./v]
[../]
[]
[AuxKernels]
[./this_could_be_bad]
type = FunctionSeriesToAux
function = const
variable = v
[../]
[]
[Functions]
[./const]
type = ConstantFunction
value = -1
[../]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
(modules/porous_flow/test/tests/poroperm/PermFromPoro02.i)
# Testing permeability from porosity
# Trivial test, checking calculated permeability is correct
# k = k_anisotropic * k0 * (1-phi0)^m/phi0^n * phi^n/(1-phi)^m
[Mesh]
type = GeneratedMesh
dim = 1
nx = 3
xmin = 0
xmax = 3
[]
[GlobalParams]
block = 0
PorousFlowDictator = dictator
[]
[Variables]
[pp]
[InitialCondition]
type = ConstantIC
value = 0
[]
[]
[]
[Kernels]
[flux]
type = PorousFlowAdvectiveFlux
gravity = '0 0 0'
variable = pp
[]
[]
[BCs]
[ptop]
type = DirichletBC
variable = pp
boundary = right
value = 0
[]
[pbase]
type = DirichletBC
variable = pp
boundary = left
value = 1
[]
[]
[AuxVariables]
[poro]
order = CONSTANT
family = MONOMIAL
[]
[perm_x]
order = CONSTANT
family = MONOMIAL
[]
[perm_y]
order = CONSTANT
family = MONOMIAL
[]
[perm_z]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[poro]
type = PorousFlowPropertyAux
property = porosity
variable = poro
[]
[perm_x]
type = PorousFlowPropertyAux
property = permeability
variable = perm_x
row = 0
column = 0
[]
[perm_y]
type = PorousFlowPropertyAux
property = permeability
variable = perm_y
row = 1
column = 1
[]
[perm_z]
type = PorousFlowPropertyAux
property = permeability
variable = perm_z
row = 2
column = 2
[]
[]
[Postprocessors]
[perm_x_bottom]
type = PointValue
variable = perm_x
point = '0 0 0'
[]
[perm_y_bottom]
type = PointValue
variable = perm_y
point = '0 0 0'
[]
[perm_z_bottom]
type = PointValue
variable = perm_z
point = '0 0 0'
[]
[perm_x_top]
type = PointValue
variable = perm_x
point = '3 0 0'
[]
[perm_y_top]
type = PointValue
variable = perm_y
point = '3 0 0'
[]
[perm_z_top]
type = PointValue
variable = perm_z
point = '3 0 0'
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureVG
# unimportant in this fully-saturated test
m = 0.8
alpha = 1e-4
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 2.2e9
viscosity = 1e-3
density0 = 1000
thermal_expansion = 0
[]
[]
[]
[Materials]
[permeability]
type = PorousFlowPermeabilityKozenyCarman
k_anisotropy = '1 0 0 0 2 0 0 0 0.1'
poroperm_function = kozeny_carman_phi0
k0 = 1e-10
phi0 = 0.05
m = 2
n = 7
[]
[temperature]
type = PorousFlowTemperature
[]
[massfrac]
type = PorousFlowMassFraction
[]
[eff_fluid_pressure]
type = PorousFlowEffectiveFluidPressure
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pp
capillary_pressure = pc
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[porosity]
type = PorousFlowPorosity
porosity_zero = 0.1
[]
[relperm]
type = PorousFlowRelativePermeabilityCorey
n = 0 # unimportant in this fully-saturated situation
phase = 0
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
[]
[]
[Executioner]
solve_type = Newton
type = Steady
l_tol = 1E-5
nl_abs_tol = 1E-3
nl_rel_tol = 1E-8
l_max_its = 200
nl_max_its = 400
petsc_options_iname = '-pc_type -pc_asm_overlap -sub_pc_type -ksp_type -ksp_gmres_restart'
petsc_options_value = ' asm 2 lu gmres 200'
[]
[Outputs]
csv = true
execute_on = 'timestep_end'
[]
(test/tests/utils/moose_mesh_utils/moose_mesh_utils.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
[]
[]
[UserObjects/test]
type = MooseMeshUtilsTest
[]
[Executioner]
type = Steady
[]
(test/tests/kernels/scalar_constraint/scalar_constraint_kernel_disp.i)
#
# This test is identical to scalar_constraint_kernel.i, but it everything is evaluated on the displaced mesh
#
[GlobalParams]
use_displaced_mesh = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 2
ny = 2
elem_type = QUAD9
displacements = 'disp_x disp_y'
[]
[Functions]
[./exact_fn]
type = ParsedFunction
value = 'x*x+y*y'
[../]
[./ffn]
type = ParsedFunction
value = -4
[../]
[./bottom_bc_fn]
type = ParsedFunction
value = -2*y
[../]
[./right_bc_fn]
type = ParsedFunction
value = 2*x
[../]
[./top_bc_fn]
type = ParsedFunction
value = 2*y
[../]
[./left_bc_fn]
type = ParsedFunction
value = -2*x
[../]
[]
[AuxVariables]
[./disp_x]
family = LAGRANGE
order = SECOND
[../]
[./disp_y]
family = LAGRANGE
order = SECOND
[../]
[]
[AuxKernels]
[./disp_x_ak]
type = ConstantAux
variable = disp_x
value = 0
[../]
[./disp_y_ak]
type = ConstantAux
variable = disp_y
value = 0
[../]
[]
# NL
[Variables]
[./u]
family = LAGRANGE
order = SECOND
[../]
[./lambda]
family = SCALAR
order = FIRST
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./ffnk]
type = BodyForce
variable = u
function = ffn
[../]
[./sk_lm]
type = ScalarLagrangeMultiplier
variable = u
lambda = lambda
[../]
[]
[ScalarKernels]
[./constraint]
type = AverageValueConstraint
variable = lambda
pp_name = pp
value = 2.666666666666666
# overrride the global setting, scalar kernels do not live on a mesh
use_displaced_mesh = false
[../]
[]
[BCs]
[./bottom]
type = FunctionNeumannBC
variable = u
boundary = '0'
function = bottom_bc_fn
[../]
[./right]
type = FunctionNeumannBC
variable = u
boundary = '1'
function = right_bc_fn
[../]
[./top]
type = FunctionNeumannBC
variable = u
boundary = '2'
function = top_bc_fn
[../]
[./left]
type = FunctionNeumannBC
variable = u
boundary = '3'
function = left_bc_fn
[../]
[]
[Postprocessors]
[./pp]
type = ElementIntegralVariablePostprocessor
variable = u
execute_on = linear
[../]
[./l2_err]
type = ElementL2Error
variable = u
function = exact_fn
execute_on = 'initial timestep_end'
[../]
[]
[Preconditioning]
[./pc]
type = SMP
full = true
solve_type = 'PJFNK'
[../]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-14
l_tol = 1e-7
[]
[Outputs]
exodus = true
hide = lambda
[]
(test/tests/auxkernels/build_array_variable_aux/build_array_variable_aux.i)
[Mesh]
[meshgen]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[]
[]
[Variables]
[a]
order = FIRST
family = LAGRANGE
[]
[b]
order = FIRST
family = LAGRANGE
[]
[c]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[d]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[]
[Kernels]
[diff_a]
type = Diffusion
variable = a
[]
[diff_b]
type = Diffusion
variable = b
[]
[]
[FVKernels]
[diff_c]
type = FVDiffusion
variable = c
coeff = 1
[]
[diff_d]
type = FVDiffusion
variable = d
coeff = 1
[]
[]
[BCs]
[a1]
type = DirichletBC
variable = a
boundary = left
value = 0
[]
[a2]
type = DirichletBC
variable = a
boundary = right
value = 1
[]
[b1]
type = DirichletBC
variable = b
boundary = bottom
value = 0
[]
[b2]
type = DirichletBC
variable = b
boundary = top
value = 1
[]
[]
[FVBCs]
[c1]
type = FVDirichletBC
variable = c
boundary = left
value = 0
[]
[c2]
type = FVDirichletBC
variable = c
boundary = right
value = 1
[]
[d1]
type = FVDirichletBC
variable = d
boundary = bottom
value = 0
[]
[d2]
type = FVDirichletBC
variable = d
boundary = top
value = 1
[]
[]
[Problem]
kernel_coverage_check = off
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[AuxVariables]
[ab]
order = FIRST
family = LAGRANGE
components = 2
[]
[cd]
order = CONSTANT
family = MONOMIAL
components = 2
[]
[]
[AuxKernels]
[build_ab]
type = BuildArrayVariableAux
variable = ab
component_variables = 'a b'
[]
[build_cd]
type = BuildArrayVariableAux
variable = cd
component_variables = 'c d'
[]
[]
[Outputs]
exodus = true
[]
(test/tests/ics/postprocessor_interface/postprocessor_interface.i)
[Mesh]
type = GeneratedMesh
dim = 1
xmin = 0
xmax = 10
nx = 10
[]
[Functions]
# The integral of this function is 2*3 + 3*6 + 5*2 = 34
[test_fn]
type = PiecewiseConstant
axis = x
x = '0 2 5'
y = '3 6 2'
[]
[]
[Postprocessors]
[integral_pp]
type = FunctionElementIntegral
function = test_fn
execute_on = 'INITIAL'
[]
[pp2]
type = FunctionValuePostprocessor
function = 6
execute_on = 'INITIAL'
[]
[]
[AuxVariables]
[test_var]
order = CONSTANT
family = MONOMIAL
[]
[]
[ICs]
[test_var_ic]
type = PostprocessorIC
variable = test_var
pp1 = integral_pp
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Postprocessors]
# This PP should have the sum of the other two PPs: 34 + 6 = 40
[test_var_pp]
type = ElementAverageValue
variable = test_var
execute_on = 'INITIAL'
[]
[]
[Outputs]
csv = true
[]
(test/tests/misc/check_error/deprecated_block_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[DeprecatedBlock]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/misc/check_error/mesh_pointer_error_check.i)
[Mesh]
file = mesh_pointer.e
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/multiapps/initial_transfer/sub.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
[]
[Problem]
kernel_coverage_check = false
[]
[Variables][dummy][][]
[Postprocessors]
[scaled]
type = ScalePostprocessor
value = receiver
scaling_factor = 2
# Note: during subapp initial setup, master postprocessor has not been transferred
execute_on = 'initial timestep_end'
[]
[receiver]
type = Receiver
default = 0
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
[]
(test/tests/meshgenerators/sidesets_from_points_generator/sidesets_from_points.i)
[Mesh]
[./fmg]
type = FileMeshGenerator
file = cylinder.e
#parallel_type = replicated
[]
[./sidesets]
type = SideSetsFromPointsGenerator
input = fmg
points = '0 0 0.5
0.1 0 0
0 0 -0.5'
new_boundary = 'top side bottom'
[]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = u
boundary = bottom
value = 0
[../]
[./top]
type = DirichletBC
variable = u
boundary = top
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/mortar/convergence-studies/gap-conductance/gap-conductance.i)
[Problem]
error_on_jacobian_nonzero_reallocation = true
[]
[Mesh]
second_order = true
[./left_block]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
elem_type = QUAD4
[../]
[./left_block_sidesets]
type = RenameBoundaryGenerator
input = left_block
old_boundary_id = '0 1 2 3'
new_boundary = 'lb_bottom lb_right lb_top lb_left'
[../]
[./left_block_id]
type = SubdomainIDGenerator
input = left_block_sidesets
subdomain_id = 1
[../]
[./right_block]
type = GeneratedMeshGenerator
dim = 2
xmin = 2
xmax = 3
ymin = 0
ymax = 1
nx = 2
ny = 2
elem_type = QUAD4
[../]
[./right_block_id]
type = SubdomainIDGenerator
input = right_block
subdomain_id = 2
[../]
[right_block_change_boundary_id]
type = RenameBoundaryGenerator
input = right_block_id
old_boundary_id = '0 1 2 3'
new_boundary_id = '100 101 102 103'
[]
[./combined]
type = MeshCollectionGenerator
inputs = 'left_block_id right_block_change_boundary_id'
[../]
[./block_rename]
type = RenameBlockGenerator
input = combined
old_block = '1 2'
new_block = 'left_block right_block'
[../]
[right_right_sideset]
type = SideSetsAroundSubdomainGenerator
input = block_rename
new_boundary = rb_right
block = right_block
normal = '1 0 0'
[]
[right_left_sideset]
type = SideSetsAroundSubdomainGenerator
input = right_right_sideset
new_boundary = rb_left
block = right_block
normal = '-1 0 0'
[]
[right_top_sideset]
type = SideSetsAroundSubdomainGenerator
input = right_left_sideset
new_boundary = rb_top
block = right_block
normal = '0 1 0'
[]
[right_bottom_sideset]
type = SideSetsAroundSubdomainGenerator
input = right_top_sideset
new_boundary = rb_bottom
block = right_block
normal = '0 -1 0'
[]
[secondary]
input = right_bottom_sideset
type = LowerDBlockFromSidesetGenerator
sidesets = 'lb_right'
new_block_id = '10001'
new_block_name = 'secondary_lower'
[]
[primary]
input = secondary
type = LowerDBlockFromSidesetGenerator
sidesets = 'rb_left'
new_block_id = '10000'
new_block_name = 'primary_lower'
[]
[]
[Variables]
[./T]
block = 'left_block right_block'
order = SECOND
[../]
[./lambda]
block = 'secondary_lower'
family = MONOMIAL
order = CONSTANT
[../]
[]
[BCs]
[./neumann]
type = FunctionGradientNeumannBC
exact_solution = exact_soln_primal
variable = T
boundary = 'lb_bottom lb_top lb_left rb_bottom rb_right rb_top'
[../]
[]
[Kernels]
[./conduction]
type = Diffusion
variable = T
block = 'left_block right_block'
[../]
[./sink]
type = Reaction
variable = T
block = 'left_block right_block'
[../]
[./forcing_function]
type = BodyForce
variable = T
function = forcing_function
block = 'left_block right_block'
[../]
[]
[Functions]
[./forcing_function]
type = ParsedFunction
value = ''
[../]
[./exact_soln_primal]
type = ParsedFunction
value = ''
[../]
[exact_soln_lambda]
type = ParsedFunction
value = ''
[]
[mms_secondary]
type = ParsedFunction
value = ''
[]
[mms_primary]
type = ParsedFunction
value = ''
[]
[]
[Debug]
show_var_residual_norms = 1
[]
[Constraints]
[./mortar]
type = GapHeatConductanceTest
primary_boundary = rb_left
secondary_boundary = lb_right
primary_subdomain = primary_lower
secondary_subdomain = secondary_lower
secondary_variable = T
variable = lambda
secondary_gap_conductance = 1
primary_gap_conductance = 1
secondary_mms_function = mms_secondary
primary_mms_function = mms_primary
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
solve_type = NEWTON
type = Steady
petsc_options = '-snes_converged_reason'
# petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
# petsc_options_value = 'lu superlu_dist'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
csv = true
[dofmap]
type = DOFMap
execute_on = 'initial'
[]
[]
[Postprocessors]
[L2lambda]
type = ElementL2Error
variable = lambda
function = exact_soln_lambda
execute_on = 'timestep_end'
block = 'secondary_lower'
[]
[L2u]
type = ElementL2Error
variable = T
function = exact_soln_primal
execute_on = 'timestep_end'
block = 'left_block right_block'
[]
[h]
type = AverageElementSize
block = 'left_block right_block'
[]
[]
(modules/heat_conduction/test/tests/radiation_transfer_action/radiative_transfer_action_external_boundary_ray_tracing.i)
[Problem]
kernel_coverage_check = false
[]
[Mesh]
[cmg]
type = CartesianMeshGenerator
dim = 2
dx = '1 1.3 1.9'
ix = '3 3 3'
dy = '6'
iy = '9'
subdomain_id = '0 1 2'
[]
[inner_left]
type = SideSetsBetweenSubdomainsGenerator
input = cmg
primary_block = 0
paired_block = 1
new_boundary = 'inner_left'
[]
[inner_right]
type = SideSetsBetweenSubdomainsGenerator
input = inner_left
primary_block = 2
paired_block = 1
new_boundary = 'inner_right'
[]
[inner_top]
type = ParsedGenerateSideset
combinatorial_geometry = 'abs(y - 6) < 1e-10'
normal = '0 1 0'
included_subdomain_ids = 1
new_sideset_name = 'inner_top'
input = 'inner_right'
[]
[inner_bottom]
type = ParsedGenerateSideset
combinatorial_geometry = 'abs(y) < 1e-10'
normal = '0 -1 0'
included_subdomain_ids = 1
new_sideset_name = 'inner_bottom'
input = 'inner_top'
[]
[rename]
type = RenameBlockGenerator
old_block = '2'
new_block = '0'
input = inner_bottom
[]
[]
[Variables]
[temperature]
block = 0
[]
[]
[Kernels]
[heat_conduction]
type = HeatConduction
variable = temperature
block = 0
diffusion_coefficient = 5
[]
[]
[GrayDiffuseRadiation]
[cavity]
boundary = '4 5 6 7'
emissivity = '0.9 0.8 0.4 1'
n_patches = '2 2 2 3'
partitioners = 'centroid centroid centroid centroid'
centroid_partitioner_directions = 'x y y x'
temperature = temperature
adiabatic_boundary = '7'
fixed_temperature_boundary = '6'
fixed_boundary_temperatures = '800'
view_factor_calculator = ray_tracing
[]
[]
[BCs]
[left]
type = DirichletBC
variable = temperature
boundary = left
value = 1000
[]
[right]
type = DirichletBC
variable = temperature
boundary = right
value = 300
[]
[]
[Postprocessors]
[average_T_inner_right]
type = SideAverageValue
variable = temperature
boundary = inner_right
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(tutorials/tutorial01_app_development/step08_test_harness/test/tests/kernels/darcy_pressure/zero_viscosity_error.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Problem]
solve = false
[]
[Variables]
[u]
[]
[]
[Kernels]
[zero_viscosity]
type = DarcyPressure
variable = u
permeability = 0.8451e-09
viscosity = 0 # The viscosity must be a non-zero number, so this input should invoke an error
[]
[]
[Executioner]
type = Steady
[]
(test/tests/multiapps/override_cliargs/primary.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 1
[]
[]
[Problem]
solve = false
[]
[MultiApps]
[sub]
type = OverrideCliArgs
input_files = sub.i
xmax = 12
[]
[]
[Executioner]
type = Steady
[]
(test/tests/variables/fe_hier/hier-1-1d.i)
###########################################################
# This is a simple test demonstrating the use of the
# Hierarchic variable type.
#
# @Requirement F3.10
###########################################################
[Mesh]
type = GeneratedMesh
dim = 1
xmin = -1
xmax = 1
nx = 5
elem_type = EDGE3
[]
[Functions]
[./bc_fnl]
type = ParsedFunction
value = -1
[../]
[./bc_fnr]
type = ParsedFunction
value = 1
[../]
[./forcing_fn]
type = ParsedFunction
value = x
[../]
[./solution]
type = ParsedGradFunction
value = x
grad_x = 1
[../]
[]
# Hierarchic Variable type
[Variables]
[./u]
order = FIRST
family = HIERARCHIC
[../]
[]
[Kernels]
active = 'diff forcing reaction'
[./diff]
type = Diffusion
variable = u
[../]
[./reaction]
type = Reaction
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
[./bc_left]
type = FunctionNeumannBC
variable = u
boundary = 'left'
function = bc_fnl
[../]
[./bc_right]
type = FunctionNeumannBC
variable = u
boundary = 'right'
function = bc_fnr
[../]
[]
[Postprocessors]
[./dofs]
type = NumDOFs
[../]
[./h]
type = AverageElementSize
[../]
[./L2error]
type = ElementL2Error
variable = u
function = solution
[../]
[./H1error]
type = ElementH1Error
variable = u
function = solution
[../]
[./H1Semierror]
type = ElementH1SemiError
variable = u
function = solution
[../]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-11
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
csv = true
[]
(test/tests/mesh/face_info/face_info_quads.i)
[Mesh]
[generated]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
nx = 3
ymin = -2
ymax = 3
ny = 5
[]
[]
[Problem]
kernel_coverage_check = false
[]
[Variables]
[u]
[]
[trigger_fv_on]
fv = true
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxVariables]
[v]
family = MONOMIAL
order = CONSTANT
[]
[]
[VectorPostprocessors]
[face_info]
type = TestFaceInfo
vars = 'u v'
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
[]
(test/tests/meshgenerators/boundary_deletion_generator/boundary_deletion.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 2
[]
[boundary_removal]
type = BoundaryDeletionGenerator
input = gmg
boundary_names = 'right top'
[]
allow_renumbering = false
[]
[Reporters/mesh_info]
type = MeshInfo
items = sideset_elems
[]
[Outputs]
[out]
type = JSON
execute_system_information_on = NONE
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
(test/tests/multiapps/secant_postprocessor/steady_sub.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
parallel_type = replicated
uniform_refine = 1
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[sink]
type = BodyForce
variable = u
value = -1
[]
[]
[BCs]
[right]
type = PostprocessorDirichletBC
variable = u
boundary = right
postprocessor = 'from_main'
[]
[]
[Postprocessors]
[from_main]
type = Receiver
default = 0
[]
[to_main]
type = SideAverageValue
variable = u
boundary = left
[]
[average]
type = ElementAverageValue
variable = u
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
nl_abs_tol = 1e-14
fixed_point_algorithm = 'secant'
[]
[Outputs]
csv = true
exodus = false
[]
(test/tests/restart/restartable_types/restartable_types2.i)
###########################################################
# This is a simple test of the restart/recover capability.
# The test object "RestartableTypesChecker" is used
# to reload data from a previous simulation written out
# with the object "RestartableTypes".
#
# See "restartable_types.i"
#
# @Requirement F1.60
###########################################################
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[UserObjects]
[./restartable_types]
type = RestartableTypesChecker
[../]
[]
[Problem]
type = FEProblem
solve = false
restart_file_base = restartable_types_out_cp/LATEST
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/variables/fe_monomial_const/monomial-const-2d.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 100
ny = 100
elem_type = QUAD4
[]
[Functions]
[./bc_fn]
type=ParsedFunction
value=0
[../]
[./bc_fnt]
type = ParsedFunction
value = 0
[../]
[./bc_fnb]
type = ParsedFunction
value = 0
[../]
[./bc_fnl]
type = ParsedFunction
value = 0
[../]
[./bc_fnr]
type = ParsedFunction
value = 0
[../]
[./forcing_fn]
# type = ParsedFunction
# value = 0
type = MTPiecewiseConst2D
[../]
[./solution]
type = MTPiecewiseConst2D
[../]
[]
[Variables]
[./u]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
active = 'diff forcing reaction'
[./diff]
type = Diffusion
variable = u
[../]
[./reaction]
type = Reaction
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
# Note: MOOSE's DirichletBCs do not work properly with shape functions that do not
# have DOFs at the element edges. This test works because the solution
# has been designed to be zero at the boundary which is satisfied by the IC
# Ticket #1352
active = ''
[./bc_all]
type=FunctionDirichletBC
variable = u
boundary = 'top bottom left right'
function = bc_fn
[../]
[./bc_top]
type = FunctionNeumannBC
variable = u
boundary = 'top'
function = bc_fnt
[../]
[./bc_bottom]
type = FunctionNeumannBC
variable = u
boundary = 'bottom'
function = bc_fnb
[../]
[./bc_left]
type = FunctionNeumannBC
variable = u
boundary = 'left'
function = bc_fnl
[../]
[./bc_right]
type = FunctionNeumannBC
variable = u
boundary = 'right'
function = bc_fnr
[../]
[]
[Postprocessors]
[./dofs]
type = NumDOFs
[../]
[./h]
type = AverageElementSize
[../]
[./L2error]
type = ElementL2Error
variable = u
function = solution
[../]
[./H1error]
type = ElementH1Error
variable = u
function = solution
[../]
[./H1Semierror]
type = ElementH1SemiError
variable = u
function = solution
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
nl_rel_tol = 1.e-10
[./Adaptivity]
[../]
[]
[Outputs]
execute_on = 'timestep_end'
csv = true
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[]
(test/tests/nodalkernels/penalty_dirichlet/nodal_penalty_dirichlet.i)
#In order to compare the solution generated using preset BC, the penalty was set to 1e10.
#Large penalty number should be used with caution.
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 10
ny = 10
elem_type = QUAD4
[]
[Functions]
[./forcing_fn]
type = ParsedFunction
value = -2*(x*x+y*y-2)
[../]
[./solution]
type = ParsedGradFunction
value = (1-x*x)*(1-y*y)
grad_x = 2*(x*y*y-x)
grad_y = 2*(x*x*y-y)
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[NodalKernels]
[./bc_all]
type = PenaltyDirichletNodalKernel
variable = u
value = 0
boundary = 'top left right bottom'
penalty = 1e10
[../]
[]
# [BCs]
# [./fix]
# type = DirichletBC
# preset = true
# variable = u
# value = 0
# boundary = 'top left right bottom'
# [../]
# []
[Postprocessors]
[./L2error]
type = ElementL2Error
variable = u
function = solution
[../]
[./H1error]
type = ElementH1Error
variable = u
function = solution
[../]
[./H1Semierror]
type = ElementH1SemiError
variable = u
function = solution
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
nl_rel_tol = 1e-14
[]
[Outputs]
file_base = nodal_preset_bc_out
exodus = true
[]
(test/tests/meshgenerators/concentric_circle_mesh_generator/concentric_circle_mesh2.i)
[Mesh]
[ccmg]
type = ConcentricCircleMeshGenerator
num_sectors = 6
radii = '0.2546 0.3368 0.3600 0.3818 0.3923 0.4025 0.4110 0.4750'
rings = '5 3 2 1 1 1 1 3 5'
has_outer_square = on
pitch = 1.42063
#portion = left_half
preserve_volumes = off
smoothing_max_it = 3
[]
[]
[AuxVariables]
[winding_order]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[winding_order]
type = WindingOrder
variable = winding_order
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Postprocessors]
[min_winding_order]
type = ElementExtremeValue
value_type = min
variable = winding_order
[]
[max_winding_order]
type = ElementExtremeValue
value_type = max
variable = winding_order
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
csv = true
hide = winding_order
[]
(test/tests/vectorpostprocessors/nearest_point_integral/nearest_point_integral.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 10
ny = 10
nz = 10
[]
[Variables]
[u]
[]
[]
[AuxVariables]
[np_layered_average]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[AuxKernels]
[np_layered_average]
type = SpatialUserObjectAux
variable = np_layered_average
execute_on = timestep_end
user_object = npi
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[bottom]
type = DirichletBC
variable = u
boundary = bottom
value = 1.5
[]
[one]
type = DirichletBC
variable = u
boundary = 'right back top'
value = 1
[]
[]
[VectorPostprocessors]
[npi]
type = NearestPointIntegralVariablePostprocessor
variable = u
points = '0.25 0.25 0.25
0.75 0.25 0.25
0.25 0.75 0.75
0.75 0.75 0.75'
[]
# getting the points from the user object itself is here exactly equivalent to the points
# provided in the 'spatial_manually_provided' vector postprocessor
[spatial_from_uo]
type = SpatialUserObjectVectorPostprocessor
userobject = npi
[]
[spatial_manually_provided]
type = SpatialUserObjectVectorPostprocessor
userobject = npi
points = '0.25 0.25 0.25
0.75 0.25 0.25
0.25 0.75 0.75
0.75 0.75 0.75'
[]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
csv = true
execute_on = final
[]
(modules/tensor_mechanics/test/tests/ad_elastic/green-lagrange.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 3
ny = 3
nz = 4
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[Kernels]
[./stress_x]
type = ADStressDivergenceTensors
component = 0
variable = disp_x
[../]
[./stress_y]
type = ADStressDivergenceTensors
component = 1
variable = disp_y
[../]
[./stress_z]
type = ADStressDivergenceTensors
component = 2
variable = disp_z
[../]
[]
[BCs]
[./symmy]
type = DirichletBC
variable = disp_y
boundary = back
value = 0
[../]
[./symmx]
type = DirichletBC
variable = disp_x
boundary = back
value = 0
[../]
[./symmz]
type = DirichletBC
variable = disp_z
boundary = back
value = 0
[../]
[./tdisp]
type = DirichletBC
variable = disp_z
boundary = front
value = 0.3
[../]
[]
[Materials]
[./elasticity]
type = ADComputeIsotropicElasticityTensor
poissons_ratio = 0.45
youngs_modulus = 1
[../]
[]
[Materials]
[./strain]
type = ADComputeGreenLagrangeStrain
[../]
[./stress]
type = ADComputeLinearElasticStress
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
execute_on = 'FINAL'
exodus = true
[]
(modules/richards/test/tests/jacobian_1/jn_fu_07.i)
# unsaturated = false
# gravity = true
# supg = true
# transient = false
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = -1
xmax = 1
ymin = -1
ymax = 1
zmin = -1
zmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGstandard
sat_UO = Saturation
seff_UO = SeffVG
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0 # notice small quantity, so the PETSc constant state works
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1 # notice small quantity, so the PETSc constant state works
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.2
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 0.1
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = RandomIC
block = 0
min = 0
max = 1
[../]
[../]
[]
[Kernels]
active = 'richardsf'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFullyUpwindFlux
variable = pressure
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
viscosity = 1E-3
gravity = '1 2 3'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -snes_type'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000 test'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = jn07
exodus = false
[]
(modules/functional_expansion_tools/test/tests/errors/multiple_series_duo.i)
[Mesh]
type = GeneratedMesh
dim = 3
[]
[Functions]
[./series]
type = FunctionSeries
series_type = CylindricalDuo
orders = '0 1'
physical_bounds = '-1.0 1.0 0.0 0.0 1'
x = Legendre
disc = Zernike
y = Legendre
[../]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
(test/tests/meshgenerators/mesh_extruder_generator/gen_extrude.i)
[Mesh]
[./gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 6
ny = 6
nz = 0
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[./extrude]
type = MeshExtruderGenerator
input = gmg
num_layers = 6
extrusion_vector = '1 0 1'
bottom_sideset = 'new_front'
top_sideset = 'new_back'
[]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./first]
type = DirichletBC
variable = u
boundary = 'new_front'
value = 0
[../]
[./second]
type = DirichletBC
variable = u
boundary = 'new_back'
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/action/two_block.i)
[Mesh]
[generated_mesh]
type = GeneratedMeshGenerator
dim = 2
nx = 4
ny = 4
[]
[block1]
type = SubdomainBoundingBoxGenerator
block_id = 1
bottom_left = '0 0 0'
top_right = '0.5 1 0'
input = generated_mesh
[]
[block2]
type = SubdomainBoundingBoxGenerator
block_id = 2
bottom_left = '0.5 0 0'
top_right = '1 1 0'
input = block1
[]
[]
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Modules/TensorMechanics/Master]
[./block1]
strain = FINITE
add_variables = true
#block = 1
[../]
[./block2]
strain = SMALL
add_variables = true
block = 2
[../]
[]
[AuxVariables]
[./stress_theta]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_theta]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./stress_theta]
type = RankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 2
variable = stress_theta
execute_on = timestep_end
[../]
[./strain_theta]
type = RankTwoAux
rank_two_tensor = total_strain
index_i = 2
index_j = 2
variable = strain_theta
execute_on = timestep_end
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e10
poissons_ratio = 0.345
[../]
[./_elastic_stress1]
type = ComputeFiniteStrainElasticStress
block = 1
[../]
[./_elastic_stress2]
type = ComputeLinearElasticStress
block = 2
[../]
[]
[BCs]
[./left]
type = DirichletBC
boundary = 'left'
variable = disp_x
value = 0.0
[../]
[./top]
type = DirichletBC
boundary = 'top'
variable = disp_y
value = 0.0
[../]
[./right]
type = DirichletBC
boundary = 'right'
variable = disp_x
value = 0.01
[../]
[./bottom]
type = DirichletBC
boundary = 'bottom'
variable = disp_y
value = 0.01
[../]
[]
[Debug]
show_var_residual_norms = true
[]
[Executioner]
type = Steady
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = ' 201 hypre boomeramg 10'
line_search = 'none'
nl_rel_tol = 5e-9
nl_abs_tol = 1e-10
nl_max_its = 15
l_tol = 1e-3
l_max_its = 50
[]
[Outputs]
exodus = true
[]
(test/tests/ics/dependency/test.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
[]
[AuxVariables]
[./a]
[../]
[./b]
[../]
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[ICs]
[./u_ic]
type = ConstantIC
variable = u
value = -1
[../]
[./v_ic]
type = MTICSum
variable = v
var1 = u
var2 = a
[../]
[./a_ic]
type = ConstantIC
variable = a
value = 10
[../]
[./b_ic]
type = MTICMult
variable = b
var1 = v
factor = 2
[../]
[]
[AuxKernels]
[./a_ak]
type = ConstantAux
variable = a
value = 256
[../]
[./b_ak]
type = ConstantAux
variable = b
value = 42
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[BCs]
[./left_u]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = left
value = 2
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
nl_rel_tol = 1e-10
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/xda/xda.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
xda = true
[]
(test/tests/controls/syntax_based_naming_access/param.i)
[Mesh]
type = GeneratedMesh
dim = 2
elem_type = QUAD4
# use odd numbers so points do not fall on element boundaries
nx = 31
ny = 31
[]
[Variables]
[./diffused]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = diffused
[../]
[]
[DiracKernels]
[./test_object]
type = MaterialPointSource
point = '0.5 0.5 0'
variable = diffused
[../]
[]
[BCs]
[./bottom_diffused]
type = DirichletBC
variable = diffused
boundary = 'bottom'
value = 2
[../]
[./top_diffused]
type = DirichletBC
variable = diffused
boundary = 'top'
value = 0
[../]
[]
[Materials]
[./mat]
type = GenericConstantMaterial
prop_names = 'matp'
prop_values = '1'
block = 0
[../]
[]
[Postprocessors]
[./test_object]
type = FunctionValuePostprocessor
function = '2*(x+y)'
point = '0.5 0.5 0'
[../]
[./other_point_test_object]
type = FunctionValuePostprocessor
function = '3*(x+y)'
point = '0.5 0.5 0'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
[Controls]
[./point_control]
type = TestControl
test_type = 'point'
parameter = '*/*/point'
execute_on = 'initial'
[../]
[]
(test/tests/meshgenerators/subdomain_bounding_box_generator/bounding_box_integers.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
xmax = 1
ymax = 1
extra_element_integers = test_id
[]
[subdomains]
type = SubdomainBoundingBoxGenerator
input = gmg
bottom_left = '0 0 0'
block_id = 1
top_right = '0.9 0.9 0'
integer_name = test_id
[]
[another_subdomains]
type = SubdomainBoundingBoxGenerator
input = subdomains
bottom_left = '0 0 0'
block_id = 2
top_right = '0.9 0.9 0'
location = OUTSIDE
integer_name = test_id
[]
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[AuxVariables]
[test_id]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[test_id]
type = ExtraElementIDAux
variable = test_id
extra_id_name = test_id
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/transfers/multiapp_high_order_variable_transfer/sub_L2_Lagrange.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
[]
[AuxVariables]
[./power_density]
family = L2_LAGRANGE
order = FIRST
[../]
[]
[Variables]
[./temp]
[../]
[]
[Kernels]
[./heat_conduction]
type = Diffusion
variable = temp
[../]
[./heat_source_fuel]
type = CoupledForce
variable = temp
v = power_density
[../]
[]
[BCs]
[bc]
type = DirichletBC
variable = temp
boundary = '0 1 2 3'
value = 450
[]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart '
petsc_options_value = 'hypre boomeramg 100'
nl_abs_tol = 1e-7
nl_rel_tol = 1e-7
[]
[Postprocessors]
[./temp_fuel_avg]
type = ElementAverageValue
variable = temp
block = '0'
execute_on = 'initial timestep_end'
[../]
[./pwr_density]
type = ElementIntegralVariablePostprocessor
block = '0'
variable = power_density
execute_on = 'initial timestep_end'
[../]
[]
[Outputs]
perf_graph = true
exodus = true
color = true
[]
(modules/richards/test/tests/jacobian_1/jn_fu_01.i)
# unsaturated = false
# gravity = false
# supg = false
# transient = false
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = -1
xmax = 1
ymin = -1
ymax = 1
zmin = -1
zmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGnone
sat_UO = Saturation
seff_UO = SeffVG
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0 # notice small quantity, so the PETSc constant state works
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1 # notice small quantity, so the PETSc constant state works
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.2
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGnone]
type = RichardsSUPGnone
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = RandomIC
block = 0
min = 0
max = 1
[../]
[../]
[]
[Kernels]
active = 'richardsf'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFullyUpwindFlux
variable = pressure
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
viscosity = 1E-3
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -snes_type'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000 test'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = jn01
exodus = false
[]
(examples/ex11_prec/fdp.i)
[Mesh]
file = square.e
[]
[Variables]
[./diffused]
order = FIRST
family = LAGRANGE
[../]
[./forced]
order = FIRST
family = LAGRANGE
[../]
[]
# The Preconditioning block
[Preconditioning]
active = 'FDP_jfnk'
[./FDP_jfnk]
type = FDP
off_diag_row = 'forced'
off_diag_column = 'diffused'
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -mat_fd_coloring_err -mat_fd_type'
petsc_options_value = 'lu 1e-6 ds'
[../]
[./FDP_n]
type = FDP
off_diag_row = 'forced'
off_diag_column = 'diffused'
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -mat_fd_coloring_err -mat_fd_type'
petsc_options_value = 'lu 1e-6 ds'
[../]
[./FDP_n_full]
type = FDP
full = true
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -mat_fd_coloring_err -mat_fd_type'
petsc_options_value = 'lu 1e-6 ds'
[../]
[]
[Kernels]
[./diff_diffused]
type = Diffusion
variable = diffused
[../]
[./conv_forced]
type = CoupledForce
variable = forced
v = diffused
[../]
[./diff_forced]
type = Diffusion
variable = forced
[../]
[]
[BCs]
#Note we have active on, and neglect the right_forced BC
active = 'left_diffused right_diffused left_forced'
[./left_diffused]
type = DirichletBC
variable = diffused
boundary = 'left'
value = 0
[../]
[./right_diffused]
type = DirichletBC
variable = diffused
boundary = 'right'
value = 100
[../]
[./left_forced]
type = DirichletBC
variable = forced
boundary = 'left'
value = 0
[../]
[./right_forced]
type = DirichletBC
variable = forced
boundary = 'right'
value = 0
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/combined/examples/phase_field-mechanics/interface_stress.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 50
ny = 50
nz = 50
xmax = 10
ymax = 10
zmax = 10
xmin = -10
ymin = -10
zmin = -10
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Functions]
[./sphere]
type = ParsedFunction
value = 'r:=sqrt(x^2+y^2+z^2); R:=(4.0-r)/2.0; if(R>1,1,if(R<0,0,3*R^2-2*R^3))'
[../]
[]
[AuxVariables]
[./eta]
[./InitialCondition]
type = FunctionIC
function = sphere
[../]
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
generate_output = 'hydrostatic_stress stress_xx'
[../]
[]
[Materials]
[./ym]
type = DerivativeParsedMaterial
f_name = ym
function = (1-eta)*7+0.5
args = eta
[../]
[./elasticity]
type = ComputeVariableIsotropicElasticityTensor
poissons_ratio = 0.45
youngs_modulus = ym
args = eta
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[./interface]
type = ComputeInterfaceStress
v = eta
stress = 1.0
[../]
[]
[VectorPostprocessors]
[./line]
type = SphericalAverage
variable = 'hydrostatic_stress'
radius = 10
bin_number = 40
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
csv = true
[]
(test/tests/fixedbugs/i8575/test.i)
# This tests for the bug https://github.com/idaholab/moose/issues/8575.
# It makes sure that the material property dependency checking accounts for
# the fact that materials provided on "ANY_BLOCK" count as satisfying requests
# for that property on all block IDs.
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[GlobalParams]
block = 0
[]
[AddMatAndKernel]
[]
[Executioner]
type = Steady
solve_type = PJFNK
[]
(modules/porous_flow/test/tests/relperm/vangenuchten2.i)
# Test van Genuchten relative permeability curve by varying saturation over the mesh
# van Genuchten exponent m = 0.4 for both phases
# Phase 0 residual saturation s0r = 0.1
# Phase 1 residual saturation s1r = 0.2
[Mesh]
type = GeneratedMesh
dim = 1
nx = 100
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Variables]
[p0]
initial_condition = 1e6
[]
[s1]
[]
[]
[AuxVariables]
[s0aux]
family = MONOMIAL
order = CONSTANT
[]
[s1aux]
family = MONOMIAL
order = CONSTANT
[]
[kr0aux]
family = MONOMIAL
order = CONSTANT
[]
[kr1aux]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[s0]
type = PorousFlowPropertyAux
property = saturation
phase = 0
variable = s0aux
[]
[s1]
type = PorousFlowPropertyAux
property = saturation
phase = 1
variable = s1aux
[]
[kr0]
type = PorousFlowPropertyAux
property = relperm
phase = 0
variable = kr0aux
[]
[kr1]
type = PorousFlowPropertyAux
property = relperm
phase = 1
variable = kr1aux
[]
[]
[Functions]
[s1]
type = ParsedFunction
value = x
[]
[]
[ICs]
[s1]
type = FunctionIC
variable = s1
function = s1
[]
[]
[Kernels]
[p0]
type = Diffusion
variable = p0
[]
[s1]
type = Diffusion
variable = s1
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'p0 s1'
number_fluid_phases = 2
number_fluid_components = 2
[]
[pc]
type = PorousFlowCapillaryPressureConst
pc = 0
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow2PhasePS
phase0_porepressure = p0
phase1_saturation = s1
capillary_pressure = pc
[]
[kr0]
type = PorousFlowRelativePermeabilityVG
phase = 0
m = 0.4
s_res = 0.1
sum_s_res = 0.3
[]
[kr1]
type = PorousFlowRelativePermeabilityVG
phase = 1
m = 0.4
s_res = 0.2
sum_s_res = 0.3
wetting = false
[]
[]
[VectorPostprocessors]
[vpp]
type = LineValueSampler
warn_discontinuous_face_values = false
variable = 's0aux s1aux kr0aux kr1aux'
start_point = '0 0 0'
end_point = '1 0 0'
num_points = 20
sort_by = id
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
nl_abs_tol = 1e-7
[]
[BCs]
[sleft]
type = DirichletBC
variable = s1
value = 0
boundary = left
[]
[sright]
type = DirichletBC
variable = s1
value = 1
boundary = right
[]
[]
[Outputs]
csv = true
execute_on = timestep_end
[]
(test/tests/ics/check_error/two_ics_on_same_block_global.i)
[Mesh]
type = FileMesh
file = 'rectangle.e'
[]
[Variables]
[./u]
[../]
[]
[ICs]
[./block]
type = ConstantIC
variable = u
value = 2
[../]
[./block2]
type = ConstantIC
variable = u
value = 0.5
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
[]
(test/tests/reporters/perf_graph_reporter/perf_graph_reporter.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 1
ny = 1
[]
[]
[Variables/u]
[]
[Kernels/diff]
type = Diffusion
variable = u
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Reporters/perf_graph]
type = PerfGraphReporter
execute_on = FINAL
[]
[Outputs/json]
type = JSON
execute_on = 'INITIAL FINAL'
[]
(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/2d-average-with-temp.i)
mu=1.1
rho=1.1
k=1.1
cp=1.1
advected_interp_method='average'
velocity_interp_method='average'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 2
ymin = -1
ymax = 1
nx = 2
ny = 2
[]
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
two_term_boundary_expansion = false
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
two_term_boundary_expansion = false
[]
[pressure]
type = INSFVPressureVariable
two_term_boundary_expansion = false
[]
[temperature]
type = INSFVEnergyVariable
two_term_boundary_expansion = false
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[u_forcing]
type = INSFVBodyForce
variable = u
functor = forcing_u
momentum_component = 'x'
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[v_forcing]
type = INSFVBodyForce
variable = v
functor = forcing_v
momentum_component = 'y'
[]
[temp_conduction]
type = FVDiffusion
coeff = 'k'
variable = temperature
[]
[temp_advection]
type = INSFVEnergyAdvection
variable = temperature
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
[]
[temp_forcing]
type = FVBodyForce
variable = temperature
function = forcing_t
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = 'exact_u'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = 'exact_v'
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = u
function = 'exact_u'
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = v
function = 'exact_v'
[]
[inlet-and-walls-t]
type = FVFunctionDirichletBC
boundary = 'left top bottom'
variable = temperature
function = 'exact_t'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 'exact_p'
[]
[]
[Materials]
[const]
type = ADGenericFunctorMaterial
prop_names = 'k cp'
prop_values = '${k} ${cp}'
[]
[ins_fv]
type = INSFVEnthalpyMaterial
temperature = 'temperature'
rho = ${rho}
[]
[]
[Functions]
[exact_u]
type = ParsedFunction
value = 'sin((1/2)*y*pi)*cos((1/2)*x*pi)'
[]
[exact_rhou]
type = ParsedFunction
value = 'rho*sin((1/2)*y*pi)*cos((1/2)*x*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_u]
type = ADParsedFunction
value = '(1/2)*pi^2*mu*sin((1/2)*y*pi)*cos((1/2)*x*pi) - 1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi) + (1/2)*pi*rho*sin((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)^2 - pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi) - 1/4*pi*sin((1/4)*x*pi)*sin((3/2)*y*pi)'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_v]
type = ParsedFunction
value = 'sin((1/4)*x*pi)*cos((1/2)*y*pi)'
[]
[exact_rhov]
type = ParsedFunction
value = 'rho*sin((1/4)*x*pi)*cos((1/2)*y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_v]
type = ADParsedFunction
value = '(5/16)*pi^2*mu*sin((1/4)*x*pi)*cos((1/2)*y*pi) - pi*rho*sin((1/4)*x*pi)^2*sin((1/2)*y*pi)*cos((1/2)*y*pi) - 1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*y*pi) + (1/4)*pi*rho*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi) + (3/2)*pi*cos((1/4)*x*pi)*cos((3/2)*y*pi)'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_p]
type = ParsedFunction
value = 'sin((3/2)*y*pi)*cos((1/4)*x*pi)'
[]
[forcing_p]
type = ParsedFunction
value = '-1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi) - 1/2*pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[exact_t]
type = ParsedFunction
value = 'sin((1/4)*x*pi)*cos((1/2)*y*pi)'
[]
[forcing_t]
type = ParsedFunction
value = '-pi*cp*rho*sin((1/4)*x*pi)^2*sin((1/2)*y*pi)*cos((1/2)*y*pi) - 1/2*pi*cp*rho*sin((1/4)*x*pi)*sin((1/2)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*y*pi) + (1/4)*pi*cp*rho*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi) + (5/16)*pi^2*k*sin((1/4)*x*pi)*cos((1/2)*y*pi)'
vars = 'k rho cp'
vals = '${k} ${rho} ${cp}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[./L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2v]
type = ElementL2Error
variable = v
function = exact_v
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2p]
variable = pressure
function = exact_p
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2t]
variable = temperature
function = exact_t
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[]
(test/tests/meshgenerators/fancy_extruder_generator/fancy_extruder_with_element_extra_integer_swap.i)
[Problem]
solve = false
[]
[Mesh]
[./fg]
type = FileMeshGenerator
file = mesh_2d.e
exodus_extra_element_integers = 'element_extra_integer_1 element_extra_integer_2'
[]
[./extrude]
type = FancyExtruderGenerator
input = fg
heights = '1 2 3'
num_layers = '1 2 3'
direction = '0 0 1'
elem_integer_names_to_swap = 'element_extra_integer_1 element_extra_integer_2'
elem_integers_swaps = '1 4 2 8;
2 7;
1 6;
1 8 2 4;
2 5;
1 6'
[]
[]
[AuxVariables]
[element_extra_integer_1]
family = MONOMIAL
order = CONSTANT
[]
[element_extra_integer_2]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[element_extra_integer_1]
type = ExtraElementIDAux
variable = element_extra_integer_1
extra_id_name = element_extra_integer_1
execute_on = 'initial'
[]
[element_extra_integer_2]
type = ExtraElementIDAux
variable = element_extra_integer_2
extra_id_name = element_extra_integer_2
execute_on = 'initial'
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
execute_on = final
[]
(test/tests/postprocessors/element_extreme_functor_value/extreme_proxy_value.i)
[Problem]
type = FEProblem
solve = false
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 40
ny = 40
[]
[AuxVariables]
[u]
type = MooseVariableFVReal
[]
[w]
type = MooseVariableFVReal
[]
[v_x]
type = MooseVariableFVReal
[]
[v_y]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[u]
type = FunctionAux
variable = u
function = u_f
[]
[w]
type = FunctionAux
variable = w
function = w_f
[]
[v_x]
type = FunctionAux
variable = v_x
function = v_x_f
[]
[v_y]
type = FunctionAux
variable = v_y
function = v_y_f
[]
[]
[Functions]
[u_f] # reaches a maximum value at (0.5, 0.6)
type = ParsedFunction
value = 'sin(pi*x)*sin(pi*y/1.2)'
[]
[w_f] # reaches a minium value at (0.7, 0.8)
type = ParsedFunction
value = '-sin(pi*x/1.4)*sin(pi*y/1.6)'
[]
[v_x_f]
type = ParsedFunction
value = 'x'
[]
[v_y_f]
type = ParsedFunction
value = 'y'
[]
[]
[Postprocessors]
[max_u]
type = ADElementExtremeFunctorValue
functor = 'u'
[]
[min_w_f]
type = ElementExtremeFunctorValue
functor = 'w_f'
value_type = min
[]
[max_v_x]
type = ADElementExtremeFunctorValue
functor = 'v_x'
[]
[min_v_y]
type = ADElementExtremeFunctorValue
functor = 'v_y'
value_type = min
[]
# because we set v_x and v_y equal to the x and y coordinates, these two postprocessors
# should just return the point at which u reaches a maximum value
[max_v_from_proxy_x]
type = ADElementExtremeFunctorValue
functor = v_x
proxy_functor = u
value_type = max
[]
[max_v_from_proxy_y]
type = ADElementExtremeFunctorValue
functor = v_y
proxy_functor = u
value_type = max
[]
# because we set v_x and v_y equal to the x and y coordinates, these two postprocessors
# should just return the point at which w reaches a minimum value
[min_v_from_proxy_x]
type = ADElementExtremeFunctorValue
functor = v_x
proxy_functor = w
value_type = min
[]
[min_v_from_proxy_y]
type = ADElementExtremeFunctorValue
functor = v_y
proxy_functor = w
value_type = min
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
[]
(modules/fluid_properties/test/tests/materials/ad_surface_tension_material/ad_surface_tension_material.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
xmin = 0
xmax = 1
[]
[Modules]
[./FluidProperties]
[./fp_2phase]
type = StiffenedGasTwoPhaseFluidProperties
[../]
[../]
[]
[Materials]
[./T_mat]
type = ADGenericConstantMaterial
prop_names = 'T_test'
prop_values = '300'
[../]
[./sigma_mat]
type = ADSurfaceTensionMaterial
T = T_test
surface_tension = surface_tension_test
fp_2phase = fp_2phase
[../]
[]
[Postprocessors]
[./surface_tension_test_pp]
type = ADElementIntegralMaterialProperty
mat_prop = surface_tension_test
execute_on = 'INITIAL'
[../]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
execute_on = 'INITIAL'
[]
(test/tests/outputs/debug/show_top_residuals_debug.i)
[Mesh]
block_id = '0 1'
block_name = 'block_zero block_one'
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 2
[]
[./subdomain_id]
input = gen
type = SubdomainIDGenerator
subdomain_id = 1
[../]
[]
[Variables]
[./u]
family = LAGRANGE
order = FIRST
[../]
[./v]
family = MONOMIAL
order = CONSTANT
[../]
[./w]
family = SCALAR
order = FIRST
[../]
[]
[Kernels]
[./u_kernel]
type = Diffusion
variable = u
[../]
[./v_kernel]
type = Diffusion
variable = v
[../]
[]
[BCs]
[./u_bc]
type = DirichletBC
variable = u
value = 100
boundary = left
[../]
[./v_bc]
type = NeumannBC
variable = v
value = 100
boundary = left
[../]
[]
[ScalarKernels]
[./w_kernel]
type = AlphaCED
variable = w
value = 100
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
# For this test, we don't actually want the solution to converge because we
# want nonzero nonlinear residual entries at the end of the time step.
nl_abs_tol = 0.999
nl_rel_tol = 0.999
l_max_its = 1
petsc_options_iname = '-pc_type'
petsc_options_value = 'none'
[]
[Debug]
show_top_residuals = 10
[]
(test/tests/variables/side_hierarchic/side_hierarchic.i)
[Problem]
solve = false
[]
[Mesh]
type = GeneratedMesh
elem_type = QUAD9
dim = 2
nx = 2
ny = 2
[]
[Variables]
[./side_var]
order = CONSTANT
family = SIDE_HIERARCHIC
[../]
[]
[AuxVariables]
[./aux_side_var]
order = FIRST
family = SIDE_HIERARCHIC
[../]
[]
[Functions]
[./nl_var]
type = ParsedFunction
value = 'x+y+1'
[../]
[./aux_var]
type = ParsedFunction
value = 'x-y+10'
[../]
[]
[ICs]
[./side_nl]
type = FunctionIC
variable = side_var
function = nl_var
[../]
[./side_aux]
type = FunctionIC
variable = aux_side_var
function = aux_var
[../]
[]
[Outputs]
exodus = true
[]
[Executioner]
type = Steady
[]
(modules/navier_stokes/test/tests/finite_element/ins/velocity_channel/velocity_inletBC_no_parts.i)
# This input file tests outflow boundary conditions for the incompressible NS equations.
[GlobalParams]
gravity = '0 0 0'
integrate_p_by_parts = false
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 3.0
ymin = 0
ymax = 1.0
nx = 30
ny = 10
elem_type = QUAD9
[]
[./corner_node]
type = ExtraNodesetGenerator
new_boundary = top_right
coord = '3 1'
input = gen
[../]
[]
[Variables]
[./vel_x]
order = SECOND
family = LAGRANGE
[../]
[./vel_y]
order = SECOND
family = LAGRANGE
[../]
[./p]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./mass]
type = INSMass
variable = p
u = vel_x
v = vel_y
pressure = p
[../]
[./x_momentum_space]
type = INSMomentumLaplaceForm
variable = vel_x
u = vel_x
v = vel_y
pressure = p
component = 0
[../]
[./y_momentum_space]
type = INSMomentumLaplaceForm
variable = vel_y
u = vel_x
v = vel_y
pressure = p
component = 1
[../]
[]
[BCs]
[./x_no_slip]
type = DirichletBC
variable = vel_x
boundary = 'top bottom'
value = 0.0
[../]
[./y_no_slip]
type = DirichletBC
variable = vel_y
boundary = 'left top bottom'
value = 0.0
[../]
[./x_inlet]
type = FunctionDirichletBC
variable = vel_x
boundary = 'left'
function = 'inlet_func'
[../]
[./p_corner]
# Since the pressure is not integrated by parts in this example,
# it is only specified up to a constant by the natural outflow BC.
# Therefore, we need to pin its value at a single location.
type = DirichletBC
boundary = top_right
value = 0
variable = p
[../]
[]
[Materials]
[./const]
type = GenericConstantMaterial
block = 0
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[]
[Preconditioning]
[./SMP_PJFNK]
type = SMP
full = true
solve_type = NEWTON
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-ksp_gmres_restart -pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = '300 bjacobi ilu 4'
line_search = none
nl_rel_tol = 1e-12
nl_max_its = 6
l_tol = 1e-6
l_max_its = 300
[]
[Outputs]
[./out]
type = Exodus
[../]
[]
[Functions]
[./inlet_func]
type = ParsedFunction
value = '-4 * (y - 0.5)^2 + 1'
[../]
[]
(test/tests/multiapps/steffensen/steady_sub.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[v]
[]
[]
[AuxVariables]
[u]
[]
[]
[Kernels]
[diff_v]
type = Diffusion
variable = v
[]
[force_v]
type = CoupledForce
variable = v
v = u
[]
[]
[BCs]
[left_v]
type = DirichletBC
variable = v
boundary = left
value = 1
[]
[right_v]
type = DirichletBC
variable = v
boundary = right
value = 0
[]
[]
[Postprocessors]
[vnorm]
type = ElementL2Norm
variable = v
[]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
nl_abs_tol = 1e-14
fixed_point_algorithm = 'steffensen'
[]
[Outputs]
csv = true
exodus = false
[]
(modules/heat_conduction/test/tests/code_verification/spherical_test_no2.i)
# Problem III.2
#
# A spherical shell has a thermal conductivity that varies linearly
# with temperature. The inside and outside surfaces of the shell are
# exposed to constant temperatures.
#
# REFERENCE:
# A. Toptan, et al. (Mar.2020). Tech. rep. CASL-U-2020-1939-000, SAND2020-3887 R. DOI:10.2172/1614683.
[Mesh]
[./geom]
type = GeneratedMeshGenerator
dim = 1
elem_type = EDGE2
xmin = 0.2
nx = 4
[../]
[]
[Variables]
[./u]
order = FIRST
[../]
[]
[Problem]
coord_type = RSPHERICAL
[]
[Functions]
[./exact]
type = ParsedFunction
vars = 'ri ro beta ki ko ui uo'
vals = '0.2 1.0 1e-3 5.3 5 300 0'
value = 'uo+(ko/beta)* ( ( 1 + beta*(ki+ko)*(ui-uo)*( (1/x-1/ro) / (1/ri-1/ro) )/(ko^2))^0.5 -1 )'
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = u
[../]
[]
[BCs]
[./ui]
type = DirichletBC
boundary = left
variable = u
value = 300
[../]
[./uo]
type = DirichletBC
boundary = right
variable = u
value = 0
[../]
[]
[Materials]
[./property]
type = GenericConstantMaterial
prop_names = 'density specific_heat'
prop_values = '1.0 1.0'
[../]
[./thermal_conductivity]
type = ParsedMaterial
f_name = 'thermal_conductivity'
args = u
function = '5 + 1e-3 * (u-0)'
[../]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[./error]
type = ElementL2Error
function = exact
variable = u
[../]
[./h]
type = AverageElementSize
[]
[]
[Outputs]
csv = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/boussinesq/boussinesq_stabilized.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmax = .05
ymax = .05
nx = 20
ny = 20
elem_type = QUAD9
[]
[./bottom_left]
type = ExtraNodesetGenerator
new_boundary = corner
coord = '0 0'
input = gen
[../]
[]
[Preconditioning]
[./Newton_SMP]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-12
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_shift_type -ksp_gmres_restart'
petsc_options_value = 'bjacobi lu NONZERO 200'
[]
[Debug]
show_var_residual_norms = true
[]
[Outputs]
[out]
type = Exodus
execute_on = 'final'
[]
[]
[Variables]
[velocity]
family = LAGRANGE_VEC
[]
[p][]
[temp]
initial_condition = 340
scaling = 1e-4
[]
[]
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[BCs]
[./velocity_dirichlet]
type = VectorDirichletBC
boundary = 'left right bottom top'
variable = velocity
# The third entry is to satisfy RealVectorValue
values = '0 0 0'
[../]
# Even though we are integrating by parts, because there are no integrated
# boundary conditions on the velocity p doesn't appear in the system of
# equations. Thus we must pin the pressure somewhere in order to ensure a
# unique solution
[./p_zero]
type = DirichletBC
boundary = corner
variable = p
value = 0
[../]
[./cold]
type = DirichletBC
variable = temp
boundary = left
value = 300
[../]
[./hot]
type = DirichletBC
variable = temp
boundary = right
value = 400
[../]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[mass_pspg]
type = INSADMassPSPG
variable = p
[]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[momentum_advection]
type = INSADMomentumAdvection
variable = velocity
[]
[momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
integrate_p_by_parts = true
[]
[./buoyancy]
type = INSADBoussinesqBodyForce
variable = velocity
temperature = temp
gravity = '0 -9.81 0'
[../]
[./gravity]
type = INSADGravityForce
variable = velocity
gravity = '0 -9.81 0'
[../]
[supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[]
[temp_advection]
type = INSADEnergyAdvection
variable = temp
[]
[temp_conduction]
type = ADHeatConduction
variable = temp
thermal_conductivity = 'k'
[../]
[temp_supg]
type = INSADEnergySUPG
variable = temp
velocity = velocity
[]
[]
[Materials]
[./ad_const]
type = ADGenericConstantMaterial
# alpha = coefficient of thermal expansion where rho = rho0 -alpha * rho0 * delta T
prop_names = 'mu rho alpha k cp'
prop_values = '30.74e-6 .5757 2.9e-3 46.38e-3 1054'
[../]
[./const]
type = GenericConstantMaterial
prop_names = 'temp_ref'
prop_values = '900'
[../]
[ins_mat]
type = INSADStabilized3Eqn
velocity = velocity
pressure = p
temperature = temp
[]
[]
(modules/navier_stokes/test/tests/finite_element/ins/boussinesq/boussinesq_square.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmax = .05
ymax = .05
nx = 20
ny = 20
elem_type = QUAD9
[]
[./bottom_left]
type = ExtraNodesetGenerator
new_boundary = corner
coord = '0 0'
input = gen
[../]
[]
[Preconditioning]
[./Newton_SMP]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-12
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_shift_type -ksp_gmres_restart'
petsc_options_value = 'bjacobi lu NONZERO 200'
[]
[Debug]
show_var_residual_norms = true
[]
[Outputs]
[out]
type = Exodus
execute_on = 'final'
[]
[]
[Variables]
[velocity]
family = LAGRANGE_VEC
order = SECOND
[]
[p][]
[./temp]
order = SECOND
initial_condition = 340
scaling = 1e-4
[../]
[]
[BCs]
[./velocity_dirichlet]
type = VectorDirichletBC
boundary = 'left right bottom top'
variable = velocity
# The third entry is to satisfy RealVectorValue
values = '0 0 0'
[../]
# Even though we are integrating by parts, because there are no integrated
# boundary conditions on the velocity p doesn't appear in the system of
# equations. Thus we must pin the pressure somewhere in order to ensure a
# unique solution
[./p_zero]
type = DirichletBC
boundary = corner
variable = p
value = 0
[../]
[./cold]
type = DirichletBC
variable = temp
boundary = left
value = 300
[../]
[./hot]
type = DirichletBC
variable = temp
boundary = right
value = 400
[../]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[momentum_advection]
type = INSADMomentumAdvection
variable = velocity
[]
[momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
integrate_p_by_parts = true
[]
[temp_advection]
type = INSADEnergyAdvection
variable = temp
[]
[temp_conduction]
type = ADHeatConduction
variable = temp
thermal_conductivity = 'k'
[../]
[./buoyancy]
type = INSADBoussinesqBodyForce
variable = velocity
temperature = temp
gravity = '0 -9.81 0'
[../]
[./gravity]
type = INSADGravityForce
variable = velocity
gravity = '0 -9.81 0'
[../]
[]
[Materials]
[./ad_const]
type = ADGenericConstantMaterial
# alpha = coefficient of thermal expansion where rho = rho0 -alpha * rho0 * delta T
prop_names = 'mu rho alpha k cp'
prop_values = '30.74e-6 .5757 2.9e-3 46.38e-3 1054'
[../]
[./const]
type = GenericConstantMaterial
prop_names = 'temp_ref'
prop_values = '900'
[../]
[ins_mat]
type = INSAD3Eqn
velocity = velocity
pressure = p
temperature = temp
[]
[]
(modules/thermal_hydraulics/test/tests/utils/smooth_transition/ad_smooth_transition.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 100
xmin = -2
xmax = 2
[]
[Variables]
[u]
[]
[]
[ICs]
[u_ic]
type = FunctionIC
variable = u
function = u_ic_fn
[]
[]
[Functions]
[u_ic_fn]
type = ParsedFunction
value = 'x'
[]
[]
[Materials]
[test_mat]
type = ADSmoothTransitionTestMaterial
transition_type = weighted
var = u
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[VectorPostprocessors]
[test_vpp]
type = ADSampler1DReal
block = 0
property = myadmatprop
sort_by = x
execute_on = 'INITIAL'
[]
[]
[Outputs]
csv = true
file_base = 'ad_weighted'
execute_on = 'INITIAL'
[]
(modules/combined/test/tests/linear_elasticity/applied_strain.i)
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
nz = 0
xmin = 0
xmax = 2
ymin = 0
ymax = 2
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Modules/TensorMechanics/Master/All]
strain = SMALL
eigenstrain_names = eigenstrain
add_variables = true
generate_output = 'strain_xx strain_yy strain_xy'
[]
[Materials]
[./elasticity_tensor]
type = ComputeElasticityTensor
fill_method = symmetric9
C_ijkl = '1e6 0 0 1e6 0 1e6 .5e6 .5e6 .5e6'
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[./eigenstrain]
type = ComputeEigenstrain
eigen_base = '0.1 0.05 0 0 0 0.01'
prefactor = -1
eigenstrain_name = eigenstrain
[../]
[]
[BCs]
[./bottom_y]
type = DirichletBC
variable = disp_y
boundary = 'bottom'
value = 0
[../]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = 'left'
value = 0
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/bc_with_aux_var.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./v]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./rea]
type = Reaction
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = v
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/pressure_channel/open_bc_pressure_BC.i)
# This input file tests Dirichlet pressure in/outflow boundary conditions for the incompressible NS equations.
[GlobalParams]
gravity = '0 0 0'
[]
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 3.0
ymin = 0
ymax = 1.0
nx = 30
ny = 10
elem_type = QUAD9
[]
[Variables]
[./vel_x]
order = SECOND
family = LAGRANGE
[../]
[./vel_y]
order = SECOND
family = LAGRANGE
[../]
[./p]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./mass]
type = INSMass
variable = p
u = vel_x
v = vel_y
pressure = p
[../]
[./x_momentum_space]
type = INSMomentumLaplaceForm
variable = vel_x
u = vel_x
v = vel_y
pressure = p
component = 0
integrate_p_by_parts = false
[../]
[./y_momentum_space]
type = INSMomentumLaplaceForm
variable = vel_y
u = vel_x
v = vel_y
pressure = p
component = 1
integrate_p_by_parts = false
[../]
[]
[BCs]
[./x_no_slip]
type = DirichletBC
variable = vel_x
boundary = 'top bottom'
value = 0.0
[../]
[./y_no_slip]
type = DirichletBC
variable = vel_y
boundary = 'left top bottom'
value = 0.0
[../]
[./inlet_p]
type = DirichletBC
variable = p
boundary = left
value = 1.0
[../]
[./outlet_p]
type = DirichletBC
variable = p
boundary = right
value = 0.0
[../]
[]
[Materials]
[./const]
type = GenericConstantMaterial
block = 0
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[]
[Preconditioning]
[./SMP_PJFNK]
type = SMP
full = true
solve_type = PJFNK
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-ksp_gmres_restart -pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = '300 bjacobi ilu 4'
line_search = none
nl_rel_tol = 1e-12
nl_max_its = 6
l_tol = 1e-6
l_max_its = 300
[]
[Outputs]
file_base = open_bc_out_pressure_BC
exodus = true
[]
(test/tests/executioners/executioner/steady.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 5
ny = 5
elem_type = QUAD9
[]
[Variables]
active = 'u'
[./u]
order = SECOND
family = LAGRANGE
[../]
[]
[Functions]
[./forcing_fn]
type = ParsedFunction
value = -4
[../]
[./exact_fn]
type = ParsedFunction
value = ((x*x)+(y*y))
[../]
[]
[Kernels]
active = 'diff ffn'
[./diff]
type = Diffusion
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
active = 'all'
[./all]
type = FunctionDirichletBC
variable = u
boundary = '0 1 2 3'
function = exact_fn
[../]
[]
[Postprocessors]
[./l2_err]
type = ElementL2Error
variable = u
function = exact_fn
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
file_base = out_steady
exodus = true
[]
(test/tests/materials/material/three_coupled_mat_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 10
ny = 10
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = MatDiffusionTest
variable = u
prop_name = a
[../]
[./conv]
type = MatConvection
variable = u
x = 1
y = 0
mat_prop = b
[../]
[]
[BCs]
[./right]
type = NeumannBC
variable = u
boundary = 1
value = 1
[../]
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[]
[Materials]
[./matA]
type = CoupledMaterial
block = 0
mat_prop = 'a'
coupled_mat_prop = 'b'
[../]
[./matB]
type = CoupledMaterial
block = 0
mat_prop = 'b'
coupled_mat_prop = 'c'
[../]
[./matC]
type = CoupledMaterial
block = 0
mat_prop = 'c'
coupled_mat_prop = 'd'
[../]
[./matD]
type = GenericConstantMaterial
block = 0
prop_names = 'd'
prop_values = '2'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out_three
exodus = true
[]
(test/tests/ics/array_constant_ic/array_constant_ic_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 8
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[Variables]
[u]
components = 2
[]
[]
[AuxVariables]
[v]
components = 8
[]
[]
[ICs]
[uic]
type = ArrayConstantIC
variable = u
value = '0.1 3'
[]
[vic]
type = ArrayConstantIC
variable = v
value = '2 6 9 7 1.1 2 5 4'
[]
[]
[Postprocessors]
[uint0]
type = ElementIntegralArrayVariablePostprocessor
variable = u
component = 0
[]
[uint1]
type = ElementIntegralArrayVariablePostprocessor
variable = u
component = 1
[]
[vint0]
type = ElementIntegralArrayVariablePostprocessor
variable = v
component = 0
[]
[vint1]
type = ElementIntegralArrayVariablePostprocessor
variable = v
component = 1
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/partitioners/custom_partition_generated_mesh/custom_partition_generated_mesh.i)
[Mesh]
[generate_2d]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[extrude]
type = MeshExtruderGenerator
input = generate_2d
extrusion_vector = '0 0 1'
num_layers = 5
[]
[Partitioner]
type = GridPartitioner
nx = 1
ny = 1
nz = 4
[]
[]
[Variables]
[u]
[]
[]
[AuxVariables]
[pid]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[pid]
type = ProcessorIDAux
variable = pid
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/variables/array_variable/array_variable_action.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 3
ny = 3
[]
[]
[Testing/LotsOfDiffusion/lots]
number = 1
array = true
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(examples/ex04_bcs/neumann_bc.i)
[Mesh]
file = square.e
uniform_refine = 4
[]
[Variables]
[./convected]
order = FIRST
family = LAGRANGE
[../]
[./diffused]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff_convected]
type = Diffusion
variable = convected
[../]
[./conv]
type = ExampleConvection
variable = convected
some_variable = diffused
[../]
[./diff_diffused]
type = Diffusion
variable = diffused
[../]
[]
[BCs]
active = 'left_convected right_convected_neumann left_diffused right_diffused'
[./left_convected]
type = DirichletBC
variable = convected
boundary = 'left'
value = 0
[../]
# Note: This BC is not active in this input file
[./right_convected_dirichlet]
type = CoupledDirichletBC
variable = convected
boundary = 'right'
alpha = 2
some_var = diffused
[../]
[./right_convected_neumann]
type = CoupledNeumannBC
variable = convected
boundary = 'right'
alpha = 2
some_var = diffused
[../]
[./left_diffused]
type = DirichletBC
variable = diffused
boundary = 'left'
value = 0
[../]
[./right_diffused]
type = DirichletBC
variable = diffused
boundary = 'right'
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(modules/richards/test/tests/darcy/jac.i)
# Test to show that DarcyFlux produces the correct jacobian
[GlobalParams]
variable = pressure
fluid_weight = '0 0 -1.5'
fluid_viscosity = 1
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
[]
[Variables]
[./pressure]
[./InitialCondition]
type = RandomIC
block = 0
min = 0
max = 1
[../]
[../]
[]
[Kernels]
[./darcy]
type = DarcyFlux
variable = pressure
[../]
[]
[Materials]
[./solid]
type = DarcyMaterial
block = 0
mat_permeability = '1 0 0 0 2 0 0 0 3'
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-snes_type'
petsc_options_value = 'test'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = jac
exodus = false
[]
(modules/navier_stokes/test/tests/finite_volume/cns/mms/1d-with-bcs/regular-straight-channel.i)
[GlobalParams]
fp = fp
[]
[Mesh]
[./gen_mesh]
type = GeneratedMeshGenerator
dim = 1
xmax = 1.5
nx = 15
[../]
[]
[Modules]
[FluidProperties]
[fp]
type = IdealGasFluidProperties
[]
[]
[]
[Variables]
[rho]
type = MooseVariableFVReal
initial_condition = 1.28969
scaling = 1e3
[]
[rho_u]
type = MooseVariableFVReal
initial_condition = 1.28969
[]
[rho_et]
type = MooseVariableFVReal
initial_condition = 2.525e5
scaling = 1e-2
[]
[]
[FVKernels]
[mass_advection]
type = CNSFVMassHLLC
variable = rho
fp = fp
[]
[momentum_x_advection]
type = CNSFVMomentumHLLC
variable = rho_u
momentum_component = x
fp = fp
[]
[drag]
type = FVReaction
variable = rho_u
rate = 1000
[]
[fluid_energy_advection]
type = CNSFVFluidEnergyHLLC
variable = rho_et
fp = fp
[]
[]
[FVBCs]
[mass_in]
variable = rho
type = CNSFVHLLCSpecifiedMassFluxAndTemperatureMassBC
boundary = left
temperature = 273.15
rhou = 1.28969
[]
[momentum_in]
variable = rho_u
type = CNSFVHLLCSpecifiedMassFluxAndTemperatureMomentumBC
boundary = left
temperature = 273.15
rhou = 1.28969
momentum_component = 'x'
[]
[energy_in]
variable = rho_et
type = CNSFVHLLCSpecifiedMassFluxAndTemperatureFluidEnergyBC
boundary = left
temperature = 273.15
rhou = 1.28969
[]
[mass_out]
variable = rho
type = CNSFVHLLCSpecifiedPressureMassBC
boundary = right
pressure = 1.01e5
[]
[momentum_out]
variable = rho_u
type = CNSFVHLLCSpecifiedPressureMomentumBC
boundary = right
pressure = 1.01e5
momentum_component = 'x'
[]
[energy_out]
variable = rho_et
type = CNSFVHLLCSpecifiedPressureFluidEnergyBC
boundary = right
pressure = 1.01e5
[]
[]
[Materials]
[var_mat]
type = ConservedVarValuesMaterial
rho = rho
rhou = rho_u
rho_et = rho_et
[]
[]
[Executioner]
solve_type = NEWTON
type = Steady
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
nl_max_its = 50
line_search = none
[]
[Outputs]
exodus = true
csv = true
[]
[Debug]
show_var_residual_norms = true
[]
(test/tests/auxkernels/bounds/constant_bounds.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 10
ny = 10
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[./v]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./bounds_dummy]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[BCs]
[./left_u]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = 3
value = 0
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = 1
value = 1
[../]
[]
[Bounds]
[./u_upper_bound]
type = ConstantBoundsAux
variable = bounds_dummy
bounded_variable = u
bound_type = upper
bound_value = 1
[../]
[./u_lower_bound]
type = ConstantBoundsAux
variable = bounds_dummy
bounded_variable = u
bound_type = lower
bound_value = 0
[../]
[./v_upper_bound]
type = ConstantBoundsAux
variable = bounds_dummy
bounded_variable = v
bound_type = upper
bound_value = 3
[../]
[./v_lower_bound]
type = ConstantBoundsAux
variable = bounds_dummy
bounded_variable = v
bound_type = lower
bound_value = -1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(modules/phase_field/test/tests/MultiSmoothCircleIC/latticesmoothcircleIC_bounds.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
xmin = 0
xmax = 50
ymin = 0
ymax = 50
elem_type = QUAD4
[]
[Variables]
[./c]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./c]
type = LatticeSmoothCircleIC
variable = c
invalue = 1.0
outvalue = 0.0001
circles_per_side = '2 2'
pos_variation = 10.0
radius = 8.0
int_width = 5.0
radius_variation_type = uniform
avoid_bounds = false
[../]
[]
[BCs]
[./Periodic]
[./c]
variable = c
auto_direction = 'x y'
[../]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = c
[../]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/phase_field/test/tests/new_initial_conditions/PolycrystalVariables_initial_from_file.i)
[Mesh]
file = prepare_mesh_out.e
[]
[Variables]
[./PolycrystalVariables]
op_num = 4
var_name_base = gr
initial_from_file = true
[../]
[]
[Executioner]
type = Steady
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[Outputs]
exodus = true
execute_on = FINAL
[]
(test/tests/materials/derivative_material_interface/ad_const.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
[]
[AuxVariables]
[./dummy]
[../]
[]
[Materials]
[./provider]
type = ADDerivativeMaterialInterfaceTestProvider
block = 0
[../]
[./client]
type = ADDerivativeMaterialInterfaceTestClient
prop_name = prop
block = 0
outputs = exodus
[../]
[./client2]
type = ADDerivativeMaterialInterfaceTestClient
prop_name = 1.0
block = 0
outputs = exodus
[../]
[./dummy]
type = ADGenericConstantMaterial
prop_names = prop
block = 0
prop_values = 0
[../]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/heat_conduction/coupled_convective_heat_flux/const_hw.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./t_infinity]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./force]
type = BodyForce
variable = u
value = 1000
[../]
[]
[AuxKernels]
[./t_infinity]
type = ConstantAux
variable = t_infinity
value = 500
execute_on = initial
[../]
[]
[BCs]
[./right]
type = CoupledConvectiveHeatFluxBC
variable = u
boundary = right
htc = 10
T_infinity = t_infinity
[../]
[]
[Executioner]
type = Steady
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/kernel_with_aux_var.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./v]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./rea]
type = Reaction
variable = v
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/utils/mathutils/poly.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Problem]
solve = false
[]
[Functions]
[./constant]
type = PolyTestFunction
coefficients = '1'
[../]
[./constant_exact]
type = ParsedFunction
value = '1'
[../]
[./quadratic]
type = PolyTestFunction
coefficients = '2 0 0'
[../]
[./quadratic_exact]
type = ParsedFunction
value = '2 * x * x'
[../]
[./tenth]
type = PolyTestFunction
coefficients = '-1.0 0.9 -0.8 0.7 -0.6 0.5 -0.4 0.3 -0.2 0.1 -0.1'
[../]
[./tenth_exact]
type = ParsedFunction
value = '-0.1 + 0.1 * x - 0.2 * x^2 + 0.3 * x^3 - 0.4 * x^4 + 0.5 * x^5 - 0.6 * x^6 + 0.7 * x^7 - 0.8 * x^8 + 0.9 * x^9 - 1.0 * x^10'
[../]
[./tenth_derivative]
type = PolyTestFunction
coefficients = '-1.0 0.9 -0.8 0.7 -0.6 0.5 -0.4 0.3 -0.2 0.1 -0.1'
derivative = true
[../]
[./tenth_derivative_exact]
type = ParsedFunction
value = '0.1 - 2.0 * 0.2 * x^1 + 3.0 * 0.3 * x^2 - 4.0 * 0.4 * x^3 + 5.0 * 0.5 * x^4 - 6.0 * 0.6 * x^5 + 7.0 * 0.7 * x^6 - 8.0 * 0.8 * x^7 + 9.0 * 0.9 * x^8 - 10.0 * 1.0 * x^9'
[../]
[]
[VectorPostprocessors]
[./out]
type = LineFunctionSampler
functions = 'constant constant_exact quadratic quadratic_exact tenth tenth_exact tenth_derivative tenth_derivative_exact'
start_point = '0 0 0'
end_point = '1 0 0'
num_points = 10
sort_by = x
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
[]
(test/tests/variables/fe_hermite/hermite-3-2d.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 5
ny = 5
elem_type = QUAD9
[]
[Functions]
[./bc_fnt]
type = ParsedFunction
value = 3*y*y
[../]
[./bc_fnb]
type = ParsedFunction
value = -3*y*y
[../]
[./bc_fnl]
type = ParsedFunction
value = -3*x*x
[../]
[./bc_fnr]
type = ParsedFunction
value = 3*x*x
[../]
[./forcing_fn]
type = ParsedFunction
value = -6*x-6*y+(x*x*x)+(y*y*y)
[../]
[./solution]
type = ParsedGradFunction
value = (x*x*x)+(y*y*y)
grad_x = 3*x*x
grad_y = 3*y*y
[../]
[]
[Variables]
[./u]
order = THIRD
family = HERMITE
[../]
[]
[Kernels]
active = 'diff forcing reaction'
[./diff]
type = Diffusion
variable = u
[../]
[./reaction]
type = Reaction
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
[./bc_top]
type = FunctionNeumannBC
variable = u
boundary = 'top'
function = bc_fnt
[../]
[./bc_bottom]
type = FunctionNeumannBC
variable = u
boundary = 'bottom'
function = bc_fnb
[../]
[./bc_left]
type = FunctionNeumannBC
variable = u
boundary = 'left'
function = bc_fnl
[../]
[./bc_right]
type = FunctionNeumannBC
variable = u
boundary = 'right'
function = bc_fnr
[../]
[]
[Postprocessors]
[./dofs]
type = NumDOFs
[../]
[./h]
type = AverageElementSize
[../]
[./L2error]
type = ElementL2Error
variable = u
function = solution
[../]
[./H1error]
type = ElementH1Error
variable = u
function = solution
[../]
[./H1Semierror]
type = ElementH1SemiError
variable = u
function = solution
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
csv = true
[]
(test/tests/multiapps/command_line/master_wrong_size.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
[]
[MultiApps]
[sub]
type = FullSolveMultiApp
positions = '0 0 0
1 1 1'
input_files = 'sub.i'
cli_args = 'Mesh/xmax=1.1 Mesh/xmax=1.2 Mesh/xmax=1.3'
[]
[]
(test/tests/materials/var_coupling/var_stateful_coupling.i)
# Test for making sure that a coupled variable can be used inside of initQpStatefulProperties
# of a Material object.
[Mesh]
type = GeneratedMesh
dim = 2
nx = 3
ny = 3
[]
[Variables]
[./u]
[../]
[]
[ICs]
[./u_ic]
type = ConstantIC
value = 1.2345
variable = u
[../]
[]
[Materials]
[./coupling_u]
type = VarCouplingMaterial
var = u
declare_old = true
outputs = exodus
[../]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'TIMESTEP_END'
exodus = true
hide = 'u'
[]
(modules/porous_flow/examples/tutorial/00_2D.i)
# Creates the mesh for the remainder of the tutorial
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
xmin = 1.0
xmax = 10
bias_x = 1.4
ny = 3
ymin = -6
ymax = 6
[]
[aquifer]
type = SubdomainBoundingBoxGenerator
block_id = 1
bottom_left = '0 -2 0'
top_right = '10 2 0'
input = gen
[]
[injection_area]
type = ParsedGenerateSideset
combinatorial_geometry = 'x<1.0001'
included_subdomain_ids = 1
new_sideset_name = 'injection_area'
input = 'aquifer'
[]
[rename]
type = RenameBlockGenerator
old_block = '0 1'
new_block = 'caps aquifer'
input = 'injection_area'
[]
[]
[Variables]
[dummy_var]
[]
[]
[Kernels]
[dummy_diffusion]
type = Diffusion
variable = dummy_var
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
file_base = 2D_mesh
exodus = true
[]
(test/tests/restart/restart_transient_from_steady/steady_with_2subs_sub.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 3
ny = 3
xmax = 0.3
ymax = 0.3
[]
[AuxVariables]
[power_density]
[]
[]
[Variables]
[temp]
[]
[]
[Kernels]
[heat_conduction]
type = Diffusion
variable = temp
[]
[heat_source_fuel]
type = CoupledForce
variable = temp
v = power_density
[]
[]
[BCs]
[bc]
type = DirichletBC
variable = temp
boundary = '1 3'
value = 100
[]
[bc2]
type = NeumannBC
variable = temp
boundary = '0 2'
value = 10.0
[]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart '
petsc_options_value = 'hypre boomeramg 100'
nl_abs_tol = 1e-7
nl_rel_tol = 1e-7
[]
[Postprocessors]
[temp_fuel_avg]
type = ElementAverageValue
variable = temp
execute_on = 'initial timestep_end'
[]
[pwr_density]
type = ElementIntegralVariablePostprocessor
variable = power_density
execute_on = 'initial timestep_end'
[]
[]
[Outputs]
perf_graph = true
exodus = true
color = true
csv = true
[]
(modules/tensor_mechanics/test/tests/ad_isotropic_elasticity_tensor/bulk_modulus_shear_modulus_test.i)
[Mesh]
type = GeneratedMesh
dim = 3
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[AuxVariables]
[./stress_11]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
add_variables = true
use_automatic_differentiation = true
[../]
[]
[AuxKernels]
[./stress_11]
type = ADRankTwoAux
variable = stress_11
rank_two_tensor = stress
index_j = 1
index_i = 1
[../]
[]
[BCs]
[./bottom]
type = ADDirichletBC
variable = disp_y
boundary = bottom
value = 0
[../]
[./left]
type = ADDirichletBC
variable = disp_x
boundary = left
value = 0
[../]
[./back]
type = ADDirichletBC
variable = disp_z
boundary = back
value = 0
[../]
[./top]
type = ADDirichletBC
variable = disp_y
boundary = top
value = 0.001
[../]
[]
[Materials]
[./stress]
type = ADComputeLinearElasticStress
[../]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
bulk_modulus = 416666
shear_modulus = 454545
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
l_max_its = 20
nl_max_its = 10
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(test/tests/auxkernels/nearest_node_value/nearest_node_value.i)
[Mesh]
file = nonmatching.e
dim = 2
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./nearest_node_value]
block = left
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = u
boundary = 'leftbottom rightbottom'
value = 0
[../]
[./top]
type = DirichletBC
variable = u
boundary = 'lefttop righttop'
value = 1
[../]
[]
[AuxKernels]
[./nearest_node_value]
type = NearestNodeValueAux
variable = nearest_node_value
boundary = leftright
paired_variable = u
paired_boundary = rightleft
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/mesh_modifiers/boundingbox_nodeset/boundingbox_nodeset_inside_test.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 2
[]
[middle_node]
type = BoundingBoxNodeSetGenerator
input = gen
new_boundary = middle_node
top_right = '1.1 1.1 0'
bottom_left = '0.49 0.49 0'
[]
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[]
[middle]
type = DirichletBC
variable = u
boundary = middle_node
value = -1
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
[]
[Outputs]
file_base = boundingbox_nodeset_inside_out
exodus = true
[]
(modules/phase_field/test/tests/grain_tracker_test/grain_tracker_volume.i)
# This test calculates the volume of a few simple shapes
# Using the FeatureVolumeVectorPostprocessor
[Mesh]
# Required for use with distributed mesh
type = GeneratedMesh
dim = 2
nx = 40
ny = 40
nz = 0
xmin = -2
xmax = 2
ymin = -2
ymax = 2
zmax = 0
elem_type = QUAD4
[]
[Variables]
[./gr0]
[../]
[./gr1]
[../]
[]
[ICs]
[./circle]
type = SmoothCircleIC
x1 = 0
y1 = 0
radius = 1
int_width = 0.01
invalue = 1
outvalue = 0
variable = gr0
[../]
[./boxes]
type = MultiBoundingBoxIC
corners = '-1 -1 0
0 0 0'
opposite_corners = '-0.5 -0.5 0
1 1 0'
inside = 1
outside = 0
variable = gr1
[../]
[]
[Postprocessors]
[./grain_tracker]
type = GrainTracker
variable = 'gr0 gr1'
threshold = 0.1
compute_var_to_feature_map = true
execute_on = 'initial'
[../]
[./avg_feature_vol]
type = AverageGrainVolume
feature_counter = grain_tracker
execute_on = 'initial'
[../]
[]
[VectorPostprocessors]
[./grain_volumes]
type = FeatureVolumeVectorPostprocessor
flood_counter = grain_tracker
execute_on = 'initial'
[../]
[]
[Executioner]
type = Steady
[./Adaptivity]
initial_adaptivity = 3
refine_fraction = 0.7
coarsen_fraction = 0.1
max_h_level = 3
[../]
[]
[Problem]
solve = false
[]
[Outputs]
exodus = true
csv = true
[]
(modules/porous_flow/test/tests/fluids/methane.i)
# Test MethaneFluidProperties
# Reference data from Irvine Jr, T. F. and Liley, P. E. (1984) Steam and
# Gas Tables with Computer Equations
#
# For temperature = 350K, the fluid properties should be:
# density = 55.13 kg/m^3
# viscosity = 0.01276 mPa.s
# h = 708.5 kJ/kg
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[]
[Variables]
[pp]
initial_condition = 10e6
[]
[]
[Kernels]
[dummy]
type = Diffusion
variable = pp
[]
[]
[AuxVariables]
[temp]
initial_condition = 350.0
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
temperature = 'temp'
[]
[ppss]
type = PorousFlow1PhaseFullySaturated
porepressure = pp
[]
[methane]
type = PorousFlowSingleComponentFluid
temperature_unit = Kelvin
fp = methane
phase = 0
[]
[]
[Modules]
[FluidProperties]
[methane]
type = MethaneFluidProperties
[]
[]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Postprocessors]
[pressure]
type = ElementIntegralVariablePostprocessor
variable = pp
[]
[temperature]
type = ElementIntegralVariablePostprocessor
variable = temp
[]
[density]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_fluid_phase_density_qp0'
[]
[viscosity]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_viscosity_qp0'
[]
[enthalpy]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_fluid_phase_enthalpy_qp0'
[]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = methane
csv = true
[]
(modules/stochastic_tools/test/tests/surrogates/load_store/sub.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 100
xmax = 10
[]
[Variables]
[u]
[]
[]
[Kernels]
[diffusion]
type = MatDiffusion
variable = u
diffusivity = D
[]
[absorption]
type = MaterialReaction
variable = u
coefficient = sig
[]
[source]
type = BodyForce
variable = u
value = 1.0
[]
[]
[Materials]
[diffusivity]
type = GenericConstantMaterial
prop_names = D
prop_values = 2.0
[]
[xs]
type = GenericConstantMaterial
prop_names = sig
prop_values = 2.0
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 0
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Controls]
[stochastic]
type = SamplerReceiver
[]
[]
[Postprocessors]
[avg]
type = AverageNodalVariableValue
variable = u
[]
[max]
type = NodalExtremeValue
variable = u
value_type = max
[]
[]
[Outputs]
[]
(test/tests/misc/data_file_name/test.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
[]
[]
[UserObjects]
[data_file]
type = DataFileNameTest
data_file = README.md
[]
[]
[Problem]
solve = false
kernel_coverage_check = false
[]
[Executioner]
type = Steady
[]
(test/tests/meshgenerators/sidesets_bounding_box_generator/error_no_side_sets_found.i)
[Mesh]
[./gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
#parallel_type = replicated
[]
[./createNewSidesetOne]
type = SideSetsFromBoundingBoxGenerator
input = gmg
boundary_id_old = 'right'
boundary_id_new = 11
bottom_left = '-0.1 -0.1 0'
top_right = '0.9 0.9 0'
block_id = 0
[]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./leftBC]
type = DirichletBC
variable = u
boundary = 'left'
value = 1
[../]
[./rightBC]
type = DirichletBC
variable = u
boundary = 11
value = 0
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/phase_field/test/tests/reconstruction/1phase_reconstruction.i)
#
# In this test we set the initial condition of a set of order parameters
# by pulling out the grain data from given EBSD data file ignoring the phase completely.
#
[Problem]
type = FEProblem
solve = false
kernel_coverage_check = false
[]
# The following sections are extracted in the documentation in
# moose/docs/content/modules/phase_field/ICs/EBSD.md
[Mesh]
# Create a mesh representing the EBSD data
[ebsd_mesh]
type = EBSDMeshGenerator
filename = IN100_001_28x28_Marmot.txt
[]
[]
[GlobalParams]
# Define the number and names of the order parameters used to represent the grains
op_num = 4
var_name_base = gr
[]
[UserObjects]
[ebsd_reader]
# Read in the EBSD data. Uses the filename given in the mesh block.
type = EBSDReader
[]
[ebsd]
type = PolycrystalEBSD
coloring_algorithm = bt
ebsd_reader = ebsd_reader
output_adjacency_matrix = true
[]
[grain_tracker]
type = GrainTracker
# For displaying HALO fields
compute_halo_maps = true
# Link in the ebsd userobject here so that grain tracker can extract info from it
polycrystal_ic_uo = ebsd
[]
[]
[Variables]
[PolycrystalVariables]
# Create all the order parameters
order = FIRST
family = LAGRANGE
[]
[]
[ICs]
[PolycrystalICs]
[PolycrystalColoringIC]
# Uses the data from the user object 'ebsd' to initialize the variables for all the order parameters.
polycrystal_ic_uo = ebsd
[]
[]
[]
#ENDDOC - End of the file section that is included in the documentation. Do not change this line!
[GlobalParams]
execute_on = 'initial'
family = MONOMIAL
order = CONSTANT
[]
[AuxVariables]
[PHI1]
[]
[PHI]
[]
[PHI2]
[]
[GRAIN]
[]
[unique_grains]
[]
[var_indices]
[]
[halo0]
[]
[halo1]
[]
[halo2]
[]
[halo3]
[]
[]
[AuxKernels]
[phi1_aux]
type = EBSDReaderPointDataAux
variable = PHI1
ebsd_reader = ebsd_reader
data_name = 'phi1'
[]
[phi_aux]
type = EBSDReaderPointDataAux
variable = PHI
ebsd_reader = ebsd_reader
data_name = 'phi'
[]
[phi2_aux]
type = EBSDReaderPointDataAux
variable = PHI2
ebsd_reader = ebsd_reader
data_name = 'phi2'
[]
[grain_aux]
type = EBSDReaderPointDataAux
variable = GRAIN
ebsd_reader = ebsd_reader
data_name = 'feature_id'
[]
[unique_grains]
type = FeatureFloodCountAux
variable = unique_grains
flood_counter = grain_tracker
field_display = UNIQUE_REGION
[]
[var_indices]
type = FeatureFloodCountAux
variable = var_indices
flood_counter = grain_tracker
field_display = VARIABLE_COLORING
[]
[halo0]
type = FeatureFloodCountAux
variable = halo0
map_index = 0
field_display = HALOS
flood_counter = grain_tracker
[]
[halo1]
type = FeatureFloodCountAux
variable = halo1
map_index = 1
field_display = HALOS
flood_counter = grain_tracker
[]
[halo2]
type = FeatureFloodCountAux
variable = halo2
map_index = 2
field_display = HALOS
flood_counter = grain_tracker
[]
[halo3]
type = FeatureFloodCountAux
variable = halo3
map_index = 3
field_display = HALOS
flood_counter = grain_tracker
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/displacement/displacement_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
displacements = 'u u'
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out_displaced
[./exodus]
type = Exodus
use_displaced = true
[../]
[]
(tutorials/tutorial01_app_development/step10_auxkernels/test/tests/auxkernels/darcy_velocity/darcy_velocity_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[pressure]
order = FIRST
family = LAGRANGE
[]
[]
[AuxVariables]
[velocity]
order = CONSTANT
family = MONOMIAL_VEC
[]
[]
[Kernels]
[diffusion]
type = DarcyPressure
variable = pressure
[]
[]
[AuxKernels]
[velocity]
type = DarcyVelocity
variable = velocity
pressure = pressure
execute_on = TIMESTEP_END
[]
[]
[Materials]
[column]
type = PackedColumn
[]
[]
[BCs]
[left]
type = ADDirichletBC
variable = pressure
boundary = left
value = 0
[]
[right]
type = ADDirichletBC
variable = pressure
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
l_tol = 1e-07 # tighter tolerance to acheive a numerically constant velocity field on 64-bit procs
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/3D_RZ_error_check.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 2
ny = 2
nz = 2
zmin = 0
zmax = 1
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
# Try to specify an RZ problem with a 3D mesh
[Problem]
coord_type = 'RZ'
block = '0'
[]
(test/tests/kernels/hfem/robin_adapt.i)
[Mesh]
[square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[]
build_all_side_lowerd_mesh = true
[]
[Variables]
[u]
order = THIRD
family = MONOMIAL
block = 0
components = 2
[]
[lambda]
order = CONSTANT
family = MONOMIAL
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
components = 2
[]
[]
[AuxVariables]
[v]
order = CONSTANT
family = MONOMIAL
block = 0
initial_condition = '1'
[]
[]
[Kernels]
[diff]
type = ArrayDiffusion
variable = u
block = 0
diffusion_coefficient = dc
[]
[source]
type = ArrayCoupledForce
variable = u
v = v
coef = '1 2'
block = 0
[]
[]
[DGKernels]
[surface]
type = ArrayHFEMDiffusion
variable = u
lowerd_variable = lambda
[]
[]
[BCs]
[all]
type = ArrayVacuumBC
boundary = 'left right top bottom'
variable = u
[]
[]
[Materials]
[dc]
type = GenericConstantArray
prop_name = dc
prop_value = '1 1'
[]
[]
[Postprocessors]
[intu]
type = ElementIntegralArrayVariablePostprocessor
variable = u
block = 0
[]
[lambdanorm]
type = ElementArrayL2Norm
variable = lambda
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu basic mumps'
[]
[Outputs]
exodus = true
[]
[Adaptivity]
steps = 1
marker = box
max_h_level = 2
initial_steps = 2
[Markers]
[box]
bottom_left = '0 0 0'
inside = refine
top_right = '0.5 0.5 0'
outside = do_nothing
type = BoxMarker
[]
[]
[]
(test/tests/postprocessors/difference_pps/difference_pps.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
[]
[AuxVariables]
[./v]
[../]
[]
[Variables]
[./u]
[../]
[]
[ICs]
[./u_ic]
type = ConstantIC
variable = u
value = 2
[../]
[]
[AuxKernels]
[./one]
type = ConstantAux
variable = v
value = 1
execute_on = 'initial timestep_end'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Postprocessors]
[./u_avg]
type = ElementAverageValue
variable = u
execute_on = 'initial timestep_end'
[../]
[./v_avg]
type = ElementAverageValue
variable = v
execute_on = 'initial timestep_end'
[../]
[./diff]
type = DifferencePostprocessor
value1 = v_avg
value2 = u_avg
execute_on = 'initial timestep_end'
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/materials/declare_overlap/error.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 1
[]
[./left_domain]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '0 0 0'
top_right = '0.5 1 0'
block_id = 10
[../]
[]
[Variables]
[./u]
initial_condition = 2
[../]
[]
[Kernels]
[./diff]
type = MatDiffusionTest
variable = u
prop_name = 'p'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 2
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 3
[../]
[]
[Materials]
[./all]
type = GenericConstantMaterial
prop_names = 'f f_prime p'
prop_values = '2 2.5 2.468'
block = ANY_BLOCK_ID
outputs = all
[../]
[./left]
type = GenericConstantMaterial
prop_names = 'f f_prime p'
prop_values = '1 0.5 1.2345'
block = 10
outputs = all
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
print_linear_residuals = true
perf_graph = true
[]
(test/tests/vectorpostprocessors/work_balance/work_balance.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
partitioner = linear
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./someaux]
[../]
[./otheraux]
family = MONOMIAL
order = CONSTANT
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[VectorPostprocessors]
[./nl_wb]
type = WorkBalance
execute_on = initial
system = nl
[]
[./aux_wb]
type = WorkBalance
execute_on = initial
system = aux
[]
[./all_wb]
type = WorkBalance
execute_on = initial
system = all
[]
[]
[Outputs]
csv = true
[]
(test/tests/userobjects/layered_average/layered_average_bounds_error.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./layered_average]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./layered_average]
type = SpatialUserObjectAux
variable = layered_average
execute_on = timestep_end
user_object = average
[../]
[]
[BCs]
[./top]
type = DirichletBC
variable = u
boundary = top
value = 1
[../]
[./bottom]
type = DirichletBC
variable = u
boundary = bottom
value = 0
[../]
[]
[UserObjects]
[./average]
type = LayeredAverage
variable = u
direction = y
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/kernels/vector_fe/vector_kernel.i)
# This example reproduces the libmesh vector_fe example 3 results
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
xmin = -1
ymin = -1
elem_type = QUAD9
[]
[Variables]
[./u]
family = NEDELEC_ONE
order = FIRST
[../]
[]
[Kernels]
[./diff]
type = VectorFEWave
variable = u
x_forcing_func = 'x_ffn'
y_forcing_func = 'y_ffn'
[../]
[]
[BCs]
[./bnd]
type = VectorCurlPenaltyDirichletBC
boundary = 'left right top bottom'
penalty = 1e10
function_x = 'x_sln'
function_y = 'y_sln'
variable = u
[../]
[]
[Functions]
[./x_ffn]
type = ParsedFunction
value = '(2*pi*pi + 1)*cos(pi*x)*sin(pi*y)'
[../]
[./y_ffn]
type = ParsedFunction
value = '-(2*pi*pi + 1)*sin(pi*x)*cos(pi*y)'
[../]
[./x_sln]
type = ParsedFunction
value = 'cos(pi*x)*sin(pi*y)'
[../]
[./y_sln]
type = ParsedFunction
value = '-sin(pi*x)*cos(pi*y)'
[../]
[]
[Preconditioning]
[./pre]
type = SMP
[../]
[]
[Executioner]
type = Steady
solve_type = 'LINEAR'
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
petsc_options = '-snes_converged_reason -ksp_converged_reason -snes_linesearch_monitor'
[]
[Outputs]
exodus = true
[]
(test/tests/interfacekernels/1d_interface/coupled_value_coupled_flux_with_jump_material.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 10
xmax = 2
[]
[./subdomain1]
type = SubdomainBoundingBoxGenerator
bottom_left = '1.0 0 0'
block_id = 1
top_right = '2.0 1.0 0'
input = gen
[../]
[./interface]
type = SideSetsBetweenSubdomainsGenerator
input = subdomain1
primary_block = '0'
paired_block = '1'
new_boundary = 'primary0_interface'
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
block = '0'
[../]
[./v]
order = FIRST
family = LAGRANGE
block = '1'
[../]
[]
[Kernels]
[./diff_u]
type = CoeffParamDiffusion
variable = u
D = 4
block = 0
[../]
[./diff_v]
type = CoeffParamDiffusion
variable = v
D = 2
block = 1
[../]
[]
[InterfaceKernels]
[./penalty_interface]
type = PenaltyInterfaceDiffusion
variable = u
neighbor_var = v
boundary = primary0_interface
penalty = 1e6
jump_prop_name = jump
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 'left'
value = 1
[../]
[./right]
type = DirichletBC
variable = v
boundary = 'right'
value = 0
[../]
[]
[Materials]
[./jump]
type = JumpInterfaceMaterial
var = u
neighbor_var = v
boundary = primary0_interface
[../]
[./stateful]
type = StatefulMaterial
initial_diffusivity = 1
boundary = primary0_interface
[../]
[./block0]
type = GenericConstantMaterial
block = '0'
prop_names = 'D'
prop_values = '4'
[../]
[./block1]
type = GenericConstantMaterial
block = '1'
prop_names = 'D'
prop_values = '2'
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
print_linear_residuals = true
[]
[Debug]
show_var_residual_norms = true
[]
(test/tests/multiapps/picard/steady_picard_master.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
parallel_type = replicated
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./v]
[../]
[]
[Kernels]
[./diff]
type = CoefDiffusion
variable = u
coef = 0.1
[../]
[./force_u]
type = CoupledForce
variable = u
v = v
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Postprocessors]
[./unorm]
type = ElementL2Norm
variable = u
execute_on = 'initial timestep_end'
[../]
[./vnorm]
type = ElementL2Norm
variable = v
execute_on = 'initial timestep_end'
[../]
[]
[Executioner]
type = Steady
nl_abs_tol = 1e-14
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
fixed_point_max_its = 10
fixed_point_rel_tol = 1e-6
[]
[Outputs]
exodus = true
[]
[MultiApps]
[./sub]
type = FullSolveMultiApp
input_files = steady_picard_sub.i
no_backup_and_restore = true
[../]
[]
[Transfers]
[./v_from_sub]
type = MultiAppNearestNodeTransfer
from_multi_app = sub
source_variable = v
variable = v
[../]
[./u_to_sub]
type = MultiAppNearestNodeTransfer
to_multi_app = sub
source_variable = u
variable = u
[../]
[]
(test/tests/misc/block_user_object_check/coupled_check.i)
[Mesh]
[./generator]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 5
[../]
[./left_block]
type = SubdomainBoundingBoxGenerator
input = generator
block_id = 1
bottom_left = '0 0 0'
top_right = '0.5 1 0'
[../]
[./right_block]
type = SubdomainBoundingBoxGenerator
input = left_block
block_id = 2
bottom_left = '0.5 0 0'
top_right = '1 1 0'
[../]
[]
[Variables]
[./var_0]
[../]
[./var_1]
block = 1
initial_condition = 100
[../]
[./var_2]
block = 2
initial_condition = 200
[../]
[]
[Kernels]
[./obj]
type = CoupledConvection
variable = var_0
velocity_vector = var_1
#block = 1 # this is being tested
[../]
[]
[Problem]
type = FEProblem
kernel_coverage_check = true
solve = false
[]
[Executioner]
type = Steady
[]
(modules/navier_stokes/test/tests/finite_element/ins/lid_driven/lid_driven_stabilized.i)
[GlobalParams]
gravity = '0 0 0'
laplace = true
integrate_p_by_parts = true
family = LAGRANGE
order = FIRST
# There are multiple types of stabilization possible in incompressible
# Navier Stokes. The user can specify supg = true to apply streamline
# upwind petrov-galerkin stabilization to the momentum equations. This
# is most useful for high Reynolds numbers, e.g. when inertial effects
# dominate over viscous effects. The user can also specify pspg = true
# to apply pressure stabilized petrov-galerkin stabilization to the mass
# equation. PSPG is a form of Galerkin Least Squares. This stabilization
# allows equal order interpolations to be used for pressure and velocity.
# Finally, the alpha parameter controls the amount of stabilization.
# For PSPG, decreasing alpha leads to increased accuracy but may induce
# spurious oscillations in the pressure field. Some numerical experiments
# suggest that alpha between .1 and 1 may be optimal for accuracy and
# robustness.
supg = true
pspg = true
alpha = 1e-1
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
nx = 64
ny = 64
elem_type = QUAD4
[]
[./corner_node]
type = ExtraNodesetGenerator
new_boundary = 'pinned_node'
nodes = '0'
input = gen
[../]
[]
[Variables]
[./vel_x]
[../]
[./vel_y]
[../]
[./p]
[../]
[]
[Kernels]
# mass
[./mass]
type = INSMass
variable = p
u = vel_x
v = vel_y
pressure = p
[../]
# x-momentum, space
[./x_momentum_space]
type = INSMomentumLaplaceForm
variable = vel_x
u = vel_x
v = vel_y
pressure = p
component = 0
[../]
# y-momentum, space
[./y_momentum_space]
type = INSMomentumLaplaceForm
variable = vel_y
u = vel_x
v = vel_y
pressure = p
component = 1
[../]
[]
[BCs]
[./x_no_slip]
type = DirichletBC
variable = vel_x
boundary = 'bottom right left'
value = 0.0
[../]
[./lid]
type = FunctionDirichletBC
variable = vel_x
boundary = 'top'
function = 'lid_function'
[../]
[./y_no_slip]
type = DirichletBC
variable = vel_y
boundary = 'bottom right top left'
value = 0.0
[../]
[./pressure_pin]
type = DirichletBC
variable = p
boundary = 'pinned_node'
value = 0
[../]
[]
[Materials]
[./const]
type = GenericConstantMaterial
block = 0
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[]
[Functions]
[./lid_function]
# We pick a function that is exactly represented in the velocity
# space so that the Dirichlet conditions are the same regardless
# of the mesh spacing.
type = ParsedFunction
value = '4*x*(1-x)'
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_asm_overlap -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = 'asm 2 ilu 4'
line_search = 'none'
nl_rel_tol = 1e-12
nl_abs_tol = 1e-13
nl_max_its = 6
l_tol = 1e-6
l_max_its = 500
[]
[Outputs]
exodus = true
print_linear_converged_reason = false
print_nonlinear_converged_reason = false
[]
[Postprocessors]
[lin]
type = NumLinearIterations
[]
[nl]
type = NumNonlinearIterations
[]
[lin_tot]
type = CumulativeValuePostprocessor
postprocessor = 'lin'
[]
[nl_tot]
type = CumulativeValuePostprocessor
postprocessor = 'nl'
[]
[]
(modules/heat_conduction/test/tests/heat_source_bar/heat_source_bar.i)
# This is a simple 1D test of the volumetric heat source with material properties
# of a representative ceramic material. A bar is uniformly heated, and a temperature
# boundary condition is applied to the left side of the bar.
# Important properties of problem:
# Length: 0.01 m
# Thermal conductivity = 3.0 W/(mK)
# Specific heat = 300.0 J/K
# density = 10431.0 kg/m^3
# Prescribed temperature on left side: 600 K
# When it has reached steady state, the temperature as a function of position is:
# T = -q/(2*k) (x^2 - 2*x*length) + 600
# or
# T = -6.3333e+7 * (x^2 - 0.02*x) + 600
# on left side: T=600, on right side, T=6933.3
[Mesh]
type = GeneratedMesh
dim = 1
xmax = 0.01
nx = 20
[]
[Variables]
[./temp]
initial_condition = 300.0
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[./heatsource]
type = HeatSource
function = volumetric_heat
variable = temp
[../]
[]
[BCs]
[./lefttemp]
type = DirichletBC
boundary = left
variable = temp
value = 600
[../]
[]
[Materials]
[./density]
type = GenericConstantMaterial
prop_names = 'density thermal_conductivity'
prop_values = '10431.0 3.0'
[../]
[]
[Functions]
[./volumetric_heat]
type = ParsedFunction
value = 3.8e+8
[../]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[./right]
type = SideAverageValue
variable = temp
boundary = right
[../]
[./error]
type = NodalL2Error
function = '-3.8e+8/(2*3) * (x^2 - 2*x*0.01) + 600'
variable = temp
[../]
[]
[Outputs]
execute_on = FINAL
exodus = true
[]
(modules/functional_expansion_tools/test/tests/errors/missing_series_duo_disc.i)
[Mesh]
type = GeneratedMesh
dim = 3
[]
[Functions]
[./series]
type = FunctionSeries
series_type = CylindricalDuo
orders = '0 1'
physical_bounds = '-1.0 1.0 0.0 0.0 1'
x = Legendre
[../]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
(modules/phase_field/test/tests/flood_counter_aux_test/simple.i)
[Mesh]
file = square_nodes.e
uniform_refine = 0
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[./v]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./bubble_map0]
order = FIRST
family = LAGRANGE
[../]
[./bubble_map1]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./diffv]
type = Diffusion
variable = v
[../]
[]
[AuxKernels]
[./mapper0]
type = FeatureFloodCountAux
variable = bubble_map0
execute_on = timestep_end
flood_counter = bubbles
map_index = 0
[../]
[./mapper1]
type = FeatureFloodCountAux
variable = bubble_map1
execute_on = timestep_end
flood_counter = bubbles
map_index = 1
[../]
[]
[BCs]
[./bott_left]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[./bott_right]
type = DirichletBC
variable = v
boundary = 2
value = 1
[../]
[./up_right]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[./up_left]
type = DirichletBC
variable = v
boundary = 4
value = 1
[../]
[./the_rest_u]
type = DirichletBC
variable = u
boundary = '5 6 7 8'
value = 0
[../]
[./the_rest_v]
type = DirichletBC
variable = v
boundary = '5 6 7 8'
value = 0
[../]
[]
[UserObjects]
[./bubbles]
use_single_map = false
type = FeatureFloodCount
variable = 'u v'
threshold = 0.3
execute_on = timestep_end
outputs = none
flood_entity_type = NODAL
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/cylindrical/diverging.i)
mu=1
rho=1
advected_interp_method='average'
velocity_interp_method='rc'
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[Mesh]
file = diverging.msh
uniform_refine = 2
[]
[Problem]
fv_bcs_integrity_check = true
coord_type = 'RZ'
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1e-15
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1e-15
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
# we can think of the axis as a slip wall boundary, no normal velocity and no viscous shear
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[]
[FVBCs]
active = 'inlet-u inlet-v free-slip-wall-u free-slip-wall-v outlet-p axis-u axis-v'
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = u
function = 0
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = v
function = 1
[]
[free-slip-wall-u]
type = INSFVNaturalFreeSlipBC
boundary = 'right'
variable = u
momentum_component = 'x'
[]
[free-slip-wall-v]
type = INSFVNaturalFreeSlipBC
boundary = 'right'
variable = v
momentum_component = 'y'
[]
[no-slip-wall-u]
type = INSFVNoSlipWallBC
boundary = 'right'
variable = u
function = 0
[]
[no-slip-wall-v]
type = INSFVNoSlipWallBC
boundary = 'right'
variable = v
function = 0
[]
[outlet-p]
type = INSFVOutletPressureBC
boundary = 'top'
variable = pressure
function = 0
[]
[axis-u]
type = INSFVSymmetryVelocityBC
boundary = 'left'
variable = u
u = u
v = v
mu = ${mu}
momentum_component = x
[]
[axis-v]
type = INSFVSymmetryVelocityBC
boundary = 'left'
variable = v
u = u
v = v
mu = ${mu}
momentum_component = y
[]
[axis-p]
type = INSFVSymmetryPressureBC
boundary = 'left'
variable = pressure
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options = '-options_left'
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_shift_type -ksp_gmres_restart'
petsc_options_value = 'asm lu NONZERO 200'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Debug]
show_var_residual_norms = true
[]
[Postprocessors]
[in]
type = SideIntegralVariablePostprocessor
variable = v
boundary = 'bottom'
[]
[out]
type = SideIntegralVariablePostprocessor
variable = v
boundary = 'top'
[]
[num_lin]
type = NumLinearIterations
outputs = 'console'
[]
[num_nl]
type = NumNonlinearIterations
outputs = 'console'
[]
[cum_lin]
type = CumulativeValuePostprocessor
outputs = 'console'
postprocessor = 'num_lin'
[]
[cum_nl]
type = CumulativeValuePostprocessor
outputs = 'console'
postprocessor = 'num_nl'
[]
[]
[Outputs]
exodus = true
csv = true
[]
(modules/phase_field/test/tests/free_energy_material/RegularSolutionFreeEnergy.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmax = 1
ymax = 500
elem_type = QUAD4
[]
[Variables]
[./c]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = x
[../]
[../]
[./myT]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = y
[../]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = c
[../]
[./diff2]
type = Diffusion
variable = myT
[../]
[]
[BCs]
[./left]
type = FunctionDirichletBC
variable = c
boundary = left
function = x
[../]
[./bottom]
type = FunctionDirichletBC
variable = myT
boundary = bottom
function = y
[../]
[./right]
type = FunctionDirichletBC
variable = c
boundary = right
function = x
[../]
[./top]
type = FunctionDirichletBC
variable = myT
boundary = top
function = y
[../]
[]
[Materials]
[./free_energy]
type = RegularSolutionFreeEnergy
f_name = F
c = c
T = myT
outputs = out
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
l_max_its = 1
nl_max_its = 1
nl_abs_tol = 1
[]
[Outputs]
execute_on = 'timestep_end'
[./out]
type = Exodus
execute_on = timestep_end
[../]
[]
(test/tests/vectorpostprocessors/element_value_sampler/element_value_sampler.i)
# Tests the ElementValueSampler vector post-processor. In this test, 2 constant
# monomial variables are given distributions by a function and are output to a CSV file.
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Functions]
[./u_fn]
type = ParsedFunction
value = '2 * x + 3 * y'
[../]
[./v_fn]
type = ParsedFunction
value = 'x + y'
[../]
[]
[AuxVariables]
[./u]
family = MONOMIAL
order = CONSTANT
[../]
[./v]
family = MONOMIAL
order = CONSTANT
[../]
[]
[ICs]
[./u_ic]
type = FunctionIC
variable = u
function = u_fn
[../]
[./v_ic]
type = FunctionIC
variable = v
function = v_fn
[../]
[]
[VectorPostprocessors]
[./element_value_sampler]
type = ElementValueSampler
variable = 'u v'
sort_by = id
execute_on = 'initial'
[../]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
file_base = 'element_value_sampler'
csv = true
execute_on = 'initial'
[]
(test/tests/outputs/console/console.i)
###########################################################
# This test exercises console Output control. Various
# controls are implemented using this input file including
# turning off color, changing Postprocessor output,
# toggling the performance logging, and verifying
# simulation information on the console.
#
# @Requirement U1.40
###########################################################
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[AuxVariables]
[./aux0]
order = SECOND
family = SCALAR
[../]
[./aux1]
family = SCALAR
initial_condition = 5
[../]
[./aux2]
family = SCALAR
initial_condition = 10
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./diff_v]
type = CoefDiffusion
variable = v
coef = 2
[../]
[]
[BCs]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[./left_u]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = right
value = 3
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = left
value = 2
[../]
[]
[Postprocessors]
[./num_vars]
type = NumVars
system = 'NL'
[../]
[./num_aux]
type = NumVars
system = 'AUX'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
color = false
[./screen]
type = Console
fit_mode = 40
[../]
[]
[ICs]
[./aux0_IC]
variable = aux0
values = '12 13'
type = ScalarComponentIC
[../]
[]
(test/tests/parser/hit_error/hit_error.i)
[Mesh]
file = file.e
[]
[Executioner]
type = Steady
(test/tests/problems/eigen_problem/eigensolvers/ne_coupled_picard_sub.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 10
ymin = 0
ymax = 10
elem_type = QUAD4
nx = 8
ny = 8
[]
[Variables]
[./T]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./power]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff_T]
type = Diffusion
variable = T
[../]
[./src_T]
type = CoupledForce
variable = T
v = power
[../]
[]
[BCs]
[./homogeneousT]
type = DirichletBC
variable = T
boundary = '0 1 2 3'
value = 0
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
execute_on = 'timestep_end'
[]
(test/tests/transfers/multiapp_copy_transfer/second_lagrange_to_sub/sub.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
elem_type = QUAD9
[]
[Variables]
[./u]
order = SECOND
family = LAGRANGE
[../]
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/bcs/second_deriv/test_lap_bc.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
xmin = -1
xmax = 1
ymin = -1
ymax = 1
elem_type = QUAD9
[]
[Variables]
[./u]
order = SECOND
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = force_fn
[../]
[]
[Functions]
[./left_bc_func]
type = ParsedFunction
value = '1+y*y'
[../]
[./top_bc_func]
type = ParsedFunction
value = '1+x*x'
[../]
[./bottom_bc_func]
type = ParsedFunction
value = '1+x*x'
[../]
[./force_fn]
type = ParsedFunction
value = -4
[../]
[]
[BCs]
[./left]
type = FunctionDirichletBC
variable = u
boundary = left
function = left_bc_func
[../]
[./bottom]
type = FunctionDirichletBC
variable = u
boundary = bottom
function = bottom_bc_func
[../]
[./top]
type = FunctionDirichletBC
variable = u
boundary = top
function = top_bc_func
[../]
[./right_test]
type = TestLapBC
variable = u
boundary = right
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/misc/serialized_solution/serialized_solution.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./lag]
initial_condition = 2
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Postprocessors]
[./aux]
type = TestSerializedSolution
system = aux
execute_on = 'initial timestep_end'
[../]
[./nl]
type = TestSerializedSolution
system = nl
execute_on = 'initial timestep_end'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/porous_flow/examples/tutorial/00.i)
# Creates the mesh for the remainder of the tutorial
[Mesh]
[annular]
type = AnnularMeshGenerator
nr = 10
rmin = 1.0
rmax = 10
growth_r = 1.4
nt = 4
dmin = 0
dmax = 90
[]
[make3D]
type = MeshExtruderGenerator
extrusion_vector = '0 0 12'
num_layers = 3
bottom_sideset = 'bottom'
top_sideset = 'top'
input = annular
[]
[shift_down]
type = TransformGenerator
transform = TRANSLATE
vector_value = '0 0 -6'
input = make3D
[]
[aquifer]
type = SubdomainBoundingBoxGenerator
block_id = 1
bottom_left = '0 0 -2'
top_right = '10 10 2'
input = shift_down
[]
[injection_area]
type = ParsedGenerateSideset
combinatorial_geometry = 'x*x+y*y<1.01'
included_subdomain_ids = 1
new_sideset_name = 'injection_area'
input = 'aquifer'
[]
[rename]
type = RenameBlockGenerator
old_block = '0 1'
new_block = 'caps aquifer'
input = 'injection_area'
[]
[]
[Variables]
[dummy_var]
[]
[]
[Kernels]
[dummy_diffusion]
type = Diffusion
variable = dummy_var
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
file_base = 3D_mesh
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-rc-no-slip.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 10
ymin = -1
ymax = 1
nx = 100
ny = 20
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = 1
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_x
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_y
function = '0'
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = vel_x
function = 0
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = vel_y
function = 0
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = '0'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 200 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[]
(test/tests/materials/get_material_property_names/get_material_property_boundary_names.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Materials]
[./material]
type = GenericConstantMaterial
prop_names = combo
boundary = 'left right'
prop_values = 12345
[../]
[]
[UserObjects]
[./get_material_boundary_names_test]
type = GetMaterialPropertyBoundaryBlockNamesTest
expected_names = 'left right'
property_name = combo
test_type = 'boundary'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/ray_tracing/test/tests/raykernels/aux_ray_kernel/const_monomial_only.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
[]
[]
[UserObjects/study]
type = RepeatableRayStudy
start_points = '0 0 0'
directions = '1 0 0'
names = 'ray'
execute_on = INITIAL
[]
[AuxVariables/aux]
[]
[RayKernels/distance]
type = RayDistanceAux
variable = aux
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
(test/tests/kernels/hfem/dirichlet.i)
[Mesh]
[square]
type = GeneratedMeshGenerator
nx = 3
ny = 3
dim = 2
[]
build_all_side_lowerd_mesh = true
[]
[Variables]
[u]
order = THIRD
family = MONOMIAL
block = 0
[]
[uhat]
order = CONSTANT
family = MONOMIAL
block = BOUNDARY_SIDE_LOWERD_SUBDOMAIN
[]
[lambda]
order = CONSTANT
family = MONOMIAL
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
[]
[lambdab]
order = CONSTANT
family = MONOMIAL
block = BOUNDARY_SIDE_LOWERD_SUBDOMAIN
[]
[]
[AuxVariables]
[v]
order = CONSTANT
family = MONOMIAL
block = 0
initial_condition = '1'
[]
[]
[Kernels]
[diff]
type = MatDiffusion
variable = u
diffusivity = '1'
block = 0
[]
[source]
type = CoupledForce
variable = u
v = v
coef = '1'
block = 0
[]
[reaction]
type = Reaction
variable = uhat
rate = '1'
block = BOUNDARY_SIDE_LOWERD_SUBDOMAIN
[]
[uhat_coupled]
type = CoupledForce
variable = uhat
block = BOUNDARY_SIDE_LOWERD_SUBDOMAIN
v = lambdab
coef = '1'
[]
[]
[DGKernels]
[surface]
type = HFEMDiffusion
variable = u
lowerd_variable = lambda
[]
[]
[BCs]
[all]
type = HFEMDirichletBC
boundary = 'left right top bottom'
variable = u
lowerd_variable = lambdab
uhat = uhat
[]
[]
[Postprocessors]
[intu]
type = ElementIntegralVariablePostprocessor
variable = u
block = 0
[]
[lambdanorm]
type = ElementL2Norm
variable = lambda
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu basic mumps'
[]
[Outputs]
[out]
# we hide lambda because it may flip sign due to element
# renumbering with distributed mesh
type = Exodus
hide = lambda
[]
csv = true
[]
(modules/combined/test/tests/multiphase_mechanics/twophasestress.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
xmin = 0
xmax = 2
ymin = 0
ymax = 2
elem_type = QUAD4
[]
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./eta]
[./InitialCondition]
type = FunctionIC
function = 'x/2'
[../]
[../]
[./e11_aux]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./matl_e11]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 0
variable = e11_aux
[../]
[]
[Kernels]
[./TensorMechanics]
[../]
[]
[Materials]
[./elasticity_tensor_A]
type = ComputeElasticityTensor
base_name = A
fill_method = symmetric9
C_ijkl = '1e6 1e5 1e5 1e6 0 1e6 .4e6 .2e6 .5e6'
[../]
[./strain_A]
type = ComputeSmallStrain
base_name = A
eigenstrain_names = eigenstrain
[../]
[./stress_A]
type = ComputeLinearElasticStress
base_name = A
[../]
[./eigenstrain_A]
type = ComputeEigenstrain
base_name = A
eigen_base = '0.1 0.05 0 0 0 0.01'
prefactor = -1
eigenstrain_name = eigenstrain
[../]
[./elasticity_tensor_B]
type = ComputeElasticityTensor
base_name = B
fill_method = symmetric9
C_ijkl = '1e6 0 0 1e6 0 1e6 .5e6 .5e6 .5e6'
[../]
[./strain_B]
type = ComputeSmallStrain
base_name = B
eigenstrain_names = 'B_eigenstrain'
[../]
[./stress_B]
type = ComputeLinearElasticStress
base_name = B
[../]
[./eigenstrain_B]
type = ComputeEigenstrain
base_name = B
eigen_base = '0.1 0.05 0 0 0 0.01'
prefactor = -1
eigenstrain_name = 'B_eigenstrain'
[../]
[./switching]
type = SwitchingFunctionMaterial
eta = eta
[../]
[./combined]
type = TwoPhaseStressMaterial
base_A = A
base_B = B
[../]
[]
[BCs]
[./bottom_y]
type = DirichletBC
variable = disp_y
boundary = 'bottom'
value = 0
[../]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = 'left'
value = 0
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(test/tests/outputs/postprocessor/postprocessor_invalid.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[AuxVariables]
[./aux0]
order = SECOND
family = SCALAR
[../]
[./aux1]
family = SCALAR
initial_condition = 5
[../]
[./aux2]
family = SCALAR
initial_condition = 10
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./diff_v]
type = CoefDiffusion
variable = v
coef = 2
[../]
[]
[BCs]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[./left_u]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = right
value = 3
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = left
value = 2
[../]
[]
[Postprocessors]
[./num_vars]
type = NumVars
system = 'NL'
outputs = 'exodus2 console'
[../]
[./num_aux]
type = NumVars
system = 'AUX'
outputs = 'exodus'
[../]
[./num_nonlinear]
type = NumVars
system = 'NL'
outputs = 'all'
[../]
[./num_dofs]
type = NumDOFs
outputs = 'none'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
[./exodus]
type = Exodus
[../]
[./exodus2]
type = Exodus
[../]
[]
[ICs]
[./aux0_IC]
variable = aux0
values = '12 13'
type = ScalarComponentIC
[../]
[]
(test/tests/mesh/mesh_generation/mesh_generation_test.i)
###########################################################
# This is a simple test of the Mesh System. This
# test demonstrates the usage of GeneratedMesh. It
# builds a square domain on demand.
#
# @Requirement F2.10
###########################################################
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
nz = 0
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
# Mesh Generation produces boundaries in counter-clockwise fashion
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/misc/check_error/function_file_test3.i)
# Test for usage of missing function
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = ic_function
[../]
[../]
[]
[Functions]
[./ic_function]
type = PiecewiseLinear
data_file = piecewise_linear_mixed_lengths.csv #Will generate error because length of data doesn't match on all rows
format = rows
scale_factor = 1.0
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/fvkernels/vector-interpolation/test.i)
a=1.1
[Mesh]
[gen_mesh]
type = GeneratedMeshGenerator
dim = 1
xmin = 0.1
xmax = 1.1
nx = 20
[]
[]
[GlobalParams]
limiter = 'vanLeer'
[]
[ICs]
[u]
type = FunctionIC
variable = u
function = exact
[]
[v]
type = FunctionIC
variable = v
function = exact
[]
[w]
type = FunctionIC
variable = w
function = exact
[]
[]
[Variables]
[u]
type = MooseVariableFVReal
[]
[v]
type = MooseVariableFVReal
[]
[w]
type = MooseVariableFVReal
[]
[]
[FVKernels]
[advection_u]
type = FVLimitedVectorAdvection
variable = u
velocity = '${a} 0 0'
boundaries_to_force = 'right'
x_functor = 'u'
y_functor = 'v'
z_functor = 'w'
component = 0
[]
[body_u]
type = FVBodyForce
variable = u
function = 'forcing'
[]
[advection_v]
type = FVLimitedVectorAdvection
variable = v
velocity = '${a} 0 0'
boundaries_to_force = 'right'
x_functor = 'u'
y_functor = 'v'
z_functor = 'w'
component = 1
[]
[body_v]
type = FVBodyForce
variable = v
function = 'forcing'
[]
[advection_w]
type = FVLimitedVectorAdvection
variable = w
velocity = '${a} 0 0'
boundaries_to_force = 'right'
x_functor = 'u'
y_functor = 'v'
z_functor = 'w'
component = 2
[]
[body_w]
type = FVBodyForce
variable = w
function = 'forcing'
[]
[]
[FVBCs]
[left_u]
type = FVFunctionNeumannBC
boundary = 'left'
function = 'advection'
variable = u
[]
[left_v]
type = FVFunctionNeumannBC
boundary = 'left'
function = 'advection'
variable = v
[]
[left_w]
type = FVFunctionNeumannBC
boundary = 'left'
function = 'advection'
variable = w
[]
[]
[Functions]
[exact]
type = ParsedFunction
value = 'cos(x)'
[]
[advection]
type = ParsedFunction
value = '${a} * cos(x)'
[]
[forcing]
type = ParsedFunction
value = '-${a} * sin(x)'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
[]
[Outputs]
exodus = true
[]
(test/tests/geomsearch/fake_block_to_boundary/fake_block_to_boundary.i)
[Mesh]
type = FileMesh
file = fake_geom_search.e
dim = 2
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./distance_to_left_nodes]
[../]
[./penetration_to_left]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./nodal_distance_aux]
type = NearestNodeDistanceAux
variable = distance_to_left_nodes
boundary = 100
paired_boundary = left
[../]
[./penetration_aux]
type = PenetrationAux
variable = penetration_to_left
boundary = 100
paired_boundary = left
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/append_date/append_date.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
append_date = true
[./date]
type = Exodus
append_date_format = '%m-%d-%Y'
[../]
[]
(test/tests/interfacekernels/3d_interface/vector_3d.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
nx = 2
xmax = 2
ny = 2
ymax = 2
nz = 2
zmax = 2
elem_type = HEX20
[]
[./subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '0 0 0'
top_right = '1 1 1'
block_id = 1
[../]
[./break_boundary]
type = BreakBoundaryOnSubdomainGenerator
input = subdomain1
[../]
[./interface]
type = SideSetsBetweenSubdomainsGenerator
input = break_boundary
primary_block = '0'
paired_block = '1'
new_boundary = 'primary0_interface'
[../]
[]
[Variables]
[./u]
order = FIRST
family = NEDELEC_ONE
block = 0
[../]
[./v]
order = FIRST
family = NEDELEC_ONE
block = 1
[../]
[]
[Kernels]
[./curl_u_plus_u]
type = VectorFEWave
variable = u
x_forcing_func = 1
y_forcing_func = 1
z_forcing_func = 1
block = 0
[../]
[./curl_v_plus_v]
type = VectorFEWave
variable = v
block = 1
[../]
[]
[InterfaceKernels]
[./parallel]
type = VectorPenaltyInterfaceDiffusion
variable = u
neighbor_var = v
boundary = primary0_interface
penalty = 1e6
[../]
[]
[BCs]
# Natural condition of VectorFEWave weak form is curl(u) = 0, curl(v) = 0
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
[]
[Outputs]
exodus = true
print_linear_residuals = true
[]
(test/tests/transfers/multiapp_copy_transfer/constant_monomial_to_sub/sub.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
family = MONOMIAL
order = CONSTANT
[../]
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/stochastic_tools/test/tests/surrogates/pod_rb/errors/sub.i)
[Problem]
type = FEProblem
extra_tag_vectors = 'diff react bodyf'
[]
[Mesh]
type = GeneratedMesh
dim = 1
nx = 15
xmax = 10
[]
[Variables]
[u]
[]
[]
[Kernels]
[diffusion]
type = MatDiffusion
variable = u
diffusivity = k
extra_vector_tags = 'diff'
[]
[reaction]
type = MaterialReaction
variable = u
coefficient = alpha
extra_vector_tags = 'react'
[]
[source]
type = BodyForce
variable = u
value = 1.0
extra_vector_tags = 'bodyf'
[]
[]
[Materials]
[k]
type = GenericConstantMaterial
prop_names = k
prop_values = 1.0
[]
[alpha]
type = GenericConstantMaterial
prop_names = alpha
prop_values = 1.0
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 0
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Controls]
[stochastic]
type = SamplerReceiver
[]
[]
[Outputs]
[]
(test/tests/performance/input.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/debug/show_top_residuals_nonlinear_only.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[./debug] # This is only a test, this should be turned on via the [Debug] block
type = TopResidualDebugOutput
num_residuals = 1
execute_on = nonlinear
[../]
[]
(modules/tensor_mechanics/test/tests/lagrangian/updated/stabilization/cook_small.i)
[GlobalParams]
displacements = 'disp_x disp_y'
large_kinematics = false
stabilize_strain = true
[]
[Mesh]
type = FileMesh
file = cook_mesh.exo
dim = 2
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[]
[Kernels]
[sdx]
type = UpdatedLagrangianStressDivergence
variable = disp_x
component = 0
[]
[sdy]
type = UpdatedLagrangianStressDivergence
variable = disp_y
component = 1
[]
[]
[AuxVariables]
[strain_xx]
order = CONSTANT
family = MONOMIAL
[]
[strain_yy]
order = CONSTANT
family = MONOMIAL
[]
[strain_zz]
order = CONSTANT
family = MONOMIAL
[]
[strain_xy]
order = CONSTANT
family = MONOMIAL
[]
[strain_xz]
order = CONSTANT
family = MONOMIAL
[]
[strain_yz]
order = CONSTANT
family = MONOMIAL
[]
[stress_xx]
order = CONSTANT
family = MONOMIAL
[]
[stress_yy]
order = CONSTANT
family = MONOMIAL
[]
[stress_zz]
order = CONSTANT
family = MONOMIAL
[]
[stress_xy]
order = CONSTANT
family = MONOMIAL
[]
[stress_yz]
order = CONSTANT
family = MONOMIAL
[]
[stress_xz]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[stress_xx]
type = RankTwoAux
rank_two_tensor = cauchy_stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[]
[stress_yy]
type = RankTwoAux
rank_two_tensor = cauchy_stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[]
[stress_zz]
type = RankTwoAux
rank_two_tensor = cauchy_stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[]
[stress_xy]
type = RankTwoAux
rank_two_tensor = cauchy_stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[]
[stress_xz]
type = RankTwoAux
rank_two_tensor = cauchy_stress
variable = stress_xz
index_i = 0
index_j = 2
execute_on = timestep_end
[]
[stress_yz]
type = RankTwoAux
rank_two_tensor = cauchy_stress
variable = stress_yz
index_i = 1
index_j = 2
execute_on = timestep_end
[]
[strain_xx]
type = RankTwoAux
rank_two_tensor = mechanical_strain
variable = strain_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[]
[strain_yy]
type = RankTwoAux
rank_two_tensor = mechanical_strain
variable = strain_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[]
[strain_zz]
type = RankTwoAux
rank_two_tensor = mechanical_strain
variable = strain_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[]
[strain_xy]
type = RankTwoAux
rank_two_tensor = mechanical_strain
variable = strain_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[]
[strain_xz]
type = RankTwoAux
rank_two_tensor = mechanical_strain
variable = strain_xz
index_i = 0
index_j = 2
execute_on = timestep_end
[]
[strain_yz]
type = RankTwoAux
rank_two_tensor = mechanical_strain
variable = strain_yz
index_i = 1
index_j = 2
execute_on = timestep_end
[]
[]
[BCs]
[fixed_x]
type = DirichletBC
preset = true
variable = disp_x
boundary = canti
value = 0.0
[]
[fixed_y]
type = DirichletBC
preset = true
variable = disp_y
boundary = canti
value = 0.0
[]
[pull]
type = NeumannBC
variable = disp_y
boundary = loading
value = 10.0
[]
[]
[Materials]
[elastic_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 250.0
poissons_ratio = 0.4999999
[]
[compute_stress]
type = ComputeLagrangianLinearElasticStress
[]
[compute_strain]
type = ComputeLagrangianStrain
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = 'newton'
line_search = 'none'
petsc_options_iname = -pc_type
petsc_options_value = lu
nl_abs_tol = 1e-10
nl_rel_tol = 1e-6
l_tol = 1e-10
[]
[Postprocessors]
[value]
type = PointValue
variable = disp_y
point = '48 60 0'
use_displaced_mesh = false
[]
[]
[Outputs]
exodus = false
csv = true
[]
(modules/thermal_hydraulics/test/tests/utils/smooth_transition/smooth_transition.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 100
xmin = -2
xmax = 2
[]
[Variables]
[u]
[]
[]
[ICs]
[u_ic]
type = FunctionIC
variable = u
function = u_ic_fn
[]
[]
[Functions]
[u_ic_fn]
type = ParsedFunction
value = 'x'
[]
[]
[Materials]
[test_mat]
type = SmoothTransitionTestMaterial
transition_type = cubic
var = u
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[VectorPostprocessors]
[test_vpp]
type = Sampler1DReal
block = 0
property = mymatprop
sort_by = x
execute_on = 'INITIAL'
[]
[]
[Outputs]
csv = true
file_base = 'cubic_nonad'
execute_on = 'INITIAL'
[]
(modules/thermal_hydraulics/test/tests/vectorpostprocessors/sampler_1d_real/sampler_1d_real.i)
# Tests the Sampler1DReal vector post-processor, which samples a scalar-valued
# material on a block of a 1-D mesh. This test solves a diffusion problem and
# sets up a constant material to sample.
[Mesh]
type = GeneratedMesh
xmax = 10
dim = 1
nx = 5
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Materials]
[mat]
type = ConstantMaterial
property_name = test_property
value = 7
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[VectorPostprocessors]
[test_property_vpp]
type = Sampler1DReal
block = 0
property = test_property
sort_by = x
[]
[]
[Outputs]
[out]
type = CSV
file_base = out
execute_vector_postprocessors_on = timestep_end
show = 'test_property_vpp'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-scalar-transport-action.i)
mu=1
rho=1
k=1e-3
diff=1e-3
cp=1
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 10
ymin = -1
ymax = 1
nx = 100
ny = 20
[]
[]
[Variables]
inactive = 'vel_x vel_y pressure T_fluid scalar'
[vel_x]
type = 'INSFVVelocityVariable'
initial_condition = 1
block=0
[]
[vel_y]
type = 'INSFVVelocityVariable'
initial_condition = 1
block=0
[]
[pressure]
type = 'INSFVPressureVariable'
initial_condition = 0
block=0
[]
[T_fluid]
type = 'INSFVEnergyVariable'
initial_condition = 0
[]
[scalar]
type = MooseVariableFVReal
initial_condition = 0
[]
[]
[Modules]
[NavierStokesFV]
compressibility = 'incompressible'
add_energy_equation = true
passive_scalar_names = 'scalar'
density = ${rho}
dynamic_viscosity = ${mu}
thermal_conductivity = ${k}
specific_heat = ${cp}
passive_scalar_diffusivity = ${diff}
passive_scalar_source = 0.1
passive_scalar_coupled_source = U
passive_scalar_coupled_source_coeff = 0.1
initial_velocity = '1 1 0'
initial_pressure = 0.0
initial_temperature = 0.0
inlet_boundaries = 'left'
momentum_inlet_types = 'fixed-velocity'
momentum_inlet_function = '1 0'
energy_inlet_types = 'fixed-temperature'
energy_inlet_function = '1'
passive_scalar_inlet_types = 'fixed-value'
passive_scalar_inlet_function = '1'
wall_boundaries = 'top bottom'
momentum_wall_types = 'noslip noslip'
energy_wall_types = 'heatflux heatflux'
energy_wall_function = '0 0'
outlet_boundaries = 'right'
momentum_outlet_types = 'fixed-pressure'
pressure_function = '0'
[]
[]
[AuxVariables]
[U]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[]
[AuxKernels]
[mag]
type = VectorMagnitudeAux
variable = U
x = vel_x
y = vel_y
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[]
(test/tests/auxkernels/volume_aux/side.i)
[Mesh]
[cmg]
type = CartesianMeshGenerator
dim = 2
dx = '1'
dy = '0.5 1.2'
ix = '1'
iy = '4 6'
[]
[]
[AuxVariables/volume]
order = CONSTANT
family = MONOMIAL
[]
[AuxKernels/volume_aux]
type = VolumeAux
variable = volume
boundary = right
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/interfacekernels/ik_displaced/displaced.i)
[Mesh]
displacements = 'disp_x disp_y'
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 2
xmax = 2
ny = 2
ymax = 2
[]
[./subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '0 0 0'
top_right = '1 1 0'
block_id = 1
[../]
[./interface]
type = SideSetsBetweenSubdomainsGenerator
input = subdomain1
primary_block = '0'
paired_block = '1'
new_boundary = 'primary0_interface'
[../]
[./break_boundary]
input = interface
type = BreakBoundaryOnSubdomainGenerator
[../]
[]
[AuxVariables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
block = 0
[../]
[./v]
order = FIRST
family = LAGRANGE
block = 1
[../]
[]
[Kernels]
[./diff_u]
type = CoeffParamDiffusion
variable = u
D = 4
block = 0
[../]
[./diff_v]
type = CoeffParamDiffusion
variable = v
D = 2
block = 1
[../]
[./source_u]
type = BodyForce
variable = u
value = 1
[../]
[]
[InterfaceKernels]
[./interface]
type = InterfacialSource
variable = u
neighbor_var = v
boundary = primary0_interface
use_displaced_mesh = true
[../]
[]
[BCs]
[./u]
type = VacuumBC
variable = u
boundary = 'left_to_0 bottom_to_0 right top'
[../]
[./v]
type = VacuumBC
variable = v
boundary = 'left_to_1 bottom_to_1'
[../]
[]
[Postprocessors]
[./u_int]
type = ElementIntegralVariablePostprocessor
variable = u
block = 0
[../]
[./v_int]
type = ElementIntegralVariablePostprocessor
variable = v
block = 1
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
file_base = displaced
exodus = true
[]
[Functions]
[./disp_x_func]
type = ParsedFunction
value = x
[../]
[./disp_y_func]
type = ParsedFunction
value = y
[../]
[]
[ICs]
[./disp_x_ic]
function = disp_x_func
variable = disp_x
type = FunctionIC
[../]
[./disp_y_ic]
function = disp_y_func
variable = disp_y
type = FunctionIC
[../]
[]
(test/tests/misc/line_source/line_source.i)
[Mesh]
type = FileMesh
file = line_source_cube.e
dim = 2
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
block = bulk
[../]
[./heating]
type = BodyForce
variable = u
function = 1
block = heater
[../]
[]
[BCs]
[./outside]
type = DirichletBC
variable = u
boundary = outside
value = 0
[../]
[]
[Materials]
[./diffusivity]
type = GenericConstantMaterial
block = 'bulk heater'
prop_names = diffusivity
prop_values = 1
[../]
[]
[Postprocessors]
[./total_flux]
type = SideDiffusiveFluxIntegral
variable = u
boundary = outside
diffusivity = diffusivity
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/kernels/ad_simple_diffusion/ad_simple_diffusion.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = ADDiffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
# Preconditioned JFNK (default)
solve_type = 'Newton'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
l_tol = 1e-10
nl_rel_tol = 1e-9
nl_max_its = 1
[]
[Outputs]
exodus = true
[]
(test/tests/postprocessors/side_diffusive_flux_integral/vector_functor_prop.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Functions]
[./right_bc]
# Flux BC for computing the analytical solution in the postprocessor
type = ParsedFunction
value = exp(y)+1
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = FunctionNeumannBC
variable = u
boundary = right
function = right_bc
[../]
[]
[Materials]
[./mat_props_vector_functor]
type = ADGenericVectorFunctorMaterial
prop_names = diffusivity_vec
prop_values = '1 1.5 1'
[../]
[conversion]
type = PropFromFunctorProp
vector_functor = diffusivity_vec
vector_prop = diffusivity_vec
[]
[]
[Postprocessors]
[./avg_flux_right]
# Computes -\int(exp(y)+1) from 0 to 1 which is -2.718281828
type = ADSideVectorDiffusivityFluxIntegral
variable = u
boundary = right
diffusivity = diffusivity_vec
[../]
[./avg_flux_top]
type = ADSideVectorDiffusivityFluxIntegral
variable = u
boundary = top
diffusivity = diffusivity_vec
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/chemical_reactions/test/tests/jacobian/coupled_convreact2.i)
# Test the Jacobian terms for the CoupledConvectionReactionSub Kernel using
# activity coefficients not equal to unity
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
[./a]
order = FIRST
family = LAGRANGE
[../]
[./b]
order = FIRST
family = LAGRANGE
[../]
[./pressure]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./pressure]
type = RandomIC
variable = pressure
min = 1
max = 5
[../]
[./a]
type = RandomIC
variable = a
max = 1
min = 0
[../]
[./b]
type = RandomIC
variable = b
max = 1
min = 0
[../]
[]
[Kernels]
[./diff]
type = DarcyFluxPressure
variable = pressure
[../]
[./diff_b]
type = Diffusion
variable = b
[../]
[./a1conv]
type = CoupledConvectionReactionSub
variable = a
v = b
log_k = 2
weight = 1
sto_v = 2.5
sto_u = 2
p = pressure
gamma_eq = 2
gamma_u = 2.5
gamma_v = 1.5
[../]
[]
[Materials]
[./porous]
type = GenericConstantMaterial
prop_names = 'diffusivity conductivity porosity'
prop_values = '1e-4 1e-4 0.2'
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
perf_graph = true
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
(test/tests/fvkernels/fv_simple_diffusion/unstructured-rz.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
elem_type = TRI3
[]
[Variables]
[v]
family = MONOMIAL
order = CONSTANT
fv = true
[]
[]
[FVKernels]
[diff]
type = FVDiffusion
variable = v
coeff = coeff
[]
[]
[Materials]
[diff]
type = ADGenericFunctorMaterial
prop_names = 'coeff'
prop_values = '1'
[]
[]
[FVBCs]
[right]
type = FVDirichletBC
boundary = right
value = 1
variable = v
[]
[]
[Problem]
type = FEProblem
coord_type = RZ
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/mesh_modifiers/add_side_sets_from_bounding_box/error_no_nodes_found.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[createNewSidesetOne]
type = SideSetsFromBoundingBoxGenerator
input = gen
block_id = 0
boundary_id_old = 'right'
boundary_id_new = 11
bottom_left = '0.5 0.5 0'
top_right = '1.9 1.9 0'
[]
[createNewSidesetTwo]
type = SideSetsFromBoundingBoxGenerator
input = createNewSidesetOne
block_id = 0
boundary_id_old = 'top right'
boundary_id_new = 10
bottom_left = '-0.1 -0.1 0'
top_right = '0.7 0.3 0'
boundary_id_overlap = true
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[leftBC]
type = DirichletBC
variable = u
boundary = 10
value = 1
[]
[rightBC]
type = DirichletBC
variable = u
boundary = 11
value = 0
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/debug/show_material_props.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[./subdomains]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '0.1 0.1 0'
block_id = 1
top_right = '0.9 0.9 0'
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Materials]
[./block]
type = GenericConstantMaterial
block = '0 1'
prop_names = 'property0 property1 property2 property3 property4 property5 property6 property7 property8 property9 property10'
prop_values = '0 1 2 3 4 5 6 7 8 9 10'
[../]
[./boundary]
type = GenericConstantMaterial
prop_names = bnd_prop
boundary = top
prop_values = 12345
[../]
[./restricted]
type = GenericConstantMaterial
block = 1
prop_names = 'restricted0 restricted1'
prop_values = '10 11'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[./debug] # This is only a test, you should turn this on via [Debug] block
type = MaterialPropertyDebugOutput
[../]
[]
(modules/navier_stokes/test/tests/finite_volume/cns/mms/1d-with-bcs/porous-hllc.i)
eps=0.9
[GlobalParams]
fp = fp
[]
[Mesh]
[cartesian]
type = GeneratedMeshGenerator
dim = 1
xmin = .1
xmax = 1.1
nx = 2
[]
[]
[Modules]
[FluidProperties]
[fp]
type = IdealGasFluidProperties
[]
[]
[]
[Variables]
[rho]
type = MooseVariableFVReal
[]
[rho_ud]
type = MooseVariableFVReal
[]
[rho_et]
type = MooseVariableFVReal
[]
[]
[ICs]
[rho]
type = FunctionIC
variable = rho
function = 'exact_rho'
[]
[rho_ud]
type = FunctionIC
variable = rho_ud
function = 'exact_rho_ud'
[]
[rho_et]
type = FunctionIC
variable = rho_et
function = 'exact_rho_et'
[]
[]
[FVKernels]
[mass_advection]
type = PCNSFVMassHLLC
variable = rho
fp = fp
[]
[mass_fn]
type = FVBodyForce
variable = rho
function = 'forcing_rho'
[]
[momentum_x_advection]
type = PCNSFVMomentumHLLC
variable = rho_ud
momentum_component = x
fp = fp
[]
[momentum_fn]
type = FVBodyForce
variable = rho_ud
function = 'forcing_rho_ud'
[]
[fluid_energy_advection]
type = PCNSFVFluidEnergyHLLC
variable = rho_et
fp = fp
[]
[energy_fn]
type = FVBodyForce
variable = rho_et
function = 'forcing_rho_et'
[]
[]
[FVBCs]
[mass_in]
variable = rho
type = PCNSFVHLLCSpecifiedMassFluxAndTemperatureMassBC
boundary = left
temperature = 'exact_T'
superficial_rhou = 'exact_rho_ud'
[]
[momentum_in]
variable = rho_ud
type = PCNSFVHLLCSpecifiedMassFluxAndTemperatureMomentumBC
boundary = left
temperature = 'exact_T'
superficial_rhou = 'exact_rho_ud'
momentum_component = 'x'
[]
[energy_in]
variable = rho_et
type = PCNSFVHLLCSpecifiedMassFluxAndTemperatureFluidEnergyBC
boundary = left
temperature = 'exact_T'
superficial_rhou = 'exact_rho_ud'
[]
[mass_out]
variable = rho
type = PCNSFVHLLCSpecifiedPressureMassBC
boundary = right
pressure = 'exact_p'
[]
[momentum_out]
variable = rho_ud
type = PCNSFVHLLCSpecifiedPressureMomentumBC
boundary = right
pressure = 'exact_p'
momentum_component = 'x'
[]
[energy_out]
variable = rho_et
type = PCNSFVHLLCSpecifiedPressureFluidEnergyBC
boundary = right
pressure = 'exact_p'
[]
[]
[Materials]
[var_mat]
type = PorousConservedVarMaterial
rho = rho
superficial_rhou = rho_ud
rho_et = rho_et
porosity = porosity
[]
[porosity]
type = GenericConstantMaterial
prop_names = 'porosity'
prop_values = '${eps}'
[]
[]
[Functions]
[exact_rho]
type = ParsedFunction
value = '3.48788261470924*cos(x)'
[]
[forcing_rho]
type = ParsedFunction
value = '-3.83667087618017*eps*sin(1.1*x)'
vars = 'eps'
vals = '${eps}'
[]
[exact_rho_ud]
type = ParsedFunction
value = '3.48788261470924*eps*cos(1.1*x)'
vars = 'eps'
vals = '${eps}'
[]
[forcing_rho_ud]
type = ParsedFunction
value = 'eps*(-(10.6975765229419*cos(1.2*x)/cos(x) - 0.697576522941849*cos(1.1*x)^2/cos(x)^2)*sin(x) + (10.6975765229419*sin(x)*cos(1.2*x)/cos(x)^2 - 1.3951530458837*sin(x)*cos(1.1*x)^2/cos(x)^3 + 1.53466835047207*sin(1.1*x)*cos(1.1*x)/cos(x)^2 - 12.8370918275302*sin(1.2*x)/cos(x))*cos(x)) + 3.48788261470924*eps*sin(x)*cos(1.1*x)^2/cos(x)^2 - 7.67334175236034*eps*sin(1.1*x)*cos(1.1*x)/cos(x)'
vars = 'eps'
vals = '${eps}'
[]
[exact_rho_et]
type = ParsedFunction
value = '26.7439413073546*cos(1.2*x)'
[]
[forcing_rho_et]
type = ParsedFunction
value = '1.0*eps*(3.48788261470924*(3.06706896551724*cos(1.2*x)/cos(x) - 0.2*cos(1.1*x)^2/cos(x)^2)*cos(x) + 26.7439413073546*cos(1.2*x))*sin(x)*cos(1.1*x)/cos(x)^2 - 1.1*eps*(3.48788261470924*(3.06706896551724*cos(1.2*x)/cos(x) - 0.2*cos(1.1*x)^2/cos(x)^2)*cos(x) + 26.7439413073546*cos(1.2*x))*sin(1.1*x)/cos(x) + 1.0*eps*(-(10.6975765229419*cos(1.2*x)/cos(x) - 0.697576522941849*cos(1.1*x)^2/cos(x)^2)*sin(x) + (10.6975765229419*sin(x)*cos(1.2*x)/cos(x)^2 - 1.3951530458837*sin(x)*cos(1.1*x)^2/cos(x)^3 + 1.53466835047207*sin(1.1*x)*cos(1.1*x)/cos(x)^2 - 12.8370918275302*sin(1.2*x)/cos(x))*cos(x) - 32.0927295688256*sin(1.2*x))*cos(1.1*x)/cos(x)'
vars = 'eps'
vals = '${eps}'
[]
[exact_T]
type = ParsedFunction
value = '0.0106975765229418*cos(1.2*x)/cos(x) - 0.000697576522941848*cos(1.1*x)^2/cos(x)^2'
vars = 'eps'
vals = '${eps}'
[]
[exact_p]
type = ParsedFunction
value = '3.48788261470924*(3.06706896551724*cos(1.2*x)/cos(x) - 0.2*cos(1.1*x)^2/cos(x)^2)*cos(x)'
vars = 'eps'
vals = '${eps}'
[]
[]
[Executioner]
solve_type = NEWTON
type = Steady
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
nl_max_its = 50
line_search = none
nl_rel_tol = 1e-12
nl_abs_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[]
[Debug]
show_var_residual_norms = true
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2rho]
type = ElementL2Error
variable = rho
function = exact_rho
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2rho_ud]
variable = rho_ud
function = exact_rho_ud
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2rho_et]
variable = rho_et
function = exact_rho_et
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(test/tests/functions/parsed/vector_function.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
uniform_refine = 1
[]
[Variables]
[./u]
[../]
[]
[Functions]
[./conductivity]
type = ParsedVectorFunction
value_y = 0.1
value_x = 0.8
[../]
[]
[Kernels]
[./diff]
type = DiffTensorKernel
variable = u
conductivity = conductivity
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./bottom]
type = DirichletBC
variable = u
boundary = bottom
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/view_factors_symmetry/cavity_with_pillars.i)
[Mesh]
[cartesian]
type = CartesianMeshGenerator
dim = 3
dx = '0.5 0.5 0.5 0.5 0.5 0.5'
dy = '0.5 0.75 0.5'
dz = '1.5 0.5'
subdomain_id = '
1 1 1 1 1 1
1 2 1 1 2 1
1 1 1 1 1 1
1 1 1 1 1 1
1 1 1 1 1 1
1 1 1 1 1 1
'
[]
[add_obstruction]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 2
paired_block = 1
new_boundary = obstruction
input = cartesian
[]
[add_new_back]
type = ParsedGenerateSideset
combinatorial_geometry = 'abs(z) < 1e-10'
included_subdomain_ids = '1'
normal = '0 0 -1'
new_sideset_name = back_2
input = add_obstruction
[]
[]
[UserObjects]
[view_factor_study]
type = ViewFactorRayStudy
execute_on = initial
boundary = 'left right top bottom front back_2 obstruction'
face_order = FOURTH
[]
[view_factor]
type = RayTracingViewFactor
boundary = 'left right top bottom front back_2 obstruction'
execute_on = INITIAL
normalize_view_factor = false
ray_study_name = view_factor_study
[]
[]
[RayBCs/viewfactor]
type = ViewFactorRayBC
boundary = 'left right top bottom front back_2 obstruction'
[]
[Postprocessors]
[left_right]
type = ViewFactorPP
from_boundary = left
to_boundary = right
view_factor_object_name = view_factor
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
[]
(modules/richards/test/tests/gravity_head_2/gh_fu_01.i)
# unsaturated = true
# gravity = false
# supg = false
# transient = false
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
xmin = 0
xmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = 'DensityWater DensityGas'
relperm_UO = 'RelPermWater RelPermGas'
SUPG_UO = 'SUPGwater SUPGgas'
sat_UO = 'SatWater SatGas'
seff_UO = 'SeffWater SeffGas'
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = 'pwater pgas'
[../]
[./DensityWater]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0E2
[../]
[./DensityGas]
type = RichardsDensityConstBulk
dens0 = 0.5
bulk_mod = 0.5E2
[../]
[./SeffWater]
type = RichardsSeff2waterVG
m = 0.8
al = 1
[../]
[./SeffGas]
type = RichardsSeff2gasVG
m = 0.8
al = 1
[../]
[./RelPermWater]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./RelPermGas]
type = RichardsRelPermPower
simm = 0.0
n = 3
[../]
[./SatWater]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.15
[../]
[./SatGas]
type = RichardsSat
s_res = 0.05
sum_s_res = 0.15
[../]
[./SUPGwater]
type = RichardsSUPGnone
[../]
[./SUPGgas]
type = RichardsSUPGnone
[../]
[]
[Variables]
[./pwater]
order = FIRST
family = LAGRANGE
[../]
[./pgas]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./water_ic]
type = RandomIC
min = 0.4
max = 0.6
variable = pwater
[../]
[./gas_ic]
type = RandomIC
min = 1.4
max = 1.6
variable = pgas
[../]
[]
[Kernels]
active = 'richardsfwater richardsfgas'
[./richardstwater]
type = RichardsMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFullyUpwindFlux
variable = pwater
[../]
[./richardstgas]
type = RichardsMassChange
variable = pgas
[../]
[./richardsfgas]
type = RichardsFullyUpwindFlux
variable = pgas
[../]
[]
[AuxVariables]
[./seffgas]
[../]
[./seffwater]
[../]
[]
[AuxKernels]
[./seffgas_kernel]
type = RichardsSeffAux
pressure_vars = 'pwater pgas'
seff_UO = SeffGas
variable = seffgas
[../]
[./seffwater_kernel]
type = RichardsSeffAux
pressure_vars = 'pwater pgas'
seff_UO = SeffWater
variable = seffwater
[../]
[]
[Postprocessors]
[./mwater_init]
type = RichardsMass
variable = pwater
execute_on = timestep_begin
outputs = none
[../]
[./mgas_init]
type = RichardsMass
variable = pgas
execute_on = timestep_begin
outputs = none
[../]
[./mwater_fin]
type = RichardsMass
variable = pwater
execute_on = timestep_end
outputs = none
[../]
[./mgas_fin]
type = RichardsMass
variable = pgas
execute_on = timestep_end
outputs = none
[../]
[./mass_error_water]
type = FunctionValuePostprocessor
function = fcn_mass_error_w
outputs = none # no reason why mass should be conserved
[../]
[./mass_error_gas]
type = FunctionValuePostprocessor
function = fcn_mass_error_g
outputs = none # no reason why mass should be conserved
[../]
[./pw_left]
type = PointValue
point = '0 0 0'
variable = pwater
outputs = none
[../]
[./pw_right]
type = PointValue
point = '1 0 0'
variable = pwater
outputs = none
[../]
[./error_water]
type = FunctionValuePostprocessor
function = fcn_error_water
[../]
[./pg_left]
type = PointValue
point = '0 0 0'
variable = pgas
outputs = none
[../]
[./pg_right]
type = PointValue
point = '1 0 0'
variable = pgas
outputs = none
[../]
[./error_gas]
type = FunctionValuePostprocessor
function = fcn_error_gas
[../]
[]
[Functions]
[./fcn_mass_error_w]
type = ParsedFunction
value = 'abs(0.5*(mi-mf)/(mi+mf))'
vars = 'mi mf'
vals = 'mwater_init mwater_fin'
[../]
[./fcn_mass_error_g]
type = ParsedFunction
value = 'abs(0.5*(mi-mf)/(mi+mf))'
vars = 'mi mf'
vals = 'mgas_init mgas_fin'
[../]
[./fcn_error_water]
type = ParsedFunction
value = 'abs((p0-p1)/p1)'
vars = 'b gdens0 p0 xval p1'
vals = '1E2 -1 pw_left 1 pw_right'
[../]
[./fcn_error_gas]
type = ParsedFunction
value = 'abs((p0-p1)/p1)'
vars = 'b gdens0 p0 xval p1'
vals = '0.5E2 -0.5 pg_left 1 pg_right'
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
viscosity = '1E-3 0.5E-3'
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-pc_factor_shift_type'
petsc_options_value = 'nonzero'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
nl_rel_tol = 1.e-10
nl_max_its = 10
[]
[Outputs]
execute_on = 'timestep_end'
file_base = gh_fu_01
csv = true
[]
(test/tests/transfers/multiapp_high_order_variable_transfer/master_L2_Lagrange.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
[]
[Variables]
[power_density]
family = L2_LAGRANGE
order = FIRST
[]
[]
[Functions]
[pwr_func]
type = ParsedFunction
value = '1e3*x*(1-x)+5e2'
[]
[]
[Kernels]
[diff]
type = Reaction
variable = power_density
[]
[coupledforce]
type = BodyForce
variable = power_density
function = pwr_func
[]
[]
[Postprocessors]
[pwr_avg]
type = ElementAverageValue
block = '0'
variable = power_density
execute_on = 'initial timestep_end'
[]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart '
petsc_options_value = 'hypre boomeramg 100'
nl_abs_tol = 1e-8
nl_rel_tol = 1e-12
[]
[MultiApps]
[sub]
type = FullSolveMultiApp
app_type = MooseTestApp
positions = '0 0 0'
input_files = sub_L2_Lagrange.i
execute_on = 'timestep_end'
[]
[]
[Transfers]
[p_to_sub]
type = MultiAppMeshFunctionTransfer
source_variable = power_density
variable = power_density
to_multi_app = sub
execute_on = 'timestep_end'
[]
[]
[Outputs]
exodus = true
perf_graph = true
[]
(test/tests/userobjects/element_quality_check/failure_warning.i)
[Mesh]
file = Quad.e
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./top]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[UserObjects]
[./elem_quality_check]
type = ElementQualityChecker
metric_type = STRETCH
failure_type = WARNING
upper_bound = 1.0
lower_bound = 0.5
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(python/peacock/tests/input_tab/InputTreeWriter/gold/simple_diffusion_no_diff.i)
[Mesh]
[generate]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
inactive = 'diff'
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[]
[]
[Executioner]
# Preconditioned JFNK (default)
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_mortar/ref-displaced.i)
[Mesh]
file = 3blk.e
displacements = 'disp_x disp_y'
[]
[AuxVariables]
[./disp_x]
block = 1
[../]
[./disp_y]
block = 1
[../]
[]
[AuxKernels]
[./disp_x_kernel]
type = ConstantAux
variable = disp_x
value = 0.1
[../]
[./disp_y_kernel]
type = ConstantAux
variable = disp_y
value = 0
[../]
[]
[Variables]
[./temp]
order = FIRST
family = LAGRANGE
block = '1 2 3'
[../]
[]
[Materials]
[./left]
type = HeatConductionMaterial
block = 1
thermal_conductivity = 1000
specific_heat = 1
[../]
[./right]
type = HeatConductionMaterial
block = 2
thermal_conductivity = 500
specific_heat = 1
[../]
[./middle]
type = HeatConductionMaterial
block = 3
thermal_conductivity = 100
specific_heat = 1
[../]
[]
[Kernels]
[./hc]
type = HeatConduction
variable = temp
use_displaced_mesh = true
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = temp
boundary = 'left'
value = 1
[../]
[./right]
type = DirichletBC
variable = temp
boundary = 'right'
value = 0
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
nl_rel_tol = 1e-11
l_tol = 1e-11
[]
[Outputs]
exodus = true
[]
(test/tests/kernels/forcing_function/forcing_function_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
uniform_refine = 4
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
active = 'forcing_func'
[./forcing_func]
type = ParsedFunction
value = alpha*alpha*pi*pi*sin(alpha*pi*x)
vars = 'alpha'
vals = '16'
[../]
[]
[Kernels]
active = 'diff forcing'
[./diff]
type = Diffusion
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_func
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-12
[]
[Outputs]
execute_on = 'timestep_end'
file_base = out
exodus = true
[]
(test/tests/geomsearch/quadrature_nearest_node_locator/quadrature_nearest_node_locator.i)
[Mesh]
file = 2dcontact_collide.e
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./distance]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./distance]
type = NearestNodeDistanceAux
variable = distance
boundary = 2
paired_boundary = 3
[../]
[]
[BCs]
[./block1_left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./block1_right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[./block2_left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./block2_right]
type = DirichletBC
variable = u
boundary = 4
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/debug/show_material_props_consumed.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[]
[Variables/u]
[]
[Kernels]
[diff]
type = MatDiffusion
variable = u
[]
[diff2]
type = MatDiffusion
variable = u
diffusivity = 'andrew'
[]
[]
[Materials]
[block]
type = GenericConstantMaterial
block = '0'
prop_names = 'D andrew'
prop_values = '1 1980'
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
[debug] # This is only a test, you should turn this on via [Debug] block
type = MaterialPropertyDebugOutput
[]
[]
(test/tests/ics/function_ic/spline_function.i)
#
# Test the gradient calculation in spline function and the gradient pass-through in FunctionIC
#
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 3
ymin = 0
ymax = 1
nx = 10
ny = 2
[]
[Variables]
[./u]
order = THIRD
family = HERMITE
[../]
[]
[Functions]
[./spline_function]
type = SplineFunction
x = '0 1 2 3'
y = '0 1 0 1'
[../]
[]
[ICs]
[./u_ic]
type = FunctionIC
variable = 'u'
function = spline_function
[../]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Outputs]
file_base = spline
[./OverSampling]
type = Exodus
refinements = 3
[../]
[]
(test/tests/userobjects/nearest_point_layered_average/nearest_point_layered_average.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 10
ny = 10
nz = 10
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./np_layered_average]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./np_layered_average]
type = SpatialUserObjectAux
variable = np_layered_average
execute_on = timestep_end
user_object = npla
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./one]
type = DirichletBC
variable = u
boundary = 'right back top'
value = 1
[../]
[]
[UserObjects]
[./npla]
type = NearestPointLayeredAverage
direction = y
num_layers = 10
variable = u
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/mortar/continuity-2d-conforming/conforming_two_var.i)
[Mesh]
[file]
type = FileMeshGenerator
file = 2blk-conf.e
[]
[secondary]
input = file
type = LowerDBlockFromSidesetGenerator
sidesets = '101'
new_block_id = '10001'
new_block_name = 'secondary_lower'
[]
[primary]
input = secondary
type = LowerDBlockFromSidesetGenerator
sidesets = '100'
new_block_id = '10000'
new_block_name = 'primary_lower'
[]
[]
[Functions]
[./exact_sln]
type = ParsedFunction
value = y
[../]
[./ffn]
type = ParsedFunction
value = 0
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
block = '1 2'
[../]
[./lm_u]
order = FIRST
family = LAGRANGE
block = 'secondary_lower'
[../]
[./v]
order = FIRST
family = LAGRANGE
block = '1 2'
[../]
[./lm_v]
order = FIRST
family = LAGRANGE
block = 'secondary_lower'
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = ffn
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[./coupled_u]
type = CoupledForce
variable = v
v = u
[../]
[]
[Constraints]
[./ced_u]
type = EqualValueConstraint
variable = lm_u
secondary_variable = u
primary_boundary = 100
primary_subdomain = 10000
secondary_boundary = 101
secondary_subdomain = 10001
[../]
[./ced_v]
type = EqualValueConstraint
variable = lm_v
secondary_variable = v
primary_boundary = 100
primary_subdomain = 10000
secondary_boundary = 101
secondary_subdomain = 10001
[../]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
boundary = '1 2 3 4'
function = exact_sln
[../]
[./allv]
type = DirichletBC
variable = v
boundary = '1 2 3 4'
value = 0
[../]
[]
[Postprocessors]
[./l2_error]
type = ElementL2Error
variable = u
function = exact_sln
block = '1 2'
execute_on = 'initial timestep_end'
[../]
[./l2_v]
type = ElementL2Norm
variable = v
block = '1 2'
execute_on = 'initial timestep_end'
[../]
[]
[Preconditioning]
[./fmp]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-12
l_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(modules/functional_expansion_tools/test/tests/errors/bc_flux_bad_function.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Variables]
[./v]
[../]
[]
[BCs]
[./this_could_be_bad]
type = FXFluxBC
boundary = right
function = const
variable = v
[../]
[]
[Functions]
[./const]
type = ConstantFunction
value = -1
[../]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
(modules/tensor_mechanics/test/tests/action/two_coord.i)
[Mesh]
[generated_mesh]
type = GeneratedMeshGenerator
dim = 2
nx = 16
ny = 8
xmin = -1
xmax = 1
[]
[block1]
type = SubdomainBoundingBoxGenerator
block_id = 1
bottom_left = '-1 0 0'
top_right = '0 1 0'
input = generated_mesh
[]
[block2]
type = SubdomainBoundingBoxGenerator
block_id = 2
bottom_left = '0 0 0'
top_right = '1 1 0'
input = block1
[]
[]
[Problem]
coord_type = 'XYZ RZ'
block = '1 2'
[]
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Modules/TensorMechanics/Master]
active = 'block1 block2'
[./error]
strain = SMALL
add_variables = true
[../]
[./block1]
strain = SMALL
add_variables = true
block = 1
[../]
[./block2]
strain = SMALL
add_variables = true
block = 2
[../]
[]
[AuxVariables]
[./vmstress]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./vmstress]
type = RankTwoScalarAux
rank_two_tensor = total_strain
variable = vmstress
scalar_type = VonMisesStress
execute_on = timestep_end
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e10
poissons_ratio = 0.345
[../]
[./_elastic_stress]
type = ComputeLinearElasticStress
block = '1 2'
[../]
[]
[BCs]
[./topx]
type = DirichletBC
boundary = 'top'
variable = disp_x
value = 0.0
[../]
[./topy]
type = DirichletBC
boundary = 'top'
variable = disp_y
value = 0.0
[../]
[./bottomx]
type = DirichletBC
boundary = 'bottom'
variable = disp_x
value = 0.0
[../]
[./bottomy]
type = DirichletBC
boundary = 'bottom'
variable = disp_y
value = 0.05
[../]
[]
[Debug]
show_var_residual_norms = true
[]
[Executioner]
type = Steady
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = ' 201 hypre boomeramg 10'
line_search = 'none'
nl_rel_tol = 5e-9
nl_abs_tol = 1e-10
nl_max_its = 15
l_tol = 1e-3
l_max_its = 50
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/code_verification/spherical_test_no4.i)
# Problem III.4
#
# A spherical shell has thermal conductivity k and heat generation q.
# It has an inner radius ri and outer radius ro. A constant heat flux is
# applied to the inside surface qin and the outside surface is exposed
# to a fluid temperature uf and heat transfer coefficient h.
#
# REFERENCE:
# A. Toptan, et al. (Mar.2020). Tech. rep. CASL-U-2020-1939-000, SAND2020-3887 R. DOI:10.2172/1614683.
[Mesh]
[./geom]
type = GeneratedMeshGenerator
dim = 1
elem_type = EDGE2
xmin = 0.2
nx = 4
[../]
[]
[Variables]
[./u]
order = FIRST
[../]
[]
[Problem]
coord_type = RSPHERICAL
[]
[Functions]
[./exact]
type = ParsedFunction
vars = 'qin q k ri ro uf h'
vals = '100 1200 1.0 0.2 1 100 10'
value = 'uf+ (q/(6*k)) * ( ro^2-x^2 + 2*k*(ro^3-ri^3)/(h*ro^2) + 2 * ri^3 * (1/ro-1/x) ) + (1/x-1/ro+k/(h*ro^2)) * qin * ri^2 / k'
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = u
[../]
[./heatsource]
type = HeatSource
function = 1200
variable = u
[../]
[]
[BCs]
[./ui]
type = NeumannBC
boundary = left
variable = u
value = 100
[../]
[./uo]
type = CoupledConvectiveHeatFluxBC
boundary = right
variable = u
htc = 10.0
T_infinity = 100
[../]
[]
[Materials]
[./property]
type = GenericConstantMaterial
prop_names = 'density specific_heat thermal_conductivity'
prop_values = '1.0 1.0 1.0'
[../]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[./error]
type = ElementL2Error
function = exact
variable = u
[../]
[./h]
type = AverageElementSize
[]
[]
[Outputs]
csv = true
[]
(test/tests/outputs/debug/show_top_residuals_scalar.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./lambda]
order=FIRST
family=SCALAR
[../]
[]
[ScalarKernels]
[./alpha]
type = AlphaCED
variable = lambda
value = 0.123
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[./debug] # This is only test, use [Debug] block to enable this
type = TopResidualDebugOutput
num_residuals = 1
[../]
[]
(test/tests/controls/tag_based_naming_access/param.i)
[Mesh]
type = GeneratedMesh
dim = 2
elem_type = QUAD4
# use odd numbers so points do not fall on element boundaries
nx = 31
ny = 31
[]
[Variables]
[./diffused]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = diffused
[../]
[]
[DiracKernels]
[./test_object]
type = MaterialPointSource
point = '0.5 0.5 0'
variable = diffused
control_tags = 'tag'
[../]
[]
[BCs]
[./bottom_diffused]
type = DirichletBC
variable = diffused
boundary = 'bottom'
value = 2
[../]
[./top_diffused]
type = DirichletBC
variable = diffused
boundary = 'top'
value = 0
[../]
[]
[Materials]
[./mat]
type = GenericConstantMaterial
prop_names = 'matp'
prop_values = '1'
block = 0
[../]
[]
[Postprocessors]
[./test_object]
type = FunctionValuePostprocessor
function = '2*(x+y)'
point = '0.5 0.5 0'
control_tags = 'tag'
[../]
[./other_point_test_object]
type = FunctionValuePostprocessor
function = '3*(x+y)'
point = '0.5 0.5 0'
control_tags = 'tag'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
[Controls]
[./point_control]
type = TestControl
test_type = 'point'
parameter = 'tag/*/point'
execute_on = 'initial'
[../]
[]
(test/tests/materials/discrete/recompute.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 1
[]
[./left_domain]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '0 0 0'
top_right = '0.5 1 0'
block_id = 10
[../]
[]
[Variables]
[./u]
initial_condition = 2
[../]
[]
[Kernels]
[./diff]
type = MatDiffusionTest
variable = u
prop_name = 'p'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 2
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 3
[../]
[]
[Materials]
[./recompute_props]
type = RecomputeMaterial
block = 0
f_name = 'f'
f_prime_name = 'f_prime'
p_name = 'p'
outputs = all
output_properties = 'f f_prime p'
compute = false # make this material "discrete"
[../]
[./newton]
type = NewtonMaterial
block = 0
outputs = all
f_name = 'f'
f_prime_name = 'f_prime'
p_name = 'p'
material = 'recompute_props'
[../]
[./left]
type = GenericConstantMaterial
prop_names = 'f f_prime p'
prop_values = '1 0.5 1.2345'
block = 10
outputs = all
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
print_linear_residuals = true
perf_graph = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/wall_convection/steady-action.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
nx = 16
ny = 16
[]
[]
[Variables]
active = ''
[temperature][]
[]
[Modules]
[IncompressibleNavierStokes]
equation_type = steady-state
velocity_boundary = 'bottom right top left'
velocity_function = '0 0 0 0 lid_function 0 0 0'
initial_velocity = '1e-15 1e-15 0'
add_standard_velocity_variables_for_ad = false
pressure_pinned_node = 0
density_name = rho
dynamic_viscosity_name = mu
use_ad = true
laplace = true
family = LAGRANGE
order = FIRST
add_temperature_equation = true
fixed_temperature_boundary = 'bottom top'
temperature_function = '1 0'
has_ambient_convection = true
ambient_convection_alpha = 1
ambient_temperature = 0.5
supg = true
pspg = true
[]
[]
[Materials]
[const]
type = ADGenericConstantMaterial
prop_names = 'rho mu cp k'
prop_values = '1 1 1 .01'
[]
[]
[Functions]
[lid_function]
# We pick a function that is exactly represented in the velocity
# space so that the Dirichlet conditions are the same regardless
# of the mesh spacing.
type = ParsedFunction
value = '4*x*(1-x)'
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_levels -ksp_gmres_restart'
petsc_options_value = 'asm 6 200'
line_search = 'none'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
exodus = true
[]
(test/tests/geomsearch/penetration_locator/penetration_locator_test.i)
###########################################################
# This is a test of the Geometric Search System. This test
# uses the penetration location object through the
# PenetrationAux Auxilary Kernel to detect overlaps of
# specified interfaces (boundaries) in the domain.
#
# @Requirement F6.50
###########################################################
[Mesh]
file = 2dcontact_collide.e
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./penetration]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
active = 'penetrate'
[./penetrate]
type = PenetrationAux
variable = penetration
boundary = 2
paired_boundary = 3
[../]
[]
[BCs]
active = 'block1_left block1_right block2_left block2_right'
[./block1_left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./block1_right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[./block2_left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./block2_right]
type = DirichletBC
variable = u
boundary = 4
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/misc/check_error/kernel_with_empty_var.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./rea]
type = Reaction
variable = ''
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/heat_conduction/test/tests/meshed_gap_thermal_contact/meshed_annulus_thermal_contact.i)
[Mesh]
[fmesh]
type = FileMeshGenerator
file = meshed_annulus.e
[]
[rename]
type = RenameBlockGenerator
input = fmesh
old_block = '1 2 3'
new_block = '1 4 3'
[]
[]
[Variables]
[./temp]
block = '1 3'
initial_condition = 1.0
[../]
[]
[Kernels]
[./hc]
type = HeatConduction
variable = temp
block = '1 3'
[../]
[./source]
type = HeatSource
variable = temp
block = 3
value = 10.0
[../]
[]
[BCs]
[./outside]
type = DirichletBC
variable = temp
boundary = 1
value = 1.0
[../]
[]
[ThermalContact]
[./gap_conductivity]
type = GapHeatTransfer
variable = temp
primary = 2
secondary = 3
emissivity_primary = 0
emissivity_secondary = 0
gap_conductivity = 0.5
[../]
[]
[Materials]
[./hcm]
type = HeatConductionMaterial
block = '1 3'
temp = temp
thermal_conductivity = 1
[../]
[]
[Problem]
type = FEProblem
kernel_coverage_check = false
material_coverage_check = false
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
[./out]
type = Exodus
[../]
[]
(modules/navier_stokes/test/tests/finite_element/ins/coupled-force/gravity-object.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
nx = 16
ny = 16
[]
[./corner_node]
type = ExtraNodesetGenerator
new_boundary = 'pinned_node'
nodes = '0'
input = gen
[../]
[]
[Variables]
[./velocity]
family = LAGRANGE_VEC
[../]
[./p]
[../]
[u]
family = LAGRANGE_VEC
[]
[]
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[./mass_pspg]
type = INSADMassPSPG
variable = p
[../]
[./momentum_convection]
type = INSADMomentumAdvection
variable = velocity
[../]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
integrate_p_by_parts = true
[../]
[momentum_coupled_force]
type = INSADMomentumCoupledForce
variable = velocity
coupled_vector_var = u
[]
[gravity]
type = INSADGravityForce
variable = velocity
gravity = '0 -9.81 0'
[]
[./momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[../]
[u_diff]
type = VectorDiffusion
variable = u
[]
[]
[BCs]
[./no_slip]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom right left top'
[../]
[./pressure_pin]
type = DirichletBC
variable = p
boundary = 'pinned_node'
value = 0
[../]
[u_left]
type = VectorFunctionDirichletBC
variable = u
boundary = 'left'
function_x = 1
function_y = 1
[]
[u_right]
type = VectorFunctionDirichletBC
variable = u
boundary = 'right'
function_x = -1
function_y = -1
[]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[ins_mat]
type = INSADTauMaterial
velocity = velocity
pressure = p
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_levels -ksp_gmres_restart'
petsc_options_value = 'asm 6 200'
line_search = 'none'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
exodus = true
[]
(test/tests/mesh/nemesis/nemesis_test.i)
###########################################################
# This test exercises the parallel computation aspect of
# the framework. Seperate input mesh files are read on
# different processors and separate output files are
# produced on different processors.
#
# @Requirement P1.10
###########################################################
[Mesh]
file = cylinder/cylinder.e
nemesis = true
# This option lets us exodiff against a gold standard generated
# without repartitioning
skip_partitioning = true
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./aux_elem]
order = CONSTANT
family = MONOMIAL
[../]
[./aux_nodal]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./aux_elem]
type = CoupledAux
variable = aux_elem
operator = '*'
value = 1
coupled = u
[../]
[./aux_nodal]
type = CoupledAux
variable = aux_nodal
operator = '*'
value = 1
coupled = u
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Postprocessors]
[./elem_avg]
type = ElementAverageValue
variable = u
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
file_base = out
nemesis = true
[]
(test/tests/utils/shuffle/shuffle.i)
[Mesh/gen]
type = GeneratedMeshGenerator
dim = 1
[]
[Problem]
solve = 0
[]
[Executioner]
type = Steady
[]
[Reporters/test]
type = TestShuffle
test_type = swap
[]
[Outputs]
[out]
type = JSON
execute_on = FINAL
execute_system_information_on = NONE
[]
[]
(test/tests/meshgenerators/file_mesh_generator/exodus_file_mesh_with_id.i)
[Mesh]
[material_id_mesh]
type = FileMeshGenerator
file = mesh_with_material_id.e
exodus_extra_element_integers = material_id
[]
[]
[AuxVariables]
[material_id]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[set_material_id]
type = ExtraElementIDAux
variable = material_id
extra_id_name = material_id
[]
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/constraints/equal_value_embedded_constraint/embedded_constraint.i)
###########################################################
# This is a test that demonstrates a user-defined
# constraint. It forces variables in overlapping portion of
# two blocks to have the same value
###########################################################
[Mesh]
[]
[Variables]
[phi]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
[diffusion]
type = Diffusion
variable = phi
[]
[]
[BCs]
[top]
type = DirichletBC
variable = phi
boundary = 1
value = 10.0
[]
[bottom]
type = DirichletBC
variable = phi
boundary = 2
value = 0.0
[]
[left]
type = DirichletBC
variable = phi
boundary = 3
value = 10.0
[]
[right]
type = DirichletBC
variable = phi
boundary = 4
value = 0.0
[]
[]
[Constraints]
[equal]
type = EqualValueEmbeddedConstraint
secondary = 2
primary = 1
penalty = 1e3
primary_variable = phi
variable = phi
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
line_search = none
nl_rel_tol = 1e-15
nl_abs_tol = 1e-8
l_max_its = 100
nl_max_its = 10
[]
[Outputs]
exodus = true
print_linear_residuals = false
[]
(test/tests/mortar/continuity-2d-conforming/conforming.i)
[Mesh]
[file]
type = FileMeshGenerator
file = 2blk-conf.e
[]
[secondary]
input = file
type = LowerDBlockFromSidesetGenerator
sidesets = '101'
new_block_id = '10001'
new_block_name = 'secondary_lower'
[]
[primary]
input = secondary
type = LowerDBlockFromSidesetGenerator
sidesets = '100'
new_block_id = '10000'
new_block_name = 'primary_lower'
[]
[]
[Functions]
[./exact_sln]
type = ParsedFunction
value = y
[../]
[./ffn]
type = ParsedFunction
value = 0
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
block = '1 2'
[../]
[./lm]
order = FIRST
family = LAGRANGE
block = 'secondary_lower'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = ffn
[../]
[]
[Constraints]
[./ced]
type = EqualValueConstraint
variable = lm
secondary_variable = u
primary_boundary = 100
primary_subdomain = 10000
secondary_boundary = 101
secondary_subdomain = 10001
[../]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
boundary = '1 2 3 4'
function = exact_sln
[../]
[]
[Postprocessors]
[./l2_error]
type = ElementL2Error
variable = u
function = exact_sln
block = '1 2'
execute_on = 'initial timestep_end'
[../]
[]
[Preconditioning]
[./fmp]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-11
l_tol = 1e-10
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/aux_kernel_with_var.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./v]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./rea]
type = Reaction
variable = u
[../]
[]
[AuxKernels]
[./nope]
type = SelfAux
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
file_base = out
exodus = true
[]
(examples/ex05_amr/ex05.i)
[Mesh]
file = cube-hole.e
[]
# This is where mesh adaptivity magic happens:
[Adaptivity]
marker = errorfrac # this specifies which marker from 'Markers' subsection to use
steps = 2 # run adaptivity 2 times, recomputing solution, indicators, and markers each time
# Use an indicator to compute an error-estimate for each element:
[./Indicators]
# create an indicator computing an error metric for the convected variable
[./error] # arbitrary, use-chosen name
type = GradientJumpIndicator
variable = convected
outputs = none
[../]
[../]
# Create a marker that determines which elements to refine/coarsen based on error estimates
# from an indicator:
[./Markers]
[./errorfrac] # arbitrary, use-chosen name (must match 'marker=...' name above
type = ErrorFractionMarker
indicator = error # use the 'error' indicator specified above
refine = 0.5 # split/refine elements in the upper half of the indicator error range
coarsen = 0 # don't do any coarsening
outputs = none
[../]
[../]
[]
[Variables]
[./convected]
order = FIRST
family = LAGRANGE
[../]
[./diffused]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./example_diff]
type = ExampleCoefDiffusion
variable = convected
coef = 0.125
[../]
[./conv]
type = ExampleConvection
variable = convected
some_variable = diffused
[../]
[./diff]
type = Diffusion
variable = diffused
[../]
[]
[BCs]
# convected=0 on all vertical sides except the right (x-max)
[./cylinder_convected]
type = DirichletBC
variable = convected
boundary = inside
value = 1
[../]
[./exterior_convected]
type = DirichletBC
variable = convected
boundary = 'left top bottom'
value = 0
[../]
[./left_diffused]
type = DirichletBC
variable = diffused
boundary = left
value = 0
[../]
[./right_diffused]
type = DirichletBC
variable = diffused
boundary = right
value = 10
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
l_tol = 1e-3
nl_rel_tol = 1e-12
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(test/tests/preconditioners/vcp/no_condense_test.i)
[Mesh]
[original_file_mesh]
type = FileMeshGenerator
file = non_conform_2blocks.e
[]
[secondary_side]
input = original_file_mesh
type = LowerDBlockFromSidesetGenerator
sidesets = '10'
new_block_id = '100'
new_block_name = 'secondary_side'
[]
[primary_side]
input = secondary_side
type = LowerDBlockFromSidesetGenerator
sidesets = '20'
new_block_id = '200'
new_block_name = 'primary_side'
[]
[]
[Functions]
[exact_sln]
type = ParsedFunction
value = sin(2*pi*x)*sin(2*pi*y)
[]
[ffn]
type = ParsedFunction
value = 8*pi*pi*sin(2*pi*x)*sin(2*pi*y)
[]
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[lm]
order = FIRST
family = LAGRANGE
block = secondary_side
use_dual = false
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[ffn]
type = BodyForce
variable = u
function = ffn
[]
[]
[Constraints]
[ced]
type = EqualValueConstraint
variable = lm
secondary_variable = u
primary_boundary = 20
primary_subdomain = 200
secondary_boundary = 10
secondary_subdomain = 100
[]
[]
[BCs]
[all]
type = DirichletBC
variable = u
boundary = '30 40'
value = 0.0
[]
[neumann]
type = FunctionGradientNeumannBC
exact_solution = exact_sln
variable = u
boundary = '50 60'
[]
[]
[Postprocessors]
[l2_error]
type = ElementL2Error
variable = u
function = exact_sln
block = '1 2'
execute_on = 'initial timestep_end'
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options = '-snes_converged_reason -ksp_converged_reason -snes_view'
petsc_options_iname = '-pc_type -pc_factor_shift_type -pc_factor_shift_amount'
petsc_options_value = ' lu NONZERO 1e-12'
l_max_its = 100
nl_rel_tol = 1e-6
[]
[Outputs]
csv = true
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_mortar/modular_gap_heat_transfer_mortar_displaced_radiation_conduction.i)
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
[file]
type = FileMeshGenerator
file = 2blk-gap.e
[]
[secondary]
type = LowerDBlockFromSidesetGenerator
sidesets = '101'
new_block_id = 10001
new_block_name = 'secondary_lower'
input = file
[]
[primary]
type = LowerDBlockFromSidesetGenerator
sidesets = '100'
new_block_id = 10000
new_block_name = 'primary_lower'
input = secondary
[]
allow_renumbering = false
[]
[Problem]
kernel_coverage_check = false
material_coverage_check = false
[]
[Variables]
[temp]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[disp_x]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[disp_y]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[lm]
order = FIRST
family = LAGRANGE
block = 'secondary_lower'
[]
[]
[Materials]
[left]
type = ADHeatConductionMaterial
block = 1
thermal_conductivity = 0.01
specific_heat = 1
[]
[right]
type = ADHeatConductionMaterial
block = 2
thermal_conductivity = 0.005
specific_heat = 1
[]
[]
[Kernels]
[hc_displaced_block]
type = ADHeatConduction
variable = temp
use_displaced_mesh = true
block = '1'
[]
[hc_undisplaced_block]
type = ADHeatConduction
variable = temp
use_displaced_mesh = false
block = '2'
[]
[disp_x]
type = Diffusion
variable = disp_x
block = '1 2'
[]
[disp_y]
type = Diffusion
variable = disp_y
block = '1 2'
[]
[]
[UserObjects]
[radiation]
type = GapFluxModelRadiation
temperature = temp
boundary = 100
primary_emissivity = 1.0
secondary_emissivity = 1.0
use_displaced_mesh = true
[]
[conduction]
type = GapFluxModelConduction
temperature = temp
boundary = 100
gap_conductivity = 0.02
use_displaced_mesh = true
[]
[]
[Constraints]
[ced]
type = ModularGapConductanceConstraint
variable = lm
secondary_variable = temp
use_displaced_mesh = true
primary_boundary = 100
primary_subdomain = 10000
secondary_boundary = 101
secondary_subdomain = 10001
gap_flux_models = 'radiation conduction'
[]
[]
[BCs]
[left]
type = DirichletBC
variable = temp
boundary = 'left'
value = 100
[]
[right]
type = DirichletBC
variable = temp
boundary = 'right'
value = 0
[]
[left_disp_x]
type = DirichletBC
preset = false
variable = disp_x
boundary = 'left'
value = .1
[]
[right_disp_x]
type = DirichletBC
preset = false
variable = disp_x
boundary = 'right'
value = 0
[]
[bottom_disp_y]
type = DirichletBC
preset = false
variable = disp_y
boundary = 'bottom'
value = 0
[]
[]
[Preconditioning]
[fmp]
type = SMP
full = true
solve_type = 'NEWTON'
[]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-11
nl_abs_tol = 1.0e-10
[]
[VectorPostprocessors]
[NodalTemperature]
type = NodalValueSampler
sort_by = id
boundary = '100 101'
variable = 'temp'
[]
[]
[Outputs]
exodus = false
csv = true
[]
(modules/heat_conduction/test/tests/code_verification/spherical_test_no5.i)
# Problem III.5
#
# A solid sphere has a spatially dependent internal heating. It has a constant thermal
# conductivity. It is exposed to a constant temperature on its boundary.
#
# REFERENCE:
# A. Toptan, et al. (Mar.2020). Tech. rep. CASL-U-2020-1939-000, SAND2020-3887 R. DOI:10.2172/1614683.
[Mesh]
[./geom]
type = GeneratedMeshGenerator
dim = 1
elem_type = EDGE2
nx = 4
[../]
[]
[Variables]
[./u]
order = FIRST
[../]
[]
[Problem]
coord_type = RSPHERICAL
[]
[Functions]
[./volumetric_heat]
type = ParsedFunction
vars = 'q ro beta'
vals = '1200 1 0.1'
value = 'q * (1-beta*(x/ro)^2)'
[../]
[./exact]
type = ParsedFunction
vars = 'uf q k ro beta'
vals = '300 1200 1 1 0.1'
value = 'uf + (q*ro^2/(6*k)) * ( (1-(x/ro)^2) - 0.3*beta*(1-(x/ro)^4) )'
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = u
[../]
[./heatsource]
type = HeatSource
function = volumetric_heat
variable = u
[../]
[]
[BCs]
[./uo]
type = DirichletBC
boundary = 'right'
variable = u
value = 300
[../]
[]
[Materials]
[./property]
type = GenericConstantMaterial
prop_names = 'density specific_heat thermal_conductivity'
prop_values = '1.0 1.0 1.0'
[../]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[./error]
type = ElementL2Error
function = exact
variable = u
[../]
[./h]
type = AverageElementSize
[]
[]
[Outputs]
csv = true
[]
(modules/heat_conduction/test/tests/code_verification/cylindrical_test_no2.i)
# Problem II.2
#
# The thermal conductivity of an infinitely long hollow tube varies
# linearly with temperature. It is exposed on the inner
# and outer surfaces to constant temperatures.
#
# REFERENCE:
# A. Toptan, et al. (Mar.2020). Tech. rep. CASL-U-2020-1939-000, SAND2020-3887 R. DOI:10.2172/1614683.
[Mesh]
[./geom]
type = GeneratedMeshGenerator
dim = 1
elem_type = EDGE2
xmin = 0.2
nx = 4
[../]
[]
[Variables]
[./u]
order = FIRST
[../]
[]
[Problem]
coord_type = RZ
[]
[Functions]
[./exact]
type = ParsedFunction
vars = 'ri ro beta ki ko ui uo'
vals = '0.2 1.0 1e-3 5.3 5 300 0'
value = 'uo+(ko/beta)* ( ( 1 + beta*(ki+ko)*(ui-uo)*( log(x/ro) / log(ri/ro) )/(ko^2))^0.5 -1 )'
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = u
[../]
[]
[BCs]
[./ui]
type = DirichletBC
boundary = left
variable = u
value = 300
[../]
[./uo]
type = DirichletBC
boundary = right
variable = u
value = 0
[../]
[]
[Materials]
[./property]
type = GenericConstantMaterial
prop_names = 'density specific_heat'
prop_values = '1.0 1.0'
[../]
[./thermal_conductivity]
type = ParsedMaterial
f_name = 'thermal_conductivity'
args = u
function = '5 + 1e-3 * (u-0)'
[../]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[./error]
type = ElementL2Error
function = exact
variable = u
[../]
[./h]
type = AverageElementSize
[]
[]
[Outputs]
csv = true
[]
(modules/porous_flow/test/tests/newton_cooling/nc04.i)
# Newton cooling from a bar. Heat conduction
[Mesh]
type = GeneratedMesh
dim = 2
nx = 100
ny = 1
xmin = 0
xmax = 100
ymin = 0
ymax = 1
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'temp'
number_fluid_phases = 0
number_fluid_components = 0
[]
[]
[Variables]
[temp]
[]
[]
[ICs]
[temp]
type = FunctionIC
variable = temp
function = '2-x/100'
[]
[]
[Kernels]
[conduction]
type = PorousFlowHeatConduction
variable = temp
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
temperature = temp
[]
[thermal_conductivity_irrelevant]
type = PorousFlowThermalConductivityIdeal
dry_thermal_conductivity = '1E2 0 0 0 1E2 0 0 0 1E2'
[]
[]
[BCs]
[left]
type = DirichletBC
variable = temp
boundary = left
value = 2
[]
[newton]
type = PorousFlowPiecewiseLinearSink
variable = temp
boundary = right
pt_vals = '0 1 2'
multipliers = '-1 0 1'
flux_function = 1
[]
[]
[VectorPostprocessors]
[temp]
type = LineValueSampler
variable = temp
start_point = '0 0.5 0'
end_point = '100 0.5 0'
sort_by = x
num_points = 11
execute_on = timestep_end
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -snes_max_it -sub_pc_factor_shift_type -pc_asm_overlap -snes_atol -snes_rtol '
petsc_options_value = 'gmres asm lu 100 NONZERO 2 1E-14 1E-12'
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
file_base = nc04
execute_on = timestep_end
exodus = false
[along_line]
type = CSV
execute_vector_postprocessors_on = timestep_end
[]
[]
(modules/misc/test/tests/kernels/thermo_diffusion/thermo_diffusion.i)
# Steady-state test for the ThermoDiffusion kernel.
#
# This test applies a constant temperature gradient to drive thermo-diffusion
# in the variable u. At steady state, the thermo-diffusion is balanced by
# diffusion due to Fick's Law, so the total flux is
#
# J = -D ( grad(u) - ( Qstar u / R ) grad(1/T) )
#
# If there are no fluxes at the boundaries, then there is no background flux and
# these two terms must balance each other everywhere:
#
# grad(u) = ( Qstar u / R ) grad(1/T)
#
# The dx can be eliminated to give
#
# d(ln u) / d(1/T) = Qstar / R
#
# This can be solved to give the profile for u as a function of temperature:
#
# u = A exp( Qstar / R T )
#
# Here, we are using simple heat conduction with Dirichlet boundaries on 0 <= x <= 1
# to give a linear profile for temperature: T = x + 1. We also need to apply one
# boundary condition on u, which is u(x=0) = 1. These conditions give:
#
# u = exp( -(Qstar/R) (x/(x+1)) )
#
# This analytical result is tracked by the aux variable "correct_u".
[Mesh]
type = GeneratedMesh
dim = 1
nx = 100
[]
[Variables]
[./u]
initial_condition = 1
[../]
[./temp]
initial_condition = 1
[../]
[]
[Kernels]
[./soret]
type = ThermoDiffusion
variable = u
temp = temp
gas_constant = 1
[../]
[./diffC]
type = Diffusion
variable = u
[../]
# Heat diffusion gives a linear temperature profile to drive the Soret diffusion.
[./diffT]
type = Diffusion
variable = temp
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
preset = false
boundary = left
value = 1
[../]
[./leftt]
type = DirichletBC
variable = temp
preset = false
boundary = left
value = 1
[../]
[./rightt]
type = DirichletBC
variable = temp
preset = false
boundary = right
value = 2
[../]
[]
[Materials]
[./fake_material]
type = GenericConstantMaterial
block = 0
prop_names = 'mass_diffusivity heat_of_transport'
prop_values = '1 1'
[../]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[./error]
type = NodalL2Error
variable = u
function = 'exp(-x/(x+1))'
[../]
[]
[Outputs]
execute_on = FINAL
exodus = true
[]
(modules/heat_conduction/test/tests/meshed_gap_thermal_contact/meshed_gap_thermal_contact.i)
[Mesh]
[fmesh]
type = FileMeshGenerator
file = meshed_gap.e
[]
[block0]
type = SubdomainBoundingBoxGenerator
input = fmesh
bottom_left = '.5 -.5 0'
top_right = '.7 .5 0'
block_id = 4
[]
[]
[Variables]
[./temp]
block = '1 3'
initial_condition = 1.0
[../]
[]
[Kernels]
[./hc]
type = HeatConduction
variable = temp
block = '1 3'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = temp
boundary = 1
value = 1
[../]
[./right]
type = DirichletBC
variable = temp
boundary = 4
value = 2
[../]
[]
[ThermalContact]
[./gap_conductivity]
type = GapHeatTransfer
variable = temp
primary = 2
secondary = 3
emissivity_primary = 0
emissivity_secondary = 0
gap_conductivity = 0.5
[../]
[]
[Materials]
[./hcm]
type = HeatConductionMaterial
block = '1 3'
temp = temp
thermal_conductivity = 1
[../]
[]
[Problem]
type = FEProblem
kernel_coverage_check = false
material_coverage_check = false
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
[./out]
type = Exodus
[../]
[]
(modules/thermal_hydraulics/test/tests/materials/ad_wall_heat_transfer_coefficient_3eqn_dittus_boelter/test.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
allow_renumbering = false
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = ADDiffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[AuxVariables]
[Hw]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[Hw_ak]
type = ADMaterialRealAux
variable = Hw
property = Hw
[]
[]
[Materials]
[props]
type = ADGenericConstantMaterial
prop_names = 'rho vel k mu cp T T_wall D_h'
prop_values = '1000 0.1 0.001 0.1 12 300 310 0.1'
[]
[Hw_material]
type = ADWallHeatTransferCoefficient3EqnDittusBoelterMaterial
rho = rho
vel = vel
D_h = D_h
k = k
mu = mu
cp = cp
T = T
T_wall = T_wall
[]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[Hw]
type = ElementalVariableValue
elementid = 0
variable = Hw
[]
[]
[Outputs]
csv = true
execute_on = timestep_end
[]
(modules/ray_tracing/test/tests/coord_type/rspherical_line_integral.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
nx = 5
[]
[]
[Variables/u]
[]
[BCs]
[fixed]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Kernels]
[diffusion]
type = Diffusion
variable = u
[]
[source]
type = BodyForce
variable = u
value = 10
[]
[]
[UserObjects]
[study]
type = RepeatableRayStudy
names = 'ray0'
start_points = '0 0 0'
end_points = '1 0 0'
[]
[]
[RayKernels]
[variable_integral]
type = VariableIntegralRayKernel
study = study
variable = u
[]
[]
[Postprocessors]
[value]
type = RayIntegralValue
ray_kernel = variable_integral
ray = ray0
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Problem]
coord_type = RSPHERICAL
[]
[Outputs]
exodus = true
csv = true
[]
(test/tests/vectorpostprocessors/elements_along_line/2d.i)
[Mesh]
type = GeneratedMesh
parallel_type = replicated # Until RayTracing.C is fixed
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[VectorPostprocessors]
[./elems]
type = ElementsAlongLine
start = '0.05 0.05 0'
end = '0.05 0.405 0'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
csv = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/ad-rz-displacements.i)
[GlobalParams]
order = FIRST
integrate_p_by_parts = true
use_displaced_mesh = true
[]
[Mesh]
file = '2d_cone.msh'
displacements = 'disp_x disp_y'
[]
[Problem]
coord_type = RZ
[]
[AuxVariables]
[vel_x][]
[vel_y][]
[disp_x]
order = SECOND
[]
[disp_y]
order = SECOND
[]
[]
[AuxKernels]
[vel_x]
type = VectorVariableComponentAux
variable = vel_x
vector_variable = velocity
component = 'x'
[]
[vel_y]
type = VectorVariableComponentAux
variable = vel_y
vector_variable = velocity
component = 'y'
[]
[]
[Variables]
[velocity]
family = LAGRANGE_VEC
[]
[p]
[]
[]
# Need to set a non-zero initial condition because we have a velocity norm in
# the denominator for the tau coefficient of the stabilization term
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[Kernels]
[mass]
type = INSADMass
variable = p
[]
[mass_pspg]
type = INSADMassPSPG
variable = p
[]
[momentum_advection]
type = INSADMomentumAdvection
variable = velocity
[]
[momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[]
[momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
[]
[momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[]
[]
[BCs]
[inlet]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom'
function_x = 0
function_y = 'inlet_func'
[]
[wall]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'right'
function_x = 0
function_y = 0
[]
[axis]
type = ADVectorFunctionDirichletBC
variable = velocity
boundary = 'left'
set_y_comp = false
function_x = 0
[]
[]
[Functions]
[inlet_func]
type = ParsedFunction
value = '-4 * x^2 + 1'
[]
[]
[Materials]
[const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '1 1'
[]
[ins_mat]
type = INSADTauMaterial
velocity = velocity
pressure = p
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
solve_type = 'NEWTON'
[]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = 'bjacobi ilu 4'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
csv = true
[out]
type = Exodus
hide = 'disp_x disp_y'
[]
[]
[Postprocessors]
[flow_in]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'bottom'
execute_on = 'timestep_end'
[]
[flow_out]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'top'
execute_on = 'timestep_end'
[]
[]
(test/tests/meshgenerators/sidesets_bounding_box_generator/multiple_boundary_ids.i)
[Mesh]
[./gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[./createNewSidesetOne]
type = SideSetsFromBoundingBoxGenerator
input = gmg
boundary_id_old = 'left bottom'
boundary_id_new = 10
bottom_left = '-0.1 -0.1 0'
top_right = '0.2 0.9 0'
block_id = 0
[../]
[./createNewSidesetTwo]
type = SideSetsFromBoundingBoxGenerator
input = createNewSidesetOne
boundary_id_old = 'right'
boundary_id_new = 11
bottom_left = '0.5 0.5 0'
top_right = '1.1 1.1 0'
block_id = 0
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./leftBC]
type = DirichletBC
variable = u
boundary = 10
value = 1
[../]
[./rightBC]
type = DirichletBC
variable = u
boundary = 11
value = 0
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/function_file_test13.i)
# Test for usage of missing function
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = ic_function
[../]
[../]
[]
[Functions]
[./ic_function]
type = PiecewiseLinear
data_file = piecewise_linear_columns_more_data.csv
format = columns
xy_in_file_only = false
x_index_in_file = 3 #Will generate error because data does not contain 4 columns
scale_factor = 1.0
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/indicators/value_jump_indicator/value_jump_indicator_fv.i)
[Mesh]
[mesh]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[]
[Adaptivity]
[Indicators]
[error]
type = ValueJumpIndicator
variable = something
[]
[]
[]
[Variables]
[u]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[]
[ICs]
[leftright]
type = BoundingBoxIC
variable = something
inside = 1
y2 = 1
y1 = 0
x2 = 0.5
x1 = 0
[]
[]
[AuxVariables]
[something]
order = CONSTANT
family = MONOMIAL
[]
[]
[FVKernels]
[diff]
type = FVDiffusion
variable = u
coeff = coeff
[]
[]
[Materials]
[diff]
type = ADGenericFunctorMaterial
prop_names = 'coeff'
prop_values = '1'
[]
[]
[FVBCs]
[left]
type = FVDirichletBC
variable = u
boundary = 'left'
value = 0
[]
[right]
type = FVDirichletBC
variable = u
boundary = 'right'
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
exodus = true
[]
(test/tests/auxkernels/element_aux_var/l2_element_aux_var_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
second_order = true
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./l2_lagrange]
order = FIRST
family = L2_LAGRANGE
[../]
[./l2_hierarchic]
order = FIRST
family = L2_HIERARCHIC
[../]
[./one]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
# Coupling of nonlinear to Aux
[./diff]
type = Diffusion
variable = u
[../]
[./force]
type = CoupledForce
variable = u
v = one
[../]
[]
[AuxKernels]
[./coupled_l2_lagrange]
variable = l2_lagrange
type = CoupledAux
value = 2
operator = +
coupled = u
execute_on = 'initial timestep_end'
[../]
[./coupled_l2_hierarchic]
variable = l2_hierarchic
type = CoupledAux
value = 2
operator = +
coupled = u
execute_on = 'initial timestep_end'
[../]
[./constant]
variable = one
type = ConstantAux
value = 1
execute_on = 'initial timestep_end'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Postprocessors]
[./int2_u]
type = ElementL2Norm
variable = u
execute_on = 'initial timestep_end'
[../]
[./int2_l2_lagrange]
type = ElementL2Norm
variable = l2_lagrange
execute_on = 'initial timestep_end'
[../]
[./int2_l2_hierarchic]
type = ElementL2Norm
variable = l2_hierarchic
execute_on = 'initial timestep_end'
[../]
[./int_u]
type = ElementIntegralVariablePostprocessor
variable = u
execute_on = 'initial timestep_end'
[../]
[./int_l2_lagrange]
type = ElementIntegralVariablePostprocessor
variable = l2_lagrange
execute_on = 'initial timestep_end'
[../]
[./int_l2_hierarchic]
type = ElementIntegralVariablePostprocessor
variable = l2_hierarchic
execute_on = 'initial timestep_end'
[../]
[]
[Outputs]
[./ex_out]
type = Exodus
file_base = l2elemaux
elemental_as_nodal = true
[../]
[]
(test/tests/outputs/format/output_test_gnuplot_gif.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
nz = 0
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[]
[Postprocessors]
[./dofs]
type = NumDOFs
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
[./out]
type = Gnuplot
extension = gif
[../]
[]
(modules/ray_tracing/test/tests/userobjects/repeatable_ray_study/max_distance.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 5
ny = 5
xmax = 5
ymax = 5
[]
[]
# to_right_distance_kill - makes it to the right boundary at (5, 0)
# and dies due to max distance (doesn't call RayBCs)
# to_right_bc_kill - makes it to right boundary at (5, 0); is still
# 0.1 from its max distance so calls 'kill_right' RayBC which
# kills it
# to_top_corner - makes it to the top right corner at (5, 5);
# reflects with direction (-1, -1) and stops once its distance
# hits 7.0
# reflect_a_lot - reflects a bunch with the RayBC 'reflect_all'
# until it gets to a distance of 50 and dies
[UserObjects/study]
type = RepeatableRayStudy
start_points = '0 0 0
0 0 0
0 0 0
0.1 0.2 0'
directions = '1 0 0
1 0 0
1 1 0
1 0.5 0'
max_distances = '5
5.1
7.0
50'
names = 'to_right_distance_kill
to_right_bc_kill
to_top_corner
reflect_a_lot'
[]
[RayKernels/null]
type = NullRayKernel
[]
[RayBCs]
[kill_right]
type = KillRayBC
boundary = right
rays = 'to_right_bc_kill'
[]
[reflect_top_right]
type = ReflectRayBC
boundary = 'top right'
rays = 'to_top_corner'
[]
[reflect_all]
type = ReflectRayBC
boundary = 'top right bottom left'
rays = 'reflect_a_lot'
[]
[]
[Postprocessors/total_distance]
type = RayTracingStudyResult
result = 'total_distance'
study = study
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = false
csv = true
[]
(test/tests/markers/value_range_marker/value_range_marker_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
nz = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Adaptivity]
[./Markers]
[./marker]
type = ValueRangeMarker
lower_bound = 0.3
upper_bound = 0.6
buffer_size = 0.1
variable = u
third_state = DO_NOTHING
[../]
[./inverted_marker]
type = ValueRangeMarker
invert = true
lower_bound = 0.3
upper_bound = 0.6
buffer_size = 0.1
variable = u
third_state = DO_NOTHING
[../]
[../]
[]
[Outputs]
exodus = true
[]
(test/tests/mesh/mesh_generation/annulus.i)
# Generates an Annular Mesh
# Radius of inside circle=1
# Radius of outside circle=5
# Solves the diffusion equation with
# u=0 on inside
# u=log(5) on outside
[Mesh]
type = AnnularMesh
nr = 10
nt = 12
rmin = 1
rmax = 5
growth_r = 1.3
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./inner]
type = DirichletBC
variable = u
value = 0.0
boundary = rmin
[../]
[./outer]
type = FunctionDirichletBC
variable = u
function = log(5)
boundary = rmax
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
[]
[Outputs]
exodus = true
[]
(test/tests/fvkernels/scaling/auto-scaling.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
[]
[Variables]
[u]
family = MONOMIAL
order = CONSTANT
fv = true
[]
[v]
family = MONOMIAL
order = CONSTANT
fv = true
[]
[]
[FVKernels]
[diff_u]
type = FVDiffusion
variable = u
coeff = coeff_u
[]
[diff_v]
type = FVDiffusion
variable = v
coeff = coeff_v
[]
[]
[FVBCs]
[left_u]
type = FVDirichletBC
variable = u
boundary = left
value = 0
[]
[right_u]
type = FVDirichletBC
variable = u
boundary = right
value = 1
[]
[left_v]
type = FVDirichletBC
variable = v
boundary = left
value = 0
[]
[right_v]
type = FVDirichletBC
variable = v
boundary = right
value = 1
[]
[]
[Materials]
[diff]
type = ADGenericFunctorMaterial
prop_names = 'coeff_u coeff_v'
prop_values = '1 1e-20'
[]
[]
[Executioner]
type = Steady
petsc_options = '-pc_svd_monitor'
petsc_options_iname = '-pc_type'
petsc_options_value = 'svd'
automatic_scaling = true
verbose = true
[]
[Outputs]
exodus = true
[]
(test/tests/problems/reference_residual_problem/reference_residual.i)
coef=1
[Mesh]
type = GeneratedMesh
dim = 1
nx = 2
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[u][]
[v][]
[]
[Kernels]
[u_diff]
type = CoefDiffusion
variable = u
coef = ${coef}
[]
[u_rxn]
type = PReaction
variable = u
coefficient = ${coef}
power = 2
[]
[u_f]
type = BodyForce
variable = u
value = ${coef}
[]
[v_diff]
type = Diffusion
variable = v
[]
[v_rxn]
type = PReaction
variable = v
coefficient = 1
power = 2
[]
[v_f]
type = BodyForce
variable = v
value = 1
[]
[]
[BCs]
[u]
type = RobinBC
boundary = 'left right'
coef = ${coef}
variable = u
extra_vector_tags = 'ref'
[]
[v]
type = RobinBC
boundary = 'left right'
coef = 1
variable = v
extra_vector_tags = 'ref'
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/boussinesq/benchmark/benchmark.i)
rayleigh=1e3
hot_temp=${rayleigh}
temp_ref=${fparse hot_temp / 2.}
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 100
ny = 100
[]
[./bottom_left]
type = ExtraNodesetGenerator
new_boundary = corner
coord = '0 0'
input = gen
[../]
[]
[Preconditioning]
[./Newton_SMP]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-12
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_shift_type -ksp_gmres_restart'
petsc_options_value = 'bjacobi lu NONZERO 200'
[]
[Debug]
show_var_residual_norms = true
[]
[Outputs]
[out]
type = Exodus
[]
[]
[Variables]
[velocity]
family = LAGRANGE_VEC
[]
[p][]
[temp]
initial_condition = 340
scaling = 1e-4
[]
[]
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[BCs]
[./velocity_dirichlet]
type = VectorDirichletBC
boundary = 'left right bottom top'
variable = velocity
# The third entry is to satisfy RealVectorValue
values = '0 0 0'
[../]
# Even though we are integrating by parts, because there are no integrated
# boundary conditions on the velocity p doesn't appear in the system of
# equations. Thus we must pin the pressure somewhere in order to ensure a
# unique solution
[./p_zero]
type = DirichletBC
boundary = corner
variable = p
value = 0
[../]
[./hot]
type = DirichletBC
variable = temp
boundary = left
value = ${hot_temp}
[../]
[./cold]
type = DirichletBC
variable = temp
boundary = right
value = 0
[../]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[mass_pspg]
type = INSADMassPSPG
variable = p
[]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[momentum_advection]
type = INSADMomentumAdvection
variable = velocity
[]
[momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
integrate_p_by_parts = true
[]
[./buoyancy]
type = INSADBoussinesqBodyForce
variable = velocity
temperature = temp
gravity = '0 -1 0'
[../]
[./gravity]
type = INSADGravityForce
variable = velocity
gravity = '0 -1 0'
[../]
[supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[]
[temp_advection]
type = INSADEnergyAdvection
variable = temp
[]
[temp_conduction]
type = ADHeatConduction
variable = temp
thermal_conductivity = 'k'
[../]
[temp_supg]
type = INSADEnergySUPG
variable = temp
velocity = velocity
[]
[]
[Materials]
[./ad_const]
type = ADGenericConstantMaterial
# alpha = coefficient of thermal expansion where rho = rho0 -alpha * rho0 * delta T
prop_names = 'mu rho alpha k cp'
prop_values = '1 1 1 1 1'
[../]
[./const]
type = GenericConstantMaterial
prop_names = 'temp_ref'
prop_values = '${temp_ref}'
[../]
[ins_mat]
type = INSADStabilized3Eqn
velocity = velocity
pressure = p
temperature = temp
[]
[]
(modules/fluid_properties/test/tests/stiffened_gas/test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
elem_type = QUAD4
[]
[Functions]
[./f_fn]
type = ParsedFunction
value = -4
[../]
[./bc_fn]
type = ParsedFunction
value = 'x*x+y*y'
[../]
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./e]
initial_condition = 113206.45935406466
[../]
[./v]
initial_condition = 0.0007354064593540647
[../]
[./p]
family = MONOMIAL
order = CONSTANT
[../]
[./T]
family = MONOMIAL
order = CONSTANT
[../]
[./cp]
family = MONOMIAL
order = CONSTANT
[../]
[./cv]
family = MONOMIAL
order = CONSTANT
[../]
[./c]
family = MONOMIAL
order = CONSTANT
[../]
[./mu]
family = MONOMIAL
order = CONSTANT
[../]
[./k]
family = MONOMIAL
order = CONSTANT
[../]
[./g]
family = MONOMIAL
order = CONSTANT
[../]
[]
[AuxKernels]
[./p]
type = MaterialRealAux
variable = p
property = pressure
[../]
[./T]
type = MaterialRealAux
variable = T
property = temperature
[../]
[./cp]
type = MaterialRealAux
variable = cp
property = cp
[../]
[./cv]
type = MaterialRealAux
variable = cv
property = cv
[../]
[./c]
type = MaterialRealAux
variable = c
property = c
[../]
[./mu]
type = MaterialRealAux
variable = mu
property = mu
[../]
[./k]
type = MaterialRealAux
variable = k
property = k
[../]
[./g]
type = MaterialRealAux
variable = g
property = g
[../]
[]
[Modules]
[./FluidProperties]
[./sg]
type = StiffenedGasFluidProperties
gamma = 2.35
q = -1167e3
q_prime = 0
p_inf = 1.e9
cv = 1816
mu = 0.9
k = 0.6
[../]
[]
[]
[Materials]
[./fp_mat]
type = FluidPropertiesMaterial
e = e
v = v
fp = sg
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = f_fn
[../]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
boundary = 'left right top bottom'
function = bc_fn
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(modules/ray_tracing/test/tests/raykernels/variable_integral_ray_kernel/variable_integral_ray_kernel.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 5
ny = 5
xmax = 5
ymax = 5
[]
[]
[Variables/u]
[InitialCondition]
type = FunctionIC
variable = u
function = '(x < 2) * (x + 2 * y) + (x >= 2) * (2 * x + 2 * y - 2)'
[]
[]
[AuxVariables/aux]
order = CONSTANT
family = MONOMIAL
[InitialCondition]
type = FunctionIC
variable = u_ag
function = 'x + y + cos(x)'
[]
[]
[UserObjects]
[study]
type = RepeatableRayStudy
names = 'diag
top_across
bottom_across
partial'
start_points = '0 0 0
0 5 0
0 0 0
0.5 0.5 0'
end_points = '5 5 0
5 5 0
5 0 0
4.5 0.5 0'
[]
[]
[RayKernels]
[variable_integral]
type = VariableIntegralRayKernel
study = study
variable = u
[]
[aux_variable_integral]
type = VariableIntegralRayKernel
study = study
variable = aux
[]
[]
[Postprocessors]
[diag_value]
type = RayIntegralValue
ray_kernel = variable_integral
ray = diag
[]
[top_across_value]
type = RayIntegralValue
ray_kernel = variable_integral
ray = top_across
[]
[bottom_across_value]
type = RayIntegralValue
ray_kernel = variable_integral
ray = bottom_across
[]
[partial_value]
type = RayIntegralValue
ray_kernel = variable_integral
ray = partial
[]
[aux_diag_value]
type = RayIntegralValue
ray_kernel = aux_variable_integral
ray = diag
[]
[aux_top_across_value]
type = RayIntegralValue
ray_kernel = aux_variable_integral
ray = top_across
[]
[aux_bottom_across_value]
type = RayIntegralValue
ray_kernel = aux_variable_integral
ray = bottom_across
[]
[aux_partial_value]
type = RayIntegralValue
ray_kernel = aux_variable_integral
ray = partial
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = false
csv = true
[]
(test/tests/vectorpostprocessors/elements_along_plane/2d.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
# Our CSV diffs here depend on a fixed element id numbering
allow_renumbering = false
parallel_type = replicated
[]
[Problem]
solve = false
[]
[VectorPostprocessors]
[./elems]
type = ElementsAlongPlane
point = '0.525 0.525 0.0'
normal = '1.0 1.0 0.0'
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
[]
(test/tests/mesh_modifiers/add_extra_nodeset/extra_nodeset_test.i)
[Mesh]
[file]
type = FileMeshGenerator
file = square.e
[]
[middle_node]
type = ExtraNodesetGenerator
input = file
new_boundary = 'middle_node'
nodes = '2'
[]
[]
[Variables]
active = 'u'
[u]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
active = 'diff'
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
active = 'left right middle'
[left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[]
[middle]
type = DirichletBC
variable = u
boundary = 'middle_node'
value = -1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/postprocessors/side_pps/side_pps_multi_bnd_test.i)
#
# Tests elemental PPS running on multiple blocks
#
[Mesh]
type = StripeMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 3
ny = 3
elem_type = QUAD4
stripes = 3
# StripeMesh currently only works correctly with ReplicatedMesh.
parallel_type = replicated
[]
[Functions]
[./forcing_fn]
type = ParsedFunction
value = x*(y+1)
[../]
[]
[Variables]
[./u]
family = MONOMIAL
order = CONSTANT
[../]
[]
[Kernels]
[./uv]
type = Reaction
variable = u
[../]
[./fv]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[Postprocessors]
[./int_0_1]
type = SideIntegralVariablePostprocessor
variable = u
boundary = '0 1'
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
execute_on = 'timestep_end'
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[]
(test/tests/materials/piecewise_linear_interpolation_material/piecewise_linear_interpolation_material.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 3
ny = 3
nz = 0
elem_type = QUAD4
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff1]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left_u]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Materials]
[./m1]
type = PiecewiseLinearInterpolationMaterial
property = m1
variable = u
xy_data = '0 0
1 1'
block = 0
outputs = all
[../]
[./m2]
type = PiecewiseLinearInterpolationMaterial
property = m2
variable = u
x = '0 1'
y = '0 1'
block = 0
outputs = all
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/variables/fe_hier/hier-2-2d.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 5
ny = 5
elem_type = QUAD9
[]
[Functions]
[./bc_fnt]
type = ParsedFunction
value = 2*y
[../]
[./bc_fnb]
type = ParsedFunction
value = -2*y
[../]
[./bc_fnl]
type = ParsedFunction
value = -2*x
[../]
[./bc_fnr]
type = ParsedFunction
value = 2*x
[../]
[./forcing_fn]
type = ParsedFunction
value = -4+x*x+y*y
[../]
[./solution]
type = ParsedGradFunction
value = x*x+y*y
grad_x = 2*x
grad_y = 2*y
[../]
[]
[Variables]
[./u]
order = SECOND
family = HIERARCHIC
[../]
[]
[Kernels]
active = 'diff forcing reaction'
[./diff]
type = Diffusion
variable = u
[../]
[./reaction]
type = Reaction
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
[./bc_top]
type = FunctionNeumannBC
variable = u
boundary = 'top'
function = bc_fnt
[../]
[./bc_bottom]
type = FunctionNeumannBC
variable = u
boundary = 'bottom'
function = bc_fnb
[../]
[./bc_left]
type = FunctionNeumannBC
variable = u
boundary = 'left'
function = bc_fnl
[../]
[./bc_right]
type = FunctionNeumannBC
variable = u
boundary = 'right'
function = bc_fnr
[../]
[]
[Postprocessors]
[./dofs]
type = NumDOFs
[../]
[./h]
type = AverageElementSize
[../]
[./L2error]
type = ElementL2Error
variable = u
function = solution
[../]
[./H1error]
type = ElementH1Error
variable = u
function = solution
[../]
[./H1Semierror]
type = ElementH1SemiError
variable = u
function = solution
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
csv = true
[]
(test/tests/scaling/remove-singularity/test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[v][]
[w][]
[]
[Kernels]
[diff_v]
type = ADMatDiffusion
variable = v
diffusivity = 1e-20
[]
[diff_w]
type = MatDiffusion
variable = w
diffusivity = 1e-40
[]
[]
[BCs]
[left_v]
type = DirichletBC
variable = v
boundary = left
value = 0
[]
[right_v]
type = DirichletBC
variable = v
boundary = right
value = 1
[]
[left_w]
type = DirichletBC
variable = w
boundary = left
value = 0
[]
[right_w]
type = DirichletBC
variable = w
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'Newton'
petsc_options = '-pc_svd_monitor'
petsc_options_iname = '-pc_type'
petsc_options_value = 'svd'
automatic_scaling = true
verbose = true
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/cylindrical/2d-rc.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
[]
[]
[Problem]
fv_bcs_integrity_check = true
coord_type = 'RZ'
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[u_forcing]
type = INSFVBodyForce
variable = u
functor = forcing_u
momentum_component = 'x'
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[v_forcing]
type = INSFVBodyForce
variable = v
functor = forcing_v
momentum_component = 'y'
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = u
function = 'exact_u'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = v
function = 'exact_v'
[]
[no-slip-wall-u]
type = INSFVNoSlipWallBC
boundary = 'right'
variable = u
function = 'exact_u'
[]
[no-slip-wall-v]
type = INSFVNoSlipWallBC
boundary = 'right'
variable = v
function = 'exact_v'
[]
[outlet-p]
type = INSFVOutletPressureBC
boundary = 'top'
variable = pressure
function = 'exact_p'
[]
[axis-u]
type = INSFVSymmetryVelocityBC
boundary = 'left'
variable = u
u = u
v = v
mu = ${mu}
momentum_component = x
[]
[axis-v]
type = INSFVSymmetryVelocityBC
boundary = 'left'
variable = v
u = u
v = v
mu = ${mu}
momentum_component = y
[]
[axis-p]
type = INSFVSymmetryPressureBC
boundary = 'left'
variable = pressure
[]
[]
[Functions]
[exact_u]
type = ParsedFunction
value = 'sin(x*pi)^2*sin((1/2)*y*pi)'
[]
[exact_rhou]
type = ParsedFunction
value = 'rho*sin(x*pi)^2*sin((1/2)*y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_u]
type = ADParsedFunction
value = '(1/4)*pi^2*mu*sin(x*pi)^2*sin((1/2)*y*pi) - pi*sin(x*pi)*cos((1/2)*y*pi) + (4*x*pi*rho*sin(x*pi)^3*sin((1/2)*y*pi)^2*cos(x*pi) + rho*sin(x*pi)^4*sin((1/2)*y*pi)^2)/x + (-x*pi*rho*sin(x*pi)^2*sin((1/2)*y*pi)*sin(y*pi)*cos(x*pi) + (1/2)*x*pi*rho*sin(x*pi)^2*cos(x*pi)*cos((1/2)*y*pi)*cos(y*pi))/x - (-2*x*pi^2*mu*sin(x*pi)^2*sin((1/2)*y*pi) + 2*x*pi^2*mu*sin((1/2)*y*pi)*cos(x*pi)^2 + 2*pi*mu*sin(x*pi)*sin((1/2)*y*pi)*cos(x*pi))/x'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_v]
type = ParsedFunction
value = 'cos(x*pi)*cos(y*pi)'
[]
[exact_rhov]
type = ParsedFunction
value = 'rho*cos(x*pi)*cos(y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_v]
type = ADParsedFunction
value = 'pi^2*mu*cos(x*pi)*cos(y*pi) - 2*pi*rho*sin(y*pi)*cos(x*pi)^2*cos(y*pi) - 1/2*pi*sin((1/2)*y*pi)*cos(x*pi) - (-x*pi^2*mu*cos(x*pi)*cos(y*pi) - pi*mu*sin(x*pi)*cos(y*pi))/x + (-x*pi*rho*sin(x*pi)^3*sin((1/2)*y*pi)*cos(y*pi) + 2*x*pi*rho*sin(x*pi)*sin((1/2)*y*pi)*cos(x*pi)^2*cos(y*pi) + rho*sin(x*pi)^2*sin((1/2)*y*pi)*cos(x*pi)*cos(y*pi))/x'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_p]
type = ParsedFunction
value = 'cos(x*pi)*cos((1/2)*y*pi)'
[]
[forcing_p]
type = ParsedFunction
value = '-pi*rho*sin(y*pi)*cos(x*pi) + (2*x*pi*rho*sin(x*pi)*sin((1/2)*y*pi)*cos(x*pi) + rho*sin(x*pi)^2*sin((1/2)*y*pi))/x'
vars = 'rho'
vals = '${rho}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 200 lu NONZERO'
line_search = 'none'
[]
[Outputs]
exodus = true
csv = true
[dof]
type = DOFMap
execute_on = 'initial'
[]
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[./L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2v]
type = ElementL2Error
variable = v
function = exact_v
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2p]
variable = pressure
function = exact_p
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[]
(modules/richards/test/tests/pressure_pulse/pp01.i)
# investigating pressure pulse in 1D with 1 phase
# steadystate
[Mesh]
type = GeneratedMesh
dim = 1
nx = 10
xmin = 0
xmax = 100
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1000
bulk_mod = 2E9
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1E-5
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.0
sum_s_res = 0.0
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 1E3
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
initial_condition = 2E6
[../]
[]
[BCs]
[./left]
type = DirichletBC
boundary = left
value = 3E6
variable = pressure
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[Kernels]
active = 'richardsf'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = SeffVG
pressure_vars = pressure
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-15 0 0 0 1E-15 0 0 0 1E-15'
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGstandard
sat_UO = Saturation
seff_UO = SeffVG
viscosity = 1E-3
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = pp01
exodus = true
[]
(modules/ray_tracing/test/tests/traceray/lots.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 5
ny = 5
nz = 5
xmax = 5
ymax = 5
zmax = 5
[]
[]
[RayBCs]
active = 'kill_2d'
[kill_1d]
type = KillRayBC
boundary = 'left right'
[]
[kill_2d]
type = KillRayBC
boundary = 'top right bottom left'
[]
[kill_3d]
type = KillRayBC
boundary = 'top right bottom left front back'
[]
[]
# Add a dummy RayKernel to enable additional error
# checking before onSegment() is called
[RayKernels/null]
type = NullRayKernel
[]
[UserObjects/lots]
type = LotsOfRaysRayStudy
vertex_to_vertex = false
centroid_to_vertex = false
centroid_to_centroid = false
side_aq = false
centroid_aq = false
compute_expected_distance = true
execute_on = initial
[]
[Postprocessors]
[total_distance]
type = RayTracingStudyResult
study = lots
result = total_distance
[]
[expected_distance]
type = LotsOfRaysExpectedDistance
lots_of_rays_study = lots
[]
[distance_difference]
type = DifferencePostprocessor
value1 = total_distance
value2 = expected_distance
[]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Outputs]
exodus = false
csv = true
[]
(test/tests/kernels/array_kernels/array_diffusion_reaction_dg.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 4
ny = 4
[]
[subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '0.5 0.5 0'
top_right = '1 1 0'
block_id = 1
[]
[]
[Variables]
[u]
order = FIRST
family = L2_LAGRANGE
components = 2
[]
[]
[Kernels]
[diff]
type = ArrayDiffusion
variable = u
diffusion_coefficient = dc
[]
[reaction]
type = ArrayReaction
variable = u
reaction_coefficient = rc
[]
[]
[DGKernels]
[dgdiff]
type = ArrayDGDiffusion
variable = u
diff = dc
[]
[]
[BCs]
[left]
type = ArrayVacuumBC
variable = u
boundary = 1
[]
[right]
type = ArrayPenaltyDirichletBC
variable = u
boundary = 2
value = '1 2'
penalty = 4
[]
[]
[Materials]
[dc0]
type = GenericConstantArray
block = 0
prop_name = dc
prop_value = '1 1'
[]
[dc1]
type = GenericConstantArray
block = 1
prop_name = dc
prop_value = '2 1'
[]
[rc]
type = GenericConstant2DArray
block = '0 1'
prop_name = rc
prop_value = '1 0; -0.1 1'
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Postprocessors]
[intu0]
type = ElementIntegralArrayVariablePostprocessor
variable = u
component = 0
[]
[intu1]
type = ElementIntegralArrayVariablePostprocessor
variable = u
component = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(modules/geochemistry/test/tests/time_dependent_reactions/except5.i)
#Exception: incorrectly sized remove_fixed_activity vectors
[TimeDependentReactionSolver]
model_definition = definition
geochemistry_reactor_name = reactor
charge_balance_species = "Cl-"
constraint_species = "H2O H+ Na+ K+ Ca++ Mg++ Al+++ SiO2(aq) Cl- SO4-- HCO3-"
constraint_value = " 1.0 1E-5 1E-5 1E-5 1E-5 1E-5 1E-5 1E-5 1E-5 1E-5 1E-5"
constraint_meaning = "kg_solvent_water activity bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition"
constraint_unit = "kg dimensionless moles moles moles moles moles moles moles moles moles"
remove_fixed_activity_name = "H+"
remove_fixed_activity_time = "0 1"
[]
[Executioner]
type = Steady
[]
[UserObjects]
[definition]
type = GeochemicalModelDefinition
database_file = "../../../database/moose_geochemdb.json"
basis_species = "H2O H+ Na+ K+ Ca++ Mg++ Al+++ SiO2(aq) Cl- SO4-- HCO3-"
[]
[]
(modules/navier_stokes/test/tests/finite_volume/fvbcs/FVFunctorHeatFluxBC/wall_heat_transfer.i)
flux=10
[GlobalParams]
porosity = 'porosity'
splitting = 'porosity'
locality = 'global'
average_porosity = 'average_eps'
average_k_fluid='average_k_fluid'
average_k_solid='average_k_solid'
average_kappa='average_k_fluid' # because of vector matprop, should be kappa
average_kappa_solid='average_kappa_solid'
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 20
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
[]
[Variables]
[Tf]
type = MooseVariableFVReal
[]
[Ts]
type = MooseVariableFVReal
[]
[]
[AuxVariables]
[k]
type = MooseVariableFVReal
[]
[kappa]
type = MooseVariableFVReal
[]
[k_s]
type = MooseVariableFVReal
[]
[kappa_s]
type = MooseVariableFVReal
[]
[porosity]
type = MooseVariableFVReal
initial_condition = 0.2
[]
[]
[Functions]
[k_function]
type = ADParsedFunction
value = 0.1*(100*y+1)
[]
[kappa_function]
type = ADParsedFunction
value = 0.2*(200*y+1)
[]
[kappa_s_function]
type = ADParsedFunction
value = 0.4*(200*y+1)
[]
[k_s_function]
type = ADParsedFunction
value = 0.2*(200*y+1)+2*x
[]
[]
[FVKernels]
[Tf_diffusion]
type = FVDiffusion
variable = Tf
coeff = 1
[]
[Ts_diffusion]
type = FVDiffusion
variable = Ts
coeff = 1
[]
[]
[FVBCs]
[left_Ts]
type = NSFVFunctorHeatFluxBC
variable = Ts
boundary = 'left'
phase = 'solid'
value = ${flux}
k = 'k_mat'
k_s = 'k_s_mat'
kappa = 'kappa_mat'
kappa_s = 'kappa_s_mat'
[]
[right_Ts]
type = FVDirichletBC
variable = Ts
boundary = 'right'
value = 1000.0
[]
[left_Tf]
type = NSFVFunctorHeatFluxBC
variable = Tf
boundary = 'left'
phase = 'fluid'
value = ${flux}
k = 'k_mat'
k_s = 'k_s_mat'
kappa = 'kappa_mat'
kappa_s = 'kappa_s_mat'
[]
[right_Tf]
type = FVDirichletBC
variable = Tf
boundary = 'right'
value = 1000.0
[]
[]
[AuxKernels]
[k]
type = ADFunctorElementalAux
variable = k
functor = 'k_mat'
[]
[k_s]
type = ADFunctorElementalAux
variable = k_s
functor = 'k_s_mat'
[]
[kappa_s]
type = ADFunctorElementalAux
variable = kappa_s
functor = 'kappa_s_mat'
[]
[]
[Materials]
[thermal_conductivities_k]
type = ADGenericFunctorMaterial
prop_names = 'k_mat'
prop_values = 'k_function'
[]
[thermal_conductivities_k_s]
type = ADGenericFunctorMaterial
prop_names = 'k_s_mat'
prop_values = 'k_s_function'
[]
[thermal_conductivities_kappa]
type = ADGenericVectorFunctorMaterial
prop_names = 'kappa_mat'
prop_values = '0.1 0.2 .03'
[]
[thermal_conductivities_kappa_s]
type = ADGenericFunctorMaterial
prop_names = 'kappa_s_mat'
prop_values = 'kappa_s_function'
[]
[]
[Postprocessors]
[average_eps]
type = ElementAverageValue
variable = porosity
# because porosity is constant in time, we evaluate this only once
execute_on = 'initial'
[]
[average_k_fluid]
type = ElementAverageValue
variable = k
[]
[average_k_solid]
type = ElementAverageValue
variable = k_s
[]
[average_kappa_solid]
type = ElementAverageValue
variable = kappa_s
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
hide = 'porosity average_eps'
[]
(modules/tensor_mechanics/test/tests/torque/torque_small.i)
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
origin = '0 0 2'
direction = '0 0 1'
polar_moment_of_inertia = pmi
factor = t
[]
[Mesh]
[ring]
type = AnnularMeshGenerator
nr = 1
nt = 30
rmin = 0.95
rmax = 1
[]
[extrude]
type = MeshExtruderGenerator
input = ring
extrusion_vector = '0 0 2'
bottom_sideset = 'bottom'
top_sideset = 'top'
num_layers = 5
[]
[]
[AuxVariables]
[alpha_var]
[]
[shear_stress_var]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[alpha]
type = RotationAngle
variable = alpha_var
[]
[shear_stress]
type = ParsedAux
variable = shear_stress_var
args = 'stress_yz stress_xz'
function = 'sqrt(stress_yz^2 + stress_xz^2)'
[]
[]
[BCs]
# fix bottom
[fix_x]
type = DirichletBC
boundary = bottom
variable = disp_x
value = 0
[]
[fix_y]
type = DirichletBC
boundary = bottom
variable = disp_y
value = 0
[]
[fix_z]
type = DirichletBC
boundary = bottom
variable = disp_z
value = 0
[]
# twist top
[twist_x]
type = Torque
boundary = top
variable = disp_x
[]
[twist_y]
type = Torque
boundary = top
variable = disp_y
[]
[twist_z]
type = Torque
boundary = top
variable = disp_z
[]
[]
[Modules/TensorMechanics/Master]
[all]
add_variables = true
strain = SMALL
generate_output = 'vonmises_stress stress_yz stress_xz'
[]
[]
[Postprocessors]
[pmi]
type = PolarMomentOfInertia
boundary = top
# execute_on = 'INITIAL NONLINEAR'
execute_on = 'INITIAL'
[]
[alpha]
type = SideAverageValue
variable = alpha_var
boundary = top
[]
[shear_stress]
type = ElementAverageValue
variable = shear_stress_var
[]
[]
[Materials]
[stress]
type = ComputeLinearElasticStress
[]
[elastic]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 0.3
shear_modulus = 100
[]
[]
[Executioner]
# type = Steady
type = Transient
num_steps = 1
solve_type = PJFNK
petsc_options_iname = '-pctype'
petsc_options_value = 'lu'
nl_max_its = 150
[]
[Outputs]
exodus = true
print_linear_residuals = false
perf_graph = true
[]
(modules/richards/test/tests/darcy/ss.i)
# Test to show that DarcyFlux produces the correct steadystate
[GlobalParams]
variable = pressure
fluid_weight = '0 0 -1E4'
fluid_viscosity = 2
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 2
nz = 3
zmax = 0
zmin = -10
[]
[Variables]
[./pressure]
[./InitialCondition]
type = RandomIC
block = 0
min = 0
max = 1
[../]
[../]
[]
[Kernels]
[./darcy]
type = DarcyFlux
variable = pressure
[../]
[]
[AuxVariables]
[./f_0]
order = CONSTANT
family = MONOMIAL
[../]
[./f_1]
order = CONSTANT
family = MONOMIAL
[../]
[./f_2]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./f_0]
type = DarcyFluxComponent
component = x
variable = f_0
porepressure = pressure
[../]
[./f_1]
type = DarcyFluxComponent
component = y
variable = f_1
porepressure = pressure
[../]
[./f_2]
type = DarcyFluxComponent
component = z
variable = f_2
porepressure = pressure
[../]
[]
[BCs]
[./zmax]
type = DirichletBC
boundary = front
value = 0
variable = pressure
[../]
[]
[Materials]
[./solid]
type = DarcyMaterial
block = 0
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = ss
exodus = true
[]
(modules/combined/test/tests/heat_convection/heat_convection_3d_test.i)
# Test cases for convective boundary conditions.
# Input file for htc_3dtest1
# TKLarson
# 11/02/11
# Revision 0
#
# Goals of this test are:
# 1) show that the 'fluid' temperature for convective boundary condition
# is behaving as expected/desired
# 2) show that expected results ensue from application of convective boundary conditions
# Convective boundary condition:
# q = h*A*(Tw - Tf)
# where
# q - heat transfer rate (w)
# h - heat transfer coefficient (w/m^2-K)
# A - surface area (m^2)
# Tw - surface temperature (K)
# Tf - fluid temperature adjacent to the surface (K)
# The heat transfer coefficient (h) is input as a variable called 'rate'
# Tf is a two valued function specified by 'initial' and 'final' along with a variable
# called 'duration,' the length of time in seconds that it takes initial to linearly ramp
# to 'final.'
# The mesh for this test case is concocted from an ASTM standard for the so-called Brazillian Cylinder test
# (ASTM International, Standard Test Method for Splitting Tensile Strength of Cylindrical Concrete
# Specimens, C 496/C 496M-04, 2004). I turned a cylinder model into a rectangular parallelpiped,
# because I already had the cylinder model.
# The model is 3-d xyz coordinates.
#
# Brazillian Parallelpiped sample dimensions:
# z = 10.3 cm, 0.103 m, (4 in)
# y = 5.08 cm, 0.0508 m, (2 in)
# x = 5.08 cm, 0.0508 m, (2 in)
# Material properties are:
# density = 2405.28 km/m^3
# specific heat = 826.4 J/kg-K
# thermal conductivity 1.937 w/m-K
# alpha (thermal conductivity/(density*specific heat) is then 9.74e-7 m^2/s
#
# Initial parallelpiped temperature is room temperature 294.26 K (70 F)
# The initial fluid temperature is room temperature. We will ramp it to 477.6 K (400 F) in 10 minutes.
# We will use an h representative of natural convection conditions as the boundary condition for all sides
# on the parallelpiped. Akin to putting the object in an oven and turning the oven on.
# This is essentially a thermal soak.
#
# What we expect for this problem:
# 1) Use of h = 284 w/m^2-K (50 BTU/hr-ft^2-F) should cause the parallelpiped to slowly heat up to 477K.
# 2) The fluid temperature should rise from initial (294.26 K) to final (477.6 K) in 600 s.
# 3) 1) and 2) should show the convective BC is working as desired.
#
[Mesh] # Mesh Start
# 5cm x 5cm x 10cm parallelpiped not so detailed mesh, 4 elements each end, 8 elements each long face
# Only one block (Block 1), all concrete
# Sideset definitions:
# 1 - xy plane at z=0,
# 2 - xy plane at z=-0.103,
# 3 - xz plane at y=0,
# 4 - yz plane at x=0,
# 5 - xz plane at y=0.0508,
# 6 - yz plane at x=0.0508
file = heat_convection_3d_mesh.e
#
[] # Mesh END
[Variables] # Variables Start
[./temp]
order = FIRST
family = LAGRANGE
initial_condition = 294.26 # Initial parallelpiped temperature
[../]
[] # Variables END
[Kernels] # Kernels Start
[./heat]
# type = HeatConductionRZ
type = HeatConduction
variable = temp
[../]
[./heat_ie]
# type = HeatConductionTimeDerivativeRZ
type = HeatConductionTimeDerivative
variable = temp
[../]
[] # Kernels END
[BCs] # Boundary Conditions Start
# Heat transfer coefficient on outer parallelpiped radius and ends
[./convective_clad_surface] # Convective Start
# type = ConvectiveFluxRZ # Convective flux, e.g. q'' = h*(Tw - Tf)
type = ConvectiveFluxBC # Convective flux, e.g. q'' = h*(Tw - Tf)
boundary = '1 2 3 4 5 6' # BC applied on top, along length, and bottom
variable = temp
rate = 284. # convective heat transfer coefficient (w/m^2-K)[50 BTU/hr-ft^2-F]
initial = 294.26 # initial ambient (lab or oven) temperature (K)
final = 477.6 # final ambient (lab or oven) temperature (K)
duration = 600. # length of time in seconds that it takes the ambient
# temperature to ramp from initial to final
[../] # Convective End
[] # BCs END
[Materials] # Materials Start
[./thermal]
type = HeatConductionMaterial
block = 1
specific_heat = 826.4
#thermal_conductivity = 1.937 # this makes alpha 9.74e-7 m^2/s
thermal_conductivity = 193.7 # this makes alpha 9.74e-5 m^2/s
# above conductivity arbitrarily increased by 2 decades to make the
# object soak faster for the present purposes
[../]
[./density]
type = Density
block = 1
density = 2405.28
[../]
[] # Materials END
[Executioner] # Executioner Start
type = Transient
# type = Steady
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew '
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type'
petsc_options_value = '70 hypre boomeramg'
l_max_its = 60
nl_rel_tol = 1e-8
nl_abs_tol = 1e-10
l_tol = 1e-5
start_time = 0.0
dt = 60.
num_steps = 20 # Total run time 1200 s
[] # Executioner END
[Outputs] # Output Start
# Output Start
file_base = out_3d
exodus = true
[] # Output END
# # Input file END
(test/tests/kernels/tag_errors/tag_doesnt_exist/bad_tag.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/transfers/multiapp_high_order_variable_transfer/sub_L2_Lagrange_conservative.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
xmax = 0.5
ymax = 0.5
[]
[AuxVariables]
[./power_density]
family = L2_LAGRANGE
order = FIRST
[../]
[]
[Variables]
[./temp]
[../]
[]
[Kernels]
[./heat_conduction]
type = Diffusion
variable = temp
[../]
[./heat_source_fuel]
type = CoupledForce
variable = temp
v = power_density
[../]
[]
[BCs]
[bc]
type = DirichletBC
variable = temp
boundary = '0 1 2 3'
value = 450
[]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart '
petsc_options_value = 'hypre boomeramg 100'
nl_abs_tol = 1e-7
nl_rel_tol = 1e-7
[]
[Postprocessors]
[./temp_fuel_avg]
type = ElementAverageValue
variable = temp
[../]
[./pwr_density]
type = ElementIntegralVariablePostprocessor
block = '0'
variable = power_density
execute_on = 'transfer'
[../]
[]
[Outputs]
perf_graph = true
exodus = true
color = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/energy_source/steady-var.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
nx = 16
ny = 16
[]
[./corner_node]
type = ExtraNodesetGenerator
new_boundary = 'pinned_node'
nodes = '0'
input = gen
[../]
[]
[AuxVariables]
[u]
initial_condition = 1
[]
[]
[Variables]
[./velocity]
family = LAGRANGE_VEC
[../]
[./p]
[../]
[temperature][]
[]
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[./mass_pspg]
type = INSADMassPSPG
variable = p
[../]
[./momentum_convection]
type = INSADMomentumAdvection
variable = velocity
[../]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
integrate_p_by_parts = true
[../]
[./momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[../]
[./temperature_advection]
type = INSADEnergyAdvection
variable = temperature
[../]
[./temperature_conduction]
type = ADHeatConduction
variable = temperature
thermal_conductivity = 'k'
[../]
[temperature_source]
type = INSADEnergySource
variable = temperature
source_variable = u
[]
[temperature_supg]
type = INSADEnergySUPG
variable = temperature
velocity = velocity
[]
[]
[BCs]
[./no_slip]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom right left'
[../]
[./lid]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'top'
function_x = 'lid_function'
[../]
[./pressure_pin]
type = DirichletBC
variable = p
boundary = 'pinned_node'
value = 0
[../]
[./temperature_hot]
type = DirichletBC
variable = temperature
boundary = 'bottom'
value = 1
[../]
[./temperature_cold]
type = DirichletBC
variable = temperature
boundary = 'top'
value = 0
[../]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu cp k'
prop_values = '1 1 1 .01'
[../]
[ins_mat]
type = INSADStabilized3Eqn
velocity = velocity
pressure = p
temperature = temperature
[]
[]
[Functions]
[./lid_function]
# We pick a function that is exactly represented in the velocity
# space so that the Dirichlet conditions are the same regardless
# of the mesh spacing.
type = ParsedFunction
value = '4*x*(1-x)'
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_levels -ksp_gmres_restart'
petsc_options_value = 'asm 6 200'
line_search = 'none'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
[out]
type = Exodus
hide = 'u'
[]
[]
(tutorials/darcy_thermo_mech/step06_coupled_darcy_heat_conduction/tests/materials/packed_column/packed_column.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 100
ny = 10
xmax = 0.304 # Length of test chamber
ymax = 0.0257 # Test chamber radius
[]
[Variables]
[pressure]
[]
[]
[Kernels]
[darcy_pressure]
type = DarcyPressure
variable = pressure
[]
[]
[BCs]
[inlet]
type = DirichletBC
variable = pressure
boundary = left
value = 4000 # (Pa) From Figure 2 from paper. First dot for 1mm spheres.
[]
[outlet]
type = DirichletBC
variable = pressure
boundary = right
value = 0 # (Pa) Gives the correct pressure drop from Figure 2 for 1mm spheres
[]
[]
[Materials]
[column]
type = PackedColumn
temperature = 303
[]
[]
[Problem]
type = FEProblem
coord_type = RZ
rz_coord_axis = X
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/postprocessors/element_l2_error_pps/element_l2_error_pp_test.i)
###########################################################
# This is a simple test of the Postprocessor System. This
# test uses a forcing function and the MMS to verify
# correctness of the implementation.
# Grid adaptivity is applied at successively finer grids
# to verify the correct slope of the measure of error
# against the analytical solution.
#
# @Requirement F6.10
###########################################################
[Mesh]
type = GeneratedMesh
dim = 2
nx = 3
ny = 3
xmin = 0
xmax = 2
ymin = 0
ymax = 2
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
active = 'forcing_func u_func'
[./forcing_func]
type = ParsedFunction
value = alpha*alpha*pi*pi*sin(alpha*pi*x)
vars = 'alpha'
vals = '4'
[../]
[./u_func]
type = ParsedFunction
value = sin(alpha*pi*x)
vars = 'alpha'
vals = '4'
[../]
[]
[Kernels]
active = 'diff forcing'
[./diff]
type = Diffusion
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_func
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = '1'
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = '3'
value = 0
[../]
[]
[Executioner]
type = Steady
[./Adaptivity]
refine_fraction = 1.0
coarsen_fraction = 0.0
max_h_level = 10
steps = 4
[../]
[]
# Postprocessor System
[Postprocessors]
[./integral]
type = ElementL2Error
variable = u
function = u_func
execute_on = 'initial timestep_end'
[../]
[]
[Outputs]
file_base = out
exodus = false
csv = true
[]
(modules/fluid_properties/test/tests/water/water.i)
# Example of using Water97FluidProperties module in Region 1 by recovering the values
# in Table 5 of Revised Release on the IAPWS Industrial Formulation 1997 for the
# Thermodynamic Properties of Water and Steam
[Mesh]
type = GeneratedMesh
dim = 2
nx = 3
xmax = 3
# This test uses ElementalVariableValue postprocessors on specific
# elements, so element numbering needs to stay unchanged
allow_renumbering = false
[]
[Variables]
[./dummy]
[../]
[]
[AuxVariables]
[./pressure]
order = CONSTANT
family = MONOMIAL
[../]
[./temperature]
order = CONSTANT
family = MONOMIAL
[../]
[./rho]
family = MONOMIAL
order = CONSTANT
[../]
[./v]
family = MONOMIAL
order = CONSTANT
[../]
[./e]
family = MONOMIAL
order = CONSTANT
[../]
[./h]
family = MONOMIAL
order = CONSTANT
[../]
[./s]
family = MONOMIAL
order = CONSTANT
[../]
[./cp]
family = MONOMIAL
order = CONSTANT
[../]
[./cv]
family = MONOMIAL
order = CONSTANT
[../]
[./c]
family = MONOMIAL
order = CONSTANT
[../]
[./mu]
family = MONOMIAL
order = CONSTANT
[../]
[./k]
family = MONOMIAL
order = CONSTANT
[../]
[]
[Functions]
[./tic]
type = ParsedFunction
value = 'if(x<2, 300, 500)'
[../]
[./pic]
type = ParsedFunction
value = 'if(x<1,3e6, if(x<2, 80e6, 3e6))'
[../]
[]
[ICs]
[./p_ic]
type = FunctionIC
function = pic
variable = pressure
[../]
[./t_ic]
type = FunctionIC
function = tic
variable = temperature
[../]
[]
[AuxKernels]
[./rho]
type = MaterialRealAux
variable = rho
property = density
[../]
[./v]
type = ParsedAux
args = rho
function = 1/rho
variable = v
[../]
[./e]
type = MaterialRealAux
variable = e
property = e
[../]
[./h]
type = MaterialRealAux
variable = h
property = h
[../]
[./s]
type = MaterialRealAux
variable = s
property = s
[../]
[./cp]
type = MaterialRealAux
variable = cp
property = cp
[../]
[./cv]
type = MaterialRealAux
variable = cv
property = cv
[../]
[./c]
type = MaterialRealAux
variable = c
property = c
[../]
[./mu]
type = MaterialRealAux
variable = mu
property = viscosity
[../]
[./k]
type = MaterialRealAux
variable = k
property = k
[../]
[]
[Modules]
[./FluidProperties]
[./water]
type = Water97FluidProperties
[../]
[../]
[]
[Materials]
[./fp_mat]
type = FluidPropertiesMaterialPT
pressure = pressure
temperature = temperature
fp = water
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = dummy
[../]
[]
[Postprocessors]
[./density0]
type = ElementalVariableValue
variable = rho
elementid = 0
[../]
[./density1]
type = ElementalVariableValue
variable = rho
elementid = 1
[../]
[./density2]
type = ElementalVariableValue
variable = rho
elementid = 2
[../]
[./v0]
type = ElementalVariableValue
variable = v
elementid = 0
[../]
[./v1]
type = ElementalVariableValue
variable = v
elementid = 1
[../]
[./v2]
type = ElementalVariableValue
variable = v
elementid = 2
[../]
[./e0]
type = ElementalVariableValue
variable = e
elementid = 0
[../]
[./e1]
type = ElementalVariableValue
variable = e
elementid = 1
[../]
[./e2]
type = ElementalVariableValue
variable = e
elementid = 2
[../]
[./h0]
type = ElementalVariableValue
variable = h
elementid = 0
[../]
[./h1]
type = ElementalVariableValue
variable = h
elementid = 1
[../]
[./h2]
type = ElementalVariableValue
variable = h
elementid = 2
[../]
[./s0]
type = ElementalVariableValue
variable = s
elementid = 0
[../]
[./s1]
type = ElementalVariableValue
variable = s
elementid = 1
[../]
[./s2]
type = ElementalVariableValue
variable = s
elementid = 2
[../]
[./cp0]
type = ElementalVariableValue
variable = cp
elementid = 0
[../]
[./cp1]
type = ElementalVariableValue
variable = cp
elementid = 1
[../]
[./cp2]
type = ElementalVariableValue
variable = cp
elementid = 2
[../]
[./cv0]
type = ElementalVariableValue
variable = cv
elementid = 0
[../]
[./cv1]
type = ElementalVariableValue
variable = cv
elementid = 1
[../]
[./cv2]
type = ElementalVariableValue
variable = cv
elementid = 2
[../]
[./c0]
type = ElementalVariableValue
variable = c
elementid = 0
[../]
[./c1]
type = ElementalVariableValue
variable = c
elementid = 1
[../]
[./c2]
type = ElementalVariableValue
variable = c
elementid = 2
[../]
[./mu0]
type = ElementalVariableValue
variable = mu
elementid = 0
[../]
[./mu1]
type = ElementalVariableValue
variable = mu
elementid = 1
[../]
[./mu2]
type = ElementalVariableValue
variable = mu
elementid = 2
[../]
[./k0]
type = ElementalVariableValue
variable = k
elementid = 0
[../]
[./k1]
type = ElementalVariableValue
variable = k
elementid = 1
[../]
[./k2]
type = ElementalVariableValue
variable = k
elementid = 2
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
csv = true
[]
(test/tests/materials/derivative_material_interface/multiblock.i)
[Mesh]
type = FileMesh
file = rectangle.e
[]
[Variables]
[./c]
[../]
[]
[Materials]
[./mat1]
type = DefaultMatPropConsumerMaterial
block = 1
[../]
[./mat2]
type = DefaultMatPropConsumerMaterial
block = 2
[../]
[./mat1b]
type = DefaultMatPropConsumerMaterial
mat_prop = prop2
block = 1
[../]
[./mat2b]
type = DefaultMatPropConsumerMaterial
mat_prop = prop2
block = 2
[../]
[./generic]
type = GenericConstantMaterial
block = '1 2'
prop_names = prop3
prop_values = 9
[../]
[./mat1c]
type = DefaultMatPropConsumerMaterial
mat_prop = prop3
block = 1
[../]
[./mat2c]
type = DefaultMatPropConsumerMaterial
mat_prop = prop3
block = 2
[../]
[]
[Kernels]
[./kern1]
type = DefaultMatPropConsumerKernel
variable = c
block = 1
[../]
[./kern2]
type = DefaultMatPropConsumerKernel
variable = c
block = 2
[../]
[./kern1b]
type = DefaultMatPropConsumerKernel
variable = c
mat_prop = prop3
block = 1
[../]
[./kern2b]
type = DefaultMatPropConsumerKernel
variable = c
mat_prop = prop3
block = 2
[../]
[]
[Executioner]
type = Steady
[]
[Debug]
show_material_props = true
[]
[Problem]
solve = false
[]
[Outputs]
exodus = true
[]
(test/tests/bcs/function_dirichlet_bc/test.i)
###########################################################
# This is a test of Boundary Condition System. The
# FunctionDirichletBC is used to contribute the residuals
# to the boundary term operators in the weak form.
#
# @Requirement F3.40
###########################################################
[Mesh]
[./square]
type = GeneratedMeshGenerator
dim = 2
nx = 32
ny = 32
[../]
[]
[Variables]
[./u]
[../]
[]
[Functions]
[./ff_1]
type = ParsedFunction
value = alpha*alpha*pi
vars = 'alpha'
vals = '16'
[../]
[./ff_2]
type = ParsedFunction
value = pi*sin(alpha*pi*x)
vars = 'alpha'
vals = '16'
[../]
[./forcing_func]
type = CompositeFunction
functions = 'ff_1 ff_2'
[../]
[./bc_func]
type = ParsedFunction
value = sin(alpha*pi*x)
vars = 'alpha'
vals = '16'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_func
[../]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
boundary = 'left right'
function = bc_func
[../]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-12
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(test/tests/misc/check_error/dg_kernel_with_aux_var.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./v]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./rea]
type = Reaction
variable = u
[../]
[]
[DGKernels]
[./nope]
type = DGDiffusion
variable = v
epsilon = -1
sigma = 6
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/fluid_properties/test/tests/ics/specific_enthalpy_from_pressure_temperature/test.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
allow_renumbering = false
[]
[Modules]
[FluidProperties]
[fp_steam]
type = StiffenedGasFluidProperties
gamma = 1.43
cv = 1040.0
q = 2.03e6
p_inf = 0.0
q_prime = -2.3e4
k = 0.026
mu = 134.4e-7
M = 0.01801488
rho_c = 322.0
[]
[]
[]
[AuxVariables]
[h]
[]
[p]
[]
[T]
[]
[]
[ICs]
[h_ic]
type = SpecificEnthalpyFromPressureTemperatureIC
variable = h
p = p
T = T
fp = fp_steam
[]
[p_ic]
type = ConstantIC
variable = p
value = 100e3
[]
[T_ic]
type = ConstantIC
variable = T
value = 500
[]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[h_test]
type = ElementalVariableValue
elementid = 0
variable = h
execute_on = 'INITIAL TIMESTEP_END'
[]
[]
[Outputs]
csv = true
execute_on = 'INITIAL'
[]
[Problem]
solve = false
[]
(test/tests/restart/scalar-var/part2.i)
[Mesh]
[fmg]
type = FileMeshGenerator
file = part1_out.e
use_for_exodus_restart = true
[]
[]
[Variables]
[v]
family = MONOMIAL
order = CONSTANT
fv = true
initial_from_file_var = v
[]
[lambda]
family = SCALAR
order = FIRST
initial_from_file_var = lambda
[]
[]
[FVKernels]
[advection]
type = FVElementalAdvection
variable = v
velocity = '1 0 0'
[]
[lambda]
type = FVScalarLagrangeMultiplier
variable = v
lambda = lambda
phi0 = 1
[]
[]
[Executioner]
type = Steady
petsc_options_iname = '-snes_max_it'
petsc_options_value = '0'
nl_abs_tol = 1e-10
[]
[Outputs]
[out]
type = Exodus
execute_on = 'final'
[]
[]
(modules/navier_stokes/test/tests/finite_element/ins/scalar_adr/supg/2d_advection_error_testing.i)
ax=1
ay=1
[GlobalParams]
u = ${ax}
v = ${ay}
pressure = 0
tau_type = mod
transient_term = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
xmax = 1
ymax = 1
elem_type = QUAD9
[]
[Variables]
[./c]
family = LAGRANGE
order = SECOND
[../]
[]
[Kernels]
[./adv]
type = Advection
variable = c
forcing_func = 'ffn'
[../]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = c
boundary = 'left right top bottom'
function = 'c_func'
[../]
[]
[Materials]
[./mat]
type = GenericConstantMaterial
prop_names = 'mu rho'
prop_values = '0 1'
[../]
[]
[Functions]
[./ffn]
type = ParsedFunction
value = '${ax}*(0.14*pi*y*cos(0.2*pi*x*y) + 0.2*pi*cos(0.5*pi*x)) + ${ay}*(0.14*pi*x*cos(0.2*pi*x*y) + 0.4*pi*cos(pi*y))'
[../]
[./c_func]
type = ParsedFunction
value = '0.4*sin(0.5*pi*x) + 0.4*sin(pi*y) + 0.7*sin(0.2*pi*x*y) + 0.5'
[../]
[./cx_func]
type = ParsedFunction
value = '0.14*pi*y*cos(0.2*pi*x*y) + 0.2*pi*cos(0.5*pi*x)'
[../]
[]
# [Executioner]
# type = Steady
# petsc_options_iname = '-pc_type -pc_factor_shift_type'
# petsc_options_value = 'lu NONZERO'
# []
[Executioner]
type = Transient
num_steps = 10
petsc_options = '-snes_converged_reason -ksp_converged_reason -snes_view'
petsc_options_iname = '-pc_type -pc_factor_shift_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu NONZERO superlu_dist'
line_search = 'none'
nl_rel_tol = 1e-8
nl_abs_tol = 1e-12
nl_max_its = 10
l_tol = 1e-6
l_max_its = 10
[./TimeStepper]
dt = .05
type = IterationAdaptiveDT
cutback_factor = 0.4
growth_factor = 1.2
optimal_iterations = 20
[../]
[]
[Outputs]
[./exodus]
type = Exodus
[../]
[./csv]
type = CSV
[../]
[]
[Postprocessors]
[./L2c]
type = ElementL2Error
variable = c
function = c_func
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2cx]
type = ElementL2Error
variable = cx
function = cx_func
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[]
[AuxVariables]
[./cx]
family = MONOMIAL
order = FIRST
[../]
[]
[AuxKernels]
[./cx_aux]
type = VariableGradientComponent
component = x
variable = cx
gradient_variable = c
[../]
[]
(test/tests/restrictable/check_error/check_error.i)
[Mesh]
type = FileMesh
file = rectangle.e
dim = 2
[]
[Variables]
[./u]
block = '1 2'
[../]
[]
[Kernels]
[./diff]
type = BlkResTestDiffusion
variable = u
block = '1 2'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Materials]
[./mat0]
type = GenericConstantMaterial
block = '1'
prop_names = 'a b'
prop_values = '1 2'
[../]
[./mat1]
type = GenericConstantMaterial
block = '2'
prop_names = 'a'
prop_values = '10'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/postprocessors/linear_combination/linear_combination.i)
# Tests the LinearCombinationPostprocessor post-processor, which computes
# a linear combination of an arbitrary number of post-processor values.
[Mesh]
type = GeneratedMesh
dim = 1
nx = 2
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[./pp1]
# number of elements, equal to 2
type = NumElems
[../]
[./pp2]
# number of nodes, equal to 3
type = NumNodes
[../]
# post-processor value being tested; value should be the following:
# value = c1 * pp1 + c2 * pp2 + b
# = 2 * 2 + -1 * 3 + 5 = 6
[./linear_combination]
type = LinearCombinationPostprocessor
pp_names = 'pp1 pp2'
pp_coefs = '2 -1'
b = 5
[../]
[]
[Outputs]
show = linear_combination
csv = true
[]
(test/tests/materials/discrete/recompute_block_error.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 1
[]
[./left_domain]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '0 0 0'
top_right = '0.5 1 0'
block_id = 10
[../]
[]
[Variables]
[./u]
initial_condition = 2
[../]
[]
[Kernels]
[./diff]
type = MatDiffusionTest
variable = u
prop_name = 'p'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 2
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 3
[../]
[]
[Materials]
[./recompute_props]
type = RecomputeMaterial
block = 0
f_name = 'f'
f_prime_name = 'f_prime'
p_name = 'p'
outputs = all
output_properties = 'f f_prime p'
compute = false # makes this material "discrete"
[../]
[./newton]
type = NewtonMaterial
block = '0 10'
outputs = all
f_name = 'f'
f_prime_name = 'f_prime'
p_name = 'p'
material = 'recompute_props'
[../]
[./left]
type = GenericConstantMaterial
prop_names = 'f f_prime'
prop_values = '1 0.5 '
block = 10
outputs = all
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
print_linear_residuals = true
perf_graph = true
[]
(modules/porous_flow/test/tests/relperm/brooks_corey2.i)
# Test Brooks-Corey relative permeability curve by varying saturation over the mesh
# Exponent lambda = 2 for both phases
# Residual saturation of phase 0: s0r = 0.2
# Residual saturation of phase 1: s1r = 0.3
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Variables]
[p0]
initial_condition = 1e6
[]
[s1]
[]
[]
[AuxVariables]
[s0aux]
family = MONOMIAL
order = CONSTANT
[]
[s1aux]
family = MONOMIAL
order = CONSTANT
[]
[kr0aux]
family = MONOMIAL
order = CONSTANT
[]
[kr1aux]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[s0]
type = PorousFlowPropertyAux
property = saturation
phase = 0
variable = s0aux
[]
[s1]
type = PorousFlowPropertyAux
property = saturation
phase = 1
variable = s1aux
[]
[kr0]
type = PorousFlowPropertyAux
property = relperm
phase = 0
variable = kr0aux
[]
[kr1]
type = PorousFlowPropertyAux
property = relperm
phase = 1
variable = kr1aux
[]
[]
[Functions]
[s1]
type = ParsedFunction
value = x
[]
[]
[ICs]
[s1]
type = FunctionIC
variable = s1
function = s1
[]
[]
[Kernels]
[p0]
type = Diffusion
variable = p0
[]
[s1]
type = Diffusion
variable = s1
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'p0 s1'
number_fluid_phases = 2
number_fluid_components = 2
[]
[pc]
type = PorousFlowCapillaryPressureConst
pc = 0
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow2PhasePS
phase0_porepressure = p0
phase1_saturation = s1
capillary_pressure = pc
[]
[kr0]
type = PorousFlowRelativePermeabilityBC
phase = 0
lambda = 2
s_res = 0.2
sum_s_res = 0.5
[]
[kr1]
type = PorousFlowRelativePermeabilityBC
phase = 1
lambda = 2
nw_phase = true
s_res = 0.3
sum_s_res = 0.5
[]
[]
[VectorPostprocessors]
[vpp]
type = LineValueSampler
warn_discontinuous_face_values = false
variable = 's0aux s1aux kr0aux kr1aux'
start_point = '0 0 0'
end_point = '1 0 0'
num_points = 20
sort_by = id
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
nl_abs_tol = 1e-8
[]
[BCs]
[sleft]
type = DirichletBC
variable = s1
value = 0
boundary = left
[]
[sright]
type = DirichletBC
variable = s1
value = 1
boundary = right
[]
[]
[Outputs]
csv = true
execute_on = timestep_end
[]
(test/tests/outputs/xml/xml.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[VectorPostprocessors]
[const]
type = ConstantVectorPostprocessor
value = '1 2 3 4 5'
[]
[distributed]
type = TestDistributedVectorPostprocessor
parallel_type = replicated
[]
[]
[Outputs]
xml = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/boussinesq/boussinesq-action.i)
mu = 1
rho = 1
k = 1
cp = 1
alpha = 1
rayleigh=1e3
hot_temp=${rayleigh}
temp_ref=${fparse hot_temp / 2.}
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 32
ny = 32
[]
[]
[Modules]
[NavierStokesFV]
compressibility = 'incompressible'
porous_medium_treatment = false
add_energy_equation = true
boussinesq_approximation = true
density = ${rho}
dynamic_viscosity = ${mu}
thermal_conductivity = ${k}
specific_heat = ${cp}
thermal_expansion = ${alpha}
gravity = '0 -1 0'
ref_temperature = ${temp_ref}
initial_pressure = 0.0
initial_temperature = 0.0
inlet_boundaries = 'top'
momentum_inlet_types = 'fixed-velocity'
momentum_inlet_function = 'lid_function 0'
energy_inlet_types = 'heatflux'
energy_inlet_function = '0'
wall_boundaries = 'left right bottom'
momentum_wall_types = 'noslip noslip noslip'
energy_wall_types = 'fixed-temperature fixed-temperature heatflux'
energy_wall_function = '${hot_temp} 0 0'
pin_pressure = true
pinned_pressure_type = average
pinned_pressure_value = 0
momentum_advection_interpolation = 'upwind'
mass_advection_interpolation = 'upwind'
energy_advection_interpolation = 'upwind'
energy_scaling = 1e-4
[]
[]
[Functions]
[lid_function]
type = ParsedFunction
value = '4*x*(1-x)'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 300 lu NONZERO'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(modules/stochastic_tools/test/tests/surrogates/gaussian_process/sub.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 100
xmax = 1
elem_type = EDGE3
[]
[Variables]
[T]
order = SECOND
family = LAGRANGE
[]
[]
[Kernels]
[diffusion]
type = MatDiffusion
variable = T
diffusivity = k
[]
[source]
type = BodyForce
variable = T
value = 1.0
[]
[]
[Materials]
[conductivity]
type = GenericConstantMaterial
prop_names = k
prop_values = 2.0
[]
[]
[BCs]
[right]
type = DirichletBC
variable = T
boundary = right
value = 300
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Postprocessors]
[avg]
type = AverageNodalVariableValue
variable = T
[]
[]
[Outputs]
[]
(modules/phase_field/test/tests/KKS_system/derivative_parsed_material.i)
#
# This test validates the free energy material with automatic differentiation for the KKS system
#
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
nz = 0
xmin = 0
xmax = 1
ymin = 0
ymax = 1
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[BCs]
[./left]
type = DirichletBC
variable = c1
boundary = 'left'
value = 0
[../]
[./right]
type = DirichletBC
variable = c1
boundary = 'right'
value = 1
[../]
[./top]
type = DirichletBC
variable = c2
boundary = 'top'
value = 0
[../]
[./bottom]
type = DirichletBC
variable = c2
boundary = 'bottom'
value = 1
[../]
[]
[Variables]
# concentration 1
[./c1]
order = FIRST
family = LAGRANGE
[../]
# concentration 2
[./c2]
order = FIRST
family = LAGRANGE
[../]
[]
[Materials]
[./fa]
type = DerivativeParsedMaterial
f_name = F
args = 'c1 c2'
constant_names = 'T kB'
constant_expressions = '400 .000086173324'
function = 'c1^2+100*T*kB*(c2-0.5)^3+c1^4*c2^5'
outputs = exodus
[../]
[]
[Kernels]
[./c1diff]
type = Diffusion
variable = c1
[../]
[./c2diff]
type = Diffusion
variable = c2
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
file_base = derivative_parsed_material
exodus = true
[]
(test/tests/fviks/one-var-diffusion/test.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 10
xmax = 2
[]
[subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '1.0 0 0'
block_id = 1
top_right = '2.0 1.0 0'
[]
[interface_primary_side]
input = subdomain1
type = SideSetsBetweenSubdomainsGenerator
primary_block = '0'
paired_block = '1'
new_boundary = 'primary_interface'
[]
[interface_secondary_side]
input = interface_primary_side
type = SideSetsBetweenSubdomainsGenerator
primary_block = '1'
paired_block = '0'
new_boundary = 'secondary_interface'
[]
[]
[Variables]
[u]
type = MooseVariableFVReal
[]
[v]
type = MooseVariableFVReal
block = 0
[]
[w]
type = MooseVariableFVReal
block = 1
[]
[]
[FVKernels]
[diff_left]
type = FVDiffusion
variable = u
coeff = 'left'
block = 0
[]
[diff_right]
type = FVDiffusion
variable = u
coeff = 'right'
block = 1
[]
[diff_v]
type = FVDiffusion
variable = v
block = 0
coeff = 'left'
[]
[diff_w]
type = FVDiffusion
variable = w
block = 1
coeff = 'right'
[]
[]
[FVInterfaceKernels]
active = 'interface'
[interface]
type = FVOneVarDiffusionInterface
variable1 = u
boundary = primary_interface
subdomain1 = '0'
subdomain2 = '1'
coeff1 = 'left'
coeff2 = 'right'
[]
[bad1]
type = FVOneVarDiffusionInterface
variable1 = w
variable2 = u
boundary = primary_interface
subdomain1 = '0'
subdomain2 = '1'
coeff1 = 'left'
coeff2 = 'right'
[]
[bad2]
type = FVOneVarDiffusionInterface
variable1 = u
variable2 = v
boundary = primary_interface
subdomain1 = '0'
subdomain2 = '1'
coeff1 = 'left'
coeff2 = 'right'
[]
[bad3]
type = FVOneVarDiffusionInterface
variable1 = v
boundary = primary_interface
subdomain1 = '0'
subdomain2 = '1'
coeff1 = 'left'
coeff2 = 'right'
[]
[]
[FVBCs]
[left]
type = FVDirichletBC
variable = u
boundary = 'left'
value = 1
[]
[right]
type = FVDirichletBC
variable = u
boundary = 'right'
value = 0
[]
[v_left]
type = FVDirichletBC
variable = v
boundary = 'left'
value = 1
[]
[v_right]
type = FVDirichletBC
variable = v
boundary = 'primary_interface'
value = 0
[]
[w_left]
type = FVDirichletBC
variable = w
boundary = 'secondary_interface'
value = 1
[]
[w_right]
type = FVDirichletBC
variable = w
boundary = 'right'
value = 0
[]
[]
[Materials]
[block0]
type = ADGenericFunctorMaterial
block = '0'
prop_names = 'left'
prop_values = '4'
[]
[block1]
type = ADGenericFunctorMaterial
block = '1'
prop_names = 'right'
prop_values = '2'
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
csv = true
[]
[Functions]
[exact_u]
type = ParsedFunction
value = 'if(x<1, 1 - x/3, 4/3 - 2*x/3)'
[]
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(examples/ex03_coupling/ex03.i)
[Mesh]
file = mug.e
[]
[Variables]
[./convected]
order = FIRST
family = LAGRANGE
[../]
[./diffused]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff_convected]
type = Diffusion
variable = convected
[../]
[./conv]
type = ExampleConvection
variable = convected
# Couple a variable into the convection kernel using local_name = simulationg_name syntax
some_variable = diffused
[../]
[./diff_diffused]
type = Diffusion
variable = diffused
[../]
[]
[BCs]
[./bottom_convected]
type = DirichletBC
variable = convected
boundary = 'bottom'
value = 1
[../]
[./top_convected]
type = DirichletBC
variable = convected
boundary = 'top'
value = 0
[../]
[./bottom_diffused]
type = DirichletBC
variable = diffused
boundary = 'bottom'
value = 2
[../]
[./top_diffused]
type = DirichletBC
variable = diffused
boundary = 'top'
value = 0
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(modules/richards/test/tests/pressure_pulse/pp21.i)
# investigating pressure pulse in 1D with 2 phase
# steadystate
[Mesh]
type = GeneratedMesh
dim = 1
nx = 10
xmin = 0
xmax = 100
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = 'pwater pgas'
[../]
[./DensityWater]
type = RichardsDensityConstBulk
dens0 = 1000
bulk_mod = 2E9
[../]
[./DensityGas]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 2E6
[../]
[./SeffWater]
type = RichardsSeff2waterVG
m = 0.8
al = 1E-5
[../]
[./SeffGas]
type = RichardsSeff2gasVG
m = 0.8
al = 1E-5
[../]
[./RelPermWater]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./RelPermGas]
type = RichardsRelPermPower
simm = 0.0
n = 3
[../]
[./SatWater]
type = RichardsSat
s_res = 0.0
sum_s_res = 0.0
[../]
[./SatGas]
type = RichardsSat
s_res = 0.0
sum_s_res = 0.0
[../]
[./SUPGwater]
type = RichardsSUPGstandard
p_SUPG = 1E3
[../]
[./SUPGgas]
type = RichardsSUPGstandard
p_SUPG = 1E3
[../]
[]
[Variables]
[./pwater]
order = FIRST
family = LAGRANGE
[../]
[./pgas]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./water_ic]
type = ConstantIC
value = 2E6
variable = pwater
[../]
[./gas_ic]
type = ConstantIC
value = 2E6
variable = pgas
[../]
[]
[BCs]
[./left]
type = DirichletBC
boundary = left
value = 3E6
variable = pwater
[../]
[./left_gas]
type = DirichletBC
boundary = left
value = 3E6
variable = pgas
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[Kernels]
active = 'richardsfwater richardsfgas pconstraint'
[./richardstwater]
type = RichardsMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFlux
variable = pwater
[../]
[./richardstgas]
type = RichardsMassChange
variable = pgas
[../]
[./richardsfgas]
type = RichardsFlux
variable = pgas
[../]
[./pconstraint]
type = RichardsPPenalty
variable = pgas
a = 1E-8
lower_var = pwater
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = SeffWater
pressure_vars = 'pwater pgas'
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-15 0 0 0 1E-15 0 0 0 1E-15'
density_UO = 'DensityWater DensityGas'
relperm_UO = 'RelPermWater RelPermGas'
SUPG_UO = 'SUPGwater SUPGgas'
sat_UO = 'SatWater SatGas'
seff_UO = 'SeffWater SeffGas'
viscosity = '1E-3 1E-5'
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-pc_factor_shift_type'
petsc_options_value = 'nonzero'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
nl_rel_tol = 1.e-10
nl_max_its = 10
[]
[Outputs]
execute_on = 'timestep_end'
file_base = pp21
exodus = true
[]
(test/tests/auxkernels/user_object_dependency/aux_uo_deps.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
[]
[Problem]
kernel_coverage_check = false
[]
[Variables][dummy][][]
[AuxVariables]
[u]
order = FIRST
family = LAGRANGE
[]
[]
[AuxKernels]
[u]
type = PostprocessorAux
variable = u
# this aux kernel is indirectly depending on two other postprocessors, b and c
pp = a
[]
[]
[Postprocessors]
[a]
type = ScalePostprocessor
value = b
scaling_factor = 2
[]
[b]
type = ScalePostprocessor
value = c
scaling_factor = 4
[]
[c]
type = VolumePostprocessor
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/mortar/continuity-2d-non-conforming/dual-soln-continuity.i)
[Mesh]
second_order = false
[file]
type = FileMeshGenerator
file = nodal_normals_test_offset_nonmatching_gap.e
[]
[./primary]
input = file
type = LowerDBlockFromSidesetGenerator
sidesets = '2'
new_block_id = '20'
[../]
[./secondary]
input = primary
type = LowerDBlockFromSidesetGenerator
sidesets = '1'
new_block_id = '10'
[../]
[]
[Problem]
kernel_coverage_check = false
[]
[Variables]
[./T]
block = '1 2'
order = FIRST
[../]
[./lambda]
block = '10'
order = FIRST
use_dual = true
[../]
[]
[BCs]
[./neumann]
type = FunctionGradientNeumannBC
exact_solution = exact_soln
variable = T
boundary = '3 4 5 6 7 8'
[../]
[]
[Kernels]
[./conduction]
type = Diffusion
variable = T
block = '1 2'
[../]
[./sink]
type = Reaction
variable = T
block = '1 2'
[../]
[./forcing_function]
type = BodyForce
variable = T
function = forcing_function
block = '1 2'
[../]
[]
[Functions]
[./forcing_function]
type = ParsedFunction
value = '-4 + x^2 + y^2'
[../]
[./exact_soln]
type = ParsedFunction
value = 'x^2 + y^2'
[../]
[]
[Debug]
show_var_residual_norms = 1
[]
[Constraints]
[./mortar]
type = EqualValueConstraint
primary_boundary = 2
secondary_boundary = 1
primary_subdomain = 20
secondary_subdomain = 10
variable = lambda
secondary_variable = T
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
solve_type = NEWTON
type = Steady
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_shift_type -pc_factor_shift_amount'
petsc_options_value = 'lu basic NONZERO 1e-15'
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/view_factors/view_factor_2d.i)
[GlobalParams]
view_factor_object_name = unobstructed_vf
[]
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 2
ymin = 0
ymax = 1
nx = 2
ny = 2
[]
[UserObjects]
active = 'unobstructed_vf'
[unobstructed_vf]
type = UnobstructedPlanarViewFactor
boundary = 'top left right bottom'
execute_on = INITIAL
[]
[vf_study]
type = ViewFactorRayStudy
execute_on = initial
boundary = 'left right bottom top'
face_order = TENTH
polar_quad_order = 80
[]
[rt_vf]
type = RayTracingViewFactor
boundary = 'left right bottom top'
execute_on = INITIAL
normalize_view_factor = false
ray_study_name = vf_study
[]
[]
##
## Reference: bottom -> left/right = 0.19098
## bottom -> top = 0.61803
## Result at spatial order 20, angular order 200 & -r2
## bottom -> left/right = 0.1911
## bottom -> top = 0.6177
##
## For convenience, the "view_factor_object_name" for these
## PPs are set in global params for switching between methods
##
[Postprocessors]
[left_right]
type = ViewFactorPP
from_boundary = left
to_boundary = right
[]
[left_top]
type = ViewFactorPP
from_boundary = left
to_boundary = top
[]
[left_bottom]
type = ViewFactorPP
from_boundary = left
to_boundary = bottom
[../]
[bottom_left]
type = ViewFactorPP
from_boundary = bottom
to_boundary = left
[]
[bottom_right]
type = ViewFactorPP
from_boundary = bottom
to_boundary = right
[]
[bottom_top]
type = ViewFactorPP
from_boundary = bottom
to_boundary = top
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[Quadrature] # higher order quadrature for unobstructed
order = SECOND
[]
[]
[Outputs]
csv = true
[]
(modules/tensor_mechanics/test/tests/dynamics/linear_constraint/disp_mid.i)
# Constraining secondary nodes to move a linear combination of primary nodes
#
# The test consists of a 2D rectangular block divided into two Quad elements
# (along its height) which have different material properties.
# A displacement of 2 m is applied to the top surface of the block in x direction and the
# bottom surface is held fixed.
# The nodes of the interface between the two elements will tend to move as
# dictated by the material models of the two elements.
# LinearNodalConstraint forces the interface nodes to move as a linear combination
# of the nodes on the top and bottom of the block.
# primary node ids and the corresponding weights are taken as input by the LinearNodalConstraint
# along with the secondary node set or secondary node ids.
# The constraint can be applied using either penalty or kinematic formulation.
# In this example, the final x displacement of the top surface is 2m and bottom surface is 0m.
# Therefore, the final x displacement of the interface nodes would be 0.25*top+0.75*bottom = 0.5m
[Mesh]
file=rect_mid.e
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[Kernels]
[./TensorMechanics]
displacements = 'disp_x disp_y'
[../]
[]
[BCs]
[./top_2x]
type = DirichletBC
variable = disp_x
boundary = 10
value = 2.0
[../]
[./top_2y]
type = DirichletBC
variable = disp_y
boundary = 10
value = 0.0
[../]
[./bottom_1]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./bottom_2]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[]
[Materials]
[./Elasticity_tensor_1]
type = ComputeElasticityTensor
block = 1
fill_method = 'symmetric_isotropic'
C_ijkl = '400. 200.'
[../]
[./strain_1]
type = ComputeSmallStrain
block = 1
displacements = 'disp_x disp_y'
[../]
[./stress_1]
type = ComputeLinearElasticStress
block = 1
[../]
[./density_1]
type = GenericConstantMaterial
block = 1
prop_names = 'density'
prop_values = '10.'
[../]
[./Elasticity_tensor_2]
type = ComputeElasticityTensor
block = 2
fill_method = 'symmetric_isotropic'
C_ijkl = '1000. 500.'
[../]
[./strain_2]
type = ComputeSmallStrain
block = 2
displacements = 'disp_x disp_y'
[../]
[./stress_2]
type = ComputeLinearElasticStress
block = 2
[../]
[./density_2]
type = GenericConstantMaterial
block = 2
prop_names = 'density'
prop_values = '10.'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = ''
petsc_options_value = ''
line_search = 'none'
[]
[Constraints]
[./disp_x_1]
type = LinearNodalConstraint
variable = disp_x
primary = '0 5'
weights = '0.25 0.75'
# secondary_node_set = '2'
secondary_node_ids = '2 3'
penalty = 1e8
formulation = kinematic
[../]
[./disp_y_1]
type = LinearNodalConstraint
variable = disp_y
primary = '0 5'
weights = '0.25 0.75'
# secondary_node_set = '2'
secondary_node_ids = '2 3'
penalty = 1e8
formulation = kinematic
[../]
[]
[Postprocessors]
[./_dt]
type = TimestepSize
[../]
[./disp_1]
type = NodalVariableValue
nodeid = 0
variable = disp_x
[../]
[./disp_2]
type = NodalVariableValue
nodeid = 1
variable = disp_x
[../]
[./disp_3]
type = NodalVariableValue
nodeid = 2
variable = disp_x
[../]
[./disp_4]
type = NodalVariableValue
nodeid = 3
variable = disp_x
[../]
[./disp_5]
type = NodalVariableValue
nodeid = 4
variable = disp_x
[../]
[./disp_6]
type = NodalVariableValue
nodeid = 5
variable = disp_x
[../]
[]
[Outputs]
exodus = true
print_linear_residuals = true
perf_graph = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/richards/test/tests/gravity_head_1/gh06.i)
# unsaturated = true
# gravity = false
# supg = true
# transient = false
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
xmin = -1
xmax = 1
[]
[BCs]
[./left]
type = DirichletBC
boundary = left
value = -1
variable = pressure
[../]
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0E3
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 0.1
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = RandomIC
block = 0
min = -1
max = 0
[../]
[../]
[]
[Kernels]
active = 'richardsf'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGstandard
sat_UO = Saturation
seff_UO = SeffVG
viscosity = 1E-3
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = gh06
exodus = true
[]
(test/tests/materials/functor_properties/traditional-mat-props.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 10
xmax = 2
[]
[subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '1.0 0 0'
block_id = 1
top_right = '2.0 1.0 0'
[]
[interface]
input = subdomain1
type = SideSetsBetweenSubdomainsGenerator
primary_block = '0'
paired_block = '1'
new_boundary = 'primary0_interface'
[]
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
[diff_u]
type = MatDiffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 1
[]
[right]
type = DirichletBC
variable = u
boundary = 'right'
value = 0
[]
[]
[Materials]
[block0]
type = GenericConstantMaterial
block = '0'
prop_names = 'D'
prop_values = '4'
[]
[block1]
type = GenericConstantMaterial
block = '1'
prop_names = 'D'
prop_values = '2'
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/multiple_radiation_cavities/multiple_radiation_cavities.i)
[Problem]
kernel_coverage_check = false
material_coverage_check = false
[]
[Mesh]
[cartesian]
type = CartesianMeshGenerator
dim = 2
dx = '0.5 4 1 4 0.5'
ix = '2 2 2 2 2'
dy = '0.3 10 1'
iy = '2 2 2'
subdomain_id = '1 2 3 4 5
6 7 8 9 10
11 12 13 14 15'
[]
[add_side_left_left]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 6
paired_block = 7
new_boundary = left_left
input = cartesian
[]
[add_side_left_bottom]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 2
paired_block = 7
new_boundary = left_bottom
input = add_side_left_left
[]
[add_side_left_right]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 8
paired_block = 7
new_boundary = left_right
input = add_side_left_bottom
[]
[add_side_left_top]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 12
paired_block = 7
new_boundary = left_top
input = add_side_left_right
[]
[add_side_right_left]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 8
paired_block = 9
new_boundary = right_left
input = add_side_left_top
[]
[add_side_right_bottom]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 4
paired_block = 9
new_boundary = right_bottom
input = add_side_right_left
[]
[add_side_right_right]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 10
paired_block = 9
new_boundary = right_right
input = add_side_right_bottom
[]
[add_side_right_top]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 14
paired_block = 9
new_boundary = right_top
input = add_side_right_right
[]
[]
[GrayDiffuseRadiation]
[left]
boundary = 'left_left left_right left_bottom left_top'
emissivity = '0.8 0.8 0.9 0.5'
n_patches = '2 2 2 2'
temperature = temperature
ray_tracing_face_order = SECOND
[]
[right]
boundary = 'right_left right_right right_bottom right_top'
emissivity = '0.8 0.8 0.9 0.5'
n_patches = '2 2 2 2'
temperature = temperature
ray_tracing_face_order = SECOND
[]
[]
[Variables]
[temperature]
block = '1 2 3 4 5 6 8 10 11 12 13 14 15'
initial_condition = 300
[]
[]
[Kernels]
[conduction]
type = HeatConduction
variable = temperature
diffusion_coefficient = 10
block = '1 2 3 4 5 6 8 10 11 12 13 14 15'
[]
[]
[BCs]
[bottom]
type = DirichletBC
variable = temperature
value = 300
boundary = bottom
[]
[top]
type = DirichletBC
variable = temperature
value = 400
boundary = top
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/misc/jacobian/med.i)
[Mesh]
file = rectangle.e
[]
[Variables]
[./u]
block = 1
[../]
[./v]
[../]
[]
[AuxVariables]
[./w]
[../]
[]
[Kernels]
[./diffu]
type = WrongJacobianDiffusion
block = 1
jfactor = 0.9
variable = u
[../]
[./diffv]
type = WrongJacobianDiffusion
jfactor = 0.7
variable = v
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-mixing-length-action.i)
Re = 1e4
von_karman_const = 0.2
D = 1
rho = 1
bulk_u = 1
mu = ${fparse rho * bulk_u * D / Re}
advected_interp_method='upwind'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 5
ymin = 0
ymax = ${fparse 0.5 * D}
nx = 20
ny = 10
bias_y = ${fparse 1 / 1.2}
[]
[]
[Modules]
[NavierStokesFV]
compressibility = 'incompressible'
turbulence_handling = 'mixing-length'
passive_scalar_names = 'scalar'
density = ${rho}
dynamic_viscosity = ${mu}
passive_scalar_source = 0.1
passive_scalar_schmidt_number = 1.0
initial_velocity = '1 1 0'
initial_pressure = 0.0
inlet_boundaries = 'left'
momentum_inlet_types = 'fixed-velocity'
momentum_inlet_function = '1 0'
passive_scalar_inlet_types = 'fixed-value'
passive_scalar_inlet_function = '1'
wall_boundaries = 'top bottom'
momentum_wall_types = 'noslip symmetry'
outlet_boundaries = 'right'
momentum_outlet_types = 'fixed-pressure'
pressure_function = '0'
von_karman_const = ${von_karman_const}
mixing_length_delta = 1e9
mixing_length_walls = 'top bottom'
mixing_length_aux_execute_on ='initial'
momentum_advection_interpolation = ${advected_interp_method}
mass_advection_interpolation = ${advected_interp_method}
passive_scalar_advection_interpolation = ${advected_interp_method}
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 200 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(modules/ray_tracing/test/tests/raytracing/ray/errors.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
nx = 2
[]
[]
[UserObjects/study]
type = TestRay
execute_on = initial
ray_kernel_coverage_check = false
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
(test/tests/bcs/misc_bcs/vector_neumann_bc_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
nz = 0
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right top'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0.0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 2.0
[../]
[./top]
type = VectorNeumannBC
variable = u
vector_value = '1 1 0'
boundary = 2
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/postprocessor/show_hide.i)
# Having 2 postprocessors, putting one into hide list and the other one into show list
# We should only see the PPS that is in the show list in the output.
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 10
ny = 10
elem_type = QUAD4
# This test uses ElementalVariableValue postprocessors on specific
# elements, so element numbering needs to stay unchanged
allow_renumbering = false
[]
[Functions]
[./bc_fn]
type = ParsedFunction
value = x
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./all_u]
type = FunctionDirichletBC
variable = u
boundary = '1 3'
function = bc_fn
[../]
[]
[Postprocessors]
[./elem_56]
type = ElementalVariableValue
variable = u
elementid = 56
[../]
[./elem_12]
type = ElementalVariableValue
variable = u
elementid = 12
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
[./console]
type = Console
show = 'elem_56'
hide = 'elem_12'
[../]
[./out]
type = CSV
show = 'elem_56'
hide = 'elem_12'
[../]
[]
(test/tests/postprocessors/side_integral/side_integral_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmin = 0
xmax = 4
ymin = 0
ymax = 1
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Postprocessors]
[./integral]
type = SideIntegralVariablePostprocessor
boundary = 0
variable = u
[../]
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/thermal_hydraulics/test/tests/materials/prandtl_number/test.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
allow_renumbering = false
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[AuxVariables]
[Pr]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[RPr_ak]
type = MaterialRealAux
variable = Pr
property = Pr
[]
[]
[Materials]
[props]
type = GenericConstantMaterial
prop_names = 'cp mu k'
prop_values = '1 2 4'
[]
[Pr_material]
type = PrandtlNumberMaterial
cp = cp
k = k
mu = mu
[]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[Pr]
type = ElementalVariableValue
elementid = 0
variable = Pr
[]
[]
[Outputs]
csv = true
execute_on = timestep_end
[]
(test/tests/mesh_modifiers/add_side_sets/cylinder_normals_fixed.i)
[Mesh]
[file]
type = FileMeshGenerator
file = cylinder.e
[]
# Mesh Modifiers
[add_side_sets]
type = SideSetsFromNormalsGenerator
input = file
normals = '0 1 0
0 -1 0'
new_boundary = 'front back'
# This parameter makes it so that we won't
# adjust the normal for each adjacent element.
fixed_normal = true
variance = 0.5
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[front]
type = DirichletBC
variable = u
boundary = front
value = 0
[]
[back]
type = DirichletBC
variable = u
boundary = back
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/richards/test/tests/gravity_head_1/gh08.i)
# unsaturated = true
# gravity = true
# supg = true
# transient = false
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
xmin = -1
xmax = 1
[]
[BCs]
[./left]
type = DirichletBC
boundary = left
preset = false
value = -1
variable = pressure
[../]
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0E3
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 0.1
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = RandomIC
block = 0
min = -1
max = 0
[../]
[../]
[]
[Kernels]
active = 'richardsf'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGstandard
sat_UO = Saturation
seff_UO = SeffVG
viscosity = 1E-3
gravity = '-1 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = gh08
exodus = true
[]
(modules/phase_field/test/tests/functions/fourier_noise.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
[]
[Variables]
[./c]
[../]
[]
[Functions]
[./fn]
type = FourierNoise
lambda = 0.2
[../]
[]
[ICs]
[./c]
type = FunctionIC
variable = c
function = fn
[../]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/bcs/coupled_var_neumann/coupled_var_neumann_nl.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
[]
[Variables]
[u][]
[v][]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[diff_v]
type = Diffusion
variable = v
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[]
[right]
type = CoupledVarNeumannBC
variable = u
boundary = 'right'
v = v
[]
[v_left]
type = DirichletBC
variable = v
boundary = 'left'
value = 0
[]
[v_right]
type = DirichletBC
variable = v
boundary = 'right'
value = 1
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/phase_field/test/tests/feature_volume_vpp_test/boundary_area_2D.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 50
ny = 50
xmin = 0
xmax = 50
ymin = 0
ymax = 50
elem_type = QUAD4
[]
[./left_side]
type = SubdomainBoundingBoxGenerator
block_id = 1
bottom_left = '0 0 0'
top_right = '24.9 50 0'
input = gen
[../]
[./right_side]
type = SubdomainBoundingBoxGenerator
block_id = 2
bottom_left = '25.1 0 0'
top_right = '50 50 0'
input = left_side
[../]
[./iface_u]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 1
paired_block = 2
new_boundary = 10
input = right_side
[../]
[]
[Variables]
[./c]
order = FIRST
family = LAGRANGE
[]
[]
[AuxVariables]
[./unique_regions]
family = MONOMIAL
order = CONSTANT
[../]
[]
[ICs]
[./c]
type = SpecifiedSmoothCircleIC
variable = c
invalue = 1.0
outvalue = 0.0
radii = '4 5 10'
x_positions = '25 25 25'
y_positions = '37.5 25 0'
z_positions = '0 0 0'
int_width = 2.0
[]
[]
[Postprocessors]
[./flood_count]
type = FeatureFloodCount
variable = c
# Must be turned on to build data structures necessary for FeatureVolumeVPP
compute_var_to_feature_map = true
threshold = 0.001
execute_on = INITIAL
[../]
[]
[VectorPostprocessors]
[./features]
type = FeatureVolumeVectorPostprocessor
flood_counter = flood_count
# Turn on centroid output
output_centroids = true
execute_on = INITIAL
boundary = 10
single_feature_per_element = false
[../]
[]
[Kernels]
[diff]
type = Diffusion
variable = c
[]
[]
[AuxKernels]
[./unique_regions]
type = FeatureFloodCountAux
variable = unique_regions
flood_counter = flood_count
field_display = UNIQUE_REGION
[../]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
execute_on = INITIAL
[]
(modules/thermal_hydraulics/test/tests/vectorpostprocessors/sampler_1d_real/ad_sampler_1d_real.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 5
xmin = 0
xmax = 5
[]
[Functions]
[test_fn]
type = ParsedFunction
value = 'x'
[]
[]
[Materials]
[test_mat]
type = ADGenericFunctionMaterial
prop_names = 'test_prop'
prop_values = 'test_fn'
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[VectorPostprocessors]
[test_vpp]
type = ADSampler1DReal
block = 0
property = test_prop
sort_by = x
execute_on = 'INITIAL'
[]
[]
[Outputs]
csv = true
execute_on = 'INITIAL'
[]
(modules/ray_tracing/test/tests/raykernels/ad_ray_kernel/errors.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
[]
[]
[UserObjects/study]
type = RepeatableRayStudy
start_points = '0 0 0'
directions = '1 0 0'
names = 'ray'
execute_on = PRE_KERNELS
[]
[Variables/u]
[]
[RayKernels/line_source]
type = ADLineSourceRayKernel
variable = u
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
(modules/navier_stokes/test/tests/finite_volume/fviks/convection/convection_cavity.i)
mu = 1
rho = 1
k = .01
cp = 1
velocity_interp_method = 'rc'
advected_interp_method = 'average'
[Mesh]
[cmg]
type = CartesianMeshGenerator
dim = 2
dx = '1 0.5'
dy = '1'
ix = '8 5'
iy = '8'
subdomain_id = '0 1'
[]
[interface]
type = SideSetsBetweenSubdomainsGenerator
input = 'cmg'
primary_block = 0
paired_block = 1
new_boundary = 'interface'
[]
[secondary_interface]
type = SideSetsBetweenSubdomainsGenerator
input = 'interface'
primary_block = 1
paired_block = 0
new_boundary = 'secondary_interface'
[]
[]
[GlobalParams]
# retain behavior at time of test creation
two_term_boundary_expansion = false
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
block = 0
pressure = pressure
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
block = 0
[]
[v]
type = INSFVVelocityVariable
block = 0
[]
[pressure]
type = INSFVPressureVariable
block = 0
[]
[T]
type = INSFVEnergyVariable
block = 0
[]
[Ts]
type = INSFVEnergyVariable
block = 1
[]
[lambda]
family = SCALAR
order = FIRST
[]
[]
[ICs]
[T]
type = ConstantIC
variable = T
value = 1
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
block = 0
[]
[mean_zero_pressure]
type = FVScalarLagrangeMultiplier
variable = pressure
lambda = lambda
block = 0
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
rho = ${rho}
block = 0
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
block = 0
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
block = 0
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
rho = ${rho}
block = 0
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
block = 0
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
block = 0
[]
[temp_conduction]
type = FVDiffusion
coeff = 'k'
variable = T
block = 0
[]
[temp_advection]
type = INSFVEnergyAdvection
variable = T
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
block = 0
[]
[solid_temp_conduction]
type = FVDiffusion
coeff = 'k'
variable = Ts
block = 1
[]
[]
[FVInterfaceKernels]
[convection]
type = FVConvectionCorrelationInterface
variable1 = T
variable2 = Ts
boundary = 'interface'
h = 5
temp_solid = Ts
temp_fluid = T
subdomain1 = 0
subdomain2 = 1
bulk_distance = 0.3
[]
[]
[FVBCs]
[top_x]
type = INSFVNoSlipWallBC
variable = u
boundary = 'top'
function = 'lid_function'
[]
[no_slip_x]
type = INSFVNoSlipWallBC
variable = u
boundary = 'left interface bottom'
function = 0
[]
[no_slip_y]
type = INSFVNoSlipWallBC
variable = v
boundary = 'left interface top bottom'
function = 0
[]
[T_hot]
type = FVDirichletBC
variable = T
boundary = 'bottom'
value = 1
[]
[T_cold]
type = FVDirichletBC
variable = Ts
boundary = 'right'
value = 0
[]
[]
[Materials]
[functor_constants]
type = ADGenericFunctorMaterial
prop_names = 'cp k'
prop_values = '${cp} ${k}'
[]
[ins_fv]
type = INSFVEnthalpyMaterial
temperature = 'T'
rho = ${rho}
block = 0
[]
[]
[Functions]
[lid_function]
type = ParsedFunction
value = '4*x*(1-x)'
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_shift_type -ksp_gmres_restart'
petsc_options_value = 'asm lu NONZERO 200'
line_search = 'none'
nl_rel_tol = 1e-12
nl_max_its = 6
l_max_its = 200
[]
[Outputs]
exodus = true
[]
(test/tests/restrictable/internal_side_user_object/internal_side_user_object.i)
[Mesh]
type = FileMesh
file = rectangle.e
dim = 2
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Postprocessors]
[./all_pp]
type = NumInternalSides
execute_on = 'initial timestep_end'
[../]
[./block_1_pp]
type = NumInternalSides
block = 1
execute_on = 'initial timestep_end'
[../]
[./block_2_pp]
type = NumInternalSides
block = 2
execute_on = 'initial timestep_end'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = false
csv = true
[]
(test/tests/vectorpostprocessors/element_id_counters/side_element_counter.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
xmax = 1
ymax = 1
extra_element_integers = foo_id
[]
[id0]
type = SubdomainBoundingBoxGenerator
input = gmg
bottom_left = '0 0 0'
block_id = 0
top_right = '1 1 0'
integer_name = foo_id
[]
[id1]
type = SubdomainBoundingBoxGenerator
input = id0
bottom_left = '0.4 0.4 0'
block_id = 1
top_right = '0.9 0.9 0'
integer_name = foo_id
[]
[id2]
type = SubdomainBoundingBoxGenerator
input = id1
bottom_left = '0.1 0.1 0'
block_id = 2
top_right = '0.6 0.6 0'
integer_name = foo_id
[]
[subdomain]
type = SubdomainBoundingBoxGenerator
input = id2
bottom_left = '0 0.5 0'
block_id = 1
top_right = '1 1 0'
[]
[side0to1]
type = SideSetsBetweenSubdomainsGenerator
input = subdomain
primary_block = 0
paired_block = 1
new_boundary = side0to1
[]
[]
[VectorPostprocessors]
[elem_counter]
type = SideElementCounterWithID
boundary = side0to1
id_name = foo_id
[]
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
execute_on = 'timestep_end'
[]
(test/tests/interfacekernels/1d_interface/ik_save_in_test.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 2
xmax = 2
[]
[./subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '1.0 0 0'
block_id = 1
top_right = '2.0 1.0 0'
[../]
[./interface]
type = SideSetsBetweenSubdomainsGenerator
input = subdomain1
primary_block = '0'
paired_block = '1'
new_boundary = 'primary0_interface'
[../]
[./interface_again]
type = SideSetsBetweenSubdomainsGenerator
input = interface
primary_block = '1'
paired_block = '0'
new_boundary = 'primary1_interface'
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
block = '0'
[../]
[./v]
order = FIRST
family = LAGRANGE
block = '1'
[../]
[]
[AuxVariables]
[./primary_resid]
[../]
[./secondary_resid]
[../]
[./primary_jac]
[../]
[./secondary_jac]
[../]
[]
[Kernels]
[./diff_u]
type = CoeffParamDiffusion
variable = u
D = 4
block = 0
save_in = 'primary_resid'
[../]
[./diff_v]
type = CoeffParamDiffusion
variable = v
D = 2
block = 1
save_in = 'secondary_resid'
[../]
[]
[InterfaceKernels]
[./interface]
type = InterfaceDiffusion
variable = u
neighbor_var = v
boundary = primary0_interface
D = 4
D_neighbor = 2
save_in_var_side = 'm s'
save_in = 'primary_resid secondary_resid'
diag_save_in_var_side = 'm s'
diag_save_in = 'primary_jac secondary_jac'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
save_in = 'primary_resid'
[../]
[./right]
type = DirichletBC
variable = v
boundary = 'right'
value = 1
save_in = 'secondary_resid'
[../]
[./middle]
type = MatchedValueBC
variable = v
boundary = 'primary0_interface'
v = u
save_in = 'secondary_resid'
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
print_linear_residuals = true
[]
[Debug]
show_var_residual_norms = true
[]
(modules/heat_conduction/test/tests/heat_conduction_patch/heat_conduction_patch_rz_quad8.i)
#
# This problem is taken from the Abaqus verification manual:
# "1.5.8 Patch test for heat transfer elements"
#
# The temperature on the exterior nodes is -2e5+200x+100y.
#
# This gives a constant flux at all Gauss points.
#
# In addition, the temperature at all nodes follows the same formula.
#
# Node x y Temperature
# 1 1e3 0 0
# 2 1.00024e3 0 48
# 3 1.00018e3 3e-2 39
# 4 1.00004e3 2e-2 10
# 9 1.00008e3 8e-2 24
# 10 1e3 1.2e-1 12
# 14 1.00016e3 8e-2 40
# 17 1.00024e3 1.2e-1 60
[Problem]
coord_type = RZ
[]
[Mesh]#Comment
file = heat_conduction_patch_rz_quad8.e
[] # Mesh
[Functions]
[./temps]
type = ParsedFunction
value='-2e5+200*x+100*y'
[../]
[] # Functions
[Variables]
[./temp]
order = SECOND
family = LAGRANGE
[../]
[] # Variables
[Kernels]
[./heat_r]
type = HeatConduction
variable = temp
[../]
[] # Kernels
[BCs]
[./temps]
type = FunctionDirichletBC
variable = temp
boundary = 10
function = temps
[../]
[] # BCs
[Materials]
[./heat]
type = HeatConductionMaterial
block = 1
specific_heat = 0.116
thermal_conductivity = 4.85e-4
[../]
[] # Materials
[Executioner]
type = Steady
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -ksp_gmres_restart'
petsc_options_value = 'lu 101'
line_search = 'none'
nl_abs_tol = 1e-11
nl_rel_tol = 1e-10
l_max_its = 20
[./Quadrature]
order = THIRD
[../]
[] # Executioner
[Outputs]
exodus = true
[] # Outputs
(test/tests/preconditioners/fsp/fsp_test_image.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 41
ny = 41
[]
[./image]
input = gen
type = ImageSubdomainGenerator
file = kitten.png
threshold = 100
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
block = 1
[../]
[./v]
order = FIRST
family = LAGRANGE
block = 1
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./conv_v]
type = CoupledForce
variable = v
v = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[BCs]
active = 'left_u left_v right_u'
[./left_u]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 100
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = left
value = 0
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = right
value = 0
[../]
[]
[Problem]
type = FEProblem
material_coverage_check = false
kernel_coverage_check = false
[]
[Executioner]
# This is setup automatically in MOOSE (SetupPBPAction.C)
# petsc_options = '-snes_mf_operator'
# petsc_options_iname = '-pc_type'
# petsc_options_value = 'asm'
type = Steady
[]
[Preconditioning]
[./FSP]
# It is the starting point of splitting
type = FSP
topsplit = 'uv' # 'uv'
[./uv]
# Generally speaking, there are four types of splitting we could choose
# <additive,multiplicative,symmetric_multiplicative,schur>
# An approximate solution to the original system
# | A_uu A_uv | | u | _ |f_u|
# | 0 A_vv | | v | - |f_v|
# is obtained by solving the following subsystems
# A_uu u = f_u and A_vv v = f_v
# If splitting type is specified as schur, we may also want to set more options to
# control how schur works using PETSc options
# petsc_options_iname = '-pc_fieldsplit_schur_fact_type -pc_fieldsplit_schur_precondition'
# petsc_options_value = 'full selfp'
splitting = 'u v' # 'u' and 'v'
splitting_type = additive
[../]
[./u]
# PETSc options for this subsolver
# A prefix will be applied, so just put the options for this subsolver only
vars = u
petsc_options_iname = '-pc_type -ksp_type'
petsc_options_value = ' hypre preonly'
[../]
[./v]
# PETSc options for this subsolver
vars = v
petsc_options_iname = '-pc_type -ksp_type'
petsc_options_value = ' hypre preonly'
[../]
[../]
[]
[Outputs]
file_base = kitten_out
exodus = true
[]
(modules/ray_tracing/test/tests/raykernels/errors/raykernel_errors.i)
[Mesh]
active = 'gmg'
[gmg]
type = CartesianMeshGenerator
dim = 1
dx = '0.5 0.5'
ix = '1 1'
subdomain_id = '0 1'
[]
[internal]
type = SideSetsBetweenSubdomainsGenerator
input = gmg
primary_block = 1
paired_block = 0
new_boundary = internal
[]
[]
[UserObjects]
active = 'study'
[study]
type = RepeatableRayStudy
start_points = '0 0 0'
directions = '1 0 0'
names = 'ray'
execute_on = INITIAL
ray_kernel_coverage_check = false
[]
[end_study]
type = RepeatableRayStudy
start_points = '0 0 0'
end_points = '0.25 0 0'
names = 'ray'
execute_on = INITIAL
ray_kernel_coverage_check = false
[]
[]
[RayKernels]
active = ''
[kill]
type = KillRayKernel
[]
[change_after_kill]
type = ChangeRayRayKernelTest
change_start_direction = true
depends_on = kill
[]
[change]
type = ChangeRayRayKernelTest
change_start_direction = true
[]
[change_again]
type = ChangeRayRayKernelTest
change_start_direction = true
[]
[change_out_of_elem]
type = ChangeRayRayKernelTest
change_start_out_of_elem = true
[]
[change_zero]
type = ChangeRayRayKernelTest
change_direction_zero = true
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
(test/tests/preconditioners/pbp/pbp_dg_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
xmin = 0
xmax = 1
ymin = 0
ymax = 1
elem_type = QUAD4
[]
[Variables]
[./u]
order = FIRST
family = MONOMIAL
[../]
[./v]
order = FIRST
family = MONOMIAL
[../]
[]
[Preconditioning]
[./PBP]
type = PBP
solve_order = 'u v'
preconditioner = 'AMG AMG'
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./abs_u]
type = Reaction
variable = u
[../]
[./forcing_u]
type = BodyForce
variable = u
function = forcing_fn
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[./abs_v]
type = Reaction
variable = v
[../]
[./forcing_v]
type = BodyForce
variable = v
function = forcing_fn
[../]
[./conv_v]
type = CoupledForce
variable = v
v = u
[../]
[]
[DGKernels]
[./dg_diff]
type = DGDiffusion
variable = u
epsilon = -1
sigma = 6
[../]
[./dg_diff_2]
type = DGDiffusion
variable = v
epsilon = -1
sigma = 6
[../]
[]
[Functions]
[./forcing_fn]
type = ParsedFunction
value = 2*pow(e,-x-(y*y))*(1-2*y*y)
[../]
[./exact_fn]
type = ParsedGradFunction
value = pow(e,-x-(y*y))
grad_x = -pow(e,-x-(y*y))
grad_y = -2*y*pow(e,-x-(y*y))
[../]
[]
[BCs]
[./all_u]
type = DGFunctionDiffusionDirichletBC
variable = u
boundary = '0 1 2 3'
function = exact_fn
epsilon = -1
sigma = 6
[../]
[./all_v]
type = DGFunctionDiffusionDirichletBC
variable = v
boundary = '0 1 2 3'
function = exact_fn
epsilon = -1
sigma = 6
[../]
[]
[Problem]
type = FEProblem
error_on_jacobian_nonzero_reallocation = true
[]
[Executioner]
type = Steady
l_max_its = 10
nl_max_its = 10
solve_type = JFNK
[]
[Outputs]
exodus = true
[]
(modules/fluid_properties/test/tests/ics/rho_vapor_mixture_from_pressure_temperature/test.i)
# Tests the initial condition for mixture density from pressure and temperature.
# This test uses the general vapor mixture fluid properties with steam, air,
# and helium with mass fractions 0.5, 0.3, and 0.2, respectively. The individual
# specific volumes (in m^3/kg) at p = 100 kPa, T = 500 K are:
# steam: 2.298113001
# air: 1.43525
# helium: 10.3855
# For the general vapor mixture, the mixture specific volume is computed as
# v = \sum\limits_i x_i v_i ,
# where x_i is the mass fraction of component i, and v_i is the specific volume
# of component i. Therefore, the correct value for specific volume of the mixture is
# v = 3.65673150050 m^3/kg
# and thus density is
# rho = 0.27346825980066236 kg/m^3
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
allow_renumbering = false
[]
[Modules]
[FluidProperties]
[fp_steam]
type = StiffenedGasFluidProperties
gamma = 1.43
cv = 1040.0
q = 2.03e6
p_inf = 0.0
q_prime = -2.3e4
k = 0.026
mu = 134.4e-7
M = 0.01801488
rho_c = 322.0
[]
[fp_air]
type = IdealGasFluidProperties
gamma = 1.4
molar_mass = 28.965197004e-3
[]
[fp_helium]
type = IdealGasFluidProperties
gamma = 1.66
molar_mass = 4.002917432959e-3
[]
[fp_vapor_mixture]
type = IdealRealGasMixtureFluidProperties
fp_primary = fp_steam
fp_secondary = 'fp_air fp_helium'
[]
[]
[]
[AuxVariables]
[rho]
[]
[p]
[]
[T]
[]
[x_air]
[]
[x_helium]
[]
[]
[ICs]
[rho_ic]
type = RhoVaporMixtureFromPressureTemperatureIC
variable = rho
p = p
T = T
x_secondary_vapors = 'x_air x_helium'
fp_vapor_mixture = fp_vapor_mixture
[]
[p_ic]
type = ConstantIC
variable = p
value = 100e3
[]
[T_ic]
type = ConstantIC
variable = T
value = 500
[]
[x_air_ic]
type = ConstantIC
variable = x_air
value = 0.3
[]
[x_helium_ic]
type = ConstantIC
variable = x_helium
value = 0.2
[]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[rho_test]
type = ElementalVariableValue
elementid = 0
variable = rho
execute_on = 'INITIAL TIMESTEP_END'
[]
[]
[Outputs]
csv = true
execute_on = 'INITIAL'
[]
[Problem]
solve = false
[]
(test/tests/postprocessors/element_l1_error/element_l1_error.i)
# Tests the ElementL1Error post-processor.
#
# The Element L1 error is defined as follows:
# \sum\limits_i = int\limits_{\Omega_i} |y_{h,i} - y(x)| d\Omega
# where i is the element index and y_h is the approximate solution.
#
# This example uses 2 uniform elements on (0,10) with the following values:
# (0,5): y = 3, y_h = 5
# (5,10): y = 2, y_h = 6
# Thus the gold value is
# gold = 5*(5-3) + 5*(6-2) = 10 + 20 = 30
[Mesh]
type = GeneratedMesh
dim = 1
nx = 2
xmin = 0
xmax = 10
[]
[Variables]
[u]
order = CONSTANT
family = MONOMIAL
[]
[]
[ICs]
[u_ic]
type = FunctionIC
variable = u
function = u_ic_fn
[]
[]
[Functions]
[u_ic_fn]
type = ParsedFunction
value = 'if(x<5,5,6)'
[]
[u_exact_fn]
type = ParsedFunction
value = 'if(x<5,3,2)'
[]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Postprocessors]
[err]
type = ElementL1Error
variable = u
function = u_exact_fn
execute_on = 'initial'
[]
[]
[Outputs]
csv = true
execute_on = 'initial'
[]
(modules/ray_tracing/test/tests/postprocessors/ray_data_value/ray_data_value.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 5
ny = 5
xmax = 5
ymax = 5
[]
[]
[RayKernels/null]
type = NullRayKernel
[]
[UserObjects/study]
type = RepeatableRayStudy
start_points = '0.5 0.5 0
2.5 2.5 0'
end_points = '5 4.9 0
0.1 0 0'
names = 'ray0 ray1'
ray_data_names = 'data0 data1'
initial_ray_data = '1 2;
3 4'
ray_aux_data_names = 'aux_data0 aux_data1'
initial_ray_aux_data = '5 6;
7 8'
[]
[Postprocessors]
[ray0_data0]
type = RayDataValue
study = study
ray_name = ray0
data_name = data0
[]
[ray0_data1]
type = RayDataValue
study = study
ray_name = ray0
data_name = data1
[]
[ray0_aux_data0]
type = RayDataValue
study = study
ray_name = ray0
data_name = aux_data0
aux = true
[]
[ray0_aux_data1]
type = RayDataValue
study = study
ray_name = ray0
data_name = aux_data1
aux = true
[]
# For ray1, we're betting on the fact that the IDs are assigned
# in sequential order, therefore its ID should be 1. In reality,
# you should rely on the name but this is just for testing purposes.
[ray1_data0]
type = RayDataValue
study = study
ray_id = 1
data_name = data0
[]
[ray1_data1]
type = RayDataValue
study = study
ray_id = 1
data_name = data1
[]
[ray1_aux_data0]
type = RayDataValue
study = study
ray_id = 1
data_name = aux_data0
aux = true
[]
[ray1_aux_data1]
type = RayDataValue
study = study
ray_id = 1
data_name = aux_data1
aux = true
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = false
csv = true
[]
(python/peacock/tests/input_tab/InputFileEditor/gold/fsp_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
[]
[v]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
[diff_u]
type = Diffusion
variable = u
[]
[conv_v]
type = CoupledForce
variable = v
v = 'u'
[]
[diff_v]
type = Diffusion
variable = v
[]
[]
[BCs]
inactive = 'right_v'
[left_u]
type = DirichletBC
variable = u
boundary = '1'
value = 0
[]
[right_u]
type = DirichletBC
variable = u
boundary = '2'
value = 100
[]
[left_v]
type = DirichletBC
variable = v
boundary = '1'
value = 0
[]
[right_v]
type = DirichletBC
variable = v
boundary = '2'
value = 0
[]
[]
[Executioner]
# This is setup automatically in MOOSE (SetupPBPAction.C)
# petsc_options = '-snes_mf_operator'
# petsc_options_iname = '-pc_type'
# petsc_options_value = 'asm'
type = Steady
[]
[Preconditioning]
[FSP]
# It is the starting point of splitting
type = FSP
topsplit = 'uv' # uv should match the following block name
[uv]
# Generally speaking, there are four types of splitting we could choose
# <additive,multiplicative,symmetric_multiplicative,schur>
# An approximate solution to the original system
# | A_uu A_uv | | u | _ |f_u|
# | 0 A_vv | | v | - |f_v|
# is obtained by solving the following subsystems
# A_uu u = f_u and A_vv v = f_v
# If splitting type is specified as schur, we may also want to set more options to
# control how schur works using PETSc options
# petsc_options_iname = '-pc_fieldsplit_schur_fact_type -pc_fieldsplit_schur_precondition'
# petsc_options_value = 'full selfp'
splitting = 'u v' # u and v are the names of subsolvers
splitting_type = additive
[]
[u]
# PETSc options for this subsolver
# A prefix will be applied, so just put the options for this subsolver only
vars = 'u'
petsc_options_iname = '-pc_type -ksp_type'
petsc_options_value = ' hypre preonly'
[]
[v]
# PETSc options for this subsolver
vars = 'v'
petsc_options_iname = '-pc_type -ksp_type'
petsc_options_value = ' hypre preonly'
[]
[]
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/plane-poiseuille-flow.i)
mu=0.5
rho=1.1
advected_interp_method='average'
velocity_interp_method='average'
two_term_boundary_expansion=true
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 10
ymin = -1
ymax = 1
nx = 10
ny = 2
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
two_term_boundary_expansion = ${two_term_boundary_expansion}
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
two_term_boundary_expansion = ${two_term_boundary_expansion}
[]
[pressure]
type = INSFVPressureVariable
two_term_boundary_expansion = ${two_term_boundary_expansion}
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[u_forcing]
type = INSFVBodyForce
variable = u
functor = forcing_u
momentum_component = 'x'
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[v_forcing]
type = INSFVBodyForce
variable = v
functor = forcing_v
momentum_component = 'y'
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = 'exact_u'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = 'exact_v'
[]
[walls-u]
type = INSFVNoSlipWallBC
variable = u
boundary = 'top bottom'
function = 'exact_u'
[]
[walls-v]
type = INSFVNoSlipWallBC
variable = v
boundary = 'top bottom'
function = 'exact_v'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 'exact_p'
[]
[]
[Functions]
[exact_u]
type = ParsedFunction
value = '0.5*(1.0 - y^2)/mu'
vars = 'mu'
vals = '${mu}'
[]
[exact_rhou]
type = ParsedFunction
value = '0.5*rho*(1.0 - y^2)/mu'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[forcing_u]
type = ADParsedFunction
value = '0'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_v]
type = ParsedFunction
value = '0.0'
[]
[exact_rhov]
type = ParsedFunction
value = '0'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[forcing_v]
type = ADParsedFunction
value = '0'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_p]
type = ParsedFunction
value = '10.0 - x'
[]
[forcing_p]
type = ParsedFunction
value = '0'
vars = 'rho mu'
vals = '${rho} ${mu}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[./L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2v]
type = ElementL2Error
variable = v
function = exact_v
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2p]
variable = pressure
function = exact_p
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[]
(modules/tensor_mechanics/test/tests/ics/volume_weighted_weibull/volume_weighted_weibull.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 100
ny = 100
[]
[Problem]
solve = false
[]
[AuxVariables]
[u_vww]
order = CONSTANT
family = MONOMIAL
[]
[]
[ICs]
[u_vww]
type = VolumeWeightedWeibull
variable = u_vww
reference_volume = 0.0001 #This is the volume of an element for a 100x100 mesh
weibull_modulus = 15.0
median = 1.0
# When the reference_volume is equal to the element volume (so that there is no volume correction),
# this combination of Weibull modulus and median gives the same distribution that you would get with
# the following parameters in a WeibullDistribution:
# weibull_modulus = 15.0
# location = 0
# scale = 1.024735156 #median * (-1/log(0.5))^(1/weibull_modulus)
[]
[]
[VectorPostprocessors]
[./histo]
type = VariableValueVolumeHistogram
variable = u_vww
min_value = 0
max_value = 2
bin_number = 100
execute_on = initial
outputs = initial
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
[./initial]
type = CSV
execute_on = initial
[../]
[]
(test/tests/misc/check_error/function_file_test2.i)
# Test for usage of missing function
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = ic_function
[../]
[../]
[]
[Functions]
[./ic_function]
type = PiecewiseLinear
data_file = piecewise_linear_rows.csv #Will generate error because data is expected in columns
format = columns
scale_factor = 1.0
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/markers/block_restricted/marker_block.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 2
xmax = 5
ymax = 5
[]
[./lower_block]
input = gen
type = SubdomainBoundingBoxGenerator
top_right = '5 3 0'
bottom_left = '0 0 0'
block_id = 0
[../]
[./upper_block]
input = lower_block
type = SubdomainBoundingBoxGenerator
top_right = '5 5 0'
bottom_left = '0 3 0'
block_id = 1
[../]
[]
[Adaptivity]
initial_steps = 2
initial_marker = marker
[./Markers]
[./marker]
type = UniformMarker
block = 0
mark = REFINE
[../]
[../]
[]
[Variables]
[./u]
initial_condition = 0
[../]
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/stochastic_tools/test/tests/multiapps/batch_commandline_control/sub.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Variables]
[u]
initial_condition = 1980
[]
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
[]
[Materials]
[const]
type = GenericConstantMaterial
prop_names = 'A B C D'
prop_values = '1.0 2.0 3.0 4.0'
[]
[]
[Postprocessors]
[size]
type = AverageElementSize
execute_on = 'initial'
[]
[prop_A]
type = ElementAverageMaterialProperty
mat_prop = A
execute_on = 'initial'
[]
[prop_B]
type = ElementAverageMaterialProperty
mat_prop = B
execute_on = 'initial'
[]
[prop_C]
type = ElementAverageMaterialProperty
mat_prop = C
execute_on = 'initial'
[]
[prop_D]
type = ElementAverageMaterialProperty
mat_prop = D
execute_on = 'initial'
[]
[]
[Outputs]
[]
(modules/richards/test/tests/jacobian_1/jn08.i)
# unsaturated = true
# gravity = true
# supg = true
# transient = false
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = -1
xmax = 1
ymin = -1
ymax = 1
zmin = -1
zmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0 # notice small quantity, so the PETSc constant state works
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1 # notice small quantity, so the PETSc constant state works
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.2
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 0.1
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = RandomIC
block = 0
min = -1
max = 0
[../]
[../]
[]
[Kernels]
active = 'richardsf'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGstandard
sat_UO = Saturation
seff_UO = SeffVG
viscosity = 1E-3
gravity = '1 2 3'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -snes_type'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000 test'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = jn08
exodus = false
[]
(test/tests/multiapps/command_line/sub.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Variables]
[u]
initial_condition = 1980
[]
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/bad_bc_var_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = foo # Test for missing variable
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/porous_flow/examples/flow_through_fractured_media/fine_steady.i)
# Using a mixed-dimensional mesh
# Steady-state porepressure distribution along a fracture in a porous matrix
# This is used to initialise the transient solute-transport simulation
[Mesh]
type = FileMesh
# The gold mesh is used to reduce the number of large files in the MOOSE repository.
# The porepressure is not read from the gold mesh
file = 'gold/fine_steady_out.e'
block_id = '1 2 3'
block_name = 'fracture matrix1 matrix2'
boundary_id = '1 2'
boundary_name = 'bottom top'
[]
[GlobalParams]
PorousFlowDictator = dictator
gravity = '0 0 0'
[]
[Variables]
[pp]
[]
[]
[ICs]
[pp]
type = ConstantIC
variable = pp
value = 1e6
[]
[]
[BCs]
[ptop]
type = DirichletBC
variable = pp
boundary = top
value = 1e6
[]
[pbottom]
type = DirichletBC
variable = pp
boundary = bottom
value = 1.002e6
[]
[]
[Kernels]
[adv0]
type = PorousFlowAdvectiveFlux
fluid_component = 0
variable = pp
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 2e9
density0 = 1000
thermal_expansion = 0
viscosity = 1e-3
[]
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow1PhaseFullySaturated
porepressure = pp
[]
[massfrac]
type = PorousFlowMassFraction
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[relp]
type = PorousFlowRelativePermeabilityConst
phase = 0
[]
[permeability1]
type = PorousFlowPermeabilityConst
permeability = '1.8e-11 0 0 0 1.8e-11 0 0 0 1.8e-11' # kf=3e-8, a=6e-4m. 1.8e-11 = kf * a
block = 'fracture'
[]
[permeability2]
type = PorousFlowPermeabilityConst
permeability = '1e-20 0 0 0 1e-20 0 0 0 1e-20'
block = 'matrix1 matrix2'
[]
[]
[Preconditioning]
active = basic
[mumps_is_best_for_parallel_jobs]
type = SMP
full = true
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu mumps'
[]
[basic]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -sub_pc_factor_shift_type -pc_asm_overlap'
petsc_options_value = 'gmres asm lu NONZERO 2 '
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
# controls for nonlinear iterations
nl_abs_tol = 1e-9
nl_rel_tol = 1e-14
[]
[Outputs]
exodus = true
execute_on = 'timestep_end'
[]
(test/tests/mortar/continuity-3d-non-conforming/continuity_tet10.i)
[Mesh]
second_order = true
[left_block]
type = GeneratedMeshGenerator
dim = 3
nx = 1
ny = 2
nz = 2
xmin = 0
xmax = 0.3
ymin = 0
ymax = .5
zmin = 0
zmax = .5
elem_type = TET10
[]
[left_block_sidesets]
type = RenameBoundaryGenerator
input = left_block
old_boundary = '0 1 2 3 4 5'
new_boundary = 'lb_bottom lb_back lb_right lb_front lb_left lb_top'
[]
[left_block_id]
type = SubdomainIDGenerator
input = left_block_sidesets
subdomain_id = 1
[]
[right_block]
type = GeneratedMeshGenerator
dim = 3
nx = 1
ny = 2
nz = 2
xmin = 0.3
xmax = 0.6
ymin = 0
ymax = .5
zmin = 0
zmax = .5
elem_type = TET10
[]
[right_block_id]
type = SubdomainIDGenerator
input = right_block
subdomain_id = 2
[]
[right_block_change_boundary_id]
type = RenameBoundaryGenerator
input = right_block_id
old_boundary = '0 1 2 3 4 5'
new_boundary = '100 101 102 103 104 105'
[]
[combined]
type = MeshCollectionGenerator
inputs = 'left_block_id right_block_change_boundary_id'
[]
[block_rename]
type = RenameBlockGenerator
input = combined
old_block = '1 2'
new_block = 'left_block right_block'
[]
[right_right_sideset]
type = SideSetsAroundSubdomainGenerator
input = block_rename
new_boundary = rb_right
block = right_block
normal = '1 0 0'
[]
[right_left_sideset]
type = SideSetsAroundSubdomainGenerator
input = right_right_sideset
new_boundary = rb_left
block = right_block
normal = '-1 0 0'
[]
[right_top_sideset]
type = SideSetsAroundSubdomainGenerator
input = right_left_sideset
new_boundary = rb_top
block = right_block
normal = '0 0 1'
[]
[right_bottom_sideset]
type = SideSetsAroundSubdomainGenerator
input = right_top_sideset
new_boundary = rb_bottom
block = right_block
normal = '0 0 -1'
[]
[right_front_sideset]
type = SideSetsAroundSubdomainGenerator
input = right_bottom_sideset
new_boundary = rb_front
block = right_block
normal = '0 1 0'
[]
[right_back_sideset]
type = SideSetsAroundSubdomainGenerator
input = right_front_sideset
new_boundary = rb_back
block = right_block
normal = '0 -1 0'
[]
[secondary]
input = right_back_sideset
type = LowerDBlockFromSidesetGenerator
sidesets = 'lb_right'
new_block_id = '12'
new_block_name = 'secondary'
[]
[primary]
input = secondary
type = LowerDBlockFromSidesetGenerator
sidesets = 'rb_left'
new_block_id = '11'
new_block_name = 'primary'
[]
[]
[Problem]
kernel_coverage_check = false
[]
[Variables]
[T]
block = '1 2'
order = SECOND
[]
[lambda]
block = 'secondary'
family = LAGRANGE
order = SECOND
[]
[]
[BCs]
[neumann]
type = FunctionGradientNeumannBC
exact_solution = exact_soln_primal
variable = T
boundary = 'lb_back lb_front lb_left lb_top lb_bottom rb_right rb_top rb_bottom rb_front rb_back'
[]
[]
[Kernels]
[conduction]
type = Diffusion
variable = T
block = '1 2'
[]
[sink]
type = Reaction
variable = T
block = '1 2'
[]
[forcing_function]
type = BodyForce
variable = T
function = forcing_function
block = '1 2'
[]
[]
[Functions]
[forcing_function]
type = ParsedFunction
value = 'sin(x*pi)*sin(y*pi)*sin(z*pi) + 3*pi^2*sin(x*pi)*sin(y*pi)*sin(z*pi)'
[]
[exact_soln_primal]
type = ParsedFunction
value = 'sin(x*pi)*sin(y*pi)*sin(z*pi)'
[]
[exact_soln_lambda]
type = ParsedFunction
value = 'pi*sin(pi*y)*sin(pi*z)*cos(pi*x)'
[]
[]
[Debug]
show_var_residual_norms = 1
[]
[Constraints]
[mortar]
type = EqualValueConstraint
primary_boundary = 'rb_left'
secondary_boundary = 'lb_right'
primary_subdomain = '11'
secondary_subdomain = '12'
variable = lambda
secondary_variable = T
delta = .1
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
solve_type = NEWTON
type = Steady
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_shift_type '
'-pc_factor_shift_amount'
petsc_options_value = 'lu basic NONZERO 1e-15'
[]
[Outputs]
exodus = true
[]
[Postprocessors]
[L2lambda]
type = ElementL2Error
variable = lambda
function = exact_soln_lambda
execute_on = 'timestep_end'
block = 'secondary'
[]
[L2u]
type = ElementL2Error
variable = T
function = exact_soln_primal
execute_on = 'timestep_end'
block = 'left_block right_block'
[]
[h]
type = AverageElementSize
block = 'left_block right_block'
[]
[]
(test/tests/materials/derivative_material_interface/additional_derivatives.i)
#
# This test validates the correct application of the chain rule to coupled
# material properties within DerivativeParsedMaterials
#
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Variables]
[a]
[]
[]
[Materials]
[term]
type = DerivativeParsedMaterial
f_name = F
args = 'a'
function = '(a*b*d*e)^3'
material_property_names = 'b d:=c e'
derivative_order = 2
additional_derivative_symbols = 'e d'
outputs = exodus
[]
[const]
type = GenericConstantMaterial
prop_names = 'b c e'
prop_values = '1 2 3'
[]
[]
[Kernels]
[a]
type = Diffusion
variable = a
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
l_tol = 1e-03
[]
[Outputs]
execute_on = 'TIMESTEP_END'
exodus = true
print_linear_residuals = false
[]
(modules/ray_tracing/test/tests/raykernels/coupled_line_source_ray_kernel/coupled_line_source_ray_kernel.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
xmax = 5
ymax = 5
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
[]
[v]
order = FIRST
family = LAGRANGE
[]
[]
[BCs]
[u_left]
type = DirichletBC
variable = u
value = 0
boundary = 'left'
[]
[u_right]
type = DirichletBC
variable = u
value = 1
boundary = 'right'
[]
[v_left]
type = DirichletBC
variable = v
value = 0
boundary = 'left'
[]
[v_right]
type = DirichletBC
variable = v
value = 1
boundary = 'right'
[]
[]
[Kernels]
[diffusion_u]
type = Diffusion
variable = u
[]
[diffusion_v]
type = Diffusion
variable = v
[]
[]
[RayKernels]
active = 'source'
[source]
type = CoupledLineSourceRayKernelTest
variable = u
coupled = v
[]
[source_ad]
type = ADCoupledLineSourceRayKernelTest
variable = u
coupled = v
[]
[]
[UserObjects/study]
type = RepeatableRayStudy
start_points = '0 0 0
0 4.9 0'
end_points = '5 0 0
4.9 3.9 0'
names = 'ray1 ray2'
execute_on = PRE_KERNELS
[]
[Preconditioning/smp]
type = SMP
full = true
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(modules/ray_tracing/test/tests/vector_postprocessors/per_processor_ray_tracing_results_vector_postprocessor/per_processor_ray_tracing_results_vector_postprocessor.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 5
ny = 2
xmax = 5
ymax = 2
[]
[]
[AuxVariables]
[rays_started]
family = MONOMIAL
order = CONSTANT
[]
[rays_traced]
family = MONOMIAL
order = CONSTANT
[]
[rays_received]
family = MONOMIAL
order = CONSTANT
[]
[rays_sent]
family = MONOMIAL
order = CONSTANT
[]
[intersections]
family = MONOMIAL
order = CONSTANT
[]
[face_hit]
family = MONOMIAL
order = CONSTANT
[]
[vertex_hit]
family = MONOMIAL
order = CONSTANT
[]
[edge_hit]
family = MONOMIAL
order = CONSTANT
[]
[moved_through_neighbors]
family = MONOMIAL
order = CONSTANT
[]
[intersection_calls]
family = MONOMIAL
order = CONSTANT
[]
[vertex_neighbor_lookups]
family = MONOMIAL
order = CONSTANT
[]
[edge_neighbor_lookups]
family = MONOMIAL
order = CONSTANT
[]
[point_neighbor_builds]
family = MONOMIAL
order = CONSTANT
[]
[]
# these results are not output because they cannot be golded against
# but we still make sure they work:
#
# generation_time propagation_time chunks_traced
# buffers_received buffers_sent ray_pool_created
# receive_ray_pool_created receive_buffer_pool_created
[AuxKernels]
[rays_started]
type = VectorPostprocessorVisualizationAux
variable = rays_started
vpp = per_proc_ray_tracing
vector_name = rays_started
execute_on = timestep_end
[]
[rays_traced]
type = VectorPostprocessorVisualizationAux
variable = rays_traced
vpp = per_proc_ray_tracing
vector_name = rays_traced
execute_on = timestep_end
[]
[rays_received]
type = VectorPostprocessorVisualizationAux
variable = rays_received
vpp = per_proc_ray_tracing
vector_name = rays_received
execute_on = timestep_end
[]
[rays_sent]
type = VectorPostprocessorVisualizationAux
variable = rays_sent
vpp = per_proc_ray_tracing
vector_name = rays_sent
execute_on = timestep_end
[]
[intersections]
type = VectorPostprocessorVisualizationAux
variable = intersections
vpp = per_proc_ray_tracing
vector_name = intersections
execute_on = timestep_end
[]
[face_hit]
type = VectorPostprocessorVisualizationAux
variable = face_hit
vpp = per_proc_ray_tracing
vector_name = face_hit
execute_on = timestep_end
[]
[vertex_hit]
type = VectorPostprocessorVisualizationAux
variable = vertex_hit
vpp = per_proc_ray_tracing
vector_name = vertex_hit
execute_on = timestep_end
[]
[edge_hit]
type = VectorPostprocessorVisualizationAux
variable = edge_hit
vpp = per_proc_ray_tracing
vector_name = edge_hit
execute_on = timestep_end
[]
[moved_through_neighbors]
type = VectorPostprocessorVisualizationAux
variable = moved_through_neighbors
vpp = per_proc_ray_tracing
vector_name = moved_through_neighbors
execute_on = timestep_end
[]
[intersection_calls]
type = VectorPostprocessorVisualizationAux
variable = intersection_calls
vpp = per_proc_ray_tracing
vector_name = intersection_calls
execute_on = timestep_end
[]
[vertex_neighbor_lookups]
type = VectorPostprocessorVisualizationAux
variable = vertex_neighbor_lookups
vpp = per_proc_ray_tracing
vector_name = vertex_neighbor_lookups
execute_on = timestep_end
[]
[edge_neighbor_lookups]
type = VectorPostprocessorVisualizationAux
variable = edge_neighbor_lookups
vpp = per_proc_ray_tracing
vector_name = edge_neighbor_lookups
execute_on = timestep_end
[]
[point_neighbor_builds]
type = VectorPostprocessorVisualizationAux
variable = point_neighbor_builds
vpp = per_proc_ray_tracing
vector_name = point_neighbor_builds
execute_on = timestep_end
[]
[]
[UserObjects/lots]
type = LotsOfRaysRayStudy
ray_kernel_coverage_check = false # no need for RayKernels
execute_on = initial
[]
[RayBCs/kill]
type = KillRayBC
boundary = 'top left right bottom'
[]
[VectorPostprocessors/per_proc_ray_tracing]
type = PerProcessorRayTracingResultsVectorPostprocessor
execute_on = timestep_end
study = lots
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Outputs]
exodus = true
[]
(test/tests/mesh_modifiers/subdomain_bounding_box/oriented_subdomain_bounding_box.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
xmin = -6
xmax = 4
nx = 10
ymin = -2
ymax = 10
ny = 12
zmin = -5
zmax = 7
nz = 12
[]
[subdomains]
type = OrientedSubdomainBoundingBoxGenerator
input = gen
center = '-1 4 1'
width = 5
length = 10
height = 4
width_direction = '2 1 0'
length_direction = '-1 2 2'
block_id = 10
[]
[]
[Problem]
type = FEProblem
solve = false
kernel_coverage_check = false
[]
[Variables]
[u]
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
[]
[Outputs]
exodus = true
[]
(test/tests/fvkernels/fv_simple_diffusion/fv_only_refined.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 10
uniform_refine = 1
[]
[Variables]
[v]
family = MONOMIAL
order = CONSTANT
fv = true
[]
[]
[FVKernels]
[diff]
type = FVDiffusion
variable = v
coeff = coeff
[]
[]
[FVBCs]
[left]
type = FVDirichletBC
variable = v
boundary = left
value = 7
[]
[right]
type = FVDirichletBC
variable = v
boundary = right
value = 42
[]
[]
[Materials]
[diff]
type = ADGenericFunctorMaterial
prop_names = 'coeff'
prop_values = '1'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/phase_field/test/tests/grain_tracker_test/grain_tracker_volume_single.i)
# This test calculates the volume of a few simple shapes
# Using the FeatureVolumeVectorPostprocessor
[Mesh]
type = GeneratedMesh
dim = 2
nx = 40
ny = 40
nz = 0
xmin = -2
xmax = 2
ymin = -2
ymax = 2
zmax = 0
elem_type = QUAD4
[]
[Variables]
[./gr0]
[../]
[./gr1]
[../]
[]
[ICs]
[./circle]
type = SmoothCircleIC
x1 = 0
y1 = 0
radius = 1
int_width = 0.01
invalue = 1
outvalue = 0
variable = gr0
[../]
[./boxes]
type = MultiBoundingBoxIC
corners = '-1.5 -0.25 0
1 -0.5 0'
opposite_corners = '-1 0.25 0
2 0.5 0'
inside = 1
outside = 0
variable = gr1
[../]
[]
[Postprocessors]
[./grain_tracker]
type = GrainTracker
variable = 'gr0 gr1'
threshold = 0.1
compute_var_to_feature_map = true
execute_on = 'initial'
[../]
[]
[VectorPostprocessors]
[./grain_volumes]
type = FeatureVolumeVectorPostprocessor
flood_counter = grain_tracker
single_feature_per_element = true
execute_on = 'initial'
[../]
[]
[Executioner]
type = Steady
[./Adaptivity]
initial_adaptivity = 3
refine_fraction = 0.7
coarsen_fraction = 0.1
max_h_level = 3
[../]
[]
[Problem]
solve = false
[]
[Outputs]
exodus = true
csv = true
[]
(modules/richards/test/tests/jacobian_1/jn_fu_03.i)
# unsaturated = false
# gravity = true
# supg = false
# transient = false
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = -1
xmax = 1
ymin = -1
ymax = 1
zmin = -1
zmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGnone
sat_UO = Saturation
seff_UO = SeffVG
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0 # notice small quantity, so the PETSc constant state works
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1 # notice small quantity, so the PETSc constant state works
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.2
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGnone]
type = RichardsSUPGnone
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = RandomIC
block = 0
min = 0
max = 1
[../]
[../]
[]
[Kernels]
active = 'richardsf'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFullyUpwindFlux
variable = pressure
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
viscosity = 1E-3
gravity = '1 2 3'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -snes_type'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000 test'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = jn03
exodus = false
[]
(modules/combined/test/tests/heat_convection/heat_convection_3d_tf_test.i)
# Test cases for convective boundary conditions.
# Input file for htc_3dtest0
# TKLarson
# 11/02/11
# Revision 0
#
# Goals of this test are:
# 1) show that the 'fluid' temperature for convective boundary condition
# is behaving as expected/desired
# 2) show that expected results ensue from application of convective boundary conditions
# Convective boundary condition:
# q = h*A*(Tw - Tf)
# where
# q - heat transfer rate (w)
# h - heat transfer coefficient (w/m^2-K)
# A - surface area (m^2)
# Tw - surface temperature (K)
# Tf - fluid temperature adjacent to the surface (K)
# The heat transfer coefficient (h) is input as a variable called 'rate'
# Tf is a two valued function specified by 'initial' and 'final' along with a variable
# called 'duration,' the length of time in seconds that it takes initial to linearly ramp
# to 'final.'
# The mesh for this test case is concocted from an ASTM standard for the so-called Brazillian Cylinder test
# (ASTM International, Standard Test Method for Splitting Tensile Strength of Cylindrical Concrete
# Specimens, C 496/C 496M-04, 2004). I turned a cylinder model into a rectangular parallelpiped,
# because I already had the cylinder model.
# The model is 3-d xyz coordinates.
#
# Brazillian Parallelpiped sample dimensions:
# z = 10.3 cm, 0.103 m, (4 in)
# y = 5.08 cm, 0.0508 m, (2 in)
# x = 5.08 cm, 0.0508 m, (2 in)
# Material properties are:
# density = 2405.28 km/m^3
# specific heat = 826.4 J/kg-K
# thermal conductivity 1.937 w/m-K
# alpha (thermal conductivity/(density*specific heat) is then 9.74e-7 m^2/s
#
# Initial parallelpiped temperature is room temperature 294.26 K (70 F)
# The initial fluid temperature is room temperature. We will ramp it to 477.6 K (400 F) in 10 minutes.
# We will use a very large h (1000000) to make the surface temperature mimick the fluid temperature.
# What we expect for this problem:
# 1) Use of h = 1000000 should cause the parallelpiped surface temperature to track the fluid temperature
# 2) The fluid temperature should rise from initial (294.26 K) to final (477.6 K) in 600 s.
# 3) 1) and 2) should prove that the Tf boundary condition is ramping as desired.
# Note, we do the above because there is no way to plot a variable that is not on a mesh node!
[Mesh] # Mesh Start
# 5cm x 5cm x 10cm parallelpiped not so detailed mesh, 4 elements each end, 8 elements each long face
# Only one block (Block 1), all concrete
# Sideset definitions:
# 1 - xy plane at z=0,
# 2 - xy plane at z=-0.103,
# 3 - xz plane at y=0,
# 4 - yz plane at x=0,
# 5 - xz plane at y=0.0508,
# 6 - yz plane at x=0.0508
file = heat_convection_3d_mesh.e
#
[] # Mesh END
[Variables] # Variables Start
[./temp]
order = FIRST
family = LAGRANGE
initial_condition = 294.26 # Initial parallelpiped temperature
[../]
[] # Variables END
[Kernels] # Kernels Start
[./heat]
# type = HeatConductionRZ
type = HeatConduction
variable = temp
[../]
[./heat_ie]
# type = HeatConductionTimeDerivativeRZ
type = HeatConductionTimeDerivative
variable = temp
[../]
[] # Kernels END
[BCs] # Boundary Conditions Start
# Heat transfer coefficient on outer parallelpiped radius and ends
[./convective_clad_surface] # Convective Start
# type = ConvectiveFluxRZ # Convective flux, e.g. q'' = h*(Tw - Tf)
type = ConvectiveFluxBC # Convective flux, e.g. q'' = h*(Tw - Tf)
boundary = '1 2 3 4 5 6' # BC applied on top, along length, and bottom
variable = temp
rate = 1000000. # convective heat transfer coefficient (w/m^2-K)[176000 "]
# # the above h is ~ infinity for present purposes
initial = 294.26 # initial ambient (lab or oven) temperature (K)
final = 477.6 # final ambient (lab or oven) temperature (K)
duration = 600. # length of time in seconds that it takes the ambient
# temperature to ramp from initial to final
[../] # Convective End
[] # BCs END
[Materials] # Materials Start
[./thermal]
type = HeatConductionMaterial
block = 1
specific_heat = 826.4
thermal_conductivity = 1.937 # this makes alpha 9.74e-7 m^2/s
[../]
[./density]
type = Density
block = 1
density = 2405.28
[../]
[] # Materials END
[Executioner] # Executioner Start
type = Transient
# type = Steady
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew '
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type'
petsc_options_value = '70 hypre boomeramg'
l_max_its = 60
nl_rel_tol = 1e-8
nl_abs_tol = 1e-10
l_tol = 1e-5
start_time = 0.0
dt = 60.
num_steps = 20 # Total run time 1200 s
[] # Executioner END
[Outputs] # Output Start
# Output Start
file_base = out_3d_tf
exodus = true
[] # Output END
# # Input file END
(test/tests/misc/check_error/subdomain_restricted_auxkernel_mismatch.i)
[Mesh]
file = rectangle.e
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./foo]
order = FIRST
family = LAGRANGE
block = 1
[../]
[]
[Kernels]
active = 'diff body_force'
[./diff]
type = Diffusion
variable = u
[../]
[./body_force]
type = BodyForce
variable = u
block = 1
value = 10
[../]
[]
[AuxKernels]
[./foo]
type = ConstantAux
variable = foo
value = 1
block = 2
[../]
[]
[BCs]
active = 'right'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
# petsc_options = '-snes_mf_operator'
# petsc_options_iname = '-pc_type -pc_hypre_type'
# petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
file_base = out
exodus = true
[]
(tutorials/darcy_thermo_mech/step03_darcy_material/problems/step3.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 100
ny = 10
xmax = 0.304 # Length of test chamber
ymax = 0.0257 # Test chamber radius
[]
[Variables/pressure]
[]
[Kernels]
[darcy_pressure]
type = DarcyPressure
variable = pressure
[]
[]
[BCs]
[inlet]
type = DirichletBC
variable = pressure
boundary = left
value = 4000 # (Pa) From Figure 2 from paper. First data point for 1mm spheres.
[]
[outlet]
type = DirichletBC
variable = pressure
boundary = right
value = 0 # (Pa) Gives the correct pressure drop from Figure 2 for 1mm spheres
[]
[]
[Materials]
[column]
type = PackedColumn
[]
[]
[Problem]
type = FEProblem
coord_type = RZ
rz_coord_axis = X
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/dirackernels/point_caching/point_caching_uniform_refinement.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
elem_type = QUAD4
uniform_refine = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[DiracKernels]
active = 'point_source'
[./point_source]
type = CachingPointSource
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Adaptivity]
steps = 2
marker = uniform
[./Markers]
[./uniform]
type = UniformMarker
mark = refine
[../]
[../]
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(test/tests/misc/selective_reinit/selective_reinit_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./dummy]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./constant_dummy]
type = ConstantAux
variable = dummy
execute_on = 'initial timestep_end'
value = 4
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Postprocessors]
[./u_integral]
type = ElementIntegralVariablePostprocessor
variable = u
execute_on = linear
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Adaptivity]
[./Indicators]
[./indicator]
type = GradientJumpIndicator
variable = u
[../]
[../]
[./Markers]
[./box]
type = BoxMarker
bottom_left = '0.2 0.2 0'
top_right = '0.8 0.8 0'
inside = refine
outside = coarsen
[../]
[../]
[]
[Outputs]
exodus = true
show = u
[]
[LotsOfAuxVariables]
[./avar]
number = 20
[../]
[]
(modules/combined/test/tests/eigenstrain/inclusion.i)
# This test allows comparison of simulation and analytical solution for a misfitting precipitate
# using ComputeVariableEigenstrain for the simulation and the InclusionProperties material
# for the analytical solution. Increasing mesh resolution will improve agreement.
[Mesh]
type = GeneratedMesh
dim = 2
nx = 40
ny = 40
xmax = 1.5
ymax = 1.5
elem_type = QUAD4
[]
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./TensorMechanics]
[../]
[]
[AuxVariables]
[./s11_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./s12_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./s22_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./s11_an]
order = CONSTANT
family = MONOMIAL
[../]
[./s12_an]
order = CONSTANT
family = MONOMIAL
[../]
[./s22_an]
order = CONSTANT
family = MONOMIAL
[../]
[./e11_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./e12_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./e22_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./e11_an]
order = CONSTANT
family = MONOMIAL
[../]
[./e12_an]
order = CONSTANT
family = MONOMIAL
[../]
[./e22_an]
order = CONSTANT
family = MONOMIAL
[../]
[./fel_an]
order = CONSTANT
family = MONOMIAL
[../]
[./c]
[../]
[]
[AuxKernels]
[./matl_s11]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 0
variable = s11_aux
[../]
[./matl_s12]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 1
variable = s12_aux
[../]
[./matl_s22]
type = RankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 1
variable = s22_aux
[../]
[./matl_s11_an]
type = RankTwoAux
rank_two_tensor = stress_an
index_i = 0
index_j = 0
variable = s11_an
[../]
[./matl_s12_an]
type = RankTwoAux
rank_two_tensor = stress_an
index_i = 0
index_j = 1
variable = s12_an
[../]
[./matl_s22_an]
type = RankTwoAux
rank_two_tensor = stress_an
index_i = 1
index_j = 1
variable = s22_an
[../]
[./matl_e11]
type = RankTwoAux
rank_two_tensor = total_strain
index_i = 0
index_j = 0
variable = e11_aux
[../]
[./matl_e12]
type = RankTwoAux
rank_two_tensor = total_strain
index_i = 0
index_j = 1
variable = e12_aux
[../]
[./matl_e22]
type = RankTwoAux
rank_two_tensor = total_strain
index_i = 1
index_j = 1
variable = e22_aux
[../]
[./matl_e11_an]
type = RankTwoAux
rank_two_tensor = strain_an
index_i = 0
index_j = 0
variable = e11_an
[../]
[./matl_e12_an]
type = RankTwoAux
rank_two_tensor = strain_an
index_i = 0
index_j = 1
variable = e12_an
[../]
[./matl_e22_an]
type = RankTwoAux
rank_two_tensor = strain_an
index_i = 1
index_j = 1
variable = e22_an
[../]
[./matl_fel_an]
type = MaterialRealAux
variable = fel_an
property = fel_an_mat
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeElasticityTensor
block = 0
C_ijkl = '1 1'
fill_method = symmetric_isotropic
[../]
[./stress]
type = ComputeLinearElasticStress
block = 0
[../]
[./var_dependence]
type = DerivativeParsedMaterial
block = 0
function = 0.005*c^2
args = c
outputs = exodus
output_properties = 'var_dep'
f_name = var_dep
enable_jit = true
derivative_order = 2
[../]
[./eigenstrain]
type = ComputeVariableEigenstrain
block = 0
eigen_base = '1 1 0 0 0 0'
prefactor = var_dep
args = c
eigenstrain_name = eigenstrain
[../]
[./strain]
type = ComputeSmallStrain
block = 0
displacements = 'disp_x disp_y'
eigenstrain_names = eigenstrain
[../]
[./analytical]
type = InclusionProperties
a = 0.1
b = 0.1
lambda = 1
mu = 1
misfit_strains = '0.005 0.005'
strain_name = strain_an
stress_name = stress_an
energy_name = fel_an_mat
[../]
[]
[BCs]
active = 'left_x bottom_y'
[./bottom_y]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0
[../]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = left
value = 0
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart'
petsc_options_value = 'hypre boomeramg 31'
l_max_its = 30
nl_max_its = 10
nl_rel_tol = 1.0e-10
[]
[Outputs]
exodus = true
[]
[ICs]
[./c_IC]
int_width = 0.075
x1 = 0
y1 = 0
radius = 0.1
outvalue = 0
variable = c
invalue = 1
type = SmoothCircleIC
[../]
[]
(test/tests/partitioners/random_partitioner/random_partitioner.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[Partitioner]
type = RandomPartitioner
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
[AuxVariables]
[pid]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[pid_aux]
type = ProcessorIDAux
variable = pid
execute_on = 'INITIAL'
[]
[]
(test/tests/multiapps/picard/picard_custom_postprocessor.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
parallel_type = replicated
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./v]
[../]
[]
[Kernels]
[./diff]
type = CoefDiffusion
variable = u
coef = 0.1
[../]
[./force_u]
type = CoupledForce
variable = u
v = v
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Postprocessors]
[./unorm_begin]
type = ElementL2Norm
variable = u
execute_on = 'initial timestep_begin'
outputs = none
[../]
[./unorm]
type = ElementL2Norm
variable = u
execute_on = 'initial timestep_end'
[../]
[./unorm_err]
type = RelativeDifferencePostprocessor
value1 = unorm
value2 = unorm_begin
outputs = none
[../]
[./vnorm]
type = ElementL2Norm
variable = v
execute_on = 'initial timestep_end'
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
fixed_point_max_its = 30
disable_fixed_point_residual_norm_check = true
custom_pp = unorm_err
nl_abs_tol = 1e-14
[]
[Outputs]
exodus = true
[]
[MultiApps]
[./sub]
type = FullSolveMultiApp
input_files = steady_picard_sub.i
no_backup_and_restore = true
[../]
[]
[Transfers]
[./v_from_sub]
type = MultiAppNearestNodeTransfer
from_multi_app = sub
source_variable = v
variable = v
[../]
[./u_to_sub]
type = MultiAppNearestNodeTransfer
to_multi_app = sub
source_variable = u
variable = u
[../]
[]
(test/tests/functions/parsed/steady.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
initial_condition = 2
[../]
[]
[Functions]
[./right_bc]
type = ParsedFunction
value = a+1
vals = left_avg
vars = a
[../]
[./left_bc]
type = ParsedFunction
value = a
vals = left_avg
vars = a
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = FunctionDirichletBC
variable = u
boundary = left
function = left_bc
[../]
[./right]
type = FunctionDirichletBC
variable = u
boundary = 'right right'
function = right_bc
[../]
[]
[Postprocessors]
[./left_avg]
type = SideAverageValue
variable = u
execute_on = initial
boundary = left
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/utils/perf_graph_live_print/perf_graph_live_print.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Problem]
type = SlowProblem
seconds_to_sleep = 8
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
perf_graph_live_time_limit = 1
exodus = true
[]
(modules/tensor_mechanics/test/tests/action/material_output_first_lagrange_automatic.i)
# This input file is designed to test adding extra stress to ADComputeLinearElasticStress
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmax = 50
ymax = 50
[]
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Modules/TensorMechanics/Master/All]
strain = SMALL
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx hydrostatic_stress vonmises_stress'
material_output_order = 'CONSTANT CONSTANT CONSTANT CONSTANT CONSTANT CONSTANT CONSTANT FIRST'
material_output_family = 'MONOMIAL MONOMIAL MONOMIAL MONOMIAL MONOMIAL MONOMIAL MONOMIAL LAGRANGE'
use_automatic_differentiation = true
[]
[Materials]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0
[]
[stress]
type = ADComputeLinearElasticStress
extra_stress_names = 'stress_one stress_two'
[]
[stress_one]
type = GenericConstantRankTwoTensor
tensor_name = stress_one
tensor_values = '0 1e3 1e3 1e3 0 1e3 1e3 1e3 0'
[]
[stress_two]
type = GenericConstantRankTwoTensor
tensor_name = stress_two
tensor_values = '1e3 0 0 0 1e3 0 0 0 1e3'
[]
[]
[BCs]
[disp_x_BC]
type = ADDirichletBC
variable = disp_x
boundary = 'bottom top'
value = 0.5
[]
[disp_x_BC2]
type = ADDirichletBC
variable = disp_x
boundary = 'left right'
value = 0.01
[]
[disp_y_BC]
type = ADDirichletBC
variable = disp_y
boundary = 'bottom top'
value = 0.8
[]
[disp_y_BC2]
type = ADDirichletBC
variable = disp_y
boundary = 'left right'
value = 0.02
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Postprocessors]
[hydrostatic]
type = ElementAverageValue
variable = hydrostatic_stress
[]
[von_mises]
type = NodalVariableValue
variable = vonmises_stress
nodeid = 0
[]
[]
[Outputs]
exodus = true
[]
(test/tests/vectorpostprocessors/intersection_points_along_line/3d.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 10
ny = 10
nz = 10
# Ray tracing code is not yet compatible with DistributedMesh
parallel_type = replicated
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[VectorPostprocessors]
[./intersections]
type = IntersectionPointsAlongLine
start = '0.05 0.05 0.05'
end = '0.05 0.05 0.405'
[../]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Outputs]
csv = true
[]
(modules/tensor_mechanics/test/tests/ad_linear_elasticity/tensor.i)
# This input file is designed to test the RankTwoAux and RankFourAux
# auxkernels, which report values out of the Tensors used in materials
# properties.
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
xmax = 2
ymax = 2
[]
[Variables]
[./diffused]
[./InitialCondition]
type = RandomIC
[../]
[../]
[]
[AuxVariables]
[./C11]
order = CONSTANT
family = MONOMIAL
[../]
[./C12]
order = CONSTANT
family = MONOMIAL
[../]
[./C13]
order = CONSTANT
family = MONOMIAL
[../]
[./C14]
order = CONSTANT
family = MONOMIAL
[../]
[./C15]
order = CONSTANT
family = MONOMIAL
[../]
[./C16]
order = CONSTANT
family = MONOMIAL
[../]
[./C22]
order = CONSTANT
family = MONOMIAL
[../]
[./C23]
order = CONSTANT
family = MONOMIAL
[../]
[./C24]
order = CONSTANT
family = MONOMIAL
[../]
[./C25]
order = CONSTANT
family = MONOMIAL
[../]
[./C26]
order = CONSTANT
family = MONOMIAL
[../]
[./C33]
order = CONSTANT
family = MONOMIAL
[../]
[./C34]
order = CONSTANT
family = MONOMIAL
[../]
[./C35]
order = CONSTANT
family = MONOMIAL
[../]
[./C36]
order = CONSTANT
family = MONOMIAL
[../]
[./C44]
order = CONSTANT
family = MONOMIAL
[../]
[./C45]
order = CONSTANT
family = MONOMIAL
[../]
[./C46]
order = CONSTANT
family = MONOMIAL
[../]
[./C55]
order = CONSTANT
family = MONOMIAL
[../]
[./C56]
order = CONSTANT
family = MONOMIAL
[../]
[./C66]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Modules/TensorMechanics/Master/All]
strain = SMALL
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx'
use_automatic_differentiation = true
[]
[Kernels]
[./diff]
type = ADDiffusion
variable = diffused
[../]
[]
[AuxKernels]
[./matl_C11]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 0
variable = C11
[../]
[./matl_C12]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 1
index_l = 1
variable = C12
[../]
[./matl_C13]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 2
index_l = 2
variable = C13
[../]
[./matl_C14]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 1
index_l = 2
variable = C14
[../]
[./matl_C15]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 2
variable = C15
[../]
[./matl_C16]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 1
variable = C16
[../]
[./matl_C22]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 1
index_l = 1
variable = C22
[../]
[./matl_C23]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 2
index_l = 2
variable = C23
[../]
[./matl_C24]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 1
index_l = 2
variable = C24
[../]
[./matl_C25]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 0
index_l = 2
variable = C25
[../]
[./matl_C26]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 0
index_l = 1
variable = C26
[../]
[./matl_C33]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 2
index_l = 2
variable = C33
[../]
[./matl_C34]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 1
index_l = 2
variable = C34
[../]
[./matl_C35]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 0
index_l = 2
variable = C35
[../]
[./matl_C36]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 0
index_l = 1
variable = C36
[../]
[./matl_C44]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 2
index_k = 1
index_l = 2
variable = C44
[../]
[./matl_C45]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 2
index_k = 0
index_l = 2
variable = C45
[../]
[./matl_C46]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 2
index_k = 0
index_l = 1
variable = C46
[../]
[./matl_C55]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 2
index_k = 0
index_l = 2
variable = C55
[../]
[./matl_C56]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 2
index_k = 0
index_l = 1
variable = C56
[../]
[./matl_C66]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 1
index_k = 0
index_l = 1
variable = C66
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeElasticityTensor
fill_method = symmetric21
C_ijkl ='1111 1122 1133 1123 1113 1112 2222 2233 2223 2213 2212 3333 3323 3313 3312 2323 2313 2312 1313 1312 1212'
[../]
[./stress]
type = ADComputeLinearElasticStress
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = diffused
boundary = 'right'
value = 1
[../]
[./top]
type = DirichletBC
variable = diffused
boundary = 'top'
value = 0
[../]
[./disp_x_BC]
type = DirichletBC
variable = disp_x
boundary = 'bottom top'
value = 0.5
[../]
[./disp_x_BC2]
type = DirichletBC
variable = disp_x
boundary = 'left right'
value = 0.01
[../]
[./disp_y_BC]
type = DirichletBC
variable = disp_y
boundary = 'bottom top'
value = 0.8
[../]
[./disp_y_BC2]
type = DirichletBC
variable = disp_y
boundary = 'left right'
value = 0.02
[../]
[]
[Preconditioning]
[./full]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/quadrature/order/block-order.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 1
ny = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 2
[]
[bottom]
type = SubdomainBoundingBoxGenerator
input = gmg
block_id = 1
bottom_left = '0 0 0'
top_right = '1 1 0'
[]
[top]
type = SubdomainBoundingBoxGenerator
input = bottom
block_id = 2
bottom_left = '0 1 0'
top_right = '1 2 0'
[]
[middle]
type = SideSetsBetweenSubdomainsGenerator
input = top
primary_block = 1
paired_block = 2
new_boundary = middle
[]
[]
[Postprocessors]
[block1_qps]
type = NumElemQPs
block = 1
[]
[block2_qps]
type = NumElemQPs
block = 2
[]
[top_side_qps]
type = NumSideQPs
boundary = top
[]
[bottom_side_qps]
type = NumSideQPs
boundary = bottom
[]
[middle_side_qps]
type = NumSideQPs
boundary = middle
[]
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
[Quadrature]
custom_blocks = '1 2'
custom_orders = 'first second'
[]
[]
[Outputs]
execute_on = 'timestep_end'
exodus = false
csv = true
[]
(test/tests/auxkernels/ghosting_aux/no_algebraic_ghosting.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[Partitioner]
type = GridPartitioner
nx = 2
ny = 2
[]
output_ghosting = true
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
[AuxVariables]
[pid]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[pid]
type = ProcessorIDAux
variable = pid
[]
[]
[Problem]
default_ghosting = false
[]
(test/tests/reporters/mesh_info/mesh_info.i)
[Mesh]
parallel_type = DISTRIBUTED
[generate]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
# For consistent partitioning across platforms
[Partitioner]
type = GridPartitioner
nx = 2
ny = 1
[]
[]
[Adaptivity]
initial_marker = marker
[Markers/marker]
type = BoxMarker
bottom_left = '0 0 0'
top_right = '1 0.5 0'
inside = 'refine'
outside = 'do_nothing'
[]
[]
[Variables/u]
[]
[Executioner]
type = Steady
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[Reporters/mesh_info]
type = MeshInfo
[]
[Outputs]
[out]
type = JSON
execute_system_information_on = NONE
[]
[]
(test/tests/mortar/1d/1d.i)
[Mesh]
file = 2-lines.e
construct_side_list_from_node_list = true
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
block = '1 2'
[../]
[./lm]
order = FIRST
family = SCALAR
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[ScalarKernels]
[./ced]
type = NodalEqualValueConstraint
variable = lm
var = u
boundary = '100 101'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = '1'
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = '2'
value = 3
[../]
[./evc1]
type = OneDEqualValueConstraintBC
variable = u
boundary = '100'
lambda = lm
component = 0
vg = 1
[../]
[./evc2]
type = OneDEqualValueConstraintBC
variable = u
boundary = '101'
lambda = lm
component = 0
vg = -1
[../]
[]
[Preconditioning]
[./fmp]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/reactor/test/tests/meshgenerators/coarse_mesh_extra_element_id_generator/coarse_elem_subdomain_id.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 8
ymin = 0
ymax = 8
nx = 8
ny = 8
[]
[coarse_mesh]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 8
ymin = 0
ymax = 8
nx = 3
ny = 3
subdomain_ids = '0 1 2
3 3 3
4 4 4'
[]
[coarse_id]
type = CoarseMeshExtraElementIDGenerator
input = gmg
coarse_mesh = coarse_mesh
extra_element_id_name = coarse_elem_id
coarse_mesh_extra_element_id = subdomain_id
enforce_mesh_embedding = false
[]
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[AuxVariables]
[coarse_elem_id]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[coarse_elem_id]
type = ExtraElementIDAux
variable = coarse_elem_id
extra_id_name = coarse_elem_id
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/mortar/continuity-3d-non-conforming/continuity_sphere_hex27.i)
[Mesh]
second_order = true
[file]
type = FileMeshGenerator
file = spheres_hex27.e
[]
[secondary]
input = file
type = LowerDBlockFromSidesetGenerator
new_block_id = 11
new_block_name = "secondary"
sidesets = '101'
[]
[primary]
input = secondary
type = LowerDBlockFromSidesetGenerator
new_block_id = 12
new_block_name = "primary"
sidesets = '102'
[]
[]
[Problem]
kernel_coverage_check = false
[]
[Variables]
[T]
block = '1 2'
family = LAGRANGE
order = SECOND
[]
[lambda]
block = 'secondary'
family = LAGRANGE
order = FIRST
[]
[]
[BCs]
[neumann]
type = FunctionGradientNeumannBC
exact_solution = exact_soln_primal
variable = T
boundary = '1 2'
[]
[]
[Kernels]
[conduction]
type = Diffusion
variable = T
block = '1 2'
[]
[sink]
type = Reaction
variable = T
block = '1 2'
[]
[forcing_function]
type = BodyForce
variable = T
function = forcing_function
block = '1 2'
[]
[]
[Functions]
[forcing_function]
type = ParsedFunction
value = 'x^2 + y^2 + z^2 - 6'
[]
[exact_soln_primal]
type = ParsedFunction
value = 'x^2 + y^2 + z^2'
[]
[exact_soln_lambda]
type = ParsedFunction
value = '4'
[]
[]
[Debug]
show_var_residual_norms = 1
[]
[Constraints]
[mortar]
type = EqualValueConstraint
primary_boundary = 2
secondary_boundary = 1
primary_subdomain = '12'
secondary_subdomain = '11'
variable = lambda
secondary_variable = T
correct_edge_dropping = true
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
solve_type = NEWTON
type = Steady
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_shift_type '
'-pc_factor_shift_amount'
petsc_options_value = 'lu basic NONZERO 1e-15'
[]
[Outputs]
exodus = true
[]
[Postprocessors]
[L2lambda]
type = ElementL2Error
variable = lambda
function = exact_soln_lambda
execute_on = 'timestep_end'
block = 'secondary'
[]
[L2u]
type = ElementL2Error
variable = T
function = exact_soln_primal
execute_on = 'timestep_end'
block = '1 2'
[]
[h]
type = AverageElementSize
block = '1 2'
[]
[]
(modules/navier_stokes/test/tests/finite_element/ins/energy_source/steady.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
nx = 16
ny = 16
[]
[./corner_node]
type = ExtraNodesetGenerator
new_boundary = 'pinned_node'
nodes = '0'
input = gen
[../]
[]
[Variables]
[./velocity]
family = LAGRANGE_VEC
[../]
[./p]
[../]
[temperature][]
[]
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[./mass_pspg]
type = INSADMassPSPG
variable = p
[../]
[./momentum_convection]
type = INSADMomentumAdvection
variable = velocity
[../]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
integrate_p_by_parts = true
[../]
[./momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[../]
[./temperature_advection]
type = INSADEnergyAdvection
variable = temperature
[../]
[./temperature_conduction]
type = ADHeatConduction
variable = temperature
thermal_conductivity = 'k'
[../]
[temperature_source]
type = INSADEnergySource
variable = temperature
source_function = 1
[]
[temperature_supg]
type = INSADEnergySUPG
variable = temperature
velocity = velocity
[]
[]
[BCs]
[./no_slip]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom right left'
[../]
[./lid]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'top'
function_x = 'lid_function'
[../]
[./pressure_pin]
type = DirichletBC
variable = p
boundary = 'pinned_node'
value = 0
[../]
[./temperature_hot]
type = DirichletBC
variable = temperature
boundary = 'bottom'
value = 1
[../]
[./temperature_cold]
type = DirichletBC
variable = temperature
boundary = 'top'
value = 0
[../]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu cp k'
prop_values = '1 1 1 .01'
[../]
[ins_mat]
type = INSADStabilized3Eqn
velocity = velocity
pressure = p
temperature = temperature
[]
[]
[Functions]
[./lid_function]
# We pick a function that is exactly represented in the velocity
# space so that the Dirichlet conditions are the same regardless
# of the mesh spacing.
type = ParsedFunction
value = '4*x*(1-x)'
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_levels -ksp_gmres_restart'
petsc_options_value = 'asm 6 200'
line_search = 'none'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
exodus = true
[]
(test/tests/misc/save_in/block-restricted-save-in.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 2
xmax = 2
ny = 2
ymax = 2
[]
[./subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '0 0 0'
top_right = '1 1 0'
block_id = 1
[../]
[./interface]
type = SideSetsBetweenSubdomainsGenerator
input = subdomain1
primary_block = '0'
paired_block = '1'
new_boundary = 'primary0_interface'
[../]
[./break_boundary]
input = interface
type = BreakBoundaryOnSubdomainGenerator
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
block = 0
[../]
[./v]
order = FIRST
family = LAGRANGE
block = 1
[../]
[]
[AuxVariables]
[./vres]
block = 1
[../]
[]
[Kernels]
[./diff_u]
type = CoeffParamDiffusion
variable = u
D = 4
block = 0
[../]
[./diff_v]
type = CoeffParamDiffusion
variable = v
D = 2
block = 1
[../]
[./source_u]
type = BodyForce
variable = u
value = 1
[../]
[]
[InterfaceKernels]
[./interface]
type = PenaltyInterfaceDiffusion
variable = u
neighbor_var = v
boundary = primary0_interface
penalty = 1e6
[../]
[]
[BCs]
[./u]
type = VacuumBC
variable = u
boundary = 'left_to_0 bottom_to_0 right top'
[../]
[./v]
type = VacuumBC
variable = v
boundary = 'left_to_1 bottom_to_1'
save_in = 'vres'
[../]
[]
[Postprocessors]
[./u_int]
type = ElementIntegralVariablePostprocessor
variable = u
block = 0
[../]
[./v_int]
type = ElementIntegralVariablePostprocessor
variable = v
block = 1
[../]
[./vres_int]
type = ElementIntegralVariablePostprocessor
variable = vres
block = 1
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
print_linear_residuals = true
[]
(test/tests/transfers/multiapp_nearest_node_transfer/target_boundary_master.i)
[Mesh]
[drmg]
type = DistributedRectilinearMeshGenerator
dim = 2
nx = 30
ny = 30
xmax = 2
elem_type = QUAD4
partition = square
[]
[]
[Variables]
[u][]
[]
[Kernels]
[conduction]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 1
[]
[right]
type = DirichletBC
variable = u
boundary = 'right'
value = 10
[]
[]
[MultiApps]
[sub]
type = FullSolveMultiApp
app_type = MooseTestApp
input_files = 'target_boundary_sub.i'
positions = '-1.0 0.0 0.0
2. 0.0 0.0'
output_in_position = true
execute_on = 'timestep_end'
[]
[]
[Transfers]
[target_boundary]
type = MultiAppNearestNodeTransfer
source_variable = u
to_multi_app = sub
variable = source
target_boundary = 'right'
[]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-6
[]
[Outputs]
exodus = true
[]
(test/tests/bcs/sideset_from_nodeset/sideset_from_nodeset_test.i)
[Mesh]
file = cube_no_sidesets.e
construct_side_list_from_node_list = true
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = NeumannBC
variable = u
boundary = 3
value = 3
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
file_base = cube_hex_out
exodus = true
[]
(modules/porous_flow/test/tests/flux_limited_TVD_pflow/except05.i)
# Exception test: Dictator cannot determine the FEType and it is not properly specified in the AdvectiveFluxCalculator
[Mesh]
type = GeneratedMesh
dim = 1
[]
[GlobalParams]
gravity = '1 2 3'
PorousFlowDictator = dictator
[]
[Variables]
[pp]
[]
[tracer]
[]
[cm]
family = Monomial
order = constant
[]
[]
[Kernels]
[cm]
type = Diffusion
variable = cm
[]
[]
[Modules]
[FluidProperties]
[the_simple_fluid]
type = SimpleFluidProperties
[]
[]
[]
[PorousFlowUnsaturated]
porepressure = pp
mass_fraction_vars = tracer
fp = the_simple_fluid
[]
[UserObjects]
[dummy_dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp cm'
number_fluid_phases = 1
number_fluid_components = 2
[]
[advective_flux_calculator]
type = PorousFlowAdvectiveFluxCalculatorSaturated
PorousFlowDictator = dummy_dictator
[]
[]
[Materials]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1 0 0 0 2 0 0 0 3'
[]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
(examples/ex14_pps/ex14_compare_solutions_1.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 100
ny = 100
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
parallel_type = replicated # This uses SolutionUserObject which doesn't work with DistributedMesh.
[]
[Variables]
[./forced]
order = THIRD
family = HERMITE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = forced
[../]
[./forcing]
type = BodyForce
variable = forced
function = 'x*x+y*y' # Any object expecting a function name can also receive a ParsedFunction string
[../]
[]
[BCs]
[./all]
type = DirichletBC
variable = forced
boundary = 'bottom right top left'
value = 0
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
xda = true #XDA writes out the perfect internal state of all variables, allowing SolutionUserObject to read back in higher order solutions and adapted meshes
[]
(test/tests/interfaces/jvarmap/parameter_map.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Variables]
[./c0][../]
[./c1][../]
[./c2][../]
[./c3][../]
[./c4][../]
[./c5][../]
[./c6][../]
[./c7][../]
[./c8][../]
[./c9][../]
[./dummy][../]
[]
[Kernels]
[./test1]
type = JvarMapTest
variable = dummy
v0 = 'c0 c1 c2 c3 c4'
v1 = 'c5 c6 c7 c8 c9'
[../]
[./test2]
type = JvarMapTest
variable = dummy
v0 = 'c4 c3 c2 c1 c0'
v1 = 'c9 c8 c7 c6 c5'
[../]
[./test3]
type = JvarMapTest
variable = dummy
v0 = 'c4 c8 c2 c6 c0 c5'
v1 = 'c9 c3 c7 c1'
[../]
[]
[Problem]
solve = false
kernel_coverage_check = false
[]
[Executioner]
type = Steady
[]
(test/tests/executioners/eigen_executioners/normal_eigen_kernel.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 10
ymin = 0
ymax = 10
elem_type = QUAD4
nx = 8
ny = 8
uniform_refine = 0
[]
[Variables]
active = 'u'
[./u]
# second order is way better than first order
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff rea rhs'
[./diff]
type = Diffusion
variable = u
[../]
[./rea]
type = CoefReaction
variable = u
coefficient = 2.0
[../]
[./rhs]
type = MassEigenKernel
variable = u
eigen = false
[../]
[./rea1]
type = CoefReaction
variable = u
coefficient = 1.0
[../]
[]
[BCs]
[./inhomogeneous]
type = DirichletBC
variable = u
boundary = '2 3'
value = 1
[../]
[]
[Executioner]
type = Steady
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
[]
[Postprocessors]
active = 'unorm'
[./unorm]
type = ElementIntegralVariablePostprocessor
variable = u
execute_on = timestep_end
[../]
[]
[Outputs]
file_base = normal_eigen_kernel
exodus = true
[]
(test/tests/mesh/multi_elem_integers/multi_element_integer.i)
[Mesh]
type = MeshGeneratorMesh
parallel_type = 'replicated'
[gmg1]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 5
ny = 5
extra_element_integers = 'material_id'
[]
[gmg2]
type = GeneratedMeshGenerator
dim = 2
xmin = 1
xmax = 2
ymin = 0
ymax = 1
nx = 5
ny = 5
extra_element_integers = 'source_id'
[]
[stitcher]
type = StitchedMeshGenerator
inputs = 'gmg1 gmg2'
stitch_boundaries_pairs = 'right left'
[]
[set_material_id0]
type = SubdomainBoundingBoxGenerator
input = stitcher
bottom_left = '0 0 0'
top_right = '1 1 0'
block_id = 1
location = INSIDE
integer_name = material_id
[]
[set_material_id1]
type = SubdomainBoundingBoxGenerator
input = set_material_id0
bottom_left = '1 0 0'
top_right = '2 1 0'
block_id = 2
location = INSIDE
integer_name = material_id
[]
[set_material_id2]
type = SubdomainBoundingBoxGenerator
input = set_material_id1
bottom_left = '0 0 0'
top_right = '1 1 0'
block_id = 3
location = INSIDE
integer_name = source_id
[]
[set_material_id3]
type = SubdomainBoundingBoxGenerator
input = set_material_id2
bottom_left = '1 0 0'
top_right = '2 1 0'
block_id = 4
location = INSIDE
integer_name = source_id
[]
[]
[AuxVariables]
[id1]
family = MONOMIAL
order = CONSTANT
[]
[id2]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[id1]
type = ElementIntegerAux
variable = id1
integer_names = material_id
[]
[id2]
type = ElementIntegerAux
variable = id2
integer_names = source_id
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/quadrature/order/material_with_order.i)
[Mesh]
[cmg]
type = CartesianMeshGenerator
dim = 2
dx = '1 1 1'
dy = ' 1 1 1'
subdomain_id = '1 2 3
4 5 6
7 8 9'
[]
[]
[Variables]
[u]
order = FIRST
family = L2_LAGRANGE
initial_condition = 1
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[forcing]
type = BodyForce
variable = u
[]
[]
[DGKernels]
[dg_diff]
type = DGDiffusion
variable = u
epsilon = -1
sigma = 6
[]
[test]
type = MatDGKernel
variable = u
mat_prop = dummy
[]
[]
[BCs]
[bc]
type = PenaltyDirichletBC
variable = u
boundary = '0 1 2 3'
penalty = 1e4
value = 0
[]
[]
[Postprocessors]
[block1_qps]
type = NumElemQPs
block = 1
[]
[block5_qps]
type = NumElemQPs
block = 5
[]
[block6_qps]
type = NumElemQPs
block = 6
[]
[]
[Materials]
[dummy]
type = GenericConstantMaterial
block = '1 2 3 4 6 7 8 9'
prop_names = dummy
prop_values = 1
[]
[qordermaterial]
type = QuadratureMaterial
block = 5
property_name = dummy
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
execute_on = 'timestep_end'
csv = true
[]
(modules/tensor_mechanics/test/tests/isotropic_elasticity_tensor/lambda_shear_modulus_test.i)
[Mesh]
type = GeneratedMesh
dim = 3
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[AuxVariables]
[./stress_11]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
add_variables = true
[../]
[]
[AuxKernels]
[./stress_11]
type = RankTwoAux
variable = stress_11
rank_two_tensor = stress
index_j = 1
index_i = 1
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0
[../]
[./left]
type = DirichletBC
variable = disp_x
boundary = left
value = 0
[../]
[./back]
type = DirichletBC
variable = disp_z
boundary = back
value = 0
[../]
[./top]
type = DirichletBC
variable = disp_y
boundary = top
value = 0.001
[../]
[]
[Materials]
[./stress]
type = ComputeLinearElasticStress
[../]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
lambda = 113636
shear_modulus = 454545
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
l_max_its = 20
nl_max_its = 10
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(modules/richards/test/tests/jacobian_1/jn_fu_05.i)
# unsaturated = false
# gravity = false
# supg = true
# transient = false
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = -1
xmax = 1
ymin = -1
ymax = 1
zmin = -1
zmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGstandard
sat_UO = Saturation
seff_UO = SeffVG
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0 # notice small quantity, so the PETSc constant state works
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1 # notice small quantity, so the PETSc constant state works
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.2
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 0.1
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = RandomIC
block = 0
min = 0
max = 1
[../]
[../]
[]
[Kernels]
active = 'richardsf'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFullyUpwindFlux
variable = pressure
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
viscosity = 1E-3
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -snes_type'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000 test'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = jn05
exodus = false
[]
(test/tests/bcs/nodal_normals/cylinder_hexes_2nd.i)
[Mesh]
file = cylinder-hexes-2nd.e
[]
[Functions]
[./all_bc_fn]
type = ParsedFunction
value = x*x+y*y
[../]
[./f_fn]
type = ParsedFunction
value = -4
[../]
[]
[NodalNormals]
boundary = '1'
corner_boundary = 100
order = SECOND
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = f_fn
[../]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
boundary = '1'
function = 'all_bc_fn'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
nl_rel_tol = 1e-13
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/coupled-force/steady-function.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
nx = 16
ny = 16
[]
[./corner_node]
type = ExtraNodesetGenerator
new_boundary = 'pinned_node'
nodes = '0'
input = gen
[../]
[]
[Variables]
[./velocity]
family = LAGRANGE_VEC
[../]
[./p]
[../]
[u]
family = LAGRANGE_VEC
[]
[]
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[./mass_pspg]
type = INSADMassPSPG
variable = p
[../]
[./momentum_convection]
type = INSADMomentumAdvection
variable = velocity
[../]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
integrate_p_by_parts = true
[../]
[momentum_coupled_force]
type = INSADMomentumCoupledForce
variable = velocity
vector_function = 'vector_func'
[]
[./momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[../]
[u_diff]
type = VectorDiffusion
variable = u
[]
[]
[BCs]
[./no_slip]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom right left top'
[../]
[./pressure_pin]
type = DirichletBC
variable = p
boundary = 'pinned_node'
value = 0
[../]
[u_left]
type = VectorFunctionDirichletBC
variable = u
boundary = 'left'
function_x = 1
function_y = 1
[]
[u_right]
type = VectorFunctionDirichletBC
variable = u
boundary = 'right'
function_x = -1
function_y = -1
[]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[ins_mat]
type = INSADTauMaterial
velocity = velocity
pressure = p
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_levels -ksp_gmres_restart'
petsc_options_value = 'asm 6 200'
line_search = 'none'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
exodus = true
[]
[Functions]
[vector_func]
type = ParsedVectorFunction
value_x = '-2*x + 1'
value_y = '-2*x + 1'
[]
[]
(modules/richards/test/tests/kernels/simple_diffusion/simple_diffusion.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/scalar_old_integrity_check.i)
# Test that coupling a time derivative of a scalar variable (ScalarDotCouplingAux) and
# using a Steady executioner errors out
[Mesh]
type = GeneratedMesh
dim = 2
[]
[Functions]
[./a_fn]
type = ParsedFunction
value = t
[../]
[]
[AuxVariables]
[./v]
[../]
[./a]
family = SCALAR
order = FIRST
[../]
[]
[AuxScalarKernels]
[./a_sak]
type = FunctionScalarAux
variable = a
function = a_fn
[../]
[]
[AuxKernels]
[./ak_v]
type = CoupledScalarAux
variable = v
coupled = a
lag = OLD
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./td]
type = TimeDerivative
variable = u
[../]
[]
[Executioner]
type = Steady
[]
(test/tests/mortar/continuity-3d-non-conforming/continuity_non_conforming_tet.i)
[Mesh]
second_order = false
[file]
type = FileMeshGenerator
file = tet_non_mesh.e
[]
[secondary]
input = file
type = LowerDBlockFromSidesetGenerator
new_block_id = 11
new_block_name = "secondary"
sidesets = '101'
[]
[primary]
input = secondary
type = LowerDBlockFromSidesetGenerator
new_block_id = 12
new_block_name = "primary"
sidesets = '102'
[]
[]
[Problem]
kernel_coverage_check = false
[]
[Variables]
[T]
block = '1 2'
[]
[lambda]
block = 'secondary'
[]
[]
[BCs]
[neumann]
type = FunctionGradientNeumannBC
exact_solution = exact_soln_primal
variable = T
boundary = '1 2'
[]
[]
[Kernels]
[conduction]
type = Diffusion
variable = T
block = '1 2'
[]
[sink]
type = Reaction
variable = T
block = '1 2'
[]
[forcing_function]
type = BodyForce
variable = T
function = forcing_function
block = '1 2'
[]
[]
[Functions]
[forcing_function]
type = ParsedFunction
value = 'sin(x*pi)*sin(y*pi)*sin(z*pi) + 3*pi^2*sin(x*pi)*sin(y*pi)*sin(z*pi)'
[]
[exact_soln_primal]
type = ParsedFunction
value = 'sin(x*pi)*sin(y*pi)*sin(z*pi)'
[]
[exact_soln_lambda]
type = ParsedFunction
value = 'pi*sin(pi*y)*sin(pi*z)*cos(pi*x)'
[]
[]
[Debug]
show_var_residual_norms = 1
[]
[Constraints]
[mortar]
type = EqualValueConstraint
primary_boundary = 2
secondary_boundary = 1
primary_subdomain = '12'
secondary_subdomain = '11'
variable = lambda
secondary_variable = T
delta = 0.1
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
solve_type = NEWTON
type = Steady
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_shift_type '
'-pc_factor_shift_amount'
petsc_options_value = 'lu basic NONZERO 1e-15'
[]
[Outputs]
exodus = true
[]
[Postprocessors]
[L2lambda]
type = ElementL2Error
variable = lambda
function = exact_soln_lambda
execute_on = 'timestep_end'
block = 'secondary'
[]
[L2u]
type = ElementL2Error
variable = T
function = exact_soln_primal
execute_on = 'timestep_end'
block = '1 2'
[]
[h]
type = AverageElementSize
block = '1 2'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/3d-rc-no-slip.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
xmin = 0
xmax = 10
ymin = -1
ymax = 1
zmin = -1
zmax = 1
nx = 20
ny = 4
nz = 4
elem_type = TET4
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[GlobalParams]
# retain behavior at time of test creation
two_term_boundary_expansion = false
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
w = w
pressure = pressure
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1e-15
[]
[w]
type = INSFVVelocityVariable
initial_condition = 1e-15
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[w_advection]
type = INSFVMomentumAdvection
variable = v
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'z'
[]
[w_viscosity]
type = INSFVMomentumDiffusion
variable = w
mu = ${mu}
momentum_component = 'z'
[]
[w_pressure]
type = INSFVMomentumPressure
variable = w
momentum_component = 'z'
pressure = pressure
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = '0'
[]
[inlet-w]
type = INSFVInletVelocityBC
boundary = 'left'
variable = w
function = '0'
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom front back'
variable = u
function = 0
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom front back'
variable = v
function = 0
[]
[walls-w]
type = INSFVNoSlipWallBC
boundary = 'top bottom front back'
variable = w
function = 0
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = '0'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type -pc_factor_shift_type'
petsc_options_value = 'lu mumps NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[dof]
type = DOFMap
execute_on = 'initial'
[]
[]
(modules/contact/test/tests/nodal_area/nodal_area_3D.i)
[Mesh]
file = nodal_area_3D.e
[]
[Variables]
[./dummy]
[../]
[]
[AuxVariables]
[./nodal_area]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./dummy]
type = Diffusion
variable = dummy
[../]
[]
[UserObjects]
[./nodal_area]
type = NodalArea
variable = nodal_area
boundary = 1
execute_on = 'initial timestep_end'
[../]
[]
[BCs]
[./dummy]
type = DirichletBC
variable = dummy
boundary = 1
value = 100
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -ksp_gmres_restart'
petsc_options_value = 'jacobi 101'
line_search = 'none'
nl_abs_tol = 1e-11
nl_rel_tol = 1e-10
l_max_its = 20
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/tutorials/basics/part_1.1.i)
#Tensor Mechanics tutorial: the basics
#Step 1, part 1
#2D simulation of uniaxial tension with linear elasticity
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
file = necking_quad4.e
[]
[Modules/TensorMechanics/Master]
[./block1]
strain = SMALL #Small linearized strain, automatically set to XY coordinates
add_variables = true #Add the variables from the displacement string in GlobalParams
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 2.1e5
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./bottom]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./top]
type = DirichletBC
variable = disp_y
boundary = top
value = 0.05
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -sub_pc_type -pc_asm_overlap -ksp_gmres_restart'
petsc_options_value = 'asm lu 1 101'
[]
[Outputs]
exodus = true
perf_graph = true
[]
(test/tests/bcs/matched_value_bc/matched_value_bc_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
# Solves a pair of coupled diffusion equations where u=v on the boundary
[Variables]
active = 'u v'
[./u]
order = FIRST
family = LAGRANGE
initial_condition = 3
[../]
[./v]
order = FIRST
family = LAGRANGE
initial_condition = 2
[../]
[]
[Kernels]
active = 'diff_u diff_v'
[./diff_u]
type = Diffusion
variable = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[BCs]
active = 'right_v left_u'
[./right_v]
type = DirichletBC
variable = v
boundary = 1
value = 3
[../]
[./left_u]
type = MatchedValueBC
variable = u
boundary = 3
v = v
[../]
[]
[Preconditioning]
[./precond]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
nl_rel_tol = 1e-10
l_tol = 1e-12
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/postprocessors/element_extreme_material_property/element_extreme_material_property.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 4
xmin = 0
xmax = 1
[]
[Functions]
[./fn]
type = PiecewiseConstant
axis = x
x = '0 0.25 0.50 0.75'
y = '5 2 3 4'
[../]
[]
[Materials]
[./mat]
type = GenericFunctionMaterial
prop_names = 'mat_prop'
prop_values = 'fn'
[../]
[]
[Postprocessors]
[./min]
type = ElementExtremeMaterialProperty
mat_prop = mat_prop
value_type = min
execute_on = 'INITIAL'
[../]
[./max]
type = ElementExtremeMaterialProperty
mat_prop = mat_prop
value_type = max
execute_on = 'INITIAL'
[../]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
execute_on = 'INITIAL'
[]
(test/tests/userobjects/element_subdomain_modifier/steady.i)
[Problem]
solve = false
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 16
ny = 16
[]
[left]
type = SubdomainBoundingBoxGenerator
input = 'gen'
block_id = 1
bottom_left = '0 0 0'
top_right = '0.25 1 1'
[]
[right]
type = SubdomainBoundingBoxGenerator
input = 'left'
block_id = 2
bottom_left = '0.25 0 0'
top_right = '1 1 1'
[]
[]
[UserObjects]
[moving_circle]
type = CoupledVarThresholdElementSubdomainModifier
coupled_var = 'phi'
block = 2
criterion_type = BELOW
threshold = 0
subdomain_id = 1
moving_boundary_name = moving_boundary
execute_on = 'INITIAL'
[]
[]
[Functions]
[moving_circle]
type = ParsedFunction
value = '(x-t)^2+(y)^2-0.5^2'
[]
[]
[AuxVariables]
[phi]
[]
[]
[AuxKernels]
[phi]
type = FunctionAux
variable = phi
function = moving_circle
execute_on = 'INITIAL'
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/thermal_hydraulics/test/tests/postprocessors/function_side_integral_rz/err.rz_domain.i)
[Mesh]
[mg]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 2
[]
[]
[Problem]
coord_type = RSPHERICAL
[]
[Postprocessors]
[el_int]
type = FunctionSideIntegralRZ
boundary = right
axis_point = '0 0 0'
axis_dir = '0 1 0'
function = 1
execute_on = 'initial'
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
(test/tests/bcs/coupled_var_neumann/coupled_var_neumann.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 10
ny = 10
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxVariables]
[./coupled_bc_var]
[../]
[]
[ICs]
[./coupled_bc_var]
type = FunctionIC
variable = coupled_bc_var
function = set_coupled_bc_var
[../]
[]
[Functions]
[./set_coupled_bc_var]
type = ParsedFunction
value = 'y - 0.5'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = CoupledVarNeumannBC
variable = u
boundary = 1
v = coupled_bc_var
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/lid-driven/lid-driven-with-energy.i)
mu = 1
rho = 1
k = .01
cp = 1
velocity_interp_method = 'rc'
advected_interp_method = 'average'
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 32
ny = 32
[]
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
[]
[vel_y]
type = INSFVVelocityVariable
[]
[pressure]
type = INSFVPressureVariable
[]
[T_fluid]
type = INSFVEnergyVariable
[]
[lambda]
family = SCALAR
order = FIRST
[]
[]
[AuxVariables]
[U]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[]
[AuxKernels]
[mag]
type = VectorMagnitudeAux
variable = U
x = vel_x
y = vel_y
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[mean_zero_pressure]
type = FVScalarLagrangeMultiplier
variable = pressure
lambda = lambda
[]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
[]
[temp_conduction]
type = FVDiffusion
coeff = 'k'
variable = T_fluid
[]
[temp_advection]
type = INSFVEnergyAdvection
variable = T_fluid
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
[]
[]
[FVBCs]
[top_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'top'
function = 'lid_function'
[]
[no_slip_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'left right bottom'
function = 0
[]
[no_slip_y]
type = INSFVNoSlipWallBC
variable = vel_y
boundary = 'left right top bottom'
function = 0
[]
[T_hot]
type = FVDirichletBC
variable = T_fluid
boundary = 'bottom'
value = 1
[]
[T_cold]
type = FVDirichletBC
variable = T_fluid
boundary = 'top'
value = 0
[]
[]
[Materials]
[functor_constants]
type = ADGenericFunctorMaterial
prop_names = 'cp k'
prop_values = '${cp} ${k}'
[]
[ins_fv]
type = INSFVEnthalpyMaterial
temperature = 'T_fluid'
rho = ${rho}
[]
[]
[Functions]
[lid_function]
type = ParsedFunction
value = '4*x*(1-x)'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 300 lu NONZERO'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(test/tests/kernels/diffusion_with_hanging_node/simple_diffusion.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 1
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
# BCs cannot be preset due to Jacobian test
[./left]
type = DirichletBC
preset = false
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
preset = false
variable = u
boundary = right
value = 1
[../]
[]
[Preconditioning]
[./pre]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options = '-pc_svd_monitor -ksp_view_pmat'
petsc_options_iname = '-pc_type'
petsc_options_value = 'svd'
[]
[Outputs]
exodus = true
[]
[Adaptivity]
marker = box
max_h_level = 1
initial_steps = 1
[./Markers]
[./box]
type = BoxMarker
bottom_left = '0.5 0 0'
top_right = '1 1 0'
inside = 'refine'
outside = 'do_nothing'
[../]
[../]
[]
(test/tests/outputs/vpp_as_reporter/vpp_as_reporter.i)
[Mesh/gen]
type = GeneratedMeshGenerator
dim = 1
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[VectorPostprocessors/data]
type = ConstantVectorPostprocessor
vector_names = 'vector'
value = '1949 1954 1977 1980'
[]
[Outputs]
[out]
type = JSON
vectorpostprocessors_as_reporters = true
execute_system_information_on = none
[]
[]
(test/tests/mesh_modifiers/mesh_extruder/extruder_angle.i)
[Mesh]
[file]
type = FileMeshGenerator
file = chimney_quad.e
[]
[extrude]
type = MeshExtruderGenerator
input = file
num_layers = 20
extrusion_vector = '1e-2 1e-2 0'
bottom_sideset = '10'
top_sideset = '20'
[]
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[bottom]
type = DirichletBC
variable = u
boundary = 10
value = 0
[]
[top]
type = DirichletBC
variable = u
boundary = 20
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out_quad_angle
exodus = true
[]
(test/tests/parser/param_substitution/param_substitution.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
# Here we use the GetPot "DBE" function to perform a substitution.
# The parameter "FILENAME" can either exist in this file or
# be provided on the CLI
file_base = out_${FILENAME}
[]
(modules/thermal_hydraulics/test/tests/materials/ad_reynolds_number/test.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
allow_renumbering = false
[]
[Variables]
[arhoA]
[]
[arhouA]
[]
[arhoEA]
[]
[]
[AuxVariables]
[Re]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[Re_ak]
type = ADMaterialRealAux
variable = Re
property = my_Re
[]
[]
[Materials]
[rho_mat]
type = ADConstantMaterial
property_name = rho
value = 1000
[]
[vel_mat]
type = ADConstantMaterial
property_name = vel
value = 5
[]
[D_h_mat]
type = ADConstantMaterial
property_name = D_h
value = 0.002
[]
[mu_mat]
type = ADConstantMaterial
property_name = mu
value = 0.1
[]
[Re_material]
type = ADReynoldsNumberMaterial
Re = my_Re
rho = rho
vel = vel
D_h = D_h
mu = mu
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[Re]
type = ElementalVariableValue
elementid = 0
variable = Re
[]
[]
[Outputs]
csv = true
execute_on = timestep_end
[]
(test/tests/interfaces/reporterinterface/ri_errors.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
[]
[]
[UserObjects]
[error_test]
type = ReporterInterfaceErrorTest
reporter = dummy/value
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
(test/tests/meshgenerators/combiner_generator/combiner_multi_input_translate_from_file.i)
[Mesh]
[gen1]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[gen2]
type = GeneratedMeshGenerator
dim = 2
nx = 12
ny = 12
[]
[gen3]
type = GeneratedMeshGenerator
dim = 2
nx = 14
ny = 14
[]
[cmbn]
type = CombinerGenerator
inputs = 'gen1 gen2 gen3'
positions_file = 'positions.txt'
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/porosity_jump/1d-rc-epsjump.i)
mu=1.1
rho=1.1
advected_interp_method='upwind'
velocity_interp_method='rc'
[Mesh]
[mesh]
type = CartesianMeshGenerator
dim = 1
dx = '1 1'
ix = '30 30'
subdomain_id = '1 2'
[]
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = PINSFVRhieChowInterpolator
u = u
pressure = pressure
porosity = porosity
[]
[]
[Variables]
[u]
type = PINSFVSuperficialVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[AuxVariables]
[porosity]
family = MONOMIAL
order = CONSTANT
fv = true
[]
[]
[ICs]
inactive = 'porosity_continuous'
[porosity_1]
type = ConstantIC
variable = porosity
block = 1
value = 1
[]
[porosity_2]
type = ConstantIC
variable = porosity
block = 2
value = 0.5
[]
[porosity_continuous]
type = FunctionIC
variable = porosity
block = '1 2'
function = smooth_jump
[]
[]
[Functions]
[smooth_jump]
type = ParsedFunction
value = '1 - 0.5 * 1 / (1 + exp(-30*(x-1)))'
[]
[]
[FVKernels]
[mass]
type = PINSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = PINSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
porosity = porosity
momentum_component = 'x'
[]
[u_viscosity]
type = PINSFVMomentumDiffusion
variable = u
mu = ${mu}
porosity = porosity
momentum_component = 'x'
[]
[u_pressure]
type = PINSFVMomentumPressure
variable = u
pressure = pressure
porosity = porosity
momentum_component = 'x'
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = '1'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
[]
[Postprocessors]
[inlet_p]
type = SideAverageValue
variable = 'pressure'
boundary = 'left'
[]
[outlet-u]
type = SideIntegralVariablePostprocessor
variable = u
boundary = 'right'
[]
[]
[Outputs]
exodus = true
csv = false
[]
(modules/navier_stokes/test/tests/finite_volume/ins/mms/skew-correction/skewed-vortex.i)
mu=1.0
rho=1.0
[Problem]
coord_type = 'XYZ'
error_on_jacobian_nonzero_reallocation = true
[]
[Mesh]
[gen_mesh]
type = FileMeshGenerator
file = skewed.msh
[]
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = 1
face_interp_method = 'skewness-corrected'
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 1
face_interp_method = 'skewness-corrected'
[]
[pressure]
type = INSFVPressureVariable
face_interp_method = 'skewness-corrected'
[]
[lambda]
family = SCALAR
order = FIRST
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = 'skewness-corrected'
velocity_interp_method = 'rc'
rho = ${rho}
[]
[mean_zero_pressure]
type = FVScalarLagrangeMultiplier
variable = pressure
lambda = lambda
[]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
advected_interp_method = 'skewness-corrected'
velocity_interp_method = 'rc'
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
[]
[u_forcing]
type = INSFVBodyForce
variable = vel_x
functor = forcing_u
momentum_component = 'x'
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
advected_interp_method = 'skewness-corrected'
velocity_interp_method = 'rc'
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
[]
[v_forcing]
type = INSFVBodyForce
variable = vel_y
functor = forcing_v
momentum_component = 'y'
[]
[]
[FVBCs]
[no-slip-wall-u]
type = INSFVNoSlipWallBC
boundary = 'left right top bottom'
variable = vel_x
function = '0'
[]
[no-slip-wall-v]
type = INSFVNoSlipWallBC
boundary = 'left right top bottom'
variable = vel_y
function = '0'
[]
[]
[Functions]
[exact_u]
type = ParsedFunction
value = 'x^2*(1-x)^2*(2*y-6*y^2+4*y^3)'
[]
[exact_v]
type = ParsedFunction
value = '-y^2*(1-y)^2*(2*x-6*x^2+4*x^3)'
[]
[exact_p]
type = ParsedFunction
value = 'x*(1-x)-2/12'
[]
[forcing_u]
type = ADParsedFunction
value = '-4*mu/rho*(-1+2*y)*(y^2-6*x*y^2+6*x^2*y^2-y+6*x*y-6*x^2*y+3*x^2-6*x^3+3*x^4)+1-2*x+4*x^3*y^2*(2*y^2-2*y+1)*(y-1)^2*(-1+2*x)*(x-1)^3'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[forcing_v]
type = ADParsedFunction
value = '4*mu/rho*(-1+2*x)*(x^2-6*y*x^2+6*x^2*y^2-x+6*x*y-6*x*y^2+3*y^2-6*y^3+3*y^4)+4*y^3*x^2*(2*x^2-2*x+1)*(x-1)^2*(-1+2*y)*(y-1)^3'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'bjacobi 30 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-8
[]
[Outputs]
[out]
type = Exodus
hide = lambda
[]
csv = true
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2u]
type = ElementL2Error
variable = vel_x
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2v]
type = ElementL2Error
variable = vel_y
function = exact_v
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2p]
variable = pressure
function = exact_p
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(modules/tensor_mechanics/test/tests/torque/ad_torque_small.i)
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
origin = '0 0 2'
direction = '0 0 1'
polar_moment_of_inertia = pmi
factor = t
[]
[Mesh]
[ring]
type = AnnularMeshGenerator
nr = 1
nt = 30
rmin = 0.95
rmax = 1
[]
[extrude]
type = MeshExtruderGenerator
input = ring
extrusion_vector = '0 0 2'
bottom_sideset = 'bottom'
top_sideset = 'top'
num_layers = 5
[]
[]
[AuxVariables]
[alpha_var]
[]
[shear_stress_var]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[alpha]
type = RotationAngle
variable = alpha_var
[]
[shear_stress]
type = ParsedAux
variable = shear_stress_var
args = 'stress_yz stress_xz'
function = 'sqrt(stress_yz^2 + stress_xz^2)'
[]
[]
[BCs]
# fix bottom
[fix_x]
type = DirichletBC
boundary = bottom
variable = disp_x
value = 0
[]
[fix_y]
type = DirichletBC
boundary = bottom
variable = disp_y
value = 0
[]
[fix_z]
type = DirichletBC
boundary = bottom
variable = disp_z
value = 0
[]
# twist top
[twist_x]
type = ADTorque
boundary = top
variable = disp_x
[]
[twist_y]
type = ADTorque
boundary = top
variable = disp_y
[]
[twist_z]
type = ADTorque
boundary = top
variable = disp_z
[]
[]
[Modules/TensorMechanics/Master]
[all]
add_variables = true
strain = SMALL
use_automatic_differentiation = true
generate_output = 'vonmises_stress stress_yz stress_xz'
[]
[]
[Postprocessors]
[pmi]
type = PolarMomentOfInertia
boundary = top
# execute_on = 'INITIAL NONLINEAR'
execute_on = 'INITIAL'
[]
[alpha]
type = SideAverageValue
variable = alpha_var
boundary = top
[]
[shear_stress]
type = ElementAverageValue
variable = shear_stress_var
[]
[]
[Materials]
[stress]
type = ADComputeLinearElasticStress
[]
[elastic]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 0.3
shear_modulus = 100
[]
[]
[Executioner]
# type = Steady
type = Transient
num_steps = 1
solve_type = NEWTON
petsc_options_iname = '-pctype'
petsc_options_value = 'lu'
nl_max_its = 150
[]
[Outputs]
exodus = true
print_linear_residuals = false
perf_graph = true
[]
(modules/chemical_reactions/test/tests/jacobian/primary_convection.i)
# Test the Jacobian terms for the PrimaryConvection Kernel
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
[../]
[./a]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./pressure]
type = RandomIC
variable = pressure
min = 1
max = 5
[../]
[./a]
type = RandomIC
variable = a
max = 1
min = 0
[../]
[]
[Kernels]
[./diff]
type = DarcyFluxPressure
variable = pressure
[../]
[./conv]
type = PrimaryConvection
variable = a
p = pressure
[../]
[]
[Materials]
[./porous]
type = GenericConstantMaterial
prop_names = 'diffusivity conductivity porosity'
prop_values = '1e-4 1e-4 0.2'
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
perf_graph = true
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_mortar_action/modular_gap_heat_transfer_mortar_displaced_radiation_conduction_verbose.i)
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
[file]
type = FileMeshGenerator
file = 2blk-gap.e
[]
[secondary]
type = LowerDBlockFromSidesetGenerator
sidesets = '101'
new_block_id = 10001
new_block_name = 'secondary_lower'
input = file
[]
[primary]
type = LowerDBlockFromSidesetGenerator
sidesets = '100'
new_block_id = 10000
new_block_name = 'primary_lower'
input = secondary
[]
allow_renumbering = false
[]
[Problem]
kernel_coverage_check = false
material_coverage_check = false
[]
[Variables]
[temp]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[disp_x]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[disp_y]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[lm]
order = FIRST
family = LAGRANGE
block = 'secondary_lower'
[]
[]
[Materials]
[left]
type = ADHeatConductionMaterial
block = 1
thermal_conductivity = 0.01
specific_heat = 1
[]
[right]
type = ADHeatConductionMaterial
block = 2
thermal_conductivity = 0.005
specific_heat = 1
[]
[]
[Kernels]
[hc_displaced_block]
type = ADHeatConduction
variable = temp
use_displaced_mesh = true
block = '1'
[]
[hc_undisplaced_block]
type = ADHeatConduction
variable = temp
use_displaced_mesh = false
block = '2'
[]
[disp_x]
type = Diffusion
variable = disp_x
block = '1 2'
[]
[disp_y]
type = Diffusion
variable = disp_y
block = '1 2'
[]
[]
[UserObjects]
[radiation]
type = GapFluxModelRadiation
temperature = temp
boundary = 100
primary_emissivity = 1.0
secondary_emissivity = 1.0
use_displaced_mesh = true
[]
[conduction]
type = GapFluxModelConduction
temperature = temp
boundary = 100
gap_conductivity = 0.02
use_displaced_mesh = true
[]
[]
[Constraints]
[ced]
type = ModularGapConductanceConstraint
variable = lm
secondary_variable = temp
use_displaced_mesh = true
primary_boundary = 100
primary_subdomain = 10000
secondary_boundary = 101
secondary_subdomain = 10001
correct_edge_dropping = true
gap_flux_models = 'radiation conduction'
[]
[]
[BCs]
[left]
type = DirichletBC
variable = temp
boundary = 'left'
value = 100
[]
[right]
type = DirichletBC
variable = temp
boundary = 'right'
value = 0
[]
[left_disp_x]
type = DirichletBC
preset = false
variable = disp_x
boundary = 'left'
value = .1
[]
[right_disp_x]
type = DirichletBC
preset = false
variable = disp_x
boundary = 'right'
value = 0
[]
[bottom_disp_y]
type = DirichletBC
preset = false
variable = disp_y
boundary = 'bottom'
value = 0
[]
[]
[Preconditioning]
[fmp]
type = SMP
full = true
solve_type = 'NEWTON'
[]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-11
nl_abs_tol = 1.0e-10
[]
[VectorPostprocessors]
[NodalTemperature]
type = NodalValueSampler
sort_by = id
boundary = '100 101'
variable = 'temp'
[]
[]
[Outputs]
csv = true
[exodus]
type = Exodus
show = 'temp'
[]
[]
(modules/heat_conduction/test/tests/radiation_transfer_symmetry/cavity_with_pillars.i)
#
# inner_left: 8
# inner_right: 9
# inner_top: 12
# inner_bottom: 11
# inner_front: 10
# back_2: 7
# obstruction: 6
#
[Mesh]
[cartesian]
type = CartesianMeshGenerator
dim = 3
dx = '0.4 0.5 0.5 0.5 0.5 0.5 0.5 0.4'
dy = '0.5 0.75 0.5'
dz = '1.5 0.5'
subdomain_id = '
3 1 1 1 1 1 1 4
3 1 2 1 1 2 1 4
3 1 1 1 1 1 1 4
3 1 1 1 1 1 1 4
3 1 1 1 1 1 1 4
3 1 1 1 1 1 1 4
'
[]
[add_obstruction]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 2
paired_block = 1
new_boundary = obstruction
input = cartesian
[]
[add_new_back]
type = ParsedGenerateSideset
combinatorial_geometry = 'abs(z) < 1e-10'
included_subdomain_ids = '1'
normal = '0 0 -1'
new_sideset_name = back_2
input = add_obstruction
[]
[add_inner_left]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 3
paired_block = 1
new_boundary = inner_left
input = add_new_back
[]
[add_inner_right]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 4
paired_block = 1
new_boundary = inner_right
input = add_inner_left
[]
[add_inner_front]
type = ParsedGenerateSideset
combinatorial_geometry = 'abs(z - 2) < 1e-10'
included_subdomain_ids = '1'
normal = '0 0 1'
new_sideset_name = inner_front
input = add_inner_right
[]
[add_inner_bottom]
type = ParsedGenerateSideset
combinatorial_geometry = 'abs(y) < 1e-10'
included_subdomain_ids = '1'
normal = '0 -1 0'
new_sideset_name = inner_bottom
input = add_inner_front
[]
[add_inner_top]
type = ParsedGenerateSideset
combinatorial_geometry = 'abs(y - 1.75) < 1e-10'
included_subdomain_ids = '1'
normal = '0 1 0'
new_sideset_name = inner_top
input = add_inner_bottom
[]
[]
[Problem]
kernel_coverage_check = false
[]
[Variables]
[temperature]
block = '2 3 4'
initial_condition = 300
[]
[]
[Kernels]
[conduction]
type = HeatConduction
variable = temperature
block = '2 3 4'
diffusion_coefficient = 1
[]
[source]
type = BodyForce
variable = temperature
value = 1000
block = '2'
[]
[]
[BCs]
[convective]
type = CoupledConvectiveHeatFluxBC
variable = temperature
T_infinity = 300
htc = 50
boundary = 'left right'
[]
[]
[GrayDiffuseRadiation]
[cavity]
boundary = '6 7 8 9 10 11 12'
emissivity = '1 1 1 1 1 1 1'
n_patches = '1 1 1 1 1 1 1'
adiabatic_boundary = '7 10 11 12'
partitioners = 'metis metis metis metis metis metis metis'
temperature = temperature
ray_tracing_face_order = SECOND
normalize_view_factor = false
[]
[]
[Postprocessors]
[Tpv]
type = PointValue
variable = temperature
point = '0.3 0.5 0.5'
[]
[volume]
type = VolumePostprocessor
[]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/nodal_value_off_block.i)
[Mesh]
type = FileMesh
file = rectangle.e
dim = 2
# This test can only be run with renumering disabled, so the
# NodalVariableValue postprocessor's node id is well-defined.
allow_renumbering = false
[]
[Variables]
[./u]
block = '1 2'
[../]
[./v]
block = 2
[../]
[]
[Kernels]
[./diff]
type = BlkResTestDiffusion
variable = u
block = '1 2'
[../]
[./v_diff]
type = Diffusion
variable = v
block = 2
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Materials]
[./mat0]
type = GenericConstantMaterial
block = 1
prop_names = 'a b'
prop_values = '1 2'
[../]
[./mat1]
type = GenericConstantMaterial
block = 2
prop_names = a
prop_values = 10
[../]
[]
[Postprocessors]
[./off_block]
type = NodalVariableValue
variable = v
nodeid = 0
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/interface_stress/multi.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 10
ny = 10
nz = 10
xmax = 1
ymax = 1
zmax = 1
xmin = -1
ymin = -1
zmin = -1
[]
[GlobalParams]
order = CONSTANT
family = MONOMIAL
rank_two_tensor = extra_stress
[]
[Functions]
[./sphere1]
type = ParsedFunction
value = 'r:=sqrt(x^2+y^2+z^2); if(r>1,0,1-3*r^2+2*r^3)'
[../]
[./sphere2]
type = ParsedFunction
value = 'r:=sqrt(x^2+y^2+z^2); 0.5-0.5*if(r>1,0,1-3*r^2+2*r^3)'
[../]
[]
[Variables]
[./dummy]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = dummy
[../]
[]
[AuxVariables]
[./eta1]
[./InitialCondition]
type = FunctionIC
function = sphere1
[../]
order = FIRST
family = LAGRANGE
[../]
[./eta2]
[./InitialCondition]
type = FunctionIC
function = sphere2
[../]
order = FIRST
family = LAGRANGE
[../]
[./s00]
[../]
[./s01]
[../]
[./s02]
[../]
[./s10]
[../]
[./s11]
[../]
[./s12]
[../]
[./s20]
[../]
[./s21]
[../]
[./s22]
[../]
[]
[AuxKernels]
[./s00]
type = RankTwoAux
variable = s00
index_i = 0
index_j = 0
[../]
[./s01]
type = RankTwoAux
variable = s01
index_i = 0
index_j = 1
[../]
[./s02]
type = RankTwoAux
variable = s02
index_i = 0
index_j = 2
[../]
[./s10]
type = RankTwoAux
variable = s10
index_i = 1
index_j = 0
[../]
[./s11]
type = RankTwoAux
variable = s11
index_i = 1
index_j = 1
[../]
[./s12]
type = RankTwoAux
variable = s12
index_i = 1
index_j = 2
[../]
[./s20]
type = RankTwoAux
variable = s20
index_i = 2
index_j = 0
[../]
[./s21]
type = RankTwoAux
variable = s21
index_i = 2
index_j = 1
[../]
[./s22]
type = RankTwoAux
variable = s22
index_i = 2
index_j = 2
[../]
[]
[Materials]
[./interface]
type = ComputeInterfaceStress
v = 'eta1 eta2'
stress = '1.0 2.0'
op_range = '1.0 0.5'
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
file_base = test_out
execute_on = timestep_end
hide = 'dummy eta1 eta2'
[]
(test/tests/markers/reporter_point_marker/point_marker_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
elem_type = QUAD4
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Reporters]
[coords]
type=ConstantReporter
real_vector_names = 'x y z'
real_vector_values = '.31 .41 .51 .31 .41 .51 .31 .41 .51 .8;
.31 .31 .31 .41 .41 .41 .51 .51 .51 .8;
0 0 0 0 0 0 0 0 0 1;'
outputs=none
[]
[bad_coords]
type=ConstantReporter
real_vector_names = 'x y z'
real_vector_values = '.31 .41 .51;
.31 .31 .31 .41 .41 .41 .51 .51;
0 0 0 0 0 0 0 0 0 1;'
outputs=none
[]
[]
[Adaptivity]
[Markers]
active = 'box'
[box]
type = ReporterPointMarker
x_coord_name = coords/x
y_coord_name = coords/y
z_coord_name = coords/z
inside = refine
empty = do_nothing
[]
[bad_coord]
type = ReporterPointMarker
x_coord_name = bad_coords/x
y_coord_name = bad_coords/y
z_coord_name = bad_coords/z
inside = refine
empty = do_nothing
[]
[]
[]
[Outputs]
exodus=true
[]
(test/tests/variables/fe_hier/hier-1-2d.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 5
ny = 5
elem_type = QUAD9
[]
[Functions]
[./bc_fnt]
type = ParsedFunction
value = 1
[../]
[./bc_fnb]
type = ParsedFunction
value = -1
[../]
[./bc_fnl]
type = ParsedFunction
value = -1
[../]
[./bc_fnr]
type = ParsedFunction
value = 1
[../]
[./forcing_fn]
type = ParsedFunction
value = x+y
[../]
[./solution]
type = ParsedGradFunction
value = x+y
grad_x = 1
grad_y = 1
[../]
[]
[Variables]
[./u]
order = FIRST
family = HIERARCHIC
[../]
[]
[Kernels]
active = 'diff forcing reaction'
[./diff]
type = Diffusion
variable = u
[../]
[./reaction]
type = Reaction
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
[./bc_top]
type = FunctionNeumannBC
variable = u
boundary = 'top'
function = bc_fnt
[../]
[./bc_bottom]
type = FunctionNeumannBC
variable = u
boundary = 'bottom'
function = bc_fnb
[../]
[./bc_left]
type = FunctionNeumannBC
variable = u
boundary = 'left'
function = bc_fnl
[../]
[./bc_right]
type = FunctionNeumannBC
variable = u
boundary = 'right'
function = bc_fnr
[../]
[]
[Postprocessors]
[./dofs]
type = NumDOFs
[../]
[./h]
type = AverageElementSize
[../]
[./L2error]
type = ElementL2Error
variable = u
function = solution
[../]
[./H1error]
type = ElementH1Error
variable = u
function = solution
[../]
[./H1Semierror]
type = ElementH1SemiError
variable = u
function = solution
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
csv = true
[]
(test/tests/meshgenerators/plane_id_mesh_generator/plane_id_grid2d.i)
[Mesh]
[grid]
type = CartesianMeshGenerator
dim = 2
dx = '5.0 10.0 '
ix = '1 4'
dy = '5.0 10.0 '
iy = '1 4'
[]
[plane_id_gen]
type = PlaneIDMeshGenerator
input = 'grid'
plane_coordinates = '0.0 5.0 15.0'
num_ids_per_plane = ' 1 2'
plane_axis = 'x'
id_name = 'plane_id'
[]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[AuxVariables]
[plane_id]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[set_plane_id]
type = ExtraElementIDAux
variable = plane_id
extra_id_name = plane_id
[]
[]
[Outputs]
exodus = true
execute_on = timestep_end
[]
(test/tests/materials/interface_material/interface_value_material_noIK.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 2
xmax = 2
ny = 2
ymax = 2
elem_type = QUAD4
[]
[./subdomain_id]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '1 0 0'
top_right = '2 2 0'
block_id = 1
[../]
[./interface]
type = SideSetsBetweenSubdomainsGenerator
input = subdomain_id
primary_block = '0'
paired_block = '1'
new_boundary = 'interface'
[../]
[]
[Variables]
[./u]
block = 0
[../]
[./v]
block = 1
[../]
[]
[Kernels]
[./diff]
type = MatDiffusion
variable = u
diffusivity = 'diffusivity'
block = 0
[../]
[./diff_v]
type = MatDiffusion
variable = v
diffusivity = 'diffusivity'
block = 1
[../]
[]
[BCs]
[u_left]
type = DirichletBC
boundary = 'left'
variable = u
value = 1
[]
[v_right]
type = DirichletBC
boundary = 'right'
variable = v
value = 0
[]
[]
[Materials]
[./stateful1]
type = StatefulMaterial
block = 0
initial_diffusivity = 1
# outputs = all
[../]
[./stateful2]
type = StatefulMaterial
block = 1
initial_diffusivity = 2
# outputs = all
[../]
[./interface_material_avg]
type = InterfaceValueMaterial
mat_prop_primary = diffusivity
mat_prop_secondary = diffusivity
var_primary = diffusivity_var
var_secondary = diffusivity_var
mat_prop_out_basename = diff
boundary = interface
interface_value_type = average
mat_prop_var_out_basename = diff_var
nl_var_primary = u
nl_var_secondary = v
[../]
[./interface_material_jump_primary_minus_secondary]
type = InterfaceValueMaterial
mat_prop_primary = diffusivity
mat_prop_secondary = diffusivity
var_primary = diffusivity_var
var_secondary = diffusivity_var
mat_prop_out_basename = diff
boundary = interface
interface_value_type = jump_primary_minus_secondary
mat_prop_var_out_basename = diff_var
nl_var_primary = u
nl_var_secondary = v
[../]
[./interface_material_jump_secondary_minus_primary]
type = InterfaceValueMaterial
mat_prop_primary = diffusivity
mat_prop_secondary = diffusivity
var_primary = diffusivity_var
var_secondary = diffusivity_var
mat_prop_out_basename = diff
boundary = interface
interface_value_type = jump_secondary_minus_primary
mat_prop_var_out_basename = diff_var
nl_var_primary = u
nl_var_secondary = v
[../]
[./interface_material_jump_abs]
type = InterfaceValueMaterial
mat_prop_primary = diffusivity
mat_prop_secondary = diffusivity
var_primary = diffusivity_var
var_secondary = diffusivity_var
mat_prop_out_basename = diff
boundary = interface
interface_value_type = jump_abs
mat_prop_var_out_basename = diff_var
nl_var_primary = u
nl_var_secondary = v
[../]
[./interface_material_primary]
type = InterfaceValueMaterial
mat_prop_primary = diffusivity
mat_prop_secondary = diffusivity
var_primary = diffusivity_var
var_secondary = diffusivity_var
mat_prop_out_basename = diff
boundary = interface
interface_value_type = primary
mat_prop_var_out_basename = diff_var
nl_var_primary = u
nl_var_secondary = v
[../]
[./interface_material_secondary]
type = InterfaceValueMaterial
mat_prop_primary = diffusivity
mat_prop_secondary = diffusivity
var_primary = diffusivity_var
var_secondary = diffusivity_var
mat_prop_out_basename = diff
mat_prop_var_out_basename = diff_var
boundary = interface
interface_value_type = secondary
nl_var_primary = u
nl_var_secondary = v
[../]
[]
[AuxKernels]
[./interface_material_avg]
type = MaterialRealAux
property = diff_average
variable = diffusivity_average
boundary = interface
[]
[./interface_material_jump_primary_minus_secondary]
type = MaterialRealAux
property = diff_jump_primary_minus_secondary
variable = diffusivity_jump_primary_minus_secondary
boundary = interface
[]
[./interface_material_jump_secondary_minus_primary]
type = MaterialRealAux
property = diff_jump_secondary_minus_primary
variable = diffusivity_jump_secondary_minus_primary
boundary = interface
[]
[./interface_material_jump_abs]
type = MaterialRealAux
property = diff_jump_abs
variable = diffusivity_jump_abs
boundary = interface
[]
[./interface_material_primary]
type = MaterialRealAux
property = diff_primary
variable = diffusivity_primary
boundary = interface
[]
[./interface_material_secondary]
type = MaterialRealAux
property = diff_secondary
variable = diffusivity_secondary
boundary = interface
[]
[diffusivity_var]
type = MaterialRealAux
property = diffusivity
variable = diffusivity_var
[]
[]
[AuxVariables]
[diffusivity_var]
family = MONOMIAL
order = CONSTANT
[]
[./diffusivity_average]
family = MONOMIAL
order = CONSTANT
[]
[./diffusivity_jump_primary_minus_secondary]
family = MONOMIAL
order = CONSTANT
[]
[./diffusivity_jump_secondary_minus_primary]
family = MONOMIAL
order = CONSTANT
[]
[./diffusivity_jump_abs]
family = MONOMIAL
order = CONSTANT
[]
[./diffusivity_primary]
family = MONOMIAL
order = CONSTANT
[]
[./diffusivity_secondary]
family = MONOMIAL
order = CONSTANT
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(test/tests/parser/vector_range_checking/all_pass.i)
[Mesh]
type = GeneratedMesh
dim = 3
[]
[Materials]
[./vecrangecheck]
type = VecRangeCheckMaterial
block = 0
rv3 = '1.1 2.2 3.3'
iv3 = '1 2 3'
rvp = '0.1 0.2 0.3 0.4'
uvg = '2 1'
lvg = '2 1'
ivg = '2 1'
rvg = '2.0 1.0'
rvl = '0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 1.1 1.2 1.3'
rve = ''
[../]
[]
[Problem]
type = FEProblem
solve = false
#kernel_check = false
[]
[Executioner]
type = Steady
[]
[Outputs]
execute_on = 'timestep_end'
[]
(modules/navier_stokes/test/tests/finite_volume/cns/mms/1d-with-bcs/free-flow-hllc.i)
[GlobalParams]
fp = fp
[]
[Mesh]
[cartesian]
type = GeneratedMeshGenerator
dim = 1
xmin = .1
xmax = 1.1
nx = 2
[]
[]
[Modules]
[FluidProperties]
[fp]
type = IdealGasFluidProperties
[]
[]
[]
[Variables]
[rho]
type = MooseVariableFVReal
[]
[rho_u]
type = MooseVariableFVReal
[]
[rho_et]
type = MooseVariableFVReal
[]
[]
[ICs]
[rho]
type = FunctionIC
variable = rho
function = 'exact_rho'
[]
[rho_u]
type = FunctionIC
variable = rho_u
function = 'exact_rho_u'
[]
[rho_et]
type = FunctionIC
variable = rho_et
function = 'exact_rho_et'
[]
[]
[FVKernels]
[mass_advection]
type = CNSFVMassHLLC
variable = rho
[]
[mass_fn]
type = FVBodyForce
variable = rho
function = 'forcing_rho'
[]
[momentum_x_advection]
type = CNSFVMomentumHLLC
variable = rho_u
momentum_component = x
[]
[momentum_fn]
type = FVBodyForce
variable = rho_u
function = 'forcing_rho_u'
[]
[fluid_energy_advection]
type = CNSFVFluidEnergyHLLC
variable = rho_et
[]
[energy_fn]
type = FVBodyForce
variable = rho_et
function = 'forcing_rho_et'
[]
[]
[FVBCs]
[mass_in]
variable = rho
type = CNSFVHLLCSpecifiedMassFluxAndTemperatureMassBC
boundary = left
temperature = 'exact_T'
rhou = 'exact_rho_u'
[]
[momentum_in]
variable = rho_u
type = CNSFVHLLCSpecifiedMassFluxAndTemperatureMomentumBC
boundary = left
temperature = 'exact_T'
rhou = 'exact_rho_u'
momentum_component = 'x'
[]
[energy_in]
variable = rho_et
type = CNSFVHLLCSpecifiedMassFluxAndTemperatureFluidEnergyBC
boundary = left
temperature = 'exact_T'
rhou = 'exact_rho_u'
[]
[mass_out]
variable = rho
type = CNSFVHLLCSpecifiedPressureMassBC
boundary = right
pressure = 'exact_p'
[]
[momentum_out]
variable = rho_u
type = CNSFVHLLCSpecifiedPressureMomentumBC
boundary = right
pressure = 'exact_p'
momentum_component = 'x'
[]
[energy_out]
variable = rho_et
type = CNSFVHLLCSpecifiedPressureFluidEnergyBC
boundary = right
pressure = 'exact_p'
[]
[]
[Materials]
[var_mat]
type = ConservedVarValuesMaterial
rho = rho
rhou = rho_u
rho_et = rho_et
[]
[]
[Functions]
[exact_rho]
type = ParsedFunction
value = '3.48788261470924*cos(x)'
[]
[forcing_rho]
type = ParsedFunction
value = '-3.83667087618017*sin(1.1*x)'
[]
[exact_rho_u]
type = ParsedFunction
value = '3.48788261470924*cos(1.1*x)'
[]
[forcing_rho_u]
type = ParsedFunction
value = '-(10.6975765229419*cos(1.2*x)/cos(x) - 0.697576522941849*cos(1.1*x)^2/cos(x)^2)*sin(x) + (10.6975765229419*sin(x)*cos(1.2*x)/cos(x)^2 - 1.3951530458837*sin(x)*cos(1.1*x)^2/cos(x)^3 + 1.53466835047207*sin(1.1*x)*cos(1.1*x)/cos(x)^2 - 12.8370918275302*sin(1.2*x)/cos(x))*cos(x) + 3.48788261470924*sin(x)*cos(1.1*x)^2/cos(x)^2 - 7.67334175236034*sin(1.1*x)*cos(1.1*x)/cos(x)'
[]
[exact_rho_et]
type = ParsedFunction
value = '26.7439413073546*cos(1.2*x)'
[]
[forcing_rho_et]
type = ParsedFunction
value = '1.0*(3.48788261470924*(3.06706896551724*cos(1.2*x)/cos(x) - 0.2*cos(1.1*x)^2/cos(x)^2)*cos(x) + 26.7439413073546*cos(1.2*x))*sin(x)*cos(1.1*x)/cos(x)^2 - 1.1*(3.48788261470924*(3.06706896551724*cos(1.2*x)/cos(x) - 0.2*cos(1.1*x)^2/cos(x)^2)*cos(x) + 26.7439413073546*cos(1.2*x))*sin(1.1*x)/cos(x) + 1.0*(-(10.6975765229419*cos(1.2*x)/cos(x) - 0.697576522941849*cos(1.1*x)^2/cos(x)^2)*sin(x) + (10.6975765229419*sin(x)*cos(1.2*x)/cos(x)^2 - 1.3951530458837*sin(x)*cos(1.1*x)^2/cos(x)^3 + 1.53466835047207*sin(1.1*x)*cos(1.1*x)/cos(x)^2 - 12.8370918275302*sin(1.2*x)/cos(x))*cos(x) - 32.0927295688256*sin(1.2*x))*cos(1.1*x)/cos(x)'
[]
[exact_T]
type = ParsedFunction
value = '0.0106975765229418*cos(1.2*x)/cos(x) - 0.000697576522941848*cos(1.1*x)^2/cos(x)^2'
[]
[exact_p]
type = ParsedFunction
value = '3.48788261470924*(3.06706896551724*cos(1.2*x)/cos(x) - 0.2*cos(1.1*x)^2/cos(x)^2)*cos(x)'
[]
[]
[Executioner]
solve_type = NEWTON
type = Steady
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
nl_max_its = 50
line_search = none
nl_rel_tol = 1e-12
nl_abs_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[]
[Debug]
show_var_residual_norms = true
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2rho]
type = ElementL2Error
variable = rho
function = exact_rho
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2rho_u]
variable = rho_u
function = exact_rho_u
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2rho_et]
variable = rho_et
function = exact_rho_et
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(test/tests/vectorpostprocessors/nodal_value_sampler/nodal_value_sampler.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = left
value = 1
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = right
value = 0
[../]
[]
[VectorPostprocessors]
[./nodal_sample]
type = NodalValueSampler
variable = 'u v'
boundary = top
sort_by = x
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
csv = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/cylindrical/2d-average.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='average'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
[]
[]
[Problem]
fv_bcs_integrity_check = true
coord_type = 'RZ'
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
two_term_boundary_expansion = false
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
two_term_boundary_expansion = false
[]
[pressure]
type = INSFVPressureVariable
two_term_boundary_expansion = false
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[u_forcing]
type = INSFVBodyForce
variable = u
functor = forcing_u
momentum_component = 'x'
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[v_forcing]
type = INSFVBodyForce
variable = v
functor = forcing_v
momentum_component = 'y'
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = u
function = 'exact_u'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = v
function = 'exact_v'
[]
[no-slip-wall-u]
type = INSFVNoSlipWallBC
boundary = 'right'
variable = u
function = 'exact_u'
[]
[no-slip-wall-v]
type = INSFVNoSlipWallBC
boundary = 'right'
variable = v
function = 'exact_v'
[]
[outlet-p]
type = INSFVOutletPressureBC
boundary = 'top'
variable = pressure
function = 'exact_p'
[]
[axis-u]
type = INSFVSymmetryVelocityBC
boundary = 'left'
variable = u
u = u
v = v
mu = ${mu}
momentum_component = x
[]
[axis-v]
type = INSFVSymmetryVelocityBC
boundary = 'left'
variable = v
u = u
v = v
mu = ${mu}
momentum_component = y
[]
[axis-p]
type = INSFVSymmetryPressureBC
boundary = 'left'
variable = pressure
[]
[]
[Functions]
[exact_u]
type = ParsedFunction
value = 'sin(x*pi)^2*sin((1/2)*y*pi)'
[]
[exact_rhou]
type = ParsedFunction
value = 'rho*sin(x*pi)^2*sin((1/2)*y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_u]
type = ADParsedFunction
value = '(1/4)*pi^2*mu*sin(x*pi)^2*sin((1/2)*y*pi) - pi*sin(x*pi)*cos((1/2)*y*pi) + (4*x*pi*rho*sin(x*pi)^3*sin((1/2)*y*pi)^2*cos(x*pi) + rho*sin(x*pi)^4*sin((1/2)*y*pi)^2)/x + (-x*pi*rho*sin(x*pi)^2*sin((1/2)*y*pi)*sin(y*pi)*cos(x*pi) + (1/2)*x*pi*rho*sin(x*pi)^2*cos(x*pi)*cos((1/2)*y*pi)*cos(y*pi))/x - (-2*x*pi^2*mu*sin(x*pi)^2*sin((1/2)*y*pi) + 2*x*pi^2*mu*sin((1/2)*y*pi)*cos(x*pi)^2 + 2*pi*mu*sin(x*pi)*sin((1/2)*y*pi)*cos(x*pi))/x'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_v]
type = ParsedFunction
value = 'cos(x*pi)*cos(y*pi)'
[]
[exact_rhov]
type = ParsedFunction
value = 'rho*cos(x*pi)*cos(y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_v]
type = ADParsedFunction
value = 'pi^2*mu*cos(x*pi)*cos(y*pi) - 2*pi*rho*sin(y*pi)*cos(x*pi)^2*cos(y*pi) - 1/2*pi*sin((1/2)*y*pi)*cos(x*pi) - (-x*pi^2*mu*cos(x*pi)*cos(y*pi) - pi*mu*sin(x*pi)*cos(y*pi))/x + (-x*pi*rho*sin(x*pi)^3*sin((1/2)*y*pi)*cos(y*pi) + 2*x*pi*rho*sin(x*pi)*sin((1/2)*y*pi)*cos(x*pi)^2*cos(y*pi) + rho*sin(x*pi)^2*sin((1/2)*y*pi)*cos(x*pi)*cos(y*pi))/x'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_p]
type = ParsedFunction
value = 'cos(x*pi)*cos((1/2)*y*pi)'
[]
[forcing_p]
type = ParsedFunction
value = '-pi*rho*sin(y*pi)*cos(x*pi) + (2*x*pi*rho*sin(x*pi)*sin((1/2)*y*pi)*cos(x*pi) + rho*sin(x*pi)^2*sin((1/2)*y*pi))/x'
vars = 'rho'
vals = '${rho}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
[]
[Outputs]
exodus = true
csv = true
[dof]
type = DOFMap
execute_on = 'initial'
[]
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[./L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2v]
type = ElementL2Error
variable = v
function = exact_v
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2p]
variable = pressure
function = exact_p
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[]
(modules/porous_flow/test/tests/flux_limited_TVD_pflow/except01.i)
# Exception test: phase number too big
[Mesh]
type = GeneratedMesh
dim = 1
[]
[GlobalParams]
gravity = '1 2 3'
PorousFlowDictator = dictator
[]
[Variables]
[pp]
[]
[tracer]
[]
[]
[Modules]
[FluidProperties]
[the_simple_fluid]
type = SimpleFluidProperties
[]
[]
[]
[PorousFlowUnsaturated]
porepressure = pp
mass_fraction_vars = tracer
fp = the_simple_fluid
[]
[UserObjects]
[advective_flux_calculator]
type = PorousFlowAdvectiveFluxCalculatorSaturated
phase = 2
[]
[]
[Materials]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1 0 0 0 2 0 0 0 3'
[]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
(test/tests/mortar/1d/1d_nodebc_name.i)
# Tests a 'jump' across a boundary where the jump simply connects two diffusion domains
# This test uses named nodal boundaries instead of the actual node #'s
[Mesh]
file = 2-lines.e
construct_side_list_from_node_list = true
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
block = '1 2'
[../]
[./lm]
order = FIRST
family = SCALAR
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[ScalarKernels]
[./ced]
type = NodalEqualValueConstraint
variable = lm
var = u
boundary = '100 101'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = '1'
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = '2'
value = 3
[../]
[./evc1]
type = OneDEqualValueConstraintBC
variable = u
boundary = '100'
lambda = lm
component = 0
vg = 1
[../]
[./evc2]
type = OneDEqualValueConstraintBC
variable = u
boundary = '101'
lambda = lm
component = 0
vg = -1
[../]
[]
[Preconditioning]
[./fmp]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/materials/ad_material/conversion/1d_dirichlet.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 10
xmax = 2
[]
[Variables]
[v]
initial_condition = 1.1
[]
[]
[Kernels]
inactive = 'ad_diff'
[diff]
type = MatDiffusion
variable = v
diffusivity = 'coef'
[]
[ad_diff]
type = ADMatDiffusion
variable = v
diffusivity = 'ad_coef_2'
[]
[sink]
type = ADBodyForce
variable = v
function = 'sink'
[]
[]
[BCs]
[bounds]
type = DirichletBC
variable = v
boundary = 'left right'
value = 0
[]
[]
[Functions]
[sink]
type = ParsedFunction
value = '3*x^3'
[]
[]
[Materials]
[ad_coef]
type = ADParsedMaterial
f_name = 'ad_coef'
function = '0.01 * max(v, 1)'
args = 'v'
[]
[converter_to_regular]
type = MaterialADConverter
ad_props_in = 'ad_coef'
reg_props_out = 'coef'
[]
# at this point we should have lost the derivatives
[converter_to_ad]
type = MaterialADConverter
reg_props_in = 'coef'
ad_props_out = 'ad_coef_2'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(test/tests/restart/restart_transient_from_steady/steady_with_sub.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[AuxVariables]
[Tf]
[]
[]
[Variables]
[power_density]
[]
[]
[Functions]
[pwr_func]
type = ParsedFunction
value = '1e3*x*(1-x)+5e2'
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = power_density
[]
[coupledforce]
type = BodyForce
variable = power_density
function = pwr_func
[]
[]
[BCs]
[left]
type = DirichletBC
variable = power_density
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = power_density
boundary = right
value = 1e3
[]
[]
[Postprocessors]
[pwr_avg]
type = ElementAverageValue
variable = power_density
execute_on = 'initial timestep_end'
[]
[temp_avg]
type = ElementAverageValue
variable = Tf
execute_on = 'initial final'
[]
[temp_max]
type = ElementExtremeValue
value_type = max
variable = Tf
execute_on = 'initial final'
[]
[temp_min]
type = ElementExtremeValue
value_type = min
variable = Tf
execute_on = 'initial final'
[]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart '
petsc_options_value = 'hypre boomeramg 100'
nl_abs_tol = 1e-8
nl_rel_tol = 1e-12
fixed_point_rel_tol = 1E-7
fixed_point_abs_tol = 1.0e-07
fixed_point_max_its = 12
[]
[MultiApps]
[sub]
type = FullSolveMultiApp
app_type = MooseTestApp
positions = '0 0 0'
input_files = steady_with_sub_sub.i
execute_on = 'timestep_end'
[]
[]
[Transfers]
[p_to_sub]
type = MultiAppMeshFunctionTransfer
source_variable = power_density
variable = power_density
to_multi_app = sub
execute_on = 'timestep_end'
[]
[t_from_sub]
type = MultiAppMeshFunctionTransfer
source_variable = temp
variable = Tf
from_multi_app = sub
execute_on = 'timestep_end'
[]
[]
[Outputs]
exodus = true
csv = true
perf_graph = true
checkpoint = true
execute_on = 'INITIAL TIMESTEP_END FINAL'
[]
(test/tests/mesh_modifiers/mesh_extruder/extrude_remap_layer2.i)
[Mesh]
[file]
type = FileMeshGenerator
file = multiblock.e
[]
[extrude]
type = MeshExtruderGenerator
input = file
num_layers = 6
extrusion_vector = '0 0 2'
bottom_sideset = 'new_bottom'
top_sideset = 'new_top'
# Remap layers
existing_subdomains = '1 2 5'
layers = '1 3 5'
new_ids = '10 12 15' # Repeat this remapping for each layer
[]
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[bottom]
type = DirichletBC
variable = u
boundary = 'new_bottom'
value = 0
[]
[top]
type = DirichletBC
variable = u
boundary = 'new_top'
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/transfers/multiapp_projection_transfer/high_order_master.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 4
[]
[Functions]
[./test_function]
type = ParsedFunction
value = '2.5*x^2 + 0.75*y^2 + 0.15*x*y'
[../]
[]
[AuxVariables]
[./from_sub]
family = monomial
order = first
[../]
[./test_var]
family = monomial
order = first
[./InitialCondition]
type = FunctionIC
function = test_function
[../]
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
[MultiApps]
[./sub]
type = FullSolveMultiApp
app_type = MooseTestApp
execute_on = initial
positions = '0.0 0.0 0.0'
input_files = high_order_sub.i
[../]
[]
[Transfers]
[./from]
type = MultiAppProjectionTransfer
execute_on = same_as_multiapp
from_multi_app = sub
source_variable = test_var
variable = from_sub
[../]
[./to]
type = MultiAppProjectionTransfer
execute_on = same_as_multiapp
to_multi_app = sub
source_variable = test_var
variable = from_master
[../]
[]
(test/tests/parser/cli_argument/cli_arg_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 9999 # Override this value
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Materials]
active = empty
[./empty]
type = MTMaterial
block = 9999 # Override this value
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/fvkernels/mms/advective-outflow/kt-limited-advection.i)
a=1.1
c=343
max_abs_eig=${fparse c + a}
[Mesh]
[./gen_mesh]
type = GeneratedMeshGenerator
dim = 1
xmin = 0.1
xmax = 1.1
nx = 2
[../]
[]
[Problem]
fv_bcs_integrity_check = false
[]
[ICs]
[u]
type = FunctionIC
variable = u
function = exact
[]
[]
[Variables]
[./u]
two_term_boundary_expansion = true
type = MooseVariableFVReal
[../]
[]
[FVKernels]
[./advection_u]
type = FVKTLimitedAdvection
variable = u
velocity = '${a} 0 0'
limiter = 'vanLeer'
max_abs_eig = ${max_abs_eig}
add_artificial_diff = true
[../]
[body_u]
type = FVBodyForce
variable = u
function = 'forcing'
[]
[]
[FVBCs]
[left_u]
type = FVFunctionNeumannBC
boundary = 'left'
function = 'advection'
variable = u
[]
[diri_left]
type = FVFunctionDirichletBC
boundary = 'left'
function = 'exact'
variable = u
[]
[right]
type = FVConstantScalarOutflowBC
variable = u
velocity = '${a} 0 0'
boundary = 'right'
[]
[]
[Functions]
[exact]
type = ParsedFunction
value = 'cos(x)'
[]
[advection]
type = ParsedFunction
value = '${a} * cos(x)'
[]
[forcing]
type = ParsedFunction
value = '-${a} * sin(x)'
[]
[]
[Executioner]
type = Steady
petsc_options_iname = '-snes_linesearch_minlambda'
petsc_options_value = '1e-3'
nl_abs_tol = 1e-9
[]
[Outputs]
file_base = 'kt-limited-advection_out'
[csv]
type = CSV
execute_on = 'final'
[]
[exo]
type = Exodus
execute_on = 'final'
[]
[]
[Postprocessors]
[./L2u]
type = ElementL2Error
variable = u
function = exact
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(test/tests/userobjects/nearest_point_layered_side_integral/nearest_point_layered_side_integral.i)
# This input computes both a layered average and layered integral with the
# same direction, points, and number of layers. The layered integral for "bin"
# i is directly equal to the layered average for "bin" i multiplied by
# by 0.05 (side length of 1 divided by 10 layers X side length of 1 divided by 2 points).
[Mesh]
type = GeneratedMesh
dim = 3
nx = 10
ny = 10
nz = 10
[]
[Variables]
[dummy]
[]
[]
[Kernels]
[diffusion]
type = Diffusion
variable = dummy
[]
[]
[AuxVariables]
[u]
[]
[]
[AuxVariables]
[np_layered_integral]
order = CONSTANT
family = MONOMIAL
[]
[np_layered_average]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[u]
type = FunctionAux
variable = u
function = u
[]
[np_layered_integral]
type = SpatialUserObjectAux
variable = np_layered_integral
user_object = npli
boundary = 'front'
execute_on = timestep_end
[]
[np_layered_average]
type = SpatialUserObjectAux
variable = np_layered_average
user_object = npla
boundary = 'front'
execute_on = timestep_end
[]
[]
[Functions]
[u]
type = ParsedFunction
value = 'x+2*y+3*z'
[]
[]
[UserObjects]
[npla]
type = NearestPointLayeredSideAverage
direction = x
points = '0.5 0.25 0.5
0.5 0.75 0.5'
num_layers = 10
variable = u
boundary = 'front'
[]
[npli]
type = NearestPointLayeredSideIntegral
direction = x
points = '0.5 0.25 0.5
0.5 0.75 0.5'
num_layers = 10
variable = u
boundary = 'front'
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
hide = 'dummy'
[]
(modules/thermal_hydraulics/test/tests/materials/convective_heat_transfer_coefficient/test.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
allow_renumbering = false
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[AuxVariables]
[Hw]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[Hw_ak]
type = MaterialRealAux
variable = Hw
property = Hw
[]
[]
[Materials]
[props]
type = GenericConstantMaterial
prop_names = 'Nu k D_h'
prop_values = '1000 2 20'
[]
[Hw_material]
type = ConvectiveHeatTransferCoefficientMaterial
Nu = Nu
D_h = D_h
k = k
[]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[Hw]
type = ElementalVariableValue
elementid = 0
variable = Hw
[]
[]
[Outputs]
csv = true
execute_on = timestep_end
[]
(test/tests/reporters/base/special_types.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
[]
[]
[UserObjects/special_type_test]
type = ReporterSpecialTypeTest
pp_reporter = "pp/value"
vpp_reporter = "vpp/value"
[]
[Postprocessors/pp]
type = FunctionValuePostprocessor
function = 1
[]
[VectorPostprocessors/vpp]
type = ConstantVectorPostprocessor
vector_names = 'value'
value = '2'
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
execute_on = timestep_end
[]
(test/tests/transfers/multiapp_transfer_transformation/transfer_transformation.i)
[Mesh]
[./gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 3
ny = 5
nz = 0
xmax = 0.8
xmin = 0.2
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[./subdomain_id]
type = ElementSubdomainIDGenerator
input = gmg
subdomain_ids = '0 1 2
0 1 2
0 1 2
0 1 2
0 1 2'
[]
[./boundary01]
type = SideSetsBetweenSubdomainsGenerator
input = subdomain_id
primary_block = '0'
paired_block = '1'
new_boundary = 'boundary01'
[]
[./boundary10]
type = SideSetsBetweenSubdomainsGenerator
input = boundary01
primary_block = '1'
paired_block = '0'
new_boundary = 'boundary10'
[]
[./boundary12]
type = SideSetsBetweenSubdomainsGenerator
input = boundary10
primary_block = '1'
paired_block = '2'
new_boundary = 'boundary12'
[]
[./boundary21]
type = SideSetsBetweenSubdomainsGenerator
input = boundary12
primary_block = '2'
paired_block = '1'
new_boundary = 'boundary21'
[]
uniform_refine = 3
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxVariables]
[./fromsubelem]
order = constant
family = monomial
[../]
[./fromsub]
[]
[]
[BCs]
[./left0]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right0]
type = DirichletBC
variable = u
boundary = boundary01
value = 1
[../]
[./right1]
type = DirichletBC
variable = u
boundary = boundary12
value = 0
[../]
[./right2]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
[MultiApps]
[sub]
type = FullSolveMultiApp
app_type = MooseTestApp
positions = '0.0 0.0 0.0'
execute_on = 'timestep_end'
input_files = transfer_transformation_sub.i
[]
[]
[Transfers]
[from_sub]
type = MultiAppInterpolationTransfer
from_multi_app = sub
num_points = 1
shrink_gap_width = 0.2
shrink_mesh = 'source'
source_variable = 'u'
variable = 'fromsub'
exclude_gap_blocks = '1 3'
[]
[from_sub_elem]
type = MultiAppInterpolationTransfer
from_multi_app = sub
num_points = 4
shrink_gap_width = 0.2
shrink_mesh = 'source'
source_variable = 'u'
variable = 'fromsubelem'
exclude_gap_blocks = '1 3'
[]
[from_master]
type = MultiAppInterpolationTransfer
to_multi_app = sub
num_points = 1
shrink_gap_width = 0.2
shrink_mesh = 'target'
source_variable = 'u'
exclude_gap_blocks = '1 3'
variable = 'frommaster'
[]
[from_master_elem]
type = MultiAppInterpolationTransfer
to_multi_app = sub
num_points = 4
shrink_gap_width = 0.2
shrink_mesh = 'target'
source_variable = 'u'
exclude_gap_blocks = '1 3'
variable = 'frommasterelem'
[]
[]
(modules/tensor_mechanics/tutorials/basics/part_2.1.i)
#Tensor Mechanics tutorial: the basics
#Step 2, part 1
#2D axisymmetric RZ simulation of uniaxial tension linear elasticity
[GlobalParams]
displacements = 'disp_r disp_z' #change the variable names for the coordinate system
[]
[Problem]
coord_type = RZ
[]
[Mesh]
file = necking_quad4.e
uniform_refine = 1
[]
[Modules/TensorMechanics/Master]
[./block1]
strain = SMALL #detects the change in coordinate system and automatically sets the correct strain class
add_variables = true
generate_output = 'stress_zz vonmises_stress' #use stress_zz to get stress_theta quantity
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 2.1e5
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = disp_r #change the variable to reflect the new displacement names
boundary = left
value = 0.0
[../]
[./bottom]
type = DirichletBC
variable = disp_z #change the variable to reflect the new displacement names
boundary = bottom
value = 0.0
[../]
[./top]
type = DirichletBC
variable = disp_z #change the variable to reflect the new displacement names
boundary = top
value = 0.0035
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -sub_pc_type -pc_asm_overlap -ksp_gmres_restart'
petsc_options_value = 'asm lu 1 101'
[]
[Outputs]
exodus = true
perf_graph = true
[]
(modules/combined/test/tests/linear_elasticity/linear_anisotropic_material.i)
# This input file is designed to test the LinearGeneralAnisotropicMaterial class. This test is
# for regression testing. This just takes the material properties and puts them into
# aux variables; the diffusion kernel is just to have a simple kernel to run the test.
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
nz = 0
xmin = 0
xmax = 50
ymin = 0
ymax = 50
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
[./diffused]
[../]
[]
[Modules/TensorMechanics/Master/All]
strain = SMALL
incremental = true
add_variables = true
[]
[AuxVariables]
[./C11]
order = CONSTANT
family = MONOMIAL
[../]
[./C12]
order = CONSTANT
family = MONOMIAL
[../]
[./C13]
order = CONSTANT
family = MONOMIAL
[../]
[./C14]
order = CONSTANT
family = MONOMIAL
[../]
[./C15]
order = CONSTANT
family = MONOMIAL
[../]
[./C16]
order = CONSTANT
family = MONOMIAL
[../]
[./C22]
order = CONSTANT
family = MONOMIAL
[../]
[./C23]
order = CONSTANT
family = MONOMIAL
[../]
[./C24]
order = CONSTANT
family = MONOMIAL
[../]
[./C25]
order = CONSTANT
family = MONOMIAL
[../]
[./C26]
order = CONSTANT
family = MONOMIAL
[../]
[./C33]
order = CONSTANT
family = MONOMIAL
[../]
[./C34]
order = CONSTANT
family = MONOMIAL
[../]
[./C35]
order = CONSTANT
family = MONOMIAL
[../]
[./C36]
order = CONSTANT
family = MONOMIAL
[../]
[./C44]
order = CONSTANT
family = MONOMIAL
[../]
[./C45]
order = CONSTANT
family = MONOMIAL
[../]
[./C46]
order = CONSTANT
family = MONOMIAL
[../]
[./C55]
order = CONSTANT
family = MONOMIAL
[../]
[./C56]
order = CONSTANT
family = MONOMIAL
[../]
[./C66]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = diffused
[../]
[]
[AuxKernels]
[./matl_C11]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 0
variable = C11
[../]
[./matl_C12]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 1
index_l = 1
variable = C12
[../]
[./matl_C13]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 2
index_l = 2
variable = C13
[../]
[./matl_C14]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 1
index_l = 2
variable = C14
[../]
[./matl_C15]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 2
variable = C15
[../]
[./matl_C16]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 1
variable = C16
[../]
[./matl_C22]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 1
index_l = 1
variable = C22
[../]
[./matl_C23]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 2
index_l = 2
variable = C23
[../]
[./matl_C24]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 1
index_l = 2
variable = C24
[../]
[./matl_C25]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 0
index_l = 2
variable = C25
[../]
[./matl_C26]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 0
index_l = 1
variable = C26
[../]
[./matl_C33]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 2
index_l = 2
variable = C33
[../]
[./matl_C34]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 1
index_l = 2
variable = C34
[../]
[./matl_C35]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 0
index_l = 2
variable = C35
[../]
[./matl_C36]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 0
index_l = 1
variable = C36
[../]
[./matl_C44]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 2
index_k = 1
index_l = 2
variable = C44
[../]
[./matl_C45]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 2
index_k = 0
index_l = 2
variable = C45
[../]
[./matl_C46]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 2
index_k = 0
index_l = 1
variable = C46
[../]
[./matl_C55]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 2
index_k = 0
index_l = 2
variable = C55
[../]
[./matl_C56]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 2
index_k = 0
index_l = 1
variable = C56
[../]
[./matl_C66]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 1
index_k = 0
index_l = 1
variable = C66
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeElasticityTensor
fill_method = symmetric21
C_ijkl ='1.0 2.0 3.0 4.0 5.0 6.0 7.0 8.0 9.0 10.0 11.0 12.0 13.0 14.0 15.0 16.0 17.0 18.0 19.0 20.0 21.0'
[../]
[./stress]
type = ComputeStrainIncrementBasedStress
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = diffused
boundary = '1'
value = 1
[../]
[./top]
type = DirichletBC
variable = diffused
boundary = '2'
value = 0
[../]
[./disp_x_BC]
type = DirichletBC
variable = disp_x
boundary = '0 1 2 3'
value = 0.0
[../]
[./disp_y_BC]
type = DirichletBC
variable = disp_y
boundary = '0 1 2 3'
value = 0.0
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/rz_cone_by_parts_steady_stabilized_second_order.i)
# This input file tests several different things:
# .) The axisymmetric (RZ) form of the governing equations.
# .) An open boundary.
# .) Not integrating the pressure by parts, thereby requiring a pressure pin.
# .) Natural boundary condition at the outlet.
[GlobalParams]
integrate_p_by_parts = true
laplace = true
gravity = '0 0 0'
supg = true
pspg = true
order = SECOND
[]
[Mesh]
file = '2d_cone.msh'
[]
[Problem]
coord_type = RZ
[]
[Preconditioning]
[./SMP_PJFNK]
type = SMP
full = true
solve_type = Newton
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = 'bjacobi ilu 4'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
csv = true
console = true
[./out]
type = Exodus
[../]
[]
[Variables]
[./vel_x]
# Velocity in radial (r) direction
[../]
[./vel_y]
# Velocity in axial (z) direction
[../]
[./p]
order = FIRST
[../]
[]
[BCs]
[./u_in]
type = DirichletBC
boundary = bottom
variable = vel_x
value = 0
[../]
[./v_in]
type = FunctionDirichletBC
boundary = bottom
variable = vel_y
function = 'inlet_func'
[../]
[./u_axis_and_walls]
type = DirichletBC
boundary = 'left right'
variable = vel_x
value = 0
[../]
[./v_no_slip]
type = DirichletBC
boundary = 'right'
variable = vel_y
value = 0
[../]
[]
[Kernels]
[./mass]
type = INSMassRZ
variable = p
u = vel_x
v = vel_y
pressure = p
[../]
[./x_momentum_space]
type = INSMomentumLaplaceFormRZ
variable = vel_x
u = vel_x
v = vel_y
pressure = p
component = 0
[../]
[./y_momentum_space]
type = INSMomentumLaplaceFormRZ
variable = vel_y
u = vel_x
v = vel_y
pressure = p
component = 1
[../]
[]
[Materials]
[./const]
type = GenericConstantMaterial
block = 'volume'
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[]
[Functions]
[./inlet_func]
type = ParsedFunction
value = '-4 * x^2 + 1'
[../]
[]
[Postprocessors]
[./flow_in]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'bottom'
execute_on = 'timestep_end'
[../]
[./flow_out]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'top'
execute_on = 'timestep_end'
[../]
[]
(modules/combined/test/tests/heat_convection/heat_convection_rz_tf_test.i)
# Test cases for convective boundary conditions. TKLarson, 11/01/11, rev. 0.
# Input file for htc_2dtest0
# TKLarson
# 11/01/11
# Revision 0
#
# Goals of this test are:
# 1) show that the 'fluid' temperature for convective boundary condition
# is behaving as expected/desired
# 2) show that expected results ensue from application of convective boundary conditions
# Convective boundary condition:
# q = h*A*(Tw - Tf)
# where
# q - heat transfer rate (w)
# h - heat transfer coefficient (w/m^2-K)
# A - surface area (m^2)
# Tw - surface temperature (K)
# Tf - fluid temperature adjacent to the surface (K)
# The heat transfer coefficient (h) is input as a variable called 'rate'
# Tf is a two valued function specified by 'initial' and 'final' along with a variable
# called 'duration,' the length of time in seconds that it takes initial to linearly ramp
# to 'final.'
# The mesh for this test case is based on an ASTM standard for the so-called Brazillian Cylinder test
# (ASTM International, Standard Test Method for Splitting Tensile Strength of Cylindrical Concrete
# Specimens, C 496/C 496M-04, 2004) (because I already had a version of the model). While the
# Brazillian Cylinder test is for dynamic tensile testing of concrete, the model works for the present
# purposes. The model is 2-d RZ coordinates.
#
# Brazillian Cylinder sample dimensions:
# L = 20.3 cm, 0.203 m, (8 in)
# r = 5.08 cm, 0.0508 m, (2 in)
# Material properties are:
# density = 2405.28 km/m^3
# specific heat = 826.4 J/kg-K
# thermal conductivity 1.937 w/m-K
# alpha (thermal conductivity/(density*specific heat) is then 9.74e-7 m^2/s
#
# Initial cylinder temperature is room temperature 294.26 K (70 F)
# The initial fluid temperature is room temperature. We will ramp it to 477.6 K (400 F) in 10 minutes.
# We will use a very large h (1000000) to make the surface temperature mimick the fluid temperature.
# What we expect for this problem:
# 1) Use of h = 1000000 should cause the cylinder surface temperature to track the fluid temperature
# 2) The fluid temperature should rise from initial (294.26 K) to final (477.6 K) in 600 s.
# 3) 1) and 2) should prove that the Tf boundary condition is ramping as desired.
# Note, we do the above because there is no way to plot a variable that is not on a mesh node!
[Problem]
coord_type = RZ
[]
[Mesh] # Mesh Start
# 10cm x 20cm cylinder not so detailed mesh, 2 radial, 6 axial nodes
# Only one block (Block 1), all concrete
# Sideset 1 - top of cylinder, Sideset 2 - length of cylinder, Sideset 3 - bottom of cylinder
file = heat_convection_rz_mesh.e
[] # Mesh END
[Variables] # Variables Start
[./temp]
order = FIRST
family = LAGRANGE
initial_condition = 294.26 # Initial cylinder temperature
[../]
[] # Variables END
[Kernels] # Kernels Start
[./heat]
type = HeatConduction
variable = temp
[../]
[./heat_ie]
type = HeatConductionTimeDerivative
variable = temp
[../]
[] # Kernels END
[BCs] # Boundary Conditions Start
# Heat transfer coefficient on outer cylinder radius and ends
[./convective_clad_surface] # Convective Start
type = ConvectiveFluxBC # Convective flux, e.g. q'' = h*(Tw - Tf)
boundary = '1 2 3' # BC applied on top, along length, and bottom
variable = temp
rate = 1000000. # convective heat transfer coefficient (w/m^2-K)[176000 "]
# # the above h is ~ infinity for present purposes
initial = 294.26 # initial ambient (lab or oven) temperature (K)
final = 477.6 # final ambient (lab or oven) temperature (K)
duration = 600. # length of time in seconds that it takes the ambient
# temperature to ramp from initial to final
[../] # Convective End
[] # BCs END
[Materials] # Materials Start
[./thermal]
type = HeatConductionMaterial
block = 1
specific_heat = 826.4
thermal_conductivity = 1.937 # this makes alpha 9.74e-7 m^2/s
[../]
[./density]
type = Density
block = 1
density = 2405.28
[../]
[] # Materials END
[Executioner] # Executioner Start
type = Transient
# type = Steady
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew '
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type'
petsc_options_value = '70 hypre boomeramg'
l_max_its = 60
nl_rel_tol = 1e-8
nl_abs_tol = 1e-10
l_tol = 1e-5
start_time = 0.0
dt = 60.
num_steps = 20 # Total run time 1200 s
[] # Executioner END
[Outputs] # Output Start
# Output Start
file_base = out_rz_tf
exodus = true
[] # Output END
# # Input file END
(test/tests/fvkernels/mms/cylindrical/diffusion.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
[v]
family = MONOMIAL
order = CONSTANT
fv = true
[]
[]
[Problem]
coord_type = 'RZ'
[]
[FVKernels]
[diff_v]
type = FVDiffusion
variable = v
coeff = coeff
[]
[body_v]
type = FVBodyForce
variable = v
function = 'forcing'
[]
[]
[FVBCs]
[boundary]
type = FVFunctionDirichletBC
boundary = 'left right top bottom'
function = 'exact'
variable = v
[]
[]
[Materials]
[diff]
type = ADGenericFunctorMaterial
prop_names = 'coeff'
prop_values = '1'
[]
[]
[Functions]
[exact]
type = ParsedFunction
value = '1.1*sin(0.9*x)*cos(1.2*y)'
[]
[forcing]
type = ParsedFunction
value = '1.584*sin(0.9*x)*cos(1.2*y) - (-0.891*x*sin(0.9*x)*cos(1.2*y) + 0.99*cos(0.9*x)*cos(1.2*y))/x'
[]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[./error]
type = ElementL2Error
variable = v
function = exact
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(test/tests/outputs/format/output_test_tecplot.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
nz = 0
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
tecplot = true
[]
(test/tests/restart/pointer_restart_errors/pointer_load_error.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[UserObjects]
[./restartable_types]
type = PointerLoadError
[../]
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
checkpoint = true
[]
(test/tests/kernels/vector_fe/ad_lagrange_vec.i)
# This example reproduces the libmesh vector_fe example 1 results
[Mesh]
type = GeneratedMesh
dim = 2
nx = 15
ny = 15
xmin = -1
ymin = -1
elem_type = QUAD9
[]
[Variables]
[./u]
family = LAGRANGE_VEC
order = SECOND
[../]
[]
[Kernels]
[./diff]
type = ADVectorDiffusion
variable = u
[../]
[./body_force]
type = VectorBodyForce
variable = u
function_x = 'ffx'
function_y = 'ffy'
[../]
[]
[BCs]
[./bnd]
type = ADVectorFunctionDirichletBC
variable = u
function_x = 'x_exact_sln'
function_y = 'y_exact_sln'
boundary = 'left right top bottom'
[../]
[]
[Functions]
[./x_exact_sln]
type = ParsedFunction
value = 'cos(.5*pi*x)*sin(.5*pi*y)'
[../]
[./y_exact_sln]
type = ParsedFunction
value = 'sin(.5*pi*x)*cos(.5*pi*y)'
[../]
[./ffx]
type = ParsedFunction
value = '.5*pi*pi*cos(.5*pi*x)*sin(.5*pi*y)'
[../]
[./ffy]
type = ParsedFunction
value = '.5*pi*pi*sin(.5*pi*x)*cos(.5*pi*y)'
[../]
[]
[Preconditioning]
[./pre]
type = SMP
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(modules/ray_tracing/test/tests/userobjects/ray_tracing_study/bc_create_ray/bc_create_ray.i)
[Mesh]
active = gmg_2d
[gmg_2d]
type = GeneratedMeshGenerator
dim = 2
nx = 3
ny = 3
xmax = 3
ymax = 3
[]
[gmg_3d]
type = GeneratedMeshGenerator
dim = 3
nx = 3
ny = 3
nz = 3
xmax = 3
ymax = 3
zmax = 3
[]
[]
[RayBCs]
active = 'kill_2d create_2d'
[kill_2d]
type = KillRayBC
boundary = 'top right bottom left'
[]
[create_2d]
type = CreateRayRayBCTest
boundary = 'top right bottom left'
[]
[kill_3d]
type = KillRayBC
boundary = 'top right bottom left front back'
[]
[create_3d]
type = CreateRayRayBCTest
boundary = 'top right bottom left front back'
[]
[]
[UserObjects/lots]
type = LotsOfRaysRayStudy
execute_on = initial
vertex_to_vertex = true
centroid_to_vertex = true
centroid_to_centroid = true
ray_kernel_coverage_check = false
[]
[Postprocessors]
[total_distance]
type = RayTracingStudyResult
study = lots
result = total_distance
[]
[total_rays_started]
type = RayTracingStudyResult
study = lots
result = total_rays_started
[]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Outputs]
exodus = false
csv = true
[]
(modules/tensor_mechanics/test/tests/ad_action/two_block_new.i)
[Mesh]
[generated_mesh]
type = GeneratedMeshGenerator
dim = 2
nx = 4
ny = 4
[]
[block1]
type = SubdomainBoundingBoxGenerator
block_id = 1
bottom_left = '0 0 0'
top_right = '0.5 1 0'
input = generated_mesh
[]
[block2]
type = SubdomainBoundingBoxGenerator
block_id = 2
bottom_left = '0.5 0 0'
top_right = '1 1 0'
input = block1
[]
[]
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Modules/TensorMechanics/Master]
# parameters that apply to all subblocks are specified at this level. They
# can be overwritten in the subblocks.
add_variables = true
strain = FINITE
generate_output = 'stress_xx'
[./block1]
# the `block` parameter is only valid insde a subblock.
block = 1
use_automatic_differentiation = true
[../]
[./block2]
block = 2
# the `additional_generate_output` parameter is also only valid inside a
# subblock. Values specified here are appended to the `generate_output`
# parameter values.
additional_generate_output = 'strain_yy'
use_automatic_differentiation = true
[../]
[]
[AuxVariables]
[./stress_theta]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_theta]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./stress_theta]
type = ADRankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 2
variable = stress_theta
execute_on = timestep_end
[../]
[./strain_theta]
type = ADRankTwoAux
rank_two_tensor = total_strain
index_i = 2
index_j = 2
variable = strain_theta
execute_on = timestep_end
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1e10
poissons_ratio = 0.345
[../]
[./_elastic_stress1]
type = ADComputeFiniteStrainElasticStress
block = 1
[../]
[./_elastic_stress2]
type = ADComputeFiniteStrainElasticStress
block = 2
[../]
[]
[BCs]
[./left]
type = DirichletBC
boundary = 'left'
variable = disp_x
value = 0.0
[../]
[./top]
type = DirichletBC
boundary = 'top'
variable = disp_y
value = 0.0
[../]
[./right]
type = DirichletBC
boundary = 'right'
variable = disp_x
value = 0.01
[../]
[./bottom]
type = DirichletBC
boundary = 'bottom'
variable = disp_y
value = 0.01
[../]
[]
[Debug]
show_var_residual_norms = true
[]
[Preconditioning]
[./full]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = ' 201 hypre boomeramg 10'
line_search = 'none'
nl_rel_tol = 5e-9
nl_abs_tol = 1e-10
nl_max_its = 15
l_tol = 1e-3
l_max_its = 50
[]
[Outputs]
exodus = true
[]
(test/tests/utils/libtorch_nn/test.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
[]
[]
[UserObjects]
[test]
type = LibtorchArtificialNeuralNetTest
activation_functions = 'relu relu'
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
(test/tests/misc/check_error/assertion_test.i)
[Mesh]
file = square.e # Read a Mesh
[./Generation] # AND create a Mesh...
dim = 2
nx = 2
ny = 2
nz = 0
zmin = 0
zmax = 0
elem_type = QUAD4
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Materials]
active = empty
[./empty]
type = EmptyMaterial
block = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/kernels/2d_diffusion/2d_diffusion_test.i)
###########################################################
# This is a simple test of the Kernel System.
# It solves the Laplacian equation on a small 2x2 grid.
# The "Diffusion" kernel is used to calculate the
# residuals of the weak form of this operator.
#
# @Requirement F3.30
###########################################################
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
# BCs cannot be preset due to Jacobian test
active = 'left right'
[./left]
type = DirichletBC
variable = u
preset = false
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
preset = false
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/userobjects/nearest_point_layered_integral/nearest_point_layered_integral.i)
[Mesh]
type = GeneratedMesh
dim = 3
xmax = 1.5
ymax = 1.5
zmax = 1.2
nx = 10
ny = 10
nz = 10
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./np_layered_average]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./np_layered_average]
type = SpatialUserObjectAux
variable = np_layered_average
execute_on = timestep_end
user_object = npla
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./one]
type = DirichletBC
variable = u
boundary = 'right back top'
value = 1
[../]
[]
[UserObjects]
[./npla]
type = NearestPointLayeredIntegral
direction = y
num_layers = 10
variable = u
points_file = points.txt
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/radiation_transfer_symmetry/cavity_with_pillars_symmetry_bc.i)
#
# inner_left: 8
# inner_top: 11
# inner_bottom: 10
# inner_front: 9
# back_2: 7
# obstruction: 6
#
[Mesh]
[cartesian]
type = CartesianMeshGenerator
dim = 3
dx = '0.4 0.5 0.5 0.5'
dy = '0.5 0.75 0.5'
dz = '1.5 0.5'
subdomain_id = '
3 1 1 1
3 1 2 1
3 1 1 1
3 1 1 1
3 1 1 1
3 1 1 1
'
[]
[add_obstruction]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 2
paired_block = 1
new_boundary = obstruction
input = cartesian
[]
[add_new_back]
type = ParsedGenerateSideset
combinatorial_geometry = 'abs(z) < 1e-10'
included_subdomain_ids = '1'
normal = '0 0 -1'
new_sideset_name = back_2
input = add_obstruction
[]
[add_inner_left]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 3
paired_block = 1
new_boundary = inner_left
input = add_new_back
[]
[add_inner_front]
type = ParsedGenerateSideset
combinatorial_geometry = 'abs(z - 2) < 1e-10'
included_subdomain_ids = '1'
normal = '0 0 1'
new_sideset_name = inner_front
input = add_inner_left
[]
[add_inner_bottom]
type = ParsedGenerateSideset
combinatorial_geometry = 'abs(y) < 1e-10'
included_subdomain_ids = '1'
normal = '0 -1 0'
new_sideset_name = inner_bottom
input = add_inner_front
[]
[add_inner_top]
type = ParsedGenerateSideset
combinatorial_geometry = 'abs(y - 1.75) < 1e-10'
included_subdomain_ids = '1'
normal = '0 1 0'
new_sideset_name = inner_top
input = add_inner_bottom
[]
[]
[Problem]
kernel_coverage_check = false
[]
[Variables]
[temperature]
block = '2 3'
initial_condition = 300
[]
[]
[Kernels]
[conduction]
type = HeatConduction
variable = temperature
block = '2 3'
diffusion_coefficient = 1
[]
[source]
type = BodyForce
variable = temperature
value = 1000
block = '2'
[]
[]
[BCs]
[convective]
type = CoupledConvectiveHeatFluxBC
variable = temperature
T_infinity = 300
htc = 50
boundary = 'left'
[]
[]
[GrayDiffuseRadiation]
[./cavity]
boundary = '6 7 8 9 10 11'
emissivity = '1 1 1 1 1 1'
n_patches = '1 1 1 1 1 1'
adiabatic_boundary = '7 9 10 11'
symmetry_boundary = '2'
partitioners = 'metis metis metis metis metis metis'
temperature = temperature
ray_tracing_face_order = SECOND
normalize_view_factor = false
[../]
[]
[Postprocessors]
[Tpv]
type = PointValue
variable = temperature
point = '0.3 0.5 0.5'
[]
[volume]
type = VolumePostprocessor
[]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/reactor/test/tests/meshgenerators/reporting_id/cartesian_id/core_zigzag_reporting_id.i)
[Mesh]
[pin1]
type = ConcentricCircleMeshGenerator
num_sectors = 2
radii = '0.4 0.5'
rings = '1 1 1'
has_outer_square = on
pitch = 1.26
preserve_volumes = yes
smoothing_max_it = 3
[]
[pin2]
type = ConcentricCircleMeshGenerator
num_sectors = 2
radii = '0.3 0.4'
rings = '1 1 1'
has_outer_square = on
pitch = 1.26
preserve_volumes = yes
smoothing_max_it = 3
[]
[pin_dummy]
type = RenameBlockGenerator
input = 'pin1'
old_block = '1 2 3'
new_block = '9999 9999 9999'
[]
[assembly1]
type = CartesianIDPatternedMeshGenerator
inputs = 'pin1 pin2'
pattern = ' 1 0 1 0;
0 1 0 1;
1 0 1 0;
0 1 0 1'
assign_type = 'cell'
id_name = 'pin_id'
[]
[assembly2]
type = CartesianIDPatternedMeshGenerator
inputs = 'pin1 pin2'
pattern = ' 0 1 1 0;
1 0 0 1;
1 0 0 1;
0 1 1 0'
assign_type = 'cell'
id_name = 'pin_id'
[]
[assembly_dummy]
type = CartesianIDPatternedMeshGenerator
inputs = 'pin_dummy'
pattern = ' 0 0 0 0;
0 0 0 0;
0 0 0 0;
0 0 0 0'
assign_type = 'cell'
id_name = 'pin_id'
[]
[core_base]
type = CartesianIDPatternedMeshGenerator
inputs = 'assembly1 assembly2 assembly_dummy'
pattern = '0 1;
2 0'
assign_type = 'cell'
id_name = 'assembly_id'
exclude_id = 'assembly_dummy'
[]
[core]
type = BlockDeletionGenerator
input = 'core_base'
block = 9999 # dummy
new_boundary = 'zagged'
[]
final_generator = core
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[AuxVariables]
[pin_id]
family = MONOMIAL
order = CONSTANT
[]
[assembly_id]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[set_pin_id]
type = ExtraElementIDAux
variable = pin_id
extra_id_name = pin_id
[]
[set_assembly_id]
type = ExtraElementIDAux
variable = assembly_id
extra_id_name = assembly_id
[]
[]
[Outputs]
exodus = true
execute_on = timestep_end
[]
(modules/richards/test/tests/jacobian_1/jn04.i)
# unsaturated = true
# gravity = true
# supg = false
# transient = false
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = -1
xmax = 1
ymin = -1
ymax = 1
zmin = -1
zmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0 # notice small quantity, so the PETSc constant state works
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1 # notice small quantity, so the PETSc constant state works
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.2
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGnone]
type = RichardsSUPGnone
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = RandomIC
block = 0
min = -1
max = 0
[../]
[../]
[]
[Kernels]
active = 'richardsf'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGnone
sat_UO = Saturation
seff_UO = SeffVG
viscosity = 1E-3
gravity = '1 2 3'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -snes_type'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000 test'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = jn04
exodus = false
[]
(test/tests/materials/discrete/recompute_warning.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 1
[]
[./left_domain]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '0 0 0'
top_right = '0.5 1 0'
block_id = 10
[../]
[]
[Variables]
[./u]
initial_condition = 2
[../]
[]
[Kernels]
[./diff]
type = MatDiffusionTest
variable = u
prop_name = 'p'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 2
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 3
[../]
[]
[Materials]
[./recompute_props]
type = GenericConstantMaterial
prop_names = 'f f_prime'
prop_values = '22 24'
block = 0
compute = true # the default, but should trigger a warning because newton is calling getMaterial on this
[../]
[./newton]
type = NewtonMaterial
block = 0
outputs = all
f_name = 'f'
f_prime_name = 'f_prime'
p_name = 'p'
material = recompute_props
max_iterations = 0
[../]
[./left]
type = GenericConstantMaterial
prop_names = 'f f_prime p'
prop_values = '1 0.5 1.2345'
block = 10
outputs = all
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
print_linear_residuals = true
perf_graph = true
[]
(modules/fluid_properties/test/tests/materials/saturation_pressure_material/saturation_pressure_material.i)
# This tests SaturationPressureMaterial, which computes a saturation pressure material
# property from a temperature material property and a TwoPhaseFluidProperties object.
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
xmin = 0
xmax = 1
[]
[Modules]
[FluidProperties]
[fp_2phase]
type = StiffenedGasTwoPhaseFluidProperties
[]
[]
[]
[Materials]
[T_mat]
type = ADGenericConstantMaterial
prop_names = 'T'
prop_values = '400'
[]
[p_sat_mat]
type = ADSaturationPressureMaterial
T = T
p_sat = p_sat
fp_2phase = fp_2phase
[]
[]
[Postprocessors]
[p_sat_pp]
type = ADElementAverageMaterialProperty
mat_prop = p_sat
execute_on = 'INITIAL'
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
execute_on = 'INITIAL'
[]
(test/tests/fvkernels/mms/mat-advection.i)
a=1.1
[GlobalParams]
advected_interp_method = 'average'
[]
[Mesh]
[./gen_mesh]
type = GeneratedMeshGenerator
dim = 1
xmin = -0.6
xmax = 0.6
nx = 2
[../]
[]
[Variables]
[./v]
family = MONOMIAL
order = CONSTANT
fv = true
[../]
[]
[FVKernels]
[./advection]
type = FVMatAdvection
variable = v
vel = 'fv_velocity'
[../]
[body_v]
type = FVBodyForce
variable = v
function = 'forcing'
[]
[]
[FVBCs]
[boundary]
type = FVMatAdvectionFunctionBC
boundary = 'left right'
variable = v
vel = 'fv_velocity'
flux_variable_exact_solution = 'exact'
vel_x_exact_solution = '${a}'
[]
[]
[Materials]
[adv_material]
type = ADCoupledVelocityMaterial
vel_x = '${a}'
rho = 'v'
velocity = 'fv_velocity'
[]
[]
[Functions]
[exact]
type = ParsedFunction
value = '1.1 * sin(1.1 * x)'
[]
[forcing]
type = ParsedFunction
value = '${a} * 1.1 * 1.1 * cos(1.1 * x)'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm NONZERO'
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[./error]
type = ElementL2Error
variable = v
function = exact
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(test/tests/mesh_modifiers/add_side_sets_from_bounding_box/add_side_sets_from_bounding_box.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[createNewSidesetOne]
type = SideSetsFromBoundingBoxGenerator
input = gen
block_id = 0
boundary_id_old = 'left'
boundary_id_new = 10
bottom_left = '-0.1 -0.1 0'
top_right = '0.5 0.5 0'
[]
[createNewSidesetTwo]
type = SideSetsFromBoundingBoxGenerator
input = createNewSidesetOne
block_id = 0
boundary_id_old = 'right'
boundary_id_new = 11
bottom_left = '0.5 0.5 0'
top_right = '1.1 1.1 0'
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[leftBC]
type = DirichletBC
variable = u
boundary = 10
value = 1
[]
[rightBC]
type = DirichletBC
variable = u
boundary = 11
value = 0
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/iterative/iterative_steady.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
preset = false
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
preset = false
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
[./out]
type = Exodus
execute_on = 'initial timestep_end failed nonlinear linear'
sequence = false
[../]
[]
(test/tests/meshgenerators/rename_block_generator/rename_block.i)
[Mesh]
[gmg]
type = CartesianMeshGenerator
dim = 2
dx = '1 1'
dy = '1 1'
ix = '2 2'
iy = '2 2'
subdomain_id = '0 1 2 3'
[]
[set_names]
type = RenameBlockGenerator
old_block = '0 1 2 3'
new_block = 'block0 block1 block2 block3'
input = gmg
[]
# Rename parameters supplied through the "tests" specifications
[rename]
type = RenameBlockGenerator
input = set_names
[]
# We compare by element numbers, which are not consistent in parallel
# if this is true
allow_renumbering = false
[]
[Reporters/mesh_info]
type = MeshInfo
items = subdomain_elems
[]
[Outputs/out]
type = JSON
execute_system_information_on = NONE
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
(test/tests/preconditioners/fsp/fsp_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u v'
[./u]
order = FIRST
family = LAGRANGE
[../]
[./v]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff_u conv_v diff_v'
[./diff_u]
type = Diffusion
variable = u
[../]
[./conv_v]
type = CoupledForce
variable = v
v = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[BCs]
active = 'left_u right_u left_v'
[./left_u]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 100
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = 3
value = 0
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Steady
# This is setup automatically in MOOSE (SetupPBPAction.C)
# petsc_options = '-snes_mf_operator'
# petsc_options_iname = '-pc_type'
# petsc_options_value = 'asm'
[]
[Preconditioning]
active = 'FSP'
[./FSP]
type = FSP
# It is the starting point of splitting
topsplit = 'uv' # 'uv' should match the following block name
[./uv]
splitting = 'u v' # 'u' and 'v' are the names of subsolvers
# Generally speaking, there are four types of splitting we could choose
# <additive,multiplicative,symmetric_multiplicative,schur>
splitting_type = additive
# An approximate solution to the original system
# | A_uu A_uv | | u | _ |f_u|
# | 0 A_vv | | v | - |f_v|
# is obtained by solving the following subsystems
# A_uu u = f_u and A_vv v = f_v
# If splitting type is specified as schur, we may also want to set more options to
# control how schur works using PETSc options
# petsc_options_iname = '-pc_fieldsplit_schur_fact_type -pc_fieldsplit_schur_precondition'
# petsc_options_value = 'full selfp'
[../]
[./u]
vars = 'u'
# PETSc options for this subsolver
# A prefix will be applied, so just put the options for this subsolver only
petsc_options_iname = '-pc_type -ksp_type'
petsc_options_value = ' hypre preonly'
[../]
[./v]
vars = 'v'
# PETSc options for this subsolver
petsc_options_iname = '-pc_type -ksp_type'
petsc_options_value = ' hypre preonly'
[../]
[../]
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/materials/derivative_material_interface/warn.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
[]
[AuxVariables]
[./dummy]
[../]
[]
[Materials]
[./provider]
type = DerivativeMaterialInterfaceTestProvider
block = 0
[../]
[./client]
type = DerivativeMaterialInterfaceTestClient
prop_name = prop
block = 0
outputs = exodus
[../]
[./client2]
type = DerivativeMaterialInterfaceTestClient
prop_name = 1.0
block = 0
outputs = exodus
[../]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Outputs]
exodus = true
[]
(test/tests/reporters/constant_reporter/constant_reporter.i)
[Mesh/mesh]
type = GeneratedMeshGenerator
dim = 1
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[Reporters]
active = constant
[constant]
type = ConstantReporter
integer_names = 'int_1 int_2 int_3'
integer_values = '1 2 -3'
real_names = 'num_1 num_2'
real_values = '4.0 5.0'
string_names = 'str'
string_values = 'six'
dof_id_type_names = 'dofid_1 dofid_2 dofid_3'
dof_id_type_values = '1 2 3'
integer_vector_names = 'int_vec'
integer_vector_values = '7 8'
real_vector_names = 'vec_1 vec_2'
real_vector_values = '8.0 80.0 800.0; 9.0 90.0'
string_vector_names = 'str_vec'
string_vector_values = 'ten eleven twelve thirteen'
dof_id_type_vector_names = 'dofid_vec'
dof_id_type_vector_values = '7 3'
[]
[error]
type = ConstantReporter
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
execute_on = 'timestep_end'
[out]
type = JSON
execute_system_information_on = none
[]
[]
(test/tests/vectorpostprocessors/element_id_counters/element_counter.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
xmax = 1
ymax = 1
extra_element_integers = foo_id
[]
[subdomain0]
type = SubdomainBoundingBoxGenerator
input = gmg
bottom_left = '0 0 0'
block_id = 0
top_right = '1 1 0'
integer_name = foo_id
[]
[subdomain1]
type = SubdomainBoundingBoxGenerator
input = subdomain0
bottom_left = '0.4 0.4 0'
block_id = 1
top_right = '0.9 0.9 0'
integer_name = foo_id
[]
[subdomain2]
type = SubdomainBoundingBoxGenerator
input = subdomain1
bottom_left = '0.1 0.1 0'
block_id = 2
top_right = '0.6 0.6 0'
integer_name = foo_id
[]
[]
[VectorPostprocessors]
[elem_counter]
type = ElementCounterWithID
id_name = foo_id
[]
[elem_counter_subdomain]
type = ElementCounterWithID
id_name = subdomain_id
[]
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
execute_on = 'timestep_end'
[]
(modules/navier_stokes/test/tests/finite_volume/cns/userobject/HLLC/hllc_uo_2D_tri.i)
rho_left = 1.162633159
E_left = 2.1502913276e+05
v_left = 40
rho_right = 1.116127833
E_right = 1.7919094397e+05
v_right = 50
[Mesh]
[./cartesian]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 2
nx = 1
ny = 1
elem_type = 'TRI3'
[../]
[]
[Modules]
[./FluidProperties]
[./fp]
type = IdealGasFluidProperties
allow_imperfect_jacobians = true
[../]
[../]
[]
[Problem]
kernel_coverage_check = false
[]
[Variables]
[./rho]
order = CONSTANT
family = MONOMIAL
[../]
[./rho_v]
order = CONSTANT
family = MONOMIAL
[../]
[./rho_E]
order = CONSTANT
family = MONOMIAL
[../]
[]
[ICs]
[./rho_ic]
type = FunctionIC
variable = rho
function = 'if (y / (2 * x) < 0.5, ${rho_left}, ${rho_right})'
[../]
[./rho_v_ic]
type = FunctionIC
variable = rho_v
function = 'if (y / (2 * x) < 0.5, ${fparse rho_left * v_left}, ${fparse rho_right * v_right})'
[../]
[./rho_E_ic]
type = FunctionIC
variable = rho_E
function = 'if (y / (2 * x) < 0.5, ${fparse E_left * rho_left}, ${fparse E_right * rho_right})'
[../]
[]
[Materials]
[./var_mat]
type = ConservedVarValuesMaterial
rho = rho
rhou = 0
rhov = rho_v
rho_et = rho_E
fp = fp
[../]
[]
[UserObjects]
[./hllc]
type = HLLCUserObject
fp = fp
[../]
[]
[VectorPostprocessors]
[./wave_speeds]
type = WaveSpeedVPP
hllc_uo = hllc
elem_id = 0
side_id = 2
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
exodus = true
[]
(tutorials/tutorial02_multiapps/app/test/tests/kernels/simple_diffusion/simple_diffusion.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/fvkernels/mms/cylindrical/advection.i)
a=1.1
[Mesh]
[./gen_mesh]
type = GeneratedMeshGenerator
dim = 1
xmin = 2
xmax = 3
nx = 2
[../]
[]
[Problem]
coord_type = 'RZ'
[]
[Variables]
[./v]
family = MONOMIAL
order = CONSTANT
fv = true
initial_condition = 1
[../]
[]
[FVKernels]
# Flux kernel
[./advection]
type = FVAdvection
variable = v
velocity = '${a} 0 0'
advected_interp_method = 'average'
[../]
[body_v]
type = FVBodyForce
variable = v
function = 'forcing'
[]
[]
[FVBCs]
[advection]
type = FVAdvectionFunctionBC
boundary = 'left right'
exact_solution = 'exact'
variable = v
velocity = '${a} 0 0'
advected_interp_method = 'average'
[]
[]
[Functions]
[exact]
type = ParsedFunction
value = 'sin(x)'
[]
[forcing]
type = ParsedFunction
value = '(x*a*cos(x) + a*sin(x))/x'
vars = 'a'
vals = '${a}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_shift_type -sub_pc_type'
petsc_options_value = 'asm NONZERO lu'
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[./error]
type = ElementL2Error
variable = v
function = exact
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/rotated/rotated-pp-flow.i)
mu=0.5
rho=1.1
advected_interp_method='average'
velocity_interp_method='average'
two_term_boundary_expansion=true
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 10
ymin = -1
ymax = 1
nx = 10
ny = 2
[]
[rotate]
type = TransformGenerator
input = gen
transform = 'rotate'
vector_value = '45 0 0'
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[AuxVariables]
[vel_exact_x][]
[vel_exact_y][]
[p_exact][]
[]
[AuxKernels]
[u_exact]
type = FunctionAux
variable = vel_exact_x
function = exact_u
[]
[v_exact]
type = FunctionAux
variable = vel_exact_y
function = exact_v
[]
[p_exact]
type = FunctionAux
variable = p_exact
function = exact_p
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
two_term_boundary_expansion = ${two_term_boundary_expansion}
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
two_term_boundary_expansion = ${two_term_boundary_expansion}
[]
[pressure]
type = INSFVPressureVariable
two_term_boundary_expansion = ${two_term_boundary_expansion}
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[u_forcing]
type = INSFVBodyForce
variable = u
functor = forcing_u
momentum_component = 'x'
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[v_forcing]
type = INSFVBodyForce
variable = v
functor = forcing_v
momentum_component = 'y'
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = 'exact_u'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = 'exact_v'
[]
[walls-u]
type = INSFVNoSlipWallBC
variable = u
boundary = 'top bottom'
function = 'exact_u'
[]
[walls-v]
type = INSFVNoSlipWallBC
variable = v
boundary = 'top bottom'
function = 'exact_v'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 'exact_p'
[]
[]
[Functions]
[exact_u]
type = ParsedFunction
value = '0.25*sqrt(2)*(1.0 - 1/2*(-x + y)^2)/mu'
vars = 'mu'
vals = '${mu}'
[]
[exact_rhou]
type = ParsedFunction
value = '0.25*sqrt(2)*rho*(1.0 - 1/2*(-x + y)^2)/mu'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[forcing_u]
type = ADParsedFunction
value = '0'
[]
[exact_v]
type = ParsedFunction
value = '0.25*sqrt(2)*(1.0 - 1/2*(-x + y)^2)/mu'
vars = 'mu'
vals = '${mu}'
[]
[exact_rhov]
type = ParsedFunction
value = '0.25*sqrt(2)*rho*(1.0 - 1/2*(-x + y)^2)/mu'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[forcing_v]
type = ADParsedFunction
value = '0'
[]
[exact_p]
type = ParsedFunction
value = '-1/2*sqrt(2)*(x + y) + 10.0'
[]
[forcing_p]
type = ParsedFunction
value = '0'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
[]
[Outputs]
exodus = true
csv = true
[dof]
type = DOFMap
execute_on = 'initial'
[]
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[./L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2v]
type = ElementL2Error
variable = v
function = exact_v
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2p]
variable = pressure
function = exact_p
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[]
(tutorials/darcy_thermo_mech/step03_darcy_material/tests/kernels/darcy_pressure/darcy_pressure.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 100
ny = 10
xmax = 0.304 # Length of test chamber
ymax = 0.0257 # Test chamber radius
[]
[Variables]
[pressure]
[]
[]
[Kernels]
[darcy_pressure]
type = DarcyPressure
variable = pressure
[]
[]
[BCs]
[inlet]
type = DirichletBC
variable = pressure
boundary = left
value = 4000 # (Pa) From Figure 2 from paper. First dot for 1mm spheres.
[]
[outlet]
type = DirichletBC
variable = pressure
boundary = right
value = 0 # (Pa) Gives the correct pressure drop from Figure 2 for 1mm spheres
[]
[]
[Materials]
[pressure]
type = ADGenericConstantMaterial
prop_values = '0.8451e-9 7.98e-4'
prop_names = 'permeability viscosity'
[]
[]
[Problem]
type = FEProblem
coord_type = RZ
rz_coord_axis = X
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/thermal_hydraulics/test/tests/jacobians/bcs/convection_heat_transfer_rz_bc/convection_heat_transfer_rz_bc.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
[]
[Variables]
[T]
initial_condition = 300
[]
[]
[BCs]
[bc]
type = ConvectionHeatTransferRZBC
variable = T
boundary = 2
htc_ambient = 0.5
T_ambient = 400
axis_point = '0 0 0'
axis_dir = '1 0 0'
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Problem]
kernel_coverage_check = false
[]
[Executioner]
type = Steady
petsc_options = '-snes_test_jacobian'
petsc_options_iname = '-snes_test_error'
petsc_options_value = '1e-8'
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-scalar-transport.i)
mu=1
rho=1
k=1e-3
diff=1e-3
cp=1
advected_interp_method='average'
velocity_interp_method='rc'
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 10
ymin = -1
ymax = 1
nx = 100
ny = 20
[]
[]
[AuxVariables]
[U]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[]
[AuxKernels]
[mag]
type = VectorMagnitudeAux
variable = U
x = vel_x
y = vel_y
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = 1
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[T_fluid]
type = INSFVEnergyVariable
[]
[scalar]
type = INSFVScalarFieldVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
[]
[energy_advection]
type = INSFVEnergyAdvection
variable = T_fluid
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
[]
[energy_diffusion]
type = FVDiffusion
coeff = ${k}
variable = T_fluid
[]
[scalar_advection]
type = INSFVScalarFieldAdvection
variable = scalar
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
[]
[scalar_diffusion]
type = FVDiffusion
coeff = ${diff}
variable = scalar
[]
[scalar_src]
type = FVBodyForce
variable = scalar
value = 0.1
[]
[scalar_coupled_source]
type = FVCoupledForce
variable = scalar
v = U
coef = 0.1
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_x
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_y
function = 0
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = vel_x
function = 0
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = vel_y
function = 0
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 0
[]
[inlet_t]
type = FVDirichletBC
boundary = 'left'
variable = T_fluid
value = 1
[]
[inlet_scalar]
type = FVDirichletBC
boundary = 'left'
variable = scalar
value = 1
[]
[]
[Materials]
[const]
type = ADGenericFunctorMaterial
prop_names = 'cp'
prop_values = '${cp}'
[]
[ins_fv]
type = INSFVEnthalpyMaterial
rho = ${rho}
temperature = 'T_fluid'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[]
(test/tests/postprocessors/function_element_integral/function_element_integral.i)
dx = 2
y1 = 3
y2 = 6
y3 = 8
integral = ${fparse dx * ((y1 + y2) * 0.5 + (y2 + y3) * 0.5)}
[Mesh]
type = GeneratedMesh
dim = 1
nx = 2
xmax = 4
[]
[Functions]
[./function]
type = PiecewiseLinear
axis = x
x = '0 2 4'
y = '${y1} ${y2} ${y3}'
[../]
[]
[Postprocessors]
[./integral_pp]
type = FunctionElementIntegral
function = function
execute_on = 'initial'
[../]
[./integral_rel_err]
type = RelativeDifferencePostprocessor
value1 = integral_pp
value2 = ${integral}
execute_on = 'initial'
[../]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
show = 'integral_rel_err'
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-rc-no-slip-outflow-bcs.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 10
ymin = -1
ymax = 1
nx = 100
ny = 20
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = 1
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_x
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_y
function = '0'
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = vel_x
function = 0
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = vel_y
function = 0
[]
[outlet_u]
type = INSFVMomentumAdvectionOutflowBC
variable = vel_x
u = vel_x
v = vel_y
boundary = 'right'
momentum_component = 'x'
rho = ${rho}
[]
[outlet_v]
type = INSFVMomentumAdvectionOutflowBC
variable = vel_y
u = vel_x
v = vel_y
boundary = 'right'
momentum_component = 'y'
rho = ${rho}
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = '0'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 200 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[dof]
type = DOFMap
execute_on = 'initial'
[]
[]
(test/tests/dirackernels/material_point_source/material_error_check.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
elem_type = QUAD4
uniform_refine = 4
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[DiracKernels]
[./material_source]
type = MaterialPointSource
variable = u
point = '0.2 0.3 0.0'
material_prop = 'diffusivity'
prop_state = 'old'
[../]
[]
[Materials]
[./stateful]
type = StatefulMaterial
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/utils/param_error/param_error.i)
[Mesh/gen]
type = GeneratedMeshGenerator
dim =1
[]
[Variables/u]
[]
[Kernels]
[diffusion]
type = CoeffParamDiffusion
variable = u
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
(test/tests/interfacekernels/hybrid/interface.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 40
xmax = 2
ny = 40
ymax = 2
[]
[subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '0.5 0.5 0'
top_right = '1.5 1.5 0'
block_id = 1
[]
[interface]
type = SideSetsBetweenSubdomainsGenerator
input = subdomain1
primary_block = '1'
paired_block = '0'
new_boundary = 'primary1_interface'
[]
[]
[Variables]
[u]
block = 0
[]
[v]
block = 1
[]
[]
[Kernels]
[diff_u]
type = MatDiffusion
variable = u
diffusivity = D
block = 0
[]
[diff_v]
type = MatDiffusion
variable = v
diffusivity = D
block = 1
[]
[source_u]
type = BodyForce
variable = u
value = 1
block = 0
[]
[source_v]
type = BodyForce
variable = v
value = 1
block = 1
[]
[]
[BCs]
[u]
type = VacuumBC
variable = u
boundary = 'left bottom right top'
[]
[interface_bc]
type = ADMatchedValueBC
variable = v
v = u
boundary = primary1_interface
[]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
print_linear_residuals = true
[]
[InterfaceKernels]
active = 'diffusion'
[./diffusion]
type = InterfaceDiffusion
variable = v
neighbor_var = u
boundary = primary1_interface
D = 'D'
D_neighbor = 'D'
[../]
[./penalty]
type = PenaltyInterfaceDiffusion
variable = v
neighbor_var = u
boundary = primary1_interface
penalty = 1e3
[../]
[]
[Materials]
[mat0]
type = GenericConstantMaterial
prop_names = 'D'
prop_values = '1'
block = 0
[]
[mat1]
type = GenericConstantMaterial
prop_names = 'D'
prop_values = '1'
block = 1
[]
[]
[AuxVariables]
[c][]
[]
[AuxKernels]
[u]
type = ParsedAux
variable = c
args = 'u'
function = 'u'
block = 0
[]
[v]
type = ParsedAux
variable = c
args = 'v'
function = 'v'
block = 1
[]
[]
(test/tests/misc/execute_on/execute_on_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmax = 1
ymax = 1
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[AuxVariables]
[./initial]
[../]
[./timestep_begin]
[../]
[./timestep_end]
[../]
[./nonlinear]
[../]
[./linear]
[../]
[./custom]
initial_condition = 999
[../]
[]
[AuxKernels]
[./initial]
type = CheckCurrentExecAux
variable = initial
execute_on = initial
[../]
[./timestep_begin]
type = CheckCurrentExecAux
variable = timestep_begin
execute_on = timestep_begin
[../]
[./timestep_end]
type = CheckCurrentExecAux
variable = timestep_end
execute_on = timestep_end
[../]
[./nonlinear]
type = CheckCurrentExecAux
variable = nonlinear
execute_on = nonlinear
[../]
[./linear]
type = CheckCurrentExecAux
variable = linear
execute_on = linear
[../]
[./custom]
# this kernel will be never executed by Steady, so the initial value of this variable is not going to change
type = CheckCurrentExecAux
variable = custom
execute_on = custom
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/auxkernels/solution_aux/aux_nonlinear_solution.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./u_aux]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./aux_kernel]
type = FunctionAux
function = x*y
variable = u_aux
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
nl_rel_tol = 1e-10
[]
[Outputs]
exodus = true
xda = true
[./xdr]
type = XDR
[../]
[]
(test/tests/mesh_modifiers/mesh_extruder/extrude_remap_layer1.i)
[Mesh]
[file]
type = FileMeshGenerator
file = multiblock.e
[]
[extrude]
type = MeshExtruderGenerator
input = file
num_layers = 6
extrusion_vector = '0 0 2'
bottom_sideset = 'new_bottom'
top_sideset = 'new_top'
# Remap layers
existing_subdomains = '1 2 5'
layers = '1 3 5'
new_ids = '10 12 15
30 32 35
50 52 55'
[]
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[bottom]
type = DirichletBC
variable = u
boundary = 'new_bottom'
value = 0
[]
[top]
type = DirichletBC
variable = u
boundary = 'new_top'
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/heated/2d-rc-heated-effective.i)
mu=1
rho=1
k=1e-3
cp=1
u_inlet=1
T_inlet=200
advected_interp_method='average'
velocity_interp_method='rc'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 10
ymin = 0
ymax = 1
nx = 100
ny = 20
[]
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = PINSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
porosity = porosity
[]
[]
[Variables]
inactive = 'temp_solid'
[u]
type = PINSFVSuperficialVelocityVariable
initial_condition = ${u_inlet}
[]
[v]
type = PINSFVSuperficialVelocityVariable
initial_condition = 1e-6
[]
[pressure]
type = INSFVPressureVariable
[]
[temperature]
type = INSFVEnergyVariable
[]
[temp_solid]
family = 'MONOMIAL'
order = 'CONSTANT'
fv = true
[]
[]
[AuxVariables]
[temp_solid]
family = 'MONOMIAL'
order = 'CONSTANT'
fv = true
initial_condition = 100
[]
[porosity]
family = MONOMIAL
order = CONSTANT
fv = true
initial_condition = 0.5
[]
[]
[FVKernels]
inactive = 'solid_energy_diffusion solid_energy_convection'
[mass]
type = PINSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = PINSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
porosity = porosity
momentum_component = 'x'
[]
[u_viscosity]
type = PINSFVMomentumDiffusion
variable = u
mu = ${mu}
porosity = porosity
momentum_component = 'x'
[]
[u_pressure]
type = PINSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
porosity = porosity
[]
[v_advection]
type = PINSFVMomentumAdvection
variable = v
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
porosity = porosity
momentum_component = 'y'
[]
[v_viscosity]
type = PINSFVMomentumDiffusion
variable = v
mu = ${mu}
porosity = porosity
momentum_component = 'y'
[]
[v_pressure]
type = PINSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
porosity = porosity
[]
[energy_advection]
type = PINSFVEnergyAdvection
variable = temperature
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
[]
[energy_diffusion]
type = PINSFVEnergyAnisotropicDiffusion
kappa = 'kappa'
variable = temperature
porosity = porosity
[]
[energy_convection]
type = PINSFVEnergyAmbientConvection
variable = temperature
is_solid = false
T_fluid = temperature
T_solid = temp_solid
h_solid_fluid = 'h_cv'
[]
[solid_energy_diffusion]
type = FVDiffusion
coeff = ${k}
variable = temp_solid
[]
[solid_energy_convection]
type = PINSFVEnergyAmbientConvection
variable = temp_solid
is_solid = true
T_fluid = temperature
T_solid = temp_solid
h_solid_fluid = 'h_cv'
[]
[]
[FVBCs]
inactive = 'heated-side'
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = ${u_inlet}
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = 0
[]
[inlet-T]
type = FVNeumannBC
variable = temperature
value = ${fparse u_inlet * rho * cp * T_inlet}
boundary = 'left'
[]
[no-slip-u]
type = INSFVNoSlipWallBC
boundary = 'top'
variable = u
function = 0
[]
[no-slip-v]
type = INSFVNoSlipWallBC
boundary = 'top'
variable = v
function = 0
[]
[heated-side]
type = FVDirichletBC
boundary = 'top'
variable = 'temp_solid'
value = 150
[]
[symmetry-u]
type = PINSFVSymmetryVelocityBC
boundary = 'bottom'
variable = u
u = u
v = v
mu = ${mu}
momentum_component = 'x'
[]
[symmetry-v]
type = PINSFVSymmetryVelocityBC
boundary = 'bottom'
variable = v
u = u
v = v
mu = ${mu}
momentum_component = 'y'
[]
[symmetry-p]
type = INSFVSymmetryPressureBC
boundary = 'bottom'
variable = pressure
[]
[outlet-p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 0.1
[]
[]
[Materials]
[constants]
type = ADGenericFunctorMaterial
prop_names = 'h_cv'
prop_values = '1'
[]
[functor_constants]
type = ADGenericFunctorMaterial
prop_names = 'cp'
prop_values = '${cp}'
[]
[kappa]
type = ADGenericVectorFunctorMaterial
prop_names = 'kappa'
prop_values = '1e-3 1e-2 1e-1'
[]
[ins_fv]
type = INSFVEnthalpyMaterial
rho = ${rho}
temperature = 'temperature'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
# Some basic Postprocessors to examine the solution
[Postprocessors]
[inlet-p]
type = SideAverageValue
variable = pressure
boundary = 'left'
[]
[outlet-u]
type = SideAverageValue
variable = u
boundary = 'right'
[]
[outlet-temp]
type = SideAverageValue
variable = temperature
boundary = 'right'
[]
[solid-temp]
type = ElementAverageValue
variable = temp_solid
[]
[]
[Outputs]
exodus = true
csv = false
[]
(test/tests/misc/check_error/dirac_kernel_with_aux_var.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./v]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./rea]
type = Reaction
variable = u
[../]
[]
[DiracKernels]
[./nope]
type = CachingPointSource
variable = v
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/postprocessors/side_diffusive_flux_integral/side_diffusive_flux_integral.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Functions]
[./right_bc]
# Flux BC for computing the analytical solution in the postprocessor
type = ParsedFunction
value = exp(y)+1
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = FunctionNeumannBC
variable = u
boundary = right
function = right_bc
[../]
[]
[Materials]
[./mat_props]
type = GenericConstantMaterial
block = 0
prop_names = diffusivity
prop_values = 2
[../]
[./mat_props_bnd]
type = GenericConstantMaterial
boundary = right
prop_names = diffusivity
prop_values = 1
[../]
[./mat_props_vector]
type = GenericConstantVectorMaterial
boundary = 'right top'
prop_names = diffusivity_vec
prop_values = '1 1.5 1'
[../]
[]
[Postprocessors]
inactive = 'avg_flux_top'
[./avg_flux_right]
# Computes -\int(exp(y)+1) from 0 to 1 which is -2.718281828
type = SideDiffusiveFluxIntegral
variable = u
boundary = right
diffusivity = diffusivity
[../]
[./avg_flux_top]
type = SideVectorDiffusivityFluxIntegral
variable = u
boundary = top
diffusivity = diffusivity_vec
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/bad_parsed_function_vars.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
nz = 2
[]
[Variables]
[./u]
block = 0
[../]
[]
[Functions]
[./sin_func]
type = ParsedFunction
value = sin(y)
vars = y # <- This is a bad - you can't specify x, y, z, or t
vals = 0
[../]
[]
[Kernels]
[./diffused]
type = Diffusion
variable = u
block = 0
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 1
[../]
[./right]
type = FunctionDirichletBC
variable = u
boundary = right
function = sin_func
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_balance/large_gap_heat_transfer_test_rz_cylinder.i)
rpv_core_gap_size = 0.2
core_outer_radius = 2
rpv_inner_radius = '${fparse 2 + rpv_core_gap_size}'
rpv_outer_radius = '${fparse 2.5 + rpv_core_gap_size}'
rpv_width = '${fparse rpv_outer_radius - rpv_inner_radius}'
rpv_outer_htc = 10 # W/m^2/K
rpv_outer_Tinf = 300 # K
core_blocks = '1'
rpv_blocks = '3'
[Mesh]
[gmg]
type = CartesianMeshGenerator
dim = 2
dx = '${core_outer_radius} ${rpv_core_gap_size} ${rpv_width}'
ix = '400 1 100'
dy = 1
iy = '5'
[]
[set_block_id1]
type = SubdomainBoundingBoxGenerator
input = gmg
bottom_left = '0 0 0'
top_right = '${core_outer_radius} 1 0'
block_id = 1
location = INSIDE
[]
[rename_core_bdy]
type = SideSetsBetweenSubdomainsGenerator
input = set_block_id1
primary_block = 1
paired_block = 0
new_boundary = 'core_outer'
[]
[set_block_id3]
type = SubdomainBoundingBoxGenerator
input = rename_core_bdy
bottom_left = '${rpv_inner_radius} 0 0'
top_right = '${rpv_outer_radius} 1 0'
block_id = 3
location = INSIDE
[]
[rename_inner_rpv_bdy]
type = SideSetsBetweenSubdomainsGenerator
input = set_block_id3
primary_block = 3
paired_block = 0
new_boundary = 'rpv_inner'
[]
# comment out for test without gap
[2d_mesh]
type = BlockDeletionGenerator
input = rename_inner_rpv_bdy
block = 0
[]
[]
[Problem]
coord_type = RZ
[]
[Variables]
[Tsolid]
initial_condition = 500
[]
[]
[Kernels]
[heat_source]
type = CoupledForce
variable = Tsolid
block = '${core_blocks}'
v = power_density
[]
[heat_conduction]
type = HeatConduction
variable = Tsolid
[]
[]
[BCs]
[RPV_out_BC] # k \nabla T = h (T- T_inf) at RPV outer boundary
type = ConvectiveFluxFunction # (Robin BC)
variable = Tsolid
boundary = 'right' # outer RPV
coefficient = ${rpv_outer_htc}
T_infinity = ${rpv_outer_Tinf}
[]
[]
[ThermalContact]
[RPV_gap]
type = GapHeatTransfer
gap_geometry_type = 'CYLINDER'
emissivity_primary = 0.8
emissivity_secondary = 0.8
variable = Tsolid
primary = 'core_outer'
secondary = 'rpv_inner'
gap_conductivity = 0.1
quadrature = true
[]
[]
[AuxVariables]
[power_density]
block = '${core_blocks}'
initial_condition = 50e3
[]
[]
[Materials]
[simple_mat]
type = HeatConductionMaterial
thermal_conductivity = 34.6 # W/m/K
[]
[]
[Postprocessors]
[Tcore_avg]
type = ElementAverageValue
variable = Tsolid
block = '${core_blocks}'
[]
[Tcore_max]
type = ElementExtremeValue
value_type = max
variable = Tsolid
block = '${core_blocks}'
[]
[Tcore_min]
type = ElementExtremeValue
value_type = min
variable = Tsolid
block = '${core_blocks}'
[]
[Trpv_avg]
type = ElementAverageValue
variable = Tsolid
block = '${rpv_blocks}'
[]
[Trpv_max]
type = ElementExtremeValue
value_type = max
variable = Tsolid
block = '${rpv_blocks}'
[]
[Trpv_min]
type = ElementExtremeValue
value_type = min
variable = Tsolid
block = '${rpv_blocks}'
[]
[ptot]
type = ElementIntegralVariablePostprocessor
variable = power_density
block = '${core_blocks}'
[]
[rpv_convective_out]
type = ConvectiveHeatTransferSideIntegral
T_solid = Tsolid
boundary = 'right' # outer RVP
T_fluid = ${rpv_outer_Tinf}
htc = ${rpv_outer_htc}
[]
[heat_balance] # should be equal to 0 upon convergence
type = ParsedPostprocessor
function = '(rpv_convective_out - ptot) / ptot'
pp_names = 'rpv_convective_out ptot'
[]
[flux_from_core] # converges to ptot as the mesh is refined
type = SideDiffusiveFluxIntegral
variable = Tsolid
boundary = core_outer
diffusivity = thermal_conductivity
[]
[flux_into_rpv] # converges to rpv_convective_out as the mesh is refined
type = SideDiffusiveFluxIntegral
variable = Tsolid
boundary = rpv_inner
diffusivity = thermal_conductivity
[]
[]
[Executioner]
type = Steady
automatic_scaling = true
compute_scaling_once = false
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart '
petsc_options_value = 'hypre boomeramg 100'
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
l_max_its = 100
[Quadrature]
# order = fifth
side_order = seventh
[]
line_search = none
[]
[Outputs]
exodus = false
csv = true
[]
(modules/porous_flow/test/tests/relperm/unity.i)
# Test perfectly mobile relative permeability curve by varying saturation over the mesh
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Variables]
[p0]
initial_condition = 1e6
[]
[s1]
[]
[]
[AuxVariables]
[s0aux]
family = MONOMIAL
order = CONSTANT
[]
[s1aux]
family = MONOMIAL
order = CONSTANT
[]
[kr0aux]
family = MONOMIAL
order = CONSTANT
[]
[kr1aux]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[s0]
type = PorousFlowPropertyAux
property = saturation
phase = 0
variable = s0aux
[]
[s1]
type = PorousFlowPropertyAux
property = saturation
phase = 1
variable = s1aux
[]
[kr0]
type = PorousFlowPropertyAux
property = relperm
phase = 0
variable = kr0aux
[]
[kr1]
type = PorousFlowPropertyAux
property = relperm
phase = 1
variable = kr1aux
[]
[]
[Functions]
[s1]
type = ParsedFunction
value = x
[]
[]
[ICs]
[s1]
type = FunctionIC
variable = s1
function = s1
[]
[]
[Kernels]
[p0]
type = Diffusion
variable = p0
[]
[s1]
type = Diffusion
variable = s1
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'p0 s1'
number_fluid_phases = 2
number_fluid_components = 2
[]
[pc]
type = PorousFlowCapillaryPressureConst
pc = 0
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow2PhasePS
phase0_porepressure = p0
phase1_saturation = s1
capillary_pressure = pc
[]
[kr0]
type = PorousFlowRelativePermeabilityConst
phase = 0
[]
[kr1]
type = PorousFlowRelativePermeabilityConst
phase = 1
[]
[]
[VectorPostprocessors]
[vpp]
type = LineValueSampler
warn_discontinuous_face_values = false
variable = 's0aux s1aux kr0aux kr1aux'
start_point = '0 0 0'
end_point = '1 0 0'
num_points = 20
sort_by = id
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
nl_abs_tol = 1e-8
[]
[BCs]
[sleft]
type = DirichletBC
variable = s1
value = 0
boundary = left
[]
[sright]
type = DirichletBC
variable = s1
value = 1
boundary = right
[]
[]
[Outputs]
csv = true
execute_on = timestep_end
[]
(modules/richards/test/tests/gravity_head_2/gh02.i)
# unsaturated = true
# gravity = true
# supg = false
# transient = false
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
xmin = 0
xmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = 'pwater pgas'
[../]
[./DensityWater]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0E2
[../]
[./DensityGas]
type = RichardsDensityConstBulk
dens0 = 0.5
bulk_mod = 0.5E2
[../]
[./SeffWater]
type = RichardsSeff2waterVG
m = 0.8
al = 1
[../]
[./SeffGas]
type = RichardsSeff2gasVG
m = 0.8
al = 1
[../]
[./RelPermWater]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./RelPermGas]
type = RichardsRelPermPower
simm = 0.0
n = 3
[../]
[./SatWater]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.15
[../]
[./SatGas]
type = RichardsSat
s_res = 0.05
sum_s_res = 0.15
[../]
[./SUPGwater]
type = RichardsSUPGnone
[../]
[./SUPGgas]
type = RichardsSUPGnone
[../]
[]
[Variables]
[./pwater]
order = FIRST
family = LAGRANGE
[../]
[./pgas]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
# get nonconvergence if initial condition is too crazy
[./water_ic]
type = FunctionIC
function = pwater_initial
variable = pwater
[../]
[./gas_ic]
type = FunctionIC
function = pgas_initial
variable = pgas
[../]
[]
[Kernels]
active = 'richardsfwater richardsfgas'
[./richardstwater]
type = RichardsMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFlux
variable = pwater
[../]
[./richardstgas]
type = RichardsMassChange
variable = pgas
[../]
[./richardsfgas]
type = RichardsFlux
variable = pgas
[../]
[]
[AuxVariables]
[./seffgas]
[../]
[./seffwater]
[../]
[]
[AuxKernels]
[./seffgas_kernel]
type = RichardsSeffAux
pressure_vars = 'pwater pgas'
seff_UO = SeffGas
variable = seffgas
[../]
[./seffwater_kernel]
type = RichardsSeffAux
pressure_vars = 'pwater pgas'
seff_UO = SeffWater
variable = seffwater
[../]
[]
[Postprocessors]
[./mwater_init]
type = RichardsMass
variable = pwater
execute_on = timestep_begin
outputs = none
[../]
[./mgas_init]
type = RichardsMass
variable = pgas
execute_on = timestep_begin
outputs = none
[../]
[./mwater_fin]
type = RichardsMass
variable = pwater
execute_on = timestep_end
outputs = none
[../]
[./mgas_fin]
type = RichardsMass
variable = pgas
execute_on = timestep_end
outputs = none
[../]
[./mass_error_water]
type = FunctionValuePostprocessor
function = fcn_mass_error_w
outputs = none # no reason why mass should be conserved
[../]
[./mass_error_gas]
type = FunctionValuePostprocessor
function = fcn_mass_error_g
outputs = none # no reason why mass should be conserved
[../]
[./pw_left]
type = PointValue
point = '0 0 0'
variable = pwater
outputs = none
[../]
[./pw_right]
type = PointValue
point = '1 0 0'
variable = pwater
outputs = none
[../]
[./error_water]
type = FunctionValuePostprocessor
function = fcn_error_water
[../]
[./pg_left]
type = PointValue
point = '0 0 0'
variable = pgas
outputs = none
[../]
[./pg_right]
type = PointValue
point = '1 0 0'
variable = pgas
outputs = none
[../]
[./error_gas]
type = FunctionValuePostprocessor
function = fcn_error_gas
[../]
[]
[Functions]
[./pwater_initial]
type = ParsedFunction
value = 1-x/2
[../]
[./pgas_initial]
type = ParsedFunction
value = 2-x/5
[../]
[./fcn_mass_error_w]
type = ParsedFunction
value = 'abs(0.5*(mi-mf)/(mi+mf))'
vars = 'mi mf'
vals = 'mwater_init mwater_fin'
[../]
[./fcn_mass_error_g]
type = ParsedFunction
value = 'abs(0.5*(mi-mf)/(mi+mf))'
vars = 'mi mf'
vals = 'mgas_init mgas_fin'
[../]
[./fcn_error_water]
type = ParsedFunction
value = 'abs((-b*log(-(gdens0*xval+(-b*exp(-p0/b)))/b)-p1)/p1)'
vars = 'b gdens0 p0 xval p1'
vals = '1E2 -1 pw_left 1 pw_right'
[../]
[./fcn_error_gas]
type = ParsedFunction
value = 'abs((-b*log(-(gdens0*xval+(-b*exp(-p0/b)))/b)-p1)/p1)'
vars = 'b gdens0 p0 xval p1'
vals = '0.5E2 -0.5 pg_left 1 pg_right'
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
density_UO = 'DensityWater DensityGas'
relperm_UO = 'RelPermWater RelPermGas'
SUPG_UO = 'SUPGwater SUPGgas'
sat_UO = 'SatWater SatGas'
seff_UO = 'SeffWater SeffGas'
viscosity = '1E-3 0.5E-3'
gravity = '-1 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -sub_pc_factor_shift_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'gmres asm lu NONZERO 1E-10 1E-10 10000'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = gh02
csv = true
[]
(test/tests/auxkernels/element_length/element_length.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 100
[]
[AuxVariables]
[./min]
order = CONSTANT
family = MONOMIAL
[../]
[./max]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./min]
type = ElementLengthAux
variable = min
method = min
execute_on = initial
[../]
[./max]
type = ElementLengthAux
variable = max
method = max
execute_on = initial
[../]
[../]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
execute_on = 'TIMESTEP_END'
exodus = true
[]
(test/tests/variables/curvilinear_element/curvilinear_element_test.i)
[Mesh]
file = curvi.e
# This mesh only has one element. It does seem to work if you
# use ReplicatedMesh on two processors, but it hangs with DistributedMesh
# on two processors.
parallel_type = replicated
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Postprocessors]
[./integral]
type = ElementIntegralVariablePostprocessor
variable = u
[../]
[]
[Outputs]
file_base = out
exodus = true
csv = true
[]
(modules/phase_field/test/tests/feature_volume_vpp_test/boundary_area_2D_single.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 50
ny = 50
xmin = 0
xmax = 50
ymin = 0
ymax = 50
elem_type = QUAD4
[]
[./left_side]
input = gen
type = SubdomainBoundingBoxGenerator
block_id = 1
bottom_left = '0 0 0'
top_right = '24.9 50 0'
[../]
[./right_side]
input = left_side
type = SubdomainBoundingBoxGenerator
block_id = 2
bottom_left = '25.1 0 0'
top_right = '50 50 0'
[../]
[./iface_u]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 1
paired_block = 2
new_boundary = 10
input = right_side
[../]
[]
[Variables]
[./c]
order = FIRST
family = LAGRANGE
[]
[]
[AuxVariables]
[./unique_regions]
family = MONOMIAL
order = CONSTANT
[../]
[]
[ICs]
[./c]
type = SpecifiedSmoothCircleIC
variable = c
invalue = 1.0
outvalue = 0.0
radii = '4 5 10'
x_positions = '25 25 25'
y_positions = '37.5 25 0'
z_positions = '0 0 0'
int_width = 2.0
[]
[]
[Postprocessors]
[./flood_count]
type = FeatureFloodCount
variable = c
# Must be turned on to build data structures necessary for FeatureVolumeVPP
compute_var_to_feature_map = true
threshold = 0.5
execute_on = INITIAL
[../]
[]
[VectorPostprocessors]
[./features]
type = FeatureVolumeVectorPostprocessor
flood_counter = flood_count
# Turn on centroid output
output_centroids = true
execute_on = INITIAL
boundary = 10
single_feature_per_element = true
[../]
[]
[Kernels]
[diff]
type = Diffusion
variable = c
[]
[]
[AuxKernels]
[./unique_regions]
type = FeatureFloodCountAux
variable = unique_regions
flood_counter = flood_count
field_display = UNIQUE_REGION
[../]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
execute_on = INITIAL
[]
(test/tests/executioners/full_jacobian_thread_active_bcs/full_jacobian_thread_active_bcs.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 5
[]
[Variables]
[./u]
[../]
[]
[ICs]
[./ic]
type = ConstantIC
variable = u
value = 1
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = RobinBC
variable = u
boundary = left
enable = false
[../]
[./right]
type = RobinBC
variable = u
boundary = right
[../]
[]
[Preconditioning]
[./pc]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
nl_max_its = 1
[]
(modules/contact/test/tests/nodal_area/nodal_area_2D.i)
[Mesh]
file = nodal_area_2D.e
[]
[Problem]
coord_type = RZ
[]
[Variables]
[./dummy]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./nodal_area]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./dummy]
type = Diffusion
variable = dummy
[../]
[]
[UserObjects]
[./nodal_area]
type = NodalArea
variable = nodal_area
boundary = 1
execute_on = 'initial timestep_end'
[../]
[]
[BCs]
[./dummy]
type = DirichletBC
variable = dummy
boundary = 1
value = 100
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -ksp_gmres_restart'
petsc_options_value = 'jacobi 101'
line_search = 'none'
nl_abs_tol = 1e-11
nl_rel_tol = 1e-10
l_max_its = 20
[]
[Outputs]
exodus = true
[]
(test/tests/mortar/continuity-3d-non-conforming/continuity_tet4.i)
[Mesh]
second_order = false
[left_block]
type = GeneratedMeshGenerator
dim = 3
nx = 1
ny = 2
nz = 2
xmin = 0
xmax = 0.3
ymin = 0
ymax = .5
zmin = 0
zmax = .5
elem_type = TET4
[]
[left_block_sidesets]
type = RenameBoundaryGenerator
input = left_block
old_boundary = '0 1 2 3 4 5'
new_boundary = 'lb_bottom lb_back lb_right lb_front lb_left lb_top'
[]
[left_block_id]
type = SubdomainIDGenerator
input = left_block_sidesets
subdomain_id = 1
[]
[right_block]
type = GeneratedMeshGenerator
dim = 3
nx = 1
ny = 2
nz = 2
xmin = 0.3
xmax = 0.6
ymin = 0
ymax = .5
zmin = 0
zmax = .5
elem_type = TET4
[]
[right_block_id]
type = SubdomainIDGenerator
input = right_block
subdomain_id = 2
[]
[right_block_change_boundary_id]
type = RenameBoundaryGenerator
input = right_block_id
old_boundary = '0 1 2 3 4 5'
new_boundary = '100 101 102 103 104 105'
[]
[combined]
type = MeshCollectionGenerator
inputs = 'left_block_id right_block_change_boundary_id'
[]
[block_rename]
type = RenameBlockGenerator
input = combined
old_block = '1 2'
new_block = 'left_block right_block'
[]
[right_right_sideset]
type = SideSetsAroundSubdomainGenerator
input = block_rename
new_boundary = rb_right
block = right_block
normal = '1 0 0'
[]
[right_left_sideset]
type = SideSetsAroundSubdomainGenerator
input = right_right_sideset
new_boundary = rb_left
block = right_block
normal = '-1 0 0'
[]
[right_top_sideset]
type = SideSetsAroundSubdomainGenerator
input = right_left_sideset
new_boundary = rb_top
block = right_block
normal = '0 0 1'
[]
[right_bottom_sideset]
type = SideSetsAroundSubdomainGenerator
input = right_top_sideset
new_boundary = rb_bottom
block = right_block
normal = '0 0 -1'
[]
[right_front_sideset]
type = SideSetsAroundSubdomainGenerator
input = right_bottom_sideset
new_boundary = rb_front
block = right_block
normal = '0 1 0'
[]
[right_back_sideset]
type = SideSetsAroundSubdomainGenerator
input = right_front_sideset
new_boundary = rb_back
block = right_block
normal = '0 -1 0'
[]
[secondary]
input = right_back_sideset
type = LowerDBlockFromSidesetGenerator
sidesets = 'lb_right'
new_block_id = '12'
new_block_name = 'secondary'
[]
[primary]
input = secondary
type = LowerDBlockFromSidesetGenerator
sidesets = 'rb_left'
new_block_id = '11'
new_block_name = 'primary'
[]
[]
[Problem]
kernel_coverage_check = false
[]
[Variables]
[T]
block = '1 2'
order = FIRST
[]
[lambda]
block = 'secondary'
family = MONOMIAL
order = CONSTANT
[]
[]
[BCs]
[neumann]
type = FunctionGradientNeumannBC
exact_solution = exact_soln_primal
variable = T
boundary = 'lb_back lb_front lb_left lb_top lb_bottom rb_right rb_top rb_bottom rb_front rb_back'
[]
[]
[Kernels]
[conduction]
type = Diffusion
variable = T
block = '1 2'
[]
[sink]
type = Reaction
variable = T
block = '1 2'
[]
[forcing_function]
type = BodyForce
variable = T
function = forcing_function
block = '1 2'
[]
[]
[Functions]
[forcing_function]
type = ParsedFunction
value = 'sin(x*pi)*sin(y*pi)*sin(z*pi) + 3*pi^2*sin(x*pi)*sin(y*pi)*sin(z*pi)'
[]
[exact_soln_primal]
type = ParsedFunction
value = 'sin(x*pi)*sin(y*pi)*sin(z*pi)'
[]
[exact_soln_lambda]
type = ParsedFunction
value = 'pi*sin(pi*y)*sin(pi*z)*cos(pi*x)'
[]
[]
[Debug]
show_var_residual_norms = 1
[]
[Constraints]
[mortar]
type = EqualValueConstraint
primary_boundary = 'rb_left'
secondary_boundary = 'lb_right'
primary_subdomain = '11'
secondary_subdomain = '12'
variable = lambda
secondary_variable = T
delta = .1
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
solve_type = NEWTON
type = Steady
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_shift_type '
'-pc_factor_shift_amount'
petsc_options_value = 'lu basic NONZERO 1e-15'
[]
[Outputs]
exodus = true
[]
[Postprocessors]
[L2lambda]
type = ElementL2Error
variable = lambda
function = exact_soln_lambda
execute_on = 'timestep_end'
block = 'secondary'
[]
[L2u]
type = ElementL2Error
variable = T
function = exact_soln_primal
execute_on = 'timestep_end'
block = 'left_block right_block'
[]
[h]
type = AverageElementSize
block = 'left_block right_block'
[]
[]
(modules/richards/test/tests/gravity_head_1/gh_fu_01.i)
# unsaturated = false
# gravity = false
# supg = false
# transient = false
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
xmin = -1
xmax = 1
[]
[BCs]
[./left]
type = DirichletBC
boundary = left
value = 1
variable = pressure
[../]
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGnone
sat_UO = Saturation
seff_UO = SeffVG
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0E3
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGnone]
type = RichardsSUPGnone
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = RandomIC
block = 0
min = 0
max = 1
[../]
[../]
[]
[AuxVariables]
[./RFUF_Residual]
[../]
[./RFUF_Jacobian]
[../]
[]
[Kernels]
active = 'richardsf'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFullyUpwindFlux
richardsVarNames_UO = PPNames
variable = pressure
save_in = RFUF_Residual
diag_save_in = RFUF_Jacobian
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
viscosity = 1E-3
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = gh_fu_01
[./Exodus]
hide = 'RFUF_Residual RFUF_Jacobian'
type = Exodus
[../]
[]
(test/tests/geomsearch/quadrature_nearest_node_locator/qnnl_ad.i)
[Mesh]
file = 2dcontact_collide.e
displacements = 'disp_x disp_y'
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./distance]
order = CONSTANT
family = MONOMIAL
[../]
[disp_x][]
[disp_y][]
[]
[Kernels]
[./diff]
type = ADDiffusion
variable = u
use_displaced_mesh = true
[../]
[]
[AuxKernels]
[./distance]
type = NearestNodeDistanceAux
variable = distance
boundary = 2
paired_boundary = 3
[../]
[]
[BCs]
[./block1_left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./block1_right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[./block2_left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./block2_right]
type = DirichletBC
variable = u
boundary = 4
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
file_base = qnnl_ad
[]
(test/tests/interfacekernels/ad_coupled_value/coupled.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 20
xmax = 2
[]
[./subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '1.0 0 0'
block_id = 1
top_right = '2.0 1.0 0'
[../]
[./interface]
input = subdomain1
type = SideSetsBetweenSubdomainsGenerator
primary_block = '0'
paired_block = '1'
new_boundary = 'primary0_interface'
[../]
[]
[Variables]
[./u]
block = '0'
[../]
[./v]
block = '1'
[../]
[w][]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
block = 0
[../]
[./diff_v]
type = Diffusion
variable = v
block = 1
[../]
[diff_w]
type = Diffusion
variable = w
[]
[]
[InterfaceKernels]
[./interface]
type = ADCoupledInterfacialSource
variable = u
neighbor_var = v
var_source = w
boundary = primary0_interface
D = 1
D_neighbor = 1
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[../]
[./right]
type = DirichletBC
variable = v
boundary = 'right'
value = 10
[../]
[./middle]
type = MatchedValueBC
variable = v
boundary = 'primary0_interface'
v = u
[../]
[w_left]
type = DirichletBC
variable = w
boundary = 'left'
value = 0
[]
[w_right]
type = DirichletBC
variable = w
boundary = 'right'
value = 4
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(test/tests/fvkernels/mms/grad-reconstruction/rz.i)
a=1.1
diff=1.1
[Mesh]
[./gen_mesh]
type = GeneratedMeshGenerator
dim = 2
xmin = 2
xmax = 3
ymin = 0
ymax = 1
nx = 2
ny = 2
[../]
[]
[Problem]
coord_type = 'RZ'
[]
[Variables]
[./v]
family = MONOMIAL
order = CONSTANT
fv = true
initial_condition = 1
[../]
[]
[FVKernels]
[./advection]
type = FVElementalAdvection
variable = v
velocity = '${a} ${a} 0'
[../]
[reaction]
type = FVReaction
variable = v
[]
[diff_v]
type = FVDiffusion
variable = v
coeff = ${diff}
[]
[body_v]
type = FVBodyForce
variable = v
function = 'forcing'
[]
[]
[FVBCs]
[diri]
type = FVFunctionDirichletBC
boundary = 'left right top bottom'
function = 'exact'
variable = v
[]
[]
[Functions]
[exact]
type = ParsedFunction
value = 'sin(x)*cos(y)'
[]
[forcing]
type = ParsedFunction
value = '-a*sin(x)*sin(y) + diff*sin(x)*cos(y) + sin(x)*cos(y) + (x*a*cos(x)*cos(y) + a*sin(x)*cos(y))/x - (-x*diff*sin(x)*cos(y) + diff*cos(x)*cos(y))/x'
vars = 'a diff'
vals = '${a} ${diff}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_shift_type -sub_pc_type'
petsc_options_value = 'asm NONZERO lu'
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[./error]
type = ElementL2Error
variable = v
function = exact
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(test/tests/multiapps/override_cliargs/sub.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 10
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
value = 0
boundary = left
[]
[right]
type = DirichletBC
variable = u
value = 1
boundary = left
[]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[integral]
type = ElementIntegralVariablePostprocessor
variable = u
[]
[]
[Outputs]
exodus = true
[]
(modules/phase_field/test/tests/initial_conditions/MultiBoundingBoxIC1D.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
[]
[Variables]
[./c1]
order = FIRST
family = LAGRANGE
[../]
[./c2]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./c1]
type = MultiBoundingBoxIC
corners = '0.1 0 0 0.8 0 0 0.3 0 0'
opposite_corners = '0.2 0 0 0.6 0 0 0.4 0 0'
inside = '1.0'
outside = 0.1
variable = c1
[../]
[./c2]
type = MultiBoundingBoxIC
corners = '0.1 0 0 0.8 0 0 0.3 0 0'
opposite_corners = '0.2 0 0 0.4 0 0 0.5 0 0'
inside = '1.0 2.0 3.0'
outside = 0.1
variable = c2
[../]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
kernel_coverage_check = false
[]
[Outputs]
exodus = true
[]
(test/tests/fvkernels/fv_coupled_var/coupled.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 2
[]
[Variables]
[u][]
[v]
family = MONOMIAL
order = CONSTANT
fv = true
[]
[w]
family = MONOMIAL
order = CONSTANT
fv = true
[]
[s][]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[rxn]
type = Reaction
variable = u
rate = 2.0
[]
[diffs]
type = Diffusion
variable = s
[]
[prod]
type = CoupledForce
variable = s
v = u
[]
[]
[FVKernels]
[diff]
type = FVDiffusion
variable = v
coeff = coeff
[]
[rxn]
type = FVReaction
variable = v
rate = 2.0
[]
[diffw]
type = FVDiffusion
variable = w
coeff = coeff
[]
[prod]
type = FVCoupledForce
variable = w
v = 'v'
[]
[]
[FVBCs]
[left]
type = FVDirichletBC
variable = v
boundary = left
value = 0
[]
[right]
type = FVDirichletBC
variable = v
boundary = right
value = 1
[]
[leftw]
type = FVDirichletBC
variable = w
boundary = left
value = 0
[]
[rightw]
type = FVDirichletBC
variable = w
boundary = right
value = 1
[]
[]
[Materials]
[diff]
type = ADGenericFunctorMaterial
prop_names = 'coeff'
prop_values = '1'
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[lefts]
type = DirichletBC
variable = s
boundary = left
value = 0
[]
[rights]
type = DirichletBC
variable = s
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(test/tests/variables/fe_hermite_convergence/hermite_converge_periodic.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 4
ny = 4
elem_type = QUAD4
# This test will not work in parallel with DistributedMesh enabled
# due to a bug in PeriodicBCs.
parallel_type = replicated
[]
[Functions]
[./bc_fn]
type = ParsedGradFunction
value = -sin(pi*x)*sin(pi*y)
grad_x = -pi*cos(pi*x)*sin(pi*y)
grad_y = -pi*sin(pi*x)*cos(pi*y)
[../]
[./bc_fnt]
type = ParsedFunction
value = -pi*sin(pi*x)*cos(pi*y)
[../]
[./bc_fnb]
type = ParsedFunction
value = pi*sin(pi*x)*cos(pi*y)
[../]
[./forcing_fn]
type = ParsedFunction
value = -2*pi*pi*sin(pi*x)*sin(pi*y)-sin(pi*x)*sin(pi*y)
[../]
[]
[Variables]
[./u]
order = THIRD
family = HERMITE
[../]
[]
[Kernels]
active = 'diff forcing reaction'
[./diff]
type = Diffusion
variable = u
[../]
[./reaction]
type = Reaction
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
[./Periodic]
[./all]
variable = u
auto_direction= 'x y'
[../]
[../]
[./bc_top]
type=FunctionNeumannBC
variable = u
boundary = 'top'
function = bc_fnt
[../]
[./bc_bottom]
type=FunctionNeumannBC
variable = u
boundary = 'bottom'
function = bc_fnb
[../]
[]
[Postprocessors]
[./dofs]
type = NumDOFs
[../]
[./h]
type = AverageElementSize
[../]
[./L2error]
type = ElementL2Error
variable = u
function = bc_fn
[../]
[./H1error]
type = ElementH1Error
variable = u
function = bc_fn
[../]
[./H1Semierror]
type = ElementH1SemiError
variable = u
function = bc_fn
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
# We use higher-order quadrature to ensure that the forcing function
# is integrated accurately.
[./Quadrature]
order=ELEVENTH
[../]
[]
[Adaptivity]
steps = 2
marker = uniform
[./Markers]
[./uniform]
type = UniformMarker
mark = refine
[../]
[../]
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
csv = true
print_mesh_changed_info = true
[]
(test/tests/misc/check_error/coupling_nonexistent_scalar.i)
[Mesh]
type = GeneratedMesh
dim = 2
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./slm]
type = ScalarLagrangeMultiplier
variable = u
# 'b' does not exist -> error
lambda = b
[../]
[]
[Executioner]
type = Steady
[]
(tutorials/tutorial01_app_development/step09_mat_props/test/tests/materials/packed_column/packed_column_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
xmax = 1
ymax = 1
[]
[Problem]
solve = false
[]
[Variables]
[u]
[]
[]
[Materials]
[filter]
type = PackedColumn
diameter = 2
viscosity = 1e-03
output_properties = 'permeability viscosity'
outputs = exodus
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/multiapps/picard_postprocessor/steady_main.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
parallel_type = replicated
uniform_refine = 1
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[source]
type = BodyForce
variable = u
value = 1
[]
[]
[BCs]
[left]
type = PostprocessorDirichletBC
variable = u
boundary = left
postprocessor = 'from_sub'
[]
[]
[Postprocessors]
[from_sub]
type = Receiver
default = 0
[]
[to_sub]
type = SideAverageValue
variable = u
boundary = right
[]
[average]
type = ElementAverageValue
variable = u
[]
[]
[Executioner]
type = Steady
# Solve parameters
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
nl_abs_tol = 1e-14
# App coupling parameters
fixed_point_max_its = 100
fixed_point_rel_tol = 0.5 # pseudo transient is slow to converge
relaxation_factor = 0.8
transformed_postprocessors = 'from_sub'
[]
[Outputs]
csv = true
exodus = false
[]
[MultiApps]
[sub]
type = FullSolveMultiApp
app_type = MooseTestApp
positions = '0 0 0'
input_files = steady_sub.i
clone_master_mesh = true
execute_on = 'timestep_begin'
relaxation_factor = 0.8
transformed_postprocessors = 'from_main'
[]
[]
[Transfers]
[left_from_sub]
type = MultiAppPostprocessorTransfer
from_multi_app = sub
from_postprocessor = 'to_main'
to_postprocessor = 'from_sub'
reduction_type = 'average'
[]
[right_to_sub]
type = MultiAppPostprocessorTransfer
to_multi_app = sub
from_postprocessor = 'to_sub'
to_postprocessor = 'from_main'
[]
[]
(test/tests/mesh/mixed_dim/1d_3d.i)
[Mesh]
file = 1d_3d.e
# 1d_3d.e contains HEX8 and BEAM2 elements - no additional input file
# changes are necessary to handle mixed-dim meshes.
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 4
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[./bottom]
type = DirichletBC
variable = u
boundary = 100
value = 0
[../]
[./top]
type = DirichletBC
variable = u
boundary = 101
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = 1d_3d_out
exodus = true
[]
(modules/stochastic_tools/test/tests/surrogates/pod_rb/boundary/sub.i)
[Problem]
type = FEProblem
extra_tag_vectors = 'diff react bodyf dir_src dir_imp'
[]
[Mesh]
type = GeneratedMesh
dim = 1
nx = 15
xmax = 10
[]
[Variables]
[u]
[]
[]
[Kernels]
[diffusion]
type = MatDiffusion
variable = u
diffusivity = k
extra_vector_tags = 'diff'
[]
[reaction]
type = MaterialReaction
variable = u
coefficient = alpha
extra_vector_tags = 'react'
[]
[source]
type = BodyForce
variable = u
value = 1.0
extra_vector_tags = 'bodyf'
[]
[]
[Materials]
[k]
type = GenericConstantMaterial
prop_names = k
prop_values = 1.0
[]
[alpha]
type = GenericConstantMaterial
prop_names = alpha
prop_values = 1.0
[]
[]
[BCs]
[dummy_1]
type = DirichletBC
variable = u
boundary = left
value = 0
extra_vector_tags = 'dir_imp'
[]
[dummy_2]
type = DirichletBCModifier
variable = u
boundary = left
value = 1
extra_vector_tags = 'dir_src'
[]
[left]
type = DirichletBC
variable = u
boundary = left
value = 1
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 0
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Controls]
[stochastic]
type = SamplerReceiver
[]
[]
[Outputs]
[]
(test/tests/outputs/iterative/iterative_steady_sequence.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
preset = false
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
preset = false
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
[./out]
type = Exodus
execute_on = 'initial timestep_end failed nonlinear linear'
sequence = true
[../]
[]
(test/tests/constraints/equal_value_boundary_constraint/equal_value_boundary_constraint_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 6
ny = 6
elem_type = QUAD4
allow_renumbering = false
[]
[Variables]
[./diffused]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = diffused
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = diffused
preset = false
boundary = 'left'
value = 1.0
[../]
[./right]
type = DirichletBC
variable = diffused
preset = false
boundary = 'right'
value = 0.0
[../]
[]
# Constraint System
[Constraints]
[./y_top]
type = EqualValueBoundaryConstraint
variable = diffused
primary = '45' # node on boundary
secondary = 'top' # boundary
penalty = 10e6
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = ''
petsc_options_value = ''
line_search = 'none'
[]
[Postprocessors]
active = ' '
[./residual]
type = Residual
[../]
[./nl_its]
type = NumNonlinearIterations
[../]
[./lin_its]
type = NumLinearIterations
[../]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = out
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/lid-driven/lid-driven-with-energy-action.i)
mu = 1
rho = 1
k = .01
cp = 1
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 32
ny = 32
[]
[]
[Modules]
[NavierStokesFV]
compressibility = 'incompressible'
add_energy_equation = true
density = 'rho'
dynamic_viscosity = 'mu'
thermal_conductivity = 'k'
specific_heat = 'cp'
initial_pressure = 0.0
initial_temperature = 0.0
inlet_boundaries = 'top'
momentum_inlet_types = 'fixed-velocity'
momentum_inlet_function = 'lid_function 0'
energy_inlet_types = 'fixed-temperature'
energy_inlet_function = '0'
wall_boundaries = 'left right bottom'
momentum_wall_types = 'noslip noslip noslip'
energy_wall_types = 'heatflux heatflux fixed-temperature'
energy_wall_function = '0 0 1'
pin_pressure = true
pinned_pressure_type = average
pinned_pressure_value = 0
[]
[]
[AuxVariables]
[U]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[]
[AuxKernels]
[mag]
type = VectorMagnitudeAux
variable = U
x = vel_x
y = vel_y
[]
[]
[Materials]
[functor_constants]
type = ADGenericFunctorMaterial
prop_names = 'cp k rho mu'
prop_values = '${cp} ${k} ${rho} ${mu}'
[]
[]
[Functions]
[lid_function]
type = ParsedFunction
value = '4*x*(1-x)'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 300 lu NONZERO'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/stress_recovery/stress_concentration/stress_concentration.i)
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
type = FileMesh
file = geo.msh
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[]
[AuxVariables]
[stress_xx]
order = CONSTANT
family = MONOMIAL
[]
[stress_yy]
order = CONSTANT
family = MONOMIAL
[]
[stress_xx_recovered]
order = FIRST
family = LAGRANGE
[]
[stress_yy_recovered]
order = FIRST
family = LAGRANGE
[]
[]
[AuxKernels]
[stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = 'timestep_end'
[]
[stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = 'timestep_end'
[]
[stress_xx_recovered]
type = NodalPatchRecoveryAux
variable = stress_xx_recovered
nodal_patch_recovery_uo = stress_xx_patch
execute_on = 'TIMESTEP_END'
[]
[stress_yy_recovered]
type = NodalPatchRecoveryAux
variable = stress_yy_recovered
nodal_patch_recovery_uo = stress_yy_patch
execute_on = 'TIMESTEP_END'
[]
[]
[Kernels]
[solid_x]
type = StressDivergenceTensors
variable = disp_x
component = 0
[]
[solid_y]
type = StressDivergenceTensors
variable = disp_y
component = 1
[]
[]
[Materials]
[strain]
type = ComputeSmallStrain
[]
[Cijkl]
type = ComputeIsotropicElasticityTensor
poissons_ratio = 0.3
youngs_modulus = 2.1e+5
[]
[stress]
type = ComputeLinearElasticStress
[]
[]
[BCs]
[top_xdisp]
type = FunctionDirichletBC
variable = disp_y
boundary = 'top'
function = 0
[]
[top_ydisp]
type = FunctionDirichletBC
variable = disp_y
boundary = 'top'
function = 0.01
[]
[bottom_xdisp]
type = FunctionDirichletBC
variable = disp_x
boundary = 'bottom'
function = 0
[]
[bottom_ydisp]
type = FunctionDirichletBC
variable = disp_y
boundary = 'bottom'
function = 0
[]
[]
[UserObjects]
[stress_xx_patch]
type = NodalPatchRecoveryMaterialProperty
patch_polynomial_order = FIRST
property = 'stress'
component = '0 0'
execute_on = 'TIMESTEP_END'
[]
[stress_yy_patch]
type = NodalPatchRecoveryMaterialProperty
patch_polynomial_order = FIRST
property = 'stress'
component = '1 1'
execute_on = 'TIMESTEP_END'
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
ksp_norm = default
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
petsc_options_iname = '-ksp_type -pc_type'
petsc_options_value = 'preonly lu'
nl_rel_tol = 1e-14
l_max_its = 100
nl_max_its = 30
[]
[Outputs]
interval = 1
exodus = true
print_linear_residuals = false
[]
(modules/functional_expansion_tools/test/tests/errors/missing_series_duo_axis.i)
[Mesh]
type = GeneratedMesh
dim = 3
[]
[Functions]
[./series]
type = FunctionSeries
series_type = CylindricalDuo
orders = '0 1'
physical_bounds = '-1.0 1.0 0.0 0.0 1'
disc = Zernike
[../]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
(test/tests/ics/vector_function_ic/vector_function_ic.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 2
ny = 2
nz = 2
[]
[Problem]
solve = false
kernel_coverage_check = false
[]
[Variables/A]
family = LAGRANGE_VEC
[]
[ICs/A]
type = VectorFunctionIC
variable = A
function = func
[]
[Functions/func]
type = ParsedVectorFunction
value_x = '2*x'
value_y = '3*y'
value_z = 'z*z'
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/auxkernels/solution_aux/aux_nonlinear_solution_adapt_xda.i)
[Mesh]
# This test uses SolutionUserObject which doesn't work with DistributedMesh.
type = FileMesh
file = aux_nonlinear_solution_adapt_out_0004_mesh.xda
parallel_type = replicated
[]
[Adaptivity]
marker = error_frac
steps = 2
[./Indicators]
[./jump_indicator]
type = GradientJumpIndicator
variable = u
[../]
[../]
[./Markers]
[./error_frac]
type = ErrorFractionMarker
indicator = jump_indicator
refine = 0.7
[../]
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./u_aux]
[../]
[]
[Functions]
[./u_xda_func]
type = SolutionFunction
solution = xda_u
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./aux_xda_kernel]
type = SolutionAux
variable = u_aux
solution = xda_u_aux
execute_on = initial
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 2
[../]
[]
[UserObjects]
[./xda_u_aux]
type = SolutionUserObject
system = aux0
mesh = aux_nonlinear_solution_adapt_out_0004_mesh.xda
es = aux_nonlinear_solution_adapt_out_0004.xda
system_variables = u_aux
execute_on = initial
[../]
[./xda_u]
type = SolutionUserObject
system = nl0
mesh = aux_nonlinear_solution_adapt_out_0004_mesh.xda
es = aux_nonlinear_solution_adapt_out_0004.xda
system_variables = u
execute_on = initial
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
nl_rel_tol = 1e-10
[]
[Outputs]
exodus = true
[]
[ICs]
[./u_func_ic]
function = u_xda_func
variable = u
type = FunctionIC
[../]
[]
(test/tests/multiapps/secant_postprocessor/steady_main.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
parallel_type = replicated
uniform_refine = 1
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[source]
type = BodyForce
variable = u
value = 1
[]
[]
[BCs]
[left]
type = PostprocessorDirichletBC
variable = u
boundary = left
postprocessor = 'from_sub'
[]
[]
[Postprocessors]
[from_sub]
type = Receiver
default = 0
[]
[to_sub]
type = SideAverageValue
variable = u
boundary = right
[]
[average]
type = ElementAverageValue
variable = u
[]
[]
[Executioner]
type = Steady
# Solve parameters
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
nl_abs_tol = 1e-14
# App coupling parameters
fixed_point_algorithm = 'secant'
fixed_point_max_its = 100
transformed_postprocessors = 'from_sub'
[]
[Outputs]
csv = true
exodus = false
[]
[MultiApps]
[sub]
type = FullSolveMultiApp
app_type = MooseTestApp
positions = '0 0 0'
input_files = steady_sub.i
clone_master_mesh = true
execute_on = 'timestep_begin'
transformed_postprocessors = 'from_main'
[]
[]
[Transfers]
[left_from_sub]
type = MultiAppPostprocessorTransfer
from_multi_app = sub
from_postprocessor = 'to_main'
to_postprocessor = 'from_sub'
reduction_type = 'average'
[]
[right_to_sub]
type = MultiAppPostprocessorTransfer
to_multi_app = sub
from_postprocessor = 'to_sub'
to_postprocessor = 'from_main'
[]
[]
(test/tests/bcs/nodal_normals/square_quads.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[NodalNormals]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(test/tests/misc/check_error/function_file_test10.i)
# Test for usage of missing function
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = ic_function
[../]
[../]
[]
[Functions]
[./ic_function]
type = PiecewiseLinear
xy_data = '1 2'
scale_factor = 1.0
axis = 3
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/pins/mms/1d-rc-no-diffusion.i)
mu=1e-15
rho=1.1
advected_interp_method='upwind'
velocity_interp_method='rc'
[Mesh]
[mesh]
type = GeneratedMeshGenerator
dim = 1
nx = 2
xmax = 0.5
[]
[]
[GlobalParams]
two_term_boundary_expansion = true
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = PINSFVRhieChowInterpolator
u = u
pressure = pressure
porosity = porosity
[]
[]
[Variables]
[u]
type = PINSFVSuperficialVelocityVariable
initial_condition = .1
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[AuxVariables]
[porosity]
family = MONOMIAL
order = CONSTANT
fv = true
initial_condition = 0.8
[]
[]
[Problem]
error_on_jacobian_nonzero_reallocation = true
[]
[Functions]
[exact_u]
type = ParsedFunction
value = 'cos((1/2)*x*pi)'
[]
[forcing_u]
type = ADParsedFunction
value = '-1.25*pi*rho*sin((1/2)*x*pi)*cos((1/2)*x*pi) + 0.8*cos(x)'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_p]
type = ParsedFunction
value = 'sin(x)'
[]
[forcing_p]
type = ParsedFunction
value = '-1/2*pi*rho*sin((1/2)*x*pi)'
vars = 'rho'
vals = '${rho}'
[]
[]
[FVKernels]
[mass]
type = PINSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[u_advection]
type = PINSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
porosity = porosity
momentum_component = 'x'
[]
[u_pressure]
type = PINSFVMomentumPressureFlux
variable = u
pressure = pressure
porosity = porosity
momentum_component = 'x'
[]
[u_forcing]
type = INSFVBodyForce
variable = u
functor = forcing_u
momentum_component = 'x'
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = 'exact_u'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 'exact_p'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'bt'
[]
[Postprocessors]
[inlet_p]
type = SideAverageValue
variable = 'pressure'
boundary = 'left'
[]
[outlet-u]
type = SideIntegralVariablePostprocessor
variable = u
boundary = 'right'
[]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2p]
variable = pressure
function = exact_p
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
[Outputs]
exodus = true
csv = true
[]
(modules/geochemistry/test/tests/time_dependent_reactions/except1.i)
#Exception: incorrect size of source_species
[TimeDependentReactionSolver]
model_definition = definition
geochemistry_reactor_name = reactor
charge_balance_species = "Cl-"
constraint_species = "H2O H+ Na+ K+ Ca++ Mg++ Al+++ SiO2(aq) Cl- SO4-- HCO3-"
constraint_value = " 1.0 1E-5 1E-5 1E-5 1E-5 1E-5 1E-5 1E-5 1E-5 1E-5 1E-5"
constraint_meaning = "kg_solvent_water activity bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition"
constraint_unit = "kg dimensionless moles moles moles moles moles moles moles moles moles"
source_species_names = "Al+++"
source_species_rates = "1 0"
[]
[Executioner]
type = Steady
[]
[UserObjects]
[definition]
type = GeochemicalModelDefinition
database_file = "../../../database/moose_geochemdb.json"
basis_species = "H2O H+ Na+ K+ Ca++ Mg++ Al+++ SiO2(aq) Cl- SO4-- HCO3-"
[]
[]
(test/tests/misc/app_name/simple-diffusion.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/controls/syntax_based_naming_access/system_asterisk_param.i)
[Mesh]
type = GeneratedMesh
dim = 2
elem_type = QUAD4
# use odd numbers so points do not fall on element boundaries
nx = 31
ny = 31
[]
[Variables]
[./diffused]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = diffused
[../]
[]
[DiracKernels]
[./test_object]
type = MaterialPointSource
point = '0.5 0.5 0'
variable = diffused
[../]
[]
[BCs]
[./bottom_diffused]
type = DirichletBC
variable = diffused
boundary = 'bottom'
value = 2
[../]
[./top_diffused]
type = DirichletBC
variable = diffused
boundary = 'top'
value = 0
[../]
[]
[Materials]
[./mat]
type = GenericConstantMaterial
prop_names = 'matp'
prop_values = '1'
block = 0
[../]
[]
[Postprocessors]
[./test_object]
type = FunctionValuePostprocessor
function = '2*(x+y)'
point = '0.5 0.5 0'
[../]
[./other_point_test_object]
type = FunctionValuePostprocessor
function = '3*(x+y)'
point = '0.5 0.5 0'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
[Controls]
[./point_control]
type = TestControl
test_type = 'point'
parameter = 'Postprocessors/*/point'
execute_on = 'initial'
[../]
[]
(test/tests/relationship_managers/geometric_neighbors/geometric_edge_neighbors.i)
# This test will show 2 layers of geometric ghosting and 0 layers of evaluable
# ghosting. The 2 layers of geometric ghosting corresponds to the 2 layers we
# have explicitly requested. There is no evaulable ghosting because we have not
# requested any algebraic or coupling functors.
[Mesh]
type = GeneratedMesh
dim = 2
nx = 8
ny = 8
# We are testing geometric ghosted functors
# so we have to use distributed mesh
parallel_type = distributed
[]
[GlobalParams]
order = CONSTANT
family = MONOMIAL
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[ghosting0]
[]
[ghosting1]
[]
[ghosting2]
[]
[evaluable0]
[]
[evaluable1]
[]
[evaluable2]
[]
[proc]
[]
[]
[AuxKernels]
[ghosting0]
type = ElementUOAux
variable = ghosting0
element_user_object = ghosting_uo0
field_name = "ghosted"
execute_on = initial
[]
[ghosting1]
type = ElementUOAux
variable = ghosting1
element_user_object = ghosting_uo1
field_name = "ghosted"
execute_on = initial
[]
[ghosting2]
type = ElementUOAux
variable = ghosting2
element_user_object = ghosting_uo2
field_name = "ghosted"
execute_on = initial
[]
[evaluable0]
type = ElementUOAux
variable = evaluable0
element_user_object = ghosting_uo0
field_name = "evaluable"
execute_on = initial
[]
[evaluable1]
type = ElementUOAux
variable = evaluable1
element_user_object = ghosting_uo1
field_name = "evaluable"
execute_on = initial
[]
[evaluable2]
type = ElementUOAux
variable = evaluable2
element_user_object = ghosting_uo2
field_name = "evaluable"
execute_on = initial
[]
[proc]
type = ProcessorIDAux
variable = proc
execute_on = initial
[]
[]
[UserObjects]
[ghosting_uo0]
type = ElemSideNeighborLayersGeomTester
execute_on = initial
element_side_neighbor_layers = 2
rank = 0
[]
[ghosting_uo1]
type = ElemSideNeighborLayersGeomTester
execute_on = initial
element_side_neighbor_layers = 2
rank = 1
[]
[ghosting_uo2]
type = ElemSideNeighborLayersGeomTester
execute_on = initial
element_side_neighbor_layers = 2
rank = 2
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
[Problem]
solve = false
kernel_coverage_check = false
[]
(test/tests/dgkernels/dg_block_restrict/1d_dg_block_restrict.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 100
xmax = 2
[]
[./subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '1.0 0 0'
block_id = 1
top_right = '2.0 0 0'
[../]
[./interface]
input = subdomain1
type = SideSetsBetweenSubdomainsGenerator
primary_block = '0'
paired_block = '1'
new_boundary = 'primary0_interface'
[../]
[./interface_again]
type = SideSetsBetweenSubdomainsGenerator
input = interface
primary_block = '1'
paired_block = '0'
new_boundary = 'primary1_interface'
[../]
[]
[Variables]
[./u]
order = FIRST
family = MONOMIAL
block = 0
[../]
[./v]
order = FIRST
family = MONOMIAL
block = 1
[../]
[]
[Kernels]
[./test_u]
type = Diffusion
variable = u
block = 0
[../]
[./adv_u]
type = ConservativeAdvection
variable = u
velocity = '1 0 0'
block = 0
[../]
[./test_v]
type = Diffusion
variable = v
block = 1
[../]
[./adv_v]
type = ConservativeAdvection
variable = v
velocity = '1 0 0'
block = 1
[../]
[]
[DGKernels]
[./dg_advection_u]
type = DGConvection
variable = u
velocity = '1 0 0'
block = 0
[../]
[./dg_diffusion_u]
type = DGDiffusion
variable = u
sigma = 0
epsilon = -1
block = 0
[../]
[./dg_advection_v]
type = DGConvection
variable = v
velocity = '1 0 0'
block = 1
[../]
[./dg_diffusion_v]
type = DGDiffusion
variable = v
sigma = 0
epsilon = -1
block = 1
[../]
[]
[BCs]
[./left]
type = InflowBC
variable = u
boundary = 'left'
inlet_conc = 2
velocity = '1 0 0'
[../]
[./primary0_inteface]
type = RobinBC
variable = u
boundary = 'primary0_interface'
[../]
[./primary1_interface]
type = InflowBC
variable = v
boundary = 'primary1_interface'
inlet_conc = 4
velocity = '1 0 0'
[../]
[./right]
type = RobinBC
variable = v
boundary = 'right'
[../]
[]
[ICs]
[./u_ic]
type = ConstantIC
variable = u
value = 0
[../]
[./v_ic]
type = ConstantIC
variable = v
value = 0
[../]
[]
[Preconditioning]
[./fdp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
nl_abs_tol = 1e-12
solve_type = NEWTON
[]
[Outputs]
exodus = true
print_linear_residuals = false
[]
[Debug]
show_var_residual_norms = true
[]
(test/tests/outputs/nemesis/nemesis.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
nemesis = true
[]
(modules/ray_tracing/test/tests/traceray/nonplanar/nonplanar.i)
[Mesh]
[file]
type = FileMeshGenerator
file = nonplanar.e
[]
[]
[RayBCs/kill]
type = KillRayBC
boundary = 'top right bottom left front back'
[]
[RayKernels/null]
type = NullRayKernel
[]
[UserObjects/lots]
type = LotsOfRaysRayStudy
vertex_to_vertex = true
centroid_to_vertex = true
centroid_to_centroid = true
side_aq = true
centroid_aq = true
compute_expected_distance = true
warn_non_planar = false
execute_on = initial
[]
[Postprocessors]
[total_distance]
type = RayTracingStudyResult
study = lots
result = total_distance
[]
[expected_distance]
type = LotsOfRaysExpectedDistance
lots_of_rays_study = lots
[]
[distance_difference]
type = DifferencePostprocessor
value1 = total_distance
value2 = expected_distance
[]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Outputs]
exodus = false
csv = true
[]
(test/tests/executioners/executioner/steady-adapt.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 3
ny = 3
elem_type = QUAD4
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
[./forcing_fn]
type = ParsedFunction
value = -4
[../]
[./exact_fn]
type = ParsedFunction
value = ((x*x)+(y*y))
[../]
[]
[Kernels]
active = 'diff ffn'
[./diff]
type = Diffusion
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
active = 'all'
[./all]
type = FunctionDirichletBC
variable = u
boundary = '0 1 2 3'
function = exact_fn
[../]
[]
[Postprocessors]
[./l2_err]
type = ElementL2Error
variable = u
function = exact_fn
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[./Adaptivity]
steps = 3
coarsen_fraction = 0.1
refine_fraction = 0.2
max_h_level = 5
[../]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = out_steady_adapt
exodus = true
print_mesh_changed_info = true
[]
(modules/tensor_mechanics/examples/umat_build/test.i)
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
[]
[]
[Modules/TensorMechanics/Master]
[all]
add_variables = true
strain = FINITE
[]
[]
[Materials]
[umat]
type = AbaqusUMATStress
constant_properties = '1000 0.3'
num_state_vars = 0
plugin = umat
use_one_based_indexing = true
[]
[]
[Executioner]
type = Steady
[]
(test/tests/userobjects/layered_integral/layered_integral_test.i)
###########################################################
# This is a test of the UserObject System. The
# LayeredIntegral UserObject executes independently during
# the solve to compute a user-defined value. In this case
# an integral value in discrete layers along a vector
# in the domain. (Type: ElementalUserObject)
#
# @Requirement F6.40
###########################################################
[Mesh]
type = GeneratedMesh
dim = 2
nx = 6
ny = 6
nz = 6
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./layered_integral]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./liaux]
type = SpatialUserObjectAux
variable = layered_integral
execute_on = timestep_end
user_object = layered_integral
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = u
boundary = bottom
value = 0
[../]
[./top]
type = DirichletBC
variable = u
boundary = top
value = 1
[../]
[]
[UserObjects]
[./layered_integral]
type = LayeredIntegral
direction = y
num_layers = 3
variable = u
execute_on = linear
[../]
[]
[VectorPostprocessors]
[int]
type = SpatialUserObjectVectorPostprocessor
userobject = layered_integral
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
file_base = out
exodus = true
csv = true
[]
(tutorials/tutorial01_app_development/step02_input_file/test/tests/kernels/simple_diffusion/simple_diffusion.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/kernels/vector_fe/lagrange_vec.i)
# This example reproduces the libmesh vector_fe example 1 results
[Mesh]
type = GeneratedMesh
dim = 2
nx = 15
ny = 15
xmin = -1
ymin = -1
elem_type = QUAD9
[]
[Variables]
[./u]
family = LAGRANGE_VEC
order = SECOND
[../]
[]
[Kernels]
[./diff]
type = VectorDiffusion
variable = u
[../]
[./body_force]
type = VectorBodyForce
variable = u
function_x = 'ffx'
function_y = 'ffy'
[../]
[]
[BCs]
[./bnd]
type = VectorFunctionDirichletBC
variable = u
function_x = 'x_exact_sln'
function_y = 'y_exact_sln'
function_z = '0'
boundary = 'left right top bottom'
[../]
[]
[Functions]
[./x_exact_sln]
type = ParsedFunction
value = 'cos(.5*pi*x)*sin(.5*pi*y)'
[../]
[./y_exact_sln]
type = ParsedFunction
value = 'sin(.5*pi*x)*cos(.5*pi*y)'
[../]
[./ffx]
type = ParsedFunction
value = '.5*pi*pi*cos(.5*pi*x)*sin(.5*pi*y)'
[../]
[./ffy]
type = ParsedFunction
value = '.5*pi*pi*sin(.5*pi*x)*cos(.5*pi*y)'
[../]
[]
[Preconditioning]
[./pre]
type = SMP
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/misc/jacobian/inf_nan.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./td]
type = NanKernel
variable = u
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
(modules/navier_stokes/test/tests/finite_volume/pins/mms/2d-rc.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 2
ymin = -1
ymax = 1
nx = 8
ny = 8
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[Variables]
[u]
type = PINSFVSuperficialVelocityVariable
initial_condition = 1
[]
[v]
type = PINSFVSuperficialVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[AuxVariables]
[porosity]
family = MONOMIAL
order = CONSTANT
fv = true
initial_condition = 0.8
[]
[]
[GlobalParams]
porosity = porosity
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = PINSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
porosity = porosity
[]
[]
[FVKernels]
[mass]
type = PINSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[u_advection]
type = PINSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = PINSFVMomentumDiffusion
variable = u
mu = ${mu}
porosity = porosity
momentum_component = 'x'
[]
[u_pressure]
type = PINSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[u_forcing]
type = INSFVBodyForce
variable = u
functor = forcing_u
momentum_component = 'x'
[]
[v_advection]
type = PINSFVMomentumAdvection
variable = v
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = PINSFVMomentumDiffusion
variable = v
mu = ${mu}
porosity = porosity
momentum_component = 'y'
[]
[v_pressure]
type = PINSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[v_forcing]
type = INSFVBodyForce
variable = v
functor = forcing_v
momentum_component = 'y'
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = 'exact_u'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = 'exact_v'
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = u
function = 'exact_u'
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = v
function = 'exact_v'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 'exact_p'
[]
[]
[Functions]
[exact_u]
type = ParsedFunction
value = 'sin((1/2)*y*pi)*cos((1/2)*x*pi)'
[]
[forcing_u]
type = ADParsedFunction
value = '0.5*pi^2*mu*sin((1/2)*y*pi)*cos((1/2)*x*pi) - 0.625*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi) + 0.625*pi*rho*sin((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)^2 - 1.25*pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi) - 0.2*pi*sin((1/4)*x*pi)*sin((3/2)*y*pi)'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_v]
type = ParsedFunction
value = 'sin((1/4)*x*pi)*cos((1/2)*y*pi)'
[]
[forcing_v]
type = ADParsedFunction
value = '0.3125*pi^2*mu*sin((1/4)*x*pi)*cos((1/2)*y*pi) - 1.25*pi*rho*sin((1/4)*x*pi)^2*sin((1/2)*y*pi)*cos((1/2)*y*pi) - 0.625*pi*rho*sin((1/4)*x*pi)*sin((1/2)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*y*pi) + 0.3125*pi*rho*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi) + 1.2*pi*cos((1/4)*x*pi)*cos((3/2)*y*pi)'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_p]
type = ParsedFunction
value = 'sin((3/2)*y*pi)*cos((1/4)*x*pi)'
[]
[forcing_p]
type = ParsedFunction
value = '-1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi) - 1/2*pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2v]
type = ElementL2Error
variable = v
function = exact_v
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2p]
type = ElementL2Error
variable = pressure
function = exact_p
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(test/tests/ics/zero_ic/test.i)
# This test makes sure that when people use an initial condition that accesses _zero
# the code does not crash. The "problem" is that InitialCondition uses _qp which for
# nodal variables loops over nodes, rather then q-points. Thus if people have more
# nodes that q-points (they have to dial a lower q-rule in the Executioner block), the
# code would do an out-of-bounds access and crash.
[Mesh]
type = GeneratedMesh
dim = 3
elem_type = HEX27
[]
[Variables]
[./u]
family = LAGRANGE
order = SECOND
[../]
[]
[ICs]
[./ic_u]
type = ZeroIC
variable = u
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./all]
type = DirichletBC
variable = u
boundary = 'left right top bottom front back'
value = 0
[../]
[]
[Postprocessors]
[./l2_norm]
type = ElementL2Norm
variable = u
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[./Quadrature]
type = GAUSS
order = FIRST
[../]
[]
[Outputs]
csv = true
[]
(modules/fluid_properties/test/tests/brine/brine.i)
# Test BrineFluidProperties calculations of density, viscosity and thermal
# conductivity
#
# Experimental density values from Pitzer et al, "Thermodynamic properties
# of aqueous sodium chloride solution", Journal of Physical and Chemical
# Reference Data, 13, 1-102 (1984)
#
# Experimental viscosity values from Phillips et al, "Viscosity of NaCl and
# other solutions up to 350C and 50MPa pressures", LBL-11586 (1980)
#
# Thermal conductivity values from Ozbek and Phillips, "Thermal conductivity of
# aqueous NaCl solutions from 20C to 330C", LBL-9086 (1980)
#
# --------------------------------------------------------------
# Pressure (Mpa) | 20 | 20 | 40
# Temperature (C) | 50 | 200 | 200
# NaCl molality (mol/kg) | 2 | 2 | 5
# NaCl mass fraction (kg/kg) | 0.1047 | 0.1047 | 0.2261
# --------------------------------------------------------------
# Expected values
# --------------------------------------------------------------
# Density (kg/m^3) | 1068.52 | 959.27 | 1065.58
# Viscosity (1e-6Pa.s) | 679.8 | 180.0 | 263.1
# Thermal conductivity (W/m/K) | 0.630 | 0.649 | 0.633
# --------------------------------------------------------------
# Calculated values
# --------------------------------------------------------------
# Density (kg/m^3) | 1067.18 | 958.68 | 1065.46
# Viscosity (1e-6 Pa.s) | 681.1 | 181.98 | 266.1
# Thermal conductivity (W/m/K) | 0.637 | 0.662 | 0.658
# --------------------------------------------------------------
#
# All results are within expected accuracy
[Mesh]
type = GeneratedMesh
dim = 2
nx = 3
ny = 1
xmax = 3
# This test uses ElementalVariableValue postprocessors on specific
# elements, so element numbering needs to stay unchanged
allow_renumbering = false
[]
[Variables]
[./dummy]
[../]
[]
[AuxVariables]
[./pressure]
family = MONOMIAL
order = CONSTANT
[../]
[./temperature]
family = MONOMIAL
order = CONSTANT
[../]
[./xnacl]
family = MONOMIAL
order = CONSTANT
[../]
[./density]
family = MONOMIAL
order = CONSTANT
[../]
[./enthalpy]
family = MONOMIAL
order = CONSTANT
[../]
[./internal_energy]
family = MONOMIAL
order = CONSTANT
[../]
[]
[Functions]
[./pic]
type = ParsedFunction
value = 'if(x<2,20e6, 40e6)'
[../]
[./tic]
type = ParsedFunction
value = 'if(x<1, 323.15, 473.15)'
[../]
[./xic]
type = ParsedFunction
value = 'if(x<2,0.1047, 0.2261)'
[../]
[]
[ICs]
[./p_ic]
type = FunctionIC
function = pic
variable = pressure
[../]
[./t_ic]
type = FunctionIC
function = tic
variable = temperature
[../]
[./x_ic]
type = FunctionIC
function = xic
variable = xnacl
[../]
[]
[AuxKernels]
[./density]
type = MaterialRealAux
variable = density
property = density
[../]
[./enthalpy]
type = MaterialRealAux
variable = enthalpy
property = enthalpy
[../]
[./internal_energy]
type = MaterialRealAux
variable = internal_energy
property = e
[../]
[]
[Modules]
[./FluidProperties]
[./brine]
type = BrineFluidProperties
[../]
[../]
[]
[Materials]
[./fp_mat]
type = MultiComponentFluidPropertiesMaterialPT
pressure = pressure
temperature = temperature
xmass = xnacl
fp = brine
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = dummy
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Postprocessors]
[./density0]
type = ElementalVariableValue
variable = density
elementid = 0
[../]
[./density1]
type = ElementalVariableValue
variable = density
elementid = 1
[../]
[./density2]
type = ElementalVariableValue
variable = density
elementid = 2
[../]
[./enthalpy0]
type = ElementalVariableValue
variable = enthalpy
elementid = 0
[../]
[./enthalpy1]
type = ElementalVariableValue
variable = enthalpy
elementid = 1
[../]
[./enthalpy2]
type = ElementalVariableValue
variable = enthalpy
elementid = 2
[../]
[./e0]
type = ElementalVariableValue
variable = internal_energy
elementid = 0
[../]
[./e1]
type = ElementalVariableValue
variable = internal_energy
elementid = 1
[../]
[./e2]
type = ElementalVariableValue
variable = internal_energy
elementid = 2
[../]
[]
[Outputs]
csv = true
[]
(modules/porous_flow/test/tests/fluids/brine1_tabulated.i)
# Test the density and viscosity calculated by the brine material using a
# TabulatedFluidProperties userobject for water
# Pressure 20 MPa
# Temperature 50C
# xnacl = 0.1047 (equivalent to 2.0 molality)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[]
[Variables]
[pp]
initial_condition = 20e6
[]
[]
[Kernels]
[dummy]
type = Diffusion
variable = pp
[]
[]
[AuxVariables]
[temp]
initial_condition = 50
[]
[xnacl]
initial_condition = 0.1047
[]
[]
[Modules]
[FluidProperties]
[water]
type = Water97FluidProperties
[]
[watertab]
type = TabulatedFluidProperties
fp = water
save_file = false
[]
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
temperature = temp
[]
[ppss]
type = PorousFlow1PhaseFullySaturated
porepressure = pp
[]
[brine]
type = PorousFlowBrine
water_fp = watertab
temperature_unit = Celsius
xnacl = 0.1047
phase = 0
[]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Postprocessors]
[pressure]
type = ElementIntegralVariablePostprocessor
variable = pp
[]
[temperature]
type = ElementIntegralVariablePostprocessor
variable = temp
[]
[xnacl]
type = ElementIntegralVariablePostprocessor
variable = xnacl
[]
[density]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_fluid_phase_density_qp0'
[]
[viscosity]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_viscosity_qp0'
[]
[enthalpy]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_fluid_phase_enthalpy_qp0'
[]
[internal_energy]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_fluid_phase_internal_energy_qp0'
[]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = brine1
csv = true
[]
(test/tests/misc/check_error/nan_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./nan]
type = NanKernel
variable = u
[../]
[]
[BCs]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-rc-ambient-convection-action.i)
mu=1
rho=1
k=1e-3
cp=1
alpha=1
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 5
ymin = -1
ymax = 1
nx = 50
ny = 16
[]
[]
[Modules]
[NavierStokesFV]
compressibility = 'incompressible'
porous_medium_treatment = false
add_energy_equation = true
density = 'rho'
dynamic_viscosity = 'mu'
thermal_conductivity = 'k'
specific_heat = 'cp'
initial_velocity = '1 1 0'
initial_pressure = 0.0
initial_temperature = 0.0
inlet_boundaries = 'left'
momentum_inlet_types = 'fixed-velocity'
momentum_inlet_function = '1 0'
energy_inlet_types = 'fixed-temperature'
energy_inlet_function = '1'
wall_boundaries = 'top bottom'
momentum_wall_types = 'noslip noslip'
energy_wall_types = 'heatflux heatflux'
energy_wall_function = '0 0'
outlet_boundaries = 'right'
momentum_outlet_types = 'fixed-pressure'
pressure_function = '0'
ambient_convection_alpha = 'alpha'
ambient_temperature = '100'
[]
[]
[Materials]
[const_functor]
type = ADGenericFunctorMaterial
prop_names = 'cp k rho mu alpha'
prop_values = '${cp} ${k} ${rho} ${mu} ${alpha}'
[]
[]
[Postprocessors]
[temp]
type = ElementAverageValue
variable = T_fluid
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[]
(modules/ray_tracing/test/tests/raykernels/line_source_ray_kernel/line_source_ray_kernel.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
xmax = 5
ymax = 5
[]
[Variables/u]
order = FIRST
family = LAGRANGE
[]
[BCs/zero]
type = DirichletBC
variable = u
value = 0
boundary = 'top right bottom left'
[]
[Kernels/diffusion]
type = Diffusion
variable = u
[]
[Postprocessors/postprocessor]
type = FunctionValuePostprocessor
function = 3
execute_on = initial
[]
[RayKernels]
[constant_source]
type = LineSourceRayKernel
variable = u
value = 5
rays = constant_source
[]
[pp_source]
type = LineSourceRayKernel
variable = u
postprocessor = postprocessor
rays = pp_source
[]
[function_source]
type = LineSourceRayKernel
variable = u
function = 'x + 2 * y'
rays = function_source
[]
[mixed_source]
type = LineSourceRayKernel
variable = u
value = 5
postprocessor = postprocessor
function = 'x + 2 * y'
rays = mixed_source
[]
[data_source]
type = LineSourceRayKernel
variable = u
ray_data_factor_names = data
rays = data_source
[]
[aux_data_source]
type = LineSourceRayKernel
variable = u
ray_aux_data_factor_names = aux_data
rays = aux_data_source
[]
[]
[UserObjects/study]
type = RepeatableRayStudy
start_points = '0 2 0
0.5 0.5 0
1 1 0
5 5 0
2 2 0
3 3 0'
end_points = '3 5 0
4.5 1.5 0
2 2 0
4 1 0
3 1 0
3 2 0'
names = 'constant_source
pp_source
function_source
mixed_source
data_source
aux_data_source'
ray_data_names = 'data'
ray_aux_data_names = 'aux_data'
initial_ray_data = '0; 0; 0; 0; 8; 0'
initial_ray_aux_data = '0; 0; 0; 0; 0; 10'
execute_on = PRE_KERNELS
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/png/adv_diff_reaction_test.i)
[Mesh]
dim = 2
file = Mesh24.e
[]
[Variables]
active = 'phi'
[./phi]
order = SECOND
family = LAGRANGE
[../]
[]
[Kernels]
active = 'advection diffusion source'
[./advection]
type = Advection0
variable = phi
Au = 10.
Bu = -6.
Cu = 5.
Av = 10.
Bv = 8.
Cv = -1.
[../]
[./diffusion]
type = Diffusion0
variable = phi
Ak = 10.
Bk = 0.1
Ck = 0.1
[../]
[./source]
type = ForcingFunctionXYZ0
variable = phi
omega0 = 2.
A0 = 1.
B0 = 1.2
C0 = 0.8
Au = 10.
Bu = -6.
Cu = 5.
Av = 10.
Bv = 8.
Cv = -1.
Ak = 10.
Bk = 0.1
Ck = 0.1
[../]
[]
[BCs]
active = 'btm_sca rgt_sca top_sca lft_sca'
[./btm_sca]
type = DirichletBCfuncXYZ0
variable = phi
boundary = 1
omega0 = 2.
A0 = 1.
B0 = 1.2
C0 = 0.8
[../]
[./rgt_sca]
type = DirichletBCfuncXYZ0
variable = phi
boundary = 2
omega0 = 2.
A0 = 1.
B0 = 1.2
C0 = 0.8
[../]
[./top_sca]
type = DirichletBCfuncXYZ0
variable = phi
boundary = 3
omega0 = 2.
A0 = 1.
B0 = 1.2
C0 = 0.8
[../]
[./lft_sca]
type = DirichletBCfuncXYZ0
variable = phi
boundary = 4
omega0 = 2.
A0 = 1.
B0 = 1.2
C0 = 0.8
[../]
[]
[Executioner]
type = Steady
nl_rel_tol = 1.e-10
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_levels -pc_factor_mat_ordering_type'
petsc_options_value = 'ilu 20 rcm'
[]
[Outputs]
[png]
type = PNGOutput
resolution = 25
color = RWB
variable = 'phi'
[]
[]
(test/tests/outputs/misc/warehouse_access.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
console = false
[./exodus2]
type = Exodus
file_base = exodus2
[../]
[./test]
type = OutputObjectTest
[../]
[]
(test/tests/auxkernels/element_quality_aux/element_quality_aux.i)
[Mesh]
type = FileMesh
file = mesh.e
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
[AuxVariables]
[quality]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[qa]
type = ElementQualityAux
variable = quality
metric = SHAPE
[]
[]
(test/tests/materials/boundary_material/fv_material_quadrature.i)
# Parsed material properties depend on the physical location of the element
# This requires the initialization of the quadrature in the FVFlux loop
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 4
ny = 4
elem_type = QUAD9
[]
[Functions]
[linear_x]
type = ADParsedFunction
value = 'x'
[]
[piecewise_linear_x]
type = ADPiecewiseLinear
x = '-1 2'
y = '-1 2'
axis = 'x'
[]
[]
[Variables]
[u]
family = MONOMIAL
order = CONSTANT
fv = true
[]
[]
[FVKernels]
[diff]
type = FVDiffusion
variable = u
coeff = k1
[]
[r]
type = FVReaction
variable = u
[]
[]
[FVBCs]
[all]
type = FVDirichletBC
variable = u
boundary = 'left right bottom top'
value = 1
[]
[]
[Materials]
active = 'k1'
[k1]
type = ADGenericFunctorMaterial
prop_names = 'k1'
prop_values = linear_x
block = 0
[]
[k1_piecewise]
type = ADGenericFunctorMaterial
prop_names = 'k1'
prop_values = piecewise_linear_x
block = 0
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(test/tests/outputs/tecplot/tecplot_binary.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
[./out]
type = Tecplot
binary = true
[../]
[]
(modules/fluid_properties/test/tests/ics/rho_from_pressure_temperature/test.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
allow_renumbering = false
[]
[Modules]
[FluidProperties]
[fp_steam]
type = StiffenedGasFluidProperties
gamma = 1.43
cv = 1040.0
q = 2.03e6
p_inf = 0.0
q_prime = -2.3e4
k = 0.026
mu = 134.4e-7
M = 0.01801488
rho_c = 322.0
[]
[]
[]
[AuxVariables]
[rho]
[]
[p]
[]
[T]
[]
[]
[ICs]
[rho_ic]
type = RhoFromPressureTemperatureIC
variable = rho
p = p
T = T
fp = fp_steam
[]
[p_ic]
type = ConstantIC
variable = p
value = 100e3
[]
[T_ic]
type = ConstantIC
variable = T
value = 500
[]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[rho_test]
type = ElementalVariableValue
elementid = 0
variable = rho
execute_on = 'INITIAL TIMESTEP_END'
[]
[]
[Outputs]
csv = true
execute_on = 'INITIAL'
[]
[Problem]
solve = false
[]
(test/tests/mesh/face_info/face_info_tri.i)
[Mesh]
[generated]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
nx = 2
ymin = -2
ymax = 3
ny = 3
elem_type = 'TRI3'
[]
[]
[Problem]
kernel_coverage_check = false
[]
[Variables]
[u]
[]
[trigger_fv_on]
fv = true
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxVariables]
[v]
family = MONOMIAL
order = CONSTANT
[]
[]
[VectorPostprocessors]
[face_info]
type = TestFaceInfo
vars = 'u v'
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
[]
(test/tests/geomsearch/3d_penetration_locator/3d_tet.i)
[Mesh]
file = 3d_thermal_contact_tet.e
dim = 2
construct_side_list_from_node_list = true
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./gap_distance]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = leftleft
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = rightright
value = 1
[../]
[]
[AuxKernels]
[./distance]
type = PenetrationAux
variable = gap_distance
boundary = leftright
paired_boundary = rightleft
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/porous_flow/test/tests/relperm/brooks_corey1.i)
# Test Brooks-Corey relative permeability curve by varying saturation over the mesh
# Exponent lambda = 2 for both phases
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Variables]
[p0]
initial_condition = 1e6
[]
[s1]
[]
[]
[AuxVariables]
[s0aux]
family = MONOMIAL
order = CONSTANT
[]
[s1aux]
family = MONOMIAL
order = CONSTANT
[]
[kr0aux]
family = MONOMIAL
order = CONSTANT
[]
[kr1aux]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[s0]
type = PorousFlowPropertyAux
property = saturation
phase = 0
variable = s0aux
[]
[s1]
type = PorousFlowPropertyAux
property = saturation
phase = 1
variable = s1aux
[]
[kr0]
type = PorousFlowPropertyAux
property = relperm
phase = 0
variable = kr0aux
[]
[kr1]
type = PorousFlowPropertyAux
property = relperm
phase = 1
variable = kr1aux
[]
[]
[Functions]
[s1]
type = ParsedFunction
value = x
[]
[]
[ICs]
[s1]
type = FunctionIC
variable = s1
function = s1
[]
[]
[Kernels]
[p0]
type = Diffusion
variable = p0
[]
[s1]
type = Diffusion
variable = s1
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'p0 s1'
number_fluid_phases = 2
number_fluid_components = 2
[]
[pc]
type = PorousFlowCapillaryPressureConst
pc = 0
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow2PhasePS
phase0_porepressure = p0
phase1_saturation = s1
capillary_pressure = pc
[]
[kr0]
type = PorousFlowRelativePermeabilityBC
phase = 0
lambda = 2
[]
[kr1]
type = PorousFlowRelativePermeabilityBC
phase = 1
lambda = 2
nw_phase = true
[]
[]
[VectorPostprocessors]
[vpp]
type = LineValueSampler
warn_discontinuous_face_values = false
variable = 's0aux s1aux kr0aux kr1aux'
start_point = '0 0 0'
end_point = '1 0 0'
num_points = 20
sort_by = id
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
nl_abs_tol = 1e-8
[]
[BCs]
[sleft]
type = DirichletBC
variable = s1
value = 0
boundary = left
[]
[sright]
type = DirichletBC
variable = s1
value = 1
boundary = right
[]
[]
[Outputs]
csv = true
execute_on = timestep_end
[]
(modules/ray_tracing/test/tests/userobjects/cone_ray_study/cone_ray_study_3d.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 3
nx = 5
ny = 5
nz = 2
xmax = 5
ymax = 5
zmax = 2
[]
[]
[Variables/u]
[]
[Kernels]
[reaction]
type = Reaction
variable = u
[]
[diffusion]
type = Diffusion
variable = u
[]
[]
[UserObjects/study]
type = ConeRayStudy
start_points = '2.5 2.5 0'
directions = '0 0 1'
half_cone_angles = 10
# Must be set with RayKernels that
# contribute to the residual
execute_on = PRE_KERNELS
# For outputting Rays
always_cache_traces = true
ray_data_name = weight
[]
[RayKernels/null]
type = NullRayKernel
[]
# Rays only hit the front surface
[RayBCs/kill]
type = KillRayBC
boundary = 'front'
[]
[RayKernels/line_source]
type = LineSourceRayKernel
variable = u
# Scale by the weights in the ConeRayStudy
ray_data_factor_names = weight
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[rays]
type = RayTracingExodus
study = study
execute_on = FINAL
[]
[]
[Adaptivity]
steps = 0 # 6 for pretty pictures
marker = marker
initial_marker = marker
max_h_level = 6
[Indicators/indicator]
type = GradientJumpIndicator
variable = u
[]
[Markers/marker]
type = ErrorFractionMarker
indicator = indicator
coarsen = 0.25
refine = 0.5
[]
[]
(modules/reactor/test/tests/meshgenerators/reporting_id/hexagonal_id/core_reporting_id_exclude.i)
[Mesh]
[assembly]
type = SimpleHexagonGenerator
hexagon_size = 5.0
hexagon_size_style = 'apothem'
block_id = '1'
[]
[dummy]
type = SimpleHexagonGenerator
hexagon_size = 5.0
hexagon_size_style = 'apothem'
block_id = '2'
[]
[core]
type = HexIDPatternedMeshGenerator
inputs = 'assembly dummy'
pattern_boundary = none
pattern = ' 1 0 1;
0 0 0 0;
1 0 0 0 1;
0 0 0 0;
1 0 1'
assign_type = 'cell'
id_name = 'assembly_id'
exclude_id = 'dummy'
[]
[del_dummy]
type = BlockDeletionGenerator
block = 2
input = core
new_boundary = core_out
[]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[AuxVariables]
[assembly_id]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[set_assembly_id]
type = ExtraElementIDAux
variable = assembly_id
extra_id_name = assembly_id
[]
[]
[Outputs]
exodus = true
execute_on = timestep_end
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_mortar_action/modular_gap_heat_transfer_mortar_displaced_radiation_conduction_action_existing_UOs.i)
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
[file]
type = FileMeshGenerator
file = 2blk-gap.e
[]
allow_renumbering = false
[]
[Problem]
kernel_coverage_check = false
material_coverage_check = false
[]
[Variables]
[temp]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[disp_x]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[disp_y]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[]
[Materials]
[left]
type = ADHeatConductionMaterial
block = 1
thermal_conductivity = 0.01
specific_heat = 1
[]
[right]
type = ADHeatConductionMaterial
block = 2
thermal_conductivity = 0.005
specific_heat = 1
[]
[]
[Kernels]
[hc_displaced_block]
type = ADHeatConduction
variable = temp
use_displaced_mesh = true
block = '1'
[]
[hc_undisplaced_block]
type = ADHeatConduction
variable = temp
use_displaced_mesh = false
block = '2'
[]
[disp_x]
type = Diffusion
variable = disp_x
block = '1 2'
[]
[disp_y]
type = Diffusion
variable = disp_y
block = '1 2'
[]
[]
[MortarGapHeatTransfer]
[mortar_heat_transfer]
temperature = temp
boundary = 100
use_displaced_mesh = true
primary_boundary = 100
secondary_boundary = 101
user_created_gap_flux_models = 'radiation_uo conduction_uo'
[]
[]
[UserObjects]
[radiation_uo]
type = GapFluxModelRadiation
temperature = temp
boundary = 100
primary_emissivity = 1.0
secondary_emissivity = 1.0
use_displaced_mesh = true
[]
[conduction_uo]
type = GapFluxModelConduction
temperature = temp
boundary = 100
gap_conductivity = 0.02
use_displaced_mesh = true
[]
[]
[BCs]
[left]
type = DirichletBC
variable = temp
boundary = 'left'
value = 100
[]
[right]
type = DirichletBC
variable = temp
boundary = 'right'
value = 0
[]
[left_disp_x]
type = DirichletBC
preset = false
variable = disp_x
boundary = 'left'
value = .1
[]
[right_disp_x]
type = DirichletBC
preset = false
variable = disp_x
boundary = 'right'
value = 0
[]
[bottom_disp_y]
type = DirichletBC
preset = false
variable = disp_y
boundary = 'bottom'
value = 0
[]
[]
[Preconditioning]
[fmp]
type = SMP
full = true
solve_type = 'NEWTON'
[]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-11
nl_abs_tol = 1.0e-10
[]
[VectorPostprocessors]
[NodalTemperature]
type = NodalValueSampler
sort_by = id
boundary = '100 101'
variable = 'temp'
[]
[]
[Outputs]
csv = true
[exodus]
type = Exodus
show = 'temp'
[]
[]
(test/tests/executioners/solve_type_linear/linear_with_full_smp.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
[]
[Variables]
[u]
[]
[v]
[]
[]
[Kernels]
[u_diffusion]
type = Diffusion
variable = u
[]
[v_diffusion]
type = Diffusion
variable = v
[]
[u_reaction]
type = Reaction
variable = u
[]
[v_reaction]
type = Reaction
variable = v
[]
[u_force]
type = BodyForce
variable = u
[]
[v_force]
type = CoupledForce
variable = v
v = u
[]
[]
[Executioner]
type = Steady
solve_type = LINEAR
[]
[Outputs]
exodus = true
[]
(modules/porous_flow/test/tests/thm_rehbinder/free_outer.i)
[Mesh]
[annular]
type = AnnularMeshGenerator
nr = 40
nt = 16
rmin = 0.1
rmax = 1
dmin = 0.0
dmax = 90
growth_r = 1.1
[]
[make3D]
input = annular
type = MeshExtruderGenerator
bottom_sideset = bottom
top_sideset = top
extrusion_vector = '0 0 1'
num_layers = 1
[]
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
PorousFlowDictator = dictator
biot_coefficient = 1.0
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[disp_z]
[]
[porepressure]
[]
[temperature]
[]
[]
[BCs]
# sideset 1 = outer
# sideset 2 = cavity
# sideset 3 = ymin
# sideset 4 = xmin
[plane_strain]
type = DirichletBC
variable = disp_z
value = 0
boundary = 'top bottom'
[]
[ymin]
type = DirichletBC
variable = disp_y
value = 0
boundary = dmin
[]
[xmin]
type = DirichletBC
variable = disp_x
value = 0
boundary = dmax
[]
[cavity_temperature]
type = DirichletBC
variable = temperature
value = 1000
boundary = rmin
[]
[cavity_porepressure]
type = DirichletBC
variable = porepressure
value = 1E6
boundary = rmin
[]
[cavity_zero_effective_stress_x]
type = Pressure
variable = disp_x
function = 1E6
boundary = rmin
use_displaced_mesh = false
[]
[cavity_zero_effective_stress_y]
type = Pressure
variable = disp_y
function = 1E6
boundary = rmin
use_displaced_mesh = false
[]
[outer_temperature]
type = DirichletBC
variable = temperature
value = 0
boundary = rmax
[]
[outer_pressure]
type = DirichletBC
variable = porepressure
value = 0
boundary = rmax
[]
[]
[AuxVariables]
[stress_rr]
family = MONOMIAL
order = CONSTANT
[]
[stress_pp]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[stress_rr]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = stress_rr
scalar_type = RadialStress
point1 = '0 0 0'
point2 = '0 0 1'
[]
[stress_pp]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = stress_pp
scalar_type = HoopStress
point1 = '0 0 0'
point2 = '0 0 1'
[]
[]
[Modules]
[FluidProperties]
[the_simple_fluid]
type = SimpleFluidProperties
thermal_expansion = 0.0
bulk_modulus = 1E12
viscosity = 1.0E-3
density0 = 1000.0
cv = 1000.0
cp = 1000.0
porepressure_coefficient = 0.0
[]
[]
[]
[PorousFlowBasicTHM]
coupling_type = ThermoHydroMechanical
multiply_by_density = false
add_stress_aux = true
porepressure = porepressure
temperature = temperature
eigenstrain_names = thermal_contribution
gravity = '0 0 0'
fp = the_simple_fluid
[]
[Materials]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1E10
poissons_ratio = 0.2
[]
[strain]
type = ComputeSmallStrain
eigenstrain_names = thermal_contribution
[]
[thermal_contribution]
type = ComputeThermalExpansionEigenstrain
temperature = temperature
thermal_expansion_coeff = 1E-6
eigenstrain_name = thermal_contribution
stress_free_temperature = 0.0
[]
[stress]
type = ComputeLinearElasticStress
[]
[porosity]
type = PorousFlowPorosityConst # only the initial value of this is ever used
porosity = 0.1
[]
[biot_modulus]
type = PorousFlowConstantBiotModulus
solid_bulk_compliance = 1E-10
fluid_bulk_modulus = 1E12
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1E-12 0 0 0 1E-12 0 0 0 1E-12'
[]
[thermal_expansion]
type = PorousFlowConstantThermalExpansionCoefficient
fluid_coefficient = 1E-6
drained_coefficient = 1E-6
[]
[thermal_conductivity]
type = PorousFlowThermalConductivityIdeal
dry_thermal_conductivity = '1E6 0 0 0 1E6 0 0 0 1E6'
[]
[]
[VectorPostprocessors]
[P]
type = LineValueSampler
start_point = '0.1 0 0'
end_point = '1.0 0 0'
num_points = 10
sort_by = x
variable = porepressure
[]
[T]
type = LineValueSampler
start_point = '0.1 0 0'
end_point = '1.0 0 0'
num_points = 10
sort_by = x
variable = temperature
[]
[U]
type = LineValueSampler
start_point = '0.1 0 0'
end_point = '1.0 0 0'
num_points = 10
sort_by = x
variable = disp_x
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -snes_rtol'
petsc_options_value = 'gmres asm lu 1E-8'
[]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
file_base = free_outer
execute_on = timestep_end
csv = true
[]
(modules/heat_conduction/test/tests/heat_conduction/coupled_convective_heat_flux/on_off.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./t_infinity]
[../]
[./active]
initial_condition = 1
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./force]
type = BodyForce
variable = u
value = 1000
[../]
[]
[AuxKernels]
[./t_infinity]
type = ConstantAux
variable = t_infinity
value = 500
execute_on = initial
[../]
[./active_right]
type = ConstantAux
variable = active
value = 0
boundary = right
[../]
[]
[BCs]
[./right]
type = CoupledConvectiveHeatFluxBC
variable = u
boundary = 'left right top bottom'
htc = 10
T_infinity = t_infinity
scale_factor = active
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/mms/rc.i)
mu=1.1
rho=1.1
[GlobalParams]
two_term_boundary_expansion = false
rhie_chow_user_object = 'rc'
velocity_interp_method = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 2
ny = 2
[]
[]
[Problem]
fv_bcs_integrity_check = false
error_on_jacobian_nonzero_reallocation = true
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[lambda]
family = SCALAR
order = FIRST
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = 'average'
rho = ${rho}
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[mean_zero_pressure]
type = FVScalarLagrangeMultiplier
variable = pressure
lambda = lambda
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_interp_method = 'average'
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[u_forcing]
type = INSFVBodyForce
variable = u
functor = forcing_u
momentum_component = 'x'
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_interp_method = 'average'
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[v_forcing]
type = INSFVBodyForce
variable = v
functor = forcing_v
momentum_component = 'y'
[]
[]
[FVBCs]
[no-slip-wall-u]
type = INSFVNoSlipWallBC
boundary = 'left right top bottom'
variable = u
function = 'exact_u'
[]
[no-slip-wall-v]
type = INSFVNoSlipWallBC
boundary = 'left right top bottom'
variable = v
function = 'exact_v'
[]
[]
[Functions]
[exact_u]
type = ParsedFunction
value = 'sin(y)*cos((1/2)*x*pi)'
[]
[exact_rhou]
type = ParsedFunction
value = 'rho*sin(y)*cos((1/2)*x*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_u]
type = ADParsedFunction
value = 'mu*sin(y)*cos((1/2)*x*pi) + (1/4)*pi^2*mu*sin(y)*cos((1/2)*x*pi) - 1/2*pi*rho*sin(x)*sin(y)*sin((1/2)*y*pi)*cos((1/2)*x*pi) + rho*sin(x)*cos(y)*cos((1/2)*x*pi)*cos((1/2)*y*pi) - pi*rho*sin(y)^2*sin((1/2)*x*pi)*cos((1/2)*x*pi) + sin(y)*cos(x)'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_v]
type = ParsedFunction
value = 'sin(x)*cos((1/2)*y*pi)'
[]
[exact_rhov]
type = ParsedFunction
value = 'rho*sin(x)*cos((1/2)*y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_v]
type = ADParsedFunction
value = 'mu*sin(x)*cos((1/2)*y*pi) + (1/4)*pi^2*mu*sin(x)*cos((1/2)*y*pi) - pi*rho*sin(x)^2*sin((1/2)*y*pi)*cos((1/2)*y*pi) - 1/2*pi*rho*sin(x)*sin(y)*sin((1/2)*x*pi)*cos((1/2)*y*pi) + rho*sin(y)*cos(x)*cos((1/2)*x*pi)*cos((1/2)*y*pi) + sin(x)*cos(y)'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_p]
type = ParsedFunction
value = 'sin(x)*sin(y)'
[]
[forcing_p]
type = ParsedFunction
value = '-1/2*pi*rho*sin(x)*sin((1/2)*y*pi) - 1/2*pi*rho*sin(y)*sin((1/2)*x*pi)'
vars = 'rho'
vals = '${rho}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 30 lu NONZERO'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[./L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2v]
variable = v
function = exact_v
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2p]
variable = pressure
function = exact_p
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[]
(test/tests/kernels/hfem/3d-lower-d-volumes.i)
[Mesh]
[square]
type = GeneratedMeshGenerator
nx = 3
ny = 3
nz = 3
dim = 3
[]
build_all_side_lowerd_mesh = true
[]
[Variables]
[u]
order = THIRD
family = MONOMIAL
block = 0
[]
[uhat]
order = CONSTANT
family = MONOMIAL
block = BOUNDARY_SIDE_LOWERD_SUBDOMAIN
[]
[lambda]
order = CONSTANT
family = MONOMIAL
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
[]
[lambdab]
order = CONSTANT
family = MONOMIAL
block = BOUNDARY_SIDE_LOWERD_SUBDOMAIN
[]
[]
[AuxVariables]
[v]
order = CONSTANT
family = MONOMIAL
block = 0
initial_condition = '1'
[]
[]
[Kernels]
[diff]
type = MatDiffusion
variable = u
diffusivity = '1'
block = 0
[]
[source]
type = CoupledForce
variable = u
v = v
coef = '1'
block = 0
[]
[reaction]
type = Reaction
variable = uhat
rate = '1'
block = BOUNDARY_SIDE_LOWERD_SUBDOMAIN
[]
[uhat_coupled]
type = CoupledForce
variable = uhat
block = BOUNDARY_SIDE_LOWERD_SUBDOMAIN
v = lambdab
coef = '1'
[]
[]
[DGKernels]
[surface]
type = TestLowerDVolumes
variable = u
lowerd_variable = lambda
l = 1
n = 3
[]
[]
[BCs]
[all]
type = HFEMDirichletBC
boundary = 'left right top bottom back front'
variable = u
lowerd_variable = lambdab
uhat = uhat
[]
[]
[Postprocessors]
[intu]
type = ElementIntegralVariablePostprocessor
variable = u
block = 0
[]
[lambdanorm]
type = ElementL2Norm
variable = lambda
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu basic mumps'
[]
[Outputs]
[out]
# we hide lambda because it may flip sign due to element
# renumbering with distributed mesh
type = Exodus
hide = lambda
[]
csv = true
[]
(modules/ray_tracing/test/tests/userobjects/cone_ray_study/cone_ray_study.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
xmax = 5
ymax = 5
[]
[]
[Variables/u]
[]
[Kernels]
[reaction]
type = Reaction
variable = u
[]
[diffusion]
type = Diffusion
variable = u
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[UserObjects/study]
type = ConeRayStudy
start_points = '1 1.5 0'
directions = '2 1 0'
half_cone_angles = 2.5
ray_data_name = weight
# Must be set with RayKernels that
# contribute to the residual
execute_on = PRE_KERNELS
# For outputting Rays
always_cache_traces = true
[]
[RayBCs]
[reflect]
type = ReflectRayBC
boundary = 'right'
[]
[kill_rest]
type = KillRayBC
boundary = 'top'
[]
[]
[RayKernels/line_source]
type = LineSourceRayKernel
variable = u
# Scale by the weights in the ConeRayStudy
ray_data_factor_names = weight
[]
[Outputs]
exodus = true
[rays]
type = RayTracingExodus
study = study
execute_on = FINAL
[]
[]
[Adaptivity]
steps = 0 # 6 for pretty pictures
marker = marker
initial_marker = marker
max_h_level = 6
[Indicators/indicator]
type = GradientJumpIndicator
variable = u
[]
[Markers/marker]
type = ErrorFractionMarker
indicator = indicator
coarsen = 0.25
refine = 0.5
[]
[]
(test/tests/reporters/declare_initial_setup/declare_initial_setup.i)
[Mesh]
[generate]
type = GeneratedMeshGenerator
dim = 1
[]
[]
[Variables/u]
[]
[Executioner]
type = Steady
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[Reporters]
active = initialSetup
[initialSetup]
type = TestDeclareInitialSetupReporter
value = 1980
[]
[info]
type = MeshInfo
items = num_elements
[]
[]
[Outputs]
[out]
type = JSON
execute_on = FINAL
execute_system_information_on = NONE
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/cylindrical/cartesian-version/2d-rc-symmetry.i)
mu=1.1
rho=1.1
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = -1
ymax = 1
nx = 2
ny = 2
[]
[]
[Problem]
fv_bcs_integrity_check = false
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
two_term_boundary_expansion = true
advected_interp_method = 'average'
velocity_interp_method = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
[]
[v]
type = INSFVVelocityVariable
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[ICs]
[u]
type = FunctionIC
function = 'exact_u'
variable = u
[]
[v]
type = FunctionIC
function = 'exact_v'
variable = v
[]
[pressure]
type = FunctionIC
function = 'exact_p'
variable = pressure
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
rho = ${rho}
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[u_forcing]
type = INSFVBodyForce
variable = u
functor = forcing_u
momentum_component = 'x'
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[v_forcing]
type = INSFVBodyForce
variable = v
functor = forcing_v
momentum_component = 'y'
[]
[]
[FVBCs]
[u_wall]
type = INSFVNoSlipWallBC
variable = u
boundary = 'right'
function = 'exact_u'
[]
[v_wall]
type = INSFVNoSlipWallBC
variable = v
boundary = 'right'
function = 'exact_v'
[]
[u_axis]
type = INSFVSymmetryVelocityBC
variable = u
boundary = 'left'
mu = ${mu}
u = u
v = v
momentum_component = 'x'
[]
[v_axis]
type = INSFVSymmetryVelocityBC
variable = v
boundary = 'left'
mu = ${mu}
u = u
v = v
momentum_component = 'y'
[]
[p_axis]
type = INSFVSymmetryPressureBC
variable = pressure
boundary = 'left'
[]
[p]
type = INSFVOutletPressureBC
variable = pressure
function = 'exact_p'
boundary = 'top'
[]
[inlet_u]
type = INSFVInletVelocityBC
variable = u
function = 'exact_u'
boundary = 'bottom'
[]
[inlet_v]
type = INSFVInletVelocityBC
variable = v
function = 'exact_v'
boundary = 'bottom'
[]
[]
[Functions]
[exact_u]
type = ParsedFunction
value = 'sin(x*pi)*cos(y*pi)'
[]
[forcing_u]
type = ADParsedFunction
value = '2*pi^2*mu*sin(x*pi)*cos(y*pi) - 2*pi*rho*sin(x*pi)*sin(y*pi)*cos(1.3*x)*cos(y*pi) + 2*pi*rho*sin(x*pi)*cos(x*pi)*cos(y*pi)^2 - 1.5*sin(1.5*x)*cos(1.6*y)'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_v]
type = ParsedFunction
value = 'cos(1.3*x)*cos(y*pi)'
[]
[forcing_v]
type = ADParsedFunction
value = '1.69*mu*cos(1.3*x)*cos(y*pi) + pi^2*mu*cos(1.3*x)*cos(y*pi) - 1.3*rho*sin(1.3*x)*sin(x*pi)*cos(y*pi)^2 - 2*pi*rho*sin(y*pi)*cos(1.3*x)^2*cos(y*pi) + pi*rho*cos(1.3*x)*cos(x*pi)*cos(y*pi)^2 - 1.6*sin(1.6*y)*cos(1.5*x)'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_p]
type = ParsedFunction
value = 'cos(1.5*x)*cos(1.6*y)'
[]
[forcing_p]
type = ParsedFunction
value = '-pi*rho*sin(y*pi)*cos(1.3*x) + pi*rho*cos(x*pi)*cos(y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_shift_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu NONZERO superlu_dist'
line_search = 'none'
nl_rel_tol = 1e-12
nl_abs_tol = 1e-12
[]
[Outputs]
exodus = false
csv = true
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[./L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2v]
type = ElementL2Error
variable = v
function = exact_v
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2p]
variable = pressure
function = exact_p
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[p_avg]
type = ElementAverageValue
variable = pressure
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(modules/navier_stokes/test/tests/finite_element/ins/jacobian_test/jacobian_traction_stabilized.i)
# This input file tests the jacobians of many of the INS kernels
[GlobalParams]
gravity = '1.1 1.1 1.1'
u = vel_x
v = vel_y
w = vel_z
pressure = p
integrate_p_by_parts = false
laplace = false
supg = true
pspg = true
alpha = 1.1
[]
[Mesh]
type = GeneratedMesh
dim = 3
xmin = 0
xmax = 3.0
ymin = 0
ymax = 1.5
zmax = 1.1
nx = 1
ny = 1
nz = 1
elem_type = HEX27
[]
[Variables]
[./vel_x]
order = SECOND
family = LAGRANGE
[../]
[./vel_y]
order = SECOND
family = LAGRANGE
[../]
[./vel_z]
order = SECOND
family = LAGRANGE
[../]
[./p]
order = SECOND
family = LAGRANGE
[../]
[]
[Kernels]
[./mass]
type = INSMass
variable = p
[../]
[./x_momentum_space]
type = INSMomentumTractionForm
variable = vel_x
component = 0
[../]
[./y_momentum_space]
type = INSMomentumTractionForm
variable = vel_y
component = 1
[../]
[./z_momentum_space]
type = INSMomentumTractionForm
variable = vel_z
component = 2
[../]
[]
[Materials]
[./const]
type = GenericConstantMaterial
block = 0
prop_names = 'rho mu'
prop_values = '0.5 1.5'
[../]
[]
[Preconditioning]
[./SMP_PJFNK]
type = SMP
full = true
[../]
[]
[Executioner]
solve_type = NEWTON
type = Steady
petsc_options_iname = '-snes_type'
petsc_options_value = 'test'
[]
[ICs]
[./p]
type = RandomIC
variable = p
min = 0.5
max = 1.5
[../]
[./vel_x]
type = RandomIC
variable = vel_x
min = 0.5
max = 1.5
[../]
[./vel_y]
type = RandomIC
variable = vel_y
min = 0.5
max = 1.5
[../]
[./vel_z]
type = RandomIC
variable = vel_z
min = 0.5
max = 1.5
[../]
[]
(test/tests/multiapps/secant/steady_main.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
parallel_type = replicated
uniform_refine = 1
[]
[Variables]
[u]
[]
[]
[AuxVariables]
[v]
[]
[]
[Kernels]
[diff]
type = CoefDiffusion
variable = u
coef = 0.1
[]
[force_u]
type = CoupledForce
variable = u
v = v
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Postprocessors]
[unorm]
type = ElementL2Norm
variable = u
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
nl_abs_tol = 1e-14
fixed_point_algorithm = 'secant'
fixed_point_max_its = 30
transformed_variables = 'u'
[]
[Outputs]
csv = true
exodus = false
[]
[MultiApps]
[sub]
type = FullSolveMultiApp
app_type = MooseTestApp
positions = '0 0 0'
input_files = 'steady_sub.i'
clone_master_mesh = true
transformed_variables = 'v'
[]
[]
[Transfers]
[v_from_sub]
type = MultiAppNearestNodeTransfer
from_multi_app = sub
source_variable = v
variable = v
[]
[u_to_sub]
type = MultiAppNearestNodeTransfer
to_multi_app = sub
source_variable = u
variable = u
[]
[]
(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/heated/2d-rc-heated-boussinesq-action.i)
mu=1
rho=1
k=1e-3
cp=1
v_inlet=1
T_inlet=200
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 2
ymin = 0
ymax = 10
nx = 20
ny = 100
[]
[]
[AuxVariables]
[T_solid]
type = MooseVariableFVReal
initial_condition = 100
[]
[porosity]
type = MooseVariableFVReal
initial_condition = 0.4
[]
[]
[Modules]
[NavierStokesFV]
compressibility = 'incompressible'
porous_medium_treatment = true
add_energy_equation = true
boussinesq_approximation = true
density = ${rho}
dynamic_viscosity = ${mu}
thermal_conductivity = ${k}
specific_heat = ${cp}
porosity = 'porosity'
thermal_expansion = 8e-4
gravity = '0 -9.81 0'
ref_temperature = 150
initial_velocity = '1e-6 ${v_inlet} 0'
initial_pressure = 0.0
initial_temperature = 0.0
inlet_boundaries = 'bottom'
momentum_inlet_types = 'fixed-velocity'
momentum_inlet_function = '0 ${v_inlet}'
energy_inlet_types = 'heatflux'
energy_inlet_function = '${fparse v_inlet * rho * cp * T_inlet}'
wall_boundaries = 'right left'
momentum_wall_types = 'noslip symmetry'
energy_wall_types = 'heatflux heatflux'
energy_wall_function = '0 0'
outlet_boundaries = 'top'
momentum_outlet_types = 'fixed-pressure'
pressure_function = '0'
ambient_convection_alpha = 1e-3
ambient_temperature = 'T_solid'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
# Some basic Postprocessors to examine the solution
[Postprocessors]
[inlet-p]
type = SideAverageValue
variable = pressure
boundary = 'top'
[]
[outlet-v]
type = SideAverageValue
variable = superficial_vel_y
boundary = 'top'
[]
[outlet-temp]
type = SideAverageValue
variable = T_fluid
boundary = 'top'
[]
[]
[Outputs]
exodus = true
csv = false
[]
(test/tests/meshgenerators/combiner_generator/combiner_generator_from_file.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[cmbn]
type = CombinerGenerator
inputs = 'gen'
positions_file = 'positions.txt'
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/bcs/function_neumann_bc/test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
dim = 2
nx = 32
ny = 32
[../]
[]
[Variables]
[./u]
[../]
[]
[Functions]
[./exact_func]
type = ParsedFunction
value = x*x
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
value = 2
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = FunctionNeumannBC
function = exact_func
variable = u
boundary = right
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
execute_on = 'timestep_end'
file_base = neumannbc_out
exodus = true
[]
(test/tests/partitioners/block_weighted_partitioner/block_weighted_partitioner.i)
[Mesh]
type = FileMesh
file = block_weighted_partitioner.e
[Partitioner]
type = BlockWeightedPartitioner
block = '1 2 3'
weight = '3 1 10'
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = Newton
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
[AuxVariables]
[pid]
family = MONOMIAL
order = CONSTANT
[]
[npid]
family = Lagrange
order = first
[]
[]
[AuxKernels]
[pid_aux]
type = ProcessorIDAux
variable = pid
execute_on = 'INITIAL'
[]
[npid_aux]
type = ProcessorIDAux
variable = npid
execute_on = 'INITIAL'
[]
[]
(test/tests/misc/deprecation/deprecated_coupled_var.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[v][]
[]
[Kernels]
active = 'diff_u coupled_u diff_v deprecated_coupled_v'
[./diff_u]
type = Diffusion
variable = u
[../]
[coupled_u]
type = DeprecatedCoupledVarKernel
variable = u
source = v
[]
[diff_v]
type = Diffusion
variable = v
[]
[deprecated_coupled_v]
type = DeprecatedCoupledVarKernel
variable = v
stupid_name = u
[]
[blessed_coupled_v]
type = DeprecatedCoupledVarKernel
variable = v
source = u
[]
[]
[BCs]
[./left_u]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = left
value = 1
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = right
value = 0
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(modules/ray_tracing/test/tests/userobjects/cone_ray_study/cone_ray_study_errors.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
[]
[]
[UserObjects/study]
type = ConeRayStudy
start_points = '1 1.5 0'
directions = '2 1 0'
half_cone_angles = 2.5
ray_data_name = weight
[]
[Executioner]
type = Steady
[]
(test/tests/outputs/displaced/non_displaced_fallback.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 2
[]
[AuxVariables]
[./a]
[../]
[]
[AuxKernels]
[./a_ak]
type = ConstantAux
variable = a
value = 1.
execute_on = initial
[../]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
[./exodus]
type = Exodus
use_displaced = true
[../]
[]
(modules/thermal_hydraulics/test/tests/userobjects/function_element_loop_integral_uo/function_element_loop_integral_uo.i)
[Mesh]
type = GeneratedMesh
dim = 1
xmin = 0
xmax = 10
nx = 10
[]
[Functions]
# Integral of this function should be 2*3 + 3*6 + 5*2 = 34
[test_fn]
type = PiecewiseConstant
axis = x
x = '0 2 5'
y = '3 6 2'
[]
[]
[UserObjects]
[test_uo]
type = FunctionElementLoopIntegralUserObject
function = test_fn
execute_on = 'INITIAL'
[]
[]
[Postprocessors]
[test_pp]
type = FunctionElementLoopIntegralGetValueTestPostprocessor
function_element_loop_integral_uo = test_uo
execute_on = 'INITIAL'
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
[]
(test/tests/misc/check_error/range_check_param.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
bias_x = 0.1
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/thermal_hydraulics/test/tests/jacobians/bcs/external_app_convection_heat_transfer_rz_bc/external_app_convection_heat_transfer_rz_bc.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
[]
[Variables]
[T]
initial_condition = 300
[]
[]
[AuxVariables]
[T_ext]
initial_condition = 400
[]
[htc_ext]
initial_condition = 0.5
[]
[]
[BCs]
[bc]
type = ExternalAppConvectionHeatTransferRZBC
variable = T
boundary = 2
htc_ext = htc_ext
T_ext = T_ext
axis_point = '0 0 0'
axis_dir = '1 0 0'
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Problem]
kernel_coverage_check = false
[]
[Executioner]
type = Steady
petsc_options = '-snes_test_jacobian'
petsc_options_iname = '-snes_test_error'
petsc_options_value = '1e-8'
[]
(test/tests/postprocessors/volume/sphere1D.i)
# The volume of each block should be 3
[Mesh]#Comment
file = sphere1D.e
[] # Mesh
[Problem]
coord_type = RSPHERICAL
[]
[Functions]
[./fred]
type = ParsedFunction
value='200'
[../]
[] # Functions
[AuxVariables]
[./constantVar]
order = FIRST
family = LAGRANGE
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
initial_condition = 100
[../]
[] # Variables
[AuxKernels]
[./fred]
type = ConstantAux
variable = constantVar
block = 1
value = 1
[../]
[]
[ICs]
[./ic1]
type = ConstantIC
variable = constantVar
value = 1
block = 1
[../]
[]
[Kernels]
[./heat_r]
type = Diffusion
variable = u
[../]
[] # Kernels
[BCs]
[./temps]
type = FunctionDirichletBC
variable = u
boundary = 1
function = fred
[../]
[] # BCs
[Materials]
[] # Materials
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -snes_ls -ksp_gmres_restart'
petsc_options_value = 'lu basic 101'
line_search = 'none'
nl_abs_tol = 1e-11
nl_rel_tol = 1e-10
l_max_its = 20
[] # Executioner
[Postprocessors]
[./should_be_one]
type = ElementAverageValue
block = 1
variable = constantVar
execute_on = 'initial timestep_end'
[../]
[./volume1]
type = VolumePostprocessor
block = 1
execute_on = 'initial timestep_end'
[../]
[./volume2]
type = VolumePostprocessor
block = 2
execute_on = 'initial timestep_end'
[../]
[./volume3]
type = VolumePostprocessor
block = 3
execute_on = 'initial timestep_end'
[../]
[]
[Outputs]
exodus = true
[] # Output
(modules/combined/test/tests/restart-transient-from-ss-with-stateful/master_ss.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
nx = 8
ny = 8
xmin = -82.627
xmax = 82.627
ymin = -82.627
ymax = 82.627
dim = 2
[]
[]
[Variables]
[./temp]
order = FIRST
family = LAGRANGE
initial_condition = 500
[../]
[]
[AuxVariables]
[./power]
order = FIRST
family = L2_LAGRANGE
initial_condition = 350
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[./heat_source_fuel]
type = CoupledForce
variable = temp
v = 'power'
[../]
[]
[BCs]
[./all]
type = DirichletBC
variable = temp
boundary = 'bottom top left right'
value = 300
[../]
[]
[Materials]
[./heat_material]
type = HeatConductionMaterial
temp = temp
specific_heat = 1000
thermal_conductivity = 500
[../]
[./density]
type = Density
density = 2000
[../]
[]
[Postprocessors]
[./avg_temp]
type = ElementAverageValue
variable = temp
execute_on = 'initial timestep_end'
[../]
[./avg_power]
type = ElementAverageValue
variable = power
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart'
petsc_options_value = 'hypre boomeramg 300'
line_search = 'none'
l_tol = 1e-05
nl_rel_tol = 1e-12
nl_abs_tol = 1e-9
l_max_its = 50
nl_max_its = 25
[]
[Outputs]
perf_graph = true
color = true
csv = true
exodus = true
[checkpoint]
type = Checkpoint
num_files = 2
additional_execute_on = 'FINAL' # seems to be a necessary to avoid a Checkpoint bug
[]
[]
[MultiApps]
[./bison]
type = FullSolveMultiApp
positions = '0 0 0'
input_files = 'sub_ss.i'
execute_on = 'timestep_end'
[../]
[]
[Transfers]
[./to_bison_mechanics]
type = MultiAppProjectionTransfer
to_multi_app = bison
variable = temp
source_variable = temp
execute_on = 'timestep_end'
[../]
[]
(test/tests/mesh_modifiers/mesh_extruder/gen_extrude.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 6
ny = 6
nz = 0
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[extrude]
type = MeshExtruderGenerator
input = gen
num_layers = 6
extrusion_vector = '1 0 1'
bottom_sideset = '10'
top_sideset = '20'
[]
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[bottom]
type = DirichletBC
variable = u
boundary = 10
value = 0
[]
[top]
type = DirichletBC
variable = u
boundary = 20
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out_gen
exodus = true
[]
(test/tests/fvkernels/fv_simple_diffusion/dirichlet.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[u]
[]
[v]
family = MONOMIAL
order = CONSTANT
fv = true
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[FVKernels]
[diff]
type = FVDiffusion
variable = v
coeff = coeff
[]
[]
[FVBCs]
[left]
type = FVDirichletBC
variable = v
boundary = left
value = 7
[]
[right]
type = FVDirichletBC
variable = v
boundary = right
value = 42
[]
[]
[Materials]
[diff]
type = ADGenericFunctorMaterial
prop_names = 'coeff'
prop_values = '1'
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 7
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 42
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/reactor/test/tests/meshgenerators/coarse_mesh_extra_element_id_generator/coarse_elem_extra_elem_id.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 8
ymin = 0
ymax = 8
nx = 8
ny = 8
[]
[coarse_mesh]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 8
ymin = 0
ymax = 8
nx = 3
ny = 3
subdomain_ids = '0 1 2
3 3 3
4 4 4'
[]
[add_id]
type = SubdomainExtraElementIDGenerator
input = coarse_mesh
subdomains = '0 1 2 3 4'
extra_element_id_names = 'test_id'
extra_element_ids = '4 3 2 1 0'
[]
[coarse_id]
type = CoarseMeshExtraElementIDGenerator
input = gmg
coarse_mesh = add_id
extra_element_id_name = coarse_elem_id
coarse_mesh_extra_element_id = test_id
enforce_mesh_embedding = false
[]
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[AuxVariables]
[coarse_elem_id]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[coarse_elem_id]
type = ExtraElementIDAux
variable = coarse_elem_id
extra_id_name = coarse_elem_id
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/porous_flow/test/tests/ics/fluidpropic.i)
# Test the correct calculation of fluid properties using PorousFlowFluidPropertyIC
#
# Variables:
# Pressure: 1 MPa
# Temperature: 323.15 K
#
# Fluid properties for water (reference values from NIST webbook)
# Density: 988.43 kg/m^3
# Enthalpy: 210.19 kJ/kg
# Internal energy: 2019.18 kJ/kg
[Mesh]
type = GeneratedMesh
dim = 2
[]
[Variables]
[pressure]
initial_condition = 1e6
[]
[temperature]
initial_condition = 323.15
[]
[]
[AuxVariables]
[enthalpy]
[]
[internal_energy]
[]
[density]
[]
[]
[ICs]
[enthalpy]
type = PorousFlowFluidPropertyIC
variable = enthalpy
property = enthalpy
porepressure = pressure
temperature = temperature
fp = water
[]
[internal_energy]
type = PorousFlowFluidPropertyIC
variable = internal_energy
property = internal_energy
porepressure = pressure
temperature = temperature
fp = water
[]
[density]
type = PorousFlowFluidPropertyIC
variable = density
property = density
porepressure = pressure
temperature = temperature
fp = water
[]
[]
[Modules]
[FluidProperties]
[water]
type = Water97FluidProperties
[]
[]
[]
[Kernels]
[pressure]
type = Diffusion
variable = pressure
[]
[temperature]
type = Diffusion
variable = temperature
[]
[]
[Executioner]
type = Steady
nl_abs_tol = 1e-12
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Postprocessors]
[enthalpy]
type = ElementAverageValue
variable = enthalpy
execute_on = 'initial timestep_end'
[]
[internal_energy]
type = ElementAverageValue
variable = internal_energy
execute_on = 'initial timestep_end'
[]
[density]
type = ElementAverageValue
variable = density
execute_on = 'initial timestep_end'
[]
[]
[Outputs]
csv = true
execute_on = initial
[]
(test/tests/outputs/exodus/invalid_hide_variables.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[AuxVariables]
[./aux0]
order = SECOND
family = SCALAR
[../]
[./aux1]
family = SCALAR
initial_condition = 5
[../]
[./aux2]
family = SCALAR
initial_condition = 10
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./diff_v]
type = CoefDiffusion
variable = v
coef = 2
[../]
[]
[BCs]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[./left_u]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = right
value = 3
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = left
value = 2
[../]
[]
[Postprocessors]
[./num_vars]
type = NumVars
system = 'NL'
[../]
[./num_aux]
type = NumVars
system = 'AUX'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
[./exodus]
type = Exodus
hide = 'aux27 v num_aux'
[../]
[]
[ICs]
[./aux0_IC]
variable = aux0
values = '12 13'
type = ScalarComponentIC
[../]
[]
(test/tests/fvkernels/mms/advective-outflow/advection.i)
a=1.1
[GlobalParams]
advected_interp_method = 'average'
[]
[Mesh]
[./gen_mesh]
type = GeneratedMeshGenerator
dim = 1
xmin = 0.1
xmax = 1.1
nx = 2
[../]
[]
[Variables]
[./u]
family = MONOMIAL
order = CONSTANT
fv = true
two_term_boundary_expansion = false
type = MooseVariableFVReal
[../]
[./v]
family = MONOMIAL
order = CONSTANT
fv = true
two_term_boundary_expansion = true
type = MooseVariableFVReal
[../]
[]
[FVKernels]
[./advection_u]
type = FVAdvection
variable = u
velocity = '${a} 0 0'
force_boundary_execution = true
[../]
[body_u]
type = FVBodyForce
variable = u
function = 'forcing'
[]
[./advection_v]
type = FVAdvection
variable = v
velocity = '${a} 0 0'
force_boundary_execution = true
[../]
[body_v]
type = FVBodyForce
variable = v
function = 'forcing'
[]
[]
[FVBCs]
[left_u]
type = FVFunctionDirichletBC
boundary = 'left'
function = 'exact'
variable = u
[]
[left_v]
type = FVFunctionDirichletBC
boundary = 'left'
function = 'exact'
variable = v
[]
[]
[Functions]
[exact]
type = ParsedFunction
value = 'cos(x)'
[]
[forcing]
type = ParsedFunction
value = '-${a} * sin(x)'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[./L2u]
type = ElementL2Error
variable = u
function = exact
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2v]
type = ElementL2Error
variable = v
function = exact
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(test/tests/misc/check_error/kernel_with_vector_var.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE_VEC
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/ray_tracing/test/tests/raykernels/line_source_ray_kernel/fv_simple_diffusion_line_source.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
xmax = 5
ymax = 5
[]
[]
[Variables/v]
family = MONOMIAL
order = CONSTANT
fv = true
[]
[FVKernels/diff]
type = FVDiffusion
variable = v
coeff = coeff
[]
[FVBCs]
[left]
type = FVDirichletBC
variable = v
boundary = left
value = 0
[]
[right]
type = FVDirichletBC
variable = v
boundary = right
value = 1
[]
[top_bottom]
type = FVDirichletBC
variable = v
boundary = 'top bottom'
value = 2
[]
[]
[Materials/diff]
type = ADGenericFunctorMaterial
prop_names = 'coeff'
prop_values = '1'
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
[Problem]
kernel_coverage_check = false
[]
[UserObjects/study]
type = RepeatableRayStudy
names = 'line_source_ray'
start_points = '1 1 0'
end_points = '5 2 0'
execute_on = PRE_KERNELS # must be set for line sources!
[]
[RayKernels/line_source]
type = ADLineSourceRayKernel
variable = v
value = 5
[]
(test/tests/misc/check_error/vector_kernel_with_standard_var.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = VectorDiffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/rz-x-axial-coord/pipe-flow.i)
# 2d siumulation of a water through a pipe.
mu=1e-3 # Nsm^-2
rho=997.0 # kgm^-3
Re=1000.0
pipe_length=1 # m
pipe_radius=0.1 # m
u_inlet=${fparse (mu * Re)/(2 * pipe_radius * rho)} # ms^-1
[GlobalParams]
integrate_p_by_parts = false
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${pipe_length}
ymin = 0
ymax = ${pipe_radius}
nx = 50
ny = 5
[]
[]
[Problem]
coord_type = 'RZ'
rz_coord_axis = x
[]
[Variables]
[velocity]
family = LAGRANGE_VEC
[]
[p][]
[]
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[Kernels]
[mass]
type = INSADMass
variable = p
[]
[mass_pspg]
type = INSADMassPSPG
variable = p
[]
[momentum_convection]
type = INSADMomentumAdvection
variable = velocity
[]
[momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[]
[momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
[]
[momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[]
[]
[BCs]
[inlet]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'left'
function_x = ${u_inlet}
function_y = 0
[../]
[wall]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'top'
function_x = 0
function_y = 0
[]
[axis]
type = ADVectorFunctionDirichletBC
variable = velocity
boundary = 'bottom'
set_x_comp = false
function_y = 0
[]
# pressure is not integrated by parts so we cannot remove the nullspace through a natural condition
[p_corner]
type = DirichletBC
boundary = 'right'
value = 0
variable = p
[]
[]
[Materials]
[const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '${rho} ${mu}'
[]
[ins_mat]
type = INSADTauMaterial
velocity = velocity
pressure = p
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_levels -ksp_gmres_restart'
petsc_options_value = 'asm 6 200'
nl_rel_tol = 1e-12
nl_abs_tol = 1e-12
l_max_its = 200
line_search = 'none'
[]
[Outputs]
exodus = true
[]
(tutorials/tutorial01_app_development/step09_mat_props/test/tests/kernels/darcy_pressure/darcy_pressure_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[pressure]
[]
[]
[Kernels]
[diffusion]
type = DarcyPressure
variable = pressure
[]
[]
[Materials]
[column]
type = PackedColumn
[]
[]
[BCs]
[left]
type = ADDirichletBC
variable = pressure
boundary = left
value = 0
[]
[right]
type = ADDirichletBC
variable = pressure
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/vectorpostprocessors/side_value_sampler/side_value_sampler.i)
[Mesh]
[mesh]
type = CartesianMeshGenerator
dim = 2
dx = '0.5 0.5'
dy = '1'
ix = '5 5'
iy = '10'
subdomain_id = '1 1'
[]
# Limited to 1 side to avoid inconsistencies in parallel
[internal_sideset]
type = ParsedGenerateSideset
combinatorial_geometry = 'y<0.51 & y>0.49 & x<0.11'
new_sideset_name = 'center'
input = 'mesh'
[]
# this keeps numbering continuous so tests dont fail on different ids in CSV
allow_renumbering = false
[]
[Variables]
[u]
[]
[v]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[diff_v]
type = Diffusion
variable = v
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[left_v]
type = DirichletBC
variable = v
boundary = left
value = 1
[]
[right_v]
type = DirichletBC
variable = v
boundary = right
value = 0
[]
[]
[VectorPostprocessors]
inactive = 'internal_sample'
[side_sample]
type = SideValueSampler
variable = 'u v'
boundary = top
sort_by = x
[]
[internal_sample]
type = SideValueSampler
variable = 'u v'
boundary = center
sort_by = 'id'
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
[vpp_csv]
type = CSV
[]
[]
(test/tests/outputs/error/duplicate_output_files.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
[./exodus]
type = Exodus
file_base = duplicate_output_files_out
[../]
[./exodus_two]
type = Exodus
file_base = duplicate_output_files_out
[../]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-rc.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 10
ymin = -1
ymax = 1
nx = 100
ny = 20
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = 1
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_x
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_y
function = 0
[]
[walls-u]
type = INSFVNaturalFreeSlipBC
boundary = 'top bottom'
variable = vel_x
momentum_component = 'x'
[]
[walls-v]
type = INSFVNaturalFreeSlipBC
boundary = 'top bottom'
variable = vel_y
momentum_component = 'y'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 0
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_mortar/bc_gap_heat_transfer_displaced_radiation.i)
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
[file]
type = FileMeshGenerator
file = 2blk-gap.e
[]
allow_renumbering = false
[]
[Problem]
kernel_coverage_check = false
material_coverage_check = false
[]
[Variables]
[temp]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[disp_x]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[disp_y]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[]
[Materials]
[left]
type = ADHeatConductionMaterial
block = 1
thermal_conductivity = 0.01
specific_heat = 1
[]
[right]
type = ADHeatConductionMaterial
block = 2
thermal_conductivity = 0.005
specific_heat = 1
[]
[]
[Kernels]
[hc_displaced_block]
type = ADHeatConduction
variable = temp
use_displaced_mesh = true
block = '1'
[]
[hc_undisplaced_block]
type = ADHeatConduction
variable = temp
use_displaced_mesh = false
block = '2'
[]
[disp_x]
type = Diffusion
variable = disp_x
block = '1 2'
[]
[disp_y]
type = Diffusion
variable = disp_y
block = '1 2'
[]
[]
[ThermalContact]
[thermal_contact]
type = GapHeatTransfer
variable = temp
primary = 100
secondary = 101
emissivity_primary = 1.0
emissivity_secondary = 1.0
gap_conductivity = 1.0e-12
quadrature = true
[]
[]
[BCs]
[left]
type = DirichletBC
variable = temp
boundary = 'left'
value = 100
[]
[right]
type = DirichletBC
variable = temp
boundary = 'right'
value = 0
[]
[left_disp_x]
type = DirichletBC
preset = false
variable = disp_x
boundary = 'left'
value = .1
[]
[right_disp_x]
type = DirichletBC
preset = false
variable = disp_x
boundary = 'right'
value = 0
[]
[bottom_disp_y]
type = DirichletBC
preset = false
variable = disp_y
boundary = 'bottom'
value = 0
[]
[]
[Preconditioning]
[fmp]
type = SMP
full = true
solve_type = 'NEWTON'
[]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-11
nl_abs_tol = 1.0e-10
[]
[VectorPostprocessors]
[NodalTemperature]
type = NodalValueSampler
sort_by = id
boundary = '100 101'
variable = 'temp'
[]
[]
[Outputs]
exodus = false
csv = true
[]
(test/tests/kernels/ad_coupled_convection/ad_coupled_convection.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 4
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[Kernels]
[./diff]
type = ADDiffusion
variable = u
[../]
[./convection]
type = ADCoupledConvection
variable = u
velocity_vector = v
[../]
[./diff_v]
type = ADDiffusion
variable = v
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = left
value = 0
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = right
value = 1
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = 'Newton'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
l_tol = 1e-10
nl_rel_tol = 1e-9
nl_max_its = 2
[]
[Outputs]
exodus = true
[]
(test/tests/vectorpostprocessors/elements_along_line/3d.i)
[Mesh]
type = GeneratedMesh
parallel_type = replicated # Until RayTracing.C is fixed
dim = 3
nx = 10
ny = 10
nz = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[VectorPostprocessors]
[./elems]
type = ElementsAlongLine
start = '0.05 0.05 0.05'
end = '0.05 0.05 0.405'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
csv = true
[]
(stork/test/tests/kernels/simple_diffusion/simple_diffusion.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/utils/mathutils/smootherstep.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Problem]
solve = false
[]
[Functions]
[./smootherstep_value]
type = SmootherStepTestFunction
[../]
[./exact_value]
type = ParsedFunction
value = 'u := (x - 0.2) / (0.8 - 0.2);
val := 6.0 * u^5 - 15 * u^4 + 10 * u^3;
if(x < 0.2, 0, if(x > 0.8, 1, val))'
[../]
[./smootherstep_derivative]
type = SmootherStepTestFunction
derivative = true
[../]
[./exact_derivative]
type = ParsedFunction
value = 'u := (x - 0.2) / (0.8 - 0.2);
val := 30.0 * u^4 - 60 * u^3 + 30 * u^2;
if(x < 0.2, 0, if(x > 0.8, 0, val / (0.8 - 0.2)))'
[../]
[]
[VectorPostprocessors]
[./functions]
type = LineFunctionSampler
functions = 'smootherstep_value exact_value smootherstep_derivative exact_derivative'
start_point = '0 0 0'
end_point = '1 0 0'
num_points = 10
sort_by = x
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
[]
(test/tests/relationship_managers/default_ghosting/default_ghosting.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[console]
type = Console
system_info = 'framework mesh aux nonlinear relationship execution'
[]
[]
# Show that we can enable and see that libmesh Ghosting Functors are active
[Problem]
default_ghosting = true
[]
(test/tests/misc/check_error/multiple_bad_ic_test.i)
[Mesh]
file = sq-2blk.e
uniform_refine = 1
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./u_aux]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./ic_u_1]
type = ConstantIC
variable = u
value = 42
block = '1'
[../]
[./ic_u_2]
type = ConstantIC
variable = u
value = 24
# Oops - can't have two ICs on the same block
[../]
[./ic_u_aux_1]
type = ConstantIC
variable = u_aux
value = 6.25
block = '1'
[../]
[./ic_u_aux_2]
type = ConstantIC
variable = u_aux
value = 9.99
block = '2'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
nl_rel_tol = 1e-10
[]
[Outputs]
exodus = true
[]
(test/tests/kernels/ad_2d_diffusion/2d_diffusion_test.i)
###########################################################
# This is a simple test of the Kernel System.
# It solves the Laplacian equation on a small 2x2 grid.
# The "Diffusion" kernel is used to calculate the
# residuals of the weak form of this operator.
#
# @Requirement F3.30
###########################################################
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = ADDiffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/tensor_mechanics/test/tests/action/material_output_order.i)
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
origin = '0 0 2'
direction = '0 0 1'
polar_moment_of_inertia = pmi
factor = t
[]
[Mesh]
[ring]
type = AnnularMeshGenerator
nr = 1
nt = 30
rmin = 0.95
rmax = 1
[]
[extrude]
type = MeshExtruderGenerator
input = ring
extrusion_vector = '0 0 2'
bottom_sideset = 'bottom'
top_sideset = 'top'
num_layers = 5
[]
[]
[AuxVariables]
[alpha_var]
[]
[shear_stress_var]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[alpha]
type = RotationAngle
variable = alpha_var
[]
[shear_stress]
type = ParsedAux
variable = shear_stress_var
args = 'stress_yz stress_xz'
function = 'sqrt(stress_yz^2 + stress_xz^2)'
[]
[]
[BCs]
# fix bottom
[fix_x]
type = DirichletBC
boundary = bottom
variable = disp_x
value = 0
[]
[fix_y]
type = DirichletBC
boundary = bottom
variable = disp_y
value = 0
[]
[fix_z]
type = DirichletBC
boundary = bottom
variable = disp_z
value = 0
[]
# twist top
[twist_x]
type = Torque
boundary = top
variable = disp_x
[]
[twist_y]
type = Torque
boundary = top
variable = disp_y
[]
[twist_z]
type = Torque
boundary = top
variable = disp_z
[]
[]
[Modules/TensorMechanics/Master]
[all]
add_variables = true
strain = SMALL
generate_output = 'vonmises_stress stress_yz stress_xz'
[]
[]
[Postprocessors]
[pmi]
type = PolarMomentOfInertia
boundary = top
# execute_on = 'INITIAL NONLINEAR'
execute_on = 'INITIAL'
[]
[alpha]
type = SideAverageValue
variable = alpha_var
boundary = top
[]
[shear_stress]
type = ElementAverageValue
variable = shear_stress_var
[]
[]
[Materials]
[stress]
type = ComputeLinearElasticStress
[]
[elastic]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 0.3
shear_modulus = 100
[]
[]
[Executioner]
# type = Steady
type = Transient
num_steps = 1
solve_type = PJFNK
petsc_options_iname = '-pctype'
petsc_options_value = 'lu'
nl_max_its = 150
[]
[Outputs]
exodus = true
print_linear_residuals = false
perf_graph = true
[]
(test/tests/vectorpostprocessors/histogram_vector_postprocessor/histogram_vector_postprocessor.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[VectorPostprocessors]
[./constant]
type = ConstantVectorPostprocessor
value = '9 1 1 2 3 2 4 6 3 6 9'
[../]
[./histo]
type = HistogramVectorPostprocessor
vpp = constant
num_bins = 4
[../]
[]
[Outputs]
csv = true
[]
(modules/tensor_mechanics/test/tests/gravity/gravity_test.i)
#
# Gravity Test
#
# This test is designed to apply a gravity body force.
#
# The mesh is composed of one block with a single element.
# The bottom is fixed in all three directions. Poisson's ratio
# is zero and the density is 20/9.81
# which makes it trivial to check displacements.
#
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
type = GeneratedMesh
dim = 3
[]
[Modules/TensorMechanics/Master]
[all]
add_variables = true
[]
[]
[Kernels]
[gravity_y]
type = Gravity
variable = disp_y
value = -9.81
[]
[]
[BCs]
[no_x]
type = DirichletBC
variable = disp_x
boundary = bottom
value = 0.0
[]
[no_y]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[]
[no_z]
type = DirichletBC
variable = disp_z
boundary = bottom
value = 0.0
[]
[]
[Materials]
[Elasticity_tensor]
type = ComputeElasticityTensor
fill_method = symmetric_isotropic
C_ijkl = '0 0.5e6'
[]
[stress]
type = ComputeLinearElasticStress
[]
[density]
type = GenericConstantMaterial
prop_names = density
prop_values = 2.0387
[]
[]
[Executioner]
type = Steady
nl_abs_tol = 1e-10
l_max_its = 20
[]
[Outputs]
[out]
type = Exodus
elemental_as_nodal = true
[]
[]
(test/tests/bcs/ad_bcs/ad_bc.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = ADDiffusion
variable = u
[../]
[]
[BCs]
[./left]
type = ADFunctionDirichletBC
variable = u
boundary = left
function = '1'
[../]
[./right]
type = ADRobinBC
variable = u
boundary = right
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/homogenization/heatConduction2D.i)
#
# Homogenization of thermal conductivity according to
# Homogenization of Temperature-Dependent Thermal Conductivity in Composite
# Materials, Journal of Thermophysics and Heat Transfer, Vol. 15, No. 1,
# January-March 2001.
#
# The problem solved here is a simple square with two blocks. The square is
# divided vertically between the blocks. One block has a thermal conductivity
# of 10. The other block's thermal conductivity is 100.
#
# The analytic solution for the homogenized thermal conductivity in the
# horizontal direction is found by summing the thermal resistance, recognizing
# that the blocks are in series:
#
# R = L/A/k = R1 + R2 = L1/A1/k1 + L2/A2/k2 = .5/1/10 + .5/1/100
# Since L = A = 1, k_xx = 18.1818.
#
# The analytic solution for the homogenized thermal conductivity in the vertical
# direction is found by summing reciprocals of resistance, recognizing that
# the blocks are in parallel:
#
# 1/R = k*A/L = 1/R1 + 1/R2 = 10*.5/1 + 100*.5/1
# Since L = A = 1, k_yy = 55.0.
#
[Mesh]
file = heatConduction2D.e
[] # Mesh
[Variables]
[./temp_x]
order = FIRST
family = LAGRANGE
initial_condition = 100
[../]
[./temp_y]
order = FIRST
family = LAGRANGE
initial_condition = 100
[../]
[] # Variables
[Kernels]
[./heat_x]
type = HeatConduction
variable = temp_x
[../]
[./heat_y]
type = HeatConduction
variable = temp_y
[../]
[./heat_rhs_x]
type = HomogenizedHeatConduction
variable = temp_x
component = 0
[../]
[./heat_rhs_y]
type = HomogenizedHeatConduction
variable = temp_y
component = 1
[../]
[] # Kernels
[BCs]
[./Periodic]
[./left_right]
primary = 10
secondary = 20
translation = '1 0 0'
[../]
[./bottom_top]
primary = 30
secondary = 40
translation = '0 1 0'
[../]
[../]
[./fix_center_x]
type = DirichletBC
variable = temp_x
value = 100
boundary = 1
[../]
[./fix_center_y]
type = DirichletBC
variable = temp_y
value = 100
boundary = 1
[../]
[] # BCs
[Materials]
[./heat1]
type = HeatConductionMaterial
block = 1
specific_heat = 0.116
thermal_conductivity = 10
[../]
[./heat2]
type = HeatConductionMaterial
block = 2
specific_heat = 0.116
thermal_conductivity = 100
[../]
[] # Materials
[Executioner]
type = Steady
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -ksp_gmres_restart'
petsc_options_value = 'lu 101'
line_search = 'none'
nl_abs_tol = 1e-11
nl_rel_tol = 1e-10
l_max_its = 20
[] # Executioner
[Outputs]
exodus = true
[] # Outputs
[Postprocessors]
[./k_xx]
type = HomogenizedThermalConductivity
variable = temp_x
temp_x = temp_x
temp_y = temp_y
component = 0
execute_on = 'initial timestep_end'
[../]
[./k_yy]
type = HomogenizedThermalConductivity
variable = temp_y
temp_x = temp_x
temp_y = temp_y
component = 1
execute_on = 'initial timestep_end'
[../]
[]
(test/tests/multiapps/command_line/master.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
[]
[MultiApps]
[sub]
type = FullSolveMultiApp
positions = '0 0 0
1 1 1'
input_files = 'sub.i'
cli_args = 'Mesh/nx=10 Mesh/nx=100'
[]
[]
(test/tests/variables/fe_monomial_const/monomial-const-3d.i)
[Mesh]
type = GeneratedMesh
dim = 3
xmin = -1
xmax = 1
ymin = -1
ymax = 1
zmin = -1
zmax = 1
nx = 21
ny = 21
nz = 21
elem_type = HEX8
[]
[Functions]
[./bc_fn]
type=ParsedFunction
value=0
[../]
[./bc_fnt]
type = ParsedFunction
value = 0
[../]
[./bc_fnb]
type = ParsedFunction
value = 0
[../]
[./bc_fnl]
type = ParsedFunction
value = 0
[../]
[./bc_fnr]
type = ParsedFunction
value = 0
[../]
[./forcing_fn]
# type = ParsedFunction
# value = 0
type = MTPiecewiseConst3D
[../]
[./solution]
type = MTPiecewiseConst3D
[../]
[]
[Variables]
[./u]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
active = 'diff forcing reaction'
[./diff]
type = Diffusion
variable = u
[../]
[./reaction]
type = Reaction
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
# Note: MOOSE's DirichletBCs do not work properly with shape functions that do not
# have DOFs at the element edges. This test works because the solution
# has been designed to be zero at the boundary which is satisfied by the IC
# Ticket #1352
active = ''
[./bc_all]
type=FunctionDirichletBC
variable = u
boundary = 'top bottom left right'
function = bc_fn
[../]
[./bc_top]
type = FunctionNeumannBC
variable = u
boundary = 'top'
function = bc_fnt
[../]
[./bc_bottom]
type = FunctionNeumannBC
variable = u
boundary = 'bottom'
function = bc_fnb
[../]
[./bc_left]
type = FunctionNeumannBC
variable = u
boundary = 'left'
function = bc_fnl
[../]
[./bc_right]
type = FunctionNeumannBC
variable = u
boundary = 'right'
function = bc_fnr
[../]
[]
[Postprocessors]
[./dofs]
type = NumDOFs
[../]
[./h]
type = AverageElementSize
[../]
[./L2error]
type = ElementL2Error
variable = u
function = solution
[../]
[./H1error]
type = ElementH1Error
variable = u
function = solution
[../]
[./H1Semierror]
type = ElementH1SemiError
variable = u
function = solution
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
nl_rel_tol = 1.e-9
[./Adaptivity]
[../]
[]
[Outputs]
execute_on = 'timestep_end'
csv = true
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[]
(modules/phase_field/test/tests/KKS_system/bug.i)
#
# This test validates the phase concentration calculation for the KKS system
#
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
nz = 0
xmin = 0
xmax = 1
ymin = 0
ymax = 1
zmin = 0
zmax = 0
elem_type = QUAD4
[]
# We set u
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0.1
[../]
[./right]
type = DirichletBC
variable = u
boundary = 'right'
value = 0.9
[../]
[]
[Variables]
# primary variable
[./u]
order = FIRST
family = LAGRANGE
[../]
# secondary variable
[./v]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./udiff]
type = Diffusion
variable = u
[../]
[./valgebra]
type = AlgebraDebug
variable = v
v = u
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
#solve_type = 'NEWTON'
[]
#[Preconditioning]
# [./mydebug]
# type = FDP
# full = true
# [../]
#[]
[Outputs]
execute_on = 'timestep_end'
file_base = bug
exodus = true
[]
(modules/phase_field/test/tests/KKS_system/kks_phase_concentration.i)
#
# This test validates the phase concentration calculation for the KKS system
#
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
nz = 0
xmin = 0
xmax = 1
ymin = 0
ymax = 1
zmin = 0
zmax = 0
elem_type = QUAD4
[]
# We set c and eta...
[BCs]
# (and ca for debugging purposes)
[./left]
type = DirichletBC
variable = c
boundary = 'left'
value = 0.1
[../]
[./right]
type = DirichletBC
variable = c
boundary = 'right'
value = 0.9
[../]
[./top]
type = DirichletBC
variable = eta
boundary = 'top'
value = 0.1
[../]
[./bottom]
type = DirichletBC
variable = eta
boundary = 'bottom'
value = 0.9
[../]
[]
[Variables]
# concentration
[./c]
order = FIRST
family = LAGRANGE
initial_condition = 0.5
[../]
# order parameter
[./eta]
order = FIRST
family = LAGRANGE
initial_condition = 0.1
[../]
# phase concentration a
[./ca]
order = FIRST
family = LAGRANGE
initial_condition = 0.2
[../]
# phase concentration b
[./cb]
order = FIRST
family = LAGRANGE
initial_condition = 0.3
[../]
[]
[Materials]
# simple toy free energy
[./fa]
type = DerivativeParsedMaterial
f_name = Fa
args = 'ca'
function = 'ca^2'
[../]
[./fb]
type = DerivativeParsedMaterial
f_name = Fb
args = 'cb'
function = '(1-cb)^2'
[../]
# h(eta)
[./h_eta]
type = SwitchingFunctionMaterial
h_order = HIGH
eta = eta
outputs = exodus
[../]
[]
[Kernels]
active = 'cdiff etadiff phaseconcentration chempot'
##active = 'cbdiff cdiff etadiff chempot'
#active = 'cadiff cdiff etadiff phaseconcentration'
##active = 'cadiff cbdiff cdiff etadiff'
[./cadiff]
type = Diffusion
variable = ca
[../]
[./cbdiff]
type = Diffusion
variable = cb
[../]
[./cdiff]
type = Diffusion
variable = c
[../]
[./etadiff]
type = Diffusion
variable = eta
[../]
# ...and solve for ca and cb
[./phaseconcentration]
type = KKSPhaseConcentration
ca = ca
variable = cb
c = c
eta = eta
[../]
[./chempot]
type = KKSPhaseChemicalPotential
variable = ca
cb = cb
fa_name = Fa
fb_namee = Fb
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
#solve_type = 'NEWTON'
petsc_options_iname = '-pctype -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = ' asm lu nonzero'
[]
[Preconditioning]
active = 'full'
#active = 'mydebug'
#active = ''
[./full]
type = SMP
full = true
[../]
[./mydebug]
type = FDP
full = true
[../]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = kks_phase_concentration
exodus = true
[]
(test/tests/outputs/subdir_output/subdir_output.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
file_base = sub1/sub2/subdir_output_out
exodus = true
[]
(test/tests/fvkernels/fv_simple_diffusion/neumann.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[u]
[]
[v]
family = MONOMIAL
order = CONSTANT
fv = true
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[FVKernels]
[diff]
type = FVDiffusion
variable = v
coeff = coeff
[]
[]
[FVBCs]
[left]
type = FVNeumannBC
variable = v
boundary = left
value = 5
[]
[right]
type = FVDirichletBC
variable = v
boundary = right
value = 42
[]
[]
[Materials]
[diff]
type = ADGenericFunctorMaterial
prop_names = 'coeff'
prop_values = '1'
[]
[]
[BCs]
[left]
type = NeumannBC
variable = u
boundary = left
value = 5
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 42
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/energy_source/steady-var-action.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
nx = 16
ny = 16
[]
[]
[AuxVariables]
[u]
initial_condition = 1
[]
[]
[Modules]
[IncompressibleNavierStokes]
equation_type = steady-state
velocity_boundary = 'bottom right top left'
velocity_function = '0 0 0 0 lid_function 0 0 0'
initial_velocity = '1e-15 1e-15 0'
add_standard_velocity_variables_for_ad = false
pressure_pinned_node = 0
density_name = rho
dynamic_viscosity_name = mu
use_ad = true
laplace = true
family = LAGRANGE
order = FIRST
add_temperature_equation = true
fixed_temperature_boundary = 'bottom top'
temperature_function = '1 0'
has_heat_source = true
heat_source_var = u
supg = true
pspg = true
[]
[]
[Materials]
[const]
type = ADGenericConstantMaterial
prop_names = 'rho mu cp k'
prop_values = '1 1 1 .01'
[]
[]
[Functions]
[lid_function]
# We pick a function that is exactly represented in the velocity
# space so that the Dirichlet conditions are the same regardless
# of the mesh spacing.
type = ParsedFunction
value = '4*x*(1-x)'
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_levels -ksp_gmres_restart'
petsc_options_value = 'asm 6 200'
line_search = 'none'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
[out]
type = Exodus
hide = 'u'
[]
[]
(modules/tensor_mechanics/test/tests/ad_linear_elasticity/thermal_expansion.i)
# This input file is designed to test the RankTwoAux and RankFourAux
# auxkernels, which report values out of the Tensors used in materials
# properties.
# Materials properties into AuxVariables - these are elemental variables, not nodal variables.
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
xmax = 2
ymax = 2
[]
[Modules/TensorMechanics/Master/All]
strain = SMALL
eigenstrain_names = eigenstrain
add_variables = true
generate_output = 'stress_xx stress_yy stress_xy'
use_automatic_differentiation = true
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0
[../]
[./stress]
type = ADComputeLinearElasticStress
[../]
[./eigenstrain]
type = ADComputeEigenstrain
eigen_base = '1e-4'
eigenstrain_name = eigenstrain
[../]
[]
[BCs]
[./bottom_y]
type = DirichletBC
variable = disp_y
boundary = 'bottom'
value = 0
[../]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = 'left'
value = 0
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
nl_rel_tol = 1e-14
[]
[Outputs]
exodus = true
[]
(python/peacock/tests/input_tab/InputTree/gold/simple_diffusion.i)
[Mesh]
[generate]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[]
[]
[Executioner]
# Preconditioned JFNK (default)
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/coupling_nonexistent_field.i)
[Mesh]
type = GeneratedMesh
dim = 2
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./coupled]
type = CoupledForce
variable = u
# 'a' does not exist -> error
v = a
[../]
[]
[Executioner]
type = Steady
[]
(modules/tensor_mechanics/test/tests/ad_linear_elasticity/applied_strain.i)
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
xmax = 2
ymax = 2
[]
[Modules/TensorMechanics/Master/All]
strain = SMALL
eigenstrain_names = eigenstrain
add_variables = true
generate_output = 'strain_xx strain_yy strain_xy'
use_automatic_differentiation = true
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0
[../]
[./stress]
type = ADComputeLinearElasticStress
[../]
[./eigenstrain]
type = ADComputeEigenstrain
eigen_base = '0.1 0.05 0 0 0 0.01'
prefactor = -1
eigenstrain_name = eigenstrain
[../]
[]
[BCs]
[./bottom_y]
type = ADDirichletBC
variable = disp_y
boundary = 'bottom'
value = 0
[../]
[./left_x]
type = ADDirichletBC
variable = disp_x
boundary = 'left'
value = 0
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(test/tests/functions/constant_function/constant_function_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 4
ny = 4
elem_type = QUAD4
[]
[Functions]
[./bc_fn]
type = ParsedFunction
value = 'x*x+y*y'
[../]
[./icfn]
type = ConstantFunction
value = 1
[../]
[./ffn]
type = ConstantFunction
value = -4
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = icfn
[../]
[../]
[]
[Kernels]
# Coupling of nonlinear to Aux
[./diff]
type = Diffusion
variable = u
[../]
[./force]
type = BodyForce
variable = u
function = ffn
[../]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
boundary = '0 1 2 3'
function = bc_fn
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/scalar_adr/supg/advection_error_testing.i)
velocity=1
[GlobalParams]
u = ${velocity}
pressure = 0
tau_type = mod
[]
[Mesh]
type = GeneratedMesh
dim = 1
nx = 4
xmax = 1
elem_type = EDGE2
[]
[Variables]
[./c]
family = LAGRANGE
order = FIRST
[../]
[]
[Kernels]
[./adv]
type = Advection
variable = c
forcing_func = 'ffn'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = c
boundary = left
value = 0
[../]
[]
[Materials]
[./mat]
type = GenericConstantMaterial
prop_names = 'mu rho'
prop_values = '0 1'
[../]
[]
[Functions]
[./ffn]
type = ParsedFunction
value = '1-x^2'
[../]
[./c_func]
type = ParsedFunction
value = 'x-x^3/3'
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
[]
[Outputs]
[./exodus]
type = Exodus
[../]
[./csv]
type = CSV
[../]
[]
[Postprocessors]
[./L2c]
type = ElementL2Error
variable = c
function = c_func
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2cx]
type = ElementL2Error
variable = cx
function = ffn
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[]
[AuxVariables]
[./cx]
family = MONOMIAL
order = FIRST
[../]
[]
[AuxKernels]
[./cx]
type = VariableGradientComponent
component = x
variable = cx
gradient_variable = c
[../]
[]
(test/tests/userobjects/layered_integral/layered_integral_fv_test.i)
###########################################################
# This is a test of the UserObject System. The
# LayeredIntegral UserObject executes independently during
# the solve to compute a user-defined value. In this case
# an integral value in discrete layers along a vector
# in the domain. (Type: ElementalUserObject)
#
# @Requirement F6.40
###########################################################
[Mesh]
type = GeneratedMesh
dim = 2
nx = 6
ny = 6
nz = 6
[]
[Variables]
[./u]
order = CONSTANT
family = MONOMIAL
fv = true
[../]
[]
[AuxVariables]
[./layered_integral]
order = CONSTANT
family = MONOMIAL
[../]
[]
[FVKernels]
[./diff]
type = FVDiffusion
variable = u
coeff = 1
[../]
[]
[AuxKernels]
[./liaux]
type = SpatialUserObjectAux
variable = layered_integral
execute_on = timestep_end
user_object = layered_integral
[../]
[]
[FVBCs]
[./bottom]
type = FVDirichletBC
variable = u
boundary = bottom
value = 0
[../]
[./top]
type = FVDirichletBC
variable = u
boundary = top
value = 1
[../]
[]
[UserObjects]
[./layered_integral]
type = LayeredIntegral
direction = y
num_layers = 3
variable = u
execute_on = linear
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
file_base = fv_out
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/pressure_channel/open_bc_pressure_BC_action.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 3.0
ymin = 0
ymax = 1.0
nx = 30
ny = 10
elem_type = QUAD9
[]
[Modules]
[IncompressibleNavierStokes]
equation_type = steady-state
velocity_boundary = 'bottom top left'
velocity_function = '0 0 0 0 NA 0'
pressure_boundary = 'left right'
pressure_function = '1 0'
density_name = rho
dynamic_viscosity_name = mu
integrate_p_by_parts = false
order = SECOND
[]
[]
[Materials]
[const]
type = GenericConstantMaterial
block = 0
prop_names = 'rho mu'
prop_values = '1 1'
[]
[]
[Preconditioning]
[SMP_PJFNK]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-ksp_gmres_restart -pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = '300 bjacobi ilu 4'
line_search = none
nl_rel_tol = 1e-12
nl_max_its = 6
l_tol = 1e-6
l_max_its = 300
[]
[Outputs]
file_base = open_bc_out_pressure_BC
exodus = true
[]
(modules/chemical_reactions/test/tests/jacobian/coupled_diffreact.i)
# Test the Jacobian terms for the CoupledDiffusionReactionSub Kernel
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
[./a]
order = FIRST
family = LAGRANGE
[../]
[./b]
order = FIRST
family = LAGRANGE
[../]
[./pressure]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./pressure]
type = RandomIC
variable = pressure
min = 1
max = 5
[../]
[./a]
type = RandomIC
variable = a
max = 1
min = 0
[../]
[./b]
type = RandomIC
variable = b
max = 1
min = 0
[../]
[]
[Kernels]
[./diff]
type = DarcyFluxPressure
variable = pressure
[../]
[./diff_b]
type = Diffusion
variable = b
[../]
[./a1diff]
type = CoupledDiffusionReactionSub
variable = a
v = b
log_k = 2
weight = 2
sto_v = 1.5
sto_u = 2
[../]
[]
[Materials]
[./porous]
type = GenericConstantMaterial
prop_names = 'diffusivity conductivity porosity'
prop_values = '1e-4 1e-4 0.2'
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
perf_graph = true
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
(test/tests/materials/ad_material/ad_material.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 4
[]
[Variables]
[./u]
initial_condition = 1
[../]
[]
[Kernels]
[./diff]
type = ADMatDiffusionTest
variable = u
prop_to_use = 'AdAd'
ad_mat_prop = ad_diffusivity
regular_mat_prop = regular_diffusivity
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
preset = false
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
preset = false
boundary = right
value = 1
[../]
[]
[Materials]
[./ad_coupled_mat]
type = ADCoupledMaterial
coupled_var = u
ad_mat_prop = ad_diffusivity
regular_mat_prop = regular_diffusivity
[../]
[]
[Executioner]
type = Steady
solve_type = 'Newton'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
l_tol = 1e-10
nl_rel_tol = 1e-9
[]
[Outputs]
exodus = true
[]
(test/tests/postprocessors/variable_inner_product/variable_inner_product.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
xmin = -1
xmax = 1
ymin = 0
ymax = 1
elem_type = QUAD9
[]
[AuxVariables]
[./f]
order = SECOND
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = leg2
[../]
[../]
[./g]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = leg1
[../]
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[Functions]
[./leg1]
type = ParsedFunction
value = 'x'
[../]
[./leg2]
type = ParsedFunction
value = '0.5*(3.0*x*x-1.0)'
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[./Quadrature]
order = fourth
[]
[]
[Postprocessors]
[./f_dot_g]
type = VariableInnerProduct
variable = f
second_variable = g
[../]
[./f_dot_f]
type = VariableInnerProduct
variable = f
second_variable = f
[../]
[./norm_f]
type = ElementL2Norm
variable = f
[../]
[]
[Outputs]
file_base = variable_inner_product
csv = true
[]
(test/tests/mortar/continuity-3d-non-conforming/continuity_sphere_hex8.i)
[Mesh]
second_order = false
[file]
type = FileMeshGenerator
file = spheres_hex8.e
[]
[secondary]
input = file
type = LowerDBlockFromSidesetGenerator
new_block_id = 11
new_block_name = "secondary"
sidesets = '101'
[]
[primary]
input = secondary
type = LowerDBlockFromSidesetGenerator
new_block_id = 12
new_block_name = "primary"
sidesets = '102'
[]
[]
[Problem]
kernel_coverage_check = false
[]
[Variables]
[T]
block = '1 2'
[]
[lambda]
block = 'secondary'
[]
[]
[BCs]
[neumann]
type = FunctionGradientNeumannBC
exact_solution = exact_soln_primal
variable = T
boundary = '1 2'
[]
[]
[Kernels]
[conduction]
type = Diffusion
variable = T
block = '1 2'
[]
[sink]
type = Reaction
variable = T
block = '1 2'
[]
[forcing_function]
type = BodyForce
variable = T
function = forcing_function
block = '1 2'
[]
[]
[Functions]
[forcing_function]
type = ParsedFunction
value = 'x^2 + y^2 + z^2 - 6'
[]
[exact_soln_primal]
type = ParsedFunction
value = 'x^2 + y^2 + z^2'
[]
[exact_soln_lambda]
type = ParsedFunction
value = '4'
[]
[]
[Debug]
show_var_residual_norms = 1
[]
[Constraints]
[mortar]
type = EqualValueConstraint
primary_boundary = 2
secondary_boundary = 1
primary_subdomain = '12'
secondary_subdomain = '11'
variable = lambda
secondary_variable = T
correct_edge_dropping = true
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
solve_type = NEWTON
type = Steady
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_shift_type '
'-pc_factor_shift_amount'
petsc_options_value = 'lu basic NONZERO 1e-15'
[]
[Outputs]
exodus = true
[]
[Postprocessors]
[L2lambda]
type = ElementL2Error
variable = lambda
function = exact_soln_lambda
execute_on = 'timestep_end'
block = 'secondary'
[]
[L2u]
type = ElementL2Error
variable = T
function = exact_soln_primal
execute_on = 'timestep_end'
block = '1 2'
[]
[h]
type = AverageElementSize
block = '1 2'
[]
[]
(test/tests/postprocessors/postprocessor_comparison/postprocessor_comparison.i)
# This tests the PostprocessorComparison post-processor, which compares two
# post-processors.
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
xmin = 0
xmax = 1
[]
[Postprocessors]
[./pp_to_compare]
type = LinearCombinationPostprocessor
pp_names = ''
pp_coefs = ''
b = 1
[../]
[./pp_comparison]
type = PostprocessorComparison
value_a = pp_to_compare
value_b = 2
comparison_type = greater_than
execute_on = 'initial'
[../]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
file_base = greater_than
csv = true
show = 'pp_comparison'
execute_on = 'initial'
[]
(test/tests/bcs/vectorpostprocessor/vectorpostprocessor.i)
[Mesh]
type = GeneratedMesh
nx = 10
ny = 10
xmax = 1
ymax = 1
dim = 2
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[Kernels]
[./conv]
type = ConservativeAdvection
variable = u
velocity = '0 1 0'
[../]
[./diff]
type = Diffusion
variable = u
[../]
[./src]
type = BodyForce
variable = u
function = ffn
[../]
[./diffv]
type = Diffusion
variable = v
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = bottom
value = 2
[../]
[./right]
type = ChannelGradientBC
variable = u
boundary = right
channel_gradient_pps = channel_gradient
axis = y
h_name = h
[../]
[./top]
type = OutflowBC
variable = u
boundary = top
velocity = '0 1 0'
[../]
[./leftv]
type = DirichletBC
variable = v
boundary = left
value = 0
[../]
[./rightv]
type = DirichletBC
variable = v
boundary = right
value = 1
[../]
[]
[Materials]
[./mat]
type = GenericConstantMaterial
prop_names = 'h'
#Nu = 4
#k = 1
#half_channel_length = 0.5
#h=Nu*k/half_channel_length
prop_values = '8'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
[VectorPostprocessors]
[./lv1]
num_points = 30
start_point = '0 0 0'
end_point = '0 1 0'
sort_by = 'y'
variable = u
type = LineValueSampler
execute_on = 'timestep_begin nonlinear timestep_end linear'
[../]
[./lv2]
num_points = 30
start_point = '1 0 0'
end_point = '1 1 0'
sort_by = 'y'
variable = v
type = LineValueSampler
execute_on = 'timestep_begin nonlinear timestep_end linear'
[../]
[./channel_gradient]
lv1 = lv1
lv2 = lv2
var1 = u
var2 = v
axis = y
type = ChannelGradientVectorPostprocessor
execute_on = 'timestep_begin nonlinear timestep_end linear'
[../]
[]
[Functions]
[./ffn]
type = ParsedFunction
value = '1'
[../]
[]
(test/tests/scaling/off-diag-scaling/test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 4
elem_type = quad9
[]
[Problem]
error_on_jacobian_nonzero_reallocation = true
[]
[Variables]
[./u]
[../]
[./v]
[../]
[./w]
order = SECOND
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[./diff_w]
type = Diffusion
variable = w
[../]
[./ad_coupled_value]
type = ADCoupledValueTest
variable = u
v = v
[../]
[./ad_coupled_value_w]
type = ADCoupledValueTest
variable = u
v = w
[../]
[./ad_coupled_value_x]
type = ADCoupledValueTest
variable = u
# v = 2.0 (Using the default value)
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = left
value = 0
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = right
value = 1
[../]
[./left_w]
type = DirichletBC
variable = w
boundary = left
value = 0
[../]
[./right_w]
type = DirichletBC
variable = w
boundary = right
value = 1
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = 'Newton'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
automatic_scaling = true
verbose = true
[]
[Outputs]
exodus = true
[]
(test/tests/coord_type/coord_type_rz.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Problem]
type = FEProblem
coord_type = RZ
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/quadrature/order/order5.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
nz = 0
elem_type = QUAD4
[]
[Postprocessors]
[./numsideqps]
type = NumSideQPs
boundary = 0
[../]
[./numelemqps]
type = NumElemQPs
block = 0
[../]
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
[./Quadrature]
order = fifth
[]
[]
[Outputs]
execute_on = 'timestep_end'
exodus = false
csv = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/2d-average.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='average'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 2
ymin = -1
ymax = 1
nx = 2
ny = 2
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
two_term_boundary_expansion = false
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
two_term_boundary_expansion = false
[]
[pressure]
type = INSFVPressureVariable
two_term_boundary_expansion = false
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[u_forcing]
type = INSFVBodyForce
variable = u
functor = forcing_u
momentum_component = 'x'
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[v_forcing]
type = INSFVBodyForce
variable = v
functor = forcing_v
momentum_component = 'y'
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = 'exact_u'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = 'exact_v'
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = u
function = 'exact_u'
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = v
function = 'exact_v'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 'exact_p'
[]
[]
[Functions]
[exact_u]
type = ParsedFunction
value = 'sin((1/2)*y*pi)*cos((1/2)*x*pi)'
[]
[exact_rhou]
type = ParsedFunction
value = 'rho*sin((1/2)*y*pi)*cos((1/2)*x*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_u]
type = ADParsedFunction
value = '(1/2)*pi^2*mu*sin((1/2)*y*pi)*cos((1/2)*x*pi) - 1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi) + (1/2)*pi*rho*sin((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)^2 - pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi) - 1/4*pi*sin((1/4)*x*pi)*sin((3/2)*y*pi)'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_v]
type = ParsedFunction
value = 'sin((1/4)*x*pi)*cos((1/2)*y*pi)'
[]
[exact_rhov]
type = ParsedFunction
value = 'rho*sin((1/4)*x*pi)*cos((1/2)*y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_v]
type = ADParsedFunction
value = '(5/16)*pi^2*mu*sin((1/4)*x*pi)*cos((1/2)*y*pi) - pi*rho*sin((1/4)*x*pi)^2*sin((1/2)*y*pi)*cos((1/2)*y*pi) - 1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*y*pi) + (1/4)*pi*rho*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi) + (3/2)*pi*cos((1/4)*x*pi)*cos((3/2)*y*pi)'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_p]
type = ParsedFunction
value = 'sin((3/2)*y*pi)*cos((1/4)*x*pi)'
[]
[forcing_p]
type = ParsedFunction
value = '-1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi) - 1/2*pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[./L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2v]
type = ElementL2Error
variable = v
function = exact_v
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2p]
variable = pressure
function = exact_p
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[]
(test/tests/interfacekernels/1d_interface/single_variable_coupled_flux.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 10
xmax = 2
[]
[./subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '1.0 0 0'
block_id = 1
top_right = '2.0 1.0 0'
[../]
[./interface]
type = SideSetsBetweenSubdomainsGenerator
input = subdomain1
primary_block = '0'
paired_block = '1'
new_boundary = 'primary0_interface'
[../]
[./interface_again]
type = SideSetsBetweenSubdomainsGenerator
input = interface
primary_block = '1'
paired_block = '0'
new_boundary = 'primary1_interface'
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff0]
type = CoeffParamDiffusion
variable = u
D = 4
block = 0
[../]
[./diff1]
type = CoeffParamDiffusion
variable = u
D = 2
block = 1
[../]
[]
[InterfaceKernels]
[./interface]
type = InterfaceDiffusion
variable = u
neighbor_var = u
boundary = primary0_interface
D = 4
D_neighbor = 2
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 'left'
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = 'right'
value = 0
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
print_linear_residuals = true
[]
[Debug]
show_var_residual_norms = true
[]
(test/tests/interfacekernels/2d_interface/vector_2d.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 2
xmax = 2
ny = 2
ymax = 2
elem_type = QUAD9
[]
[./subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '0 0 0'
top_right = '1 1 0'
block_id = 1
[../]
[./break_boundary]
type = BreakBoundaryOnSubdomainGenerator
input = subdomain1
[../]
[./interface]
type = SideSetsBetweenSubdomainsGenerator
input = break_boundary
primary_block = '0'
paired_block = '1'
new_boundary = 'primary0_interface'
[../]
[]
[Variables]
[./u]
order = FIRST
family = NEDELEC_ONE
block = 0
[../]
[./v]
order = FIRST
family = NEDELEC_ONE
block = 1
[../]
[]
[Kernels]
[./curl_u_plus_u]
type = VectorFEWave
variable = u
x_forcing_func = 1
y_forcing_func = 1
z_forcing_func = 1
block = 0
[../]
[./curl_v_plus_v]
type = VectorFEWave
variable = v
block = 1
[../]
[]
[InterfaceKernels]
[./parallel]
type = VectorPenaltyInterfaceDiffusion
variable = u
neighbor_var = v
boundary = primary0_interface
penalty = 1e6
[../]
[]
[BCs]
# Natural condition of VectorFEWave weak form is curl(u) = 0, curl(v) = 0
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
[]
[Outputs]
exodus = true
print_linear_residuals = true
[]
(test/tests/preconditioners/smp/smp_single_adapt_test.i)
#
# This is not very strong test since the problem being solved is linear, so the difference between
# full Jacobian and block diagonal preconditioner is not that big
#
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 5
ny = 5
elem_type = QUAD4
[]
[Functions]
[./exact_v]
type = ParsedFunction
value = sin(pi*x)*sin(pi*y)
[../]
[./force_fn_v]
type = ParsedFunction
value = 2*pi*pi*sin(pi*x)*sin(pi*y)
[../]
[]
[Variables]
active = 'u v'
[./u]
order = FIRST
family = LAGRANGE
[../]
[./v]
order = FIRST
family = LAGRANGE
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
off_diag_row = 'u'
off_diag_column = 'v'
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./conv_u]
type = CoupledForce
variable = u
v = v
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[./ffn_v]
type = BodyForce
variable = v
function = force_fn_v
[../]
[]
[BCs]
[./left_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[./all_v]
type = FunctionDirichletBC
variable = v
boundary = '0 1 2 3'
function = exact_v
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[./Adaptivity]
steps = 3
coarsen_fraction = 0.1
refine_fraction = 0.2
max_h_level = 5
[../]
[]
[Outputs]
exodus = true
print_mesh_changed_info = true
[]
(test/tests/actions/meta_action/meta_action_test.i)
###########################################################
# This is a test of the Action System. An Action is created
# to build other objects pro grammatically. Two blocks in
# the input file have been commented out to demonstrate
# usage.
#
# @Requirement F1.50
###########################################################
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
uniform_refine = 4
[]
# This is our new custom Convection Diffusion "Meta" block
# that adds multiple kernels into our simulation
#
# Convection and Diffusion kernels on the first variable
# Diffusion kernel on the second variable
# The Convection kernel is coupled to the Diffusion kernel on the second variable
[ConvectionDiffusion]
variables = 'convected diffused'
[]
#[Variables]
# [./convected]
# [../]
# [./diffused]
# [../]
#[]
#
#[Kernels]
# [./diff_v]
# type = Diffusion
# variable = convected
# [../]
# [./diff_u]
# type = Diffusion
# variable = diffused
# [../]
#[]
[BCs]
active = 'left_convected right_convected left_diffused right_diffused'
[./left_convected]
type = DirichletBC
variable = convected
boundary = '3'
value = 0
[../]
[./right_convected]
type = DirichletBC
variable = convected
boundary = '1'
value = 1
[../]
[./left_diffused]
type = DirichletBC
variable = diffused
boundary = '3'
value = 0
[../]
[./right_diffused]
type = DirichletBC
variable = diffused
boundary = '1'
value = 1
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
file_base = out
[]
(test/tests/auxkernels/solution_aux/aux_nonlinear_solution_xda.i)
[Mesh]
# This test uses SolutionUserObject which doesn't work with DistributedMesh.
type = GeneratedMesh
parallel_type = replicated
dim = 2
nx = 2
ny = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./u_aux]
[../]
[]
[Functions]
[./u_xda_func]
type = SolutionFunction
solution = xda_u
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./aux_xda_kernel]
type = SolutionAux
variable = u_aux
solution = xda_u_aux
execute_on = initial
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 2
[../]
[]
[UserObjects]
[./xda_u_aux]
type = SolutionUserObject
system = aux0
mesh = aux_nonlinear_solution_out_0001_mesh.xda
es = aux_nonlinear_solution_out_0001.xda
system_variables = u_aux
execute_on = initial
[../]
[./xda_u]
type = SolutionUserObject
system = nl0
mesh = aux_nonlinear_solution_out_0001_mesh.xda
es = aux_nonlinear_solution_out_0001.xda
system_variables = u
execute_on = initial
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
nl_rel_tol = 1e-10
[]
[Outputs]
exodus = true
[]
[ICs]
[./u_func_ic]
function = u_xda_func
variable = u
type = FunctionIC
[../]
[]
(modules/phase_field/test/tests/MultiPhase/multibarrierfunction.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 50
ny = 50
nz = 0
xmin = 0
xmax = 20
ymin = 0
ymax = 20
elem_type = QUAD4
[]
[AuxVariables]
[./eta1]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = SmoothCircleIC
x1 = 7.0
y1 = 10.0
radius = 5.0
invalue = 0.9
outvalue = 0.1
int_width = 2.0
[../]
[../]
[./eta2]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = SmoothCircleIC
x1 = 13.0
y1 = 10.0
radius = 5.0
invalue = 0.9
outvalue = 0.1
int_width = 2.0
[../]
[../]
[]
[BCs]
[./Periodic]
[./All]
auto_direction = 'x y'
[../]
[../]
[]
[Materials]
[./multibarrier]
type = MultiBarrierFunctionMaterial
etas = 'eta1 eta2'
function_name = g
outputs = exodus
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Problem]
solve = false
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/function_file_test15.i)
# Test for usage of missing function
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = ic_function
[../]
[../]
[]
[Functions]
[./ic_function]
type = PiecewiseLinear
data_file = piecewise_linear_rows_more_data.csv
xy_in_file_only = false
x_index_in_file = 3 # will generate an error because no forth row of data
scale_factor = 1.0
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/porous_flow/test/tests/poroperm/PermTensorFromVar03.i)
# Testing permeability calculated from scalar and tensor
# Trivial test, checking calculated permeability is correct
# when k_anisotropy is not specified.
# k = k_anisotropy * perm
[Mesh]
type = GeneratedMesh
dim = 1
nx = 3
xmin = 0
xmax = 3
[]
[GlobalParams]
block = 0
PorousFlowDictator = dictator
[]
[Variables]
[pp]
[InitialCondition]
type = ConstantIC
value = 0
[]
[]
[]
[Kernels]
[flux]
type = PorousFlowAdvectiveFlux
gravity = '0 0 0'
variable = pp
[]
[]
[BCs]
[ptop]
type = DirichletBC
variable = pp
boundary = right
value = 0
[]
[pbase]
type = DirichletBC
variable = pp
boundary = left
value = 1
[]
[]
[AuxVariables]
[perm_var]
order = CONSTANT
family = MONOMIAL
[]
[perm_x]
order = CONSTANT
family = MONOMIAL
[]
[perm_y]
order = CONSTANT
family = MONOMIAL
[]
[perm_z]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[perm_var]
type = ConstantAux
value = 2
variable = perm_var
[]
[perm_x]
type = PorousFlowPropertyAux
property = permeability
variable = perm_x
row = 0
column = 0
[]
[perm_y]
type = PorousFlowPropertyAux
property = permeability
variable = perm_y
row = 1
column = 1
[]
[perm_z]
type = PorousFlowPropertyAux
property = permeability
variable = perm_z
row = 2
column = 2
[]
[]
[Postprocessors]
[perm_x_left]
type = PointValue
variable = perm_x
point = '0.5 0 0'
[]
[perm_y_left]
type = PointValue
variable = perm_y
point = '0.5 0 0'
[]
[perm_z_left]
type = PointValue
variable = perm_z
point = '0.5 0 0'
[]
[perm_x_right]
type = PointValue
variable = perm_x
point = '2.5 0 0'
[]
[perm_y_right]
type = PointValue
variable = perm_y
point = '2.5 0 0'
[]
[perm_z_right]
type = PointValue
variable = perm_z
point = '2.5 0 0'
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureVG
# unimportant in this fully-saturated test
m = 0.8
alpha = 1e-4
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
[]
[]
[]
[Materials]
[permeability]
type = PorousFlowPermeabilityTensorFromVar
perm = perm_var
[]
[temperature]
type = PorousFlowTemperature
[]
[massfrac]
type = PorousFlowMassFraction
[]
[eff_fluid_pressure]
type = PorousFlowEffectiveFluidPressure
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pp
capillary_pressure = pc
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[porosity]
type = PorousFlowPorosity
porosity_zero = 0.1
[]
[relperm]
type = PorousFlowRelativePermeabilityCorey
n = 0 # unimportant in this fully-saturated situation
phase = 0
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
[]
[]
[Executioner]
solve_type = Newton
type = Steady
l_tol = 1E-5
nl_abs_tol = 1E-3
nl_rel_tol = 1E-8
l_max_its = 200
nl_max_its = 400
petsc_options_iname = '-pc_type -pc_asm_overlap -sub_pc_type -ksp_type -ksp_gmres_restart'
petsc_options_value = ' asm 2 lu gmres 200'
[]
[Outputs]
csv = true
execute_on = 'timestep_end'
[]
(test/tests/outputs/nemesis/nemesis_elemental.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 4
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./proc_id]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./proc_id]
type = ProcessorIDAux
variable = proc_id
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
nemesis = true
[]
(test/tests/mesh/splitting/geometric_neighbors.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 8
ny = 2
xmax = 8
ymax = 2
# We are testing geometric ghosted functors
# so we have to use distributed mesh
parallel_type = distributed
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./ghosted_elements]
order = CONSTANT
family = MONOMIAL
[../]
[./proc]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./random_elemental]
type = ElementUOAux
variable = ghosted_elements
element_user_object = ghost_uo
field_name = "ghosted"
execute_on = initial
[../]
[./proc]
type = ProcessorIDAux
variable = proc
execute_on = initial
[../]
[]
[UserObjects]
[./ghost_uo]
type = ElemSideNeighborLayersGeomTester
execute_on = initial
element_side_neighbor_layers = 2
[../]
[]
[Postprocessors]
[./num_elems]
type = NumElems
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
[Problem]
solve = false
kernel_coverage_check = false
[]
(modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/ad_rz_cone_by_parts_steady_stabilized.i)
[GlobalParams]
order = FIRST
integrate_p_by_parts = true
[]
[Mesh]
file = '2d_cone.msh'
[]
[Problem]
coord_type = RZ
[]
[AuxVariables]
[vel_x]
[]
[vel_y]
[]
[]
[AuxKernels]
[vel_x]
type = VectorVariableComponentAux
variable = vel_x
vector_variable = velocity
component = 'x'
[]
[vel_y]
type = VectorVariableComponentAux
variable = vel_y
vector_variable = velocity
component = 'y'
[]
[]
[Variables]
[./velocity]
family = LAGRANGE_VEC
[../]
[./p]
[../]
[]
# Need to set a non-zero initial condition because we have a velocity norm in
# the denominator for the tau coefficient of the stabilization term
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[mass_pspg]
type = INSADMassPSPG
variable = p
[]
[momentum_advection]
type = INSADMomentumAdvection
variable = velocity
[]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
[../]
[momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[]
[]
[BCs]
[inlet]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom'
function_x = 0
function_y = 'inlet_func'
[../]
[wall]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'right'
function_x = 0
function_y = 0
[]
[axis]
type = ADVectorFunctionDirichletBC
variable = velocity
boundary = 'left'
set_y_comp = false
function_x = 0
[]
[]
[Functions]
[./inlet_func]
type = ParsedFunction
value = '-4 * x^2 + 1'
[../]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[ins_mat]
type = INSADTauMaterial
velocity = velocity
pressure = p
[]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = 'bjacobi ilu 4'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
csv = true
console = true
[./out]
type = Exodus
[../]
[]
[Postprocessors]
[./flow_in]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'bottom'
execute_on = 'timestep_end'
[../]
[./flow_out]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'top'
execute_on = 'timestep_end'
[../]
[]
(test/tests/vectorpostprocessors/csv_reader/transfer/master.i)
[Mesh]
type = GeneratedMesh
parallel_type = 'replicated'
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[MultiApps]
[./master]
type = FullSolveMultiApp
input_files = 'sub.i'
execute_on = initial
[../]
[]
[Transfers]
[./transfer]
type = MultiAppUserObjectTransfer
to_multi_app = master
user_object = data
variable = aux
[../]
[]
[VectorPostprocessors]
[./data]
type = CSVReader
csv_file = 'example.csv'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/auxkernels/solution_aux/solution_aux_direct.i)
[Mesh]
type = FileMesh
file = build_out_0001_mesh.xda
# This test uses SolutionUserObject which doesn't work with DistributedMesh.
parallel_type = replicated
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./u_aux]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./initial_cond_aux]
type = SolutionAux
solution = soln
variable = u_aux
execute_on = initial
direct = true
[../]
[]
[UserObjects]
[./soln]
type = SolutionUserObject
mesh = build_out_0001_mesh.xda
es = build_out_0001.xda
system_variables = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
nl_rel_tol = 1e-10
[]
[Outputs]
exodus = true
[]
(test/tests/misc/debug_pid_aux/debug_pid_aux.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 8
ny = 8
[Partitioner]
type = GridPartitioner
nx = 2
ny = 2
nz = 1
[]
[]
[Debug]
pid_aux = true
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/vectorpostprocessors/intersection_points_along_line/2d.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
# Ray tracing code is not yet compatible with DistributedMesh
parallel_type = replicated
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[VectorPostprocessors]
[./intersections]
type = IntersectionPointsAlongLine
start = '0.05 0.05 0'
end = '0.05 0.405 0'
[../]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Outputs]
csv = true
[]
(test/tests/auxkernels/nodal_aux_var/nodal_sort_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./one]
order = FIRST
family = LAGRANGE
initial_condition = 0
[../]
[./two]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
# Intentionally out of order to test sorting capabiilties
active = 'one two'
[./two]
variable = two
type = CoupledAux
value = 2
operator = '/'
coupled = one
[../]
[./one]
variable = one
type = ConstantAux
value = 1
[../]
[./five]
type = ConstantAux
variable = five
boundary = '3 1'
value = 5
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[]
(modules/porous_flow/test/tests/poroperm/PermTensorFromVar01.i)
# Testing permeability calculated from scalar and tensor
# Trivial test, checking calculated permeability is correct
# k = k_anisotropy * perm
[Mesh]
type = GeneratedMesh
dim = 1
nx = 3
xmin = 0
xmax = 3
[]
[GlobalParams]
block = 0
PorousFlowDictator = dictator
[]
[Variables]
[pp]
[InitialCondition]
type = ConstantIC
value = 0
[]
[]
[]
[Kernels]
[flux]
type = PorousFlowAdvectiveFlux
gravity = '0 0 0'
variable = pp
[]
[]
[BCs]
[ptop]
type = DirichletBC
variable = pp
boundary = right
value = 0
[]
[pbase]
type = DirichletBC
variable = pp
boundary = left
value = 1
[]
[]
[AuxVariables]
[perm_var]
order = CONSTANT
family = MONOMIAL
[]
[perm_x]
order = CONSTANT
family = MONOMIAL
[]
[perm_y]
order = CONSTANT
family = MONOMIAL
[]
[perm_z]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[perm_var]
type = ConstantAux
value = 2
variable = perm_var
[]
[perm_x]
type = PorousFlowPropertyAux
property = permeability
variable = perm_x
row = 0
column = 0
[]
[perm_y]
type = PorousFlowPropertyAux
property = permeability
variable = perm_y
row = 1
column = 1
[]
[perm_z]
type = PorousFlowPropertyAux
property = permeability
variable = perm_z
row = 2
column = 2
[]
[]
[Postprocessors]
[perm_x_left]
type = PointValue
variable = perm_x
point = '0.5 0 0'
[]
[perm_y_left]
type = PointValue
variable = perm_y
point = '0.5 0 0'
[]
[perm_z_left]
type = PointValue
variable = perm_z
point = '0.5 0 0'
[]
[perm_x_right]
type = PointValue
variable = perm_x
point = '2.5 0 0'
[]
[perm_y_right]
type = PointValue
variable = perm_y
point = '2.5 0 0'
[]
[perm_z_right]
type = PointValue
variable = perm_z
point = '2.5 0 0'
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureVG
# unimportant in this fully-saturated test
m = 0.8
alpha = 1e-4
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
[]
[]
[]
[Materials]
[permeability]
type = PorousFlowPermeabilityTensorFromVar
k_anisotropy = '1 0 0 0 2 0 0 0 0.1'
perm = perm_var
[]
[temperature]
type = PorousFlowTemperature
[]
[massfrac]
type = PorousFlowMassFraction
[]
[eff_fluid_pressure]
type = PorousFlowEffectiveFluidPressure
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pp
capillary_pressure = pc
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[porosity]
type = PorousFlowPorosity
porosity_zero = 0.1
[]
[relperm]
type = PorousFlowRelativePermeabilityCorey
n = 0 # unimportant in this fully-saturated situation
phase = 0
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
[]
[]
[Executioner]
solve_type = Newton
type = Steady
l_tol = 1E-5
nl_abs_tol = 1E-3
nl_rel_tol = 1E-8
l_max_its = 200
nl_max_its = 400
petsc_options_iname = '-pc_type -pc_asm_overlap -sub_pc_type -ksp_type -ksp_gmres_restart'
petsc_options_value = ' asm 2 lu gmres 200'
[]
[Outputs]
csv = true
execute_on = 'timestep_end'
[]
(test/tests/postprocessors/element_integral/element_integral_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Postprocessors]
[./integral]
type = ElementIntegralVariablePostprocessor
variable = u
[../]
[]
[Outputs]
file_base = out
exodus = false
csv = true
[]
(test/tests/userobjects/geometry_snap/geometrysphere.i)
[Mesh]
type = GeneratedMesh
dim = 2
[]
[Variables]
[./u]
initial_condition = 1
[../]
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[Executioner]
type = Steady
[]
[UserObjects]
[./sphere]
type = GeometrySphere
boundary = 'left right top bottom'
center = '0.5 0.5 0'
radius = 0.7071
[../]
[]
[Adaptivity]
[./Markers]
[./const]
type = UniformMarker
mark = REFINE
[../]
[../]
marker = const
steps = 3
[]
[Outputs]
[./out]
type = Exodus
[../]
[]
(test/tests/fvkernels/mms/skewness-correction/two_term_extrapol/advection-outflow.i)
diff=1
a=1
[GlobalParams]
advected_interp_method = 'average'
[]
[Mesh]
[./gen_mesh]
type = FileMeshGenerator
file = skewed.msh
[../]
[]
[Variables]
[./v]
type = MooseVariableFVReal
face_interp_method = 'skewness-corrected'
cache_face_gradients = false
cache_face_values = true
[../]
[]
[FVKernels]
[./advection]
type = FVAdvection
variable = v
velocity = '${a} 0 0'
[../]
[./diffusion]
type = FVDiffusion
variable = v
coeff = coeff
[../]
[./body]
type = FVBodyForce
variable = v
function = 'forcing'
[../]
[]
[FVBCs]
[left]
type = FVFunctionDirichletBC
boundary = 'left'
function = 'exact'
variable = v
[]
[top]
type = FVNeumannBC
boundary = 'top'
value = 0
variable = v
[]
[bottom]
type = FVNeumannBC
boundary = 'bottom'
value = 0
variable = v
[]
[right]
type = FVConstantScalarOutflowBC
variable = v
velocity = '${a} 0 0'
boundary = 'right'
[]
[]
[Materials]
[diff]
type = ADGenericFunctorMaterial
prop_names = 'coeff'
prop_values = '${diff}'
[]
[]
[Functions]
[exact]
type = ParsedFunction
value = 'cos(x)'
[]
[forcing]
type = ParsedFunction
value = 'cos(x) - sin(x)'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_hypre_type -snes_linesearch_minlambda'
petsc_options_value = 'hypre boomeramg 1e-9'
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[./error]
type = ElementL2Error
variable = v
function = exact
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(test/tests/functions/parsed/function_curl.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmin = -1
ymin = -1
elem_type = QUAD9
[]
[Variables]
# u = (y, -x, 0)
[./u]
family = NEDELEC_ONE
order = FIRST
[../]
[]
[Functions]
# Simple "clockwise rotating" field in XY plane. curl(u) = (0, 0, -2)
[./field]
type = ParsedVectorFunction
value_x = 'y'
value_y = '-x'
curl_z = '-2'
[../]
[./ffn_x]
type = ParsedFunction
value = 'y'
[../]
[./ffn_y]
type = ParsedFunction
value = '-x'
[../]
[]
[Kernels]
[./diff]
type = VectorFEWave
variable = u
x_forcing_func = ffn_x
y_forcing_func = ffn_y
[../]
[]
[BCs]
[./top]
type = VectorCurlBC
curl_value = field
variable = u
boundary = 'left right top bottom'
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/vectorpostprocessors/csv_reader/read.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[UserObjects]
[./tester]
type = TestCSVReader
vectorpostprocessor = reader
vector = year
gold = '1980 1980 2011 2013'
rank = 1
[../]
[]
[VectorPostprocessors]
[./reader]
type = CSVReader
csv_file = example.csv
[../]
[]
[Outputs]
csv = true
[]
(test/tests/auxkernels/element_aux_var/element_high_order_aux_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./high_order]
order = NINTH
family = MONOMIAL
[../]
[./one]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
# Coupling of nonlinear to Aux
[./diff]
type = Diffusion
variable = u
[../]
[./force]
type = CoupledForce
variable = u
v = one
[../]
[]
[AuxKernels]
[./coupled_high_order]
variable = high_order
type = CoupledAux
value = 2
operator = +
coupled = u
execute_on = 'initial timestep_end'
[../]
[./constant]
variable = one
type = ConstantAux
value = 1
execute_on = 'initial timestep_end'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Postprocessors]
[./int2_u]
type = ElementL2Norm
variable = u
execute_on = 'initial timestep_end'
[../]
[./int2_ho]
type = ElementL2Norm
variable = high_order
execute_on = 'initial timestep_end'
[../]
[./int_u]
type = ElementIntegralVariablePostprocessor
variable = u
execute_on = 'initial timestep_end'
[../]
[./int_ho]
type = ElementIntegralVariablePostprocessor
variable = high_order
execute_on = 'initial timestep_end'
[../]
[]
[Outputs]
[./ex_out]
type = Exodus
file_base = ho
elemental_as_nodal = true
[../]
[]
(test/tests/multiapps/picard_postprocessor/steady_sub.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
parallel_type = replicated
uniform_refine = 1
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[sink]
type = BodyForce
variable = u
value = -1
[]
[]
[BCs]
[right]
type = PostprocessorDirichletBC
variable = u
boundary = right
postprocessor = 'from_main'
[]
[]
[Postprocessors]
[from_main]
type = Receiver
default = 0
[]
[to_main]
type = SideAverageValue
variable = u
boundary = left
[]
[average]
type = ElementAverageValue
variable = u
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
nl_abs_tol = 1e-14
[]
[Outputs]
csv = true
exodus = false
[]
(test/tests/ics/dependency/monomial.i)
[GlobalParams]
family = MONOMIAL
order = FIRST
[]
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
[]
[AuxVariables]
[./a]
[../]
[./b]
[../]
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[ICs]
[./u_ic]
type = ConstantIC
variable = u
value = -1
[../]
[./v_ic]
type = MTICSum
variable = v
var1 = u
var2 = a
[../]
[./a_ic]
type = ConstantIC
variable = a
value = 10
[../]
[./b_ic]
type = MTICMult
variable = b
var1 = v
factor = 2
[../]
[]
[AuxKernels]
[./a_ak]
type = ConstantAux
variable = a
value = 256
[../]
[./b_ak]
type = ConstantAux
variable = b
value = 42
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[BCs]
[./left_u]
type = PenaltyDirichletBC
variable = u
boundary = left
value = 0
penalty = 1000
[../]
[./right_u]
type = PenaltyDirichletBC
variable = u
boundary = right
value = 1
penalty = 1000
[../]
[./left_v]
type = PenaltyDirichletBC
variable = v
boundary = left
value = 2
penalty = 1000
[../]
[./right_v]
type = PenaltyDirichletBC
variable = v
boundary = right
value = 1
penalty = 1000
[../]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
nl_rel_tol = 1e-10
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/code_verification/cylindrical_test_no3.i)
# Problem II.3
#
# The thermal conductivity of an infinitely long hollow cylinder varies
# linearly with temperature: k = k0(1+beta*u). The tube inside radius is ri and
# outside radius is ro. It has a constant internal heat generation q and
# is exposed to the same constant temperature on both surfaces: u(ri) = u(ro) = uo.
#
# REFERENCE:
# A. Toptan, et al. (Mar.2020). Tech. rep. CASL-U-2020-1939-000, SAND2020-3887 R. DOI:10.2172/1614683.
[Mesh]
[./geom]
type = GeneratedMeshGenerator
dim = 1
elem_type = EDGE2
xmin = 0.2
nx = 4
[../]
[]
[Variables]
[./u]
order = FIRST
[../]
[]
[Problem]
coord_type = RZ
[]
[Functions]
[./exact]
type = ParsedFunction
vars = 'q k0 ri ro beta u0'
vals = '1200 1 0.2 1.0 1e-3 0'
value = 'u0+(1/beta)*( ( 1 + 0.5*beta*((ro^2-x^2)-(ro^2-ri^2) * log(ro/x)/log(ro/ri))*q/k0 )^0.5 - 1)'
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = u
[../]
[./heatsource]
type = HeatSource
function = 1200
variable = u
[../]
[]
[BCs]
[./uo]
type = DirichletBC
boundary = 'left right'
variable = u
value = 0
[../]
[]
[Materials]
[./property]
type = GenericConstantMaterial
prop_names = 'density specific_heat'
prop_values = '1.0 1.0'
[../]
[./thermal_conductivity]
type = ParsedMaterial
f_name = 'thermal_conductivity'
args = u
function = '1 * (1 + 1e-3*u)'
[../]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[./error]
type = ElementL2Error
function = exact
variable = u
[../]
[./h]
type = AverageElementSize
[]
[]
[Outputs]
csv = true
[]
(test/tests/postprocessors/interface_diffusive_flux/interface_diffusive_flux_fv.i)
postprocessor_type = InterfaceDiffusiveFluxAverage
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 6
xmax = 3
ny = 9
ymax = 3
elem_type = QUAD4
[]
[subdomain_id]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '0 0 0'
top_right = '2 1 0'
block_id = 1
[]
[interface]
input = subdomain_id
type = SideSetsBetweenSubdomainsGenerator
primary_block = '1'
paired_block = '0'
new_boundary = 'interface'
[]
[]
[Functions]
[fn_exact]
type = ParsedFunction
value = 'x*x+y*y'
[]
[]
[Variables]
[u]
type = MooseVariableFVReal
block = 0
[]
[v]
type = MooseVariableFVReal
block = 1
[]
[]
[FVKernels]
[diff_u]
type = FVDiffusion
variable = u
coeff = 1
[]
[body_u]
type = FVBodyForce
variable = u
function = 1
[]
[diff_v]
type = FVDiffusion
variable = v
coeff = 1
[]
[body_v]
type = FVBodyForce
variable = v
function = -1
[]
[]
[FVInterfaceKernels]
[reaction]
type = FVDiffusionInterface
variable1 = u
variable2 = v
coeff1 = 1
coeff2 = 2
boundary = 'interface'
subdomain1 = '0'
subdomain2 = '1'
[]
[]
[FVBCs]
[all]
type = FVFunctionDirichletBC
variable = u
boundary = '0 1 2 3'
function = fn_exact
[]
[]
[Postprocessors]
[diffusive_flux]
type = ${postprocessor_type}
variable = v
neighbor_variable = u
diffusivity = 1
execute_on = TIMESTEP_END
boundary = 'interface'
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
file_base = ${raw ${postprocessor_type} _fv}
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/velocity_channel/velocity_inletBC_by_parts.i)
# This input file tests outflow boundary conditions for the incompressible NS equations.
[GlobalParams]
gravity = '0 0 0'
integrate_p_by_parts = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 3.0
ymin = 0
ymax = 1.0
nx = 30
ny = 10
elem_type = QUAD9
[]
[Variables]
[./vel_x]
order = SECOND
family = LAGRANGE
[../]
[./vel_y]
order = SECOND
family = LAGRANGE
[../]
[./p]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./mass]
type = INSMass
variable = p
u = vel_x
v = vel_y
pressure = p
[../]
[./x_momentum_space]
type = INSMomentumLaplaceForm
variable = vel_x
u = vel_x
v = vel_y
pressure = p
component = 0
[../]
[./y_momentum_space]
type = INSMomentumLaplaceForm
variable = vel_y
u = vel_x
v = vel_y
pressure = p
component = 1
[../]
[]
[BCs]
[./x_no_slip]
type = DirichletBC
variable = vel_x
boundary = 'top bottom'
value = 0.0
[../]
[./y_no_slip]
type = DirichletBC
variable = vel_y
boundary = 'left top bottom'
value = 0.0
[../]
[./x_inlet]
type = FunctionDirichletBC
variable = vel_x
boundary = 'left'
function = 'inlet_func'
[../]
[]
[Materials]
[./const]
type = GenericConstantMaterial
block = 0
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[]
[Preconditioning]
[./SMP_PJFNK]
type = SMP
full = true
solve_type = NEWTON
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-ksp_gmres_restart -pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = '300 bjacobi ilu 4'
line_search = none
nl_rel_tol = 1e-12
nl_max_its = 6
l_tol = 1e-6
l_max_its = 300
[]
[Outputs]
[./out]
type = Exodus
[../]
[]
[Functions]
[./inlet_func]
type = ParsedFunction
value = '-4 * (y - 0.5)^2 + 1'
[../]
[]
(modules/tensor_mechanics/test/tests/elasticitytensor/rotation_matrix_2_rotations.i)
# This input file is designed to rotate an elasticity tensor both with euler angles
# and a rotation matrix. The rotated tensor components should match between the
# two methods.
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
xmax = 1
[]
[AuxVariables]
[./C1111_aux_matrix] # C11
order = CONSTANT
family = MONOMIAL
[../]
[./C1122_aux_matrix] # C12
order = CONSTANT
family = MONOMIAL
[../]
[./C1133_aux_matrix] # C13
order = CONSTANT
family = MONOMIAL
[../]
[./C1112_aux_matrix] # C16
order = CONSTANT
family = MONOMIAL
[../]
[./C1111_aux_euler] # C11
order = CONSTANT
family = MONOMIAL
[../]
[./C1122_aux_euler] # C12
order = CONSTANT
family = MONOMIAL
[../]
[./C1133_aux_euler] # C13
order = CONSTANT
family = MONOMIAL
[../]
[./C1112_aux_euler] # C16
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./matl_C1111_matrix] # C11
type = RankFourAux
rank_four_tensor = rotation_matrix_elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 0
variable = C1111_aux_matrix
execute_on = initial
[../]
[./matl_C1122_matrix] # C12
type = RankFourAux
rank_four_tensor = rotation_matrix_elasticity_tensor
index_i = 0
index_j = 0
index_k = 1
index_l = 1
variable = C1122_aux_matrix
execute_on = initial
[../]
[./matl_C1133_matrix] # C13
type = RankFourAux
rank_four_tensor = rotation_matrix_elasticity_tensor
index_i = 0
index_j = 0
index_k = 2
index_l = 2
variable = C1133_aux_matrix
execute_on = initial
[../]
[./matl_C1112_matrix] # C16
type = RankFourAux
rank_four_tensor = rotation_matrix_elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 1
variable = C1112_aux_matrix
execute_on = initial
[../]
[./matl_C1111_euler] # C11
type = RankFourAux
rank_four_tensor = euler_elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 0
variable = C1111_aux_euler
execute_on = initial
[../]
[./matl_C1122_euler] # C12
type = RankFourAux
rank_four_tensor = euler_elasticity_tensor
index_i = 0
index_j = 0
index_k = 1
index_l = 1
variable = C1122_aux_euler
execute_on = initial
[../]
[./matl_C1133_euler] # C13
type = RankFourAux
rank_four_tensor = euler_elasticity_tensor
index_i = 0
index_j = 0
index_k = 2
index_l = 2
variable = C1133_aux_euler
execute_on = initial
[../]
[./matl_C1112_euler] # C16
type = RankFourAux
rank_four_tensor = euler_elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 1
variable = C1112_aux_euler
execute_on = initial
[../]
[]
[Materials]
[./elasticity_matrix]
type = ComputeElasticityTensor
block = 0
base_name = 'rotation_matrix'
fill_method = symmetric9
C_ijkl = '1111 1122 1133 2222 2233 3333 2323 1313 1212'
# rotation matrix for rotating a vector
# 1. 45 degrees about z-axis
# 2. ~54.7 degrees (arccos(1/sqrt(3)) radians) about x-axis
# then taking the tranpose to give sample-to-crystal rotation,
# ie. R*([0,0,1]) = [1,1,1], meaning the <001> direction of the sample
# (or simulation) frame points along the <111> direction of the crystal
rotation_matrix = '0.70710678 0.40824829 0.57735027
-0.70710678 0.40824829 0.57735027
0. -0.81649658 0.57735027'
[../]
[./elasticity_euler]
type = ComputeElasticityTensor
block = 0
base_name = 'euler'
fill_method = symmetric9
C_ijkl = '1111 1122 1133 2222 2233 3333 2323 1313 1212'
# the angles here are the same as used to build the rotation matrix above because
# we build the _transpose_ from euler angles in MOOSE, but we also transposed
# the matrix for this example, so it goes back to the original;
# the reversed order is due to the "extrinsic" convention used by MOOSE
euler_angle_1 = 0.
euler_angle_2 = 54.73561032
euler_angle_3 = 45.
[../]
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[Executioner]
type = Steady
[]
[Postprocessors]
# corresponding values in "matrix" and "euler" postprocessors should match
[./C11_matrix]
type = ElementAverageValue
variable = C1111_aux_matrix
execute_on = 'INITIAL TIMESTEP_END'
[../]
[./C12_matrix]
type = ElementAverageValue
variable = C1122_aux_matrix
execute_on = 'INITIAL TIMESTEP_END'
[../]
[./C13_matrix]
type = ElementAverageValue
variable = C1133_aux_matrix
execute_on = 'INITIAL TIMESTEP_END'
[../]
[./C16_matrix]
type = ElementAverageValue
variable = C1112_aux_matrix
execute_on = 'INITIAL TIMESTEP_END'
[../]
[./C11_euler]
type = ElementAverageValue
variable = C1111_aux_euler
execute_on = 'INITIAL TIMESTEP_END'
[../]
[./C12_euler]
type = ElementAverageValue
variable = C1122_aux_euler
execute_on = 'INITIAL TIMESTEP_END'
[../]
[./C13_euler]
type = ElementAverageValue
variable = C1133_aux_euler
execute_on = 'INITIAL TIMESTEP_END'
[../]
[./C16_euler]
type = ElementAverageValue
variable = C1112_aux_euler
execute_on = 'INITIAL TIMESTEP_END'
[../]
[]
[Outputs]
exodus = true
[]
(test/tests/interfaces/postprocessorinterface/ppi_errors.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
[]
[]
[UserObjects/error_test]
type = PostprocessorInterfaceErrorTest
pps = '0 1'
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
(test/tests/indicators/analytical_indicator/analytical_indicator_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
nz = 10
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
[]
[]
[Functions]
[solution]
type = ParsedFunction
value = (exp(x)-1)/(exp(1)-1)
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[conv]
type = Convection
variable = u
velocity = '1 0 0'
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Adaptivity]
[Indicators]
[error]
type = AnalyticalIndicator
variable = u
function = solution
[]
[]
[]
[Outputs]
exodus = true
[]
(test/tests/mesh/split_uniform_refine/3d_diffusion.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 16
ny = 16
nz = 16
dim = 3
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
preset = false
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
preset = false
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(test/tests/variables/coupled_scalar/coupled_scalar_default.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./aux_scalar]
order = SECOND
family = SCALAR
[../]
[./coupled]
[../]
[./coupled_1]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./coupled]
type = CoupledScalarAux
variable = coupled
# Using default value
[../]
[./coupled_1]
# Coupling to the "1" component of an aux scalar
type = CoupledScalarAux
variable = coupled_1
component = 1
# Setting explicit default
coupled = 3.14159
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
[ICs]
[./aux_scalar_ic]
variable = aux_scalar
values = '1.2 4.3'
type = ScalarComponentIC
[../]
[]
(test/tests/vectorpostprocessors/element_id_counters/element_counter_block_restricted.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
xmax = 1
ymax = 1
extra_element_integers = foo_id
[]
[id0]
type = SubdomainBoundingBoxGenerator
input = gmg
bottom_left = '0 0 0'
block_id = 0
top_right = '1 1 0'
integer_name = foo_id
[]
[id1]
type = SubdomainBoundingBoxGenerator
input = id0
bottom_left = '0.4 0.4 0'
block_id = 1
top_right = '0.9 0.9 0'
integer_name = foo_id
[]
[id2]
type = SubdomainBoundingBoxGenerator
input = id1
bottom_left = '0.1 0.1 0'
block_id = 2
top_right = '0.6 0.6 0'
integer_name = foo_id
[]
[subdomain]
type = SubdomainBoundingBoxGenerator
input = id2
bottom_left = '0 0.5 0'
block_id = 1
top_right = '1 1 0'
[]
[]
[VectorPostprocessors]
[elem_counter0]
type = ElementCounterWithID
id_name = foo_id
block = 0
[]
[elem_counter1]
type = ElementCounterWithID
id_name = foo_id
block = 1
[]
[elem_counter]
type = ElementCounterWithID
id_name = subdomain_id
[]
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
execute_on = 'timestep_end'
[]
(modules/chemical_reactions/test/tests/equilibrium_const/constant.i)
# Test of EquilibriumConstantAux with a single log(K) value.
# The resulting equilibrium constant should simple be constant.
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
[]
[AuxVariables]
[./logk]
[../]
[]
[AuxKernels]
[./logk]
type = EquilibriumConstantAux
temperature = temperature
temperature_points = 300
logk_points = 1.23
variable = logk
[../]
[]
[Variables]
[./temperature]
[../]
[]
[Kernels]
[./temperature]
type = Diffusion
variable = temperature
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = temperature
value = 150
boundary = left
[../]
[./right]
type = DirichletBC
variable = temperature
value = 400
boundary = right
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/controls/control_connection/control_connection.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = CoefDiffusion
variable = u
coef = 0.1
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Controls]
[./control]
type = TestControl
execute_on = INITIAL
test_type = 'connection'
parameter = 'Kernels/diff/coef'
[../]
[]
[Outputs]
exodus = true
[]
(test/tests/dgkernels/stateful-coupled-var/test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
elem_type = QUAD4
[]
[Variables]
[u]
order = FIRST
family = MONOMIAL
[]
[]
[Functions]
[exact_fn]
type = ParsedGradFunction
value = pow(e,-x-(y*y))
grad_x = -pow(e,-x-(y*y))
grad_y = -2*y*pow(e,-x-(y*y))
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[DGKernels]
[dg_diff]
type = DGDiffusion
variable = u
epsilon = -1
sigma = 6
diff = diffusion
[]
[]
[Materials]
[coupled_mat]
type = VarCouplingMaterial
var = u
declare_old = true
use_tag = false
[]
[]
[BCs]
[all]
type = DGFunctionDiffusionDirichletBC
variable = u
boundary = '0 1 2 3'
function = exact_fn
epsilon = -1
sigma = 6
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/ad_rz_cone_by_parts_steady_stabilized_second_order.i)
[GlobalParams]
order = SECOND
integrate_p_by_parts = true
[]
[Mesh]
file = '2d_cone.msh'
[]
[Problem]
coord_type = RZ
[]
[AuxVariables]
[vel_x]
[]
[vel_y]
[]
[]
[AuxKernels]
[vel_x]
type = VectorVariableComponentAux
variable = vel_x
vector_variable = velocity
component = 'x'
[]
[vel_y]
type = VectorVariableComponentAux
variable = vel_y
vector_variable = velocity
component = 'y'
[]
[]
[Variables]
[./velocity]
family = LAGRANGE_VEC
[../]
[./p]
order = FIRST
[../]
[]
# Need to set a non-zero initial condition because we have a velocity norm in
# the denominator for the tau coefficient of the stabilization term
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[mass_pspg]
type = INSADMassPSPG
variable = p
[]
[momentum_advection]
type = INSADMomentumAdvection
variable = velocity
[]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
[../]
[momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[]
[]
[BCs]
[inlet]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom'
function_x = 0
function_y = 'inlet_func'
[../]
[wall]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'right'
function_x = 0
function_y = 0
[]
[axis]
type = ADVectorFunctionDirichletBC
variable = velocity
boundary = 'left'
set_y_comp = false
function_x = 0
[]
[]
[Functions]
[./inlet_func]
type = ParsedFunction
value = '-4 * x^2 + 1'
[../]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[ins_mat]
type = INSADTauMaterial
velocity = velocity
pressure = p
[]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = 'bjacobi ilu 4'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
csv = true
console = true
[./out]
type = Exodus
[../]
[]
[Postprocessors]
[./flow_in]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'bottom'
execute_on = 'timestep_end'
[../]
[./flow_out]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'top'
execute_on = 'timestep_end'
[../]
[]
(modules/porous_flow/test/tests/capillary_pressure/brooks_corey1.i)
# Test Brooks-Corey capillary pressure curve by varying saturation over the mesh
# lambda = 2, sat_lr = 0.1, log_extension = false
[Mesh]
type = GeneratedMesh
dim = 1
nx = 500
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Variables]
[p0]
initial_condition = 1e6
[]
[s1]
[]
[]
[AuxVariables]
[s0aux]
family = MONOMIAL
order = CONSTANT
[]
[s1aux]
family = MONOMIAL
order = CONSTANT
[]
[p0aux]
family = MONOMIAL
order = CONSTANT
[]
[p1aux]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[s0]
type = PorousFlowPropertyAux
property = saturation
phase = 0
variable = s0aux
[]
[s1]
type = PorousFlowPropertyAux
property = saturation
phase = 1
variable = s1aux
[]
[p0]
type = PorousFlowPropertyAux
property = pressure
phase = 0
variable = p0aux
[]
[p1]
type = PorousFlowPropertyAux
property = pressure
phase = 1
variable = p1aux
[]
[]
[Functions]
[s1]
type = ParsedFunction
value = x
[]
[]
[ICs]
[s1]
type = FunctionIC
variable = s1
function = s1
[]
[]
[Kernels]
[p0]
type = Diffusion
variable = p0
[]
[s1]
type = Diffusion
variable = s1
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'p0 s1'
number_fluid_phases = 2
number_fluid_components = 2
[]
[pc]
type = PorousFlowCapillaryPressureBC
lambda = 2
log_extension = false
pe = 1e5
sat_lr = 0.1
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow2PhasePS
phase0_porepressure = p0
phase1_saturation = s1
capillary_pressure = pc
[]
[kr0]
type = PorousFlowRelativePermeabilityVG
phase = 0
m = 0.5
[]
[kr1]
type = PorousFlowRelativePermeabilityCorey
phase = 1
n = 2
[]
[]
[VectorPostprocessors]
[vpp]
type = LineValueSampler
variable = 's0aux s1aux p0aux p1aux'
start_point = '0 0 0'
end_point = '1 0 0'
num_points = 500
sort_by = id
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
nl_abs_tol = 1e-6
[]
[BCs]
[sleft]
type = DirichletBC
variable = s1
value = 0
boundary = left
[]
[sright]
type = DirichletBC
variable = s1
value = 1
boundary = right
[]
[]
[Outputs]
csv = true
execute_on = timestep_end
[]
(test/tests/mesh/mixed_dim/1d_2d_w_matl.i)
# Using different mesh file where 1D elements will come before 2D ones.
# This is important for testing the robustness of re-initializing materials
[Mesh]
file = 1d_2d-2.e
# Mixed-dimension meshes don't seem to work with DistributedMesh. The
# program hangs, I can't get a useful stack trace when I attach to
# it. See also #2130.
parallel_type = replicated
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = MatDiffusionTest
variable = u
prop_name = matp
[../]
[]
[Materials]
[./mat1]
type = MTMaterial
block = '1 2'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 4
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[./bottom]
type = DirichletBC
variable = u
boundary = 100
value = 0
[../]
[./top]
type = DirichletBC
variable = u
boundary = 101
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/mesh/gmsh_bcs/gmsh_bc_test.i)
[Mesh]
file = plate_hole.msh
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 12
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 10
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(test/tests/interfaces/userobjectinterface/uoi.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
[]
[]
[UserObjects]
[other_uo]
type = UserObjectInterfaceTest
[]
[test]
type = UserObjectInterfaceTest
uo = other_uo
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
(test/tests/dgkernels/dg_displacement/dg_displacement.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
displacements = 'disp_x disp_y'
[]
[Variables]
[./u]
order = FIRST
family = MONOMIAL
[../]
[]
[AuxVariables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[Functions]
[./forcing_fn]
type = ParsedFunction
value = 2*pow(e,-x-(y*y))*(1-2*y*y)
[../]
[./exact_fn]
type = ParsedGradFunction
value = pow(e,-x-(y*y))
grad_x = -pow(e,-x-(y*y))
grad_y = -2*y*pow(e,-x-(y*y))
[../]
[./disp_func]
type = ParsedFunction
value = x
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./abs]
type = Reaction
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[DGKernels]
[./dg_diff]
type = DGDiffusion
variable = u
epsilon = -1
sigma = 6
use_displaced_mesh = true
[../]
[]
[BCs]
[./all]
type = DGFunctionDiffusionDirichletBC
variable = u
boundary = '0 1 2 3'
function = exact_fn
epsilon = -1
sigma = 6
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
nl_rel_tol = 1e-10
[]
[Outputs]
execute_on = 'timestep_end'
file_base = out
exodus = true
[]
[ICs]
[./disp_x_ic]
function = disp_func
variable = disp_x
type = FunctionIC
[../]
[]
(test/tests/functions/solution_function/solution_function_grad_p1.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
parallel_type = replicated
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./test_variable]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = initial_cond_func
[../]
[../]
[]
[Functions]
[./initial_cond_func]
type = ParsedFunction
value = 2*x+4*y
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-10
[]
[Outputs]
file_base = solution_function_grad_p1
exodus = true
[]
(test/tests/auxkernels/solution_aux/output_error.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
xmin = 1
xmax = 4
ymin = 1
ymax = 3
# This test uses SolutionUserObject which doesn't work with DistributedMesh.
parallel_type = replicated
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./u_aux]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./initial_cond_aux]
type = SolutionAux
solution = xda_soln
execute_on = initial
variable = u_aux
direct = false
[../]
[]
[UserObjects]
[./xda_soln]
type = SolutionUserObject
mesh = build_out_0001_mesh.xda
es = build_out_0001.xda
system_variables = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
nl_rel_tol = 1e-10
[]
[Outputs]
exodus = true
xda = true
[]
(modules/thermal_hydraulics/test/tests/userobjects/layered_flow_area_change/layered_flow_area_2D.i)
[Mesh]
[generated]
type = CartesianMeshGenerator
dim = 2
dx = '1 1 1'
dy = '4'
ix = '1 1 1'
iy = '40'
subdomain_id = '1 2 1'
[]
[interior_walls]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 1
paired_block = 2
new_boundary = interior
input = generated
[]
[]
[Problem]
kernel_coverage_check = false
[]
[Variables]
[u]
[]
[]
[AuxVariables]
[disp_x]
[]
[disp_y]
[]
[channel_dA]
[]
[]
[ICs]
[disp_x_ic]
type = FunctionIC
variable = disp_x
function = 'if (x < 1.5, 0.5 * (y - 2) * 0.1, 0)'
[]
[]
[AuxKernels]
[channel_dA_aux]
type = SpatialUserObjectAux
variable = channel_dA
user_object = layered_area_change
[]
[]
[UserObjects]
[layered_area_change]
type = LayeredFlowAreaChange
direction = y
displacements = 'disp_x disp_y'
boundary = interior
num_layers = 40
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/fvkernels/two-var-flux-and-kernel/input.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
[]
[Variables]
[u]
family = MONOMIAL
order = CONSTANT
fv = true
[]
[v]
family = MONOMIAL
order = CONSTANT
fv = true
[]
[]
[FVKernels]
[diff_u]
type = FVDiffusion
variable = u
coeff = coeff
[]
[diff]
type = FVDiffusion
variable = v
coeff = coeff
[]
[]
[FVBCs]
[left_u]
type = FVNeumannBC
variable = u
boundary = left
value = 0
[]
[right_u]
type = FVDirichletBC
variable = u
boundary = right
value = 42
[]
[left]
type = FVDirichletBC
variable = v
boundary = left
value = 7
[]
[right]
type = FVDirichletBC
variable = v
boundary = right
value = 42
[]
[]
[Materials]
[diff]
type = ADGenericFunctorMaterial
prop_names = 'coeff'
prop_values = '1'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/thermal_hydraulics/test/tests/materials/ad_convection_heat_flux/ad_convection_heat_flux.i)
# Gold value should be the following:
# q_wall = kappa * htc_wall * (T_wall - T)
# = 0.5 * 100 * (500 - 400)
# = 5000
[GlobalParams]
execute_on = 'initial'
[]
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
[]
[AuxVariables]
[T_wall]
[]
[]
[AuxKernels]
[T_wall_ak]
type = ConstantAux
variable = T_wall
value = 500
[]
[]
[Materials]
[props]
type = ADGenericConstantMaterial
prop_names = 'T htc_wall kappa'
prop_values = '400 100 0.5'
[]
[q_wall_mat]
type = ADConvectionHeatFluxMaterial
q_wall = q_wall_prop
T = T
T_wall = T_wall
htc_wall = htc_wall
kappa = kappa
[]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Postprocessors]
[q_wall_pp]
type = ADElementAverageMaterialProperty
mat_prop = q_wall_prop
[]
[]
[Outputs]
csv = true
[]
(test/tests/interfacekernels/adaptivity/adaptivity.i)
# This input file is used for two tests:
# 1) Check that InterfaceKernels work with mesh adaptivity
# 2) Error out when InterfaceKernels are used with adaptivity
# and stateful material prpoerties
[Mesh]
parallel_type = 'replicated'
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 2
[]
[./subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '0.5 0 0'
top_right = '1 1 0'
block_id = 1
[../]
[./interface]
type = SideSetsBetweenSubdomainsGenerator
input = subdomain1
primary_block = '0'
paired_block = '1'
new_boundary = 'primary0_interface'
[../]
[./break_boundary]
input = interface
type = BreakBoundaryOnSubdomainGenerator
[../]
[]
[Variables]
[./u]
[./InitialCondition]
type = ConstantIC
value = 1
[../]
block = 0
[../]
[./u_neighbor]
[./InitialCondition]
type = ConstantIC
value = 1
[../]
block = 1
[../]
[]
[Functions]
[./forcing_fn]
type = ParsedFunction
value = (x*x*x)-6.0*x
[../]
[./bc_fn]
type = ParsedFunction
value = (x*x*x)
[../]
[]
[Kernels]
[./diff]
type = MatDiffusionTest
variable = u
prop_name = diffusivity
block = 0
[../]
[./abs]
type = Reaction
variable = u
block = 0
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
block = 0
[../]
[./diffn]
type = MatDiffusionTest
variable = u_neighbor
prop_name = diffusivity
block = 1
[../]
[./absn]
type = Reaction
variable = u_neighbor
block = 1
[../]
[./forcingn]
type = BodyForce
variable = u_neighbor
function = forcing_fn
block = 1
[../]
[]
[InterfaceKernels]
[./flux_match]
type = PenaltyInterfaceDiffusion
variable = u
neighbor_var = u_neighbor
boundary = primary0_interface
penalty = 1e6
[../]
[]
[BCs]
[./u]
type = FunctionDirichletBC
variable = u
boundary = 'left'
function = bc_fn
[../]
[./u_neighbor]
type = FunctionDirichletBC
variable = u_neighbor
boundary = 'right'
function = bc_fn
[../]
[]
[Materials]
active = 'constant'
[./stateful]
type = StatefulTest
prop_names = 'diffusivity'
prop_values = '1'
block = '0 1'
[../]
[./constant]
type = GenericConstantMaterial
prop_names = 'diffusivity'
prop_values = '1'
block = '0 1'
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Adaptivity]
marker = 'marker'
steps = 1
[./Markers]
[./marker]
type = BoxMarker
bottom_left = '0 0 0'
top_right = '1 1 0'
inside = refine
outside = coarsen
[../]
[../]
[]
[Outputs]
exodus = true
[]
(test/tests/auxkernels/diffusion_flux/normal_diffusion_flux.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmax = 1.0
ymax = 1.0
[]
[Variables]
[./dummy]
[../]
[]
[AuxVariables]
[./T]
[../]
[./flux_n]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./T]
type = ParsedFunction
value = 'x*x*y*y+1'
[../]
[]
[ICs]
[./T]
type = FunctionIC
variable = T
function = T
[../]
[]
[Kernels]
[./dummy]
type = Diffusion
variable = dummy
[../]
[]
[AuxKernels]
[./flux_n]
type = DiffusionFluxAux
diffusivity = 'thermal_conductivity'
variable = flux_n
diffusion_variable = T
component = normal
boundary = 'left right'
check_boundary_restricted = false
[../]
[]
[Materials]
[./k]
type = GenericConstantMaterial
prop_names = 'thermal_conductivity'
prop_values = '10'
[../]
[]
[Postprocessors]
[flux_right]
type = SideIntegralVariablePostprocessor
variable = flux_n
boundary = 'right'
[]
[flux_right_exact]
type = SideFluxIntegral
variable = T
diffusivity = 'thermal_conductivity'
boundary = 'right'
[]
[flux_left]
type = SideIntegralVariablePostprocessor
variable = flux_n
boundary = 'left'
[]
[flux_left_exact]
type = SideFluxIntegral
variable = T
diffusivity = 'thermal_conductivity'
boundary = 'left'
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
nl_rel_tol = 1e-12
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
hide = 'dummy'
[]
(modules/ray_tracing/test/tests/userobjects/ray_tracing_study/lots.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 4
ny = 4
[]
[]
[UserObjects/lots]
type = LotsOfRaysRayStudy
ray_kernel_coverage_check = false # no need for RayKernels
execute_on = initial
[]
[RayBCs/kill]
type = KillRayBC
boundary = 'top left right bottom'
[]
[Postprocessors/total_distance]
type = RayTracingStudyResult
study = lots
result = total_distance
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Outputs]
csv = true
exodus = false
[]
(test/tests/geomsearch/2d_interior_boundary_penetration_locator/2d_interior_boundary_penetration_locator.i)
[Mesh]
type = FileMesh
file = meshed_gap.e
dim = 2
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./gap_distance]
[../]
[./gap_value]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 4
value = 1
[../]
[]
[AuxKernels]
[./penetration]
type = PenetrationAux
variable = gap_distance
boundary = 2
paired_boundary = 3
[../]
[./gap_value]
type = GapValueAux
variable = gap_value
boundary = 2
paired_variable = u
paired_boundary = 3
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/phase_field/test/tests/solution_rasterizer/diffuse.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 20
ny = 20
nz = 20
xmin = 0.0
xmax = 10.0
ymin = 0.0
ymax = 10.0
zmin = 0.0
zmax = 10.0
[]
[Variables]
[./c]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./c]
variable = c
type = SmoothCircleIC
x1 = 5.0
y1 = 5.0
z1 = 5.0
radius = 4.0
invalue = 1.0
outvalue = 0.0
int_width = 1.0
[../]
[]
[Executioner]
type = Steady
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/boussinesq/wcnsfv.i)
mu = 1
rho = 'rho'
k = 1
cp = 1
alpha = 1
velocity_interp_method = 'rc'
advected_interp_method = 'average'
# rayleigh=1e3
cold_temp=300
hot_temp=310
[GlobalParams]
two_term_boundary_expansion = true
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 10
ymin = 0
ymax = 10
nx = 64
ny = 64
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1e-15
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1e-15
[]
[pressure]
type = INSFVPressureVariable
initial_condition = 1e5
[]
[T]
type = INSFVEnergyVariable
scaling = 1e-4
initial_condition = ${cold_temp}
[]
[lambda]
family = SCALAR
order = FIRST
[]
[]
[AuxVariables]
[U]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[vel_x]
order = FIRST
family = MONOMIAL
[]
[vel_y]
order = FIRST
family = MONOMIAL
[]
[viz_T]
order = FIRST
family = MONOMIAL
[]
[rho_out]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[mag]
type = VectorMagnitudeAux
variable = U
x = u
y = v
execute_on = 'initial timestep_end'
[]
[vel_x]
type = ParsedAux
variable = vel_x
function = 'u'
execute_on = 'initial timestep_end'
args = 'u'
[]
[vel_y]
type = ParsedAux
variable = vel_y
function = 'v'
execute_on = 'initial timestep_end'
args = 'v'
[]
[viz_T]
type = ParsedAux
variable = viz_T
function = 'T'
execute_on = 'initial timestep_end'
args = 'T'
[]
[rho_out]
type = ADFunctorElementalAux
functor = 'rho'
variable = 'rho_out'
execute_on = 'initial timestep_end'
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[mean_zero_pressure]
type = FVScalarLagrangeMultiplier
variable = pressure
lambda = lambda
phi0 = 1e5
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[u_gravity]
type = INSFVMomentumGravity
variable = u
gravity = '0 -1 0'
rho = ${rho}
momentum_component = 'x'
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[v_gravity]
type = INSFVMomentumGravity
variable = v
gravity = '0 -1 0'
rho = ${rho}
momentum_component = 'y'
[]
[temp_conduction]
type = FVDiffusion
coeff = 'k'
variable = T
[]
[temp_advection]
type = INSFVEnergyAdvection
variable = T
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
[]
[]
[FVBCs]
[no_slip_x]
type = INSFVNoSlipWallBC
variable = u
boundary = 'left right top bottom'
function = 0
[]
[no_slip_y]
type = INSFVNoSlipWallBC
variable = v
boundary = 'left right top bottom'
function = 0
[]
[T_hot]
type = FVDirichletBC
variable = T
boundary = left
value = ${hot_temp}
[]
[T_cold]
type = FVDirichletBC
variable = T
boundary = right
value = ${cold_temp}
[]
[]
[Modules]
[FluidProperties]
[fp]
type = IdealGasFluidProperties
[]
[]
[]
[Materials]
[const]
type = ADGenericConstantMaterial
prop_names = 'alpha'
prop_values = '${alpha}'
[]
[const_functor]
type = ADGenericFunctorMaterial
prop_names = 'cp k'
prop_values = '${cp} ${k}'
[]
[rho]
type = RhoFromPTFunctorMaterial
fp = fp
temperature = T
pressure = pressure
[]
[ins_fv]
type = INSFVEnthalpyMaterial
temperature = 'T'
rho = ${rho}
[]
[]
[Functions]
[lid_function]
type = ParsedFunction
value = '4*x*(1-x)'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
[]
[Outputs]
exodus = true
[]
(test/tests/quadrature/gauss_lobatto/gauss_lobatto.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
nz = 0
elem_type = QUAD4
[]
[Postprocessors]
[./num_elem_qps]
type = NumElemQPs
block = 0
[../]
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
# In 1D, 5th-order Gauss-Lobatto quadrature has 4 points, so in 2D
# it should have 16.
[./Quadrature]
type = GAUSS_LOBATTO
order = FIFTH
[../]
[]
[Outputs]
execute_on = 'timestep_end'
exodus = false
csv = true
[]
(test/tests/kernels/scalarkernel_vectorpostprocessor/scalarkernel_vectorpostprocessor.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[./scalar]
order = THIRD
family = SCALAR
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[VectorPostprocessors]
[./constant]
type = ConstantVectorPostprocessor
value = '1.7 2.3 4.7'
execute_on = 'initial'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
[ScalarKernels]
[./vppsk]
variable = scalar
vector = value
type = VectorPostprocessorScalarKernel
vpp = constant
[../]
[]
(modules/porous_flow/test/tests/density/GravDensity01.i)
# Trivial test of PorousFlowTotalGravitationalDensityFullySaturatedFromPorosity
# Porosity = 0.1
# Solid density = 3
# Fluid density = 2
# Fluid bulk modulus = 4
# Fluid pressure = 0
# Bulk density: rho = 3 * (1 - 0.1) + 2 * 0.1 = 2.9
# Derivative wrt fluid pressure: d_rho / d_pp = d_rho / d_rho_f * d_rho_f / d_pp
# = phi * rho_f / B
# where rho_f = rho_0 * exp(pp / B) is fluid density, pp is fluid pressure, phi is
# porosity and B is fluid bulk modulus
# With pp = 0, d_rho / d_pp = phi * rho_0 / B = 0.1 * 2 / 4 = 0.05
[Mesh]
type = GeneratedMesh
dim = 3
xmin = 0
xmax = 1
ymin = 0
ymax = 1
zmin = -1
zmax = 0
nx = 1
ny = 1
nz = 1
# This test uses ElementalVariableValue postprocessors on specific
# elements, so element numbering needs to stay unchanged
allow_renumbering = false
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
thermal_expansion = 0
bulk_modulus = 4
density0 = 2
[]
[]
[]
[Variables]
[pp]
[InitialCondition]
type = ConstantIC
value = 0
[]
[]
[]
[Kernels]
[dummy]
type = Diffusion
variable = pp
[]
[]
[BCs]
[p]
type = DirichletBC
variable = pp
boundary = 'front back'
value = 0
[]
[]
[AuxVariables]
[density]
order = CONSTANT
family = MONOMIAL
[]
[ddensity_dpp]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[density]
type = MaterialRealAux
property = density
variable = density
[]
[ddensity_dpp]
type = MaterialStdVectorAux
property = ddensity_dvar
variable = ddensity_dpp
index = 0
[]
[]
[Postprocessors]
[density]
type = ElementalVariableValue
elementid = 0
variable = density
execute_on = 'timestep_end'
[]
[ddensity_dpp]
type = ElementalVariableValue
elementid = 0
variable = ddensity_dpp
execute_on = 'timestep_end'
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss_qp]
type = PorousFlow1PhaseFullySaturated
porepressure = pp
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[porosity]
type = PorousFlowPorosityConst
porosity = 0.1
[]
[density]
type = PorousFlowTotalGravitationalDensityFullySaturatedFromPorosity
rho_s = 3
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
[]
[]
[Executioner]
solve_type = Newton
type = Steady
[]
[Outputs]
file_base = GravDensity01
csv = true
execute_on = 'timestep_end'
[]
(test/tests/vectorpostprocessors/material_vector_postprocessor/boundary-err.i)
# check that simulation terminates with an error when trying to use the
# postprocessor on a boundary material.
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Materials]
[./mat]
type = GenericConstantMaterial
prop_names = 'prop1 prop2 prop3'
prop_values = '1 2 42'
boundary = 'left'
[../]
[]
[VectorPostprocessors]
[./vpp]
type = MaterialVectorPostprocessor
material = 'mat'
elem_ids = '3 4 7 42 88'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'initial timestep_end'
csv = true
[]
(test/tests/kernels/hfem/robin_dist.i)
[Mesh]
[square]
type = GeneratedMeshGenerator
nx = 3
ny = 3
dim = 2
[]
build_all_side_lowerd_mesh = true
parallel_type = DISTRIBUTED
[]
[Variables]
[u]
order = THIRD
family = MONOMIAL
block = 0
components = 2
[]
[lambda]
order = CONSTANT
family = MONOMIAL
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
components = 2
[]
[]
[AuxVariables]
[v]
order = CONSTANT
family = MONOMIAL
block = 0
initial_condition = '1'
[]
[]
[Kernels]
[diff]
type = ArrayDiffusion
variable = u
block = 0
diffusion_coefficient = dc
[]
[source]
type = ArrayCoupledForce
variable = u
v = v
coef = '1 2'
block = 0
[]
[]
[DGKernels]
[surface]
type = ArrayHFEMDiffusion
variable = u
lowerd_variable = lambda
[]
[]
[BCs]
[all]
type = ArrayVacuumBC
boundary = 'left right top bottom'
variable = u
[]
[]
[Materials]
[dc]
type = GenericConstantArray
prop_name = dc
prop_value = '1 1'
[]
[]
[Postprocessors]
[intu]
type = ElementIntegralArrayVariablePostprocessor
variable = u
block = 0
[]
[lambdanorm]
type = ElementArrayL2Norm
variable = lambda
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu basic mumps'
[]
[Outputs]
[out]
# we hide lambda because it may flip sign due to element
# renumbering with distributed mesh
type = Exodus
hide = lambda
[]
csv = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-rc-no-slip-action.i)
mu=1.1
rho=1.1
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 10
ymin = -1
ymax = 1
nx = 100
ny = 20
[]
[]
[Modules]
[NavierStokesFV]
compressibility = 'incompressible'
porous_medium_treatment = false
add_energy_equation = false
density = 'rho'
dynamic_viscosity = 'mu'
initial_velocity = '1 1 0'
initial_pressure = 0.0
inlet_boundaries = 'left'
momentum_inlet_types = 'fixed-velocity'
momentum_inlet_function = '1 0'
wall_boundaries = 'top bottom'
momentum_wall_types = 'noslip noslip'
outlet_boundaries = 'right'
momentum_outlet_types = 'fixed-pressure'
pressure_function = '0'
[]
[]
[Materials]
[const]
type = ADGenericFunctorMaterial
prop_names = 'rho mu'
prop_values = '${rho} ${mu}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 200 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[]
(test/tests/outputs/common/console.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[AuxVariables]
[./aux0]
order = SECOND
family = SCALAR
[../]
[./aux1]
family = SCALAR
initial_condition = 5
[../]
[./aux2]
family = SCALAR
initial_condition = 10
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./diff_v]
type = CoefDiffusion
variable = v
coef = 2
[../]
[]
[BCs]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[./left_u]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = right
value = 3
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = left
value = 2
[../]
[]
[Postprocessors]
[./num_vars]
type = NumVars
system = 'NL'
[../]
[./num_aux]
type = NumVars
system = 'AUX'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
[]
[ICs]
[./aux0_IC]
variable = aux0
values = '12 13'
type = ScalarComponentIC
[../]
[]
(modules/heat_conduction/test/tests/conjugate_heat_transfer/conjugate_heat_transfer.i)
[Mesh]
type = FileMesh
file = simple_pb.e
[]
[Variables]
[./temp_wall]
block = 'left right'
[../]
[./temp_fluid]
block = 'center'
[../]
[]
[Kernels]
[./wall_conduction]
type = ADHeatConduction
variable = temp_wall
[../]
[./heat_source]
type = HeatSource
value = 1e3 # W/m^3
variable = temp_fluid
block = 'center'
[../]
[./center_conduction]
type = ADHeatConduction
variable = temp_fluid
block = 'center'
[../]
[]
[BCs]
[./right]
type = DirichletBC
variable = temp_wall
boundary = 'right'
value = 300
[../]
[./left]
type = DirichletBC
variable = temp_wall
boundary = 'left'
value = 100
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
[]
[Outputs]
exodus = true
csv = true
[]
[Materials]
[./walls]
type = ADHeatConductionMaterial
thermal_conductivity = 10 # W/m k
block = 'left right'
specific_heat = .49e3 # J/kg k
[../]
[./pb]
type = ADHeatConductionMaterial
thermal_conductivity = 1
specific_heat = .49e3 # J/kg K
block = 'center'
[../]
[./alpha_wall]
type = ADGenericConstantMaterial
prop_names = 'alpha_wall'
prop_values = '1'
block = 'center'
[../]
[]
[InterfaceKernels]
[./left_center_wrt_center]
type = ConjugateHeatTransfer
variable = temp_fluid
T_fluid = temp_fluid
neighbor_var = 'temp_wall'
boundary = 'left_center_wrt_center'
htc = 'alpha_wall'
[../]
[./right_center_wrt_center]
type = ConjugateHeatTransfer
variable = temp_fluid
T_fluid = temp_fluid
neighbor_var = 'temp_wall'
boundary = 'right_center_wrt_center'
htc = 'alpha_wall'
[../]
[]
[Preconditioning]
[./Hypre]
type = SMP
petsc_options_value = 'lu hypre'
full = true
petsc_options_iname = '-pc_type -pc_hypre_type'
[../]
[]
(test/tests/meshgenerators/sidesets_bounding_box_generator/error_no_elements_in_bounding_box.i)
[Mesh]
[./gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
#parallel_type = replicated
[]
[./createNewSidesetOne]
type = SideSetsFromBoundingBoxGenerator
input = gmg
boundary_id_old = 'left bottom'
boundary_id_new = 10
bottom_left = '-0.1 -0.1 0'
top_right = '0.8 0.2 0'
block_id = 0
[]
[./createNewSidesetTwo]
type = SideSetsFromBoundingBoxGenerator
input = createNewSidesetOne
boundary_id_old = 'right top'
boundary_id_new = 11
bottom_left = '1.7 0.7 0'
top_right = '2.1 1.1 0'
block_id = 0
[]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./leftBC]
type = DirichletBC
variable = u
boundary = 10
value = 1
[../]
[./rightBC]
type = DirichletBC
variable = u
boundary = 11
value = 0
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/variables/nemesis_hide.i)
# Solving for 2 variables, putting one into hide list and the other one into show list
# We should only see the variable that is in show list in the output.
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
elem_type = QUAD4
[]
# This should be the same as passing --distributed-mesh on the
# command line. You can verify this by looking at what MOOSE prints
# out for the "Mesh" information.
parallel_type = distributed
[./Partitioner]
type = LibmeshPartitioner
partitioner = linear
[../]
[]
[Functions]
[./fn_x]
type = ParsedFunction
value = x
[../]
[./fn_y]
type = ParsedFunction
value = y
[../]
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[AuxVariables]
[./aux_u]
[../]
[./aux_v]
[../]
[./proc_id]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[AuxKernels]
[./auxk_u]
type = FunctionAux
variable = aux_u
function = 'x*x+y*y'
[../]
[./auxk_v]
type = FunctionAux
variable = aux_v
function = '-(x*x+y*y)'
[../]
[./auxk_proc_id]
variable = proc_id
type = ProcessorIDAux
[../]
[]
[BCs]
[./u_bc]
type = FunctionDirichletBC
variable = u
boundary = '1 3'
function = fn_x
[../]
[./v_bc]
type = FunctionDirichletBC
variable = v
boundary = '0 2'
function = fn_y
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
console = true
[./out]
type = Nemesis
hide = 'u aux_v'
[../]
[]
(test/tests/partitioners/grid_partitioner/grid_partitioner.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[Partitioner]
type = GridPartitioner
nx = 2
ny = 2
nz = 1
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
[AuxVariables]
[pid]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[pid_aux]
type = ProcessorIDAux
variable = pid
execute_on = 'INITIAL'
[]
[]
(test/tests/preconditioners/pcside/diffusionCG.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = PenaltyDirichletBC
penalty = 1e9
variable = u
boundary = 3
value = 0
[../]
[./right]
type = PenaltyDirichletBC
penalty = 1e9
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_type -ksp_norm_type'
petsc_options_value = 'hypre boomeramg cg preconditioned'
# We are using preconditioned norm because of PenaltyDirichletBC
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/misc/check_error/missing_function_file_test.i)
# Test for usage of missing function
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = ic_function
[../]
[../]
[]
[Functions]
[./ic_function]
type = PiecewiseLinear
data_file = nonexistent_file #should generate error
scale_factor = 1.0
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/heat_conduction/test/tests/semiconductor_linear_conductivity/steinhart-hart_linear.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmax = 1.0
ymax = 1.0
[]
[Variables]
[./T]
initial_condition = 400.0 # unit in Kelvin only!!
[../]
[]
[AuxVariables]
[./elec_conduct]
order = FIRST
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = HeatConduction
variable = T
[../]
[]
[AuxKernels]
[./elec_conduct]
type = MaterialRealAux
variable = elec_conduct
property = electrical_conductivity
execute_on = timestep_end
[../]
[]
[BCs]
[./inlet]
type = DirichletBC
variable = T
boundary = left
value = 1000 # K
[../]
[./outlet]
type = DirichletBC
variable = T
boundary = right
value = 400 # K
[../]
[]
[Materials]
[./k]
type = GenericConstantMaterial
prop_names = 'thermal_conductivity'
prop_values = '10' # in W/mK
[../]
[./sigma]
type = SemiconductorLinearConductivity
temp = T
sh_coeff_A = 0.002
sh_coeff_B = 0.001
[../]
[]
[VectorPostprocessors]
[./line_sample]
type = LineValueSampler
warn_discontinuous_face_values = false
variable = 'T elec_conduct'
start_point = '0 0. 0'
end_point = '1.0 0. 0'
num_points = 11
sort_by = id
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
nl_rel_tol = 1e-12
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
execute_on = 'initial timestep_end'
csv = true
[]
(test/tests/meshgenerators/move_node_generator/test2.i)
[Mesh]
allow_renumbering=false
inactive = 'missingNode mismatchSize'
[./eg]
type = CartesianMeshGenerator
dim = 3
dx = '1'
dy = '1'
dz = '1'
ix = '4'
iy = '4'
iz = '4'
subdomain_id = '0'
[]
[modifyNode]
type = MoveNodeGenerator
input = eg
node_id = '0 1 2'
new_position = '0.1 0 0
0.35 0 0
0.6 0 0'
[]
[missingNode]
type = MoveNodeGenerator
input = eg
node_id = '999'
new_position = '0.1 0 0'
[]
[mismatchSize]
type = MoveNodeGenerator
input = eg
node_id = '0 1 2'
new_position = '0.1 0 0'
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/heat_conduction_ortho/heat_conduction_ortho.i)
#
# Three independent cubes are thermally loaded, one in x, one in y, and one in z.
# Each direction has a different thermal conductivity, resulting in a different
# temperature at the side with the Neumann bc.
#
# For x: 100/1000 = 1e-1
# For y: 100/100 = 1e+0
# for z: 100/10 = 1e+1
#
[Mesh]
file = heat_conduction_ortho.e
[]
[Variables]
[./temperature]
[../]
[]
[Kernels]
[./heat]
type = AnisoHeatConduction
variable = temperature
[../]
[]
[BCs]
[./temperatures]
type = DirichletBC
variable = temperature
boundary = 1
value = 0
[../]
[./neum]
type = NeumannBC
variable = temperature
boundary = 2
value = 100
[../]
[]
[Materials]
[./heat]
type = AnisoHeatConductionMaterial
block = 1
specific_heat = 0.116
thermal_conductivity = '10.0 0 0 0 10.0 0 0 0 10.0'
temperature = temperature
[../]
[./density]
type = GenericConstantMaterial
block = 1
prop_names = 'density'
prop_values = 0.283
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -ksp_gmres_restart'
petsc_options_value = 'lu 101'
line_search = 'none'
nl_abs_tol = 1e-11
nl_rel_tol = 1e-10
l_max_its = 20
[]
[Outputs]
exodus = true
hide = 'tcx tcy tcz'
[]
[Postprocessors]
[./tcx]
type = FunctionValuePostprocessor
function = 1000
outputs = none
execute_on = 'initial timestep_end'
[../]
[./tcy]
type = FunctionValuePostprocessor
function = 100
outputs = none
execute_on = 'initial timestep_end'
[../]
[./tcz]
type = FunctionValuePostprocessor
function = 10
outputs = none
execute_on = 'initial timestep_end'
[../]
[]
(modules/tensor_mechanics/test/tests/ad_action/two_block_no_action.i)
[Mesh]
[generated_mesh]
type = GeneratedMeshGenerator
dim = 2
nx = 4
ny = 4
[]
[block1]
type = SubdomainBoundingBoxGenerator
block_id = 1
bottom_left = '0 0 0'
top_right = '0.5 1 0'
input = generated_mesh
[]
[block2]
type = SubdomainBoundingBoxGenerator
block_id = 2
bottom_left = '0.5 0 0'
top_right = '1 1 0'
input = block1
[]
[]
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
# [Modules/TensorMechanics/Master]
# [./block1]
# strain = FINITE
# add_variables = true
# #block = 1
# use_automatic_differentiation = true
# [../]
# [./block2]
# strain = SMALL
# add_variables = true
# block = 2
# use_automatic_differentiation = true
# [../]
# []
[Kernels]
[./disp_x]
type = ADStressDivergenceTensors
variable = disp_x
component = 0
[../]
[./disp_y]
type = ADStressDivergenceTensors
variable = disp_y
component = 1
[../]
[]
[AuxVariables]
[./stress_theta]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_theta]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./stress_theta]
type = ADRankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 2
variable = stress_theta
execute_on = timestep_end
[../]
[./strain_theta]
type = ADRankTwoAux
rank_two_tensor = total_strain
index_i = 2
index_j = 2
variable = strain_theta
execute_on = timestep_end
[../]
[]
[Materials]
[./block_1]
type = ADComputeFiniteStrain
block = 1
[../]
[./block_2]
type = ADComputeSmallStrain
block = 2
[../]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1e10
poissons_ratio = 0.345
[../]
[./_elastic_stress1]
type = ADComputeFiniteStrainElasticStress
block = 1
[../]
[./_elastic_stress2]
type = ADComputeLinearElasticStress
block = 2
[../]
[]
[BCs]
[./left]
type = DirichletBC
boundary = 'left'
variable = disp_x
value = 0.0
[../]
[./top]
type = DirichletBC
boundary = 'top'
variable = disp_y
value = 0.0
[../]
[./right]
type = DirichletBC
boundary = 'right'
variable = disp_x
value = 0.01
[../]
[./bottom]
type = DirichletBC
boundary = 'bottom'
variable = disp_y
value = 0.01
[../]
[]
[Debug]
show_var_residual_norms = true
[]
[Preconditioning]
[./full]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = ' 201 hypre boomeramg 10'
line_search = 'none'
nl_rel_tol = 5e-9
nl_abs_tol = 1e-10
nl_max_its = 15
l_tol = 1e-3
l_max_its = 50
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/mixing_length_eddy_viscosity_aux/steady.i)
von_karman_const = 0.41
H = 1 #halfwidth of the channel
L = 150
Re = 100
rho = 1
bulk_u = 1
mu = ${fparse rho * bulk_u * 2 * H / Re}
advected_interp_method='upwind'
velocity_interp_method='rc'
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[Mesh]
[gen]
type = CartesianMeshGenerator
dim = 2
dx = '${L}'
dy = '0.667 0.333'
ix = '200'
iy = '10 1'
[]
[]
[Problem]
fv_bcs_integrity_check = false
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1e-6
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1e-6
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[AuxVariables]
[mixing_len]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[wall_shear_stress]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[wall_yplus]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[eddy_viscosity]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_viscosity_rans]
type = INSFVMixingLengthReynoldsStress
variable = u
rho = ${rho}
mixing_length = mixing_len
momentum_component = 'x'
u = u
v = v
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
momentum_component = 'y'
[]
[v_viscosity_rans]
type = INSFVMixingLengthReynoldsStress
variable = v
rho = ${rho}
mixing_length = mixing_len
momentum_component = 'y'
u = u
v = v
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[]
[AuxKernels]
[mixing_len]
type = WallDistanceMixingLengthAux
walls = 'top'
variable = mixing_len
execute_on = 'initial'
von_karman_const = ${von_karman_const}
delta = 0.5
[]
[turbulent_viscosity]
type = INSFVMixingLengthTurbulentViscosityAux
variable = eddy_viscosity
mixing_length = mixing_len
u = u
v = v
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = '0'
[]
[wall-u]
type = INSFVWallFunctionBC
variable = u
boundary = 'top'
u = u
v = v
mu = ${mu}
rho = ${rho}
momentum_component = x
[]
[wall-v]
type = INSFVWallFunctionBC
variable = v
boundary = 'top'
u = u
v = v
mu = ${mu}
rho = ${rho}
momentum_component = y
[]
[sym-u]
type = INSFVSymmetryVelocityBC
boundary = 'bottom'
variable = u
u = u
v = v
mu = ${mu}
momentum_component = x
[]
[sym-v]
type = INSFVSymmetryVelocityBC
boundary = 'bottom'
variable = v
u = u
v = v
mu = ${mu}
momentum_component = y
[]
[symmetry_pressure]
type = INSFVSymmetryPressureBC
boundary = 'bottom'
variable = pressure
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = '0'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 200 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(test/tests/meshgenerators/fancy_extruder_generator/need-neighbors.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
nx = 1
[]
[extrude]
type = FancyExtruderGenerator
input = gmg
heights = '1'
num_layers = '1'
direction = '0 1 0'
[]
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[bottom]
type = DirichletBC
variable = u
boundary = '0'
value = 0
[]
[top]
type = DirichletBC
variable = u
boundary = '1'
value = 1
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/kernels/anisotropic_diffusion/aniso_diffusion.i)
[Mesh]
file = mixed_block.e
uniform_refine=3
[]
[Functions]
[./top_bc]
type = ParsedFunction
value = 'x'
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = AnisotropicDiffusion
variable = u
tensor_coeff = '2 0 0
0 4 0
0 0 0'
[../]
[]
[BCs]
active = 'lower_left top'
[./lower_left]
type = DirichletBC
variable = u
boundary = '1 4'
value = 1
[../]
[./top]
type = FunctionNeumannBC
variable = u
boundary = 3
function = top_bc
[../]
[./right]
type = NeumannBC
variable = u
boundary = 2
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/kernels/material_coupled_force/material_coupled_force.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
nx = 10
ymin = 0
ymax = 2
ny = 10
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./v1]
initial_condition = 3
[../]
[./v2]
[../]
[]
[ICs]
[./v2_ic]
type = FunctionIC
variable = v2
function = v2_func
[../]
[]
[Functions]
[./v2_func]
type = ParsedFunction
value = 'x + 2 * y'
[../]
[./reference]
type = ParsedFunction
value = '3 * (-1) * 3.5 + (x + 2 * y) * 15 * 1.2'
[../]
[]
[Materials]
[./mat]
type = GenericConstantMaterial
prop_names = 'm1 m2'
prop_values = '-1 15'
[../]
[]
[Kernels]
[./reaction]
type = Reaction
variable = u
[../]
[./coupled]
type = MatCoupledForce
variable = u
v = 'v1 v2'
coef = '3.5 1.2'
material_properties = 'm1 m2'
[../]
[]
[Postprocessors]
[./error]
type = ElementL2Error
function = reference
variable = u
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/bad_second_order_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = SECOND
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/phase_field/test/tests/feature_volume_vpp_test/feature_volume_vpp_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 30
ny = 30
xmin = 0
xmax = 50
ymin = 0
ymax = 50
elem_type = QUAD4
[]
[Variables]
[c]
order = FIRST
family = LAGRANGE
[]
[]
[ICs]
[c]
type = LatticeSmoothCircleIC
variable = c
invalue = 1.0
outvalue = 0.0001
circles_per_side = '3 2'
pos_variation = 10.0
radius = 4.0
int_width = 5.0
radius_variation_type = uniform
avoid_bounds = false
[]
[]
[Postprocessors]
[./flood_count]
type = FeatureFloodCount
variable = c
# Must be turned out to build data structures necessary for FeatureVolumeVPP
compute_var_to_feature_map = true
threshold = 0.5
outputs = none
execute_on = INITIAL
[../]
[]
[VectorPostprocessors]
[./features]
type = FeatureVolumeVectorPostprocessor
flood_counter = flood_count
# Turn on centroid output
output_centroids = true
execute_on = INITIAL
[../]
[]
[Kernels]
[diff]
type = Diffusion
variable = c
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
execute_on = INITIAL
[]
(test/tests/misc/petsc_option_left/2d_diffusion_petsc_option.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
preset = false
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
preset = false
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options = "-options_left"
petsc_options_iname = "-pc_type"
petsc_options_value = "hypre"
[]
[Outputs]
exodus = true
[]
(modules/ray_tracing/test/tests/raykernels/function_integral_ray_kernel/function_integral_ray_kernel.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 5
ny = 5
xmax = 5
ymax = 5
[]
[]
[Functions/parsed_function]
type = ParsedFunction
value = 'x + sin(y)'
[]
[UserObjects/study]
type = RepeatableRayStudy
names = 'diag
top_across
bottom_across
partial'
start_points = '0 0 0
0 5 0
0 0 0
0.5 0.5 0'
end_points = '5 5 0
5 5 0
5 0 0
4.5 0.5 0'
[]
[RayKernels/function_integral]
type = FunctionIntegralRayKernel
function = parsed_function
rays = 'diag top_across bottom_across partial'
[]
[Postprocessors]
[diag_value]
type = RayIntegralValue
ray_kernel = function_integral
ray = diag
[]
[top_across_value]
type = RayIntegralValue
ray_kernel = function_integral
ray = top_across
[]
[bottom_across_value]
type = RayIntegralValue
ray_kernel = function_integral
ray = bottom_across
[]
[partial_value]
type = RayIntegralValue
ray_kernel = function_integral
ray = partial
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = false
csv = true
[]
(modules/richards/test/tests/jacobian_1/jn_fu_08.i)
# unsaturated = true
# gravity = true
# supg = true
# transient = false
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = -1
xmax = 1
ymin = -1
ymax = 1
zmin = -1
zmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGstandard
sat_UO = Saturation
seff_UO = SeffVG
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0 # notice small quantity, so the PETSc constant state works
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1 # notice small quantity, so the PETSc constant state works
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.2
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 0.1
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = RandomIC
block = 0
min = -1
max = 0
[../]
[../]
[]
[Kernels]
active = 'richardsf'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFullyUpwindFlux
variable = pressure
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
viscosity = 1E-3
gravity = '1 2 3'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -snes_type'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000 test'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = jn08
exodus = false
[]
(python/peacock/tests/input_tab/InputTreeWriter/gold/simple_diffusion.i)
[Mesh]
[generate]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[]
[]
[Executioner]
# Preconditioned JFNK (default)
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/porous_flow/test/tests/flux_limited_TVD_pflow/except03.i)
# Exception test: fe_family specified but not fe_order
[Mesh]
type = GeneratedMesh
dim = 1
[]
[GlobalParams]
gravity = '1 2 3'
PorousFlowDictator = dictator
[]
[Variables]
[pp]
[]
[tracer]
[]
[]
[Modules]
[FluidProperties]
[the_simple_fluid]
type = SimpleFluidProperties
[]
[]
[]
[PorousFlowUnsaturated]
porepressure = pp
mass_fraction_vars = tracer
fp = the_simple_fluid
[]
[UserObjects]
[advective_flux_calculator]
type = PorousFlowAdvectiveFluxCalculatorSaturated
fe_family = Lagrange
[]
[]
[Materials]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1 0 0 0 2 0 0 0 3'
[]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
(test/tests/samplers/base/mpi.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
ny = 1
[]
[Variables]
[./u]
[../]
[]
[Samplers]
[./sample]
type = TestSampler
execute_on = 'initial'
[../]
[]
[Postprocessors]
[./test]
type = SamplerTester
sampler = sample
test_type = MPI
[../]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
kernel_coverage_check = false
[]
[Outputs]
[]
(python/pyhit/tests/input.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
xmax = 3
[]
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = ADDiffusion
variable = u
[]
[]
[BCs]
[left]
type = ADDirichletBC
variable = u
boundary = left
value = 300
[]
[right]
type = ADNeumannBC
variable = u
boundary = right
value = 100
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
csv = true
[]
(test/tests/preconditioners/auto_smp/ad_coupled_convection.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 4
[]
[Variables]
[u][]
[v][]
[]
[Kernels]
[diff]
type = ADDiffusion
variable = u
[]
[convection]
type = ADCoupledConvection
variable = u
velocity_vector = v
scale = 100
[]
[diff_v]
type = ADDiffusion
variable = v
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
preset = false
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
preset = false
boundary = right
value = 1
[]
[left_v]
type = DirichletBC
variable = v
preset = false
boundary = left
value = 0
[]
[right_v]
type = DirichletBC
variable = v
preset = false
boundary = right
value = 1
[]
[]
[Preconditioning/smp]
# this block is part of what is being tested, see "tests" file
type = SMP
full = true
[]
[Executioner]
type = Steady
solve_type = NEWTON
nl_abs_tol = 1e-10 # needed to get non-preconditioned version to fail
auto_preconditioning = false # this is part of what is being tested, see "tests" file
[]
[Outputs]
exodus = true
[]
(modules/porous_flow/test/tests/gravity/grav01b.i)
# Checking that gravity head is established
# 1phase, vanGenuchten, constant and large fluid-bulk, constant viscosity, constant permeability, Corey relperm
# fully saturated
# For better agreement with the analytical solution (ana_pp), just increase nx
[Mesh]
type = GeneratedMesh
dim = 1
nx = 100
xmin = -1
xmax = 0
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Variables]
[pp]
[InitialCondition]
type = RandomIC
min = 0
max = 1
[]
[]
[]
[Kernels]
[flux0]
type = PorousFlowAdvectiveFlux
fluid_component = 0
variable = pp
gravity = '-1 0 0'
[]
[]
[Functions]
[ana_pp]
type = ParsedFunction
vars = 'g B p0 rho0'
vals = '1 1E3 0 1'
value = '-B*log(exp(-p0/B)+g*rho0*x/B)' # expected pp at base
[]
[]
[BCs]
[z]
type = DirichletBC
variable = pp
boundary = right
value = 0
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureVG
m = 0.5
alpha = 1
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 1e3
density0 = 1
viscosity = 1
thermal_expansion = 0
[]
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pp
capillary_pressure = pc
[]
[massfrac]
type = PorousFlowMassFraction
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1 0 0 0 2 0 0 0 3'
[]
[relperm]
type = PorousFlowRelativePermeabilityCorey
n = 1
phase = 0
[]
[]
[Postprocessors]
[pp_base]
type = PointValue
variable = pp
point = '-1 0 0'
[]
[pp_analytical]
type = FunctionValuePostprocessor
function = ana_pp
point = '-1 0 0'
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = grav01b
[csv]
type = CSV
[]
[]
(test/tests/bcs/ad_penalty_dirichlet_bc/penalty_dirichlet_bc_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 10
ny = 10
elem_type = QUAD9
[]
[Functions]
[./forcing_fn]
type = ParsedFunction
value = -2*(x*x+y*y-2)+(1-x*x)*(1-y*y)
[../]
[./solution]
type = ParsedGradFunction
value = (1-x*x)*(1-y*y)
grad_x = 2*(x*y*y-x)
grad_y = 2*(x*x*y-y)
[../]
[]
[Variables]
[./u]
order = SECOND
family = HIERARCHIC
[../]
[]
[Kernels]
active = 'diff forcing reaction'
[./diff]
type = ADDiffusion
variable = u
[../]
[./reaction]
type = Reaction
variable = u
[../]
[./forcing]
type = ADBodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
active = 'bc_all'
[./bc_all]
type = ADPenaltyDirichletBC
variable = u
value = 0
boundary = 'top left right bottom'
penalty = 1e5
[../]
[]
[Postprocessors]
[./dofs]
type = NumDOFs
[../]
[./h]
type = AverageElementSize
[../]
[./L2error]
type = ElementL2Error
variable = u
function = solution
[../]
[./H1error]
type = ElementH1Error
variable = u
function = solution
[../]
[./H1Semierror]
type = ElementH1SemiError
variable = u
function = solution
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
nl_rel_tol = 1e-14
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
csv = true
[]
(modules/phase_field/test/tests/reconstruction/EulerAngleVariables2RGBAux.i)
[Mesh]
[ebsd_mesh]
type = EBSDMeshGenerator
filename = IN100_001_28x28_Clean_Marmot.txt
[]
[]
[UserObjects]
[ebsd]
type = EBSDReader
[]
[]
[AuxVariables]
[phi1]
family = MONOMIAL
order = CONSTANT
[]
[phi]
family = MONOMIAL
order = CONSTANT
[]
[phi2]
family = MONOMIAL
order = CONSTANT
[]
[phase]
order = CONSTANT
family = MONOMIAL
[]
[symmetry]
order = CONSTANT
family = MONOMIAL
[]
[rgb]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[phi1_aux]
type = EBSDReaderPointDataAux
variable = phi1
ebsd_reader = ebsd
data_name = phi1
execute_on = initial
[]
[phi_aux]
type = EBSDReaderPointDataAux
variable = phi
ebsd_reader = ebsd
data_name = phi
execute_on = initial
[]
[phi2_aux]
type = EBSDReaderPointDataAux
variable = phi2
ebsd_reader = ebsd
data_name = phi2
execute_on = initial
[]
[phase_aux]
type = EBSDReaderPointDataAux
variable = phase
ebsd_reader = ebsd
data_name = phase
execute_on = initial
[]
[symmetry_aux]
type = EBSDReaderPointDataAux
variable = symmetry
ebsd_reader = ebsd
data_name = symmetry
execute_on = initial
[]
[rgb]
type = EulerAngleVariables2RGBAux
variable = rgb
phi1 = phi1
phi = phi
phi2 = phi2
phase = phase
symmetry = symmetry
execute_on = initial
[]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
kernel_coverage_check = false
[]
[Outputs]
exodus = true
show = 'rgb'
[]
(test/tests/markers/value_threshold_marker/value_threshold_marker_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
nz = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Adaptivity]
[./Markers]
[./marker]
type = ValueThresholdMarker
coarsen = 0.3
variable = u
refine = 0.7
[../]
[./inverted_marker]
type = ValueThresholdMarker
invert = true
coarsen = 0.7
refine = 0.3
variable = u
third_state = DO_NOTHING
[../]
[../]
[]
[Outputs]
exodus = true
[]
(test/tests/misc/jacobian/simple.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./s]
[../]
[./t]
[../]
[./u]
[../]
[./u2]
[../]
[./v]
[../]
[]
[AuxVariables]
[./w]
[../]
[]
[Kernels]
[./diffs]
type = WrongJacobianDiffusion
variable = s
jfactor = 0.995
[../]
[./difft]
type = WrongJacobianDiffusion
variable = t
jfactor = 2.0
[../]
[./diffu]
type = WrongJacobianDiffusion
variable = u
error = factor
jfactor = 0.0
[../]
[./diffu2]
type = WrongJacobianDiffusion
variable = u2
rfactor = 0.0
[../]
[./diffv]
type = Diffusion
variable = v
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
(test/tests/variables/fe_hermite_convergence/hermite_converge_dirichlet.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 4
ny = 4
elem_type = QUAD4
# This test will not work in parallel with DistributedMesh enabled
# due to a bug in PeriodicBCs.
parallel_type = replicated
[]
[Functions]
[./bc_fn]
type = ParsedGradFunction
value = -sin(pi*x)*sin(pi*y)
grad_x = -pi*cos(pi*x)*sin(pi*y)
grad_y = -pi*sin(pi*x)*cos(pi*y)
[../]
[./forcing_fn]
type = ParsedFunction
value = -2*pi*pi*sin(pi*x)*sin(pi*y)-sin(pi*x)*sin(pi*y)
[../]
[]
[Variables]
[./u]
order = THIRD
family = HERMITE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./reaction]
type = Reaction
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
[./all]
type = FunctionPenaltyDirichletBC
variable = u
boundary = 'bottom right top left'
function = bc_fn
penalty = 1e10
[../]
[]
[Postprocessors]
[./dofs]
type = NumDOFs
[../]
[./h]
type = AverageElementSize
[../]
[./L2error]
type = ElementL2Error
variable = u
function = bc_fn
[../]
[./H1error]
type = ElementH1Error
variable = u
function = bc_fn
[../]
[./H1Semierror]
type = ElementH1SemiError
variable = u
function = bc_fn
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
# We use higher-order quadrature to ensure that the forcing function
# is integrated accurately.
[./Quadrature]
order=ELEVENTH
[../]
[]
[Adaptivity]
steps = 2
marker = uniform
[./Markers]
[./uniform]
type = UniformMarker
mark = refine
[../]
[../]
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
csv = true
print_mesh_changed_info = true
[]
(modules/richards/test/tests/gravity_head_1/gh_fu_03.i)
# unsaturated = false
# gravity = true
# supg = false
# transient = false
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
xmin = -1
xmax = 1
[]
[BCs]
[./left]
type = DirichletBC
boundary = left
value = 1
variable = pressure
[../]
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGnone
sat_UO = Saturation
seff_UO = SeffVG
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0E3
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGnone]
type = RichardsSUPGnone
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = RandomIC
block = 0
min = 0
max = 1
[../]
[../]
[]
[Kernels]
active = 'richardsf'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFullyUpwindFlux
variable = pressure
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
viscosity = 1E-3
gravity = '-1 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = gh_fu_03
exodus = true
[]
(test/tests/fviks/diffusion/test.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 10
xmax = 2
[]
[subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '1.0 0 0'
block_id = 1
top_right = '2.0 1.0 0'
[]
[interface_primary]
input = subdomain1
type = SideSetsBetweenSubdomainsGenerator
primary_block = '0'
paired_block = '1'
new_boundary = 'primary_interface'
[]
[]
[Variables]
[u]
type = MooseVariableFVReal
block = 0
initial_condition = 0.5
[]
[v]
type = MooseVariableFVReal
block = 1
initial_condition = 0.5
[]
[]
[FVKernels]
[diff_left]
type = FVDiffusion
variable = u
coeff = 'left'
block = 0
[]
[gradient_creating]
type = FVBodyForce
variable = u
[]
[diff_right]
type = FVDiffusion
variable = v
coeff = 'right'
block = 1
[]
[gradient_creating_2]
type = FVBodyForce
variable = v
[]
[]
[FVInterfaceKernels]
[interface]
type = FVDiffusionInterface
variable1 = u
variable2 = v
boundary = 'primary_interface'
subdomain1 = '0'
subdomain2 = '1'
coeff1 = 'left'
coeff2 = 'right'
[]
[]
[FVBCs]
[left]
type = FVDirichletBC
variable = u
boundary = 'left'
value = 1
[]
[v_left]
type = FVDirichletBC
variable = v
boundary = 'right'
value = 0
[]
[]
[Materials]
[block0]
type = ADGenericFunctorMaterial
block = '0'
prop_names = 'left'
prop_values = '1'
[]
[block1]
type = ADGenericFunctorMaterial
block = '1'
prop_names = 'right'
prop_values = '1'
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(test/tests/mortar/aux-gap/gap.i)
[Mesh]
[file]
type = FileMeshGenerator
file = nodal_normals_test_offset_nonmatching_gap.e
[]
[primary]
input = file
type = LowerDBlockFromSidesetGenerator
sidesets = '2'
new_block_id = '20'
[]
[secondary]
input = primary
type = LowerDBlockFromSidesetGenerator
sidesets = '1'
new_block_id = '10'
[]
[]
[Variables]
[T]
block = '1 2'
[]
[lambda]
block = '10'
use_dual = true
[]
[]
[AuxVariables]
[gap]
block = '10'
[]
[]
[AuxKernels]
[gap]
type = WeightedGapAux
variable = gap
primary_boundary = 2
secondary_boundary = 1
primary_subdomain = 20
secondary_subdomain = 10
[]
[]
[BCs]
[neumann]
type = FunctionGradientNeumannBC
exact_solution = exact_soln
variable = T
boundary = '3 4 5 6 7 8'
[]
[]
[Kernels]
[conduction]
type = Diffusion
variable = T
block = '1 2'
[]
[sink]
type = Reaction
variable = T
block = '1 2'
[]
[forcing_function]
type = BodyForce
variable = T
function = forcing_function
block = '1 2'
[]
[]
[Functions]
[forcing_function]
type = ParsedFunction
value = '-4 + x^2 + y^2'
[]
[exact_soln]
type = ParsedFunction
value = 'x^2 + y^2'
[]
[]
[Debug]
show_var_residual_norms = 1
[]
[Constraints]
[mortar]
type = EqualValueConstraint
primary_boundary = 2
secondary_boundary = 1
primary_subdomain = 20
secondary_subdomain = 10
variable = lambda
secondary_variable = T
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
solve_type = NEWTON
type = Steady
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_shift_type -pc_factor_shift_amount'
petsc_options_value = 'lu basic NONZERO 1e-15'
[]
[Outputs]
exodus = true
[dofmap]
type = DOFMap
execute_on = 'initial'
[]
[]
(test/tests/kernels/jxw_grad_test_dep_on_displacements/jxw-cylindrical.i)
[GlobalParams]
displacements = 'disp_r disp_z'
order = SECOND
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 3
ny = 3
elem_type = QUAD9
[]
[Problem]
coord_type = RZ
[]
[Variables]
[./disp_r]
[../]
[./disp_z]
[../]
[./u]
order = FIRST
[../]
[./v]
[../]
[]
[Kernels]
[./disp_r]
type = Diffusion
variable = disp_r
[../]
[./disp_z]
type = Diffusion
variable = disp_z
[../]
[./u]
type = ADDiffusion
variable = u
use_displaced_mesh = true
[../]
[./v]
type = ADDiffusion
variable = v
use_displaced_mesh = true
[../]
[]
[BCs]
# BCs cannot be preset due to Jacobian tests
[./u_left]
type = DirichletBC
preset = false
value = 0
boundary = 'left'
variable = u
[../]
[./u_right]
type = DirichletBC
preset = false
value = 1
boundary = 'right'
variable = u
[../]
[./v_left]
type = DirichletBC
preset = false
value = 0
boundary = 'left'
variable = v
[../]
[./v_right]
type = DirichletBC
preset = false
value = 1
boundary = 'right'
variable = v
[../]
[./disp_r_left]
type = DirichletBC
preset = false
value = 0
boundary = 'left'
variable = disp_r
[../]
[./disp_r_right]
type = DirichletBC
preset = false
value = 1
boundary = 'right'
variable = disp_r
[../]
[./disp_z_left]
type = DirichletBC
preset = false
value = 0
boundary = 'bottom'
variable = disp_z
[../]
[./disp_z_right]
type = DirichletBC
preset = false
value = 1
boundary = 'top'
variable = disp_z
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
[./dofmap]
type = DOFMap
execute_on = 'initial'
[../]
exodus = true
[]
[ICs]
[./disp_r]
type = RandomIC
variable = disp_r
min = 0.01
max = 0.09
[../]
[./disp_z]
type = RandomIC
variable = disp_z
min = 0.01
max = 0.09
[../]
[./u]
type = RandomIC
variable = u
min = 0.1
max = 0.9
[../]
[./v]
type = RandomIC
variable = v
min = 0.1
max = 0.9
[../]
[]
(test/tests/controls/time_periods/error/steady_error.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = CoefDiffusion
variable = u
coef = 0.1
[../]
# The TimeDerivative existing in a Steady calculation will trigger an error itself!
# [./time]
# type = TimeDerivative
# variable = u
# [../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Dampers]
[./const_damp]
type = ConstantDamper
damping = 0.9
[../]
[]
[Outputs]
exodus = true
[]
[Controls]
[./damping_control]
type = TimePeriod
disable_objects = 'const_damp'
start_time = 0.25
execute_on = 'initial timestep_begin'
[../]
[]
(modules/heat_conduction/test/tests/fvbcs/fv_radiative_heat_flux/test.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 5
ny = 5
xmax = 2
[]
[]
[Variables]
[u]
type = MooseVariableFVReal
initial_condition = 0.5
[]
[]
[FVKernels]
[diff_left]
type = FVDiffusion
variable = u
coeff = 4
[]
[gradient_creating]
type = FVBodyForce
variable = u
[]
[]
[FVBCs]
[left]
type = FVInfiniteCylinderRadiativeBC
variable = u
boundary = 'left'
boundary_radius = 1
cylinder_radius = 12
cylinder_emissivity = 0.4
[]
[top]
type = FVInfiniteCylinderRadiativeBC
variable = u
# Test setting it separately
temperature = 'u'
boundary = 'top'
boundary_radius = 1
cylinder_radius = 12
cylinder_emissivity = 0.4
[]
[other]
type = FVDirichletBC
variable = u
boundary = 'right bottom'
value = 0
[]
[]
[Materials]
[cht]
type = ADGenericConstantMaterial
prop_names = 'htc'
prop_values = '1'
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(modules/richards/test/tests/jacobian_1/jn05.i)
# unsaturated = false
# gravity = false
# supg = true
# transient = false
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = -1
xmax = 1
ymin = -1
ymax = 1
zmin = -1
zmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0 # notice small quantity, so the PETSc constant state works
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1 # notice small quantity, so the PETSc constant state works
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.2
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 0.1
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = RandomIC
block = 0
min = 0
max = 1
[../]
[../]
[]
[Kernels]
active = 'richardsf'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGstandard
sat_UO = Saturation
seff_UO = SeffVG
viscosity = 1E-3
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -snes_type'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000 test'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = jn05
exodus = false
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_mortar/large_gap_heat_transfer_test_rz_cylinder.i)
rpv_core_gap_size = 0.2
core_outer_radius = 2
rpv_inner_radius = '${fparse 2 + rpv_core_gap_size}'
rpv_outer_radius = '${fparse 2.5 + rpv_core_gap_size}'
rpv_width = '${fparse rpv_outer_radius - rpv_inner_radius}'
rpv_outer_htc = 10 # W/m^2/K
rpv_outer_Tinf = 300 # K
core_blocks = '1'
rpv_blocks = '3'
[Mesh]
[gmg]
type = CartesianMeshGenerator
dim = 2
dx = '${core_outer_radius} ${rpv_core_gap_size} ${rpv_width}'
ix = '400 1 100'
dy = 1
iy = '5'
[]
[set_block_id1]
type = SubdomainBoundingBoxGenerator
input = gmg
bottom_left = '0 0 0'
top_right = '${core_outer_radius} 1 0'
block_id = 1
location = INSIDE
[]
[rename_core_bdy]
type = SideSetsBetweenSubdomainsGenerator
input = set_block_id1
primary_block = 1
paired_block = 0
new_boundary = 'core_outer'
[]
[set_block_id3]
type = SubdomainBoundingBoxGenerator
input = rename_core_bdy
bottom_left = '${rpv_inner_radius} 0 0'
top_right = '${rpv_outer_radius} 1 0'
block_id = 3
location = INSIDE
[]
[rename_inner_rpv_bdy]
type = SideSetsBetweenSubdomainsGenerator
input = set_block_id3
primary_block = 3
paired_block = 0
new_boundary = 'rpv_inner'
[]
# comment out for test without gap
[2d_mesh]
type = BlockDeletionGenerator
input = rename_inner_rpv_bdy
block = 0
[]
allow_renumbering = false
[]
[Problem]
coord_type = RZ
[]
[Variables]
[Tsolid]
initial_condition = 500
[]
[]
[Kernels]
[heat_source]
type = CoupledForce
variable = Tsolid
block = '${core_blocks}'
v = power_density
[]
[heat_conduction]
type = HeatConduction
variable = Tsolid
[]
[]
[BCs]
[RPV_out_BC] # k \nabla T = h (T- T_inf) at RPV outer boundary
type = ConvectiveFluxFunction # (Robin BC)
variable = Tsolid
boundary = 'right' # outer RPV
coefficient = ${rpv_outer_htc}
T_infinity = ${rpv_outer_Tinf}
[]
[]
[ThermalContact]
[RPV_gap]
type = GapHeatTransfer
gap_geometry_type = 'CYLINDER'
emissivity_primary = 0.8
emissivity_secondary = 0.8
variable = Tsolid
primary = 'core_outer'
secondary = 'rpv_inner'
gap_conductivity = 0.1
quadrature = true
[]
[]
[AuxVariables]
[power_density]
block = '${core_blocks}'
initial_condition = 50e3
[]
[]
[Materials]
[simple_mat]
type = HeatConductionMaterial
thermal_conductivity = 34.6 # W/m/K
[]
[]
[Postprocessors]
[Tcore_avg]
type = ElementAverageValue
variable = Tsolid
block = '${core_blocks}'
[]
[Tcore_max]
type = ElementExtremeValue
value_type = max
variable = Tsolid
block = '${core_blocks}'
[]
[Tcore_min]
type = ElementExtremeValue
value_type = min
variable = Tsolid
block = '${core_blocks}'
[]
[Trpv_avg]
type = ElementAverageValue
variable = Tsolid
block = '${rpv_blocks}'
[]
[Trpv_max]
type = ElementExtremeValue
value_type = max
variable = Tsolid
block = '${rpv_blocks}'
[]
[Trpv_min]
type = ElementExtremeValue
value_type = min
variable = Tsolid
block = '${rpv_blocks}'
[]
[ptot]
type = ElementIntegralVariablePostprocessor
variable = power_density
block = '${core_blocks}'
[]
[rpv_convective_out]
type = ConvectiveHeatTransferSideIntegral
T_solid = Tsolid
boundary = 'right' # outer RVP
T_fluid = ${rpv_outer_Tinf}
htc = ${rpv_outer_htc}
[]
[heat_balance] # should be equal to 0 upon convergence
type = ParsedPostprocessor
function = '(rpv_convective_out - ptot) / ptot'
pp_names = 'rpv_convective_out ptot'
[]
[flux_from_core] # converges to ptot as the mesh is refined
type = SideDiffusiveFluxIntegral
variable = Tsolid
boundary = core_outer
diffusivity = thermal_conductivity
[]
[flux_into_rpv] # converges to rpv_convective_out as the mesh is refined
type = SideDiffusiveFluxIntegral
variable = Tsolid
boundary = rpv_inner
diffusivity = thermal_conductivity
[]
[]
[VectorPostprocessors]
[NodalTemperature]
type = NodalValueSampler
sort_by = id
boundary = 'rpv_inner core_outer'
variable = Tsolid
[]
[]
[Executioner]
type = Steady
automatic_scaling = true
compute_scaling_once = false
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart '
petsc_options_value = 'hypre boomeramg 100'
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
l_max_its = 100
[Quadrature]
# order = fifth
side_order = seventh
[]
line_search = none
[]
[Outputs]
exodus = false
csv = true
[]
(test/tests/parser/param_substitution/param_substitution_in_file.i)
# Here we define a global parameter to be used for substitutions within this file
FILENAME = 'special_string'
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
# Here we use the GetPot "DBE" function to perform a substitution.
# The parameter "FILENAME" can either exist in this file or
# be provided on the CLI
file_base = out_${FILENAME}
[]
(python/chigger/tests/input/block_vars.i)
[Mesh]
[generator]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[subdomain1]
type = SubdomainBoundingBoxGenerator
input = generator
bottom_left = '0.5 0 0'
top_right = '1 1 0'
block_id = 1
[]
[]
[Variables]
[right_elemental]
block = 1
family = MONOMIAL
order = CONSTANT
[]
[right_nodal]
block = 1
[]
[]
[ICs]
[right_elemental]
type = FunctionIC
variable = right_elemental
function = 2*y
[]
[right_nodal]
type = FunctionIC
variable = right_nodal
function = 3*y
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/materials/material/material_block_bound_check.i)
###########################################################
# This is a simple test of the Material System. A
# user-defined Material (MTMaterial) is providing a
# Real property named "matp" that varies spatially
# throughout the domain. This property is used as a
# coefficient by MatDiffusionTest.
#
# This test verifies that when a material is restricted
# to a boundary, that MOOSE correctly reports that the
# volumetric material is missing.
###########################################################
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 4
ny = 4
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = MatDiffusionTest
variable = u
prop_name = matp
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 'left'
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = 'right'
value = 2
[../]
[]
# Materials System
[Materials]
[./mat]
type = MTMaterial
boundary = 'bottom'
[../]
[]
[Executioner]
type = Steady
[]
# No output, this test is designed to produce an error
(modules/heat_conduction/test/tests/heat_conduction/2d_quadrature_gap_heat_transfer/perfect.i)
[Mesh]
file = perfect.e
[]
[Variables]
[./temp]
[../]
[]
[Kernels]
[./hc]
type = HeatConduction
variable = temp
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = temp
boundary = leftleft
value = 300
[../]
[./right]
type = DirichletBC
variable = temp
boundary = rightright
value = 400
[../]
[]
[ThermalContact]
[./left_to_right]
secondary = leftright
quadrature = true
primary = rightleft
emissivity_primary = 0
emissivity_secondary = 0
variable = temp
type = GapHeatTransfer
[../]
[]
[Materials]
[./hcm]
type = HeatConductionMaterial
block = 'left right'
specific_heat = 1
thermal_conductivity = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(tutorials/darcy_thermo_mech/step02_darcy_pressure/problems/step2.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 100
ny = 10
xmax = 0.304 # Length of test chamber
ymax = 0.0257 # Test chamber radius
[]
[Variables/pressure]
[]
[Kernels]
[darcy_pressure]
type = DarcyPressure
variable = pressure
permeability = 0.8451e-9 # (m^2) 1mm spheres.
[]
[]
[BCs]
[inlet]
type = DirichletBC
variable = pressure
boundary = left
value = 4000 # (Pa) From Figure 2 from paper. First data point for 1mm spheres.
[]
[outlet]
type = DirichletBC
variable = pressure
boundary = right
value = 0 # (Pa) Gives the correct pressure drop from Figure 2 for 1mm spheres
[]
[]
[Problem]
type = FEProblem
coord_type = RZ
rz_coord_axis = X
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/heat_conduction/coupled_convective_heat_flux/coupled_convective_heat_flux_two_phase.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Functions]
[./alpha_liquid_fn]
type = ParsedFunction
value = 'sin(pi*y)'
[../]
[./T_infinity_liquid_fn]
type = ParsedFunction
value = '(x*x+y*y)+500'
[../]
[./Hw_liquid_fn]
type = ParsedFunction
value = '((1-x)*(1-x)+(1-y)*(1-y))+1000'
[../]
[./alpha_vapor_fn]
type = ParsedFunction
value = '1-sin(pi*y)'
[../]
[./T_infinity_vapor_fn]
type = ParsedFunction
value = '(x*x+y*y)+5'
[../]
[./Hw_vapor_fn]
type = ParsedFunction
value = '((1-x)*(1-x)+(1-y)*(1-y))+10'
[../]
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./T_infinity_liquid]
[../]
[./Hw_liquid]
[../]
[./alpha_liquid]
[../]
[./T_infinity_vapor]
[../]
[./Hw_vapor]
[../]
[./alpha_vapor]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./force]
type = BodyForce
variable = u
value = 1000
[../]
[]
[AuxKernels]
[./alpha_liquid_ak]
type = FunctionAux
variable = alpha_liquid
function = alpha_liquid_fn
execute_on = initial
[../]
[./T_infinity_liquid_ak]
type = FunctionAux
variable = T_infinity_liquid
function = T_infinity_liquid_fn
execute_on = initial
[../]
[./Hw_liquid_ak]
type = FunctionAux
variable = Hw_liquid
function = Hw_liquid_fn
execute_on = initial
[../]
[./alpha_vapor_ak]
type = FunctionAux
variable = alpha_vapor
function = alpha_vapor_fn
execute_on = initial
[../]
[./T_infinity_vapor_ak]
type = FunctionAux
variable = T_infinity_vapor
function = T_infinity_vapor_fn
execute_on = initial
[../]
[./Hw_vapor_ak]
type = FunctionAux
variable = Hw_vapor
function = Hw_vapor_fn
execute_on = initial
[../]
[]
[BCs]
[./right]
type = CoupledConvectiveHeatFluxBC
variable = u
boundary = right
alpha = 'alpha_liquid alpha_vapor'
htc = 'Hw_liquid Hw_vapor'
T_infinity = 'T_infinity_liquid T_infinity_vapor'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/controls/tag_based_naming_access/system_object_param.i)
[Mesh]
type = GeneratedMesh
dim = 2
elem_type = QUAD4
# use odd numbers so points do not fall on element boundaries
nx = 31
ny = 31
[]
[Variables]
[./diffused]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = diffused
[../]
[]
[DiracKernels]
[./test_object]
type = MaterialPointSource
point = '0.5 0.5 0'
variable = diffused
control_tags = 'tag'
[../]
[]
[BCs]
[./bottom_diffused]
type = DirichletBC
variable = diffused
boundary = 'bottom'
value = 2
[../]
[./top_diffused]
type = DirichletBC
variable = diffused
boundary = 'top'
value = 0
[../]
[]
[Materials]
[./mat]
type = GenericConstantMaterial
prop_names = 'matp'
prop_values = '1'
block = 0
[../]
[]
[Postprocessors]
[./test_object]
type = FunctionValuePostprocessor
function = '2*(x+y)'
point = '0.5 0.5 0'
[../]
[./other_point_test_object]
type = FunctionValuePostprocessor
function = '3*(x+y)'
point = '0.5 0.5 0'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
[Controls]
[./point_control]
type = TestControl
test_type = 'point'
parameter = 'tag/*/point'
execute_on = 'initial'
[../]
[]
(test/tests/misc/check_error/function_file_test7.i)
# Test for usage of missing function
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = ic_function
[../]
[../]
[]
[Functions]
[./ic_function]
type = PiecewiseLinear
x = '1'
scale_factor = 1.0
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/postprocessors/print_perf_data/print_perf_data.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Postprocessors]
[./elapsed]
type = PerfGraphData
section_name = "Root"
data_type = total
[../]
[./res_calls]
type = PerfGraphData
section_name = "FEProblem::computeResidualInternal"
data_type = calls
[../]
[./jac_calls]
type = PerfGraphData
section_name = "FEProblem::computeJacobianInternal"
data_type = calls
[../]
[./jac_total_time]
type = PerfGraphData
section_name = "FEProblem::computeJacobianInternal"
data_type = self
[../]
[./jac_average_time]
type = PerfGraphData
section_name = "FEProblem::computeJacobianInternal"
data_type = total_avg
[../]
[./jac_total_time_with_sub]
type = PerfGraphData
section_name = "FEProblem::computeJacobianInternal"
data_type = total
[../]
[./jac_average_time_with_sub]
type = PerfGraphData
section_name = "FEProblem::computeJacobianInternal"
data_type = total_avg
[../]
[./jac_percent_of_active_time]
type = PerfGraphData
section_name = "FEProblem::computeJacobianInternal"
data_type = self_percent
[../]
[./jac_percent_of_active_time_with_sub]
type = PerfGraphData
section_name = "FEProblem::computeJacobianInternal"
data_type = total_percent
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
csv = true
perf_graph = true
[]
(examples/ex14_pps/ex14.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 32
ny = 32
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
[]
[Variables]
[forced]
order = FIRST
family = LAGRANGE
[]
[]
[Functions]
# A ParsedFunction allows us to supply analytic expressions directly in the input file
[exact]
type = ParsedFunction
value = sin(alpha*pi*x)
vars = alpha
vals = 16
[]
# This function is an actual compiled function
[force]
type = ExampleFunction
alpha = 16
[]
[]
[Kernels]
[diff]
type = ADDiffusion
variable = forced
[]
# This Kernel can take a function name to use
[forcing]
type = ADBodyForce
variable = forced
function = force
[]
[]
[BCs]
# The BC can take a function name to use
[all]
type = FunctionDirichletBC
variable = forced
boundary = 'bottom right top left'
function = exact
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Postprocessors]
[h]
type = AverageElementSize
[]
[error]
type = ElementL2Error
variable = forced
function = exact
[]
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
csv = true
[]
(modules/navier_stokes/test/tests/finite_volume/fviks/convection/convection_channel.i)
mu = 1
rho = 1
k = .01
cp = 1
[Mesh]
[cmg]
type = CartesianMeshGenerator
dim = 2
dx = '1 0.5'
dy = '1'
ix = '8 5'
iy = '8'
subdomain_id = '0 1'
[]
[interface]
type = SideSetsBetweenSubdomainsGenerator
input = 'cmg'
primary_block = 0
paired_block = 1
new_boundary = 'interface'
[]
[fluid_side]
type = BreakBoundaryOnSubdomainGenerator
input = 'interface'
boundaries = 'top bottom'
[]
[]
[GlobalParams]
# retain behavior at time of test creation
two_term_boundary_expansion = false
rhie_chow_user_object = 'rc'
advected_interp_method = 'average'
velocity_interp_method = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
block = 0
pressure = pressure
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
block = 0
initial_condition = 1e-6
[]
[v]
type = INSFVVelocityVariable
block = 0
initial_condition = 1e-6
[]
[pressure]
type = INSFVPressureVariable
block = 0
[]
[T]
type = INSFVEnergyVariable
block = 0
initial_condition = 1
[]
[Ts]
type = INSFVEnergyVariable
block = 1
[]
[lambda]
family = SCALAR
order = FIRST
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
rho = ${rho}
[]
[mean_zero_pressure]
type = FVScalarLagrangeMultiplier
variable = pressure
lambda = lambda
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[temp_conduction]
type = FVDiffusion
coeff = 'k'
variable = T
[]
[temp_advection]
type = INSFVEnergyAdvection
variable = T
[]
[solid_temp_conduction]
type = FVDiffusion
coeff = 'k'
variable = Ts
[]
[]
[FVInterfaceKernels]
[convection]
type = FVConvectionCorrelationInterface
variable1 = T
variable2 = Ts
boundary = 'interface'
h = 5
temp_solid = Ts
temp_fluid = T
subdomain1 = 0
subdomain2 = 1
wall_cell_is_bulk = true
[]
[]
[FVBCs]
[walls_u]
type = INSFVNoSlipWallBC
variable = u
boundary = 'interface left'
function = 0
[]
[walls_v]
type = INSFVNoSlipWallBC
variable = v
boundary = 'interface left'
function = 0
[]
[inlet_u]
type = INSFVInletVelocityBC
variable = u
boundary = 'bottom_to_0'
function = 0
[]
[inlet_v]
type = INSFVInletVelocityBC
variable = v
boundary = 'bottom_to_0'
function = 1
[]
[inlet_T]
type = FVDirichletBC
variable = T
boundary = 'bottom_to_0'
value = 0.5
[]
[outlet]
type = INSFVMassAdvectionOutflowBC
variable = pressure
boundary = 'top_to_0'
u = u
v = v
rho = ${rho}
[]
[outlet_u]
type = INSFVMomentumAdvectionOutflowBC
variable = u
boundary = 'top_to_0'
u = u
v = v
momentum_component = 'x'
rho = ${rho}
[]
[outlet_v]
type = INSFVMomentumAdvectionOutflowBC
variable = v
boundary = 'top_to_0'
u = u
v = v
momentum_component = 'y'
rho = ${rho}
[]
[heater]
type = FVDirichletBC
variable = 'Ts'
boundary = 'right'
value = 10
[]
[]
[Materials]
[functor_constants]
type = ADGenericFunctorMaterial
prop_names = 'cp k'
prop_values = '${cp} ${k}'
[]
[ins_fv]
type = INSFVEnthalpyMaterial
temperature = 'T'
rho = ${rho}
block = 0
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_shift_type -ksp_gmres_restart'
petsc_options_value = 'asm lu NONZERO 200'
line_search = 'none'
nl_abs_tol = 1e-14
[]
[Postprocessors]
[max_T]
type = ElementExtremeValue
variable = T
block = 0
[]
[max_Ts]
type = ElementExtremeValue
variable = Ts
block = 1
[]
[mdot_out]
type = VolumetricFlowRate
boundary = 'top_to_0'
vel_x = u
vel_y = v
advected_quantity = ${rho}
[]
[]
[Outputs]
exodus = true
[]
(test/tests/functions/solution_function/solution_function_exodus_test.i)
# [Executioner]
# type = Steady
# petsc_options = '-snes'
# l_max_its = 800
# nl_rel_tol = 1e-10
# []
[Mesh]
type = FileMesh
file = cubesource.e
# This test uses SolutionUserObject which doesn't work with DistributedMesh.
parallel_type = replicated
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
initial_condition = 0.0
[../]
[]
[AuxVariables]
# [./ne]
# order = FIRST
# family = LAGRANGE
# [../]
# [./ee]
# order = CONSTANT
# family = MONOMIAL
# [../]
[./nn]
order = FIRST
family = LAGRANGE
[../]
[./en]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
# [./sourcee]
# type = SolutionFunction
# file_type = exodusII
# mesh = cubesource.e
# variable = source_element
# [../]
[./sourcen]
type = SolutionFunction
scale_factor = 2.0
solution = cube_soln
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
# [./ne]
# type = FunctionAux
# variable = ne
# function = sourcee
# [../]
# [./ee]
# type = FunctionAux
# variable = ee
# function = sourcee
# [../]
[./nn]
type = FunctionAux
variable = nn
function = sourcen
[../]
[./en]
type = FunctionAux
variable = en
function = sourcen
[../]
[]
[BCs]
[./stuff]
type = DirichletBC
variable = u
boundary = '1 2'
value = 0.0
[../]
[]
[UserObjects]
[./cube_soln]
type = SolutionUserObject
timestep = 2
system_variables = source_nodal
mesh = cubesource.e
[../]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
l_max_its = 800
nl_rel_tol = 1e-10
num_steps = 50
end_time = 5
dt = 0.5
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(modules/heat_conduction/test/tests/view_factors/view_factor_obstructed.i)
[Mesh]
[cartesian]
type = CartesianMeshGenerator
dim = 3
dx = '0.55 0.9 0.55'
dy = '0.55 0.9 0.55'
dz = '0.75 0.0001 0.25'
subdomain_id = '0 0 0
0 0 0
0 0 0
0 0 0
0 1 0
0 0 0
0 0 0
0 0 0
0 0 0'
[]
[side_set_around_obstruction]
type = SideSetsBetweenSubdomainsGenerator
input = cartesian
primary_block = 1
paired_block = 0
new_boundary = 'obstacle'
[]
[]
[UserObjects]
[view_factor_study]
type = ViewFactorRayStudy
execute_on = initial
boundary = 'left right top bottom front back obstacle'
face_order = FOURTH
polar_quad_order = 12
azimuthal_quad_order = 4
warn_subdomain_hmax = false
[]
[view_factor]
type = RayTracingViewFactor
boundary = 'left right top bottom front back obstacle'
execute_on = INITIAL
ray_study_name = view_factor_study
[]
[]
[RayBCs/viewfactor]
type = ViewFactorRayBC
boundary = 'left right top bottom front back obstacle'
[]
# Reference solution for front -> back view factor
# is 0.282833. This result is derived from analytical
# view factors from:
# front -> orthogonal sides around front [left right top bottom]
# front -> obstacle
# front -> everywhere must be sum to 1
#
[Postprocessors]
[front_back]
type = ViewFactorPP
from_boundary = front
to_boundary = back
view_factor_object_name = view_factor
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
[]
(test/tests/functions/linear_combination_function/lcf_vector.i)
# use the vectorValue of a LinearCombinationFunction
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
uniform_refine = 1
[]
[Variables]
[./u]
[../]
[]
[Functions]
[./conductivity_1]
type = ParsedVectorFunction
value_y = '0.1+x'
value_x = '0.5*(1+x*y)'
[../]
[./conductivity_2]
type = ParsedVectorFunction
value_y = '0.1+2*x'
value_x = '0.2+x*y'
[../]
[./conductivity]
type = LinearCombinationFunction # yields value_y=0.1, value_x=0.8
functions = 'conductivity_1 conductivity_2'
w = '2 -1'
[../]
[]
[Kernels]
[./diff]
type = DiffTensorKernel
variable = u
conductivity = conductivity
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./bottom]
type = DirichletBC
variable = u
boundary = bottom
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/common/exodus.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(test/tests/kernels/hfem/neumann.i)
[Mesh]
[square]
type = GeneratedMeshGenerator
nx = 3
ny = 3
dim = 2
[]
build_all_side_lowerd_mesh = true
[]
[Variables]
[u]
order = THIRD
family = MONOMIAL
block = 0
[]
[lambda]
order = CONSTANT
family = MONOMIAL
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
[]
[]
[Kernels]
[diff]
type = MatDiffusion
variable = u
diffusivity = '1'
block = 0
[]
[reaction]
type = Reaction
variable = u
rate = '1'
block = 0
[]
[source]
type = BodyForce
variable = u
value = '1'
block = 0
[]
[]
[DGKernels]
[surface]
type = HFEMDiffusion
variable = u
lowerd_variable = lambda
[]
[]
[BCs]
[all]
type = NeumannBC
boundary = 'left right top bottom'
variable = u
[]
[]
[Postprocessors]
[intu]
type = ElementIntegralVariablePostprocessor
variable = u
block = 0
[]
[lambdanorm]
type = ElementL2Norm
variable = lambda
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu basic mumps'
[]
[Outputs]
[out]
# we hide lambda because it may flip sign due to element
# renumbering with distributed mesh
type = Exodus
hide = lambda
[]
csv = true
[]
(test/tests/transfers/multiapp_conservative_transfer/primary_negative_adjuster.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[AuxVariables]
[var]
family = MONOMIAL
order = THIRD
[]
[]
[ICs]
[var_ic]
type = FunctionIC
variable = var
function = '-exp(x * y)'
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[MultiApps]
[sub]
type = FullSolveMultiApp
input_files = secondary_negative_adjuster.i
execute_on = timestep_end
[]
[]
[Postprocessors]
[from_postprocessor]
type = ElementIntegralVariablePostprocessor
variable = var
[]
[]
[Transfers]
[to_sub]
type = MultiAppMeshFunctionTransfer
source_variable = var
variable = var
to_multi_app = sub
from_postprocessors_to_be_preserved = 'from_postprocessor'
to_postprocessors_to_be_preserved = 'to_postprocessor'
[]
[]
[Outputs]
exodus = true
[]
(test/tests/restart/restart_transient_from_steady/steady_with_2subs.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
parallel_type = 'replicated'
[]
[AuxVariables]
[Tf]
[]
[]
[Variables]
[power_density]
[]
[]
[Functions]
[pwr_func]
type = ParsedFunction
value = '1e3*x*(1-x)+5e2'
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = power_density
[]
[coupledforce]
type = BodyForce
variable = power_density
function = pwr_func
[]
[]
[BCs]
[left]
type = DirichletBC
variable = power_density
boundary = left
value = 50
[]
[right]
type = DirichletBC
variable = power_density
boundary = right
value = 1e3
[]
[]
[Postprocessors]
[pwr_avg]
type = ElementAverageValue
variable = power_density
execute_on = 'initial timestep_end'
[]
[temp_avg]
type = ElementAverageValue
variable = Tf
execute_on = 'initial final'
[]
[temp_max]
type = ElementExtremeValue
value_type = max
variable = Tf
execute_on = 'initial final'
[]
[temp_min]
type = ElementExtremeValue
value_type = min
variable = Tf
execute_on = 'initial final'
[]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart '
petsc_options_value = 'hypre boomeramg 100'
nl_abs_tol = 1e-8
nl_rel_tol = 1e-12
fixed_point_rel_tol = 1E-7
fixed_point_abs_tol = 1.0e-07
fixed_point_max_its = 12
[]
[MultiApps]
[sub]
type = FullSolveMultiApp
app_type = MooseTestApp
positions = '0 0 0
0.5 0 0'
input_files = steady_with_sub_sub.i
execute_on = 'timestep_end'
[]
[]
[Transfers]
[p_to_sub]
type = MultiAppProjectionTransfer
source_variable = power_density
variable = power_density
to_multi_app = sub
execute_on = 'timestep_end'
[]
[t_from_sub]
type = MultiAppInterpolationTransfer
source_variable = temp
variable = Tf
from_multi_app = sub
execute_on = 'timestep_end'
[]
[]
[Outputs]
exodus = true
csv = true
perf_graph = true
checkpoint = true
execute_on = 'INITIAL TIMESTEP_END FINAL'
[]
(python/chigger/tests/input/simple_diffusion.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
uniform_refine = 2
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./aux]
family = MONOMIAL
order = CONSTANT
[../]
[]
[AuxKernels]
[./aux_kernel]
type = FunctionAux
variable = aux
function = sin(2*pi*x)*sin(2*pi*y)
execute_on = 'initial'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
# Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/geomsearch/nearest_node_locator/nearest_node_locator.i)
###########################################################
# This is a test of the Geometric Search System. This test
# uses the nearest node locator through the
# NearestNodeDistanceAux Auxilary Kernel to record the
# distance to the nearest nodes along paired
# boundaries.
#
# @Requirement F6.50
###########################################################
[Mesh]
file = 2dcontact_collide.e
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./distance]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./distance]
type = NearestNodeDistanceAux
variable = distance
boundary = 2
paired_boundary = 3
[../]
[]
[BCs]
[./block1_left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./block1_right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[./block2_left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./block2_right]
type = DirichletBC
variable = u
boundary = 4
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[./pgraph]
type = PerfGraphOutput
heaviest_branch = true
heaviest_sections = 5
level = 2
[../]
[]
(modules/reactor/test/tests/meshgenerators/reporting_id/depletion_id/depletion_id.i)
[Mesh]
[fmg]
type = FileMeshGenerator
file = depletion_id_in.e
exodus_extra_element_integers = 'material_id pin_id assembly_id'
[]
[depl_map]
type = DepletionIDGenerator
input = 'fmg'
id_name = 'assembly_id pin_id'
material_id_name = 'material_id'
[]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[AuxVariables]
[depletion_id]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[set_depletion_id]
type = ExtraElementIDAux
variable = depletion_id
extra_id_name = depletion_id
[]
[]
[Outputs]
exodus = true
execute_on = timestep_end
[]
(test/tests/variables/fe_hier/hier-1-3d.i)
[Mesh]
type = GeneratedMesh
dim = 3
xmin = -1
xmax = 1
ymin = -1
ymax = 1
zmin = -1
zmax = 1
nx = 5
ny = 5
elem_type = HEX8
[]
[Functions]
[./bc_fnt]
type = ParsedFunction
value = 1
[../]
[./bc_fnb]
type = ParsedFunction
value = -1
[../]
[./bc_fnl]
type = ParsedFunction
value = -1
[../]
[./bc_fnr]
type = ParsedFunction
value = 1
[../]
[./bc_fnf]
type = ParsedFunction
value = 1
[../]
[./bc_fnk]
type = ParsedFunction
value = -1
[../]
[./forcing_fn]
type = ParsedFunction
value = x+y+z
[../]
[./solution]
type = ParsedGradFunction
value = x+y+z
grad_x = 1
grad_y = 1
grad_z = 1
[../]
[]
[Variables]
[./u]
order = FIRST
family = HIERARCHIC
[../]
[]
[Kernels]
active = 'diff forcing reaction'
[./diff]
type = Diffusion
variable = u
[../]
[./reaction]
type = Reaction
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
[./bc_top]
type = FunctionNeumannBC
variable = u
boundary = 'top'
function = bc_fnt
[../]
[./bc_bottom]
type = FunctionNeumannBC
variable = u
boundary = 'bottom'
function = bc_fnb
[../]
[./bc_left]
type = FunctionNeumannBC
variable = u
boundary = 'left'
function = bc_fnl
[../]
[./bc_right]
type = FunctionNeumannBC
variable = u
boundary = 'right'
function = bc_fnr
[../]
[./bc_front]
type = FunctionNeumannBC
variable = u
boundary = 'front'
function = bc_fnf
[../]
[./bc_back]
type = FunctionNeumannBC
variable = u
boundary = 'back'
function = bc_fnk
[../]
[]
[Postprocessors]
[./dofs]
type = NumDOFs
[../]
[./h]
type = AverageElementSize
[../]
[./L2error]
type = ElementL2Error
variable = u
function = solution
[../]
[./H1error]
type = ElementH1Error
variable = u
function = solution
[../]
[./H1Semierror]
type = ElementH1SemiError
variable = u
function = solution
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
csv = true
[]
(modules/ray_tracing/test/tests/raykernels/variable_integral_ray_kernel/fv_simple_diffusion_line_integral.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmax = 10
ymax = 10
[]
[Variables/v]
family = MONOMIAL
order = CONSTANT
fv = true
[]
[FVKernels/diff]
type = FVDiffusion
variable = v
coeff = coeff
[]
[FVBCs]
[left]
type = FVDirichletBC
variable = v
boundary = left
value = 7
[]
[right]
type = FVDirichletBC
variable = v
boundary = right
value = 42
[]
[top_bottom]
type = FVDirichletBC
variable = v
boundary = 'top bottom'
value = 1
[]
[]
[Materials/diff]
type = ADGenericFunctorMaterial
prop_names = 'coeff'
prop_values = '1'
[]
[UserObjects/study]
type = RepeatableRayStudy
names = 'diag
right_up'
start_points = '0 0 0
10 0 0'
end_points = '10 10 0
10 10 0'
[]
[RayKernels/v_integral]
type = VariableIntegralRayKernel
study = study
variable = v
[]
[Postprocessors]
[diag_line_integral]
type = RayIntegralValue
ray_kernel = v_integral
ray = diag
[]
[right_up_line_integral]
type = RayIntegralValue
ray_kernel = v_integral
ray = right_up
[]
[]
[Problem]
kernel_coverage_check = false
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
csv = true
exodus = false
[]
(test/tests/mesh/stitched_mesh/stitched_mesh.i)
[Mesh]
type = StitchedMesh
files = 'left.e center.e right.e'
stitch_boundaries = 'right left right left'
parallel_type = 'replicated'
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/kernels/array_kernels/array_diffusion_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 4
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
components = 2
scaling = '.9 .9'
[]
[]
[Kernels]
[diff]
type = ArrayDiffusion
variable = u
diffusion_coefficient = dc
[]
[]
[BCs]
[left]
type = ArrayDirichletBC
variable = u
boundary = 1
values = '0 0'
[]
[right]
type = ArrayDirichletBC
variable = u
boundary = 2
values = '1 2'
[]
[]
[Materials]
[dc]
type = GenericConstantArray
prop_name = dc
prop_value = '1 1'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(test/tests/variables/array_variable/array_variable_size_one_test.i)
[Mesh]
[square]
type = GeneratedMeshGenerator
nx = 3
ny = 3
dim = 2
[]
[]
[Variables]
[u]
order = FIRST
family = MONOMIAL
components = 1
array = true
[]
[]
[Kernels]
[diff]
type = ArrayDiffusion
variable = u
diffusion_coefficient = dc
[]
[reaction]
type = ArrayReaction
variable = u
reaction_coefficient = rc
[]
[source]
type = ArrayBodyForce
variable = u
function = '1'
[]
[]
[BCs]
[all]
type = ArrayVacuumBC
boundary = 'left right top bottom'
variable = u
[]
[]
[Materials]
[dc]
type = GenericConstantArray
prop_name = dc
prop_value = '1'
[]
[rc]
type = GenericConstantArray
prop_name = rc
prop_value = '2'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
[out]
type = Exodus
[]
[]
(test/tests/mesh/patterned_mesh/mesh_tester.i)
[Mesh]
type = FileMesh
file = patterned_mesh_in.e
dim = 2
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = MatCoefDiffusion
variable = u
conductivity = conductivity
[../]
[]
[BCs]
[./top]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[./bottom]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Materials]
[./mat1]
type = GenericConstantMaterial
block = 1
prop_names = conductivity
prop_values = 100
[../]
[./mat2]
type = GenericConstantMaterial
block = 2
prop_names = conductivity
prop_values = 1e-4
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/misc/block_boundary_material_check/dgkernel_check_boundary.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Variables]
[./u]
[../]
[]
[DGKernels]
[./dg]
type = MatDGKernel
mat_prop = 'foo'
variable = u
boundary = 1
[../]
[]
[Problem]
type = FEProblem
solve = false
kernel_coverage_check = false
[]
[Executioner]
type = Steady
[]
[Outputs]
[]
(test/tests/outputs/hide_via_reporters_block/reporter.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Problem]
solve = false
kernel_coverage_check = false
[]
[Reporters]
[day]
type = ConstantReporter
integer_names = day
integer_values = 24
[]
[month]
type = ConstantReporter
integer_names = month
integer_values = 6
outputs = none
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
[out]
type = JSON
execute_system_information_on = None
[]
[]
(test/tests/markers/dont_mark/dont_mark_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
nz = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Adaptivity]
[./Markers]
[./box]
type = BoxMarker
bottom_left = '0.3 0.3 0'
top_right = '0.6 0.6 0'
inside = refine
outside = coarsen
[../]
[./combo]
type = ComboMarker
markers = 'box box2'
[../]
[./box2]
type = BoxMarker
bottom_left = '0.5 0.5 0'
top_right = '0.8 0.8 0'
inside = dont_mark
outside = refine
[../]
[../]
[]
[Outputs]
exodus = true
[]
(test/tests/actions/debug_show_reporters/debug_show_reporters.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
[]
[]
[Postprocessors]
[scale]
type = ScalePostprocessor
value = function
scaling_factor = 2
[]
[function]
type = FunctionValuePostprocessor
function = 1
[]
[]
[VectorPostprocessors/constant_vpp]
type = ConstantVectorPostprocessor
vector_names = 'value1 value2'
value = '1; 2'
[]
[Reporters/constant_reporter]
type = ConstantReporter
integer_names = integer
integer_values = 1
real_names = real
real_values = 2
string_names = string
string_values = 'funny'
[]
[Debug]
show_reporters = true
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
(modules/navier_stokes/test/tests/auxkernels/peclet-number-functor-aux/fv-thermal.i)
mu = 1
rho = 1
k = 1
cp = 1
[GlobalParams]
velocity_interp_method = 'rc'
# Maximum cell Peclet number is ~.1 so energy transport is stable without upwinding
advected_interp_method = 'average'
rhie_chow_user_object = 'rc'
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
[]
[v]
type = INSFVVelocityVariable
[]
[pressure]
type = INSFVPressureVariable
[]
[T]
type = INSFVEnergyVariable
[]
[lambda]
family = SCALAR
order = FIRST
[]
[]
[AuxVariables]
[Pe]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[Pe]
type = PecletNumberFunctorAux
variable = Pe
speed = speed
thermal_diffusivity = 'thermal_diffusivity'
[]
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
rho = ${rho}
[]
[mean_zero_pressure]
type = FVScalarLagrangeMultiplier
variable = pressure
lambda = lambda
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = 'mu'
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = 'mu'
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[temp_conduction]
type = FVDiffusion
coeff = ${k}
variable = T
[]
[temp_advection]
type = INSFVEnergyAdvection
variable = T
[]
[]
[FVBCs]
[top_x]
type = INSFVNoSlipWallBC
variable = u
boundary = 'top'
function = 1
[]
[no_slip_x]
type = INSFVNoSlipWallBC
variable = u
boundary = 'left right bottom'
function = 0
[]
[no_slip_y]
type = INSFVNoSlipWallBC
variable = v
boundary = 'left right top bottom'
function = 0
[]
[T_hot]
type = FVDirichletBC
variable = T
boundary = 'bottom'
value = 1
[]
[T_cold]
type = FVDirichletBC
variable = T
boundary = 'top'
value = 0
[]
[]
[Materials]
[mu]
type = ADGenericFunctorMaterial
prop_names = 'mu'
prop_values = '${mu}'
[]
[speed]
type = ADVectorMagnitudeFunctorMaterial
x_functor = u
y_functor = v
vector_magnitude_name = speed
[]
[thermal_diffusivity]
type = ThermalDiffusivityFunctorMaterial
k = ${k}
rho = ${rho}
cp = ${cp}
[]
[enthalpy]
type = INSFVEnthalpyMaterial
rho = ${rho}
temperature = T
cp = ${cp}
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(test/tests/auxkernels/nodal_aux_boundary/nodal_aux_boundary.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./aux]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./boundary_aux]
type = CoupledAux
variable = aux
value = 2
coupled = u
boundary = top
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/kernels/hfem/array_dirichlet_pjfnk.i)
[Mesh]
[square]
type = GeneratedMeshGenerator
nx = 3
ny = 3
dim = 2
[]
build_all_side_lowerd_mesh = true
[]
[Variables]
[u]
order = THIRD
family = MONOMIAL
block = 0
components = 2
[]
[lambda]
order = CONSTANT
family = MONOMIAL
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
components = 2
[]
[lambdab]
order = CONSTANT
family = MONOMIAL
block = BOUNDARY_SIDE_LOWERD_SUBDOMAIN
components = 2
[]
[]
[AuxVariables]
[v]
order = CONSTANT
family = MONOMIAL
block = 0
initial_condition = '1'
[]
[]
[Kernels]
[diff]
type = ArrayDiffusion
variable = u
block = 0
diffusion_coefficient = dc
[]
[reaction]
type = ArrayReaction
variable = u
block = 0
reaction_coefficient = re
[]
[source]
type = ArrayCoupledForce
variable = u
v = v
coef = '1 2'
block = 0
[]
[]
[DGKernels]
[surface]
type = ArrayHFEMDiffusionTest
variable = u
lowerd_variable = lambda
for_pjfnk = true
[]
[]
[BCs]
[all]
type = ArrayHFEMDirichletTestBC
boundary = 'left right top bottom'
variable = u
lowerd_variable = lambdab
for_pjfnk = true
[]
[]
[Materials]
[dc]
type = GenericConstantArray
prop_name = dc
prop_value = '1 1'
[]
[re]
type = GenericConstantArray
prop_name = re
prop_value = '0.1 0.1'
[]
[]
[Postprocessors]
[intu]
type = ElementIntegralArrayVariablePostprocessor
variable = u
block = 0
[]
[lambdanorm]
type = ElementArrayL2Norm
variable = lambda
block = INTERNAL_SIDE_LOWERD_SUBDOMAIN
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
[out]
# we hide lambda because it may flip sign due to element
# renumbering with distributed mesh
type = Exodus
hide = lambda
[]
csv = true
[]
(modules/tensor_mechanics/test/tests/isotropic_elasticity_tensor/bulk_modulus_shear_modulus_test.i)
[Mesh]
type = GeneratedMesh
dim = 3
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[AuxVariables]
[./stress_11]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
add_variables = true
[../]
[]
[AuxKernels]
[./stress_11]
type = RankTwoAux
variable = stress_11
rank_two_tensor = stress
index_j = 1
index_i = 1
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0
[../]
[./left]
type = DirichletBC
variable = disp_x
boundary = left
value = 0
[../]
[./back]
type = DirichletBC
variable = disp_z
boundary = back
value = 0
[../]
[./top]
type = DirichletBC
variable = disp_y
boundary = top
value = 0.001
[../]
[]
[Materials]
[./stress]
type = ComputeLinearElasticStress
[../]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
bulk_modulus = 416666
shear_modulus = 454545
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
l_max_its = 20
nl_max_its = 10
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(modules/porous_flow/test/tests/flux_limited_TVD_pflow/except04.i)
# Exception test: fe_order specified but not fe_family
[Mesh]
type = GeneratedMesh
dim = 1
[]
[GlobalParams]
gravity = '1 2 3'
PorousFlowDictator = dictator
[]
[Variables]
[pp]
[]
[tracer]
[]
[]
[Modules]
[FluidProperties]
[the_simple_fluid]
type = SimpleFluidProperties
[]
[]
[]
[PorousFlowUnsaturated]
porepressure = pp
mass_fraction_vars = tracer
fp = the_simple_fluid
[]
[UserObjects]
[advective_flux_calculator]
type = PorousFlowAdvectiveFluxCalculatorSaturated
fe_order = First
[]
[]
[Materials]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1 0 0 0 2 0 0 0 3'
[]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
(test/tests/mesh/subdomain_partitioner/subdomain_partitioner.i)
[Mesh]
[file]
type = FileMeshGenerator
file = test_subdomain_partitioner.e
[]
[./Partitioner]
type = LibmeshPartitioner
partitioner = subdomain_partitioner
blocks = '1 2 3 4; 1001 1002 1003 1004'
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./proc_id]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./proc_id]
type = ProcessorIDAux
variable = proc_id
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = subdomain_partitioner_out
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[]
(modules/porous_flow/examples/flow_through_fractured_media/fine_thick_fracture_steady.i)
# Using a single-dimensional mesh
# Steady-state porepressure distribution along a fracture in a porous matrix
# This is used to initialise the transient solute-transport simulation
[Mesh]
type = FileMesh
# The gold mesh is used to reduce the number of large files in the MOOSE repository.
# The porepressure is not read from the gold mesh
file = 'gold/fine_thick_fracture_steady_out.e'
block_id = '1 2 3'
block_name = 'fracture matrix1 matrix2'
boundary_id = '1 2'
boundary_name = 'bottom top'
[]
[GlobalParams]
PorousFlowDictator = dictator
gravity = '0 0 0'
[]
[Variables]
[pp]
[]
[]
[ICs]
[pp]
type = ConstantIC
variable = pp
value = 1e6
[]
[]
[BCs]
[ptop]
type = DirichletBC
variable = pp
boundary = top
value = 1e6
[]
[pbottom]
type = DirichletBC
variable = pp
boundary = bottom
value = 1.002e6
[]
[]
[Kernels]
[adv0]
type = PorousFlowAdvectiveFlux
fluid_component = 0
variable = pp
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 2e9
density0 = 1000
thermal_expansion = 0
viscosity = 1e-3
[]
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow1PhaseFullySaturated
porepressure = pp
[]
[massfrac]
type = PorousFlowMassFraction
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[relp]
type = PorousFlowRelativePermeabilityConst
phase = 0
[]
[permeability1]
type = PorousFlowPermeabilityConst
permeability = '3e-8 0 0 0 3e-8 0 0 0 3e-8' # the true permeability is used without scaling by aperture
block = 'fracture'
[]
[permeability2]
type = PorousFlowPermeabilityConst
permeability = '1e-20 0 0 0 1e-20 0 0 0 1e-20'
block = 'matrix1 matrix2'
[]
[]
[Preconditioning]
active = basic
[mumps_is_best_for_parallel_jobs]
type = SMP
full = true
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu mumps'
[]
[basic]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -sub_pc_factor_shift_type -pc_asm_overlap'
petsc_options_value = 'gmres asm lu NONZERO 2 '
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
# controls for nonlinear iterations
nl_abs_tol = 1e-9
nl_rel_tol = 1e-10
[]
[Outputs]
exodus = true
execute_on = 'timestep_end'
[]
(test/tests/materials/material_dependency/diff_kernel_aux_mat_dep.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = MatDiffusionTest
variable = u
prop_name = 'diff'
[../]
[]
[AuxKernels]
[./error]
type = ElementLpNormAux
variable = error
coupled_variable = u
[../]
[]
[AuxVariables]
[./error]
family = MONOMIAL
order = FIRST
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
preset = false
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
preset = false
boundary = right
value = 1
[../]
[]
[Materials]
[./call_me_mat]
type = IncrementMaterial
prop_names = 'diff'
prop_values = '1'
block = 0
outputs = exodus
output_properties = 'mat_prop'
[../]
[]
[Executioner]
type = Steady
# This test counts the number of residual evaluations that
# may slightly change from a PETSc version to another.
# For instance, starts from PETSc-3.8.4, the number of
# residual evaluating is reduced by one in a linear solver
# for each Newton iteration. This change causes this test
# fail. It better to restrict the test
# count the residual evaluations in the nonlinear level only.
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
[]
[Outputs]
exodus = true
[]
(modules/reactor/test/tests/meshgenerators/coarse_mesh_extra_element_id_generator/coarse_elem_id.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 8
ymin = 0
ymax = 8
nx = 8
ny = 8
[]
[coarse_mesh]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 8
ymin = 0
ymax = 8
nx = 3
ny = 3
[]
[coarse_id]
type = CoarseMeshExtraElementIDGenerator
input = gmg
coarse_mesh = coarse_mesh
extra_element_id_name = coarse_elem_id
enforce_mesh_embedding = false
[]
# need this to ensure consistent numbering of the coarse mesh when using a distributed mesh
allow_renumbering = false
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[AuxVariables]
[coarse_elem_id]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[coarse_elem_id]
type = ExtraElementIDAux
variable = coarse_elem_id
extra_id_name = coarse_elem_id
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/deprecated_param_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./nan]
type = NanKernel
variable = u
timestep_to_nan = 1000
[../]
[]
[BCs]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/mesh_modifiers/assign_element_subdomain_id/tri_with_subdomainid_test.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 2
nz = 0
zmin = 0
zmax = 0
elem_type = TRI3
[]
[subdomain_id]
type = ElementSubdomainIDGenerator
input = gen
subdomain_ids = '0 1 1 1
1 1 1 0'
[]
[]
[Variables]
active = 'u'
[u]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
active = 'diff'
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
active = 'left right'
# Mesh Generation produces boundaries in counter-clockwise fashion
[left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out_tri_subdomain_id
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/2d-rc-friction-action.i)
mu=1.1
rho=1
[Mesh]
[mesh]
type = CartesianMeshGenerator
dim = 2
dx = '2.5 2.5'
dy = '1.0'
ix = '20 20'
iy = '20'
subdomain_id = '1 2'
[]
[]
[Modules]
[NavierStokesFV]
compressibility = 'incompressible'
porous_medium_treatment = true
density = 'rho'
dynamic_viscosity = 'mu'
porosity = 'porosity'
initial_velocity = '1 1e-6 0'
initial_pressure = 0.0
inlet_boundaries = 'left'
momentum_inlet_types = 'fixed-velocity'
momentum_inlet_function = '1 0'
wall_boundaries = 'top bottom'
momentum_wall_types = 'noslip symmetry'
outlet_boundaries = 'right'
momentum_outlet_types = 'fixed-pressure'
pressure_function = '0'
friction_types = 'darcy forchheimer'
friction_coeffs = 'Darcy_coefficient Forchheimer_coefficient'
[]
[]
[Materials]
[const]
type = ADGenericFunctorMaterial
prop_names = 'rho mu'
prop_values = '${rho} ${mu}'
[]
[friction]
type = ADGenericVectorFunctorMaterial
prop_names = 'Darcy_coefficient Forchheimer_coefficient'
prop_values = '0.1 0.1 0.1 0.1 0.1 0.1'
[]
[]
[AuxVariables]
[porosity]
family = MONOMIAL
order = CONSTANT
fv = true
initial_condition = 0.5
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 200 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-11
nl_abs_tol = 1e-14
[]
# Some basic Postprocessors to visually examine the solution
[Postprocessors]
[inlet-p]
type = SideIntegralVariablePostprocessor
variable = pressure
boundary = 'left'
[]
[outlet-u]
type = SideIntegralVariablePostprocessor
variable = superficial_vel_x
boundary = 'right'
[]
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/action/no_block.i)
[Mesh]
[generated_mesh]
type = GeneratedMeshGenerator
dim = 2
nx = 4
ny = 4
[]
[block1]
type = SubdomainBoundingBoxGenerator
block_id = 1
bottom_left = '0 0 0'
top_right = '0.5 1 0'
input = generated_mesh
[]
[block2]
type = SubdomainBoundingBoxGenerator
block_id = 2
bottom_left = '0.5 0 0'
top_right = '1 1 0'
input = block1
[]
[]
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Modules/TensorMechanics/Master]
# parameters that apply to all subblocks are specified at this level. But
# no subblocks are present. This should trigger a warning.
add_variables = true
strain = FINITE
generate_output = 'stress_xx'
[]
[AuxVariables]
[./stress_theta]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_theta]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./stress_theta]
type = RankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 2
variable = stress_theta
execute_on = timestep_end
[../]
[./strain_theta]
type = RankTwoAux
rank_two_tensor = total_strain
index_i = 2
index_j = 2
variable = strain_theta
execute_on = timestep_end
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e10
poissons_ratio = 0.345
[../]
[./_elastic_stress1]
type = ComputeFiniteStrainElasticStress
block = 1
[../]
[./_elastic_stress2]
type = ComputeFiniteStrainElasticStress
block = 2
[../]
[]
[BCs]
[./left]
type = DirichletBC
boundary = 'left'
variable = disp_x
value = 0.0
[../]
[./top]
type = DirichletBC
boundary = 'top'
variable = disp_y
value = 0.0
[../]
[./right]
type = DirichletBC
boundary = 'right'
variable = disp_x
value = 0.01
[../]
[./bottom]
type = DirichletBC
boundary = 'bottom'
variable = disp_y
value = 0.01
[../]
[]
[Debug]
show_var_residual_norms = true
[]
[Executioner]
type = Steady
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = ' 201 hypre boomeramg 10'
line_search = 'none'
nl_rel_tol = 5e-9
nl_abs_tol = 1e-10
nl_max_its = 15
l_tol = 1e-3
l_max_its = 50
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/porosity_jump/2d-rc-epsjump.i)
mu=1.1
rho=1.1
advected_interp_method='upwind'
velocity_interp_method='rc'
[Mesh]
[mesh]
type = CartesianMeshGenerator
dim = 2
dx = '1 1'
dy = '0.5'
ix = '30 30'
iy = '20'
subdomain_id = '1 2'
[]
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = PINSFVRhieChowInterpolator
u = u
v = v
porosity = porosity
pressure = pressure
[]
[]
[Variables]
[u]
type = PINSFVSuperficialVelocityVariable
initial_condition = 1
[]
[v]
type = PINSFVSuperficialVelocityVariable
initial_condition = 1e-6
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[AuxVariables]
[porosity]
type = MooseVariableFVReal
[]
[]
[ICs]
inactive = 'porosity_continuous'
[porosity_1]
type = ConstantIC
variable = porosity
block = 1
value = 1
[]
[porosity_2]
type = ConstantIC
variable = porosity
block = 2
value = 0.5
[]
[porosity_continuous]
type = FunctionIC
variable = porosity
block = '1 2'
function = smooth_jump
[]
[]
[Functions]
[smooth_jump]
type = ParsedFunction
value = '1 - 0.5 * 1 / (1 + exp(-30*(x-1)))'
[]
[]
[FVKernels]
[mass]
type = PINSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = PINSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
porosity = porosity
momentum_component = 'x'
[]
[u_viscosity]
type = PINSFVMomentumDiffusion
variable = u
mu = ${mu}
porosity = porosity
momentum_component = 'x'
[]
[u_pressure]
type = PINSFVMomentumPressure
variable = u
pressure = pressure
porosity = porosity
momentum_component = 'x'
[]
[v_advection]
type = PINSFVMomentumAdvection
variable = v
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
porosity = porosity
momentum_component = 'y'
[]
[v_viscosity]
type = PINSFVMomentumDiffusion
variable = v
mu = ${mu}
porosity = porosity
momentum_component = 'y'
[]
[v_pressure]
type = PINSFVMomentumPressure
variable = v
pressure = pressure
porosity = porosity
momentum_component = 'y'
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = 0
[]
[walls-u]
type = INSFVNaturalFreeSlipBC
boundary = 'top bottom'
variable = u
momentum_component = 'x'
[]
[walls-v]
type = INSFVNaturalFreeSlipBC
boundary = 'top bottom'
variable = v
momentum_component = 'y'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 0.4
[]
[]
[Materials]
inactive = 'smooth'
[jump]
type = ADPiecewiseByBlockFunctorMaterial
prop_name = 'porosity'
subdomain_to_prop_value = '1 1
2 0.5'
[]
[smooth]
type = ADGenericFunctionFunctorMaterial
prop_names = 'porosity'
prop_values = 'smooth_jump'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-10
[]
[Postprocessors]
[inlet_p]
type = SideAverageValue
variable = 'pressure'
boundary = 'left'
[]
[outlet-u]
type = SideIntegralVariablePostprocessor
variable = u
boundary = 'right'
[]
[]
[Outputs]
exodus = true
csv = false
[]
(modules/richards/test/tests/pressure_pulse/pp_fu_01.i)
# investigating pressure pulse in 1D with 1 phase
# steadystate
[Mesh]
type = GeneratedMesh
dim = 1
nx = 10
xmin = 0
xmax = 100
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGstandard
sat_UO = Saturation
seff_UO = SeffVG
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1000
bulk_mod = 2E9
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1E-5
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.0
sum_s_res = 0.0
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 1E3
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
initial_condition = 2E6
[../]
[]
[BCs]
[./left]
type = DirichletBC
boundary = left
value = 3E6
variable = pressure
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[Kernels]
active = 'richardsf'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFullyUpwindFlux
variable = pressure
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = SeffVG
pressure_vars = pressure
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-15 0 0 0 1E-15 0 0 0 1E-15'
viscosity = 1E-3
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = pp_fu_01
exodus = true
[]
(test/tests/ics/vector_function_ic/vector_function_ic_comp.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 2
ny = 2
nz = 2
[]
[Problem]
solve = false
kernel_coverage_check = false
[]
[Variables/A]
family = LAGRANGE_VEC
[]
[ICs/A]
type = VectorFunctionIC
variable = A
function_x = func
[]
[Functions/func]
type = ParsedFunction
value = '2*x'
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/pins/materials/2d-rc-action.i)
mu=0.01
rho=2000
u_inlet = 1
advected_interp_method='upwind'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 10
ymin = 0
ymax = 1
nx = 10
ny = 6
[]
[]
[AuxVariables]
[porosity]
family = MONOMIAL
order = CONSTANT
fv = true
initial_condition = 0.5
[]
[speed_output]
type = MooseVariableFVReal
[]
[vel_x_output]
type = MooseVariableFVReal
[]
[vel_y_output]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[speed]
type = ADFunctorElementalAux
variable = 'speed_output'
functor = 'speed'
[]
[vel_x]
type = ADFunctorVectorElementalAux
variable = 'vel_x_output'
functor = 'velocity'
component = 0
[]
[vel_y]
type = ADFunctorVectorElementalAux
variable = 'vel_y_output'
functor = 'velocity'
component = 1
[]
[]
[Modules]
[NavierStokesFV]
compressibility = 'incompressible'
porous_medium_treatment = true
density = ${rho}
dynamic_viscosity = ${mu}
porosity = 'porosity'
initial_velocity = '${u_inlet} 1e-6 0'
initial_pressure = 0.0
inlet_boundaries = 'left'
momentum_inlet_types = 'fixed-velocity'
momentum_inlet_function = '${u_inlet} 0'
wall_boundaries = 'top bottom'
momentum_wall_types = 'noslip symmetry'
outlet_boundaries = 'right'
momentum_outlet_types = 'fixed-pressure'
pressure_function = '0.1'
momentum_advection_interpolation = ${advected_interp_method}
mass_advection_interpolation = ${advected_interp_method}
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
nl_abs_tol = 1e-11
[]
# Some basic Postprocessors to examine the solution
[Postprocessors]
[inlet-p]
type = SideAverageValue
variable = pressure
boundary = 'left'
[]
[outlet-u]
type = SideAverageValue
variable = superficial_vel_x
boundary = 'right'
[]
[]
[Outputs]
exodus = true
csv = false
[]
(test/tests/auxkernels/grad_component/grad_component.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./grad_u_x]
order = CONSTANT
family = MONOMIAL
[../]
[./grad_u_y]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./grad_u_x_aux]
type = VariableGradientComponent
variable = grad_u_x
component = x
gradient_variable = u
[../]
[./grad_u_y_aux]
type = VariableGradientComponent
variable = grad_u_y
component = y
gradient_variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/meshed_gap_thermal_contact/meshed_gap_thermal_contact_constant_conductance.i)
[Mesh]
[fmesh]
type = FileMeshGenerator
file = meshed_gap.e
[]
[block0]
type = SubdomainBoundingBoxGenerator
input = fmesh
bottom_left = '.5 -.5 0'
top_right = '.7 .5 0'
block_id = 4
[]
[]
[Variables]
[./temp]
block = '1 3'
initial_condition = 1.0
[../]
[]
[Kernels]
[./hc]
type = HeatConduction
variable = temp
block = '1 3'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = temp
boundary = 1
value = 1
[../]
[./right]
type = DirichletBC
variable = temp
boundary = 4
value = 2
[../]
[]
[ThermalContact]
[./gap_conductance]
type = GapHeatTransfer
variable = temp
primary = 2
secondary = 3
emissivity_primary = 0
emissivity_secondary = 0
gap_conductance = 2.5
[../]
[]
[Materials]
[./hcm]
type = HeatConductionMaterial
block = '1 3'
temp = temp
thermal_conductivity = 1
[../]
[]
[Problem]
type = FEProblem
kernel_coverage_check = false
material_coverage_check = false
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
[./out]
type = Exodus
[../]
[]
(test/tests/materials/output/output_steady.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Functions]
[./bc_func]
type = ParsedFunction
value = 0.5*y
[../]
[]
[Kernels]
[./diff]
type = CoefDiffusion
variable = u
block = 0
coef = 0.1
[../]
[]
[BCs]
[./left]
type = FunctionDirichletBC
variable = u
boundary = left
function = bc_func
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Materials]
[./k]
type = OutputTestMaterial
block = 0
outputs = all
variable = u
output_properties = 'real_property vector_property tensor_property'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/chemical_reactions/test/tests/mineral_volume_fraction/mineral.i)
# Test the MineralVolumeFraction postprocessor
[Mesh]
type = GeneratedMesh
dim = 2
xmax = 2
ymax = 2
[]
[Variables]
[./mineral_conc]
initial_condition = 0.1
[../]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[./volume_frac]
type = TotalMineralVolumeFraction
variable = mineral_conc
molar_volume = 20
execute_on = 'initial timestep_end'
[../]
[]
[Outputs]
csv = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/mixing_length_total_viscosity_material/steady.i)
von_karman_const = 0.41
H = 1 #halfwidth of the channel
L = 150
Re = 100
rho = 1
bulk_u = 1
mu = ${fparse rho * bulk_u * 2 * H / Re}
advected_interp_method='upwind'
velocity_interp_method='rc'
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Mesh]
[gen]
type = CartesianMeshGenerator
dim = 2
dx = '${L}'
dy = '0.667 0.333'
ix = '200'
iy = '10 1'
[]
[]
[Problem]
fv_bcs_integrity_check = false
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = 1e-6
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 1e-6
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[AuxVariables]
[mixing_length]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = ${mu}
momentum_component = 'x'
[]
[u_viscosity_rans]
type = INSFVMixingLengthReynoldsStress
variable = vel_x
rho = ${rho}
mixing_length = mixing_length
momentum_component = 'x'
u = vel_x
v = vel_y
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = ${mu}
momentum_component = 'y'
[]
[v_viscosity_rans]
type = INSFVMixingLengthReynoldsStress
variable = vel_y
rho = ${rho}
mixing_length = mixing_length
momentum_component = 'y'
u = vel_x
v = vel_y
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
[]
[]
[AuxKernels]
[mixing_length]
type = WallDistanceMixingLengthAux
walls = 'top'
variable = mixing_length
execute_on = 'initial'
von_karman_const = ${von_karman_const}
delta = 0.5
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_x
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_y
function = '0'
[]
[wall-u]
type = INSFVWallFunctionBC
variable = vel_x
boundary = 'top'
u = vel_x
v = vel_y
mu = ${mu}
rho = ${rho}
momentum_component = x
[]
[wall-v]
type = INSFVWallFunctionBC
variable = vel_y
boundary = 'top'
u = vel_x
v = vel_y
mu = ${mu}
rho = ${rho}
momentum_component = y
[]
[sym-u]
type = INSFVSymmetryVelocityBC
boundary = 'bottom'
variable = vel_x
u = vel_x
v = vel_y
mu = total_viscosity
momentum_component = x
[]
[sym-v]
type = INSFVSymmetryVelocityBC
boundary = 'bottom'
variable = vel_y
u = vel_x
v = vel_y
mu = total_viscosity
momentum_component = y
[]
[symmetry_pressure]
type = INSFVSymmetryPressureBC
boundary = 'bottom'
variable = pressure
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = '0'
[]
[]
[Materials]
[total_viscosity]
type = MixingLengthTurbulentViscosityMaterial
u = 'vel_x' #computes total viscosity = mu_t + mu
v = 'vel_y' #property is called total_viscosity
mixing_length = mixing_length
mu = ${mu}
rho = ${rho}
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 200 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(test/tests/ics/bounding_box_ic/bounding_box_ic_diffuse_test.i)
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
uniform_refine = 3
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = BoundingBoxIC
x1 = 0.1
y1 = 0.1
x2 = 0.6
y2 = 0.6
inside = 2.3
outside = 4.6
int_width = 0.2
[../]
[../]
[]
[AuxVariables]
active = 'u_aux'
[./u_aux]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = BoundingBoxIC
x1 = 0.1
y1 = 0.1
x2 = 0.6
y2 = 0.6
inside = 1.34
outside = 6.67
int_width = 0.2
[../]
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(modules/ray_tracing/test/tests/utils/ray_tracing_angular_quadrature/errors.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
[]
[]
[UserObjects/test]
type = RayTracingAngularQuadratureErrorTest
[]
[Executioner]
type = Steady
[]
(test/tests/outputs/console/console_warning.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[AuxVariables]
[./aux0]
order = SECOND
family = SCALAR
[../]
[./aux1]
family = SCALAR
initial_condition = 5
[../]
[./aux2]
family = SCALAR
initial_condition = 10
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./diff_v]
type = CoefDiffusion
variable = v
coef = 2
[../]
[]
[BCs]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[./left_u]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = right
value = 3
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = left
value = 2
[../]
[]
[Postprocessors]
[./num_vars]
type = NumVars
system = 'NL'
[../]
[./num_aux]
type = NumVars
system = 'AUX'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
[./screen]
type = Console
[../]
[./screen2]
type = Console
[../]
[./screen3]
type = Console
[../]
[]
[ICs]
[./aux0_IC]
variable = aux0
values = '12 13'
type = ScalarComponentIC
[../]
[]
(test/tests/kernels/array_kernels/array_diffusion_reaction_other_coupling.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 4
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
components = 2
[]
[v]
[]
[]
[Kernels]
[diff]
type = ArrayDiffusion
variable = u
diffusion_coefficient = dc
[]
[reaction]
type = ArrayReaction
variable = u
reaction_coefficient = rc
[]
[diffv]
type = Diffusion
variable = v
[]
[vu]
type = ArrayCoupledForce
variable = u
v = v
coef = '0 0.5'
[]
[uv]
type = CoupledArrayForce
variable = v
v = u
coef = '0.05 0'
[]
[]
[BCs]
[left]
type = ArrayDirichletBC
variable = u
boundary = 1
values = '0 0'
[]
[right]
type = ArrayDirichletBC
variable = u
boundary = 2
values = '1 2'
[]
[leftv]
type = DirichletBC
variable = v
boundary = 1
value = 0
[]
[rightv]
type = DirichletBC
variable = v
boundary = 2
value = 2
[]
[]
[Materials]
[dc]
type = GenericConstantArray
prop_name = dc
prop_value = '1 1'
[]
[rc]
type = GenericConstant2DArray
prop_name = rc
prop_value = '1 0; -0.1 1'
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Postprocessors]
[intu0]
type = ElementIntegralArrayVariablePostprocessor
variable = u
component = 0
[]
[intu1]
type = ElementIntegralArrayVariablePostprocessor
variable = u
component = 1
[]
[intv]
type = ElementIntegralVariablePostprocessor
variable = v
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(test/tests/auxkernels/nodal_aux_var/multi_update_var_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./tt]
order = FIRST
family = LAGRANGE
initial_condition = 0
[../]
[./ten]
order = FIRST
family = LAGRANGE
initial_condition = 1
[../]
[./2k]
order = FIRST
family = LAGRANGE
initial_condition = 2
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./do-no-1]
variable = ten
type = SelfAux
[../]
[./do-no-2]
variable = 2k
type = SelfAux
[../]
[./all]
variable = tt
type = MultipleUpdateAux
u = u
var1 = ten
var2 = 2k
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out_multi_var
exodus = true
[]
(modules/richards/test/tests/jacobian_1/jn06.i)
# unsaturated = true
# gravity = false
# supg = true
# transient = false
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = -1
xmax = 1
ymin = -1
ymax = 1
zmin = -1
zmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0 # notice small quantity, so the PETSc constant state works
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1 # notice small quantity, so the PETSc constant state works
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.2
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 0.1
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = RandomIC
block = 0
min = -1
max = 0
[../]
[../]
[]
[Kernels]
active = 'richardsf'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGstandard
sat_UO = Saturation
seff_UO = SeffVG
viscosity = 1E-3
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -snes_type'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000 test'
[../]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
file_base = jn06
exodus = false
[]
(test/tests/mesh/checkpoint/checkpoint_split.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/bcs/penalty_dirichlet_bc/function_penalty_dirichlet_bc_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 10
ny = 10
elem_type = QUAD9
[]
[Functions]
[./forcing_fn]
type = ParsedFunction
value = -4+x*x+y*y
[../]
[./solution]
type = ParsedGradFunction
value = x*x+y*y
grad_x = 2*x
grad_y = 2*y
[../]
[]
[Variables]
[./u]
order = SECOND
family = HIERARCHIC
[../]
[]
[Kernels]
active = 'diff forcing reaction'
[./diff]
type = Diffusion
variable = u
[../]
[./reaction]
type = Reaction
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
active = 'bc_all'
[./bc_all]
type = FunctionPenaltyDirichletBC
variable = u
function = solution
boundary = 'top left right bottom'
penalty = 1e6
[../]
[]
[Postprocessors]
[./dofs]
type = NumDOFs
[../]
[./h]
type = AverageElementSize
[../]
[./L2error]
type = ElementL2Error
variable = u
function = solution
[../]
[./H1error]
type = ElementH1Error
variable = u
function = solution
[../]
[./H1Semierror]
type = ElementH1SemiError
variable = u
function = solution
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
nl_rel_tol = 1e-14
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
csv = true
[]
(modules/heat_conduction/test/tests/view_factors/view_factor_3d.i)
[GlobalParams]
view_factor_object_name = unobstructed_vf
[]
[Mesh]
type = GeneratedMesh
dim = 3
xmin = 0
xmax = 1
ymin = 0
ymax = 1
zmin = 0
zmax = 1
nx = 2
ny = 2
nz = 2
[]
[UserObjects]
active = 'unobstructed_vf'
[unobstructed_vf]
type = UnobstructedPlanarViewFactor
boundary = 'left right front back bottom top'
execute_on = INITIAL
[]
[vf_study]
type = ViewFactorRayStudy
execute_on = INITIAL
boundary = 'left right front back bottom top'
face_order = FIFTH
polar_quad_order = 12
azimuthal_quad_order = 4
[]
[rt_vf]
type = RayTracingViewFactor
boundary = 'left right front back bottom top'
execute_on = INITIAL
ray_study_name = vf_study
normalize_view_factor = false
[]
[]
## For convenience, the "view_factor_object_name" for these
## PPs are set in global params for switching between methods
[Postprocessors]
[left_right]
type = ViewFactorPP
from_boundary = left
to_boundary = right
[]
[left_top]
type = ViewFactorPP
from_boundary = left
to_boundary = top
[]
[left_back]
type = ViewFactorPP
from_boundary = left
to_boundary = back
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[Quadrature] # higher order quadrature for unobstructed
order = SECOND
[]
[]
[Outputs]
csv = true
[]
(test/tests/materials/types/test.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./real]
order = CONSTANT
family = MONOMIAL
[../]
[./stdvec0]
order = CONSTANT
family = MONOMIAL
[../]
[./stdvec1]
order = CONSTANT
family = MONOMIAL
[../]
[./stdvec0_qp0]
order = CONSTANT
family = MONOMIAL
[../]
[./stdvec0_qp1]
order = CONSTANT
family = MONOMIAL
[../]
[./realvec0]
order = CONSTANT
family = MONOMIAL
[../]
[./realvec1]
order = CONSTANT
family = MONOMIAL
[../]
[./realvec2]
order = CONSTANT
family = MONOMIAL
[../]
[./densemat00]
order = CONSTANT
family = MONOMIAL
[../]
[./densemat01]
order = CONSTANT
family = MONOMIAL
[../]
[./tensor00]
order = CONSTANT
family = MONOMIAL
[../]
[./tensor11]
order = CONSTANT
family = MONOMIAL
[../]
[./tensor22]
order = CONSTANT
family = MONOMIAL
[../]
[./stdvecgrad00]
order = CONSTANT
family = MONOMIAL
[../]
[./stdvecgrad01]
order = CONSTANT
family = MONOMIAL
[../]
[./stdvecgrad02]
order = CONSTANT
family = MONOMIAL
[../]
[./stdvecgrad10]
order = CONSTANT
family = MONOMIAL
[../]
[./stdvecgrad11]
order = CONSTANT
family = MONOMIAL
[../]
[./stdvecgrad12]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./real0]
type = MaterialRealAux
variable = real
property = real_prop
execute_on = timestep_end
[../]
[./stdvec0]
type = MaterialStdVectorAux
variable = stdvec0
property = stdvec_prop
index = 0
execute_on = timestep_end
[../]
[./stdvec1]
type = MaterialStdVectorAux
variable = stdvec1
property = stdvec_prop
index = 1
execute_on = timestep_end
[../]
[./stdvec0_qp0]
type = MaterialStdVectorAux
variable = stdvec0_qp0
property = stdvec_prop_qp
index = 0
selected_qp = 0
execute_on = timestep_end
[../]
[./stdvec0_qp1]
type = MaterialStdVectorAux
variable = stdvec0_qp1
property = stdvec_prop_qp
index = 0
selected_qp = 1
execute_on = timestep_end
[../]
[./densemat00]
type = MaterialRealDenseMatrixAux
variable = densemat00
property = matrix_prop
row = 0
column = 0
execute_on = timestep_end
[../]
[./densemat01]
type = MaterialRealDenseMatrixAux
variable = densemat01
property = matrix_prop
row = 0
column = 1
execute_on = timestep_end
[../]
[./realvec0]
type = MaterialRealVectorValueAux
variable = realvec0
property = realvec_prop
component = 0
execute_on = timestep_end
[../]
[./realvec1]
type = MaterialRealVectorValueAux
variable = realvec1
property = realvec_prop
component = 1
execute_on = timestep_end
[../]
[./realvec2]
type = MaterialRealVectorValueAux
variable = realvec2
property = realvec_prop
component = 2
execute_on = timestep_end
[../]
[./realtensor00]
type = MaterialRealTensorValueAux
variable = tensor00
property = tensor_prop
row = 0
column = 0
execute_on = timestep_end
[../]
[./realtensor11]
type = MaterialRealTensorValueAux
variable = tensor11
property = tensor_prop
row = 1
column = 1
execute_on = timestep_end
[../]
[./realtensor22]
type = MaterialRealTensorValueAux
variable = tensor22
property = tensor_prop
row = 2
column = 2
execute_on = timestep_end
[../]
[./stdvecgrad00]
type = MaterialStdVectorRealGradientAux
variable = stdvecgrad00
property = stdvec_grad_prop
[../]
[./stdvecgrad01]
type = MaterialStdVectorRealGradientAux
variable = stdvecgrad01
property = stdvec_grad_prop
component = 1
[../]
[./stdvecgrad02]
type = MaterialStdVectorRealGradientAux
variable = stdvecgrad02
property = stdvec_grad_prop
component = 2
[../]
[./stdvecgrad10]
type = MaterialStdVectorRealGradientAux
variable = stdvecgrad10
index = 1
property = stdvec_grad_prop
[../]
[./stdvecgrad11]
type = MaterialStdVectorRealGradientAux
variable = stdvecgrad11
index = 1
component = 1
property = stdvec_grad_prop
[../]
[./stdvecgrad12]
type = MaterialStdVectorRealGradientAux
variable = stdvecgrad12
index = 1
component = 2
property = stdvec_grad_prop
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Materials]
[./mat]
type = TypesMaterial
block = 0
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
[]
[Outputs]
file_base = test_out
exodus = true
[]
(test/tests/vectorpostprocessors/line_material_sampler/line_material_real_sampler.i)
[Mesh]
[genmesh]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 4
ny = 4
[]
[mesh0]
type = SubdomainBoundingBoxGenerator
input = genmesh
block_id = 0
location = INSIDE
bottom_left = '0 0 0'
top_right = '1 0.5 0'
[]
[mesh01]
type = SubdomainBoundingBoxGenerator
input = mesh0
block_id = 1
location = INSIDE
bottom_left = '0 0.5 0'
top_right = '1 1 0'
[]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./mat]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = MatDiffusionTest
variable = u
prop_name = matp
[../]
[]
[AuxKernels]
[./mat]
type = MaterialRealAux
variable = mat
property = matp
execute_on = timestep_end
[../]
[]
[VectorPostprocessors]
[./mat]
type = LineMaterialRealSampler
start = '0.125 0.375 0.0'
end = '0.875 0.375 0.0'
property = matp
sort_by = id
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[./right]
type = MTBC
variable = u
boundary = 1
grad = 8
prop_name = matp
[../]
[]
[Materials]
[./mat]
type = MTMaterial
block = '0 1'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
file_base = out
csv = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_mortar/modular_gap_heat_transfer_mortar_displaced_conduction_function.i)
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
[file]
type = FileMeshGenerator
file = 2blk-gap.e
[]
[secondary]
type = LowerDBlockFromSidesetGenerator
sidesets = '101'
new_block_id = 10001
new_block_name = 'secondary_lower'
input = file
[]
[primary]
type = LowerDBlockFromSidesetGenerator
sidesets = '100'
new_block_id = 10000
new_block_name = 'primary_lower'
input = secondary
[]
allow_renumbering = false
[]
[Problem]
kernel_coverage_check = false
material_coverage_check = false
[]
[AuxVariables]
[dummy]
order = FIRST
family = LAGRANGE
initial_condition = 1.0
[]
[]
[Functions]
[function]
type = ParsedFunction
value = 'if(t > 100.0, 0.0, t)'
[]
[]
[Variables]
[temp]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[disp_x]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[disp_y]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[lm]
order = FIRST
family = LAGRANGE
block = 'secondary_lower'
[]
[]
[Materials]
[left]
type = ADHeatConductionMaterial
block = 1
thermal_conductivity = 0.01
specific_heat = 1
[]
[right]
type = ADHeatConductionMaterial
block = 2
thermal_conductivity = 0.005
specific_heat = 1
[]
[]
[Kernels]
[hc_displaced_block]
type = ADHeatConduction
variable = temp
use_displaced_mesh = true
block = '1'
[]
[hc_undisplaced_block]
type = ADHeatConduction
variable = temp
use_displaced_mesh = false
block = '2'
[]
[disp_x]
type = Diffusion
variable = disp_x
block = '1 2'
[]
[disp_y]
type = Diffusion
variable = disp_y
block = '1 2'
[]
[]
[UserObjects]
[conduction]
type = GapFluxModelConduction
temperature = temp
boundary = 100
gap_conductivity = 10.0
gap_conductivity_function_variable = dummy
gap_conductivity_function = function
[]
[]
[Constraints]
[ced]
type = ModularGapConductanceConstraint
variable = lm
secondary_variable = temp
use_displaced_mesh = true
primary_boundary = 100
primary_subdomain = 10000
secondary_boundary = 101
secondary_subdomain = 10001
gap_flux_models = conduction
[]
[]
[BCs]
[left]
type = DirichletBC
variable = temp
boundary = 'left'
value = 100
[]
[right]
type = DirichletBC
variable = temp
boundary = 'right'
value = 0
[]
[left_disp_x]
type = DirichletBC
preset = false
variable = disp_x
boundary = 'left'
value = .1
[]
[right_disp_x]
type = DirichletBC
preset = false
variable = disp_x
boundary = 'right'
value = 0
[]
[bottom_disp_y]
type = DirichletBC
preset = false
variable = disp_y
boundary = 'bottom'
value = 0
[]
[]
[Preconditioning]
[fmp]
type = SMP
full = true
solve_type = 'NEWTON'
[]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-11
nl_abs_tol = 1.0e-10
[]
[VectorPostprocessors]
[NodalTemperature]
type = NodalValueSampler
sort_by = id
boundary = '100 101'
variable = 'temp'
[]
[]
[Outputs]
exodus = false
csv = true
[]
(modules/porous_flow/test/tests/gravity/fully_saturated_upwinded_grav01c_action.i)
# Checking that gravity head is established
# 1phase, 2-component, constant fluid-bulk, constant viscosity, constant permeability
# fully saturated with fully-saturated Kernel with upwinding
# For better agreement with the analytical solution (ana_pp), just increase nx
# This is the Action version of fully_saturated_upwinded_grav01c.i
# NOTE: this test is numerically delicate because the steady-state configuration is independent of the mass fraction, so the frac variable can assume any value as long as mass-fraction is conserved
[Mesh]
type = GeneratedMesh
dim = 1
nx = 100
xmin = -1
xmax = 0
[]
[Variables]
[pp]
[InitialCondition]
type = RandomIC
min = 0
max = 1
[]
[]
[frac]
[InitialCondition]
type = RandomIC
min = 0
max = 1
[]
[]
[]
[PorousFlowFullySaturated]
porepressure = pp
mass_fraction_vars = frac
fp = simple_fluid
gravity = '-1 0 0'
multiply_by_density = true
[]
[Functions]
[ana_pp]
type = ParsedFunction
vars = 'g B p0 rho0'
vals = '1 1.2 0 1'
value = '-B*log(exp(-p0/B)+g*rho0*x/B)' # expected pp at base
[]
[]
[BCs]
[z]
type = DirichletBC
variable = pp
boundary = right
value = 0
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 1.2
density0 = 1
viscosity = 1
thermal_expansion = 0
[]
[]
[]
[Materials]
[permeability]
type = PorousFlowPermeabilityConst
PorousFlowDictator = dictator
permeability = '1 0 0 0 2 0 0 0 3'
[]
[]
[Postprocessors]
[pp_base]
type = PointValue
variable = pp
point = '-1 0 0'
[]
[pp_analytical]
type = FunctionValuePostprocessor
function = ana_pp
point = '-1 0 0'
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = Newton
nl_rel_tol = 1E-12
petsc_options_iname = '-pc_factor_shift_type'
petsc_options_value = 'NONZERO'
nl_max_its = 100
[]
[Outputs]
csv = true
[]
(modules/heat_conduction/test/tests/fvbcs/fv_thermal_resistance/test.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 5
ny = 5
xmax = 2
[]
[]
[Variables]
[u]
type = MooseVariableFVReal
initial_condition = 0.5
[]
[]
[FVKernels]
[diff_left]
type = FVDiffusion
variable = u
coeff = 4
[]
[gradient_creating]
type = FVBodyForce
variable = u
[]
[]
[FVBCs]
[left]
type = FVThermalResistanceBC
geometry = 'cartesian'
variable = u
T_ambient = 10
htc = 'htc'
emissivity = 0.2
thermal_conductivities = '0.1 0.2 0.3'
conduction_thicknesses = '1 0.7 0.2'
boundary = 'left'
# Test setting iteration parameters
step_size = 0.02
max_iterations = 120
tolerance = 1e-4
[]
[top]
type = FVThermalResistanceBC
geometry = 'cartesian'
variable = u
# Test setting the temperature separately from the variable
temperature = 'u'
T_ambient = 14
htc = 'htc'
emissivity = 0
thermal_conductivities = '0.1 0.2 0.3'
conduction_thicknesses = '1 0.7 0.4'
boundary = 'top'
[]
[other]
type = FVDirichletBC
variable = u
boundary = 'right bottom'
value = 0
[]
[]
[Materials]
[cht]
type = ADGenericConstantMaterial
prop_names = 'htc'
prop_values = '1'
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(test/tests/transfers/multiapp_nearest_node_transfer/source_boundary_sub.i)
[Mesh]
[drmg]
type = DistributedRectilinearMeshGenerator
dim = 2
nx = 30
ny = 30
elem_type = QUAD4
partition = square
[]
[]
[Variables]
[u][]
[]
[Kernels]
[conduction]
type = Diffusion
variable = u
[]
[]
[BCs]
[right]
type = DirichletBC
variable = u
boundary = 'right'
value = 5
[]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-6
[]
[Outputs]
exodus = true
[]
(modules/thermal_hydraulics/test/tests/materials/ad_material_function_product/ad_material_function_product.i)
# Gold value should be the following:
# product = scale * func
# = 0.5 * 100
# = 50
[GlobalParams]
execute_on = 'initial'
[]
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
[]
[Functions]
[func]
type = ConstantFunction
value = 100
[]
[]
[Materials]
[scale_mat]
type = ADGenericConstantMaterial
prop_names = 'scale'
prop_values = '0.5'
[]
[product_mat]
type = ADMaterialFunctionProductMaterial
mat_prop_product = product
mat_prop_scale = scale
function = func
[]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Postprocessors]
[product_pp]
type = ADElementAverageMaterialProperty
mat_prop = product
[]
[]
[Outputs]
csv = true
[]
(test/tests/mesh/custom_partitioner/custom_linear_partitioner_test.i)
###########################################################
# This is a test of the custom partitioner system. It
# demonstrates the usage of a linear partitioner on the
# elements of a mesh.
#
# @Requirement F2.30
###########################################################
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 100
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 10.0
[]
# Custom linear partitioner
[./Partitioner]
type = LibmeshPartitioner
partitioner = linear
[../]
parallel_type = replicated
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./proc_id]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./proc_id]
type = ProcessorIDAux
variable = proc_id
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = custom_linear_partitioner_test_out
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[]
(test/tests/dirackernels/point_caching/point_caching.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
elem_type = QUAD4
uniform_refine = 4
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[DiracKernels]
active = 'point_source'
[./point_source]
type = CachingPointSource
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/misc/check_error/bad_kernel_action.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
# Note: the BadKernels syntax is set up to incorrectly call addIndicator()
# when it should actually call addKernel() to test that we can detect when
# people call the wrong FEProblem methods in their Actions.
[BadKernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/kernels/tag_errors/no_tags/no_tags.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
vector_tags = ''
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/debug/show_var_residual_norms.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 10
ny = 10
elem_type = QUAD9
[]
[Functions]
[./forcing_fnu]
type = ParsedFunction
value = -5.8*(x+y)+x*x*x-x+y*y*y-y
[../]
[./forcing_fnv]
type = ParsedFunction
value = -4
[../]
[./slnu]
type = ParsedGradFunction
value = x*x*x-x+y*y*y-y
grad_x = 3*x*x-1
grad_y = 3*y*y-1
[../]
[./slnv]
type = ParsedGradFunction
value = x*x+y*y
grad_x = 2*x
grad_y = 2*y
[../]
#NeumannBC functions
[./bc_fnut]
type = ParsedFunction
value = 3*y*y-1
[../]
[./bc_fnub]
type = ParsedFunction
value = -3*y*y+1
[../]
[./bc_fnul]
type = ParsedFunction
value = -3*x*x+1
[../]
[./bc_fnur]
type = ParsedFunction
value = 3*x*x-1
[../]
[]
[Variables]
[./u]
order = THIRD
family = HIERARCHIC
[../]
[./v]
order = SECOND
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff1 diff2 test1 forceu forcev react'
[./diff1]
type = Diffusion
variable = u
[../]
[./test1]
type = CoupledConvection
variable = u
velocity_vector = v
[../]
[./diff2]
type = Diffusion
variable = v
[../]
[./react]
type = Reaction
variable = u
[../]
[./forceu]
type = BodyForce
variable = u
function = forcing_fnu
[../]
[./forcev]
type = BodyForce
variable = v
function = forcing_fnv
[../]
[]
[BCs]
active = 'bc_u_tb bc_v bc_ul bc_ur bc_ut bc_ub'
[./bc_u]
type = FunctionPenaltyDirichletBC
variable = u
function = slnu
boundary = 'left right top bottom'
penalty = 1e6
[../]
[./bc_v]
type = FunctionDirichletBC
variable = v
function = slnv
boundary = 'left right top bottom'
[../]
[./bc_u_lr]
type = FunctionPenaltyDirichletBC
variable = u
function = slnu
boundary = 'left right top bottom'
penalty = 1e6
[../]
[./bc_u_tb]
type = CoupledKernelGradBC
variable = u
var2 = v
vel = '0.1 0.1'
boundary = 'top bottom left right'
[../]
[./bc_ul]
type = FunctionNeumannBC
variable = u
function = bc_fnul
boundary = 'left'
[../]
[./bc_ur]
type = FunctionNeumannBC
variable = u
function = bc_fnur
boundary = 'right'
[../]
[./bc_ut]
type = FunctionNeumannBC
variable = u
function = bc_fnut
boundary = 'top'
[../]
[./bc_ub]
type = FunctionNeumannBC
variable = u
function = bc_fnub
boundary = 'bottom'
[../]
[]
[Preconditioning]
active = ' '
[./prec]
type = SMP
full = true
[../]
[]
[Postprocessors]
active='L2u L2v'
[./dofs]
type = NumDOFs
[../]
[./h]
type = AverageElementSize
[../]
[./L2u]
type = ElementL2Error
variable = u
function = slnu
[../]
[./L2v]
type = ElementL2Error
variable = v
function = slnv
[../]
[./H1error]
type = ElementH1Error
variable = u
function = solution
[../]
[./H1Semierror]
type = ElementH1SemiError
variable = u
function = solution
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
# petsc_options = '-snes'
nl_rel_tol = 1e-15
nl_abs_tol = 1e-13
[]
[Outputs]
execute_on = 'timestep_end'
[./debug] # This is a test, use the [Debug] block to enable this
type = VariableResidualNormsDebugOutput
[../]
[]
(test/tests/misc/check_error/incomplete_kernel_block_coverage_test.i)
[Mesh]
file = rectangle.e
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff body_force'
[./diff]
type = Diffusion
variable = u
block = 1
[../]
[./body_force]
type = BodyForce
variable = u
block = 1
value = 10
[../]
[]
[BCs]
active = 'right'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
[]
(test/tests/mesh/concentric_circle_mesh/concentric_circle_mesh.i)
[Mesh]
type = ConcentricCircleMesh
num_sectors = 6
radii = '0.2546 0.3368 0.3600 0.3818 0.3923 0.4025 0.4110 0.4750'
rings = '10 6 4 4 4 2 2 6 10'
inner_mesh_fraction = 0.6
has_outer_square = on
pitch = 1.42063
#portion = left_half
preserve_volumes = off
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/porous_flow/test/tests/fluids/simple_fluid_hr.i)
# Test the properties calculated by the simple fluid Material
# Time are chosen to be hours
# Pressure 10 MPa
# Temperature = 300 K (temperature unit = K)
# Density should equal 1500*exp(1E7/1E9-2E-4*300)=1426.844 kg/m^3
# Viscosity should equal 3.06E-7 Pa.hr
# Energy density should equal 4000 * 300 = 1.2E6 J/kg
# Specific enthalpy should equal 4000 * 300 + 10e6 / 1426.844 = 1.207008E6 J/kg
[Modules]
[FluidProperties]
[the_simple_fluid]
type = SimpleFluidProperties
thermal_expansion = 2.0E-4
cv = 4000.0
cp = 5000.0
bulk_modulus = 1.0E9
thermal_conductivity = 1.0
viscosity = 1.1E-3
density0 = 1500.0
[]
[]
[]
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp T'
number_fluid_phases = 1
number_fluid_components = 1
[]
[]
[Variables]
[pp]
initial_condition = 10E6
[]
[T]
initial_condition = 300.0
[]
[]
[Kernels]
[dummy_p]
type = Diffusion
variable = pp
[]
[dummy_T]
type = Diffusion
variable = T
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
temperature = T
[]
[ppss]
type = PorousFlow1PhaseFullySaturated
porepressure = pp
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
temperature_unit = Kelvin
time_unit = hours
fp = the_simple_fluid
phase = 0
[]
[]
[Postprocessors]
[pressure]
type = ElementIntegralVariablePostprocessor
variable = pp
[]
[temperature]
type = ElementIntegralVariablePostprocessor
variable = T
[]
[density]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_fluid_phase_density_qp0'
[]
[viscosity]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_viscosity_qp0'
[]
[internal_energy]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_fluid_phase_internal_energy_qp0'
[]
[enthalpy]
type = ElementIntegralMaterialProperty
mat_prop = 'PorousFlow_fluid_phase_enthalpy_qp0'
[]
[]
[Executioner]
type = Steady
solve_type = Newton
[]
[Outputs]
execute_on = 'timestep_end'
csv = true
[]
(test/tests/meshgenerators/patterned_mesh_generator/patterned_mesh_generator.i)
[Mesh]
[./fmg]
type = FileMeshGenerator
file = quad_mesh.e
[]
[./fmg2]
type = FileMeshGenerator
file = tri_mesh.e
[]
[./pmg]
type = PatternedMeshGenerator
inputs = 'fmg fmg2'
pattern = '0 0 0 0 0 0 0 0 0 0 0 0 0 0 ;
0 1 1 0 0 0 0 0 0 0 0 1 1 0 ;
0 1 1 1 0 0 0 0 0 0 1 1 1 0 ;
0 1 0 1 1 0 0 0 0 1 1 0 1 0 ;
0 1 0 0 1 1 0 0 1 1 0 0 1 0 ;
0 1 0 0 0 1 1 1 1 0 0 0 1 0 ;
0 1 0 0 0 0 1 1 0 0 0 0 1 0 ;
0 1 0 0 0 0 0 0 0 0 0 0 1 0 ;
0 1 0 0 0 0 0 0 0 0 0 0 1 0 ;
0 1 0 0 0 0 0 0 0 0 0 0 1 0 ;
0 1 0 0 0 0 0 0 0 0 0 0 1 0 ;
0 0 0 0 0 0 0 0 0 0 0 0 0 0'
bottom_boundary = 1
right_boundary = 2
top_boundary = 3
left_boundary = 4
[]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = MatCoefDiffusion
variable = u
conductivity = conductivity
[../]
[]
[BCs]
[./top]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[./bottom]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Materials]
[./mat1]
type = GenericConstantMaterial
block = 1
prop_names = conductivity
prop_values = 100
[../]
[./mat2]
type = GenericConstantMaterial
block = 2
prop_names = conductivity
prop_values = 1e-4
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/userobjects/layered_integral/average_sample.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 6
ny = 30
nz = 6
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./layered_integral]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./liaux]
type = SpatialUserObjectAux
variable = layered_integral
execute_on = timestep_end
user_object = layered_integral
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = u
boundary = bottom
value = 0
[../]
[./top]
type = DirichletBC
variable = u
boundary = top
value = 1
[../]
[]
[UserObjects]
[./layered_integral]
type = LayeredIntegral
direction = y
num_layers = 5
variable = u
execute_on = linear
sample_type = average
average_radius = 2
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/scaling/residual-based/residual-based-two-var.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 10
[]
[ICs]
[u]
type = FunctionIC
variable = u
function = '1000 * (1 - x)'
[]
[v]
type = FunctionIC
variable = v
function = '1e-3 * (1 - x)'
[]
[]
[Variables]
[u][]
[v][]
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
extra_vector_tags = 'ref'
[../]
[rxn]
type = PReaction
power = 2
variable = u
extra_vector_tags = 'ref'
[]
[./diff_v]
type = Diffusion
variable = v
extra_vector_tags = 'ref'
[../]
[rxn_v]
type = PReaction
power = 2
variable = v
extra_vector_tags = 'ref'
[]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 1000
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 0
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = left
value = 1e-3
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = right
value = 0
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
verbose = true
automatic_scaling = true
resid_vs_jac_scaling_param = 1
[]
[Outputs]
exodus = true
[]
(test/tests/partitioners/hierarchical_grid_partitioner/hierarchical_grid_partitioner.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 8
ny = 8
[Partitioner]
type = HierarchicalGridPartitioner
nx_nodes = 2
ny_nodes = 2
nx_procs = 2
ny_procs = 2
[]
[]
[Variables/u]
[]
[Kernels/diff]
type = Diffusion
variable = u
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
[AuxVariables/pid]
family = MONOMIAL
order = CONSTANT
[]
[Problem]
solve = false
[]
[AuxKernels/pid]
type = ProcessorIDAux
variable = pid
execute_on = 'INITIAL'
[]
(python/peacock/tests/input_tab/InputTree/gold/simple_diffusion_vp.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[]
[]
[Executioner]
# Preconditioned JFNK (default)
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
[VectorPostprocessors]
[foo]
type = LineValueSampler
num_points = 10
end_point = '1 0 0'
start_point = '0 0 0'
[]
[]
(test/tests/materials/get_material_property_names/get_material_property_any_block_id.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[./add_subdomain]
input = gen
type = SubdomainBoundingBoxGenerator
top_right = '1 1 0'
bottom_left = '0 0.5 0'
block_id = 100
block_name = 'top'
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Materials]
[./block]
type = GenericConstantMaterial
prop_names = block_prop
block = ANY_BLOCK_ID
prop_values = 12345
[../]
[]
[UserObjects]
[./get_material_block_names_test]
type = GetMaterialPropertyBoundaryBlockNamesTest
expected_names = 'ANY_BLOCK_ID'
property_name = 'block_prop'
test_type = 'block'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/misc/block_boundary_material_check/bc_check.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Variables]
[./u]
[../]
[]
[BCs]
[./bc_left]
type = MatTestNeumannBC
variable = u
boundary = left
mat_prop = 'prop'
[../]
[]
[Problem]
type = FEProblem
solve = false
kernel_coverage_check = false
[]
[Executioner]
type = Steady
[]
[Outputs]
[]
(test/tests/kernels/ad_value/ad_value.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[AuxVariables]
[./u_jac]
[../]
[./v_jac]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[./value_test_v]
type = ValueTest
variable = v
diag_save_in = v_jac
[../]
[./ad_value_test]
type = ADValueTest
variable = u
diag_save_in = u_jac
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = left
value = 0
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'Newton'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/relationship_managers/check_coupling_functor/check_no_mallocs.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Problem]
error_on_jacobian_nonzero_reallocation = true
[]
[Executioner]
type = Steady
[]
[Testing]
[./LotsOfDiffusion]
[./vars]
number = 1
[../]
[../]
[]
(test/tests/misc/block_boundary_material_check/dgkernel_check_block.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Variables]
[./u]
[../]
[]
[DGKernels]
[./dg]
type = MatDGKernel
mat_prop = 'foo'
variable = u
block = 0
[../]
[]
[Problem]
type = FEProblem
solve = false
kernel_coverage_check = false
[]
[Executioner]
type = Steady
[]
[Outputs]
[]
(test/tests/restart/pointer_restart_errors/pointer_load_error2.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[UserObjects]
[./restartable_types]
type = PointerLoadError
[../]
[]
[Problem]
type = FEProblem
solve = false
restart_file_base = pointer_load_error_out_cp/0001
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[./out]
type = Checkpoint
num_files = 1
[../]
[]
(test/tests/mortar/continuity-3d-non-conforming/continuity_mixed.i)
[Mesh]
second_order = false
[file]
type = FileMeshGenerator
file = mixed_mesh.e
[]
[secondary]
input = file
type = LowerDBlockFromSidesetGenerator
new_block_id = 11
new_block_name = "secondary"
sidesets = '101'
[]
[primary]
input = secondary
type = LowerDBlockFromSidesetGenerator
new_block_id = 12
new_block_name = "primary"
sidesets = '102'
[]
[]
[Problem]
kernel_coverage_check = false
[]
[Variables]
[T]
block = '1 2'
[]
[lambda]
block = 'secondary'
[]
[]
[BCs]
[neumann]
type = FunctionGradientNeumannBC
exact_solution = exact_soln_primal
variable = T
boundary = '1 2'
[]
[]
[Kernels]
[conduction]
type = Diffusion
variable = T
block = '1 2'
[]
[sink]
type = Reaction
variable = T
block = '1 2'
[]
[forcing_function]
type = BodyForce
variable = T
function = forcing_function
block = '1 2'
[]
[]
[Functions]
[forcing_function]
type = ParsedFunction
value = 'sin(x*pi)*sin(y*pi)*sin(z*pi) + 3*pi^2*sin(x*pi)*sin(y*pi)*sin(z*pi)'
[]
[exact_soln_primal]
type = ParsedFunction
value = 'sin(x*pi)*sin(y*pi)*sin(z*pi)'
[]
[exact_soln_lambda]
type = ParsedFunction
value = 'pi*sin(pi*y)*sin(pi*z)*cos(pi*x)'
[]
[]
[Debug]
show_var_residual_norms = 1
[]
[Constraints]
[mortar]
type = EqualValueConstraint
primary_boundary = 2
secondary_boundary = 1
primary_subdomain = '12'
secondary_subdomain = '11'
variable = lambda
secondary_variable = T
delta = 0.1
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
solve_type = NEWTON
type = Steady
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_shift_type '
'-pc_factor_shift_amount'
petsc_options_value = 'lu basic NONZERO 1e-15'
[]
[Outputs]
exodus = true
[]
[Postprocessors]
[L2lambda]
type = ElementL2Error
variable = lambda
function = exact_soln_lambda
execute_on = 'timestep_end'
block = 'secondary'
[]
[L2u]
type = ElementL2Error
variable = T
function = exact_soln_primal
execute_on = 'timestep_end'
block = '1 2'
[]
[h]
type = AverageElementSize
block = '1 2'
[]
[]
(test/tests/usability/bad.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
# Missing [] here
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/perf_graph/perf_graph.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 20
ny = 20
nz = 20
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Postprocessors]
[./num_dofs]
type = NumElems
[../]
[../]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
# perf_graph = true
[./pgraph]
type = PerfGraphOutput
level = 1
heaviest_branch = true
heaviest_sections = 10
[]
[]
(modules/geochemistry/test/tests/time_dependent_reactions/except2.i)
#Exception: bad source-species name
[TimeDependentReactionSolver]
model_definition = definition
geochemistry_reactor_name = reactor
charge_balance_species = "Cl-"
constraint_species = "H2O H+ Na+ K+ Ca++ Mg++ Al+++ SiO2(aq) Cl- SO4-- HCO3-"
constraint_value = " 1.0 1E-5 1E-5 1E-5 1E-5 1E-5 1E-5 1E-5 1E-5 1E-5 1E-5"
constraint_meaning = "kg_solvent_water activity bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition"
constraint_unit = "kg dimensionless moles moles moles moles moles moles moles moles moles"
source_species_names = "badname"
source_species_rates = "1"
[]
[Executioner]
type = Steady
[]
[UserObjects]
[definition]
type = GeochemicalModelDefinition
database_file = "../../../database/moose_geochemdb.json"
basis_species = "H2O H+ Na+ K+ Ca++ Mg++ Al+++ SiO2(aq) Cl- SO4-- HCO3-"
[]
[]
(test/tests/restrictable/undefined_ids/undefined_block_kernel.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./kernel_with_undefined_block]
type = Diffusion
variable = u
block = 10
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/fluid_properties/test/tests/methane/methane.i)
# Test MethaneFluidProperties
# Reference data from Irvine Jr, T. F. and Liley, P. E. (1984) Steam and
# Gas Tables with Computer Equations
#
# For temperature = 350K, the fluid properties should be:
# density = 55.13 kg/m^3
# viscosity = 0.01276 mPa.s
# cp = 2.375 kJ/kg/K
# h = 708.5 kJ/kg
# s = 11.30 kJ/kg/K
# c = 481.7 m/s
# k = 0.04113 W/m/K
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
[]
[Variables]
[./dummy]
[../]
[]
[AuxVariables]
[./pressure]
family = MONOMIAL
order = CONSTANT
initial_condition = 10.0e6
[../]
[./temperature]
family = MONOMIAL
order = CONSTANT
initial_condition = 350
[../]
[./density]
family = MONOMIAL
order = CONSTANT
[../]
[./viscosity]
family = MONOMIAL
order = CONSTANT
[../]
[./cp]
family = MONOMIAL
order = CONSTANT
[../]
[./cv]
family = MONOMIAL
order = CONSTANT
[../]
[./internal_energy]
family = MONOMIAL
order = CONSTANT
[../]
[./enthalpy]
family = MONOMIAL
order = CONSTANT
[../]
[./entropy]
family = MONOMIAL
order = CONSTANT
[../]
[./thermal_cond]
family = MONOMIAL
order = CONSTANT
[../]
[./c]
family = MONOMIAL
order = CONSTANT
[../]
[]
[AuxKernels]
[./density]
type = MaterialRealAux
variable = density
property = density
[../]
[./viscosity]
type = MaterialRealAux
variable = viscosity
property = viscosity
[../]
[./cp]
type = MaterialRealAux
variable = cp
property = cp
[../]
[./cv]
type = MaterialRealAux
variable = cv
property = cv
[../]
[./e]
type = MaterialRealAux
variable = internal_energy
property = e
[../]
[./enthalpy]
type = MaterialRealAux
variable = enthalpy
property = h
[../]
[./entropy]
type = MaterialRealAux
variable = entropy
property = s
[../]
[./thermal_cond]
type = MaterialRealAux
variable = thermal_cond
property = k
[../]
[./c]
type = MaterialRealAux
variable = c
property = c
[../]
[]
[Modules]
[./FluidProperties]
[./methane]
type = MethaneFluidProperties
[../]
[]
[]
[Materials]
[./fp_mat]
type = FluidPropertiesMaterialPT
pressure = pressure
temperature = temperature
fp = methane
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = dummy
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(test/tests/controls/dependency/test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./a]
family = SCALAR
order = FIRST
[../]
[]
[AuxScalarKernels]
[./a_sk]
type = ConstantScalarAux
variable = a
value = 0
[../]
[]
[Kernels]
[./diff]
type = CoefDiffusion
variable = u
coef = 0.1
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
csv = true
[]
[Functions]
[./func_coef]
type = ParsedFunction
value = 1
[../]
[]
[Controls]
# We start with a = 0, control2 sets its value to 1 and then control1 will multiply it by 3,
# so the end value has to be 3. If dependecy is broken, we multiply by 3 and then set to 1,
# which is wrong
[./control1]
type = TestControl
parameter = 'AuxScalarKernels/a_sk/value'
test_type = MULT
execute_on = 'initial timestep_begin'
depends_on = control2
[../]
[./control2]
type = RealFunctionControl
parameter = 'AuxScalarKernels/a_sk/value'
function = 'func_coef'
execute_on = 'initial timestep_begin'
[../]
[]
(modules/tensor_mechanics/tutorials/basics/part_1.2.i)
#Tensor Mechanics tutorial: the basics
#Step 1, part 2
#2D simulation of uniaxial tension with linear elasticity with visualized stress
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
file = necking_quad4.e
uniform_refine = 1
[]
[Modules/TensorMechanics/Master]
[./block1]
strain = SMALL
add_variables = true
generate_output = 'stress_xx vonmises_stress' #automatically creates the auxvariables and auxkernels
#needed to output these stress quanities
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 2.1e5
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./bottom]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./top]
type = DirichletBC
variable = disp_y
boundary = top
value = 0.0035
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -sub_pc_type -pc_asm_overlap -ksp_gmres_restart'
petsc_options_value = 'asm lu 1 101'
[]
[Outputs]
exodus = true
perf_graph = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/hydrostatic/gravity.i)
[GlobalParams]
gravity = '0 -0.001 0'
convective_term = false
integrate_p_by_parts = false
u = vel_x
v = vel_y
pressure = p
[]
[Mesh]
second_order = true
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 1
ny = 5
ymax = 5
[../]
[./corner_node]
type = ExtraNodesetGenerator
new_boundary = top_right
coord = '0 5'
input = gen
[../]
[]
[Variables]
[./vel_x]
order = SECOND
[../]
[./vel_y]
order = SECOND
[../]
[./p]
[../]
[]
[Kernels]
[./mass]
type = INSMass
variable = p
[../]
[./x_momentum_space]
type = INSMomentumLaplaceForm
variable = vel_x
component = 0
[../]
[./y_momentum_space]
type = INSMomentumLaplaceForm
variable = vel_y
component = 1
[../]
[]
[BCs]
[./x_no_slip]
type = DirichletBC
variable = vel_x
boundary = 'top bottom left right'
value = 0.0
[../]
[./y_no_slip]
type = DirichletBC
variable = vel_y
boundary = 'top bottom left right'
value = 0.0
[../]
[./p_corner]
type = DirichletBC
boundary = top_right
value = 0
variable = p
[../]
[]
[Materials]
[./const]
type = GenericConstantMaterial
prop_names = 'rho mu'
prop_values = '100 1'
[../]
[]
[Preconditioning]
[./SMP_PJFNK]
type = SMP
full = true
solve_type = NEWTON
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-ksp_gmres_restart -pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = '300 bjacobi ilu 4'
line_search = none
nl_rel_tol = 1e-12
nl_max_its = 6
l_tol = 1e-6
l_max_its = 300
[]
[Outputs]
exodus = true
execute_on = TIMESTEP_END
[]
(test/tests/postprocessors/element_average_material_property/element_average_material_property.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 4
xmin = 0
xmax = 1
[]
[Functions]
[./fn]
type = PiecewiseConstant
axis = x
x = '0 0.25 0.50 0.75'
y = '5 2 3 6'
[../]
[]
[Materials]
[./mat]
type = GenericFunctionMaterial
prop_names = 'mat_prop'
prop_values = 'fn'
[../]
[]
[Postprocessors]
[./avg]
type = ElementAverageMaterialProperty
mat_prop = mat_prop
execute_on = 'INITIAL'
[../]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
execute_on = 'INITIAL'
[]
(test/tests/meshgenerators/rename_boundary_generator/rename_boundary.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 2
[]
# Rename parameters supplied through the "tests" specifications
[rename]
type = RenameBoundaryGenerator
input = gmg
[]
# We compare by element numbers, which are not consistent in parallel
# if this is true
allow_renumbering = false
[]
[Reporters/mesh_info]
type = MeshInfo
items = sideset_elems
[]
[Outputs]
[out]
type = JSON
execute_system_information_on = NONE
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
(test/tests/problems/no_kernel_coverage_check/no_coverage_check.i)
[Mesh]
file = rectangle.e
[]
[Problem]
kernel_coverage_check = false
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
block = 1
[../]
[]
[Kernels]
active = 'diff body_force'
[./diff]
type = Diffusion
variable = u
block = 1
[../]
[./body_force]
type = BodyForce
variable = u
block = 1
value = 10
[../]
[]
[BCs]
active = 'left'
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = 2
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(modules/stochastic_tools/examples/parameter_study/nonlin_diff_react/nonlin_diff_react_sub.i)
[Functions]
[source]
type = ParsedFunction
value = "100 * sin(2 * pi * x) * sin(2 * pi * y)"
[]
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 50
xmin = 0
xmax = 1
ny = 50
ymin = 0
ymax = 1
[]
[]
[Variables]
[U]
family = lagrange
order = first
[]
[]
[Kernels]
[diffusion]
type = Diffusion
variable = U
[]
[nonlin_function]
type = ExponentialReaction
variable = U
mu1 = 0.3
mu2 = 9
[]
[source]
type = BodyForce
variable = U
function = source
[]
[]
[BCs]
[dirichlet_all]
type = DirichletBC
variable = U
boundary = 'left right top bottom'
value = 0
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Postprocessors]
[max]
type = ElementExtremeValue
variable = U
[]
[min]
type = ElementExtremeValue
variable = U
value_type = min
[]
[average]
type = ElementAverageValue
variable = U
[]
[]
[Controls]
[stochastic]
type = SamplerReceiver
[]
[]
[Outputs]
[]
(test/tests/indicators/gradient_jump_indicator/gradient_jump_indicator_test.i)
###########################################################
# This is a test of the Mesh Indicator System. It computes
# a user-defined "error" for each element in the Mesh.
#
# This test has been verified to give the same error
# calculation as the libMesh kelly_error_estimator. If
# this test is diffing... the diff is wrong!
#
# @Requirement F2.40
###########################################################
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
nz = 10
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
[./solution]
type = ParsedFunction
value = (exp(x)-1)/(exp(1)-1)
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./conv]
type = Convection
variable = u
velocity = '1 0 0'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
# Mesh Indicator System
[Adaptivity]
[Indicators]
[error]
type = GradientJumpIndicator
variable = u
[]
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/auxkernels/gap_value/gap_value_subdomain_restricted.i)
[Mesh]
file = nonmatching.e
dim = 2
# This test will not work in parallel with DistributedMesh enabled
# due to a bug in the GeometricSearch system. See #2121 for more
# information.
parallel_type = replicated
[]
[Variables]
[./u]
block = 'left right'
[../]
[]
[AuxVariables]
[./gap_value]
block = left
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = u
boundary = 'leftbottom rightbottom'
value = 0
[../]
[./top]
type = DirichletBC
variable = u
boundary = 'lefttop righttop'
value = 1
[../]
[]
[AuxKernels]
[./gap_value_aux]
type = GapValueAux
variable = gap_value
boundary = leftright
paired_variable = u
paired_boundary = rightleft
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/transfers/multiapp_copy_transfer/errors/sub.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/preconditioners/hmg/diffusion_hmg.i)
[Mesh]
[./dmg]
type = DistributedRectilinearMeshGenerator
nx = 10
ny = 10
dim = 2
[../]
[]
[Variables]
[u1][]
[u2][]
[u3][]
[]
[Kernels]
[./diff_1]
type = Diffusion
variable = u1
[../]
[./diff_2]
type = Diffusion
variable = u2
[../]
[./diff_3]
type = Diffusion
variable = u3
[../]
[]
[BCs]
[./left_1]
type = DirichletBC
variable = u1
boundary = 'left'
value = 0
[../]
[./right_1]
type = DirichletBC
variable = u1
boundary = 'right'
value = 1
[../]
[./left_2]
type = DirichletBC
variable = u2
boundary = 'left'
value = 0
[../]
[./right_2]
type = DirichletBC
variable = u2
boundary = 'right'
value = 2
[../]
[./left_3]
type = DirichletBC
variable = u3
boundary = 'left'
value = 0
[../]
[./right_3]
type = DirichletBC
variable = u3
boundary = 'right'
value = 3
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hmg_use_subspace_coarsening'
petsc_options_value = 'hmg true'
petsc_options = '-snes_view'
[]
[Outputs]
exodus = true
[]
(test/tests/ics/random_ic_test/random_ic_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 50
ny = 50
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
[]
[]
[AuxVariables]
[u_aux]
order = FIRST
family = LAGRANGE
[]
[]
[ICs]
[u]
type = RandomIC
legacy_generator = false
variable = u
[]
[u_aux]
type = RandomIC
legacy_generator = false
variable = u_aux
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/multiapps/picard/pseudo_transient_picard_master.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
parallel_type = replicated
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./v]
[../]
[]
[Kernels]
[./diff]
type = CoefDiffusion
variable = u
coef = 0.1
[../]
[./force_u]
type = CoupledForce
variable = u
v = v
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Postprocessors]
[./unorm]
type = ElementL2Norm
variable = u
execute_on = 'initial timestep_end'
[../]
[./vnorm]
type = ElementL2Norm
variable = v
execute_on = 'initial timestep_end'
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
fixed_point_max_its = 30
fixed_point_rel_tol = 1e-6
[]
[Outputs]
exodus = true
[]
[MultiApps]
[./sub]
type = FullSolveMultiApp
input_files = pseudo_transient_picard_sub.i
no_backup_and_restore = true
[../]
[]
[Transfers]
[./v_from_sub]
type = MultiAppNearestNodeTransfer
from_multi_app = sub
source_variable = v
variable = v
[../]
[./u_to_sub]
type = MultiAppNearestNodeTransfer
to_multi_app = sub
source_variable = u
variable = u
[../]
[]
(test/tests/auxkernels/vector_magnitude/vector_magnitude.i)
[Mesh]
type = GeneratedMesh
dim = 3
xmin = -1
xmax = 1
ymin = -1
ymax = 1
zmin = -1
zmax = 1
nx = 2
ny = 2
nz = 2
[../]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[AuxVariables]
[./vector_x]
initial_condition = 2
[../]
[./vector_y]
initial_condition = 1
[../]
[./vector_z]
initial_condition = 2
[../]
[./magnitude]
[../]
[]
[AuxKernels]
[./vx]
type = ConstantAux
variable = vector_x
value = 2
[../]
[./vy]
type = ConstantAux
variable = vector_y
value = 1
[../]
[./vz]
type = ConstantAux
variable = vector_z
value = 2
[../]
[./magnitude]
type = VectorMagnitudeAux
variable = magnitude
x = vector_x
y = vector_y
z = vector_z
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/exodus/exodus.i)
###########################################################
# This is a simple test demonstrating the ability to create
# a user-defined output type (ExodusII format).
#
# @Requirement F1.70
###########################################################
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
# Demonstration of using an Exodus Outputter
[./out]
type = Exodus
[../]
[]
[Debug]
show_var_residual_norms = true
#show_actions = true
[]
(test/tests/auxkernels/vectorpostprocessor/vectorpostprocessor.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./vpp_0]
order = CONSTANT
family = MONOMIAL
[../]
[./vpp_1]
order = CONSTANT
family = MONOMIAL
[../]
[./vpp_2]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./vpp_0]
type = VectorPostprocessorAux
variable = vpp_0
index = 0
vector = value
vpp = constant
[../]
[./vpp_1]
type = VectorPostprocessorAux
variable = vpp_1
index = 1
vector = value
vpp = constant
[../]
[./vpp_2]
type = VectorPostprocessorAux
variable = vpp_2
index = 2
vector = value
vpp = constant
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[VectorPostprocessors]
[./constant]
type = ConstantVectorPostprocessor
value = '1.2 3.4 9.6'
execute_on = initial
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(python/peacock/tests/common/simple_diffusion2.i)
[Mesh]
[generate]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[new_block]
type = SubdomainBoundingBoxGenerator
input = generate
bottom_left = '0.25 0.25 0'
top_right = '0.75 0.75 0'
block_id = 1980
[]
[]
[Variables]
[not_u]
[]
[]
[AuxVariables]
[aux]
initial_condition = 1980
[]
[u]
initial_condition = 624
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = not_u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = not_u
boundary = left
value = 4
[]
[right]
type = DirichletBC
variable = not_u
boundary = right
value = 6
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/cylindrical/2d-rc-slip.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 2
ymin = 0
ymax = 10
nx = 10
ny = 50
[]
[]
[Problem]
fv_bcs_integrity_check = true
coord_type = 'RZ'
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = ${mu}
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = ${mu}
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = u
function = 0
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = v
function = 1
[]
[free-slip-wall-u]
type = INSFVNaturalFreeSlipBC
boundary = 'right'
variable = u
momentum_component = 'x'
[]
[free-slip-wall-v]
type = INSFVNaturalFreeSlipBC
boundary = 'right'
variable = v
momentum_component = 'y'
[]
[outlet-p]
type = INSFVOutletPressureBC
boundary = 'top'
variable = pressure
function = 0
[]
[axis-u]
type = INSFVSymmetryVelocityBC
boundary = 'left'
variable = u
u = u
v = v
mu = ${mu}
momentum_component = x
[]
[axis-v]
type = INSFVSymmetryVelocityBC
boundary = 'left'
variable = v
u = u
v = v
mu = ${mu}
momentum_component = y
[]
[axis-p]
type = INSFVSymmetryPressureBC
boundary = 'left'
variable = pressure
[]
[]
[Postprocessors]
[in]
type = SideIntegralVariablePostprocessor
variable = v
boundary = 'bottom'
outputs = 'csv'
[]
[out]
type = SideIntegralVariablePostprocessor
variable = v
boundary = 'top'
outputs = 'csv'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
[]
[Outputs]
exodus = true
csv = true
[]
(test/tests/mesh/named_entities/named_entities_test.i)
[Mesh]
file = named_entities.e
uniform_refine = 1
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
block = '1 center_block 3'
[./InitialCondition]
type = ConstantIC
value = 20
block = 'center_block 3'
[../]
[../]
[]
[AuxVariables]
[./reporter]
order = CONSTANT
family = MONOMIAL
block = 'left_block 3'
[../]
[]
[ICs]
[./reporter_ic]
type = ConstantIC
variable = reporter
value = 10
[../]
[]
[Kernels]
active = 'diff body_force'
[./diff]
type = Diffusion
variable = u
# Note we are using both names and numbers here
block = 'left_block 2 right_block'
[../]
[./body_force]
type = BodyForce
variable = u
block = 'center_block'
value = 10
[../]
[]
[AuxKernels]
[./hardness]
type = MaterialRealAux
variable = reporter
property = 'hardness'
block = 'left_block 3'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 'left_side'
value = 1
[../]
[./right]
type = DirichletBC
variable = u
boundary = 'right_side'
value = 1
[../]
[]
[Postprocessors]
[./elem_average]
type = ElementAverageValue
variable = u
block = 'center_block'
execute_on = 'initial timestep_end'
[../]
[./side_average]
type = SideAverageValue
variable = u
boundary = 'right_side'
execute_on = 'initial timestep_end'
[../]
[]
[Materials]
[./constant]
type = GenericConstantMaterial
prop_names = 'hardness'
prop_values = 10
block = '1 right_block'
[../]
[./empty]
type = MTMaterial
block = 'center_block'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/examples/cframe_iga/cframe_iga.i)
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
[igafile]
type = FileMeshGenerator
file = cframe_iga_coarse.e
clear_spline_nodes = true
[]
[]
[Variables]
[disp_x]
order = SECOND
family = RATIONAL_BERNSTEIN
[]
[disp_y]
order = SECOND
family = RATIONAL_BERNSTEIN
[]
[disp_z]
order = SECOND
family = RATIONAL_BERNSTEIN
[]
[]
[Kernels]
[TensorMechanics]
#Stress divergence kernels
displacements = 'disp_x disp_y disp_z'
[]
[]
[AuxVariables]
[von_mises]
#Dependent variable used to visualize the von Mises stress
order = SECOND
family = MONOMIAL
[]
[Max_Princ]
#Dependent variable used to visualize the Hoop stress
order = SECOND
family = MONOMIAL
[]
[stress_xx]
order = SECOND
family = MONOMIAL
[]
[stress_yy]
order = SECOND
family = MONOMIAL
[]
[stress_zz]
order = SECOND
family = MONOMIAL
[]
[]
[AuxKernels]
[von_mises_kernel]
#Calculates the von mises stress and assigns it to von_mises
type = RankTwoScalarAux
variable = von_mises
rank_two_tensor = stress
scalar_type = VonMisesStress
[]
[MaxPrin]
type = RankTwoScalarAux
variable = Max_Princ
rank_two_tensor = stress
scalar_type = MaxPrincipal
[]
[stress_xx]
type = RankTwoAux
index_i = 0
index_j = 0
rank_two_tensor = stress
variable = stress_xx
[]
[stress_yy]
type = RankTwoAux
index_i = 1
index_j = 1
rank_two_tensor = stress
variable = stress_yy
[]
[stress_zz]
type = RankTwoAux
index_i = 2
index_j = 2
rank_two_tensor = stress
variable = stress_zz
[]
[]
[BCs]
[Pressure]
[load]
#Applies the pressure
boundary = '3'
factor = 2000 # psi
[]
[]
[anchor_x]
#Anchors the bottom and sides against deformation in the x-direction
type = DirichletBC
variable = disp_x
boundary = '2'
value = 0.0
[]
[anchor_y]
#Anchors the bottom and sides against deformation in the y-direction
type = DirichletBC
variable = disp_y
boundary = '2'
value = 0.0
[]
[anchor_z]
#Anchors the bottom and sides against deformation in the z-direction
type = DirichletBC
variable = disp_z
boundary = '2'
value = 0.0
[]
[]
[Materials]
[elasticity_tensor_AL]
#Creates the elasticity tensor using concrete parameters
youngs_modulus = 24e6 #psi
poissons_ratio = 0.33
type = ComputeIsotropicElasticityTensor
[]
[strain]
#Computes the strain, assuming small strains
type = ComputeSmallStrain
displacements = 'disp_x disp_y disp_z'
[]
[stress]
#Computes the stress, using linear elasticity
type = ComputeLinearElasticStress
[]
[density_AL]
#Defines the density of steel
type = GenericConstantMaterial
prop_names = density
prop_values = 6.99e-4 # lbm/in^3
[]
[]
[Preconditioning]
[SMP]
#Creates the entire Jacobian, for the Newton solve
type = SMP
full = true
[]
[]
[Postprocessors]
[max_principal_stress]
type = PointValue
point = '0.000000 -1.500000 -4.3'
variable = Max_Princ
use_displaced_mesh = false
[]
[maxPrincStress]
type = ElementExtremeValue
variable = Max_Princ
[]
[]
[Executioner]
# We solve a steady state problem using Newton's iteration
type = Steady
solve_type = NEWTON
nl_rel_tol = 1e-9
l_max_its = 300
l_tol = 1e-4
nl_max_its = 30
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart'
petsc_options_value = 'hypre boomeramg 31'
[]
[Outputs]
vtk = true
[]
(modules/navier_stokes/test/tests/finite_volume/cns/straight_channel_porosity_step/hllc.i)
p_initial=1.01e5
T=273.15
# u refers to the superficial velocity
u_in=1
[GlobalParams]
fp = fp
two_term_boundary_expansion = true
[]
[Mesh]
[cartesian]
type = GeneratedMeshGenerator
dim = 1
xmin = 0
xmax = 18
nx = 180
[]
[to_pt5]
input = cartesian
type = SubdomainBoundingBoxGenerator
bottom_left = '2 0 0'
top_right = '4 1 0'
block_id = 1
[]
[pt5]
input = to_pt5
type = SubdomainBoundingBoxGenerator
bottom_left = '4 0 0'
top_right = '6 1 0'
block_id = 2
[]
[to_pt25]
input = pt5
type = SubdomainBoundingBoxGenerator
bottom_left = '6 0 0'
top_right = '8 1 0'
block_id = 3
[]
[pt25]
input = to_pt25
type = SubdomainBoundingBoxGenerator
bottom_left = '8 0 0'
top_right = '10 1 0'
block_id = 4
[]
[to_pt5_again]
input = pt25
type = SubdomainBoundingBoxGenerator
bottom_left = '10 0 0'
top_right = '12 1 0'
block_id = 5
[]
[pt5_again]
input = to_pt5_again
type = SubdomainBoundingBoxGenerator
bottom_left = '12 0 0'
top_right = '14 1 0'
block_id = 6
[]
[to_one]
input = pt5_again
type = SubdomainBoundingBoxGenerator
bottom_left = '14 0 0'
top_right = '16 1 0'
block_id = 7
[]
[one]
input = to_one
type = SubdomainBoundingBoxGenerator
bottom_left = '16 0 0'
top_right = '18 1 0'
block_id = 8
[]
[]
[Modules]
[FluidProperties]
[fp]
type = IdealGasFluidProperties
[]
[]
[]
[Problem]
fv_bcs_integrity_check = false
[]
[Variables]
[pressure]
type = MooseVariableFVReal
initial_condition = ${p_initial}
[]
[sup_vel_x]
type = MooseVariableFVReal
initial_condition = 1
scaling = 1e-2
[]
[T_fluid]
type = MooseVariableFVReal
initial_condition = ${T}
scaling = 1e-5
[]
[]
[AuxVariables]
[vel_x]
type = MooseVariableFVReal
[]
[sup_mom_x]
type = MooseVariableFVReal
[]
[rho]
type = MooseVariableFVReal
[]
[worst_courant]
type = MooseVariableFVReal
[]
[porosity]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[vel_x]
type = ADMaterialRealAux
variable = vel_x
property = vel_x
execute_on = 'timestep_end'
[]
[sup_mom_x]
type = ADMaterialRealAux
variable = sup_mom_x
property = superficial_rhou
execute_on = 'timestep_end'
[]
[rho]
type = ADMaterialRealAux
variable = rho
property = rho
execute_on = 'timestep_end'
[]
[worst_courant]
type = Courant
variable = worst_courant
u = sup_vel_x
execute_on = 'timestep_end'
[]
[porosity]
type = MaterialRealAux
variable = porosity
property = porosity
execute_on = 'timestep_end'
[]
[]
[FVKernels]
[mass_advection]
type = PCNSFVMassHLLC
variable = pressure
[]
[momentum_advection]
type = PCNSFVMomentumHLLC
variable = sup_vel_x
momentum_component = 'x'
[]
[eps_grad]
type = PNSFVPGradEpsilon
variable = sup_vel_x
momentum_component = 'x'
epsilon_function = 'eps'
[]
[energy_advection]
type = PCNSFVFluidEnergyHLLC
variable = T_fluid
[]
[]
[FVBCs]
[rho_left]
type = PCNSFVStrongBC
boundary = 'left'
variable = pressure
superficial_velocity = 'ud_in'
T_fluid = ${T}
eqn = 'mass'
[]
[rhou_left]
type = PCNSFVStrongBC
boundary = 'left'
variable = sup_vel_x
superficial_velocity = 'ud_in'
T_fluid = ${T}
eqn = 'momentum'
momentum_component = 'x'
[]
[rho_et_left]
type = PCNSFVStrongBC
boundary = 'left'
variable = T_fluid
superficial_velocity = 'ud_in'
T_fluid = ${T}
eqn = 'energy'
[]
[rho_right]
type = PCNSFVStrongBC
boundary = 'right'
variable = pressure
pressure = ${p_initial}
eqn = 'mass'
[]
[rhou_right]
type = PCNSFVStrongBC
boundary = 'right'
variable = sup_vel_x
pressure = ${p_initial}
eqn = 'momentum'
momentum_component = 'x'
[]
[rho_et_right]
type = PCNSFVStrongBC
boundary = 'right'
variable = T_fluid
pressure = ${p_initial}
eqn = 'energy'
[]
# Use these to help create more accurate cell centered gradients for cells adjacent to boundaries
[T_left]
type = FVDirichletBC
variable = T_fluid
value = ${T}
boundary = 'left'
[]
[sup_vel_left]
type = FVDirichletBC
variable = sup_vel_x
value = ${u_in}
boundary = 'left'
[]
[p_right]
type = FVDirichletBC
variable = pressure
value = ${p_initial}
boundary = 'right'
[]
[]
[Functions]
[ud_in]
type = ParsedVectorFunction
value_x = '${u_in}'
[]
[eps]
type = ParsedFunction
value = 'if(x < 2, 1,
if(x < 4, 1 - .5 / 2 * (x - 2),
if(x < 6, .5,
if(x < 8, .5 - .25 / 2 * (x - 6),
if(x < 10, .25,
if(x < 12, .25 + .25 / 2 * (x - 10),
if(x < 14, .5,
if(x < 16, .5 + .5 / 2 * (x - 14),
1))))))))'
[]
[]
[Materials]
[var_mat]
type = PorousPrimitiveVarMaterial
pressure = pressure
T_fluid = T_fluid
superficial_vel_x = sup_vel_x
porosity = porosity
[]
[porosity]
type = GenericFunctionMaterial
prop_names = 'porosity'
prop_values = 'eps'
[]
[]
[Executioner]
solve_type = NEWTON
line_search = 'bt'
type = Steady
[]
[Outputs]
[out]
type = Exodus
execute_on = 'final'
[]
checkpoint = true
[]
[Debug]
show_var_residual_norms = true
[]
(test/tests/bcs/1d_neumann/1d_neumann.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 10
construct_side_list_from_node_list = true
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = NeumannBC
variable = u
boundary = right
value = 2
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/variables/fe_hier/hier-2-3d.i)
[Mesh]
type = GeneratedMesh
dim = 3
xmin = -1
xmax = 1
ymin = -1
ymax = 1
zmin = -1
zmax = 1
nx = 1
ny = 1
nz = 1
elem_type = HEX27
# This problem only has 1 element, so using DistributedMesh in parallel
# isn't really an option, and we don't care that much about DistributedMesh
# in serial.
parallel_type = replicated
[]
[Functions]
[./bc_fnt]
type = ParsedFunction
value = 2*y
[../]
[./bc_fnb]
type = ParsedFunction
value = -2*y
[../]
[./bc_fnl]
type = ParsedFunction
value = -2*x
[../]
[./bc_fnr]
type = ParsedFunction
value = 2*x
[../]
[./bc_fnf]
type = ParsedFunction
value = 2*z
[../]
[./bc_fnk]
type = ParsedFunction
value = -2*z
[../]
[./forcing_fn]
type = ParsedFunction
value = -6+x*x+y*y+z*z
[../]
[./solution]
type = ParsedGradFunction
value = x*x+y*y+z*z
grad_x = 2*x
grad_y = 2*y
grad_z = 2*z
[../]
[]
[Variables]
[./u]
order = SECOND
family = HIERARCHIC
[../]
[]
[Kernels]
active = 'diff forcing reaction'
[./diff]
type = Diffusion
variable = u
[../]
[./reaction]
type = Reaction
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
[./bc_top]
type = FunctionNeumannBC
variable = u
boundary = 'top'
function = bc_fnt
[../]
[./bc_bottom]
type = FunctionNeumannBC
variable = u
boundary = 'bottom'
function = bc_fnb
[../]
[./bc_left]
type = FunctionNeumannBC
variable = u
boundary = 'left'
function = bc_fnl
[../]
[./bc_right]
type = FunctionNeumannBC
variable = u
boundary = 'right'
function = bc_fnr
[../]
[./bc_front]
type = FunctionNeumannBC
variable = u
boundary = 'front'
function = bc_fnf
[../]
[./bc_back]
type = FunctionNeumannBC
variable = u
boundary = 'back'
function = bc_fnk
[../]
[]
[Postprocessors]
[./dofs]
type = NumDOFs
[../]
[./h]
type = AverageElementSize
[../]
[./L2error]
type = ElementL2Error
variable = u
function = solution
[../]
[./H1error]
type = ElementH1Error
variable = u
function = solution
[../]
[./H1Semierror]
type = ElementH1SemiError
variable = u
function = solution
[../]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-11
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
csv = true
[]
(modules/tensor_mechanics/test/tests/ad_linear_elasticity/linear_elastic_material.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmax = 50
ymax = 50
[]
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Variables]
[./diffused]
[./InitialCondition]
type = RandomIC
[../]
[../]
[]
[Modules/TensorMechanics/Master/All]
strain = SMALL
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx'
use_automatic_differentiation = true
[]
[Kernels]
[./diff]
type = ADDiffusion
variable = diffused
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0
[../]
[./stress]
type = ADComputeLinearElasticStress
[../]
[]
[BCs]
[./bottom]
type = ADDirichletBC
variable = diffused
boundary = 'right'
value = 1
[../]
[./top]
type = ADDirichletBC
variable = diffused
boundary = 'top'
value = 0
[../]
[./disp_x_BC]
type = ADDirichletBC
variable = disp_x
boundary = 'bottom top'
value = 0.5
[../]
[./disp_x_BC2]
type = ADDirichletBC
variable = disp_x
boundary = 'left right'
value = 0.01
[../]
[./disp_y_BC]
type = ADDirichletBC
variable = disp_y
boundary = 'bottom top'
value = 0.8
[../]
[./disp_y_BC2]
type = ADDirichletBC
variable = disp_y
boundary = 'left right'
value = 0.02
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(test/tests/markers/uniform_marker/uniform_marker.i)
###########################################################
# This is a test of the Mesh Marker System. It marks
# elements with flags indicating whether they should be
# refined, coarsened, or left alone. This system
# has the ability to use the Mesh Indicator System.
#
# @Requirement F2.50
###########################################################
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
# Mesh Marker System
[Adaptivity]
[./Markers]
[./uniform]
type = UniformMarker
mark = refine
[../]
[../]
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/advection-schemes/test.i)
mu=10
rho=1
[GlobalParams]
velocity_interp_method = 'rc'
advected_interp_method = 'sou'
rhie_chow_user_object = 'rc'
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 11
ny = 11
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
[]
[v]
type = INSFVVelocityVariable
[]
[pressure]
type = INSFVPressureVariable
[]
[lambda]
family = SCALAR
order = FIRST
[]
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
rho = ${rho}
[]
[mean_zero_pressure]
type = FVIntegralValueConstraint
variable = pressure
lambda = lambda
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = u
mu = 'mu'
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = v
mu = 'mu'
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
pressure = pressure
[]
[]
[FVBCs]
[top_x]
type = INSFVNoSlipWallBC
variable = u
boundary = 'top'
function = 1
[]
[no_slip_x]
type = INSFVNoSlipWallBC
variable = u
boundary = 'left right bottom'
function = 0
[]
[no_slip_y]
type = INSFVNoSlipWallBC
variable = v
boundary = 'left right top bottom'
function = 0
[]
[]
[Materials]
[mu]
type = ADGenericFunctorMaterial
prop_names = 'mu'
prop_values = '${mu}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(modules/geochemistry/test/tests/equilibrium_models/HCl_no_action.i)
# This is an example of an input file that does not utilize an action. Its functionality is the same as HCl.i
# This solves for molalities in a system just containing HCl
[GlobalParams]
point = '0 0 0'
[]
[Mesh]
type = GeneratedMesh
dim = 1
nx= 1
[]
[Variables]
[u]
[]
[]
[Kernels]
[u]
type = Diffusion
variable = u
[]
[]
[AuxVariables]
[solution_temperature]
[]
[kg_solvent_H2O]
[]
[activity_H2O]
[]
[bulk_moles_H2O]
[]
[pH]
[]
[molal_H+]
[]
[molal_Cl-]
[]
[molal_HCl]
[]
[molal_OH-]
[]
[mg_per_kg_H+]
[]
[mg_per_kg_Cl-]
[]
[mg_per_kg_HCl]
[]
[mg_per_kg_OH-]
[]
[activity_H+]
[]
[activity_Cl-]
[]
[activity_HCl]
[]
[activity_OH-]
[]
[bulk_moles_H+]
[]
[bulk_moles_Cl-]
[]
[bulk_moles_HCl]
[]
[bulk_moles_OH-]
[]
[]
[AuxKernels]
[solution_temperature]
type = GeochemistryQuantityAux
species = 'H+'
reactor = reactor
variable = solution_temperature
quantity = temperature
[]
[kg_solvent_H2O]
type = GeochemistryQuantityAux
species = 'H2O'
reactor = reactor
variable = kg_solvent_H2O
quantity = molal
[]
[activity_H2O]
type = GeochemistryQuantityAux
species = 'H2O'
reactor = reactor
variable = activity_H2O
quantity = activity
[]
[bulk_moles_H2O]
type = GeochemistryQuantityAux
species = 'H2O'
reactor = reactor
variable = bulk_moles_H2O
quantity = bulk_moles
[]
[pH]
type = GeochemistryQuantityAux
species = 'H+'
reactor = reactor
variable = pH
quantity = neglog10a
[]
[molal_H+]
type = GeochemistryQuantityAux
species = 'H+'
reactor = reactor
variable = 'molal_H+'
quantity = molal
[]
[molal_Cl-]
type = GeochemistryQuantityAux
species = 'Cl-'
reactor = reactor
variable = 'molal_Cl-'
quantity = molal
[]
[molal_HCl]
type = GeochemistryQuantityAux
species = 'HCl'
reactor = reactor
variable = 'molal_HCl'
quantity = molal
[]
[molal_OH-]
type = GeochemistryQuantityAux
species = 'OH-'
reactor = reactor
variable = 'molal_OH-'
quantity = molal
[]
[mg_per_kg_H+]
type = GeochemistryQuantityAux
species = 'H+'
reactor = reactor
variable = 'mg_per_kg_H+'
quantity = mg_per_kg
[]
[mg_per_kg_Cl-]
type = GeochemistryQuantityAux
species = 'Cl-'
reactor = reactor
variable = 'mg_per_kg_Cl-'
quantity = mg_per_kg
[]
[mg_per_kg_HCl]
type = GeochemistryQuantityAux
species = 'HCl'
reactor = reactor
variable = 'mg_per_kg_HCl'
quantity = mg_per_kg
[]
[mg_per_kg_OH-]
type = GeochemistryQuantityAux
species = 'OH-'
reactor = reactor
variable = 'mg_per_kg_OH-'
quantity = mg_per_kg
[]
[activity_H+]
type = GeochemistryQuantityAux
species = 'H+'
reactor = reactor
variable = 'activity_H+'
quantity = activity
[]
[activity_Cl-]
type = GeochemistryQuantityAux
species = 'Cl-'
reactor = reactor
variable = 'activity_Cl-'
quantity = activity
[]
[activity_HCl]
type = GeochemistryQuantityAux
species = 'HCl'
reactor = reactor
variable = 'activity_HCl'
quantity = activity
[]
[activity_OH-]
type = GeochemistryQuantityAux
species = 'OH-'
reactor = reactor
variable = 'activity_OH-'
quantity = activity
[]
[bulk_moles_H+]
type = GeochemistryQuantityAux
species = 'H+'
reactor = reactor
variable = 'bulk_moles_H+'
quantity = bulk_moles
[]
[bulk_moles_Cl-]
type = GeochemistryQuantityAux
species = 'Cl-'
reactor = reactor
variable = 'bulk_moles_Cl-'
quantity = bulk_moles
[]
[bulk_moles_HCl]
type = GeochemistryQuantityAux
species = 'HCl'
reactor = reactor
variable = 'bulk_moles_HCl'
quantity = bulk_moles
[]
[bulk_moles_OH-]
type = GeochemistryQuantityAux
species = 'OH-'
reactor = reactor
variable = 'bulk_moles_OH-'
quantity = bulk_moles
[]
[]
[Postprocessors]
[pH]
type = PointValue
variable = 'pH'
[]
[solvent_mass]
type = PointValue
variable = 'kg_solvent_H2O'
[]
[molal_Cl-]
type = PointValue
variable = 'molal_Cl-'
[]
[mg_per_kg_HCl]
type = PointValue
variable = 'mg_per_kg_HCl'
[]
[activity_OH-]
type = PointValue
variable = 'activity_OH-'
[]
[bulk_H+]
type = PointValue
variable = 'bulk_moles_H+'
[]
[temperature]
type = PointValue
variable = 'solution_temperature'
[]
[]
[Executioner]
type = Steady
[]
[UserObjects]
[definition]
type = GeochemicalModelDefinition
database_file = "../../../database/moose_geochemdb.json"
basis_species = "H2O H+ Cl-"
piecewise_linear_interpolation = true # to reproduce the GWB result
[]
[reactor]
type = GeochemistryTimeDependentReactor
model_definition = definition
charge_balance_species = "Cl-"
constraint_species = "H2O H+ Cl-"
constraint_value = " 1.0 -2 1E-2"
constraint_meaning = "kg_solvent_water log10activity bulk_composition"
constraint_unit = " kg dimensionless moles"
ramp_max_ionic_strength_initial = 0 # max_ionic_strength in such a simple problem does not need ramping
abs_tol = 1E-15
[]
[nnn]
type = NearestNodeNumberUO
[]
[]
[Outputs]
csv = true
[console_output]
type = GeochemistryConsoleOutput
geochemistry_reactor = reactor
nearest_node_number_UO = nnn
solver_info = true
execute_on = initial
[]
[]
(modules/heat_conduction/test/tests/code_verification/cartesian_test_no4.i)
# Problem I.4
#
# An infinite plate with constant thermal conductivity k and internal
# heat generation q. The left boundary is exposed to a constant heat flux q0.
# The right boundary is exposed to a fluid with constant temperature uf and
# heat transfer coefficient h, which results in the convective boundary condition.
#
# REFERENCE:
# A. Toptan, et al. (Mar.2020). Tech. rep. CASL-U-2020-1939-000, SAND2020-3887 R. DOI:10.2172/1614683.
[Mesh]
[./geom]
type = GeneratedMeshGenerator
dim = 1
elem_type = EDGE2
nx = 1
[../]
[]
[Variables]
[./u]
order = FIRST
[../]
[]
[Functions]
[./exact]
type = ParsedFunction
vars = 'q q0 k L uf h'
vals = '1200 200 1 1 100 10.0'
value = 'uf + (q0 + L * q)/h + 0.5 * ( 2 * q0 + q * (L + x)) * (L-x) / k'
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = u
[../]
[./heatsource]
type = HeatSource
function = 1200
variable = u
[../]
[]
[BCs]
[./ui]
type = NeumannBC
boundary = left
variable = u
value = 200
[../]
[./uo]
type = CoupledConvectiveHeatFluxBC
boundary = right
variable = u
htc = 10.0
T_infinity = 100
[../]
[]
[Materials]
[./property]
type = GenericConstantMaterial
prop_names = 'density specific_heat thermal_conductivity'
prop_values = '1.0 1.0 1.0'
[../]
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[./error]
type = ElementL2Error
function = exact
variable = u
[../]
[./h]
type = AverageElementSize
[]
[]
[Outputs]
csv = true
[]
(test/tests/fvkernels/mms/skewness-correction/diffusion/skewed.i)
a=1.1
diff=1.1
[Mesh]
[./gen_mesh]
type = FileMeshGenerator
file = skewed.msh
[../]
[]
[Variables]
[./v]
initial_condition = 1
type = MooseVariableFVReal
face_interp_method = 'skewness-corrected'
cache_face_gradients = false
cache_face_values = true
[../]
[]
[FVKernels]
[diff_v]
type = FVDiffusion
variable = v
coeff = ${diff}
[]
[body_v]
type = FVBodyForce
variable = v
function = 'forcing'
[]
[]
[FVBCs]
[exact]
type = FVFunctionDirichletBC
boundary = 'left right top bottom'
function = 'exact'
variable = v
[]
[]
[Functions]
[exact]
type = ParsedFunction
value = 'sin(x)*cos(y)'
[]
[forcing]
type = ParsedFunction
value = '2*diff*sin(x)*cos(y)'
vars = 'a diff'
vals = '${a} ${diff}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[./error]
type = ElementL2Error
variable = v
function = exact
outputs = 'console csv'
[../]
[h]
type = AverageElementSize
outputs = 'console csv'
[]
[]
(test/tests/preconditioners/fdp/fdp_test.i)
[Mesh]
type = GeneratedMesh
nx = 2
ny = 2
dim = 2
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[Preconditioning]
[./FDP]
type = FDP
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./conv_v]
type = CoupledForce
variable = v
v = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = false
[]
[ICs]
[./u]
variable = u
type = RandomIC
min = 0.1
max = 0.9
[../]
[./v]
variable = v
type = RandomIC
min = 0.1
max = 0.9
[../]
[]
(tutorials/tutorial01_app_development/step06_input_params/test/tests/kernels/simple_diffusion/simple_diffusion.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/userobjects/layered_side_integral/layered_side_average.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 6
ny = 6
nz = 6
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./layered_side_average]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = u
boundary = bottom
value = 0
[../]
[./top]
type = DirichletBC
variable = u
boundary = top
value = 1
[../]
[]
[AuxKernels]
[./lsia]
type = SpatialUserObjectAux
variable = layered_side_average
boundary = right
user_object = layered_side_average
[../]
[]
[UserObjects]
[./layered_side_average]
type = LayeredSideAverage
direction = y
num_layers = 3
variable = u
execute_on = linear
boundary = right
[../]
[]
[VectorPostprocessors]
[avg]
type = SpatialUserObjectVectorPostprocessor
userobject = layered_side_average
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
csv = true
[]
(modules/tensor_mechanics/test/tests/gravity/material_vector_body_force.i)
#
# MaterialVectorBodyForce Test
#
# This test is designed to apply gravity using the MaterialVectorBodyForce kernel/action.
#
# The mesh is composed of one block with a single element.
# The bottom is fixed in all three directions. Poisson's ratio
# is zero, which makes it trivial to check displacements.
#
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
type = GeneratedMesh
dim = 3
[]
[Modules/TensorMechanics]
[Master/all]
add_variables = true
[]
[MaterialVectorBodyForce/all]
body_force = force_density
[]
[]
[BCs]
[no_x]
type = DirichletBC
variable = disp_x
boundary = bottom
value = 0.0
[]
[no_y]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[]
[no_z]
type = DirichletBC
variable = disp_z
boundary = bottom
value = 0.0
[]
[]
[Materials]
[Elasticity_tensor]
type = ComputeElasticityTensor
fill_method = symmetric_isotropic
C_ijkl = '0 0.5e6'
[]
[stress]
type = ComputeLinearElasticStress
[]
[force_density]
type = GenericConstantVectorMaterial
prop_names = force_density
prop_values = '0 -19.9995 0'
[]
[]
[Executioner]
type = Steady
nl_abs_tol = 1e-10
l_max_its = 20
[]
[Outputs]
[out]
type = Exodus
elemental_as_nodal = true
[]
[]
(modules/tensor_mechanics/test/tests/lagrangian/total/stabilization/cook_large.i)
[GlobalParams]
displacements = 'disp_x disp_y'
large_kinematics = true
stabilize_strain = true
[]
[Mesh]
type = FileMesh
file = cook_mesh.exo
dim = 2
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[]
[Kernels]
[sdx]
type = TotalLagrangianStressDivergence
variable = disp_x
component = 0
[]
[sdy]
type = TotalLagrangianStressDivergence
variable = disp_y
component = 1
[]
[]
[AuxVariables]
[strain_xx]
order = CONSTANT
family = MONOMIAL
[]
[strain_yy]
order = CONSTANT
family = MONOMIAL
[]
[strain_zz]
order = CONSTANT
family = MONOMIAL
[]
[strain_xy]
order = CONSTANT
family = MONOMIAL
[]
[strain_xz]
order = CONSTANT
family = MONOMIAL
[]
[strain_yz]
order = CONSTANT
family = MONOMIAL
[]
[stress_xx]
order = CONSTANT
family = MONOMIAL
[]
[stress_yy]
order = CONSTANT
family = MONOMIAL
[]
[stress_zz]
order = CONSTANT
family = MONOMIAL
[]
[stress_xy]
order = CONSTANT
family = MONOMIAL
[]
[stress_yz]
order = CONSTANT
family = MONOMIAL
[]
[stress_xz]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[stress_xx]
type = RankTwoAux
rank_two_tensor = pk1_stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[]
[stress_yy]
type = RankTwoAux
rank_two_tensor = pk1_stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[]
[stress_zz]
type = RankTwoAux
rank_two_tensor = pk1_stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[]
[stress_xy]
type = RankTwoAux
rank_two_tensor = pk1_stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[]
[stress_xz]
type = RankTwoAux
rank_two_tensor = pk1_stress
variable = stress_xz
index_i = 0
index_j = 2
execute_on = timestep_end
[]
[stress_yz]
type = RankTwoAux
rank_two_tensor = pk1_stress
variable = stress_yz
index_i = 1
index_j = 2
execute_on = timestep_end
[]
[strain_xx]
type = RankTwoAux
rank_two_tensor = mechanical_strain
variable = strain_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[]
[strain_yy]
type = RankTwoAux
rank_two_tensor = mechanical_strain
variable = strain_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[]
[strain_zz]
type = RankTwoAux
rank_two_tensor = mechanical_strain
variable = strain_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[]
[strain_xy]
type = RankTwoAux
rank_two_tensor = mechanical_strain
variable = strain_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[]
[strain_xz]
type = RankTwoAux
rank_two_tensor = mechanical_strain
variable = strain_xz
index_i = 0
index_j = 2
execute_on = timestep_end
[]
[strain_yz]
type = RankTwoAux
rank_two_tensor = mechanical_strain
variable = strain_yz
index_i = 1
index_j = 2
execute_on = timestep_end
[]
[]
[BCs]
[fixed_x]
type = DirichletBC
preset = true
variable = disp_x
boundary = canti
value = 0.0
[]
[fixed_y]
type = DirichletBC
preset = true
variable = disp_y
boundary = canti
value = 0.0
[]
[pull]
type = NeumannBC
variable = disp_y
boundary = loading
value = 0.1
[]
[]
[Materials]
[compute_stress]
type = ComputeNeoHookeanStress
lambda = 416666611.0991259
mu = 8300.33333888888926
[]
[compute_strain]
type = ComputeLagrangianStrain
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = 'newton'
line_search = 'none'
petsc_options_iname = -pc_type
petsc_options_value = lu
nl_max_its = 500
nl_abs_tol = 1e-5
nl_rel_tol = 1e-6
[]
[Postprocessors]
[value]
type = PointValue
variable = disp_y
point = '48 60 0'
use_displaced_mesh = false
[]
[]
[Outputs]
exodus = false
csv = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/lid_driven/ad_lid_driven_stabilized_action.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
nx = 64
ny = 64
[]
[]
[Modules]
[IncompressibleNavierStokes]
equation_type = steady-state
velocity_boundary = 'bottom right top left'
velocity_function = '0 0 0 0 lid_function 0 0 0'
pressure_pinned_node = 0
density_name = rho
dynamic_viscosity_name = mu
initial_velocity = '1e-15 1e-15 0'
use_ad = true
pspg = true
supg = true
alpha = 0.1
family = LAGRANGE
order = FIRST
[]
[]
[Materials]
[const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '1 1'
[]
[]
[Functions]
[lid_function]
# We pick a function that is exactly represented in the velocity
# space so that the Dirichlet conditions are the same regardless
# of the mesh spacing.
type = ParsedFunction
value = '4*x*(1-x)'
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
line_search = 'none'
nl_rel_tol = 1e-12
nl_abs_tol = 1e-13
nl_max_its = 6
l_tol = 1e-6
l_max_its = 500
[]
[Outputs]
exodus = true
file_base = lid_driven_stabilized_out
[]
[Postprocessors]
[lin]
type = NumLinearIterations
[]
[nl]
type = NumNonlinearIterations
[]
[lin_tot]
type = CumulativeValuePostprocessor
postprocessor = 'lin'
[]
[nl_tot]
type = CumulativeValuePostprocessor
postprocessor = 'nl'
[]
[]
(test/tests/postprocessors/difference_pps/difference_depend_check.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./v]
[../]
[]
[AuxKernels]
[./one]
type = ConstantAux
variable = v
value = 1
[../]
[]
[Postprocessors]
# This postprocessor is listed first on purpose to give the resolver something to do
[./diff]
type = DifferencePostprocessor
value1 = nodes
value2 = elems
execute_on = 'initial timestep_end'
[../]
[./nodes]
type = NumNodes
execute_on = 'initial timestep_end'
[../]
[./elems]
type = NumElems
execute_on = 'initial timestep_end'
[../]
[]
[Problem]
type = FEProblem
solve = false
kernel_coverage_check = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
[]
(modules/ray_tracing/test/tests/traceray/internal_sidesets/internal_sidesets_2d.i)
[Mesh]
[cmg]
type = CartesianMeshGenerator
dim = 2
dx = '2 2 2'
dy = '2 2 2'
ix = '2 2 2'
iy = '2 2 2'
subdomain_id = '0 1 0
2 5 3
0 4 0'
[]
[interior_bottom]
type = SideSetsBetweenSubdomainsGenerator
input = cmg
primary_block = 5
paired_block = 1
new_boundary = 'interior_bottom'
[]
[interior_left]
type = SideSetsBetweenSubdomainsGenerator
input = interior_bottom
primary_block = 5
paired_block = 2
new_boundary = 'interior_left'
[]
[interior_right]
type = SideSetsBetweenSubdomainsGenerator
input = interior_left
primary_block = 5
paired_block = 3
new_boundary = 'interior_right'
[]
[interior_top]
type = SideSetsBetweenSubdomainsGenerator
input = interior_right
primary_block = 5
paired_block = 4
new_boundary = 'interior_top'
[]
[]
[RayBCs]
active = 'kill_internal'
# active = 'kill_external reflect_internal'
# for testing internal kill
[kill_internal]
type = KillRayBC
boundary = 'interior_top interior_right interior_bottom interior_left'
[]
# for testing internal reflect
[kill_external]
type = KillRayBC
boundary = 'top right bottom left'
[]
[reflect_internal]
type = ReflectRayBC
boundary = 'interior_top interior_right interior_bottom interior_left'
[]
[]
[UserObjects/study]
type = RepeatableRayStudy
start_points = '0 0 0
2 4 0
6 6 0
0 2.5 0
3 6 0
2.5 2.5 0'
directions = '1 1 0
1 -1 0
-1 -1 0
1 0.1 0
0 -1 0
0.5 1.5 0'
names = 'to_bottom_left_corner
at_top_left_corner
to_top_right_corner
to_left_offset
to_top_center_node
inside_to_top'
ray_distance = 10
execute_on = initial
ray_kernel_coverage_check = false
use_internal_sidesets = true
[]
[Postprocessors/total_distance]
type = RayTracingStudyResult
study = study
result = total_distance
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Outputs]
exodus = false
csv = true
[]
(test/tests/bcs/ad_1d_neumann/from_cubit.i)
[Mesh]
file = 1d_line.e
construct_side_list_from_node_list = true
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./right]
type = ADNeumannBC
variable = u
boundary = 2
value = 2
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/mesh_modifiers/assign_element_subdomain_id/quad_with_subdomainid_test.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 2
nz = 0
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[subdomain_id]
type = ElementSubdomainIDGenerator
input = gen
subdomain_ids = '0 1
1 1'
[]
[]
[Variables]
active = 'u'
[u]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
active = 'diff'
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
active = 'left right'
# Mesh Generation produces boundaries in counter-clockwise fashion
[left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out_quad_subdomain_id
exodus = true
[]
(test/tests/kernels/ad_reaction/ad_reaction.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
[]
[Variables]
[u]
[]
[]
[Kernels]
[diffusion]
type = ADDiffusion
variable = u
[]
[reaction]
type = ADReaction
variable = u
[]
[force]
type = ADBodyForce
variable = u
[]
[]
[BCs]
[left]
type = ADDirichletBC
boundary = left
variable = u
value = 0
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(test/tests/dgkernels/ad_dg_diffusion/2d_diffusion_ad_dg_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
elem_type = QUAD4
[]
[Variables]
[./u]
order = FIRST
family = MONOMIAL
[./InitialCondition]
type = ConstantIC
value = 1
[../]
[../]
[]
[Functions]
[./forcing_fn]
type = ParsedFunction
value = 2*pow(e,-x-(y*y))*(1-2*y*y)
[../]
[./exact_fn]
type = ParsedGradFunction
value = pow(e,-x-(y*y))
grad_x = -pow(e,-x-(y*y))
grad_y = -2*y*pow(e,-x-(y*y))
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./abs] # u * v
type = Reaction
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[DGKernels]
[./dg_diff]
type = ADDGDiffusion
variable = u
epsilon = -1
sigma = 6
diff = diff
[../]
[]
[Materials]
[./ad_coupled_mat]
type = ADCoupledMaterial
coupled_var = u
ad_mat_prop = diff
regular_mat_prop = diff_regular
[../]
[]
[BCs]
[./all]
type = DGFunctionDiffusionDirichletBC
variable = u
boundary = '0 1 2 3'
function = exact_fn
epsilon = -1
sigma = 6
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[./Adaptivity]
steps = 2
refine_fraction = 1.0
coarsen_fraction = 0
max_h_level = 8
[../]
nl_rel_tol = 1e-10
[]
[Postprocessors]
[./h]
type = AverageElementSize
[../]
[./dofs]
type = NumDOFs
[../]
[./l2_err]
type = ElementL2Error
variable = u
function = exact_fn
[../]
[]
[Outputs]
exodus = true
csv = true
[]
(test/tests/functions/image_function/moose_logo_test_2D.i)
[Problem]
solve = false
[]
[Mesh]
type = ImageMesh
cells_per_pixel = 1
dim = 2
file = moose_logo_small.png
[]
[Variables]
[original]
family = MONOMIAL
order = CONSTANT
[]
[scaled]
family = MONOMIAL
order = CONSTANT
[]
[shifted]
family = MONOMIAL
order = CONSTANT
[]
[]
[Functions]
[image]
type = ImageFunction
file = moose_logo_small.png
[]
[image_scale]
type = ImageFunction
file = moose_logo_small.png
scale = 0.00392156862
[]
[image_shift]
type = ImageFunction
file = moose_logo_small.png
shift = -127.5
[]
[]
[ICs]
[original_IC]
type = FunctionIC
function = image
variable = original
[]
[scaled_IC]
type = FunctionIC
function = image_scale
variable = scaled
[]
[shifted_IC]
type = FunctionIC
function = image_shift
variable = shifted
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/materials/discrete/recompute2.i)
[Mesh]
[generator]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 1
[]
[left_domain]
type = SubdomainBoundingBoxGenerator
input = generator
bottom_left = '0 0 0'
top_right = '0.5 1 0'
block_id = 10
[]
[]
[Variables]
[./u]
initial_condition = 2
[../]
[]
[Kernels]
[./diff]
type = MatDiffusionTest
variable = u
prop_name = 'p'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 2
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 3
[../]
[]
[Materials]
[./recompute_props]
type = RecomputeMaterial
block = 0
f_name = 'f'
f_prime_name = 'f_prime'
p_name = 'p'
outputs = all
output_properties = 'f f_prime p'
constant = 3
compute = false # make this material "discrete"
[../]
[./newton]
type = NewtonMaterial
block = 0
outputs = all
f_name = 'f'
f_prime_name = 'f_prime'
p_name = 'p'
material = 'recompute_props'
[../]
[./left]
type = GenericConstantMaterial
prop_names = 'f f_prime p'
prop_values = '1 0.5 1.2345'
block = 10
outputs = all
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
print_linear_residuals = true
perf_graph = true
[]
(test/tests/materials/functor_properties/wrong-type.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 10
xmax = 2
[]
[]
[Variables]
[u][]
[]
[Kernels]
[diff_u]
type = FunctorMatDiffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = 'left'
value = 1
[]
[right]
type = DirichletBC
variable = u
boundary = 'right'
value = 0
[]
[]
[Materials]
[request_ad]
type = FEFVCouplingMaterial
retrieved_prop_name = 'prop'
[]
[declare_regular]
type = GenericFunctorMaterial
prop_names = 'prop'
prop_values = '1'
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/ray_tracing/test/tests/actions/add_raykernel_action/add_raykernel_action.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
[]
[]
[UserObjects]
active = ''
[study]
type = RepeatableRayStudy
start_points = '0 0 0'
directions = '1 0 0'
names = 'ray'
[]
[another_study]
type = RepeatableRayStudy
start_points = '0 0 0'
directions = '1 0 0'
names = 'ray'
[]
[not_a_study]
type = VerifyElementUniqueID
[]
[]
[RayKernels]
active = ''
[missing_study_by_name]
type = NullRayKernel
study = dummy
[]
[not_a_study]
type = NullRayKernel
study = not_a_study
[]
[multiple_studies]
type = NullRayKernel
[]
[missing_study]
type = NullRayKernel
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
(test/tests/parser/param_substitution/unit_conversion.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Variables]
[./u]
[../]
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[./km_to_m]
type = FunctionValuePostprocessor
function = ${units 1 km -> m}
[../]
[./Jmol_to_eVat]
type = FunctionValuePostprocessor
function = ${units 1 J/mol -> eV/at}
[../]
[./mW]
type = FunctionValuePostprocessor
function = ${units 3 mW}
[../]
[]
[Outputs]
csv = true
[]
(test/tests/misc/check_error/function_file_test11.i)
# Test for usage of missing function
[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = ic_function
[../]
[../]
[]
[Functions]
[./ic_function]
type = PiecewiseLinear
data_file = piecewise_linear_columns_more_data.csv #Will generate error because data has more than two columns
format = columns
scale_factor = 1.0
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/thermal_hydraulics/test/tests/jacobians/bcs/convection_heat_transfer_bc/convection_heat_transfer_bc.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
[]
[Variables]
[T]
initial_condition = 300
[]
[]
[BCs]
[bc]
type = ConvectionHeatTransferBC
variable = T
boundary = 0
htc_ambient = 0.5
T_ambient = 400
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Problem]
kernel_coverage_check = false
[]
[Executioner]
type = Steady
petsc_options = '-snes_test_jacobian'
petsc_options_iname = '-snes_test_error'
petsc_options_value = '1e-8'
[]
(test/tests/mesh/high_order_elems/high_order_elems.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/scalar_adr/supg/tauOpt.i)
velocity=1
[GlobalParams]
u = ${velocity}
pressure = 0
tau_type = opt
[]
[Mesh]
type = GeneratedMesh
dim = 1
nx = 15
xmax = 15
[]
[Variables]
[./c]
[../]
[]
[Kernels]
[./adv]
type = Advection
variable = c
forcing_func = 'ffn'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = c
boundary = left
value = 0
[../]
[]
[Materials]
[./mat]
# These Materials are required by the INSBase class; we don't use them for anything.
type = GenericConstantMaterial
prop_names = 'mu rho'
prop_values = '0 1'
[../]
[]
[Functions]
[./ffn]
type = ParsedFunction
value = 'if(x < 6, 1 - .25 * x, if(x < 8, -2 + .25 * x, 0))'
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/json/distributed/distributed.i)
[Mesh]
[generate]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
[]
[]
[Adaptivity]
initial_marker = marker
[Markers/marker]
type = BoxMarker
bottom_left = '0 0 0'
top_right = '1 0.5 0'
inside = 'refine'
outside = 'do_nothing'
[]
[]
[Variables/u]
[]
[Executioner]
type = Steady
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[Reporters/mesh_info]
type = MeshInfo
[]
[Outputs]
json = true
[]
(test/tests/outputs/debug/show_var_residual_norms_debug.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 10
ny = 10
elem_type = QUAD9
[]
[Functions]
[./forcing_fnu]
type = ParsedFunction
value = -5.8*(x+y)+x*x*x-x+y*y*y-y
[../]
[./forcing_fnv]
type = ParsedFunction
value = -4
[../]
[./slnu]
type = ParsedGradFunction
value = x*x*x-x+y*y*y-y
grad_x = 3*x*x-1
grad_y = 3*y*y-1
[../]
[./slnv]
type = ParsedGradFunction
value = x*x+y*y
grad_x = 2*x
grad_y = 2*y
[../]
#NeumannBC functions
[./bc_fnut]
type = ParsedFunction
value = 3*y*y-1
[../]
[./bc_fnub]
type = ParsedFunction
value = -3*y*y+1
[../]
[./bc_fnul]
type = ParsedFunction
value = -3*x*x+1
[../]
[./bc_fnur]
type = ParsedFunction
value = 3*x*x-1
[../]
[]
[Variables]
[./u]
order = THIRD
family = HIERARCHIC
[../]
[./v]
order = SECOND
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff1 diff2 test1 forceu forcev react'
[./diff1]
type = Diffusion
variable = u
[../]
[./test1]
type = CoupledConvection
variable = u
velocity_vector = v
[../]
[./diff2]
type = Diffusion
variable = v
[../]
[./react]
type = Reaction
variable = u
[../]
[./forceu]
type = BodyForce
variable = u
function = forcing_fnu
[../]
[./forcev]
type = BodyForce
variable = v
function = forcing_fnv
[../]
[]
[BCs]
active = 'bc_u_tb bc_v bc_ul bc_ur bc_ut bc_ub'
[./bc_u]
type = FunctionPenaltyDirichletBC
variable = u
function = slnu
boundary = 'left right top bottom'
penalty = 1e6
[../]
[./bc_v]
type = FunctionDirichletBC
variable = v
function = slnv
boundary = 'left right top bottom'
[../]
[./bc_u_lr]
type = FunctionPenaltyDirichletBC
variable = u
function = slnu
boundary = 'left right top bottom'
penalty = 1e6
[../]
[./bc_u_tb]
type = CoupledKernelGradBC
variable = u
var2 = v
vel = '0.1 0.1'
boundary = 'top bottom left right'
[../]
[./bc_ul]
type = FunctionNeumannBC
variable = u
function = bc_fnul
boundary = 'left'
[../]
[./bc_ur]
type = FunctionNeumannBC
variable = u
function = bc_fnur
boundary = 'right'
[../]
[./bc_ut]
type = FunctionNeumannBC
variable = u
function = bc_fnut
boundary = 'top'
[../]
[./bc_ub]
type = FunctionNeumannBC
variable = u
function = bc_fnub
boundary = 'bottom'
[../]
[]
[Preconditioning]
active = ' '
[./prec]
type = SMP
full = true
[../]
[]
[Postprocessors]
active='L2u L2v'
[./dofs]
type = NumDOFs
[../]
[./h]
type = AverageElementSize
[../]
[./L2u]
type = ElementL2Error
variable = u
function = slnu
[../]
[./L2v]
type = ElementL2Error
variable = v
function = slnv
[../]
[./H1error]
type = ElementH1Error
variable = u
function = solution
[../]
[./H1Semierror]
type = ElementH1SemiError
variable = u
function = solution
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
# petsc_options = '-snes'
nl_rel_tol = 1e-15
nl_abs_tol = 1e-13
[]
[Outputs]
execute_on = 'timestep_end'
[]
[Debug]
show_var_residual_norms = true
[]
(test/tests/misc/check_error/checked_pointer_param_test.i)
# The extra 'x' before the Mesh section below is intentional.
# We want to catch this type of error.
x[Mesh]
[./square]
type = GeneratedMeshGenerator
nx = 2
ny = 2
dim = 2
[../]
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/fluid_properties/test/tests/auxkernels/stagnation_pressure_aux.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./specific_internal_energy]
[../]
[./specific_volume]
[../]
[./velocity]
[../]
[./stagnation_pressure]
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./specific_internal_energy_ak]
type = ConstantAux
variable = specific_internal_energy
value = 1026.2e3
[../]
[./specific_volume_ak]
type = ConstantAux
variable = specific_volume
value = 0.0012192
[../]
[./velocity_ak]
type = ConstantAux
variable = velocity
value = 10.0
[../]
[./stagnation_pressure_ak]
type = StagnationPressureAux
variable = stagnation_pressure
e = specific_internal_energy
v = specific_volume
vel = velocity
fp = eos
[../]
[]
[Modules]
[./FluidProperties]
[./eos]
type = StiffenedGasFluidProperties
gamma = 2.35
q = -1167e3
q_prime = 0.0
p_inf = 1e9
cv = 1816.0
[../]
[]
[]
[BCs]
[./left_u]
type = DirichletBC
variable = u
boundary = 0
value = 1
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 2
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/outputs/csv/csv_sort.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[AuxVariables]
[./aux0]
order = SECOND
family = SCALAR
[../]
[./aux1]
family = SCALAR
initial_condition = 5
[../]
[./aux2]
family = SCALAR
initial_condition = 10
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./diff_v]
type = CoefDiffusion
variable = v
coef = 2
[../]
[]
[BCs]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[./left_u]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = right
value = 3
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = left
value = 2
[../]
[]
[Postprocessors]
[./num_vars]
type = NumVars
system = 'NL'
[../]
[./num_aux]
type = NumVars
system = 'AUX'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
[./out]
type = CSV
sort_columns = true
[../]
[]
[ICs]
[./aux0_IC]
variable = aux0
values = '12 13'
type = ScalarComponentIC
[../]
[]
(test/tests/misc/save_in/save_in_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./saved]
[../]
[./bc_saved]
[../]
[./accumulated]
[../]
[./diag_saved]
[../]
[./bc_diag_saved]
[../]
[./saved_dirichlet]
[../]
[./diag_saved_dirichlet]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
save_in = 'saved accumulated saved_dirichlet'
diag_save_in = 'diag_saved diag_saved_dirichlet'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
save_in = saved_dirichlet
diag_save_in = diag_saved_dirichlet
[../]
[./nbc]
type = NeumannBC
variable = u
boundary = right
value = 1
save_in = 'bc_saved accumulated'
diag_save_in = bc_diag_saved
[../]
[]
[Postprocessors]
[./left_flux]
type = NodalSum
variable = saved
boundary = 1
[../]
[./saved_norm]
type = NodalL2Norm
variable = saved
execute_on = timestep_end
block = 0
[../]
[./saved_dirichlet_norm]
type = NodalL2Norm
variable = saved_dirichlet
execute_on = timestep_end
block = 0
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
file_base = out
exodus = true
[]
(test/tests/indicators/value_jump_indicator/value_jump_indicator_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Adaptivity]
[./Indicators]
[./error]
type = ValueJumpIndicator
variable = something
[../]
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./leftright]
type = BoundingBoxIC
variable = something
inside = 1
y2 = 1
y1 = 0
x2 = 0.5
x1 = 0
[../]
[]
[AuxVariables]
[./something]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 'left'
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 'right'
value = 1
[../]
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Steady
solve_type = PJFNK
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/ad_action/two_block.i)
[Mesh]
[generated_mesh]
type = GeneratedMeshGenerator
dim = 2
nx = 4
ny = 4
[]
[block1]
type = SubdomainBoundingBoxGenerator
block_id = 1
bottom_left = '0 0 0'
top_right = '0.5 1 0'
input = generated_mesh
[]
[block2]
type = SubdomainBoundingBoxGenerator
block_id = 2
bottom_left = '0.5 0 0'
top_right = '1 1 0'
input = block1
[]
[]
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Modules/TensorMechanics/Master]
[./block1]
strain = FINITE
add_variables = true
#block = 1
use_automatic_differentiation = true
[../]
[./block2]
strain = SMALL
add_variables = true
block = 2
use_automatic_differentiation = true
[../]
[]
[AuxVariables]
[./stress_theta]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_theta]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./stress_theta]
type = ADRankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 2
variable = stress_theta
execute_on = timestep_end
[../]
[./strain_theta]
type = ADRankTwoAux
rank_two_tensor = total_strain
index_i = 2
index_j = 2
variable = strain_theta
execute_on = timestep_end
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1e10
poissons_ratio = 0.345
[../]
[./_elastic_stress1]
type = ADComputeFiniteStrainElasticStress
block = 1
[../]
[./_elastic_stress2]
type = ADComputeLinearElasticStress
block = 2
[../]
[]
[BCs]
[./left]
type = DirichletBC
boundary = 'left'
variable = disp_x
value = 0.0
[../]
[./top]
type = DirichletBC
boundary = 'top'
variable = disp_y
value = 0.0
[../]
[./right]
type = DirichletBC
boundary = 'right'
variable = disp_x
value = 0.01
[../]
[./bottom]
type = DirichletBC
boundary = 'bottom'
variable = disp_y
value = 0.01
[../]
[]
[Debug]
show_var_residual_norms = true
[]
[Preconditioning]
[./full]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = ' 201 hypre boomeramg 10'
line_search = 'none'
nl_rel_tol = 5e-9
nl_abs_tol = 1e-10
nl_max_its = 15
l_tol = 1e-3
l_max_its = 50
[]
[Outputs]
exodus = true
[]
(test/tests/interfacekernels/1d_interface/reaction_1D_steady.i)
# Steady-state test for the InterfaceReaction kernel.
#
# Specie M transport from domain 1 (0<=x<=1) to domain 2 (1<x<=2),
# u and v are concentrations in domain 1 and domain 2.
#
# Diffusion in both domains can be described by Ficks law and diffusion
# kernel is applied.
#
# Specie M has different diffusity in different domains, here set as D1=4, D2=2.
#
# Dirichlet boundary conditions are applied, i.e., u(0)=1, v(2)=0
#
# At the interface consider the following
#
# (a) Fluxes are matched from both domains (InterfaceDiffusion kernel)
#
# (b) First-order reaction is R = kf*u - kb*v
#
# Analytical solution is
# u = -0.2*u+1, 0<=u<=1
# v = -0.4*v+0.8, 1<v<=2
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 10
xmax = 2
[]
[./subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '1.0 0 0'
block_id = 1
top_right = '2.0 1.0 0'
[../]
[./interface]
type = SideSetsBetweenSubdomainsGenerator
input = 'subdomain1'
primary_block = '0'
paired_block = '1'
new_boundary = 'primary0_interface'
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
block = '0'
[../]
[./v]
order = FIRST
family = LAGRANGE
block = '1'
[../]
[]
[Kernels]
[./diff_u]
type = MatDiffusion
variable = u
block = '0'
diffusivity = D
[../]
[./diff_v]
type = MatDiffusion
variable = v
block = '1'
diffusivity = D
[../]
[]
[InterfaceKernels]
[./interface]
type = InterfaceDiffusion
variable = u
neighbor_var = 'v'
boundary = 'primary0_interface'
D = D
D_neighbor = D
[../]
[./interface_reaction]
type = InterfaceReaction
variable = u
neighbor_var = 'v'
boundary = 'primary0_interface'
kf = 1 # Forward reaction rate coefficient
kb = 2 # Backward reaction rate coefficient
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 'left'
value = 1
[../]
[./right]
type = DirichletBC
variable = v
boundary = 'right'
value = 0
[../]
[]
[Materials]
[./block0]
type = GenericConstantMaterial
block = '0'
prop_names = 'D'
prop_values = '4'
[../]
[./block1]
type = GenericConstantMaterial
block = '1'
prop_names = 'D'
prop_values = '2'
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
nl_rel_tol = 1e-10
[]
[Outputs]
print_linear_residuals = true
execute_on = 'FINAL'
exodus = true
csv = true
[]
[Debug]
show_var_residual_norms = true
[]
[Postprocessors]
[./elemental_error_u]
type = ElementL2Error
function = -0.2*x+1
variable = 'u'
block = '0'
[../]
[./elemental_error_v]
type = ElementL2Error
function = -0.4*x+0.8
variable = 'v'
block = '1'
[../]
[]
(test/tests/materials/interface_material/interface_value_material.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 2
xmax = 2
ny = 2
ymax = 2
elem_type = QUAD4
[]
[./subdomain_id]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '1 0 0'
top_right = '2 2 0'
block_id = 1
[../]
[./interface]
type = SideSetsBetweenSubdomainsGenerator
input = subdomain_id
primary_block = '0'
paired_block = '1'
new_boundary = 'interface'
[../]
[]
[Variables]
[./u]
block = 0
[../]
[./v]
block = 1
[../]
[]
[Kernels]
[./diff]
type = MatDiffusion
variable = u
diffusivity = 'diffusivity'
block = 0
[../]
[./diff_v]
type = MatDiffusion
variable = v
diffusivity = 'diffusivity'
block = 1
[../]
[]
[InterfaceKernels]
[tied]
type = PenaltyInterfaceDiffusion
variable = u
neighbor_var = v
jump_prop_name = "average_jump"
penalty = 1e6
boundary = 'interface'
[]
[]
[BCs]
[u_left]
type = DirichletBC
boundary = 'left'
variable = u
value = 1
[]
[v_right]
type = DirichletBC
boundary = 'right'
variable = v
value = 0
[]
[]
[Materials]
[./stateful1]
type = StatefulMaterial
block = 0
initial_diffusivity = 1
# outputs = all
[../]
[./stateful2]
type = StatefulMaterial
block = 1
initial_diffusivity = 2
# outputs = all
[../]
[./interface_material_avg]
type = InterfaceValueMaterial
mat_prop_primary = diffusivity
mat_prop_secondary = diffusivity
var_primary = diffusivity_var
var_secondary = diffusivity_var
mat_prop_out_basename = diff
boundary = interface
interface_value_type = average
mat_prop_var_out_basename = diff_var
nl_var_primary = u
nl_var_secondary = v
[../]
[./interface_material_jump_primary_minus_secondary]
type = InterfaceValueMaterial
mat_prop_primary = diffusivity
mat_prop_secondary = diffusivity
var_primary = diffusivity_var
var_secondary = diffusivity_var
mat_prop_out_basename = diff
boundary = interface
interface_value_type = jump_primary_minus_secondary
mat_prop_var_out_basename = diff_var
nl_var_primary = u
nl_var_secondary = v
[../]
[./interface_material_jump_secondary_minus_primary]
type = InterfaceValueMaterial
mat_prop_primary = diffusivity
mat_prop_secondary = diffusivity
var_primary = diffusivity_var
var_secondary = diffusivity_var
mat_prop_out_basename = diff
boundary = interface
interface_value_type = jump_secondary_minus_primary
mat_prop_var_out_basename = diff_var
nl_var_primary = u
nl_var_secondary = v
[../]
[./interface_material_jump_abs]
type = InterfaceValueMaterial
mat_prop_primary = diffusivity
mat_prop_secondary = diffusivity
var_primary = diffusivity_var
var_secondary = diffusivity_var
mat_prop_out_basename = diff
boundary = interface
interface_value_type = jump_abs
mat_prop_var_out_basename = diff_var
nl_var_primary = u
nl_var_secondary = v
[../]
[./interface_material_primary]
type = InterfaceValueMaterial
mat_prop_primary = diffusivity
mat_prop_secondary = diffusivity
var_primary = diffusivity_var
var_secondary = diffusivity_var
mat_prop_out_basename = diff
boundary = interface
interface_value_type = primary
mat_prop_var_out_basename = diff_var
nl_var_primary = u
nl_var_secondary = v
[../]
[./interface_material_secondary]
type = InterfaceValueMaterial
mat_prop_primary = diffusivity
mat_prop_secondary = diffusivity
var_primary = diffusivity_var
var_secondary = diffusivity_var
mat_prop_out_basename = diff
mat_prop_var_out_basename = diff_var
boundary = interface
interface_value_type = secondary
nl_var_primary = u
nl_var_secondary = v
[../]
[]
[AuxKernels]
[./interface_material_avg]
type = MaterialRealAux
property = diff_average
variable = diffusivity_average
boundary = interface
[]
[./interface_material_jump_primary_minus_secondary]
type = MaterialRealAux
property = diff_jump_primary_minus_secondary
variable = diffusivity_jump_primary_minus_secondary
boundary = interface
[]
[./interface_material_jump_secondary_minus_primary]
type = MaterialRealAux
property = diff_jump_secondary_minus_primary
variable = diffusivity_jump_secondary_minus_primary
boundary = interface
[]
[./interface_material_jump_abs]
type = MaterialRealAux
property = diff_jump_abs
variable = diffusivity_jump_abs
boundary = interface
[]
[./interface_material_primary]
type = MaterialRealAux
property = diff_primary
variable = diffusivity_primary
boundary = interface
[]
[./interface_material_secondary]
type = MaterialRealAux
property = diff_secondary
variable = diffusivity_secondary
boundary = interface
[]
[diffusivity_var]
type = MaterialRealAux
property = diffusivity
variable = diffusivity_var
[]
[]
[AuxVariables]
[diffusivity_var]
family = MONOMIAL
order = CONSTANT
[]
[./diffusivity_average]
family = MONOMIAL
order = CONSTANT
[]
[./diffusivity_jump_primary_minus_secondary]
family = MONOMIAL
order = CONSTANT
[]
[./diffusivity_jump_secondary_minus_primary]
family = MONOMIAL
order = CONSTANT
[]
[./diffusivity_jump_abs]
family = MONOMIAL
order = CONSTANT
[]
[./diffusivity_primary]
family = MONOMIAL
order = CONSTANT
[]
[./diffusivity_secondary]
family = MONOMIAL
order = CONSTANT
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(tutorials/darcy_thermo_mech/step03_darcy_material/tests/materials/packed_column/packed_column.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 100
ny = 10
xmax = 0.304 # Length of test chamber
ymax = 0.0257 # Test chamber radius
[]
[Variables]
[pressure]
[]
[]
[Kernels]
[darcy_pressure]
type = DarcyPressure
variable = pressure
# No parameters necessary because the values will come from the material system
[]
[]
[BCs]
[inlet]
type = DirichletBC
variable = pressure
boundary = left
value = 4000 # (Pa) From Figure 2 from paper. First dot for 1mm spheres.
[]
[outlet]
type = DirichletBC
variable = pressure
boundary = right
value = 0 # (Pa) Gives the correct pressure drop from Figure 2 for 1mm spheres
[]
[]
[Materials]
[column]
type = PackedColumn
[]
[]
[Problem]
type = FEProblem
coord_type = RZ
rz_coord_axis = X
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(modules/fluid_properties/test/tests/auxkernels/specific_enthalpy_aux.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./pressure]
[../]
[./temperature]
[../]
[./specific_enthalpy]
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./pressure_ak]
type = ConstantAux
variable = pressure
value = 10e6
[../]
[./temperature_ak]
type = ConstantAux
variable = temperature
value = 400.0
[../]
[./specific_enthalpy_ak]
type = SpecificEnthalpyAux
variable = specific_enthalpy
fp = eos
p = pressure
T = temperature
[../]
[]
[Modules]
[./FluidProperties]
[./eos]
type = StiffenedGasFluidProperties
gamma = 2.35
q = -1167e3
q_prime = 0.0
p_inf = 1e9
cv = 1816.0
[../]
[]
[]
[BCs]
[./left_u]
type = DirichletBC
variable = u
boundary = 0
value = 1
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 2
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(test/tests/userobjects/layered_average/layered_average_bounds.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./layered_average]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./layered_average]
type = SpatialUserObjectAux
variable = layered_average
execute_on = timestep_end
user_object = average
[../]
[]
[BCs]
[./top]
type = DirichletBC
variable = u
boundary = top
value = 1
[../]
[./bottom]
type = DirichletBC
variable = u
boundary = bottom
value = 0
[../]
[]
[UserObjects]
[./average]
type = LayeredAverage
variable = u
direction = y
bounds = '0 0.2 0.5 1'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/functions/parsed/vals_error.i)
[Mesh]
type = GeneratedMesh
dim = 1
[]
[Variables]
[./dummy1]
[../]
[]
[Problem]
kernel_coverage_check = false
[]
[Functions]
[./left_bc]
type = ParsedFunction
value = dummy2
vals = invalid
vars = dummy2
[../]
[]
[Executioner]
type = Steady
[]
(test/tests/tag/tag_interface_kernels.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
nx = 2
xmax = 2
ny = 2
ymax = 2
nz = 2
zmax = 2
[]
[./subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '0 0 0'
top_right = '1 1 1'
block_id = 1
[../]
[./break_boundary]
input = subdomain1
type = BreakBoundaryOnSubdomainGenerator
[../]
[./interface]
type = SideSetsBetweenSubdomainsGenerator
input = break_boundary
primary_block = '0'
paired_block = '1'
new_boundary = 'primary0_interface'
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
block = 0
[../]
[./v]
order = FIRST
family = LAGRANGE
block = 1
[../]
[]
[Kernels]
[./diff_u]
type = CoeffParamDiffusion
variable = u
D = 4
block = 0
extra_matrix_tags = 'mat_tag1 mat_tag2'
extra_vector_tags = 'vec_tag1'
[../]
[./diff_v]
type = CoeffParamDiffusion
variable = v
D = 2
block = 1
extra_matrix_tags = 'mat_tag1 mat_tag2'
extra_vector_tags = 'vec_tag1'
[../]
[./source_u]
type = BodyForce
variable = u
value = 1
extra_matrix_tags = 'mat_tag1 mat_tag2'
extra_vector_tags = 'vec_tag1 vec_tag2'
[../]
[]
[InterfaceKernels]
[./interface]
type = PenaltyInterfaceDiffusion
variable = u
neighbor_var = v
boundary = primary0_interface
penalty = 1e6
extra_matrix_tags = 'mat_tag1 mat_tag2'
extra_vector_tags = 'vec_tag1 vec_tag2'
[../]
[]
[BCs]
[./u]
type = VacuumBC
variable = u
boundary = 'left_to_0 bottom_to_0 back_to_0 right top front'
extra_matrix_tags = 'mat_tag1 mat_tag2'
extra_vector_tags = 'vec_tag1'
[../]
[./v]
type = VacuumBC
variable = v
boundary = 'left_to_1 bottom_to_1 back_to_1'
extra_matrix_tags = 'mat_tag1 mat_tag2'
extra_vector_tags = 'vec_tag1'
[../]
[]
[AuxVariables]
[./tag_variable1]
order = FIRST
family = LAGRANGE
block = 0
[../]
[./tag_variable2]
order = FIRST
family = LAGRANGE
block = 1
[../]
[]
[AuxKernels]
[./TagVectorAux1]
type = TagVectorAux
variable = tag_variable1
v = u
block = 0
vector_tag = vec_tag2
execute_on = timestep_end
[../]
[./TagVectorAux2]
type = TagMatrixAux
variable = tag_variable2
v = v
block = 1
matrix_tag = mat_tag2
execute_on = timestep_end
[../]
[]
[Postprocessors]
[./u_int]
type = ElementIntegralVariablePostprocessor
variable = u
block = 0
[../]
[./v_int]
type = ElementIntegralVariablePostprocessor
variable = v
block = 1
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Problem]
type = TagTestProblem
test_tag_vectors = 'nontime residual vec_tag1 vec_tag2'
test_tag_matrices = 'mat_tag1 mat_tag2'
extra_tag_matrices = 'mat_tag1 mat_tag2'
extra_tag_vectors = 'vec_tag1 vec_tag2'
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(test/tests/materials/material/bnd_material_test.i)
[Mesh]
type = GeneratedMesh
dim = 3
xmin = 0
xmax = 1
ymin = 0
ymax = 1
zmin = 0
zmax = 1
nx = 3
ny = 3
nz = 3
[]
# Nonlinear system
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 1
[../]
[./right]
type = MTBC
variable = u
boundary = right
grad = 8
prop_name = matp
[../]
[]
# auxiliary system
[AuxVariables]
[./matp]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./prop]
type = MaterialRealAux
property = matp
variable = matp
boundary = 'left right'
[../]
[]
[Materials]
[./mat_left]
type = MTMaterial
boundary = left
[../]
[./mat_right]
type = MTMaterial
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[]
(test/include/executioners/FixedPointSteady.h)
// This file is part of the MOOSE framework
// https://www.mooseframework.org
//
// All rights reserved, see COPYRIGHT for full restrictions
// https://github.com/idaholab/moose/blob/master/COPYRIGHT
//
// Licensed under LGPL 2.1, please see LICENSE for details
// https://www.gnu.org/licenses/lgpl-2.1.html
#pragma once
#include "Steady.h"
#include "FixedPoint.h"
class FixedPointSteady : public Steady
{
public:
static InputParameters validParams();
FixedPointSteady(const InputParameters & parameters);
protected:
FixedPoint _fixed_point;
};
(test/include/executioners/SteadyWithNull.h)
// This file is part of the MOOSE framework
// https://www.mooseframework.org
//
// All rights reserved, see COPYRIGHT for full restrictions
// https://github.com/idaholab/moose/blob/master/COPYRIGHT
//
// Licensed under LGPL 2.1, please see LICENSE for details
// https://www.gnu.org/licenses/lgpl-2.1.html
#pragma once
#include "Steady.h"
/**
* Steady excecutioner setting nullspace
*/
class SteadyWithNull : public Steady
{
public:
static InputParameters validParams();
SteadyWithNull(const InputParameters & parameters);
virtual void init() override;
};
(test/include/executioners/SteadyWithPicardCheck.h)
// This file is part of the MOOSE framework
// https://www.mooseframework.org
//
// All rights reserved, see COPYRIGHT for full restrictions
// https://github.com/idaholab/moose/blob/master/COPYRIGHT
//
// Licensed under LGPL 2.1, please see LICENSE for details
// https://www.gnu.org/licenses/lgpl-2.1.html
#pragma once
#include "Steady.h"
/**
* Test executioner to show custom convergence check of Picard iterations
*/
class SteadyWithPicardCheck : public Steady
{
public:
static InputParameters validParams();
SteadyWithPicardCheck(const InputParameters & parameters);
/**
* Calls at the beginning of every Picard iterations
*/
virtual void preSolve() override;
private:
/// Absolute step tolerance on a designated postprocessor
Real _pp_step_tol;
/// The postprocessor value saved after execute
PostprocessorValue _pp_value_old;
/// Reference to the postprocessor value
const PostprocessorValue & _pp_value;
};
(test/include/executioners/TestSteady.h)
// This file is part of the MOOSE framework
// https://www.mooseframework.org
//
// All rights reserved, see COPYRIGHT for full restrictions
// https://github.com/idaholab/moose/blob/master/COPYRIGHT
//
// Licensed under LGPL 2.1, please see LICENSE for details
// https://www.gnu.org/licenses/lgpl-2.1.html
#pragma once
#include "Steady.h"
/**
* Test executioner to show exception handling
*/
class TestSteady : public Steady
{
public:
static InputParameters validParams();
TestSteady(const InputParameters & parameters);
virtual ~TestSteady();
/**
* This is called at the beginning of FEProblemBase::init.
*/
virtual void preProblemInit() override;
/**
* This will call solve() on the NonlinearSystem.
*/
virtual void preExecute() override;
/**
* Calls a custom execution flag for testing.
*/
virtual void postSolve() override;
private:
/// The type of test that this object is to perform
MooseEnum _test_type;
/// A value to report (used for addAttributeReporter test)
PostprocessorValue * _some_value_that_needs_to_be_reported;
};
(test/include/executioners/PPBindingSteady.h)
// This file is part of the MOOSE framework
// https://www.mooseframework.org
//
// All rights reserved, see COPYRIGHT for full restrictions
// https://github.com/idaholab/moose/blob/master/COPYRIGHT
//
// Licensed under LGPL 2.1, please see LICENSE for details
// https://www.gnu.org/licenses/lgpl-2.1.html
#pragma once
#include "Steady.h"
/**
* Steady excecutioner testing postprocessor binding
*/
class PPBindingSteady : public Steady
{
public:
static InputParameters validParams();
PPBindingSteady(const InputParameters & parameters);
virtual void init() override;
protected:
const PostprocessorValue & _pp;
const PostprocessorValue & _pp_old;
const PostprocessorValue & _pp_older;
};