- axisThe axis used (x, y, or z) if this is to be a function of position
C++ Type:MooseEnum
Description:The axis used (x, y, or z) if this is to be a function of position
- data_fileFile holding CSV data
C++ Type:FileName
Description:File holding CSV data
- formatrowsFormat of csv data file that is in either in columns or rows
Default:rows
C++ Type:MooseEnum
Description:Format of csv data file that is in either in columns or rows
- scale_factor1Scale factor to be applied to the ordinate values
Default:1
C++ Type:double
Description:Scale factor to be applied to the ordinate values
- xThe abscissa values
C++ Type:std::vector<double>
Description:The abscissa values
- x_index_in_file0The abscissa index in the data file
Default:0
C++ Type:unsigned int
Description:The abscissa index in the data file
- xy_dataAll function data, supplied in abscissa, ordinate pairs
C++ Type:std::vector<double>
Description:All function data, supplied in abscissa, ordinate pairs
- xy_in_file_onlyTrueIf the data file only contains abscissa and ordinate data
Default:True
C++ Type:bool
Description:If the data file only contains abscissa and ordinate data
- yThe ordinate values
C++ Type:std::vector<double>
Description:The ordinate values
- y_index_in_file1The ordinate index in the data file
Default:1
C++ Type:unsigned int
Description:The ordinate index in the data file
PiecewiseLinear
Linearly interpolates between pairs of x-y data
Description
The PiecewiseLinear function performs linear interpolations between user-provided pairs of x-y data. The x-y data can be provided in three ways. The first way is through a combination of the x and y paramaters, which are lists of the x and y coordinates of the data points that make up the function. The second way is in the xy_data parameter, which is a list of pairs of x-y data that make up the points of the function. This allows for the function data to be specified in columns by inserting line breaks after each x-y data point. Finally, the x-y data can be provided in an external file containing comma-separated values. The file name is provided in data_file, and the data can be provided in either rows (default) or columns, as specified in the format parameter.
By default, the x-data corresponds to time, but this can be changed to correspond to x, y, or z coordinate with the axis line. If the function is queried outside of its range of x data, it returns the y value associated with the closest x data point.
Example Input Syntax
[Functions]
[./ic_function]
type = PiecewiseLinear
data_file = piecewise_linear_columns.csv #Will generate error because data is expected in rows
scale_factor = 1.0
[../]
[]
Input Parameters
- control_tagsAdds user-defined labels for accessing object parameters via control logic.
C++ Type:std::vector<std::string>
Options:
Description:Adds user-defined labels for accessing object parameters via control logic.
- enableTrueSet the enabled status of the MooseObject.
Default:True
C++ Type:bool
Options:
Description:Set the enabled status of the MooseObject.
Advanced Parameters
Input Files
- (modules/richards/test/tests/dirac/q2p01.i)
- (modules/tensor_mechanics/test/tests/beam/constraints/frictionless_constraint.i)
- (modules/tensor_mechanics/test/tests/j_integral/j_integral_3d_mouth_dir.i)
- (modules/richards/test/tests/theis/th_lumped_22.i)
- (modules/xfem/test/tests/second_order_elements/square_branch_quad8_2d.i)
- (modules/tensor_mechanics/test/tests/recompute_radial_return/isotropic_plasticity_errors.i)
- (modules/tensor_mechanics/test/tests/ad_thermal_expansion_function/finite_const.i)
- (modules/tensor_mechanics/test/tests/interaction_integral/interaction_integral_3d.i)
- (test/tests/geomsearch/2d_moving_penetration/pl_test3qns.i)
- (test/tests/geomsearch/3d_moving_penetration/pl_test4tt.i)
- (modules/tensor_mechanics/test/tests/j_integral_vtest/j_int_surfbreak_ellip_crack_sym_mm_cfp_cm.i)
- (modules/richards/test/tests/rogers_stallybrass_clements/rsc02.i)
- (test/tests/misc/check_error/function_file_test3.i)
- (modules/tensor_mechanics/test/tests/interaction_integral_benchmark/input.i)
- (modules/richards/test/tests/gravity_head_1/gh_fu_22.i)
- (modules/tensor_mechanics/test/tests/smeared_cracking/cracking_xyz.i)
- (modules/contact/test/tests/normalized_penalty/normalized_penalty_kin.i)
- (modules/tensor_mechanics/test/tests/beam/dynamic/dyn_euler_small_added_mass_inertia_damping.i)
- (modules/richards/test/tests/broadbridge_white/bw02.i)
- (modules/tensor_mechanics/test/tests/strain_energy_density/rate_incr_model_elas_plas.i)
- (modules/combined/test/tests/thermal_elastic/ad-thermal_elastic.i)
- (test/tests/geomsearch/3d_moving_penetration_smoothing/pl_test4nstt.i)
- (modules/combined/test/tests/poro_mechanics/mandel.i)
- (modules/tensor_mechanics/test/tests/smeared_cracking/cracking_plane_stress.i)
- (modules/tensor_mechanics/test/tests/beam/dynamic/dyn_euler_small_rayleigh_hht_action.i)
- (modules/porous_flow/test/tests/infiltration_and_drainage/rd02.i)
- (modules/tensor_mechanics/test/tests/dynamics/time_integration/hht_test.i)
- (modules/tensor_mechanics/test/tests/central_difference/lumped/3D/3d_nodalmass_implicit.i)
- (modules/porous_flow/test/tests/infiltration_and_drainage/bw01.i)
- (modules/tensor_mechanics/test/tests/ad_smeared_cracking/cracking_multiple_softening.i)
- (modules/combined/test/tests/thermal_conductivity_temperature_function_test/thermal_conductivity_temperature_function_test.i)
- (modules/tensor_mechanics/test/tests/ad_anisotropic_creep/ad_aniso_iso_creep_x_3d.i)
- (modules/tensor_mechanics/test/tests/ad_viscoplasticity_stress_update/negative_porosity.i)
- (modules/tensor_mechanics/test/tests/beam/dynamic/dyn_euler_small_rayleigh_hht_ti.i)
- (modules/tensor_mechanics/test/tests/dynamics/time_integration/hht_test_ti.i)
- (modules/tensor_mechanics/test/tests/ad_smeared_cracking/cracking_plane_stress.i)
- (modules/tensor_mechanics/test/tests/recompute_radial_return/isotropic_plasticity_finite_strain.i)
- (modules/tensor_mechanics/test/tests/dynamics/prescribed_displacement/3D_QStatic_1_Ramped_Displacement_with_gravity.i)
- (modules/tensor_mechanics/test/tests/interaction_integral/interaction_integral_2d_rot.i)
- (modules/tensor_mechanics/test/tests/beam/static_vm/ansys_vm2.i)
- (test/tests/geomsearch/2d_moving_penetration/pl_test3ns.i)
- (modules/combined/test/tests/ad_power_law_creep/power_law_creep_restart2.i)
- (modules/porous_flow/test/tests/infiltration_and_drainage/rsc01.i)
- (test/tests/geomsearch/2d_moving_penetration/pl_test2tt.i)
- (modules/xfem/test/tests/pressure_bc/edge_2d_pressure.i)
- (test/tests/multiapps/picard/function_dt_sub.i)
- (framework/contrib/hit/test/output.i)
- (modules/navier_stokes/test/tests/ins/jeffery_hamel/wedge_dirichlet.i)
- (modules/contact/test/tests/verification/patch_tests/single_pnt_2d/single_point_2d_frictional.i)
- (modules/tensor_mechanics/test/tests/interaction_integral/interaction_integral_3d_rot.i)
- (test/tests/geomsearch/3d_moving_penetration/pl_test2.i)
- (modules/richards/test/tests/dirac/bh04.i)
- (modules/xfem/test/tests/diffusion_xfem/levelsetcut2d.i)
- (modules/xfem/test/tests/second_order_elements/diffusion_quad9_levelsetcut.i)
- (modules/porous_flow/test/tests/poro_elasticity/mandel.i)
- (modules/tensor_mechanics/test/tests/ad_smeared_cracking/cracking_function.i)
- (modules/tensor_mechanics/test/tests/ad_anisotropic_creep/ad_aniso_creep_z_3d.i)
- (modules/navier_stokes/test/tests/ins/jeffery_hamel/wedge_natural.i)
- (modules/combined/test/tests/internal_volume/hex8.i)
- (modules/tensor_mechanics/test/tests/dynamics/rayleigh_damping/rayleigh_newmark.i)
- (modules/tensor_mechanics/test/tests/scalar_material_damage/scalar_material_damage.i)
- (modules/richards/test/tests/gravity_head_2/gh_lumped_08.i)
- (modules/tensor_mechanics/test/tests/smeared_cracking/cracking_function.i)
- (modules/combined/test/tests/phase_field_fracture/crack2d_computeCrackedStress_finitestrain_plastic.i)
- (modules/tensor_mechanics/test/tests/czm/czm_patch_test.i)
- (modules/tensor_mechanics/test/tests/central_difference/lumped/2D/2d_nodalmass_explicit.i)
- (modules/richards/test/tests/dirac/bh_lumped_07.i)
- (modules/tensor_mechanics/test/tests/ad_thermal_expansion_function/small_linear.i)
- (modules/tensor_mechanics/test/tests/dynamics/prescribed_displacement/3D_QStatic_1_Ramped_Displacement_ti.i)
- (modules/tensor_mechanics/test/tests/dynamics/prescribed_displacement/3D_QStatic_1_Ramped_Displacement.i)
- (modules/richards/test/tests/theis/th22.i)
- (modules/combined/test/tests/evolving_mass_density/expand_compress_test_tensors.i)
- (modules/tensor_mechanics/test/tests/dynamics/rayleigh_damping/rayleigh_newmark_material_dependent.i)
- (modules/xfem/test/tests/second_order_elements/diffusion_2d_quad9.i)
- (test/tests/time_steppers/iteration_adaptive/piecewise_linear.i)
- (test/tests/misc/check_error/function_file_test16.i)
- (test/tests/geomsearch/3d_moving_penetration/pl_test2qtt.i)
- (modules/tensor_mechanics/test/tests/truss/truss_3d.i)
- (modules/contact/test/tests/normalized_penalty/normalized_penalty_Q8.i)
- (modules/tensor_mechanics/test/tests/1D_axisymmetric/axisymmetric_gps_finite.i)
- (modules/tensor_mechanics/test/tests/beam/dynamic/dyn_euler_small_added_mass_inertia_damping_ti.i)
- (test/tests/time_integrators/newmark-beta/newmark_beta_default_parameters.i)
- (modules/tensor_mechanics/test/tests/ad_anisotropic_elastoplasticity/ad_aniso_plasticity_x_one.i)
- (modules/richards/test/tests/buckley_leverett/bl20.i)
- (modules/contact/test/tests/hertz_spherical/hertz_contact_hex20.i)
- (modules/richards/test/tests/theis/th_lumped_01.i)
- (modules/tensor_mechanics/test/tests/volumetric_eigenstrain/volumetric_mechanical.i)
- (modules/tensor_mechanics/test/tests/ad_smeared_cracking/cracking_power.i)
- (modules/tensor_mechanics/test/tests/beam/dynamic/dyn_euler_small_added_mass_gravity.i)
- (modules/tensor_mechanics/test/tests/dynamics/wave_1D/wave_rayleigh_hht.i)
- (modules/richards/test/tests/broadbridge_white/bw01.i)
- (modules/combined/test/tests/ad_cavity_pressure/3d.i)
- (modules/tensor_mechanics/test/tests/smeared_cracking/cracking.i)
- (modules/tensor_mechanics/test/tests/ad_smeared_cracking/cracking_deprecated.i)
- (modules/richards/test/tests/buckley_leverett/bl21.i)
- (modules/tensor_mechanics/test/tests/j_integral_vtest/j_int_surfbreak_ellip_crack_sym_mm_cm.i)
- (test/tests/time_integrators/newmark-beta/newmark_beta_prescribed_parameters.i)
- (modules/tensor_mechanics/test/tests/smeared_cracking/cracking_exponential_deprecated.i)
- (modules/tensor_mechanics/test/tests/1D_axisymmetric/axisymm_plane_strain_finite.i)
- (modules/tensor_mechanics/test/tests/dynamics/wave_1D/wave_hht.i)
- (modules/combined/test/tests/ad_cavity_pressure/negative_volume.i)
- (modules/xfem/test/tests/diffusion_xfem/levelsetcut2d_aux.i)
- (modules/tensor_mechanics/test/tests/dynamics/time_integration/newmark_test.i)
- (test/tests/geomsearch/2d_moving_penetration/pl_test3qnns.i)
- (modules/tensor_mechanics/test/tests/ad_viscoplasticity_stress_update/gtn_single.i)
- (modules/tensor_mechanics/test/tests/central_difference/consistent/1D/1d_consistent_explicit.i)
- (modules/contact/test/tests/verification/patch_tests/single_pnt_2d/single_point_2d.i)
- (modules/contact/test/tests/verification/hertz_cyl/half_symm_q8/hertz_cyl_half_1deg_template3.i)
- (modules/tensor_mechanics/test/tests/interaction_integral/interaction_integral_3d_points.i)
- (modules/tensor_mechanics/test/tests/plane_stress/weak_plane_stress_incremental.i)
- (modules/tensor_mechanics/test/tests/beam/static/euler_finite_rot_y_action.i)
- (modules/richards/test/tests/gravity_head_2/gh_fu_17.i)
- (modules/tensor_mechanics/test/tests/j_integral/j_integral_3d_mouth_dir_end_dir_vec.i)
- (modules/combined/test/tests/evolving_mass_density/shear_test_tensors.i)
- (modules/combined/test/tests/cavity_pressure/multiple_postprocessors.i)
- (modules/heat_conduction/test/tests/gap_heat_transfer_htonly/gap_heat_transfer_htonly_it_plot_test.i)
- (modules/combined/test/tests/gap_heat_transfer_convex/gap_heat_transfer_convex.i)
- (modules/tensor_mechanics/test/tests/domain_integral_thermal/c_integral_2d.i)
- (modules/contact/test/tests/simple_contact/simple_contact_rz_test.i)
- (modules/combined/test/tests/cavity_pressure/rz.i)
- (modules/tensor_mechanics/test/tests/dynamics/rayleigh_damping/rayleigh_hht.i)
- (modules/tensor_mechanics/test/tests/ad_thermal_expansion_function/finite_linear.i)
- (test/tests/geomsearch/3d_moving_penetration_smoothing/pl_test3nstt.i)
- (modules/porous_flow/test/tests/dirackernels/bh04.i)
- (modules/porous_flow/test/tests/dirackernels/hfrompps.i)
- (modules/richards/test/tests/gravity_head_2/gh_fu_05.i)
- (modules/richards/test/tests/gravity_head_2/gh08.i)
- (modules/contact/test/tests/normal-nodal-lm-tan-tolerance/normal-nodal-lm-tan-tolerance.i)
- (modules/tensor_mechanics/test/tests/ad_pressure/pressure_test.i)
- (test/tests/geomsearch/2d_moving_penetration/pl_test1.i)
- (test/tests/time_steppers/cutback_factor_at_failure/function_dt_cutback.i)
- (modules/contact/examples/2d_indenter/indenter_rz_nodeface_friction.i)
- (modules/tensor_mechanics/test/tests/ad_smeared_cracking/cracking_exponential_deprecated.i)
- (modules/combined/test/tests/power_law_creep/power_law_creep_smallstrain.i)
- (modules/tensor_mechanics/test/tests/action/ad_converter_action_multi_eigenstrain.i)
- (modules/heat_conduction/test/tests/gap_heat_transfer_htonly/gap_heat_transfer_htonly_rz_test.i)
- (modules/xfem/test/tests/mechanical_constraint/glued_penalty.i)
- (modules/richards/test/tests/gravity_head_2/gh18.i)
- (test/tests/predictors/simple/predictor_test_skip_after_failed_tstep.i)
- (modules/richards/test/tests/gravity_head_1/gh23.i)
- (test/tests/misc/check_error/function_file_test15.i)
- (test/tests/geomsearch/3d_moving_penetration_smoothing/pl_test4nnstt.i)
- (test/tests/misc/check_error/function_file_test8.i)
- (modules/tensor_mechanics/test/tests/strain_energy_density/nonAD_rate_model_weak_plane.i)
- (test/tests/geomsearch/2d_moving_penetration/pl_test3.i)
- (modules/tensor_mechanics/test/tests/j_integral_vtest/j_int_surfbreak_ellip_crack_sym_mm.i)
- (test/tests/geomsearch/2d_moving_penetration/restart.i)
- (modules/tensor_mechanics/test/tests/smeared_cracking/cracking_multiple_softening.i)
- (modules/tensor_mechanics/test/tests/plane_stress/ad_weak_plane_stress_incremental.i)
- (modules/heat_conduction/test/tests/gap_heat_transfer_htonly/gap_heat_transfer_htonly_rspherical.i)
- (modules/tensor_mechanics/test/tests/central_difference/lumped/1D/1d_nodalmass_explicit.i)
- (modules/combined/test/tests/inelastic_strain/elas_plas/elas_plas_nl1_cycle.i)
- (modules/combined/test/tests/ad_cavity_pressure/multiple_postprocessors.i)
- (modules/tensor_mechanics/test/tests/domain_integral_thermal/j_integral_2d_ctefunc.i)
- (test/tests/geomsearch/2d_moving_penetration/pl_test4qtt.i)
- (modules/tensor_mechanics/test/tests/1D_axisymmetric/axisymmetric_gps_small.i)
- (modules/tensor_mechanics/test/tests/shell/dynamics/shell_dynamics_bending_moment.i)
- (test/tests/geomsearch/3d_moving_penetration/pl_test4.i)
- (framework/contrib/hit/test/input.i)
- (modules/combined/test/tests/power_law_creep/power_law_creep_restart2.i)
- (modules/tensor_mechanics/test/tests/ad_smeared_cracking/cracking_rz.i)
- (modules/combined/test/tests/ad_cavity_pressure/additional_volume.i)
- (test/tests/geomsearch/3d_moving_penetration/pl_test4qtt.i)
- (modules/tensor_mechanics/test/tests/t_stress/t_stress_ellip_crack_3d.i)
- (test/tests/misc/check_error/function_file_test1.i)
- (modules/xfem/test/tests/second_order_elements/diffusion_3d_tet10.i)
- (modules/heat_conduction/test/tests/gap_heat_transfer_htonly/planar_xy.i)
- (test/tests/geomsearch/3d_moving_penetration/pl_test3tt.i)
- (modules/tensor_mechanics/test/tests/1D_axisymmetric/axisymm_plane_strain_small.i)
- (modules/heat_conduction/test/tests/gap_heat_transfer_htonly/cyl2D.i)
- (modules/combined/test/tests/inelastic_strain/elas_plas/elas_plas_nl1.i)
- (modules/tensor_mechanics/test/tests/beam/dynamic/dyn_euler_small_added_mass.i)
- (modules/richards/test/tests/gravity_head_2/gh_lumped_07.i)
- (modules/combined/test/tests/power_law_creep/power_law_creep.i)
- (test/tests/controls/control_piecewise/controlled_piecewise.i)
- (modules/porous_flow/test/tests/dirackernels/bh05.i)
- (modules/richards/test/tests/dirac/bh_fu_04.i)
- (test/tests/geomsearch/3d_moving_penetration/pl_test1qtt.i)
- (modules/tensor_mechanics/test/tests/interaction_integral/interaction_integral_2d.i)
- (modules/tensor_mechanics/test/tests/1D_axisymmetric/axisymm_gps_finite.i)
- (modules/tensor_mechanics/test/tests/ad_anisotropic_elastoplasticity/ad_aniso_plasticity_x_one_ref.i)
- (test/tests/multiapps/sub_cycling_failure/master_gold.i)
- (modules/heat_conduction/test/tests/gap_heat_transfer_htonly/sphere2DRZ.i)
- (modules/tensor_mechanics/test/tests/jacobian_damper/cube_load.i)
- (test/tests/geomsearch/3d_moving_penetration_smoothing/pl_test3nnstt.i)
- (modules/tensor_mechanics/test/tests/central_difference/lumped/2D/2d_nodalmass_implicit.i)
- (modules/combined/test/tests/reference_residual/reference_residual_perfgraph.i)
- (modules/contact/test/tests/nodal_area/nodal_area_Hex27.i)
- (test/tests/misc/check_error/function_file_test9.i)
- (test/tests/geomsearch/3d_moving_penetration/pl_test1.i)
- (test/tests/misc/check_error/function_file_test11.i)
- (modules/tensor_mechanics/test/tests/strain_energy_density/tot_model.i)
- (modules/tensor_mechanics/test/tests/beam/dynamic/dyn_timoshenko_small.i)
- (modules/tensor_mechanics/test/tests/truss/truss_3d_action.i)
- (modules/tensor_mechanics/test/tests/truss/truss_plastic.i)
- (modules/tensor_mechanics/test/tests/j_integral/j_integral_2d.i)
- (modules/contact/test/tests/nodal_area/nodal_area_Hex20.i)
- (modules/richards/test/tests/theis/th_lumped_02.i)
- (modules/contact/test/tests/normalized_penalty/normalized_penalty.i)
- (modules/tensor_mechanics/test/tests/j_integral/j_integral_2d_topo_q_func.i)
- (modules/tensor_mechanics/test/tests/beam/dynamic/dyn_euler_small_rayleigh_hht.i)
- (modules/combined/test/tests/internal_volume/rz_quad8.i)
- (modules/contact/test/tests/verification/hertz_cyl/quart_symm_q4/hertz_cyl_qsym_1deg_template1.i)
- (modules/xfem/test/tests/diffusion_xfem/levelsetcut3d.i)
- (modules/porous_flow/test/tests/poro_elasticity/mandel_fully_saturated_volume.i)
- (test/tests/geomsearch/2d_moving_penetration/pl_test1tt.i)
- (test/tests/misc/check_error/function_file_test5.i)
- (modules/tensor_mechanics/test/tests/ad_anisotropic_plasticity/anis_plasticity_test.i)
- (modules/richards/test/tests/broadbridge_white/bw_lumped_02.i)
- (modules/tensor_mechanics/test/tests/j_integral/j_integral_2d_points.i)
- (modules/combined/test/tests/internal_volume/hex20.i)
- (modules/tensor_mechanics/test/tests/ad_anisotropic_plasticity/anis_elasticity_test.i)
- (modules/porous_flow/test/tests/infiltration_and_drainage/rd03.i)
- (modules/tensor_mechanics/test/tests/dynamics/acceleration_bc/AccelerationBC_test.i)
- (modules/richards/test/tests/rogers_stallybrass_clements/rsc_fu_01.i)
- (modules/tensor_mechanics/test/tests/strain_energy_density/rate_model_small.i)
- (modules/combined/test/tests/thermo_mech/youngs_modulus_function_temp.i)
- (modules/combined/test/tests/internal_volume/rz.i)
- (test/tests/misc/check_error/function_file_test6.i)
- (modules/tensor_mechanics/test/tests/scalar_material_damage/combined_scalar_damage.i)
- (test/tests/geomsearch/3d_moving_penetration_smoothing/pl_test4ns.i)
- (modules/richards/test/tests/recharge_discharge/rd03.i)
- (modules/porous_flow/test/tests/gravity/grav02c.i)
- (modules/tensor_mechanics/test/tests/ad_viscoplasticity_stress_update/lps_single_split.i)
- (test/tests/geomsearch/3d_moving_penetration/pl_test3.i)
- (modules/richards/test/tests/theis/th01.i)
- (modules/tensor_mechanics/test/tests/strain_energy_density/ad_rate_model_weak_plane.i)
- (modules/richards/test/tests/gravity_head_2/gh05.i)
- (modules/richards/test/tests/gravity_head_2/gh_fu_06.i)
- (modules/porous_flow/test/tests/functions/mpf1.i)
- (modules/tensor_mechanics/test/tests/ad_viscoplasticity_stress_update/lps_single.i)
- (modules/tensor_mechanics/test/tests/anisotropic_patch/anisotropic_patch_test.i)
- (modules/tensor_mechanics/test/tests/strain_energy_density/incr_model_elas_plas.i)
- (modules/xfem/test/tests/moment_fitting/diffusion_moment_fitting_six_points.i)
- (modules/tensor_mechanics/test/tests/ad_thermal_expansion_function/dilatation.i)
- (modules/xfem/test/tests/solid_mechanics_basic/square_branch_tri_2d.i)
- (modules/contact/test/tests/ring_contact/ring_contact.i)
- (modules/tensor_mechanics/test/tests/thermal_expansion_function/finite_linear.i)
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- (modules/richards/test/tests/recharge_discharge/rd02.i)
- (test/tests/geomsearch/2d_moving_penetration/pl_test4ns.i)
- (modules/combined/test/tests/adaptive_timestepping/adapt_tstep_function_change.i)
- (modules/tensor_mechanics/test/tests/central_difference/consistent/3D/3d_consistent_implicit.i)
- (modules/combined/test/tests/cavity_pressure/3d.i)
- (modules/tensor_mechanics/test/tests/elastic_patch/elastic_patch.i)
- (modules/richards/test/tests/gravity_head_2/gh17.i)
- (test/tests/geomsearch/3d_moving_penetration_smoothing/pl_test3nns.i)
- (modules/tensor_mechanics/test/tests/shell/dynamics/shell_dynamics_bending_moment_free.i)
- (modules/tensor_mechanics/test/tests/1D_axisymmetric/axisymmetric_gps_incremental.i)
- (test/tests/multiapps/picard/function_dt_master.i)
- (modules/contact/test/tests/tension_release/4ElemTensionRelease_mechanical_constraint.i)
- (modules/tensor_mechanics/test/tests/ad_viscoplasticity_stress_update/lps_dual.i)
- (modules/tensor_mechanics/test/tests/shell/dynamics/shell_dynamics_bending_moment_free_orientation_inclined.i)
- (modules/porous_flow/test/tests/infiltration_and_drainage/bw02.i)
- (modules/combined/test/tests/heat_conduction_xfem/heat.i)
- (modules/tensor_mechanics/test/tests/beam/constraints/glued_constraint.i)
- (test/tests/time_steppers/iteration_adaptive/adapt_tstep_pps_lim.i)
- (modules/tensor_mechanics/test/tests/smeared_cracking/cracking_rz_exponential.i)
- (test/tests/geomsearch/2d_moving_penetration/pl_test3tt.i)
- (test/tests/time_steppers/iteration_adaptive/multi_piecewise_linear.i)
(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/richards/test/tests/dirac/q2p01.i)
# unsaturated
# production
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = -1
xmax = 1
ymin = -1
ymax = 1
zmin = -1
zmax = 1
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1E-2 1E-1 1 1E1 1E2 1E3'
x = '0 1E-1 1 1E1 1E2 1E3'
[../]
[]
[UserObjects]
[./DensityWater]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 0.5
[../]
[./DensityGas]
type = RichardsDensityConstBulk
dens0 = 0.5
bulk_mod = 0.3
[../]
[./RelPermWater]
type = RichardsRelPermPower
simm = 0.2
n = 2
[../]
[./RelPermGas]
type = Q2PRelPermPowerGas
simm = 0.1
n = 3
[../]
[./borehole_total_outflow_water]
type = RichardsSumQuantity
[../]
[./borehole_total_outflow_gas]
type = RichardsSumQuantity
[../]
[]
[Variables]
[./pp]
[../]
[./sat]
[../]
[]
[ICs]
[./p_ic]
type = ConstantIC
variable = pp
value = 1
[../]
[./s_ic]
type = ConstantIC
variable = sat
value = 0.5
[../]
[]
[Q2P]
porepressure = pp
saturation = sat
water_density = DensityWater
water_relperm = RelPermWater
water_viscosity = 0.8
gas_density = DensityGas
gas_relperm = RelPermGas
gas_viscosity = 0.5
diffusivity = 0.0
output_total_masses_to = 'CSV'
[]
[DiracKernels]
[./bh_water]
type = Q2PBorehole
bottom_pressure = 0
point_file = bh02.bh
SumQuantityUO = borehole_total_outflow_water
variable = sat
unit_weight = '0 0 0'
character = 8E9
fluid_density = DensityWater
fluid_relperm = RelPermWater
other_var = pp
var_is_porepressure = false
fluid_viscosity = 0.8
[../]
[./bh_gas]
type = Q2PBorehole
bottom_pressure = 0
point_file = bh02.bh
SumQuantityUO = borehole_total_outflow_gas
variable = pp
unit_weight = '0 0 0'
character = 1E10
fluid_density = DensityGas
fluid_relperm = RelPermGas
other_var = sat
var_is_porepressure = true
fluid_viscosity = 0.5
[../]
[]
[Postprocessors]
[./bh_report_water]
type = RichardsPlotQuantity
uo = borehole_total_outflow_water
[../]
[./bh_report_gas]
type = RichardsPlotQuantity
uo = borehole_total_outflow_gas
[../]
[./p0]
type = PointValue
variable = pp
point = '1 1 1'
execute_on = timestep_end
[../]
[./sat0]
type = PointValue
variable = sat
point = '1 1 1'
execute_on = timestep_end
[../]
[]
[Materials]
[./rock]
type = Q2PMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-12 0 0 0 1E-12 0 0 0 1E-12'
gravity = '0 0 0'
[../]
[]
[Preconditioning]
[./usual]
type = SMP
full = true
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -ksp_max_it'
petsc_options_value = 'bcgs bjacobi 1E-10 1E-10 10000 30'
[../]
[]
[Executioner]
type = Transient
end_time = 1E3
solve_type = NEWTON
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = q2p01
execute_on = timestep_end
[./CSV]
type = CSV
[../]
[]
(modules/tensor_mechanics/test/tests/beam/constraints/frictionless_constraint.i)
# Test for frictionless beam constraint.
#
# Using a simple L-shaped geometry with a frictionless constraint at the
# corner between the two beams. The longer beam properties and loading is
# taken from an earlier beam regression test for static loading. The maximum
# applied load of 50000 lb should result in a displacement of 3.537e-3. Since
# the constraint is frictionless, the y-dir displacement of the long beam is
# 3.537e-3 and the short beam y-dir displacement is zero.
[Mesh]
file = beam_cons_patch.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[./rot_x]
order = FIRST
family = LAGRANGE
[../]
[./rot_y]
order = FIRST
family = LAGRANGE
[../]
[./rot_z]
order = FIRST
family = LAGRANGE
[../]
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = '1001 1003'
value = 0.0
[../]
[./fixy1]
type = DirichletBC
variable = disp_y
boundary = '1001 1003'
value = 0.0
[../]
[./fixz1]
type = DirichletBC
variable = disp_z
boundary = '1001 1003'
value = 0.0
[../]
[./fixr1]
type = DirichletBC
variable = rot_x
boundary = '1001 1003'
value = 0.0
[../]
[./fixr2]
type = DirichletBC
variable = rot_y
boundary = '1001 1003'
value = 0.0
[../]
[./fixr3]
type = DirichletBC
variable = rot_z
boundary = '1001 1003'
value = 0.0
[../]
[]
[Constraints]
[./tie_y_fuel]
type = NodalFrictionalConstraint
normal_force = 1000
tangential_penalty = 1.2e6
friction_coefficient = 0.0
boundary = 1005
secondary = 1004
variable = disp_y
[../]
[./tie_x_fuel]
type = NodalStickConstraint
penalty = 1.2e14
boundary = 1005
secondary = 1004
variable = disp_x
[../]
[./tie_z_fuel]
type = NodalStickConstraint
penalty = 1.2e14
boundary = 1005
secondary = 1004
variable = disp_z
[../]
[./tie_rot_y_fuel]
type = NodalStickConstraint
penalty = 1.2e14
boundary = 1005
secondary = 1004
variable = rot_y
[../]
[./tie_rot_x_fuel]
type = NodalStickConstraint
penalty = 1.2e14
boundary = 1005
secondary = 1004
variable = rot_x
[../]
[./tie_rot_z_fuel]
type = NodalStickConstraint
penalty = 1.2e14
boundary = 1005
secondary = 1004
variable = rot_z
[../]
[]
[Functions]
[./force_loading]
type = PiecewiseLinear
x = '0.0 5.0'
y = '0.0 50000.0'
[../]
[]
[NodalKernels]
[./force_x2]
type = UserForcingFunctionNodalKernel
variable = disp_y
boundary = '1004'
function = force_loading
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
line_search = 'none'
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-8
dt = 1
dtmin = 1
end_time = 5
[]
[Kernels]
[./solid_disp_x]
type = StressDivergenceBeam
block = '1 2'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 0
variable = disp_x
[../]
[./solid_disp_y]
type = StressDivergenceBeam
block = '1 2'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 1
variable = disp_y
[../]
[./solid_disp_z]
type = StressDivergenceBeam
block = '1 2'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 2
variable = disp_z
[../]
[./solid_rot_x]
type = StressDivergenceBeam
block = '1 2'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 3
variable = rot_x
[../]
[./solid_rot_y]
type = StressDivergenceBeam
block = '1 2'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 4
variable = rot_y
[../]
[./solid_rot_z]
type = StressDivergenceBeam
block = '1 2'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 5
variable = rot_z
[../]
[]
[Materials]
[./elasticity_pipe]
type = ComputeElasticityBeam
shear_coefficient = 1.0
youngs_modulus = 30e6
poissons_ratio = 0.3
block = 1
outputs = exodus
output_properties = 'material_stiffness material_flexure'
[../]
[./strain_pipe]
type = ComputeIncrementalBeamStrain
block = '1'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
area = 28.274
Ay = 0.0
Az = 0.0
Iy = 1.0
Iz = 1.0
y_orientation = '0.0 0.0 1.0'
[../]
[./stress_pipe]
type = ComputeBeamResultants
block = 1
outputs = exodus
output_properties = 'forces moments'
[../]
[./elasticity_cons]
type = ComputeElasticityBeam
shear_coefficient = 1.0
youngs_modulus = 10e2
poissons_ratio = 0.3
block = 2
outputs = exodus
output_properties = 'material_stiffness material_flexure'
[../]
[./strain_cons]
type = ComputeIncrementalBeamStrain
block = '2'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
area = 1.0
Ay = 0.0
Az = 0.0
Iy = 1.0
Iz = 1.0
y_orientation = '0.0 0.0 1.0'
[../]
[./stress_cons]
type = ComputeBeamResultants
block = 2
outputs = exodus
output_properties = 'forces moments'
[../]
[]
[Postprocessors]
[./disp_y_n4]
type = NodalVariableValue
variable = disp_y
nodeid = 3
[../]
[./disp_y_n2]
type = NodalVariableValue
variable = disp_y
nodeid = 1
[../]
[./forces_y]
type = PointValue
point = '10.0 59.9 0.0'
variable = forces_y
[../]
[]
[Outputs]
csv = true
exodus = true
[]
(modules/tensor_mechanics/test/tests/j_integral/j_integral_3d_mouth_dir.i)
#This tests the J-Integral evaluation capability.
#This is a 3d extrusion of a 2d plane strain model with 2 elements
#through the thickness, and calculates the J-Integrals using options
#to treat it as 3d.
#Crack direction is defined using the crack mouth coordinates.
#The analytic solution for J1 is 2.434. This model
#converges to that solution with a refined mesh.
#Reference: National Agency for Finite Element Methods and Standards (U.K.):
#Test 1.1 from NAFEMS publication "Test Cases in Linear Elastic Fracture
#Mechanics" R0020.
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[Mesh]
file = crack3d.e
[]
[AuxVariables]
[./SED]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./rampConstant]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = -1e2
[../]
[]
[DomainIntegral]
integrals = JIntegral
boundary = 800
crack_direction_method = CrackMouth
crack_mouth_boundary = 900
radius_inner = '4.0 5.5'
radius_outer = '5.5 7.0'
output_variable = 'disp_x'
output_q = false
incremental = true
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
[../]
[]
[AuxKernels]
[./SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[../]
[]
[BCs]
[./crack_y]
type = DirichletBC
variable = disp_y
boundary = 100
value = 0.0
[../]
[./no_z]
type = DirichletBC
variable = disp_z
boundary = 500
value = 0.0
[../]
[./no_z2]
type = DirichletBC
variable = disp_z
boundary = 510
value = 0.0
[../]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 700
value = 0.0
[../]
[./Pressure]
[./Side1]
boundary = 400
function = rampConstant
[../]
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_abs_tol = 1e-5
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Postprocessors]
[./disp_x_centercrack]
type = CrackFrontData
crack_front_definition = crackFrontDefinition
variable = disp_x
crack_front_point_index = 1
[../]
[]
[Outputs]
file_base = j_integral_3d_mouth_dir_out
exodus = true
csv = true
[]
(modules/richards/test/tests/theis/th_lumped_22.i)
# two-phase, fully-saturated
# production
# lumped
[Mesh]
type = FileMesh
file = th02_input.e
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = 'DensityWater DensityGas'
relperm_UO = 'RelPermWater RelPermGas'
SUPG_UO = 'SUPGwater SUPGgas'
sat_UO = 'SatWater SatGas'
seff_UO = 'SeffWater SeffGas'
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1 2 4 20'
x = '0 1 10 100'
[../]
[]
[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 = 1E-5
[../]
[./SUPGgas]
type = RichardsSUPGstandard
p_SUPG = 1E-5
[../]
[./total_outflow_mass]
type = RichardsSumQuantity
[../]
[]
[Variables]
[./pwater]
order = FIRST
family = LAGRANGE
[../]
[./pgas]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./water_ic]
type = FunctionIC
variable = pwater
function = initial_pressure
[../]
[./gas_ic]
type = FunctionIC
variable = pgas
function = initial_pressure
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[Kernels]
active = 'richardsfwater richardstwater richardsfgas richardstgas'
[./richardstwater]
type = RichardsLumpedMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFlux
variable = pwater
[../]
[./richardstgas]
type = RichardsLumpedMassChange
variable = pgas
[../]
[./richardsfgas]
type = RichardsFlux
variable = pgas
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = SeffWater
pressure_vars = 'pwater pgas'
[../]
[]
[DiracKernels]
[./bh]
type = RichardsPolyLineSink
pressures = '-1E9 1E9'
fluxes = '200 200'
point_file = th01.points
SumQuantityUO = total_outflow_mass
variable = pwater
[../]
[]
[Postprocessors]
[./flow_report]
type = RichardsPlotQuantity
uo = total_outflow_mass
[../]
[./p50]
type = PointValue
variable = pwater
point = '50 0 0'
execute_on = timestep_end
[../]
[]
[Functions]
[./initial_pressure]
type = ParsedFunction
value = 1E5
[../]
[]
[Materials]
[./all]
type = RichardsMaterial
block = 1
mat_porosity = 0.1
mat_permeability = '1E-10 0 0 0 1E-10 0 0 0 1E-10'
viscosity = '1E-3 1E-5'
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./usual]
type = SMP
full = true
petsc_options = '-snes_converged_reason -ksp_diagonal_scale -ksp_diagonal_scale_fix -ksp_gmres_modifiedgramschmidt -snes_linesearch_monitor'
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -sub_pc_factor_shift_type -pc_asm_overlap -snes_atol -snes_rtol -snes_max_it -ksp_rtol -ksp_atol'
petsc_options_value = 'gmres asm lu NONZERO 2 2E-7 1E-10 20 1E-10 1E-100'
[../]
[]
[Executioner]
type = Transient
end_time = 100
solve_type = NEWTON
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = th_lumped_22
exodus = true
csv = true
[]
(modules/xfem/test/tests/second_order_elements/square_branch_quad8_2d.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
volumetric_locking_correction = false
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD8
[]
[UserObjects]
[./line_seg_cut_set_uo]
type = LineSegmentCutSetUserObject
cut_data = '-1.0000e-10 6.6340e-01 6.6340e-01 -1.0000e-10 0.0 1.0
3.3120e-01 3.3200e-01 1.0001e+00 3.3200e-01 1.0 2.0'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
planar_formulation = PLANE_STRAIN
[../]
[]
[Functions]
[./right_disp_x]
type = PiecewiseLinear
x = '0 1.0 2.0 3.0'
y = '0 0.005 0.01 0.01'
[../]
[./top_disp_y]
type = PiecewiseLinear
x = '0 1.0 2.0 3.0'
y = '0 0.005 0.01 0.01'
[../]
[]
[BCs]
[./right_x]
type = FunctionDirichletBC
boundary = 1
variable = disp_x
function = right_disp_x
[../]
[./top_y]
type = FunctionDirichletBC
boundary = 2
variable = disp_y
function = top_disp_y
[../]
[./bottom_y]
type = DirichletBC
boundary = 0
variable = disp_y
value = 0.0
[../]
[./left_x]
type = DirichletBC
boundary = 3
variable = disp_x
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-16
nl_abs_tol = 1e-10
# time control
start_time = 0.0
dt = 1.0
end_time = 2.2
num_steps = 5000
[]
[Outputs]
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/tensor_mechanics/test/tests/recompute_radial_return/isotropic_plasticity_errors.i)
# This simulation uses the piece-wise linear strain hardening model
# with the incremental small strain formulation; incremental small strain
# is required to produce the strain_increment for the DiscreteRadialReturnStressIncrement
# class, which handles the calculation of the stress increment to return
# to the yield surface in a J2 (isotropic) plasticity problem.
#
# This test is used to check the error messages in the discrete radial return
# model DiscreteRRIsotropicPlasticity; cli_args are used to check all of the
# error messages in the DiscreteRRIsotropicPlasticity model.
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Functions]
[./top_pull]
type = ParsedFunction
value = t*(0.0625)
[../]
[./harden_func]
type = PiecewiseLinear
x = '0 0.0003 0.0007 0.0009'
y = '50 52 54 56'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
incremental = true
add_variables = true
generate_output = 'stress_yy plastic_strain_xx plastic_strain_yy plastic_strain_zz'
[../]
[]
[BCs]
[./y_pull_function]
type = FunctionDirichletBC
variable = disp_y
boundary = top
function = top_pull
[../]
[./x_bot]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./y_bot]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./z_bot]
type = DirichletBC
variable = disp_z
boundary = back
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
[../]
[./isotropic_plasticity]
type = IsotropicPlasticityStressUpdate
relative_tolerance = 1e-25
absolute_tolerance = 1e-5
[../]
[./radial_return_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'isotropic_plasticity'
[../]
[]
[Executioner]
type = Transient
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 100
nl_max_its = 100
nl_rel_tol = 1e-18
nl_abs_tol = 1e-10
l_tol = 1e-12
start_time = 0.0
end_time = 0.025
dt = 0.00125
dtmin = 0.0001
[]
[Outputs]
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[]
(modules/tensor_mechanics/test/tests/ad_thermal_expansion_function/finite_const.i)
# This tests the thermal expansion coefficient function using both
# options to specify that function: mean and instantaneous. There
# two blocks, each containing a single element, and these use the
# two variants of the function.
# In this test, the instantaneous CTE function has a constant value,
# while the mean CTE function is an analytic function designed to
# give the same response. If \bar{alpha}(T) is the mean CTE function,
# and \alpha(T) is the instantaneous CTE function,
# \bar{\alpha}(T) = 1/(T-Tref) \intA^{T}_{Tsf} \alpha(T) dT
# where Tref is the reference temperature used to define the mean CTE
# function, and Tsf is the stress-free temperature.
# This version of the test uses finite deformation theory.
# The two models produce very similar results. There are slight
# differences due to the large deformation treatment.
[Mesh]
file = 'blocks.e'
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[AuxVariables]
[./temp]
order = FIRST
family = LAGRANGE
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
eigenstrain_names = eigenstrain
generate_output = 'strain_xx strain_yy strain_zz'
use_automatic_differentiation = true
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = disp_x
boundary = 3
value = 0.0
[../]
[./bottom]
type = DirichletBC
variable = disp_y
boundary = 2
value = 0.0
[../]
[./back]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0.0
[../]
[]
[AuxKernels]
[./temp]
type = FunctionAux
variable = temp
block = '1 2'
function = temp_func
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./small_stress]
type = ADComputeFiniteStrainElasticStress
[../]
[./thermal_expansion_strain1]
type = ADComputeMeanThermalExpansionFunctionEigenstrain
block = 1
thermal_expansion_function = cte_func_mean
thermal_expansion_function_reference_temperature = 0.5
stress_free_temperature = 0.0
temperature = temp
eigenstrain_name = eigenstrain
[../]
[./thermal_expansion_strain2]
type = ADComputeInstantaneousThermalExpansionFunctionEigenstrain
block = 2
thermal_expansion_function = cte_func_inst
stress_free_temperature = 0.0
temperature = temp
eigenstrain_name = eigenstrain
[../]
[]
[Functions]
[./cte_func_mean]
type = ParsedFunction
vars = 'tsf tref scale' #stress free temp, reference temp, scale factor
vals = '0.0 0.5 1e-4'
value = 'scale * (t - tsf) / (t - tref)'
[../]
[./cte_func_inst]
type = PiecewiseLinear
xy_data = '0 1.0
2 1.0'
scale_factor = 1e-4
[../]
[./temp_func]
type = PiecewiseLinear
xy_data = '0 1
1 2'
[../]
[]
[Postprocessors]
[./disp_1]
type = NodalMaxValue
variable = disp_x
boundary = 101
[../]
[./disp_2]
type = NodalMaxValue
variable = disp_x
boundary = 102
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
l_max_its = 100
l_tol = 1e-4
nl_abs_tol = 1e-8
nl_rel_tol = 1e-12
start_time = 0.0
end_time = 1.0
dt = 0.1
[]
[Outputs]
csv = true
[]
(modules/tensor_mechanics/test/tests/interaction_integral/interaction_integral_3d.i)
#This tests the Interaction-Integral evaluation capability.
#This is a 3d extrusion of a 2d plane strain model with 2 elements
#through the thickness, and calculates the Interaction-Integrals using options
#to treat it as 3d.
[GlobalParams]
order = FIRST
# order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[Mesh]
file = crack3d.e
displacements = 'disp_x disp_y disp_z'
[]
[Functions]
[./rampConstant]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = -1e2
[../]
[]
[DomainIntegral]
integrals = 'InteractionIntegralKI InteractionIntegralKII InteractionIntegralKIII'
boundary = 800
crack_direction_method = CrackDirectionVector
crack_direction_vector = '1 0 0'
radius_inner = '4.0 5.5'
radius_outer = '5.5 7.0'
block = 1
youngs_modulus = 207000
poissons_ratio = 0.3
output_q = false
incremental = true
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
[../]
[]
[BCs]
[./crack_y]
type = DirichletBC
variable = disp_y
boundary = 100
value = 0.0
[../]
[./no_z]
type = DirichletBC
variable = disp_z
boundary = 500
value = 0.0
[../]
[./no_z2]
type = DirichletBC
variable = disp_z
boundary = 510
value = 0.0
[../]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 700
value = 0.0
[../]
[./Pressure]
[./Side1]
boundary = 400
function = rampConstant
[../]
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_abs_tol = 1e-5
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Outputs]
file_base = interaction_integral_3d_out
exodus = true
csv = true
[]
(test/tests/geomsearch/2d_moving_penetration/pl_test3qns.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
file = pl_test3q.e
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
normal_smoothing_distance = 0.2
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
normal_smoothing_distance = 0.2
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate10]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate13]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate14]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate15]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate16]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-10
l_max_its = 10
start_time = 0.0
dt = 0.02
end_time = 1.0
[./Quadrature]
order = THIRD
[../]
[]
[Outputs]
file_base = pl_test3qns_out
exodus = true
[]
(test/tests/geomsearch/3d_moving_penetration/pl_test4tt.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
file = pl_test4tt.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./normal_z]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./closest_point_z]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[./diff_z]
type = Diffusion
variable = disp_z
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
tangential_tolerance = 0.09
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
tangential_tolerance = 0.09
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = normal_z
boundary = 11
paired_boundary = 12
quantity = normal_z
[../]
[./penetrate10]
type = PenetrationAux
variable = normal_z
boundary = 12
paired_boundary = 11
quantity = normal_z
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate13]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate14]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate15]
type = PenetrationAux
variable = closest_point_z
boundary = 11
paired_boundary = 12
quantity = closest_point_z
[../]
[./penetrate16]
type = PenetrationAux
variable = closest_point_z
boundary = 12
paired_boundary = 11
quantity = closest_point_z
[../]
[./penetrate17]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate18]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate19]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate20]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b1z]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[./b2z]
type = DirichletBC
variable = disp_z
boundary = 2
value = 0
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-9
l_max_its = 10
start_time = 0.0
dt = 0.02
end_time = 1.0
[]
[Outputs]
file_base = pl_test4tt_out
exodus = true
[]
(modules/tensor_mechanics/test/tests/j_integral_vtest/j_int_surfbreak_ellip_crack_sym_mm_cfp_cm.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[Mesh]
file = ellip_crack_4sym_norad_mm.e
partitioner = centroid
centroid_partitioner_direction = z
[]
[AuxVariables]
[./SED]
order = CONSTANT
family = MONOMIAL
[../]
[./resid_z]
[../]
[]
[Functions]
[./rampConstantUp]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 0.1'
scale_factor = -689.5 #MPa
[../]
[]
[DomainIntegral]
integrals = JIntegral
crack_direction_method = CrackMouth
crack_mouth_boundary = 11
crack_end_direction_method = CrackDirectionVector
crack_direction_vector_end_1 = '0.0 1.0 0.0'
crack_direction_vector_end_2 = '1.0 0.0 0.0'
crack_front_points = '0 254 0
127.308 248.843 0
249.446 233.581 0
361.455 208.835 0
508.003 152.398 0
602.415 80.3208 0
635 0 0'
radius_inner = '12.5 25.0 37.5'
radius_outer = '25.0 37.5 50.0'
intersecting_boundary = '1 2'
symmetry_plane = 2
position_type = angle
incremental = true
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
[../]
[]
[AuxKernels]
[./SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[../]
[]
[BCs]
[./crack_y]
type = DirichletBC
variable = disp_z
boundary = 6
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = 12
value = 0.0
[../]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./Pressure]
[./Side1]
boundary = 5
function = rampConstantUp
[../]
[../]
[] # BCs
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 206800
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
# Two sets of linesearch options are for petsc 3.1 and 3.3 respectively
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
# petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 4'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_abs_tol = 1e-5
nl_rel_tol = 1e-11
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Postprocessors]
[./_dt]
type = TimestepSize
[../]
[./nl_its]
type = NumNonlinearIterations
[../]
[./lin_its]
type = NumLinearIterations
[../]
[./react_z]
type = NodalSum
variable = resid_z
boundary = 5
[../]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = j_int_surfbreak_ellip_crack_sym_mm_cfp_cm_out
exodus = true
csv = true
[]
(modules/richards/test/tests/rogers_stallybrass_clements/rsc02.i)
# RSC test with low-res time and spatial resolution
[Mesh]
type = GeneratedMesh
dim = 2
nx = 200
ny = 1
xmin = 0
xmax = 10 # x is the depth variable, called zeta in RSC
ymin = 0
ymax = 0.05
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '3E-2 5E-1 8E-1'
x = '0 1 5'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = 'pwater poil'
[../]
[./DensityWater]
type = RichardsDensityConstBulk
dens0 = 10
bulk_mod = 2E9
[../]
[./DensityOil]
type = RichardsDensityConstBulk
dens0 = 20
bulk_mod = 2E9
[../]
[./SeffWater]
type = RichardsSeff2waterRSC
oil_viscosity = 2E-3
scale_ratio = 2E3
shift = 10
[../]
[./SeffOil]
type = RichardsSeff2gasRSC
oil_viscosity = 2E-3
scale_ratio = 2E3
shift = 10
[../]
[./RelPerm]
type = RichardsRelPermMonomial
simm = 0
n = 1
[../]
[./Saturation]
type = RichardsSat
s_res = 0.0
sum_s_res = 0.0
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 1.0E-2
[../]
[]
[Variables]
[./pwater]
[../]
[./poil]
[../]
[]
[ICs]
[./water_init]
type = ConstantIC
variable = pwater
value = 0
[../]
[./oil_init]
type = ConstantIC
variable = poil
value = 15
[../]
[]
[Kernels]
[./richardstwater]
type = RichardsMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFlux
variable = pwater
[../]
[./richardstoil]
type = RichardsMassChange
variable = poil
[../]
[./richardsfoil]
type = RichardsFlux
variable = poil
[../]
[]
[AuxVariables]
[./SWater]
[../]
[./SOil]
[../]
[]
[AuxKernels]
[./Seff1VGwater_AuxK]
type = RichardsSeffAux
variable = SWater
seff_UO = SeffWater
pressure_vars = 'pwater poil'
[../]
[./Seff1VGoil_AuxK]
type = RichardsSeffAux
variable = SOil
seff_UO = SeffOil
pressure_vars = 'pwater poil'
[../]
[]
[BCs]
# we are pumping water into a system that has virtually incompressible fluids, hence the pressures rise enormously. this adversely affects convergence because of almost-overflows and precision-loss problems. The fixed things help keep pressures low and so prevent these awful behaviours. the movement of the saturation front is the same regardless of the fixed things.
active = 'recharge fixedoil fixedwater'
[./recharge]
type = RichardsPiecewiseLinearSink
variable = pwater
boundary = 'left'
pressures = '-1E10 1E10'
bare_fluxes = '-1 -1'
use_mobility = false
use_relperm = false
[../]
[./fixedwater]
type = DirichletBC
variable = pwater
boundary = 'right'
value = 0
[../]
[./fixedoil]
type = DirichletBC
variable = poil
boundary = 'right'
value = 15
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.25
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
density_UO = 'DensityWater DensityOil'
relperm_UO = 'RelPerm RelPerm'
SUPG_UO = 'SUPGstandard SUPGstandard'
sat_UO = 'Saturation Saturation'
seff_UO = 'SeffWater SeffOil'
viscosity = '1E-3 2E-3'
gravity = '0E-0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
active = 'andy'
[./andy]
type = SMP
full = true
petsc_options = ''
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-10 1E-10 10000'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
petsc_options = '-snes_converged_reason'
end_time = 5
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = rsc02
interval = 100000
execute_on = 'initial timestep_end final'
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
[]
(modules/tensor_mechanics/test/tests/interaction_integral_benchmark/input.i)
# Uses InteractionIntegralBenchmarkBC to test the mixed-mode stress intensity
# factor capability. InteractionIntegralBenchmarkBC applies a displacement
# field for which KI = KII = KIII = 1.0. Using the option 2d = true gives a
# q field that is constant along the tangent and returns Ki = 1.0 for all i.
# To get the correct value for all nodes with 2d = false, the mesh around the
# crack tip must be refined and the q-function radii must be reduced by at
# least two orders of magnitude.
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[Mesh]
file = 360degree_model.e
displacements = 'disp_x disp_y disp_z'
[]
[Problem]
type = FEProblem
[]
[Functions]
[./kifunc]
type = PiecewiseLinear
x = '0.0 1.0 2.0'
y = '0.0 1.0 2.0'
[../]
[]
[DomainIntegral]
integrals = 'JIntegral InteractionIntegralKI InteractionIntegralKII InteractionIntegralKIII'
boundary = 1001
crack_direction_method = CrackDirectionVector
crack_direction_vector = '1 0 0'
radius_inner = '0.5 1.0 1.5 2.0'
radius_outer = '1.0 1.5 2.0 2.5'
youngs_modulus = 30000
poissons_ratio = 0.3
block = 1
2d = true
axis_2d = 2
equivalent_k = True
incremental = true
[]
[AuxVariables]
[./dq_x]
order = CONSTANT
family = MONOMIAL
[../]
[./dq_y]
order = CONSTANT
family = MONOMIAL
[../]
[./dq_z]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
[../]
[]
[BCs]
[./all_x]
type = InteractionIntegralBenchmarkBC
variable = disp_x
component = x
boundary = 1
KI_function = kifunc
KII_function = 1.0
KIII_function = 1.0
youngs_modulus = 30000
poissons_ratio = 0.3
crack_front_definition = crackFrontDefinition
crack_front_point_index = 0
[../]
[./all_y]
type = InteractionIntegralBenchmarkBC
variable = disp_y
component = y
boundary = 1
KI_function = kifunc
KII_function = 1.0
KIII_function = 1.0
youngs_modulus = 30000
poissons_ratio = 0.3
crack_front_definition = crackFrontDefinition
crack_front_point_index = 0
[../]
[./all_z]
type = InteractionIntegralBenchmarkBC
variable = disp_z
component = z
boundary = 1
KI_function = kifunc
KII_function = 1.0
KIII_function = 1.0
youngs_modulus = 30000
poissons_ratio = 0.3
crack_front_definition = crackFrontDefinition
crack_front_point_index = 0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 30000
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_abs_tol = 1e-3
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 2
num_steps = 2
[]
[Postprocessors]
[./_dt]
type = TimestepSize
[../]
[./nl_its]
type = NumNonlinearIterations
[../]
[./lin_its]
type = NumLinearIterations
[../]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = 360degree_model_out
exodus = true
csv = true
[]
(modules/richards/test/tests/gravity_head_1/gh_fu_22.i)
# investigating validity of immobile saturation
# 50 elements, full upwinding
[Mesh]
type = GeneratedMesh
dim = 1
nx = 50
xmin = -1
xmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGnone
sat_UO = Saturation
seff_UO = SeffVG
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1 10 100 1000 10000'
x = '0 10 100 1000 10000'
[../]
[]
[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 = 0.3
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGnone]
type = RichardsSUPGnone
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
initial_condition = -1.0
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[Kernels]
active = 'richardsf richardst'
[./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-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 = Transient
solve_type = Newton
dt = 1E0
end_time = 1E5
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = gh_fu_22
execute_on = 'timestep_end final'
interval = 10000
exodus = true
[]
(modules/tensor_mechanics/test/tests/smeared_cracking/cracking_xyz.i)
#
[Mesh]
file = cracking_test.e
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Functions]
[./displx]
type = PiecewiseLinear
x = '0 1'
y = '0 0.00175'
[../]
[./velocity_y]
type = ParsedFunction
value = 'if(t < 2, 0.00175, 0)'
[../]
[./velocity_z]
type = ParsedFunction
value = 0.00175
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx'
[../]
[]
[BCs]
[./fix_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./move_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = displx
[../]
[./fix_y]
type = DirichletBC
variable = disp_y
boundary = 2
value = 0.0
[../]
[./move_y]
type = PresetVelocity
variable = disp_y
boundary = 5
function = velocity_y
# time_periods = 'p2 p3'
[../]
[./fix_z]
type = DirichletBC
variable = disp_z
boundary = 3
value = 0.0
[../]
[./move_z]
type = PresetVelocity
variable = disp_z
boundary = 6
function = velocity_z
# time_periods = 'p3'
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 186.5e9
poissons_ratio = .316
[../]
[./elastic_stress]
type = ComputeSmearedCrackingStress
cracking_stress = 119.3e6
softening_models = exponential_softening
[../]
[./exponential_softening]
type = ExponentialSoftening
[../]
[]
[Executioner]
type = Transient
petsc_options_iname = '-ksp_gmres_restart -pc_type'
petsc_options_value = '101 lu'
line_search = 'none'
l_max_its = 100
l_tol = 1e-5
nl_max_its = 100
nl_abs_tol = 1e-4
#nl_rel_tol = 1e-4
nl_rel_tol = 1e-6
start_time = 0.0
end_time = 3.0
dt = 0.01
[]
[Controls]
[./p1]
type = TimePeriod
start_time = 0.0
end_time = 1.0
disable_objects = 'BCs/move_y BCs/move_z'
reverse_on_false = false
execute_on = 'initial timestep_begin'
[../]
[./p2]
type = TimePeriod
start_time = 1.0
end_time = 2.0
disable_objects = 'BCs/move_z'
enable_objects = 'BCs/move_y'
reverse_on_false = false
execute_on = 'initial timestep_begin'
[../]
[./p3]
type = TimePeriod
start_time = 2.0
end_time = 3.0
enable_objects = 'BCs/move_y BCs/move_z'
reverse_on_false = false
execute_on = 'initial timestep_begin'
set_sync_times = true
[../]
[]
[Outputs]
exodus = true
[]
(modules/contact/test/tests/normalized_penalty/normalized_penalty_kin.i)
[GlobalParams]
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Mesh]
file = normalized_penalty.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Functions]
[./left_x]
type = PiecewiseLinear
x = '0 1 2'
y = '0 0.02 0'
[../]
[]
[AuxVariables]
[./saved_x]
[../]
[./saved_y]
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = FINITE
generate_output = 'stress_xx'
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
[]
[]
[Contact]
[./m3_s2]
primary = 3
secondary = 2
penalty = 1e10
normalize_penalty = true
tangential_tolerance = 1e-3
[../]
[]
[BCs]
[./left_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 1
function = left_x
[../]
[./y]
type = DirichletBC
variable = disp_y
boundary = '1 2 3 4'
value = 0.0
[../]
[./right]
type = DirichletBC
variable = disp_x
boundary = '3 4'
value = 0
[../]
[]
[Materials]
[./stiffStuff1]
type = ComputeIsotropicElasticityTensor
block = '1 2 3 4 1000'
youngs_modulus = 3e8
poissons_ratio = 0.0
[../]
[./stiffStuff1_stress]
type = ComputeFiniteStrainElasticStress
block = '1 2 3 4 1000'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -ksp_gmres_restart'
petsc_options_value = 'lu 101'
line_search = 'none'
nl_rel_tol = 1e-12
nl_abs_tol = 3e-8
l_max_its = 100
nl_max_its = 20
dt = 0.5
num_steps = 4
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/beam/dynamic/dyn_euler_small_added_mass_inertia_damping.i)
# Test for small strain euler beam vibration in y direction
# An impulse load is applied at the end of a cantilever beam of length 4m.
# The beam is massless with a lumped mass at the end of the beam. The lumped
# mass also has a moment of inertia associated with it.
# The properties of the cantilever beam are as follows:
# Young's modulus (E) = 1e4
# Shear modulus (G) = 4e7
# Shear coefficient (k) = 1.0
# Cross-section area (A) = 0.01
# Iy = 1e-4 = Iz
# Length (L)= 4 m
# mass (m) = 0.01899772
# Moment of inertia of lumped mass:
# Ixx = 0.2
# Iyy = 0.1
# Izz = 0.1
# mass proportional damping coefficient (eta) = 0.1
# For this beam, the dimensionless parameter alpha = kAGL^2/EI = 6.4e6
# Therefore, the beam behaves like a Euler-Bernoulli beam.
# The displacement time history from this analysis matches with that obtained from Abaqus.
# Values from the first few time steps are as follows:
# time disp_y vel_y accel_y
# 0.0 0.0 0.0 0.0
# 0.1 0.001278249649738 0.025564992994761 0.51129985989521
# 0.2 0.0049813090917644 0.048496195845768 -0.052675802875074
# 0.3 0.0094704658873002 0.041286940064947 -0.091509312741339
# 0.4 0.013082280729802 0.03094935678508 -0.115242352856
# 0.5 0.015588313103503 0.019171290688959 -0.12031896906642
[Mesh]
type = GeneratedMesh
dim = 1
nx = 10
xmin = 0.0
xmax = 4.0
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[./rot_x]
order = FIRST
family = LAGRANGE
[../]
[./rot_y]
order = FIRST
family = LAGRANGE
[../]
[./rot_z]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./vel_x]
order = FIRST
family = LAGRANGE
[../]
[./vel_y]
order = FIRST
family = LAGRANGE
[../]
[./vel_z]
order = FIRST
family = LAGRANGE
[../]
[./accel_x]
order = FIRST
family = LAGRANGE
[../]
[./accel_y]
order = FIRST
family = LAGRANGE
[../]
[./accel_z]
order = FIRST
family = LAGRANGE
[../]
[./rot_vel_x]
order = FIRST
family = LAGRANGE
[../]
[./rot_vel_y]
order = FIRST
family = LAGRANGE
[../]
[./rot_vel_z]
order = FIRST
family = LAGRANGE
[../]
[./rot_accel_x]
order = FIRST
family = LAGRANGE
[../]
[./rot_accel_y]
order = FIRST
family = LAGRANGE
[../]
[./rot_accel_z]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./accel_x]
type = NewmarkAccelAux
variable = accel_x
displacement = disp_x
velocity = vel_x
beta = 0.25
execute_on = timestep_end
[../]
[./vel_x]
type = NewmarkVelAux
variable = vel_x
acceleration = accel_x
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_y]
type = NewmarkAccelAux
variable = accel_y
displacement = disp_y
velocity = vel_y
beta = 0.25
execute_on = timestep_end
[../]
[./vel_y]
type = NewmarkVelAux
variable = vel_y
acceleration = accel_y
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_z]
type = NewmarkAccelAux
variable = accel_z
displacement = disp_z
velocity = vel_z
beta = 0.25
execute_on = timestep_end
[../]
[./vel_z]
type = NewmarkVelAux
variable = vel_z
acceleration = accel_z
gamma = 0.5
execute_on = timestep_end
[../]
[./rot_accel_x]
type = NewmarkAccelAux
variable = rot_accel_x
displacement = rot_x
velocity = rot_vel_x
beta = 0.25
execute_on = timestep_end
[../]
[./rot_vel_x]
type = NewmarkVelAux
variable = rot_vel_x
acceleration = rot_accel_x
gamma = 0.5
execute_on = timestep_end
[../]
[./rot_accel_y]
type = NewmarkAccelAux
variable = rot_accel_y
displacement = rot_y
velocity = rot_vel_y
beta = 0.25
execute_on = timestep_end
[../]
[./rot_vel_y]
type = NewmarkVelAux
variable = rot_vel_y
acceleration = rot_accel_y
gamma = 0.5
execute_on = timestep_end
[../]
[./rot_accel_z]
type = NewmarkAccelAux
variable = rot_accel_z
displacement = rot_z
velocity = rot_vel_z
beta = 0.25
execute_on = timestep_end
[../]
[./rot_vel_z]
type = NewmarkVelAux
variable = rot_vel_z
acceleration = rot_accel_z
gamma = 0.5
execute_on = timestep_end
[../]
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./fixy1]
type = DirichletBC
variable = disp_y
boundary = left
value = 0.0
[../]
[./fixz1]
type = DirichletBC
variable = disp_z
boundary = left
value = 0.0
[../]
[./fixr1]
type = DirichletBC
variable = rot_x
boundary = left
value = 0.0
[../]
[./fixr2]
type = DirichletBC
variable = rot_y
boundary = left
value = 0.0
[../]
[./fixr3]
type = DirichletBC
variable = rot_z
boundary = left
value = 0.0
[../]
[]
[NodalKernels]
[./force_y2]
type = UserForcingFunctionNodalKernel
variable = disp_y
boundary = right
function = force
[../]
[./x_inertial]
type = NodalTranslationalInertia
variable = disp_x
velocity = vel_x
acceleration = accel_x
boundary = right
beta = 0.25
gamma = 0.5
mass = 0.01899772
eta = 0.1
[../]
[./y_inertial]
type = NodalTranslationalInertia
variable = disp_y
velocity = vel_y
acceleration = accel_y
boundary = right
beta = 0.25
gamma = 0.5
mass = 0.01899772
eta = 0.1
[../]
[./z_inertial]
type = NodalTranslationalInertia
variable = disp_z
velocity = vel_z
acceleration = accel_z
boundary = right
beta = 0.25
gamma = 0.5
mass = 0.01899772
eta = 0.1
[../]
[./rot_x_inertial]
type = NodalRotationalInertia
variable = rot_x
rotations = 'rot_x rot_y rot_z'
rotational_velocities = 'rot_vel_x rot_vel_y rot_vel_z'
rotational_accelerations= 'rot_accel_x rot_accel_y rot_accel_z'
boundary = right
beta = 0.25
gamma = 0.5
Ixx = 2e-1
Iyy = 1e-1
Izz = 1e-1
eta = 0.1
component = 0
[../]
[./rot_y_inertial]
type = NodalRotationalInertia
variable = rot_y
rotations = 'rot_x rot_y rot_z'
rotational_velocities = 'rot_vel_x rot_vel_y rot_vel_z'
rotational_accelerations= 'rot_accel_x rot_accel_y rot_accel_z'
boundary = right
beta = 0.25
gamma = 0.5
Ixx = 2e-1
Iyy = 1e-1
Izz = 1e-1
eta = 0.1
component = 1
[../]
[./rot_z_inertial]
type = NodalRotationalInertia
variable = rot_z
rotations = 'rot_x rot_y rot_z'
rotational_velocities = 'rot_vel_x rot_vel_y rot_vel_z'
rotational_accelerations= 'rot_accel_x rot_accel_y rot_accel_z'
boundary = right
beta = 0.25
gamma = 0.5
Ixx = 2e-1
Iyy = 1e-1
Izz = 1e-1
eta = 0.1
component = 2
[../]
[]
[Functions]
[./force]
type = PiecewiseLinear
x = '0.0 0.1 0.2 10.0'
y = '0.0 1e-2 0.0 0.0'
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options_iname = '-ksp_type -pc_type'
petsc_options_value = 'preonly lu'
dt = 0.1
end_time = 5.0
timestep_tolerance = 1e-6
[]
[Kernels]
[./solid_disp_x]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 0
variable = disp_x
[../]
[./solid_disp_y]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 1
variable = disp_y
[../]
[./solid_disp_z]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 2
variable = disp_z
[../]
[./solid_rot_x]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 3
variable = rot_x
[../]
[./solid_rot_y]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 4
variable = rot_y
[../]
[./solid_rot_z]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 5
variable = rot_z
[../]
[]
[Materials]
[./elasticity]
type = ComputeElasticityBeam
youngs_modulus = 1.0e4
poissons_ratio = -0.999875
shear_coefficient = 1.0
block = 0
[../]
[./strain]
type = ComputeIncrementalBeamStrain
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
area = 0.01
Ay = 0.0
Az = 0.0
Iy = 1.0e-4
Iz = 1.0e-4
y_orientation = '0.0 1.0 0.0'
[../]
[./stress]
type = ComputeBeamResultants
block = 0
[../]
[]
[Postprocessors]
[./disp_x]
type = PointValue
point = '4.0 0.0 0.0'
variable = disp_x
[../]
[./disp_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = disp_y
[../]
[./vel_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = vel_y
[../]
[./accel_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = accel_y
[../]
[]
[Outputs]
exodus = true
csv = true
perf_graph = true
[]
(modules/richards/test/tests/broadbridge_white/bw02.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 200
ny = 1
xmin = -10
xmax = 10
ymin = 0
ymax = 0.05
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1E-1 5E-1 5E-1'
x = '0 1 10'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 10
bulk_mod = 2E9
[../]
[./SeffBW]
type = RichardsSeff1BWsmall
Sn = 0.0
Ss = 1.0
C = 1.5
las = 2
[../]
[./RelPermBW]
type = RichardsRelPermBW
Sn = 0.0
Ss = 1.0
Kn = 0
Ks = 1
C = 1.5
[../]
[./Saturation]
type = RichardsSat
s_res = 0.0
sum_s_res = 0.0
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 1.0E2
[../]
[]
[Variables]
active = 'pressure'
[./pressure]
order = FIRST
family = LAGRANGE
initial_condition = -9E2
[../]
[]
[Kernels]
active = 'richardsf richardst'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = SeffBW
pressure_vars = pressure
[../]
[]
[BCs]
active = 'recharge'
[./recharge]
type = RichardsPiecewiseLinearSink
variable = pressure
boundary = 'right'
pressures = '-1E10 1E10'
bare_fluxes = '-1.25 -1.25' # corresponds to Rstar being 0.5 because i have to multiply by density*porosity
use_mobility = false
use_relperm = false
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.25
mat_permeability = '1 0 0 0 1 0 0 0 1'
density_UO = DensityConstBulk
relperm_UO = RelPermBW
SUPG_UO = SUPGstandard
sat_UO = Saturation
seff_UO = SeffBW
viscosity = 4
gravity = '-0.1 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
active = 'andy'
[./andy]
type = SMP
full = true
petsc_options = ''
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-10 1E-10 10000'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
petsc_options = '-snes_converged_reason'
end_time = 2
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = bw02
interval = 10000
execute_on = 'timestep_end final'
exodus = true
[]
(modules/tensor_mechanics/test/tests/strain_energy_density/rate_incr_model_elas_plas.i)
# Single element test to check the strain energy density calculation
[GlobalParams]
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
xmin = 0
xmax = 1
ymin = 0
ymax = 2
[]
[AuxVariables]
[./SED]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./rampConstantUp]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = -100
[../]
[./ramp_disp_y]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 6.8e-6 1.36e-5'
[../]
[]
[Modules/TensorMechanics/Master]
[./master]
strain = SMALL
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress elastic_strain_xx elastic_strain_yy elastic_strain_zz plastic_strain_xx plastic_strain_yy plastic_strain_zz strain_xx strain_yy strain_zz'
planar_formulation = PLANE_STRAIN
[../]
[]
[AuxKernels]
[./SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
variable = disp_x
preset = false
boundary = 'left'
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_y
preset = false
boundary = 'bottom'
value = 0.0
[../]
[./top_disp]
type = FunctionDirichletBC
variable = disp_y
preset = false
boundary = 'top'
function = ramp_disp_y
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 30e+6
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'isoplas'
[../]
[./isoplas]
type = IsotropicPlasticityStressUpdate
yield_stress = 1e2
hardening_constant = 0.0
[../]
[./strain_energy_density]
type = StrainEnergyDensity
incremental = true
[../]
[]
[Executioner]
type = Transient
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 4'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_abs_tol = 3e-7
nl_rel_tol = 1e-12
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 2
num_steps = 2
[]
[Postprocessors]
[./epxx]
type = ElementalVariableValue
variable = elastic_strain_xx
elementid = 0
[../]
[./epyy]
type = ElementalVariableValue
variable = elastic_strain_yy
elementid = 0
[../]
[./epzz]
type = ElementalVariableValue
variable = elastic_strain_zz
elementid = 0
[../]
[./eplxx]
type = ElementalVariableValue
variable = plastic_strain_xx
elementid = 0
[../]
[./eplyy]
type = ElementalVariableValue
variable = plastic_strain_yy
elementid = 0
[../]
[./eplzz]
type = ElementalVariableValue
variable = plastic_strain_zz
elementid = 0
[../]
[./etxx]
type = ElementalVariableValue
variable = strain_xx
elementid = 0
[../]
[./etyy]
type = ElementalVariableValue
variable = strain_yy
elementid = 0
[../]
[./etzz]
type = ElementalVariableValue
variable = strain_zz
elementid = 0
[../]
[./sigxx]
type = ElementAverageValue
variable = stress_xx
[../]
[./sigyy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigzz]
type = ElementAverageValue
variable = stress_zz
[../]
[./SED]
type = ElementAverageValue
variable = SED
[../]
[]
[Outputs]
exodus = true
csv = true
[]
(modules/combined/test/tests/thermal_elastic/ad-thermal_elastic.i)
# Patch Test
# This test is designed to compute constant xx, yy, zz, xy, yz, and xz
# stress on a set of irregular hexes. The mesh is composed of one
# block with seven elements. The elements form a unit cube with one
# internal element. There is a nodeset for each exterior node.
# The cube is displaced by 1e-6 units in x, 2e-6 in y, and 3e-6 in z.
# The faces are sheared as well (1e-6, 2e-6, and 3e-6 for xy, yz, and
# zx). This gives a uniform strain/stress state for all six unique
# tensor components. This displacement is again applied in the second
# step.
# With Young's modulus at 1e6 and Poisson's ratio at 0, the shear
# modulus is 5e5 (G=E/2/(1+nu)). Therefore, for the mechanical strain,
#
# stress xx = 1e6 * 1e-6 = 1
# stress yy = 1e6 * 2e-6 = 2
# stress zz = 1e6 * 3e-6 = 3
# stress xy = 2 * 5e5 * 1e-6 / 2 = 0.5
# (2 * G * gamma_xy / 2 = 2 * G * epsilon_xy)
# stress yz = 2 * 5e5 * 2e-6 / 2 = 1
# stress zx = 2 * 5e5 * 3e-6 / 2 = 1.5
# Young's modulus is a function of temperature for this test. The
# temperature changes from 100 to 500. The Young's modulus drops
# due to that temperature change from 1e6 to 6e5.
# Poisson's ratio also is a function of temperature and changes from
# 0 to 0.25.
# At the end of the temperature ramp, E=6e5 and nu=0.25. This gives
# G=2.4e=5. lambda=E*nu/(1+nu)/(1-2*nu)=2.4E5. The final stress
# is therefore
# stress xx = 2.4e5 * 12e-6 + 2*2.4e5*2e-6 = 3.84
# stress yy = 2.4e5 * 12e-6 + 2*2.4e5*4e-6 = 4.80
# stress zz = 2.4e5 * 12e-6 + 2*2.4e5*6e-6 = 5.76
# stress xy = 2 * 2.4e5 * 2e-6 / 2 = 0.48
# (2 * G * gamma_xy / 2 = 2 * G * epsilon_xy)
# stress yz = 2 * 2.4e5 * 4e-6 / 2 = 0.96
# stress xz = 2 * 2.4e5 * 6e-6 / 2 = 1.44
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
file = thermal_elastic.e
[]
[Functions]
[./ramp1]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 2.'
scale_factor = 1e-6
[../]
[./ramp2]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 2.'
scale_factor = 2e-6
[../]
[./ramp3]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 2.'
scale_factor = 3e-6
[../]
[./ramp4]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 2.'
scale_factor = 4e-6
[../]
[./ramp6]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 2.'
scale_factor = 6e-6
[../]
[./tempFunc]
type = PiecewiseLinear
x = '0 1 2'
y = '100.0 100.0 500.0'
[../]
[]
[Variables]
[./temp]
initial_condition = 100.0
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_xz stress_yz'
strain = FINITE
use_automatic_differentiation = true
[../]
[]
[Kernels]
[./heat]
type = ADDiffusion
variable = temp
[../]
[]
[BCs]
[./node1_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./node1_y]
type = ADFunctionDirichletBC
variable = disp_y
boundary = 1
function = ramp2
[../]
[./node1_z]
type = ADFunctionDirichletBC
variable = disp_z
boundary = 1
function = ramp3
[../]
[./node2_x]
type = ADFunctionDirichletBC
variable = disp_x
boundary = 2
function = ramp1
[../]
[./node2_y]
type = ADFunctionDirichletBC
variable = disp_y
boundary = 2
function = ramp2
[../]
[./node2_z]
type = ADFunctionDirichletBC
variable = disp_z
boundary = 2
function = ramp6
[../]
[./node3_x]
type = ADFunctionDirichletBC
variable = disp_x
boundary = 3
function = ramp1
[../]
[./node3_y]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.0
[../]
[./node3_z]
type = ADFunctionDirichletBC
variable = disp_z
boundary = 3
function = ramp3
[../]
[./node4_x]
type = DirichletBC
variable = disp_x
boundary = 4
value = 0.0
[../]
[./node4_y]
type = DirichletBC
variable = disp_y
boundary = 4
value = 0.0
[../]
[./node4_z]
type = DirichletBC
variable = disp_z
boundary = 4
value = 0.0
[../]
[./node5_x]
type = ADFunctionDirichletBC
variable = disp_x
boundary = 5
function = ramp1
[../]
[./node5_y]
type = ADFunctionDirichletBC
variable = disp_y
boundary = 5
function = ramp4
[../]
[./node5_z]
type = ADFunctionDirichletBC
variable = disp_z
boundary = 5
function = ramp3
[../]
[./node6_x]
type = ADFunctionDirichletBC
variable = disp_x
boundary = 6
function = ramp2
[../]
[./node6_y]
type = ADFunctionDirichletBC
variable = disp_y
boundary = 6
function = ramp4
[../]
[./node6_z]
type = ADFunctionDirichletBC
variable = disp_z
boundary = 6
function = ramp6
[../]
[./node7_x]
type = ADFunctionDirichletBC
variable = disp_x
boundary = 7
function = ramp2
[../]
[./node7_y]
type = ADFunctionDirichletBC
variable = disp_y
boundary = 7
function = ramp2
[../]
[./node7_z]
type = ADFunctionDirichletBC
variable = disp_z
boundary = 7
function = ramp3
[../]
[./node8_x]
type = ADFunctionDirichletBC
variable = disp_x
boundary = 8
function = ramp1
[../]
[./node8_y]
type = ADFunctionDirichletBC
variable = disp_y
boundary = 8
function = ramp2
[../]
[./node8_z]
type = DirichletBC
variable = disp_z
boundary = 8
value = 0.0
[../]
[./temp]
type = ADFunctionDirichletBC
variable = temp
boundary = '10 12'
function = tempFunc
[../]
[]
[Materials]
[./youngs_modulus]
type = ADPiecewiseLinearInterpolationMaterial
x = '100 500'
y = '1e6 6e5'
property = youngs_modulus
variable = temp
[../]
[./poissons_ratio]
type = ADPiecewiseLinearInterpolationMaterial
x = '100 500'
y = '0 0.25'
property = poissons_ratio
variable = temp
[../]
[./elasticity_tensor]
type = ADComputeVariableIsotropicElasticityTensor
youngs_modulus = youngs_modulus
poissons_ratio = poissons_ratio
[../]
[./stress]
type = ADComputeFiniteStrainElasticStress
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
nl_rel_tol = 1e-9
nl_abs_tol = 1e-9
l_max_its = 20
start_time = 0.0
dt = 1.0
end_time = 2.0
[]
[Outputs]
exodus = true
[]
(test/tests/geomsearch/3d_moving_penetration_smoothing/pl_test4nstt.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
file = pl_test4tt.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./normal_z]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./closest_point_z]
[../]
# [./element_id]
# [../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[./diff_z]
type = Diffusion
variable = disp_z
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
tangential_tolerance = 0.09
normal_smoothing_distance = 0.2
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
tangential_tolerance = 0.09
normal_smoothing_distance = 0.2
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = normal_z
boundary = 11
paired_boundary = 12
quantity = normal_z
[../]
[./penetrate10]
type = PenetrationAux
variable = normal_z
boundary = 12
paired_boundary = 11
quantity = normal_z
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate13]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate14]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate15]
type = PenetrationAux
variable = closest_point_z
boundary = 11
paired_boundary = 12
quantity = closest_point_z
[../]
[./penetrate16]
type = PenetrationAux
variable = closest_point_z
boundary = 12
paired_boundary = 11
quantity = closest_point_z
[../]
# [./penetrate17]
# type = PenetrationAux
# variable = element_id
# boundary = 11
# paired_boundary = 12
# quantity = element_id
# [../]
#
# [./penetrate18]
# type = PenetrationAux
# variable = element_id
# boundary = 12
# paired_boundary = 11
# quantity = element_id
# [../]
[./penetrate19]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate20]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b1z]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[./b2z]
type = DirichletBC
variable = disp_z
boundary = 2
value = 0
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-9
l_max_its = 10
start_time = 0.0
dt = 0.02
end_time = 1.0
[]
[Outputs]
file_base = pl_test4nstt_out
exodus = true
[]
(modules/combined/test/tests/poro_mechanics/mandel.i)
# Mandel's problem of consolodation of a drained medium
#
# A sample is in plane strain.
# -a <= x <= a
# -b <= y <= b
# It is squashed with constant force by impermeable, frictionless plattens on its top and bottom surfaces (at y=+/-b)
# Fluid is allowed to leak out from its sides (at x=+/-a)
# The porepressure within the sample is monitored.
#
# As is common in the literature, this is simulated by
# considering the quarter-sample, 0<=x<=a and 0<=y<=b, with
# impermeable, roller BCs at x=0 and y=0 and y=b.
# Porepressure is fixed at zero on x=a.
# Porepressure and displacement are initialised to zero.
# Then the top (y=b) is moved downwards with prescribed velocity,
# so that the total force that is inducing this downwards velocity
# is fixed. The velocity is worked out by solving Mandel's problem
# analytically, and the total force is monitored in the simulation
# to check that it indeed remains constant.
#
# Here are the problem's parameters, and their values:
# Soil width. a = 1
# Soil height. b = 0.1
# Soil's Lame lambda. la = 0.5
# Soil's Lame mu, which is also the Soil's shear modulus. mu = G = 0.75
# Soil bulk modulus. K = la + 2*mu/3 = 1
# Drained Poisson ratio. nu = (3K - 2G)/(6K + 2G) = 0.2
# Soil bulk compliance. 1/K = 1
# Fluid bulk modulus. Kf = 8
# Fluid bulk compliance. 1/Kf = 0.125
# Soil initial porosity. phi0 = 0.1
# Biot coefficient. alpha = 0.6
# Biot modulus. M = 1/(phi0/Kf + (alpha - phi0)(1 - alpha)/K) = 4.705882
# Undrained bulk modulus. Ku = K + alpha^2*M = 2.694118
# Undrained Poisson ratio. nuu = (3Ku - 2G)/(6Ku + 2G) = 0.372627
# Skempton coefficient. B = alpha*M/Ku = 1.048035
# Fluid mobility (soil permeability/fluid viscosity). k = 1.5
# Consolidation coefficient. c = 2*k*B^2*G*(1-nu)*(1+nuu)^2/9/(1-nuu)/(nuu-nu) = 3.821656
# Normal stress on top. F = 1
#
# The solution for porepressure and displacements is given in
# AHD Cheng and E Detournay "A direct boundary element method for plane strain poroelasticity" International Journal of Numerical and Analytical Methods in Geomechanics 12 (1988) 551-572.
# The solution involves complicated infinite series, so I shall not write it here
[Mesh]
type = GeneratedMesh
dim = 3
nx = 10
ny = 1
nz = 1
xmin = 0
xmax = 1
ymin = 0
ymax = 0.1
zmin = 0
zmax = 1
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
porepressure = porepressure
block = 0
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[./porepressure]
[../]
[]
[BCs]
[./roller_xmin]
type = DirichletBC
variable = disp_x
value = 0
boundary = 'left'
[../]
[./roller_ymin]
type = DirichletBC
variable = disp_y
value = 0
boundary = 'bottom'
[../]
[./plane_strain]
type = DirichletBC
variable = disp_z
value = 0
boundary = 'back front'
[../]
[./xmax_drained]
type = DirichletBC
variable = porepressure
value = 0
boundary = right
[../]
[./top_velocity]
type = FunctionDirichletBC
variable = disp_y
function = top_velocity
boundary = top
[../]
[]
[Functions]
[./top_velocity]
type = PiecewiseLinear
x = '0 0.002 0.006 0.014 0.03 0.046 0.062 0.078 0.094 0.11 0.126 0.142 0.158 0.174 0.19 0.206 0.222 0.238 0.254 0.27 0.286 0.302 0.318 0.334 0.35 0.366 0.382 0.398 0.414 0.43 0.446 0.462 0.478 0.494 0.51 0.526 0.542 0.558 0.574 0.59 0.606 0.622 0.638 0.654 0.67 0.686 0.702'
y = '-0.041824842 -0.042730269 -0.043412712 -0.04428867 -0.045509181 -0.04645965 -0.047268246 -0.047974749 -0.048597109 -0.0491467 -0.049632388 -0.050061697 -0.050441198 -0.050776675 -0.051073238 -0.0513354 -0.051567152 -0.051772022 -0.051953128 -0.052113227 -0.052254754 -0.052379865 -0.052490464 -0.052588233 -0.052674662 -0.052751065 -0.052818606 -0.052878312 -0.052931093 -0.052977751 -0.053018997 -0.053055459 -0.053087691 -0.053116185 -0.053141373 -0.05316364 -0.053183324 -0.053200724 -0.053216106 -0.053229704 -0.053241725 -0.053252351 -0.053261745 -0.053270049 -0.053277389 -0.053283879 -0.053289615'
[../]
[]
[AuxVariables]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./tot_force]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
[../]
[./tot_force]
type = ParsedAux
args = 'stress_yy porepressure'
execute_on = timestep_end
variable = tot_force
function = '-stress_yy+0.6*porepressure'
[../]
[]
[Kernels]
[./grad_stress_x]
type = StressDivergenceTensors
variable = disp_x
component = 0
[../]
[./grad_stress_y]
type = StressDivergenceTensors
variable = disp_y
component = 1
[../]
[./grad_stress_z]
type = StressDivergenceTensors
variable = disp_z
component = 2
[../]
[./poro_x]
type = PoroMechanicsCoupling
variable = disp_x
component = 0
[../]
[./poro_y]
type = PoroMechanicsCoupling
variable = disp_y
component = 1
[../]
[./poro_z]
type = PoroMechanicsCoupling
variable = disp_z
component = 2
[../]
[./poro_timederiv]
type = PoroFullSatTimeDerivative
variable = porepressure
[../]
[./darcy_flow]
type = CoefDiffusion
variable = porepressure
coef = 1.5
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeElasticityTensor
C_ijkl = '0.5 0.75'
# bulk modulus is lambda + 2*mu/3 = 0.5 + 2*0.75/3 = 1
fill_method = symmetric_isotropic
[../]
[./strain]
type = ComputeSmallStrain
displacements = 'disp_x disp_y disp_z'
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[./poro_material]
type = PoroFullSatMaterial
porosity0 = 0.1
biot_coefficient = 0.6
solid_bulk_compliance = 1
fluid_bulk_compliance = 0.125
constant_porosity = true
[../]
[]
[Postprocessors]
[./p0]
type = PointValue
outputs = csv
point = '0.0 0 0'
variable = porepressure
[../]
[./p1]
type = PointValue
outputs = csv
point = '0.1 0 0'
variable = porepressure
[../]
[./p2]
type = PointValue
outputs = csv
point = '0.2 0 0'
variable = porepressure
[../]
[./p3]
type = PointValue
outputs = csv
point = '0.3 0 0'
variable = porepressure
[../]
[./p4]
type = PointValue
outputs = csv
point = '0.4 0 0'
variable = porepressure
[../]
[./p5]
type = PointValue
outputs = csv
point = '0.5 0 0'
variable = porepressure
[../]
[./p6]
type = PointValue
outputs = csv
point = '0.6 0 0'
variable = porepressure
[../]
[./p7]
type = PointValue
outputs = csv
point = '0.7 0 0'
variable = porepressure
[../]
[./p8]
type = PointValue
outputs = csv
point = '0.8 0 0'
variable = porepressure
[../]
[./p9]
type = PointValue
outputs = csv
point = '0.9 0 0'
variable = porepressure
[../]
[./p99]
type = PointValue
outputs = csv
point = '1 0 0'
variable = porepressure
[../]
[./xdisp]
type = PointValue
outputs = csv
point = '1 0.1 0'
variable = disp_x
[../]
[./ydisp]
type = PointValue
outputs = csv
point = '1 0.1 0'
variable = disp_y
[../]
[./total_downwards_force]
type = ElementAverageValue
outputs = csv
variable = tot_force
[../]
[./dt]
type = FunctionValuePostprocessor
outputs = console
function = if(0.15*t<0.01,0.15*t,0.01)
[../]
[]
[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-14 1E-10 10000'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
start_time = 0
end_time = 0.7
[./TimeStepper]
type = PostprocessorDT
postprocessor = dt
dt = 0.001
[../]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = mandel
[./csv]
interval = 3
type = CSV
[../]
[]
(modules/tensor_mechanics/test/tests/smeared_cracking/cracking_plane_stress.i)
################################################################################
#
# 1x1x1 cube, single element
# simulate plane stress
# pull in +y direction on right surface to produce shear strain
#
#
#
# ____________
# /| /|
# / | 5 / | -X Left 1
# /__________ / | +X Right 4
# | | 3 | | +Y Top 5
# | 1 | | 4 | -Y Bottom 2
# | |_6_____|___| y +Z Front 6
# | / | / ^ -Z Back 3
# | / 2 | / |
# |/__________|/ |
# ----> x
# /
# /
# z
#
#
#
#################################################################################
[Mesh]
file = cube.e
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Functions]
[./displ]
type = PiecewiseLinear
x = '0 0.1 0.2 0.3 0.4'
y = '0 0.0026 0 -0.0026 0'
[../]
[./pressure]
type = PiecewiseLinear
x = '0 0.1 0.2 0.3 0.4'
y = '0 0 0 0 0'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx'
[../]
[]
[BCs]
[./pull_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = displ
[../]
[./pin_x]
type = DirichletBC
variable = disp_x
boundary = '1 4'
value = 0.0
[../]
[./pin_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./back]
type = DirichletBC
variable = disp_z
boundary = '3'
value = 0.0
[../]
[./front]
type = Pressure
variable = disp_z
component = 2
boundary = 6
function = pressure
factor = 1.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 200.0e3
poissons_ratio = .3
[../]
[./elastic_stress]
type = ComputeSmearedCrackingStress
cracking_stress = 120
shear_retention_factor = 0.1
softening_models = exponential_softening
[../]
[./exponential_softening]
type = ExponentialSoftening
residual_stress = 0.1
beta = 0.1
[../]
[]
[Executioner]
type = Transient
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -sub_pc_type'
petsc_options_value = '101 asm lu'
line_search = 'none'
l_max_its = 100
nl_max_its = 100
nl_rel_tol = 1e-12
nl_abs_tol = 1e-8
l_tol = 1e-5
start_time = 0.0
end_time = 0.4
dt = 0.04
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/beam/dynamic/dyn_euler_small_rayleigh_hht_action.i)
# Test for damped small strain euler beam vibration in y direction
# An impulse load is applied at the end of a cantilever beam of length 4m.
# The properties of the cantilever beam are as follows:
# Young's modulus (E) = 1e4
# Shear modulus (G) = 4e7
# Shear coefficient (k) = 1.0
# Cross-section area (A) = 0.01
# Iy = 1e-4 = Iz
# Length (L)= 4 m
# density (rho) = 1.0
# mass proportional rayleigh damping(eta) = 0.1
# stiffness proportional rayleigh damping(eta) = 0.1
# HHT time integration parameter (alpha) = -0.3
# Corresponding Newmark beta time integration parameters beta = 0.4225 and gamma = 0.8
# For this beam, the dimensionless parameter alpha = kAGL^2/EI = 6.4e6
# Therefore, the behaves like a Euler-Bernoulli beam.
# The displacement time history from this analysis matches with that obtained from Abaqus.
# Values from the first few time steps are as follows:
# time disp_y vel_y accel_y
# 0.0 0.0 0.0 0.0
# 0.2 0.019898364318588 0.18838688112273 1.1774180070171
# 0.4 0.045577003505278 0.087329917525455 -0.92596052423724
# 0.6 0.063767907208218 0.084330765885995 0.21274543331268
# 0.8 0.073602908614573 0.020029576220975 -0.45506879373455
# 1.0 0.06841704414745 -0.071840076837194 -0.46041813317992
[Mesh]
type = GeneratedMesh
dim = 1
nx = 10
xmin = 0.0
xmax = 4.0
displacements = 'disp_x disp_y disp_z'
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./fixy1]
type = DirichletBC
variable = disp_y
boundary = left
value = 0.0
[../]
[./fixz1]
type = DirichletBC
variable = disp_z
boundary = left
value = 0.0
[../]
[./fixr1]
type = DirichletBC
variable = rot_x
boundary = left
value = 0.0
[../]
[./fixr2]
type = DirichletBC
variable = rot_y
boundary = left
value = 0.0
[../]
[./fixr3]
type = DirichletBC
variable = rot_z
boundary = left
value = 0.0
[../]
[]
[NodalKernels]
[./force_y2]
type = UserForcingFunctionNodalKernel
variable = disp_y
boundary = right
function = force
[../]
[]
[Functions]
[./force]
type = PiecewiseLinear
x = '0.0 0.2 0.4 10.0'
y = '0.0 0.01 0.0 0.0'
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
line_search = 'none'
l_tol = 1e-11
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 0.2
end_time = 5.0
timestep_tolerance = 1e-6
[]
[Modules/TensorMechanics/LineElementMaster]
[./all]
add_variables = true
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
# Geometry parameters
area = 0.01
Iy = 1e-4
Iz = 1e-4
y_orientation = '0.0 1.0 0.0'
# dynamic simulation using consistent mass/inertia matrix
dynamic_consistent_inertia = true
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y rot_vel_z'
rotational_accelerations = 'rot_accel_x rot_accel_y rot_accel_z'
density = 1.0
beta = 0.4225 # Newmark time integraion parameter
gamma = 0.8 # Newmark time integraion parameter
# optional parameters for numerical (alpha) and Rayleigh damping
alpha = -0.3 # HHT time integration parameter
eta = 0.1 # Mass proportional Rayleigh damping
zeta = 0.1 # Stiffness proportional Rayleigh damping
[../]
[]
[Materials]
[./elasticity]
type = ComputeElasticityBeam
youngs_modulus = 1.0e4
poissons_ratio = -0.999875
shear_coefficient = 1.0
block = 0
[../]
[./stress]
type = ComputeBeamResultants
block = 0
[../]
[]
[Postprocessors]
[./disp_x]
type = PointValue
point = '4.0 0.0 0.0'
variable = disp_x
[../]
[./disp_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = disp_y
[../]
[./vel_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = vel_y
[../]
[./accel_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = accel_y
[../]
[]
[Outputs]
file_base = 'dyn_euler_small_rayleigh_hht_out'
exodus = true
csv = true
perf_graph = true
[]
(modules/porous_flow/test/tests/infiltration_and_drainage/rd02.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 120
ny = 1
xmin = 0
xmax = 6
ymin = 0
ymax = 0.05
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Functions]
[dts]
type = PiecewiseLinear
y = '1E-2 1 10 500 5000 50000'
x = '0 10 100 1000 10000 500000'
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = pressure
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureVG
m = 0.336
alpha = 1.43e-4
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 2e7
viscosity = 1.01e-3
density0 = 1000
thermal_expansion = 0
[]
[]
[]
[Materials]
[massfrac]
type = PorousFlowMassFraction
[]
[temperature]
type = PorousFlowTemperature
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pressure
capillary_pressure = pc
[]
[relperm]
type = PorousFlowRelativePermeabilityVG
m = 0.336
seff_turnover = 0.99
phase = 0
[]
[porosity]
type = PorousFlowPorosityConst
porosity = 0.33
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '0.295E-12 0 0 0 0.295E-12 0 0 0 0.295E-12'
[]
[]
[Variables]
[pressure]
initial_condition = 0.0
[]
[]
[Kernels]
[mass0]
type = PorousFlowMassTimeDerivative
fluid_component = 0
variable = pressure
[]
[flux0]
type = PorousFlowAdvectiveFlux
fluid_component = 0
variable = pressure
gravity = '-10 0 0'
[]
[]
[AuxVariables]
[SWater]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[SWater]
type = MaterialStdVectorAux
property = PorousFlow_saturation_qp
index = 0
variable = SWater
[]
[]
[BCs]
[base]
type = DirichletBC
boundary = left
value = 0.0
variable = pressure
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
petsc_options = '-snes_converged_reason -ksp_diagonal_scale -ksp_diagonal_scale_fix -ksp_gmres_modifiedgramschmidt -snes_linesearch_monitor'
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -sub_pc_factor_shift_type -pc_asm_overlap -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'gmres asm lu NONZERO 2 1E-10 1E-10 10'
[]
[]
[VectorPostprocessors]
[swater]
type = LineValueSampler
variable = SWater
start_point = '0 0 0'
end_point = '6 0 0'
sort_by = x
num_points = 121
execute_on = timestep_end
[]
[]
[Executioner]
type = Transient
solve_type = Newton
petsc_options = '-snes_converged_reason'
end_time = 345600
[TimeStepper]
type = FunctionDT
function = dts
[]
[]
[Outputs]
file_base = rd02
[exodus]
type = Exodus
execute_on = 'initial final'
[]
[along_line]
type = CSV
execute_on = final
[]
[]
(modules/tensor_mechanics/test/tests/dynamics/time_integration/hht_test.i)
# Test for HHT time integration
# The test is for an 1D bar element of unit length fixed on one end
# with a ramped pressure boundary condition applied to the other end.
# alpha, beta and gamma are HHT time integration parameters
# The equation of motion in terms of matrices is:
#
# M*accel + alpha*(K*disp - K*disp_old) + K*disp = P(t+alpha dt)*Area
#
# Here M is the mass matrix, K is the stiffness matrix, P is the applied pressure
#
# This equation is equivalent to:
#
# density*accel + alpha*(Div stress - Div stress_old) +Div Stress= P(t+alpha dt)
#
# The first term on the left is evaluated using the Inertial force kernel
# The next two terms on the left involving alpha are evaluated using the
# DynamicStressDivergenceTensors Kernel
# The residual due to Pressure is evaluated using Pressure boundary condition
#
# The system will come to steady state slowly after the pressure becomes constant.
# Alpha equal to zero will result in Newmark integration.
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = 0.0
xmax = 0.1
ymin = 0.0
ymax = 1.0
zmin = 0.0
zmax = 0.1
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./vel_x]
[../]
[./accel_x]
[../]
[./vel_y]
[../]
[./accel_y]
[../]
[./vel_z]
[../]
[./accel_z]
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./DynamicTensorMechanics]
displacements = 'disp_x disp_y disp_z'
alpha = 0.11
[../]
[./inertia_x]
type = InertialForce
variable = disp_x
velocity = vel_x
acceleration = accel_x
beta = 0.25
gamma = 0.5
[../]
[./inertia_y]
type = InertialForce
variable = disp_y
velocity = vel_y
acceleration = accel_y
beta = 0.25
gamma = 0.5
[../]
[./inertia_z]
type = InertialForce
variable = disp_z
velocity = vel_z
acceleration = accel_z
beta = 0.25
gamma = 0.5
[../]
[]
[AuxKernels]
[./accel_x]
type = NewmarkAccelAux
variable = accel_x
displacement = disp_x
velocity = vel_x
beta = 0.25
execute_on = timestep_end
[../]
[./vel_x]
type = NewmarkVelAux
variable = vel_x
acceleration = accel_x
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_y]
type = NewmarkAccelAux
variable = accel_y
displacement = disp_y
velocity = vel_y
beta = 0.25
execute_on = timestep_end
[../]
[./vel_y]
type = NewmarkVelAux
variable = vel_y
acceleration = accel_y
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_z]
type = NewmarkAccelAux
variable = accel_z
displacement = disp_z
velocity = vel_z
beta = 0.25
execute_on = timestep_end
[../]
[./vel_z]
type = NewmarkVelAux
variable = vel_z
acceleration = accel_z
gamma = 0.5
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 0
index_j = 1
[../]
[./strain_yy]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_yy
index_i = 0
index_j = 1
[../]
[]
[BCs]
[./top_y]
type = DirichletBC
variable = disp_y
boundary = top
value=0.0
[../]
[./top_x]
type = DirichletBC
variable = disp_x
boundary = top
value=0.0
[../]
[./top_z]
type = DirichletBC
variable = disp_z
boundary = top
value=0.0
[../]
[./bottom_x]
type = DirichletBC
variable = disp_x
boundary = bottom
value=0.0
[../]
[./bottom_z]
type = DirichletBC
variable = disp_z
boundary = bottom
value=0.0
[../]
[./Pressure]
[./Side1]
boundary = bottom
function = pressure
factor = 1
alpha = 0.11
displacements = 'disp_x disp_y disp_z'
[../]
[../]
[]
[Materials]
[./Elasticity_tensor]
type = ComputeElasticityTensor
block = 0
fill_method = symmetric_isotropic
C_ijkl = '210e9 0'
[../]
[./strain]
type = ComputeSmallStrain
block = 0
displacements = 'disp_x disp_y disp_z'
[../]
[./stress]
type = ComputeLinearElasticStress
block = 0
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = 'density'
prop_values = '7750'
[../]
[]
[Executioner]
type = Transient
start_time = 0
end_time = 2
dt = 0.1
[]
[Functions]
[./pressure]
type = PiecewiseLinear
x = '0.0 0.1 0.2 1.0 2.0 5.0'
y = '0.0 0.1 0.2 1.0 1.0 1.0'
scale_factor = 1e9
[../]
[]
[Postprocessors]
[./_dt]
type = TimestepSize
[../]
[./disp]
type = NodalMaxValue
variable = disp_y
boundary = bottom
[../]
[./vel]
type = NodalMaxValue
variable = vel_y
boundary = bottom
[../]
[./accel]
type = NodalMaxValue
variable = accel_y
boundary = bottom
[../]
[./stress_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./strain_yy]
type = ElementAverageValue
variable = strain_yy
[../]
[]
[Outputs]
exodus = true
perf_graph = true
[]
(modules/tensor_mechanics/test/tests/central_difference/lumped/3D/3d_nodalmass_implicit.i)
# Test for the Newmark-Beta time integrator
[Mesh]
[./generated_mesh]
type = GeneratedMeshGenerator
dim = 3
nx = 1
ny = 1
nz = 2
xmin = 0.0
xmax = 1
ymin = 0.0
ymax = 1
zmin = 0.0
zmax = 2
[../]
[./all_nodes]
type = BoundingBoxNodeSetGenerator
new_boundary = 'all'
input = 'generated_mesh'
top_right = '1 1 2'
bottom_left = '0 0 0'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./vel_x]
[../]
[./accel_x]
[../]
[./vel_y]
[../]
[./accel_y]
[../]
[./vel_z]
[../]
[./accel_z]
[../]
[]
[Kernels]
[./DynamicTensorMechanics]
displacements = 'disp_x disp_y disp_z'
[../]
[]
[AuxKernels]
[./accel_x]
type = TestNewmarkTI
variable = accel_x
displacement = disp_x
first = false
[../]
[./vel_x]
type = TestNewmarkTI
variable = vel_x
displacement = disp_x
[../]
[./accel_y]
type = TestNewmarkTI
variable = accel_y
displacement = disp_y
first = false
[../]
[./vel_y]
type = TestNewmarkTI
variable = vel_y
displacement = disp_y
[../]
[./accel_z]
type = TestNewmarkTI
variable = accel_z
displacement = disp_z
first = false
[../]
[./vel_z]
type = TestNewmarkTI
variable = vel_z
displacement = disp_z
[../]
[]
[BCs]
[./x_bot]
type = PresetDisplacement
boundary = 'back'
variable = disp_x
beta = 0.25
velocity = vel_x
acceleration = accel_x
function = dispx
[../]
[./y_bot]
type = PresetDisplacement
boundary = 'back'
variable = disp_y
beta = 0.25
velocity = vel_y
acceleration = accel_y
function = dispy
[../]
[./z_bot]
type = PresetDisplacement
boundary = 'back'
variable = disp_z
beta = 0.25
velocity = vel_z
acceleration = accel_z
function = dispz
[../]
[]
[Functions]
[./dispx]
type = PiecewiseLinear
x = '0.0 1.0 2.0 3.0 4.0' # time
y = '0.0 1.0 0.0 -1.0 0.0' # displacement
[../]
[./dispy]
type = ParsedFunction
value = 0.1*t*t*sin(10*t)
[../]
[./dispz]
type = ParsedFunction
value = 0.1*t*t*sin(20*t)
[../]
[]
[NodalKernels]
[./nodal_mass_x]
type = NodalTranslationalInertia
boundary = 'all'
nodal_mass_file = 'nodal_mass_file.csv'
variable = 'disp_x'
[../]
[./nodal_mass_y]
type = NodalTranslationalInertia
boundary = 'all'
nodal_mass_file = 'nodal_mass_file.csv'
variable = 'disp_y'
[../]
[./nodal_mass_z]
type = NodalTranslationalInertia
boundary = 'all'
nodal_mass_file = 'nodal_mass_file.csv'
variable = 'disp_z'
[../]
[]
[Materials]
[./elasticity_tensor_block]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.25
block = 0
[../]
[./strain_block]
type = ComputeIncrementalSmallStrain
block = 0
displacements = 'disp_x disp_y disp_z'
[../]
[./stress_block]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
nl_abs_tol = 1e-08
nl_rel_tol = 1e-08
timestep_tolerance = 1e-6
start_time = -0.01
end_time = 0.1
dt = 0.005
[./TimeIntegrator]
type = NewmarkBeta
beta = 0.25
gamma = 0.5
[../]
[]
[Postprocessors]
[./accel_10x]
type = NodalVariableValue
nodeid = 10
variable = accel_x
[../]
[]
[Outputs]
exodus = false
csv = true
[]
(modules/porous_flow/test/tests/infiltration_and_drainage/bw01.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 400
ny = 1
xmin = -10
xmax = 10
ymin = 0
ymax = 0.05
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Functions]
[dts]
type = PiecewiseLinear
y = '1E-5 1E-2 1E-2 1E-1'
x = '0 1E-5 1 10'
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = pressure
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureBW
Sn = 0.0
Ss = 1.0
C = 1.5
las = 2
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 2e9
viscosity = 4
density0 = 10
thermal_expansion = 0
[]
[]
[]
[Materials]
[massfrac]
type = PorousFlowMassFraction
[]
[temperature]
type = PorousFlowTemperature
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pressure
capillary_pressure = pc
[]
[relperm]
type = PorousFlowRelativePermeabilityBW
Sn = 0.0
Ss = 1.0
Kn = 0
Ks = 1
C = 1.5
phase = 0
[]
[porosity]
type = PorousFlowPorosityConst
porosity = 0.25
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1 0 0 0 1 0 0 0 1'
[]
[]
[Variables]
[pressure]
initial_condition = -9E2
[]
[]
[Kernels]
[mass0]
type = PorousFlowMassTimeDerivative
fluid_component = 0
variable = pressure
[]
[flux0]
type = PorousFlowAdvectiveFlux
fluid_component = 0
variable = pressure
gravity = '-0.1 0 0'
[]
[]
[AuxVariables]
[SWater]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[SWater]
type = MaterialStdVectorAux
property = PorousFlow_saturation_qp
index = 0
variable = SWater
[]
[]
[BCs]
[recharge]
type = PorousFlowSink
variable = pressure
boundary = right
flux_function = -1.25 # corresponds to Rstar being 0.5 because i have to multiply by density*porosity
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
petsc_options = '-snes_converged_reason -ksp_diagonal_scale -ksp_diagonal_scale_fix -ksp_gmres_modifiedgramschmidt -snes_linesearch_monitor'
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -sub_pc_factor_shift_type -pc_asm_overlap -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'gmres asm lu NONZERO 2 1E-10 1E-10 10000'
[]
[]
[VectorPostprocessors]
[swater]
type = LineValueSampler
variable = SWater
start_point = '-10 0 0'
end_point = '10 0 0'
sort_by = x
num_points = 101
execute_on = timestep_end
[]
[]
[Executioner]
type = Transient
solve_type = Newton
petsc_options = '-snes_converged_reason'
end_time = 8
[TimeStepper]
type = FunctionDT
function = dts
[]
[]
[Outputs]
file_base = bw01
sync_times = '0.5 2 8'
[exodus]
type = Exodus
sync_only = true
[]
[along_line]
type = CSV
sync_only = true
[]
[]
(modules/tensor_mechanics/test/tests/ad_smeared_cracking/cracking_multiple_softening.i)
# Test of cracking with direction-specific release models in 3
# directions. Block is first pulled in one direction, and then
# held while it is sequentially pulled in the other two
# directions. Poisson's ratio is zero so that the cracking in one
# direction doesn't affect the others.
# Softening in the three directions should follow the laws for the
# prescribed models in the three directions, which are power law (x),
# exponential (y), and abrupt (z).
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Functions]
[./displx]
type = PiecewiseLinear
x = '0 1 2 3'
y = '0 1 1 1'
[../]
[./disply]
type = PiecewiseLinear
x = '0 1 2 3'
y = '0 0 1 1'
[../]
[./displz]
type = PiecewiseLinear
x = '0 1 2 3'
y = '0 0 0 1'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx'
use_automatic_differentiation = true
[../]
[]
[BCs]
[./pullx]
type = ADFunctionDirichletBC
variable = disp_x
boundary = right
function = displx
[../]
[./pully]
type = ADFunctionDirichletBC
variable = disp_y
boundary = top
function = disply
[../]
[./pullz]
type = ADFunctionDirichletBC
variable = disp_z
boundary = front
function = displz
[../]
[./left]
type = ADDirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./bottom]
type = ADDirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./back]
type = ADDirichletBC
variable = disp_z
boundary = back
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 2.8e7
poissons_ratio = 0
[../]
[./elastic_stress]
type = ADComputeSmearedCrackingStress
cracking_stress = 1.68e6
softening_models = 'power_law_softening exponential_softening abrupt_softening'
prescribed_crack_directions = 'x y z'
[../]
[./power_law_softening]
type = ADPowerLawSoftening
stiffness_reduction = 0.3333
[../]
[./exponential_softening]
type = ADExponentialSoftening
[../]
[./abrupt_softening]
type = ADAbruptSoftening
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
petsc_options_iname = '-ksp_gmres_restart -pc_type -sub_pc_type'
petsc_options_value = '101 asm lu'
line_search = 'none'
l_max_its = 100
nl_max_its = 100
nl_rel_tol = 1e-8
nl_abs_tol = 1e-8
l_tol = 1e-5
start_time = 0.0
end_time = 3.0
dt = 0.01
[]
[Outputs]
exodus = true
[]
(modules/combined/test/tests/thermal_conductivity_temperature_function_test/thermal_conductivity_temperature_function_test.i)
#
# This test evaluates the capability of HeatConductionMaterial to define
# thermal conductivity as a function of temperature. The test uses the patch test
# cube mesh with a flux bc on one side and a temperature bc on the opposite side.
# The temperature bc changes as a function of time from 100 to 200. The thermal
# conductivity is a function of temperature, with k = 1 for temps = 100-199, k = 2
# for temps _>_ 200. The flux, q = 10 is constant. The Transient Executioner is used here
# although the interial kernel is omitted, so this is really a series of two steady-state
# solutions.
#
# ---------------
# | |
# | |
# q -> | k | T2
# | |
# T1 = ? | |
# ---------------
# dx = 1
#
#
# q = -k dT/dx
#
# q = -k (T1 - T2)/dx
#
# T1 = (q/-k)*dx + T2
#
# for: T2 = 100, k = 1, q = -10
#
# T1 = 110
# --------
#
# for: T2 = 200, k = 2, q = -10
#
# T1 = 205
# --------
#
[Mesh]#Comment
file = fe_patch.e
[] # Mesh
[Functions]
[./k_func]
type = PiecewiseLinear
x = '100 199 200'
y = '1 1 2'
[../]
[./c_func]
type = PiecewiseLinear
x = '100 200'
y = '0.116 0.116'
[../]
[./t_func]
type = PiecewiseLinear
x = '0 1 2'
y = '100 100 200'
[../]
[] # Functions
[Variables]
[./temp]
order = FIRST
family = LAGRANGE
initial_condition = 100
[../]
[] # Variables
[Kernels]
[./heat_r]
type = HeatConduction
variable = temp
[../]
[] # Kernels
[BCs]
[./temps_function]
type = FunctionDirichletBC
variable = temp
boundary = 1000
function = t_func
[../]
[./flux_in]
type = NeumannBC
variable = temp
boundary = 100
value = 10
[../]
[] # BCs
[Materials]
[./heat]
type = HeatConductionMaterial
block = 1
temp = temp
thermal_conductivity_temperature_function = k_func
specific_heat_temperature_function = c_func
[../]
[./density]
type = Density
block = 1
density = 0.283
[../]
[] # Materials
[Executioner]
type = Transient
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -ksp_gmres_restart'
petsc_options_value = 'lu 101'
line_search = 'none'
l_max_its = 100
l_tol = 8e-3
nl_max_its = 15
nl_rel_tol = 1e-4
nl_abs_tol = 1e-10
start_time = 0.0
dt = 1
end_time = 2
num_steps = 2
[] # Executioner
[Outputs]
file_base = out
exodus = true
[] # Outputs
(modules/tensor_mechanics/test/tests/ad_anisotropic_creep/ad_aniso_iso_creep_x_3d.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
nx = 10
ny = 2
nz = 2
xmin = 0.0
ymin = 0.0
zmin = 0.0
xmax = 10.0
ymax = 1.0
zmax = 1.0
[]
[corner_node]
type = ExtraNodesetGenerator
new_boundary = '100'
nodes = '3 69'
input = gen
[]
[corner_node_2]
type = ExtraNodesetGenerator
new_boundary = '101'
nodes = '4 47'
input = corner_node
[]
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[AuxVariables]
[hydrostatic_stress]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_xx]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_xy]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_yy]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_zz]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_xz]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_yz]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[hydrostatic_stress]
type = ADRankTwoScalarAux
variable = hydrostatic_stress
rank_two_tensor = stress
scalar_type = Hydrostatic
[]
[creep_strain_xx]
type = ADRankTwoAux
rank_two_tensor = creep_strain
variable = creep_strain_xx
index_i = 0
index_j = 0
[]
[creep_strain_xy]
type = ADRankTwoAux
rank_two_tensor = creep_strain
variable = creep_strain_xy
index_i = 0
index_j = 1
[]
[creep_strain_yy]
type = ADRankTwoAux
rank_two_tensor = creep_strain
variable = creep_strain_yy
index_i = 1
index_j = 1
[]
[creep_strain_zz]
type = ADRankTwoAux
rank_two_tensor = creep_strain
variable = creep_strain_zz
index_i = 2
index_j = 2
[]
[creep_strain_xz]
type = ADRankTwoAux
rank_two_tensor = creep_strain
variable = creep_strain_xz
index_i = 0
index_j = 2
[]
[creep_strain_yz]
type = ADRankTwoAux
rank_two_tensor = creep_strain
variable = creep_strain_yz
index_i = 1
index_j = 2
[]
[sigma_xx]
type = ADRankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 1
index_j = 1
[]
[]
[Functions]
[pull]
type = PiecewiseLinear
x = '0 1.0e-9 1.0'
y = '0 -4e1 -4e1'
[]
[]
[Modules/TensorMechanics/Master]
[all]
strain = FINITE
generate_output = 'elastic_strain_xx stress_xx'
use_automatic_differentiation = true
add_variables = true
[]
[]
[Materials]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 700
poissons_ratio = 0.0
[]
[elastic_strain]
type = ADComputeMultipleInelasticStress
# inelastic_models = 'trial_creep_iso'
max_iterations = 50
[]
[trial_creep_aniso_iso]
type = ADHillCreepStressUpdate
coefficient = 1e-16
n_exponent = 9
m_exponent = 0
activation_energy = 0
# F G H L M N
hill_constants = "0.5 0.5 0.5 1.5 1.5 1.5"
max_inelastic_increment = 0.00003
relative_tolerance = 1e-20
absolute_tolerance = 1e-20
internal_solve_output_on = never
# Force it to not use integration error
max_integration_error = 1.0
[]
[trial_creep_iso]
type = ADPowerLawCreepStressUpdate
coefficient = 1e-16
n_exponent = 9
m_exponent = 0
activation_energy = 0
# F G H L M N
max_inelastic_increment = 0.00003
relative_tolerance = 1e-16
absolute_tolerance = 1e-16
internal_solve_output_on = never
[]
[]
[BCs]
[no_disp_x]
type = ADDirichletBC
variable = disp_x
boundary = left
value = 0.0
[]
[no_disp_y]
type = ADDirichletBC
variable = disp_y
boundary = 100
value = 0.0
[]
[no_disp_z]
type = ADDirichletBC
variable = disp_z
boundary = 101
value = 0.0
[]
[Pressure]
[Side1]
boundary = right
function = pull
[]
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
nl_rel_tol = 1e-13
nl_abs_tol = 1.0e-14
l_max_its = 90
num_steps = 10
dt = 5.0e-4
start_time = 0
automatic_scaling = true
[]
[Postprocessors]
[matl_ts_min]
type = MaterialTimeStepPostprocessor
[]
[max_disp_x]
type = ElementExtremeValue
variable = disp_x
[]
[max_disp_y]
type = ElementExtremeValue
variable = disp_y
[]
[max_hydro]
type = ElementAverageValue
variable = hydrostatic_stress
[]
[dt]
type = TimestepSize
[]
[num_lin]
type = NumLinearIterations
outputs = console
[]
[num_nonlin]
type = NumNonlinearIterations
outputs = console
[]
[creep_strain_xx]
type = ElementalVariableValue
variable = creep_strain_xx
execute_on = 'TIMESTEP_END'
elementid = 39
[]
[creep_strain_yy]
type = ElementalVariableValue
variable = creep_strain_yy
execute_on = 'TIMESTEP_END'
elementid = 39
[]
[creep_strain_zz]
type = ElementalVariableValue
variable = creep_strain_zz
execute_on = 'TIMESTEP_END'
elementid = 39
[]
[creep_strain_xy]
type = ElementalVariableValue
variable = creep_strain_xy
execute_on = 'TIMESTEP_END'
elementid = 39
[]
[creep_strain_yz]
type = ElementalVariableValue
variable = creep_strain_yz
execute_on = 'TIMESTEP_END'
elementid = 39
[]
[creep_strain_xz]
type = ElementalVariableValue
variable = creep_strain_xz
execute_on = 'TIMESTEP_END'
elementid = 39
[]
[elastic_strain_xx]
type = ElementalVariableValue
variable = elastic_strain_xx
execute_on = 'TIMESTEP_END'
elementid = 39
[]
[sigma_xx]
type = ElementalVariableValue
variable = stress_xx
execute_on = 'TIMESTEP_END'
elementid = 39
[]
[]
[Outputs]
csv = true
exodus = true
perf_graph = true
[]
(modules/tensor_mechanics/test/tests/ad_viscoplasticity_stress_update/negative_porosity.i)
# This test provides an example of an individual LPS viscoplasticity model
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
xmax = 0.002
ymax = 0.002
[]
[Modules/TensorMechanics/Master/All]
strain = FINITE
add_variables = true
generate_output = 'strain_xx strain_yy strain_xy hydrostatic_stress vonmises_stress'
use_automatic_differentiation = true
[]
[Functions]
[./pull]
type = PiecewiseLinear
x = '0 0.1'
y = '0 1e-5'
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1e10
poissons_ratio = 0.3
[../]
[./stress]
type = ADComputeMultipleInelasticStress
inelastic_models = lps
outputs = all
[../]
[./porosity]
type = ADGenericConstantMaterial
prop_names = 'porosity'
prop_values = '-0.1'
outputs = 'all'
[../]
[./lps]
type = ADViscoplasticityStressUpdate
coefficient = 'coef'
power = 3
outputs = all
relative_tolerance = 1e-11
initial_porosity = 0.1
negative_behavior = ZERO
[../]
[./coef]
type = ADParsedMaterial
f_name = coef
# Example of creep power law
function = '1e-18 * exp(-4e4 / 1.987 / 1200)'
[../]
[]
[BCs]
[./no_disp_x]
type = ADDirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./no_disp_y]
type = ADDirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./pull_disp_y]
type = ADFunctionDirichletBC
variable = disp_y
boundary = top
function = pull
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
dt = 0.01
end_time = 0.12
[]
[Postprocessors]
[./disp_x]
type = SideAverageValue
variable = disp_x
boundary = right
[../]
[./disp_y]
type = SideAverageValue
variable = disp_y
boundary = top
[../]
[./avg_hydro]
type = ElementAverageValue
variable = hydrostatic_stress
[../]
[./avg_vonmises]
type = ElementAverageValue
variable = vonmises_stress
[../]
[./dt]
type = TimestepSize
[../]
[./num_lin]
type = NumLinearIterations
outputs = console
[../]
[./num_nonlin]
type = NumNonlinearIterations
outputs = console
[../]
[./eff_creep_strain]
type = ElementAverageValue
variable = effective_viscoplasticity
[../]
[./porosity]
type = ElementAverageValue
variable = porosity
[../]
[]
[Outputs]
csv = true
[]
(modules/tensor_mechanics/test/tests/beam/dynamic/dyn_euler_small_rayleigh_hht_ti.i)
# Test for damped small strain euler beam vibration in y direction
# An impulse load is applied at the end of a cantilever beam of length 4m.
# The properties of the cantilever beam are as follows:
# Young's modulus (E) = 1e4
# Shear modulus (G) = 4e7
# Shear coefficient (k) = 1.0
# Cross-section area (A) = 0.01
# Iy = 1e-4 = Iz
# Length (L)= 4 m
# density (rho) = 1.0
# mass proportional rayleigh damping(eta) = 0.1
# stiffness proportional rayleigh damping(eta) = 0.1
# HHT time integration parameter (alpha) = -0.3
# Corresponding Newmark beta time integration parameters beta = 0.4225 and gamma = 0.8
# For this beam, the dimensionless parameter alpha = kAGL^2/EI = 6.4e6
# Therefore, the behaves like a Euler-Bernoulli beam.
# The displacement time history from this analysis matches with that obtained from Abaqus.
# Values from the first few time steps are as follows:
# time disp_y vel_y accel_y
# 0.0 0.0 0.0 0.0
# 0.2 0.019898364318588 0.18838688112273 1.1774180070171
# 0.4 0.045577003505278 0.087329917525455 -0.92596052423724
# 0.6 0.063767907208218 0.084330765885995 0.21274543331268
# 0.8 0.073602908614573 0.020029576220975 -0.45506879373455
# 1.0 0.06841704414745 -0.071840076837194 -0.46041813317992
[Mesh]
type = GeneratedMesh
nx = 10
dim = 1
xmin = 0.0
xmax = 4.0
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[./rot_x]
order = FIRST
family = LAGRANGE
[../]
[./rot_y]
order = FIRST
family = LAGRANGE
[../]
[./rot_z]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./vel_x]
order = FIRST
family = LAGRANGE
[../]
[./vel_y]
order = FIRST
family = LAGRANGE
[../]
[./vel_z]
order = FIRST
family = LAGRANGE
[../]
[./accel_x]
order = FIRST
family = LAGRANGE
[../]
[./accel_y]
order = FIRST
family = LAGRANGE
[../]
[./accel_z]
order = FIRST
family = LAGRANGE
[../]
[./rot_vel_x]
order = FIRST
family = LAGRANGE
[../]
[./rot_vel_y]
order = FIRST
family = LAGRANGE
[../]
[./rot_vel_z]
order = FIRST
family = LAGRANGE
[../]
[./rot_accel_x]
order = FIRST
family = LAGRANGE
[../]
[./rot_accel_y]
order = FIRST
family = LAGRANGE
[../]
[./rot_accel_z]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./accel_x] # These auxkernels are only to check output
type = TestNewmarkTI
displacement = disp_x
variable = accel_x
first = false
[../]
[./accel_y]
type = TestNewmarkTI
displacement = disp_y
variable = accel_y
first = false
[../]
[./accel_z]
type = TestNewmarkTI
displacement = disp_z
variable = accel_z
first = false
[../]
[./vel_x]
type = TestNewmarkTI
displacement = disp_x
variable = vel_x
[../]
[./vel_y]
type = TestNewmarkTI
displacement = disp_y
variable = vel_y
[../]
[./vel_z]
type = TestNewmarkTI
displacement = disp_z
variable = vel_z
[../]
[./rot_accel_x]
type = TestNewmarkTI
displacement = rot_x
variable = rot_accel_x
first = false
[../]
[./rot_accel_y]
type = TestNewmarkTI
displacement = rot_y
variable = rot_accel_y
first = false
[../]
[./rot_accel_z]
type = TestNewmarkTI
displacement = rot_z
variable = rot_accel_z
first = false
[../]
[./rot_vel_x]
type = TestNewmarkTI
displacement = rot_x
variable = rot_vel_x
[../]
[./rot_vel_y]
type = TestNewmarkTI
displacement = rot_y
variable = rot_vel_y
[../]
[./rot_vel_z]
type = TestNewmarkTI
displacement = rot_z
variable = rot_vel_z
[../]
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./fixy1]
type = DirichletBC
variable = disp_y
boundary = left
value = 0.0
[../]
[./fixz1]
type = DirichletBC
variable = disp_z
boundary = left
value = 0.0
[../]
[./fixr1]
type = DirichletBC
variable = rot_x
boundary = left
value = 0.0
[../]
[./fixr2]
type = DirichletBC
variable = rot_y
boundary = left
value = 0.0
[../]
[./fixr3]
type = DirichletBC
variable = rot_z
boundary = left
value = 0.0
[../]
[]
[NodalKernels]
[./force_y2]
type = UserForcingFunctionNodalKernel
variable = disp_y
boundary = right
function = force
[../]
[]
[Functions]
[./force]
type = PiecewiseLinear
x = '0.0 0.2 0.4 10.0'
y = '0.0 0.01 0.0 0.0'
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
line_search = 'none'
l_tol = 1e-11
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 0.2
end_time = 5.0
timestep_tolerance = 1e-6
# Time integrator
[./TimeIntegrator]
type = NewmarkBeta
beta = 0.4225
gamma = 0.8
[../]
[]
[Kernels]
[./solid_disp_x]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 0
variable = disp_x
zeta = 0.1
alpha = -0.3
[../]
[./solid_disp_y]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 1
variable = disp_y
zeta = 0.1
alpha = -0.3
[../]
[./solid_disp_z]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 2
variable = disp_z
zeta = 0.1
alpha = -0.3
[../]
[./solid_rot_x]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 3
variable = rot_x
zeta = 0.1
alpha = -0.3
[../]
[./solid_rot_y]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 4
variable = rot_y
zeta = 0.1
alpha = -0.3
[../]
[./solid_rot_z]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 5
variable = rot_z
zeta = 0.1
alpha = -0.3
[../]
[./inertial_force_x]
type = InertialForceBeam
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
eta = 0.1
area = 0.01
Iy = 1e-4
Iz = 1e-4
Ay = 0.0
Az = 0.0
component = 0
variable = disp_x
alpha = -0.3
[../]
[./inertial_force_y]
type = InertialForceBeam
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
eta = 0.1
area = 0.01
Iy = 1e-4
Iz = 1e-4
Ay = 0.0
Az = 0.0
component = 1
variable = disp_y
alpha = -0.3
[../]
[./inertial_force_z]
type = InertialForceBeam
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
eta = 0.1
area = 0.01
Iy = 1e-4
Iz = 1e-4
Ay = 0.0
Az = 0.0
component = 2
variable = disp_z
alpha = -0.3
[../]
[./inertial_force_rot_x]
type = InertialForceBeam
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
eta = 0.1
area = 0.01
Iy = 1e-4
Iz = 1e-4
Ay = 0.0
Az = 0.0
component = 3
variable = rot_x
alpha = -0.3
[../]
[./inertial_force_rot_y]
type = InertialForceBeam
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
eta = 0.1
area = 0.01
Iy = 1e-4
Iz = 1e-4
Ay = 0.0
Az = 0.0
component = 4
variable = rot_y
alpha = -0.3
[../]
[./inertial_force_rot_z]
type = InertialForceBeam
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
eta = 0.1
area = 0.01
Iy = 1e-4
Iz = 1e-4
Ay = 0.0
Az = 0.0
component = 5
variable = rot_z
alpha = -0.3
[../]
[]
[Materials]
[./elasticity]
type = ComputeElasticityBeam
youngs_modulus = 1.0e4
poissons_ratio = -0.999875
shear_coefficient = 1.0
block = 0
[../]
[./strain]
type = ComputeIncrementalBeamStrain
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
area = 0.01
Ay = 0.0
Az = 0.0
Iy = 1.0e-4
Iz = 1.0e-4
y_orientation = '0.0 1.0 0.0'
[../]
[./stress]
type = ComputeBeamResultants
block = 0
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = 'density'
prop_values = '1.0'
[../]
[]
[Postprocessors]
[./disp_x]
type = PointValue
point = '4.0 0.0 0.0'
variable = disp_x
[../]
[./disp_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = disp_y
[../]
[./vel_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = vel_y
[../]
[./accel_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = accel_y
[../]
[]
[Outputs]
file_base = 'dyn_euler_small_rayleigh_hht_out'
exodus = true
csv = true
perf_graph = true
[]
(modules/tensor_mechanics/test/tests/dynamics/time_integration/hht_test_ti.i)
# Test for HHT time integration
# The test is for an 1D bar element of unit length fixed on one end
# with a ramped pressure boundary condition applied to the other end.
# alpha, beta and gamma are HHT time integration parameters
# The equation of motion in terms of matrices is:
#
# M*accel + alpha*(K*disp - K*disp_old) + K*disp = P(t+alpha dt)*Area
#
# Here M is the mass matrix, K is the stiffness matrix, P is the applied pressure
#
# This equation is equivalent to:
#
# density*accel + alpha*(Div stress - Div stress_old) +Div Stress= P(t+alpha dt)
#
# The first term on the left is evaluated using the Inertial force kernel
# The next two terms on the left involving alpha are evaluated using the
# DynamicStressDivergenceTensors Kernel
# The residual due to Pressure is evaluated using Pressure boundary condition
#
# The system will come to steady state slowly after the pressure becomes constant.
# Alpha equal to zero will result in Newmark integration.
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = 0.0
xmax = 0.1
ymin = 0.0
ymax = 1.0
zmin = 0.0
zmax = 0.1
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./vel_x]
[../]
[./accel_x]
[../]
[./vel_y]
[../]
[./accel_y]
[../]
[./vel_z]
[../]
[./accel_z]
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./DynamicTensorMechanics]
displacements = 'disp_x disp_y disp_z'
alpha = 0.11
[../]
[./inertia_x]
type = InertialForce
variable = disp_x
[../]
[./inertia_y]
type = InertialForce
variable = disp_y
[../]
[./inertia_z]
type = InertialForce
variable = disp_z
[../]
[]
[AuxKernels]
[./accel_x] # These auxkernls are only for checking output
type = TestNewmarkTI
displacement = disp_x
variable = accel_x
first = false
[../]
[./accel_y]
type = TestNewmarkTI
displacement = disp_y
variable = accel_y
first = false
[../]
[./accel_z]
type = TestNewmarkTI
displacement = disp_z
variable = accel_z
first = false
[../]
[./vel_x]
type = TestNewmarkTI
displacement = disp_x
variable = vel_x
[../]
[./vel_y]
type = TestNewmarkTI
displacement = disp_y
variable = vel_y
[../]
[./vel_z]
type = TestNewmarkTI
displacement = disp_z
variable = vel_z
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 0
index_j = 1
[../]
[./strain_yy]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_yy
index_i = 0
index_j = 1
[../]
[]
[BCs]
[./top_y]
type = DirichletBC
variable = disp_y
boundary = top
value=0.0
[../]
[./top_x]
type = DirichletBC
variable = disp_x
boundary = top
value=0.0
[../]
[./top_z]
type = DirichletBC
variable = disp_z
boundary = top
value=0.0
[../]
[./bottom_x]
type = DirichletBC
variable = disp_x
boundary = bottom
value=0.0
[../]
[./bottom_z]
type = DirichletBC
variable = disp_z
boundary = bottom
value=0.0
[../]
[./Pressure]
[./Side1]
boundary = bottom
function = pressure
displacements = 'disp_x disp_y disp_z'
factor = 1
alpha = 0.11
[../]
[../]
[]
[Materials]
[./Elasticity_tensor]
type = ComputeElasticityTensor
block = 0
fill_method = symmetric_isotropic
C_ijkl = '210e9 0'
[../]
[./strain]
type = ComputeSmallStrain
block = 0
displacements = 'disp_x disp_y disp_z'
[../]
[./stress]
type = ComputeLinearElasticStress
block = 0
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = 'density'
prop_values = '7750'
[../]
[]
[Executioner]
type = Transient
start_time = 0
end_time = 2
dt = 0.1
# Time integration scheme
scheme = 'newmark-beta'
[]
[Functions]
[./pressure]
type = PiecewiseLinear
x = '0.0 0.1 0.2 1.0 2.0 5.0'
y = '0.0 0.1 0.2 1.0 1.0 1.0'
scale_factor = 1e9
[../]
[]
[Postprocessors]
[./_dt]
type = TimestepSize
[../]
[./disp]
type = NodalMaxValue
variable = disp_y
boundary = bottom
[../]
[./vel]
type = NodalMaxValue
variable = vel_y
boundary = bottom
[../]
[./accel]
type = NodalMaxValue
variable = accel_y
boundary = bottom
[../]
[./stress_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./strain_yy]
type = ElementAverageValue
variable = strain_yy
[../]
[]
[Outputs]
file_base = 'hht_test_out'
exodus = true
perf_graph = true
[]
(modules/tensor_mechanics/test/tests/ad_smeared_cracking/cracking_plane_stress.i)
################################################################################
#
# 1x1x1 cube, single element
# simulate plane stress
# pull in +y direction on right surface to produce shear strain
#
#
#
# ____________
# /| /|
# / | 5 / | -X Left 1
# /__________ / | +X Right 4
# | | 3 | | +Y Top 5
# | 1 | | 4 | -Y Bottom 2
# | |_6_____|___| y +Z Front 6
# | / | / ^ -Z Back 3
# | / 2 | / |
# |/__________|/ |
# ----> x
# /
# /
# z
#
#
#
#################################################################################
[Mesh]
file = cube.e
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Functions]
[./displ]
type = PiecewiseLinear
x = '0 0.1 0.2 0.3 0.4'
y = '0 0.0026 0 -0.0026 0'
[../]
[./pressure]
type = PiecewiseLinear
x = '0 0.1 0.2 0.3 0.4'
y = '0 0 0 0 0'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx'
use_automatic_differentiation = true
[../]
[]
[BCs]
[./pull_y]
type = ADFunctionDirichletBC
variable = disp_y
boundary = 4
function = displ
[../]
[./pin_x]
type = ADDirichletBC
variable = disp_x
boundary = '1 4'
value = 0.0
[../]
[./pin_y]
type = ADDirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./back]
type = ADDirichletBC
variable = disp_z
boundary = '3'
value = 0.0
[../]
[./front]
type = ADPressure
variable = disp_z
component = 2
boundary = 6
function = pressure
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 200.0e3
poissons_ratio = .3
[../]
[./elastic_stress]
type = ADComputeSmearedCrackingStress
cracking_stress = 120
shear_retention_factor = 0.1
softening_models = exponential_softening
[../]
[./exponential_softening]
type = ADExponentialSoftening
residual_stress = 0.1
beta = 0.1
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
petsc_options_iname = '-ksp_gmres_restart -pc_type -sub_pc_type'
petsc_options_value = '101 asm lu'
line_search = 'none'
l_max_its = 100
nl_max_its = 100
nl_rel_tol = 1e-12
nl_abs_tol = 1e-8
l_tol = 1e-5
start_time = 0.0
end_time = 0.4
dt = 0.04
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/recompute_radial_return/isotropic_plasticity_finite_strain.i)
# This simulation uses the piece-wise linear strain hardening model
# with the incremental small strain formulation; incremental small strain
# is required to produce the strain_increment for the DiscreteRadialReturnStressIncrement
# class, which handles the calculation of the stress increment to return
# to the yield surface in a J2 (isotropic) plasticity problem.
#
# This test assumes a Poissons ratio of 0.3 and applies a displacement loading
# condition on the top in the y direction.
#
# An identical problem was run in Abaqus on a similar 1 element mesh and was used
# to verify the SolidMechanics solution; this TensorMechanics code matches the
# SolidMechanics solution.
#
# Mechanical strain is the sum of the elastic and plastic strains but is different
# from total strain in cases with eigen strains, e.g. thermal strain.
[Mesh]
file = 1x1x1cube.e
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Functions]
[./top_pull]
type = ParsedFunction
value = t*(0.0625)
[../]
[./hf]
type = PiecewiseLinear
x = '0 0.001 0.003 0.023'
y = '50 52 54 56'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_yy plastic_strain_xx plastic_strain_yy plastic_strain_zz'
[../]
[]
[BCs]
[./y_pull_function]
type = FunctionDirichletBC
variable = disp_y
boundary = 5
function = top_pull
[../]
[./x_bot]
type = DirichletBC
variable = disp_x
boundary = 4
value = 0.0
[../]
[./y_bot]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.0
[../]
[./z_bot]
type = DirichletBC
variable = disp_z
boundary = 2
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 2.1e5
poissons_ratio = 0.3
[../]
[./isotropic_plasticity]
type = IsotropicPlasticityStressUpdate
yield_stress = 50.0
hardening_function = hf
[../]
[./radial_return_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'isotropic_plasticity'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 50
nl_max_its = 50
nl_rel_tol = 1e-12
nl_abs_tol = 1e-10
l_tol = 1e-9
start_time = 0.0
end_time = 0.075
dt = 0.00125
dtmin = 0.0001
[]
[Outputs]
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[]
(modules/tensor_mechanics/test/tests/dynamics/prescribed_displacement/3D_QStatic_1_Ramped_Displacement_with_gravity.i)
# One 3D element under ramped displacement loading.
#
# loading in z direction:
# time : 0.0 0.1 0.2 0.3
# disp : 0.0 0.0 -0.01 -0.01
# Gravity is applied in y direction. To equilibrate the system
# under gravity, a static analysis is run in the first time step
# by turning off the inertial terms. (see controls block and
# DynamicTensorMechanics block).
# Result: The displacement at the top node in the z direction should match
# the prescribed displacement. Also, the z acceleration should
# be two triangular pulses, one peaking at 0.1 and another peaking at
# 0.2.
# The y displacement would be offset by the gravity displacement.
# Also the y acceleration and velocity should be zero until the loading in
# the z direction starts (i.e, until 0.1s)
# Note: The time step used in the displacement data file should match
# the simulation time step (dt and dtmin in the Executioner block).
[Mesh]
type = GeneratedMesh
dim = 3 # Dimension of the mesh
nx = 1 # Number of elements in the x direction
ny = 1 # Number of elements in the y direction
nz = 1 # Number of elements in the z direction
xmin = 0.0
xmax = 1
ymin = 0.0
ymax = 1
zmin = 0.0
zmax = 1
allow_renumbering = false # So NodalVariableValue can index by id
[]
[Variables] # variables that are solved
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables] # variables that are calculated for output
[./accel_x]
[../]
[./vel_x]
[../]
[./accel_y]
[../]
[./vel_y]
[../]
[./accel_z]
[../]
[./vel_z]
[../]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./DynamicTensorMechanics] # zeta*K*vel + K * disp
displacements = 'disp_x disp_y disp_z'
zeta = 0.000025
static_initialization = true #turns off rayliegh damping for the first time step to stabilize system under gravity
[../]
[./inertia_x] # M*accel + eta*M*vel
type = InertialForce
variable = disp_x
velocity = vel_x
acceleration = accel_x
beta = 0.25 # Newmark time integration
gamma = 0.5 # Newmark time integration
eta = 19.63
[../]
[./inertia_y]
type = InertialForce
variable = disp_y
velocity = vel_y
acceleration = accel_y
beta = 0.25
gamma = 0.5
eta = 19.63
[../]
[./inertia_z]
type = InertialForce
variable = disp_z
velocity = vel_z
acceleration = accel_z
beta = 0.25
gamma = 0.5
eta = 19.63
[../]
[./gravity]
type = Gravity
variable = disp_y
value = -9.81
[../]
[]
[AuxKernels]
[./accel_x] # Calculates and stores acceleration at the end of time step
type = NewmarkAccelAux
variable = accel_x
displacement = disp_x
velocity = vel_x
beta = 0.25
execute_on = timestep_end
[../]
[./vel_x] # Calculates and stores velocity at the end of the time step
type = NewmarkVelAux
variable = vel_x
acceleration = accel_x
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_y]
type = NewmarkAccelAux
variable = accel_y
displacement = disp_y
velocity = vel_y
beta = 0.25
execute_on = timestep_end
[../]
[./vel_y]
type = NewmarkVelAux
variable = vel_y
acceleration = accel_y
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_z]
type = NewmarkAccelAux
variable = accel_z
displacement = disp_z
velocity = vel_z
beta = 0.25
execute_on = timestep_end
[../]
[./vel_z]
type = NewmarkVelAux
variable = vel_z
acceleration = accel_z
gamma = 0.5
execute_on = timestep_end
[../]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
[../]
[./strain_xx]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_xx
index_i = 0
index_j = 0
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
[../]
[./strain_yy]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_yy
index_i = 1
index_j = 1
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
[../]
[./strain_zz]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_zz
index_i = 2
index_j = 2
[../]
[]
[Functions]
[./displacement_front]
type = PiecewiseLinear
data_file = 'displacement.csv'
format = columns
[../]
[]
[BCs]
[./prescribed_displacement]
type = PresetDisplacement
variable = disp_z
velocity = vel_z
acceleration = accel_z
beta = 0.25
boundary = front
function = displacement_front
[../]
[./anchor_x]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./anchor_y]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./anchor_z]
type = DirichletBC
variable = disp_z
boundary = back
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
youngs_modulus = 325e6 #Pa
poissons_ratio = 0.3
type = ComputeIsotropicElasticityTensor
block = 0
[../]
[./strain]
#Computes the strain, assuming small strains
type = ComputeSmallStrain
block = 0
displacements = 'disp_x disp_y disp_z'
[../]
[./stress]
#Computes the stress, using linear elasticity
type = ComputeLinearElasticStress
block = 0
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = density
prop_values = 2000 #kg/m3
[../]
[]
[Controls] # turns off inertial terms for the first time step
[./period0]
type = TimePeriod
disable_objects = '*/vel_x */vel_y */vel_z */accel_x */accel_y */accel_z */inertia_x */inertia_y */inertia_z'
start_time = 0.0
end_time = 0.1 # dt used in the simulation
[../]
[../]
[Executioner]
type = Transient
start_time = 0
end_time = 3.0
l_tol = 1e-6
nl_rel_tol = 1e-6
nl_abs_tol = 1e-6
dt = 0.1
timestep_tolerance = 1e-6
[]
[Postprocessors] # These quantites are printed to a csv file at every time step
[./_dt]
type = TimestepSize
[../]
[./accel_6x]
type = NodalVariableValue
nodeid = 6
variable = accel_x
[../]
[./accel_6y]
type = NodalVariableValue
nodeid = 6
variable = accel_y
[../]
[./accel_6z]
type = NodalVariableValue
nodeid = 6
variable = accel_z
[../]
[./vel_6x]
type = NodalVariableValue
nodeid = 6
variable = vel_x
[../]
[./vel_6y]
type = NodalVariableValue
nodeid = 6
variable = vel_y
[../]
[./vel_6z]
type = NodalVariableValue
nodeid = 6
variable = vel_z
[../]
[./disp_6x]
type = NodalVariableValue
nodeid = 6
variable = disp_x
[../]
[./disp_6y]
type = NodalVariableValue
nodeid = 6
variable = disp_y
[../]
[./disp_6z]
type = NodalVariableValue
nodeid = 6
variable = disp_z
[../]
[]
[Outputs]
exodus = true
csv = true
perf_graph = true
[]
(modules/tensor_mechanics/test/tests/interaction_integral/interaction_integral_2d_rot.i)
#This tests the Interaction-Integral evaluation capability.
#This is a 2d nonlinear-plane strain model
[GlobalParams]
order = FIRST
# order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[Mesh]
file = crack2d_rot.e
displacements = 'disp_x disp_y'
[]
[Functions]
[./rampConstant]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = -1e2
[../]
[]
[DomainIntegral]
integrals = 'InteractionIntegralKI InteractionIntegralKII InteractionIntegralKIII'
boundary = 800
crack_direction_method = CrackDirectionVector
crack_direction_vector = '0 1 0'
2d = true
axis_2d = 2
radius_inner = '4.0 4.5 5.0 5.5 6.0'
radius_outer = '4.5 5.0 5.5 6.0 6.5'
block = 1
youngs_modulus = 207000
poissons_ratio = 0.3
output_q = false
incremental = true
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
planar_formulation = PLANE_STRAIN
[../]
[]
[BCs]
[./crack_y]
type = DirichletBC
variable = disp_x
boundary = 100
value = 0.0
[../]
[./no_x]
type = DirichletBC
variable = disp_y
boundary = 700
value = 0.0
[../]
[./Pressure]
[./Side1]
boundary = 400
function = rampConstant
[../]
[../]
[] # BCs
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_abs_tol = 1e-5
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Outputs]
file_base = interaction_integral_2d_rot_out
exodus = true
csv = true
[]
(modules/tensor_mechanics/test/tests/beam/static_vm/ansys_vm2.i)
# This is a reproduction of test number 2 of ANSYS apdl verification manual.
# This test checks for the deformation at the center of a beam with simply
# supported boundary conditions and a uniform load w = 10,000 lb/ft.
# ||||||||| def. ||||||||
# *---*---*---*---*---*---*---*---*
# /\ /\
# /// oo
# a l a
# <-----> <--------------> <----->
#
# l = 240 in, a = 120 in, A = 50.65 in^2, Iz = 7892 in^2
# E = 30e6 psi
# Solution deflection: 0.182 in. (dispz_5: -1.824633e-01)
[Mesh]
[generated_mesh]
type = GeneratedMeshGenerator
dim = 1
nx = 8
xmin = 0.0
xmax = 480.0
[]
[cnode]
type = ExtraNodesetGenerator
coord = '0.0'
new_boundary = 'one'
input = generated_mesh
[]
[cnode1]
type = ExtraNodesetGenerator
coord = '60.0'
new_boundary = 'two'
input = cnode
[]
[cnode2]
type = ExtraNodesetGenerator
coord = '420.0'
new_boundary = 'eight'
input = cnode1
[]
[cnode3]
type = ExtraNodesetGenerator
coord = '480.0'
new_boundary = 'nine'
input = cnode2
[]
[cnode4]
type = ExtraNodesetGenerator
coord = '120.0'
new_boundary = 'BC1'
input = cnode3
[]
[cnode5]
type = ExtraNodesetGenerator
coord = '360.0'
new_boundary = 'BC2'
input = cnode4
[]
[]
[Modules/TensorMechanics/LineElementMaster]
[./all]
add_variables = true
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
# Geometry parameters
area = 50.65
Ay = 0.0
Az = 0.0
Iy = 7892.0
Iz = 7892.0
y_orientation = '0 1.0 0.0'
[../]
[]
[Materials]
[./elasticity]
type = ComputeElasticityBeam
youngs_modulus = 30.0e6
# poissons_ratio = -0.9998699638
poissons_ratio = 0.33
# poissons_ratio = 0.3
shear_coefficient = 0.85
block = 0
[../]
[./stress]
type = ComputeBeamResultants
block = 0
[../]
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = 'BC1'
value = 0.0
[../]
[./fixy1]
type = DirichletBC
variable = disp_y
boundary = 'BC1'
value = 0.0
[../]
[./fixz1]
type = DirichletBC
variable = disp_z
boundary = 'BC1'
value = 0.0
[../]
[./fixy2]
type = DirichletBC
variable = disp_y
boundary = 'BC2'
value = 0.0
[../]
[./fixz2]
type = DirichletBC
variable = disp_z
boundary = 'BC2'
value = 0.0
[../]
[]
[Functions]
[./force_50e3]
type = PiecewiseLinear
x = '0.0 10.0'
y = '0.0 50000.0'
[../]
[./force_25e3]
type = PiecewiseLinear
x = '0.0 10.0'
y = '0.0 25000.0'
[../]
[]
[NodalKernels]
[./force_z2]
type = UserForcingFunctionNodalKernel
variable = disp_z
boundary = 'two'
function = force_50e3
[../]
[./force_z8]
type = UserForcingFunctionNodalKernel
variable = disp_z
boundary = 'eight'
function = force_50e3
[../]
[./force_z1]
type = UserForcingFunctionNodalKernel
variable = disp_z
boundary = 'one'
function = force_25e3
[../]
[./force_z9]
type = UserForcingFunctionNodalKernel
variable = disp_z
boundary = 'nine'
function = force_25e3
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = JFNK
line_search = 'none'
nl_max_its = 15
nl_rel_tol = 1e-06
nl_abs_tol = 1e-06
dt = 1.0
dtmin = 0.001
end_time = 10
[]
[Postprocessors]
[./disp_z1]
type = PointValue
point = '0.0 0.0 0.0'
variable = disp_z
[../]
[./disp_x1]
type = PointValue
point = '0.0 0.0 0.0'
variable = disp_x
[../]
[./disp_z2]
type = PointValue
point = '60.0 0.0 0.0'
variable = disp_z
[../]
[./disp_zBC1]
type = PointValue
point = '120.0 0.0 0.0'
variable = disp_z
[../]
[./disp_z5]
type = PointValue
point = '240.0 0.0 0.0'
variable = disp_z
[../]
[./disp_zBC2]
type = PointValue
point = '360.0 0.0 0.0'
variable = disp_z
[../]
[./disp_xBC2]
type = PointValue
point = '360.0 0.0 0.0'
variable = disp_x
[../]
[./disp_z8]
type = PointValue
point = '420.0 0.0 0.0'
variable = disp_z
[../]
[./disp_z9]
type = PointValue
point = '480.0 0.0 0.0'
variable = disp_z
[../]
[]
[Debug]
show_var_residual_norms = true
[]
[Outputs]
csv = true
exodus = false
[]
(test/tests/geomsearch/2d_moving_penetration/pl_test3ns.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
file = pl_test3.e
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
normal_smoothing_distance = 0.2
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
normal_smoothing_distance = 0.2
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate10]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate13]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate14]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate15]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate16]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-10
l_max_its = 10
start_time = 0.0
dt = 0.0125
end_time = 1.0
[]
[Outputs]
file_base = pl_test3ns_out
exodus = true
[]
(modules/combined/test/tests/ad_power_law_creep/power_law_creep_restart2.i)
# 1x1x1 unit cube with uniform pressure on top face
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
[]
[Variables]
[./temp]
order = FIRST
family = LAGRANGE
initial_condition = 1000.0
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
incremental = true
add_variables = true
generate_output = 'stress_yy creep_strain_xx creep_strain_yy creep_strain_zz elastic_strain_yy'
use_automatic_differentiation = true
[../]
[]
[Functions]
[./top_pull]
type = PiecewiseLinear
x = '0 1'
y = '1 1'
[../]
[]
[Kernels]
[./heat]
type = ADHeatConduction
variable = temp
[../]
[./heat_ie]
type = ADHeatConductionTimeDerivative
variable = temp
[../]
[]
[BCs]
[./u_top_pull]
type = ADPressure
variable = disp_y
component = 1
boundary = top
constant = -10.0e6
function = top_pull
[../]
[./u_bottom_fix]
type = ADDirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./u_yz_fix]
type = ADDirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./u_xy_fix]
type = ADDirichletBC
variable = disp_z
boundary = back
value = 0.0
[../]
[./temp_fix]
type = DirichletBC
variable = temp
boundary = 'bottom top'
value = 1000.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 2e11
poissons_ratio = 0.3
constant_on = SUBDOMAIN
[../]
[./radial_return_stress]
type = ADComputeMultipleInelasticStress
inelastic_models = 'power_law_creep'
[../]
[./power_law_creep]
type = ADPowerLawCreepStressUpdate
coefficient = 1.0e-15
n_exponent = 4
activation_energy = 3.0e5
temperature = temp
[../]
[./thermal]
type = ADHeatConductionMaterial
specific_heat = 1.0
thermal_conductivity = 100.
[../]
[./density]
type = ADDensity
density = 1.0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 20
nl_max_its = 20
nl_rel_tol = 1e-6
nl_abs_tol = 1e-6
l_tol = 1e-5
start_time = 0.6
end_time = 1.0
num_steps = 12
dt = 0.1
[]
[Outputs]
file_base = power_law_creep_out
exodus = true
[]
[Problem]
restart_file_base = power_law_creep_restart1_out_cp/0006
[]
(modules/porous_flow/test/tests/infiltration_and_drainage/rsc01.i)
# RSC test with high-res time and spatial resolution
[Mesh]
type = GeneratedMesh
dim = 2
nx = 600
ny = 1
xmin = 0
xmax = 10 # x is the depth variable, called zeta in RSC
ymin = 0
ymax = 0.05
[]
[GlobalParams]
PorousFlowDictator = dictator
gravity = '0 0 0'
[]
[Functions]
[dts]
type = PiecewiseLinear
y = '3E-3 3E-2 0.05'
x = '0 1 5'
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pwater poil'
number_fluid_phases = 2
number_fluid_components = 2
[]
[pc]
type = PorousFlowCapillaryPressureRSC
oil_viscosity = 2E-3
scale_ratio = 2E3
shift = 10
[]
[]
[Modules]
[FluidProperties]
[water]
type = SimpleFluidProperties
bulk_modulus = 2e9
density0 = 10
thermal_expansion = 0
viscosity = 1e-3
[]
[oil]
type = SimpleFluidProperties
bulk_modulus = 2e9
density0 = 20
thermal_expansion = 0
viscosity = 2e-3
[]
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow2PhasePP
phase0_porepressure = pwater
phase1_porepressure = poil
capillary_pressure = pc
[]
[massfrac]
type = PorousFlowMassFraction
mass_fraction_vars = 'massfrac_ph0_sp0 massfrac_ph1_sp0'
[]
[water]
type = PorousFlowSingleComponentFluid
fp = water
phase = 0
compute_enthalpy = false
compute_internal_energy = false
[]
[oil]
type = PorousFlowSingleComponentFluid
fp = oil
phase = 1
compute_enthalpy = false
compute_internal_energy = false
[]
[relperm_water]
type = PorousFlowRelativePermeabilityCorey
n = 1
phase = 0
[]
[relperm_oil]
type = PorousFlowRelativePermeabilityCorey
n = 1
phase = 1
[]
[porosity]
type = PorousFlowPorosityConst
porosity = 0.25
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
[]
[]
[Variables]
[pwater]
[]
[poil]
[]
[]
[ICs]
[water_init]
type = ConstantIC
variable = pwater
value = 0
[]
[oil_init]
type = ConstantIC
variable = poil
value = 15
[]
[]
[Kernels]
[mass0]
type = PorousFlowMassTimeDerivative
fluid_component = 0
variable = pwater
[]
[flux0]
type = PorousFlowAdvectiveFlux
fluid_component = 0
variable = pwater
[]
[mass1]
type = PorousFlowMassTimeDerivative
fluid_component = 1
variable = poil
[]
[flux1]
type = PorousFlowAdvectiveFlux
fluid_component = 1
variable = poil
[]
[]
[AuxVariables]
[SWater]
family = MONOMIAL
order = CONSTANT
[]
[SOil]
family = MONOMIAL
order = CONSTANT
[]
[massfrac_ph0_sp0]
initial_condition = 1
[]
[massfrac_ph1_sp0]
initial_condition = 0
[]
[]
[AuxKernels]
[SWater]
type = MaterialStdVectorAux
property = PorousFlow_saturation_qp
index = 0
variable = SWater
[]
[SOil]
type = MaterialStdVectorAux
property = PorousFlow_saturation_qp
index = 1
variable = SOil
[]
[]
[BCs]
# we are pumping water into a system that has virtually incompressible fluids, hence the pressures rise enormously. this adversely affects convergence because of almost-overflows and precision-loss problems. The fixed things help keep pressures low and so prevent these awful behaviours. the movement of the saturation front is the same regardless of the fixed things.
active = 'recharge fixedoil fixedwater'
[recharge]
type = PorousFlowSink
variable = pwater
boundary = 'left'
flux_function = -1.0
[]
[fixedwater]
type = DirichletBC
variable = pwater
boundary = 'right'
value = 0
[]
[fixedoil]
type = DirichletBC
variable = poil
boundary = 'right'
value = 15
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
petsc_options = '-snes_converged_reason -ksp_diagonal_scale -ksp_diagonal_scale_fix -ksp_gmres_modifiedgramschmidt -snes_linesearch_monitor'
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -sub_pc_factor_shift_type -pc_asm_overlap -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'gmres asm lu NONZERO 2 1E-10 1E-10 10000'
[]
[]
[VectorPostprocessors]
[swater]
type = LineValueSampler
variable = SWater
start_point = '0 0 0'
end_point = '7 0 0'
sort_by = x
num_points = 21
execute_on = timestep_end
[]
[]
[Executioner]
type = Transient
solve_type = Newton
petsc_options = '-snes_converged_reason'
end_time = 5
[TimeStepper]
type = FunctionDT
function = dts
[]
[]
[Outputs]
file_base = rsc01
[along_line]
type = CSV
execute_vector_postprocessors_on = final
[]
[exodus]
type = Exodus
execute_on = 'initial final'
[]
[]
(test/tests/geomsearch/2d_moving_penetration/pl_test2tt.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
file = pl_test2.e
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
tangential_tolerance = 0.1
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
tangential_tolerance = 0.1
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate10]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate13]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate14]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate15]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate16]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 0.7 -0.7 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-9
l_max_its = 10
start_time = 0.0
dt = 0.05
end_time = 1.0
[]
[Outputs]
file_base = pl_test2tt_out
exodus = true
[]
(modules/xfem/test/tests/pressure_bc/edge_2d_pressure.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
volumetric_locking_correction = False
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 9
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.0 0.5 0.5 0.5'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
generate_output = 'stress_xx stress_yy'
[../]
[]
[Functions]
[./pressure]
type = PiecewiseLinear
x = '0 1.0 2.0'
y = '0 500 1000'
[../]
[]
[BCs]
[./bottom_y]
type = DirichletBC
boundary = 0
variable = disp_y
value = 0.0
[../]
[./top_y]
type = DirichletBC
boundary = 2
variable = disp_y
value = 0.0
[../]
[./bottom_x]
type = DirichletBC
boundary = 0
variable = disp_x
value = 0.0
[../]
[]
[DiracKernels]
[./pressure_x]
type = XFEMPressure
variable = disp_x
component = 0
function = pressure
[../]
[./pressure_y]
type = XFEMPressure
variable = disp_y
component = 1
function = pressure
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-12
# time control
start_time = 0.0
dt = 1
end_time = 2
[]
[Outputs]
file_base = edge_2d_pressure_out
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(test/tests/multiapps/picard/function_dt_sub.i)
[Mesh]
type = GeneratedMesh
dim = 1
xmin = 0
xmax = 1
nx = 10
[]
[Functions]
[./u_fn]
type = ParsedFunction
value = t*x
[../]
[./ffn]
type = ParsedFunction
value = x
[../]
[./dts]
type = PiecewiseLinear
x = '0.1 10'
y = '0.1 10'
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./td]
type = TimeDerivative
variable = u
[../]
[./fn]
type = BodyForce
variable = u
function = ffn
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = FunctionDirichletBC
variable = u
boundary = right
function = u_fn
[../]
[]
[Executioner]
type = Transient
dt = 0.1
solve_type = 'PJFNK'
nl_abs_tol = 1e-10
start_time = 0
num_steps = 3
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
exodus = true
[]
(framework/contrib/hit/test/output.i)
# This tests the thermal expansion coefficient function using both
# options to specify that function: mean and instantaneous. There
# two blocks, each containing a single element, and these use the
# two variants of the function.
# In this test, the instantaneous CTE function has a constant value,
# while the mean CTE function is an analytic function designed to
# give the same response. If \bar{alpha}(T) is the mean CTE function,
# and \alpha(T) is the instantaneous CTE function,
# \bar{\alpha}(T) = 1/(T-Tref) \intA^{T}_{Tsf} \alpha(T) dT
# where Tref is the reference temperature used to define the mean CTE
# function, and Tsf is the stress-free temperature.
# The two models produce very similar results. There are slight
# differences due to the large deformation treatment.
[Mesh]
file = 'blocks.e'
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./temp]
order = FIRST
family = LAGRANGE
[../]
[]
[SolidMechanics]
[./solid]
disp_x = disp_x
disp_y = disp_y
disp_z = disp_z
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = disp_y
boundary = 2
value = 0.0
[../]
[left]
type = FunctionDirichletBC
variable = disp_x
function = 0.02*t
boundary = 3
[]
[back]
type = FunctionDirichletBC
variable = disp_z
function = 0.01*t
boundary = 1
[]
[]
[AuxKernels]
[./temp]
type = FunctionAux
variable = temp
block = '1 2'
function = temp_func
[../]
[]
[Materials]
[./mean_alpha]
type = Elastic
block = 1
youngs_modulus = 1e6
poissons_ratio = .3
disp_x = disp_x
disp_y = disp_y
disp_z = disp_z
temp = temp
thermal_expansion_function = cte_func_mean
stress_free_temperature = 0.0
thermal_expansion_reference_temperature = 0.5
thermal_expansion_function_type = mean
[../]
[./inst_alpha]
type = Elastic
block = 2
youngs_modulus = 1e6
poissons_ratio = .3
disp_x = disp_x
disp_y = disp_y
disp_z = disp_z
temp = temp
thermal_expansion_function = cte_func_inst
stress_free_temperature = 0.0
thermal_expansion_function_type = instantaneous
[../]
[]
[Functions]
[./cte_func_mean]
type = ParsedFunction
vars = 'tsf tref scale' #stress free temp, reference temp, scale factor
vals = '0.0 0.5 1e-4'
value = 'scale * (t - tsf) / (t - tref)'
[../]
[./cte_func_inst]
type = PiecewiseLinear
xy_data = '0 1.0
2 1.0'
scale_factor = 1e-4
[../]
[./temp_func]
type = PiecewiseLinear
xy_data = '0 1
1 2'
[../]
[]
[Postprocessors]
[./disp_1]
type = NodalMaxValue
variable = disp_x
boundary = 101
[../]
[./disp_2]
type = NodalMaxValue
variable = disp_x
boundary = 102
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
l_max_its = 100
l_tol = 1e-4
nl_abs_tol = 1e-8
nl_rel_tol = 1e-12
start_time = 0.0
end_time = 1.0
dt = 0.1
[]
[Outputs]
file_base = const_alpha_out
exodus = true
csv = true
[]
(modules/navier_stokes/test/tests/ins/jeffery_hamel/wedge_dirichlet.i)
# This input file tests whether we can converge to the semi-analytical
# solution for flow in a 2D wedge.
[GlobalParams]
gravity = '0 0 0'
# Params used by the WedgeFunction for computing the exact solution.
# The value of K is only required for comparing the pressure to the
# exact solution, and is computed by the associated jeffery_hamel.py
# script.
alpha_degrees = 15
Re = 30
K = -9.78221333616
f = f_theta
[]
[Mesh]
[file]
type = FileMeshGenerator
# file = wedge_4x6.e
file = wedge_8x12.e
# file = wedge_16x24.e
# file = wedge_32x48.e
# file = wedge_64x96.e
[]
[./corner_node]
# Pin is on the centerline of the channel on the left-hand side of
# the domain at r=1. If you change the domain, you will need to
# update this pin location for the pressure exact solution to
# work.
type = ExtraNodesetGenerator
new_boundary = pinned_node
coord = '1 0'
input = file
[../]
[]
[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
p = p
[../]
[./x_momentum_time]
type = INSMomentumTimeDerivative
variable = vel_x
[../]
[./x_momentum_space]
type = INSMomentumLaplaceForm
variable = vel_x
u = vel_x
v = vel_y
p = p
component = 0
[../]
[./y_momentum_time]
type = INSMomentumTimeDerivative
variable = vel_y
[../]
[./y_momentum_space]
type = INSMomentumLaplaceForm
variable = vel_y
u = vel_x
v = vel_y
p = p
component = 1
[../]
[]
[BCs]
[./vel_x_no_slip]
type = DirichletBC
variable = vel_x
boundary = 'top_wall bottom_wall'
value = 0.0
[../]
[./vel_y_no_slip]
type = DirichletBC
variable = vel_y
boundary = 'top_wall bottom_wall'
value = 0.0
[../]
[./vel_x_inlet]
type = FunctionDirichletBC
variable = vel_x
boundary = 'inlet outlet'
function = 'vel_x_exact'
[../]
[./vel_y_inlet]
type = FunctionDirichletBC
variable = vel_y
boundary = 'inlet outlet'
function = 'vel_y_exact'
[../]
[./pressure_pin]
type = DirichletBC
variable = p
boundary = 'pinned_node'
value = 0
[../]
[]
[Materials]
[./const]
type = GenericConstantMaterial
block = 1
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[]
[Preconditioning]
[./SMP_PJFNK]
type = SMP
full = true
solve_type = NEWTON
[../]
[]
[Executioner]
type = Transient
dt = 1.e-2
dtmin = 1.e-2
num_steps = 5
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-13
nl_abs_tol = 1e-11
nl_max_its = 10
l_tol = 1e-6
l_max_its = 300
[]
[Outputs]
exodus = true
[]
[Functions]
[./f_theta]
# Non-dimensional solution values f(eta), 0 <= eta <= 1 for
# alpha=15 deg, Re=30. Note: this introduces an input file
# ordering dependency: this Function must appear *before* the two
# functions below which use it since apparently proper dependency
# resolution is not done in this scenario.
type = PiecewiseLinear
data_file = 'f.csv'
format = 'columns'
[../]
[./vel_x_exact]
type = WedgeFunction
var_num = 0
mu = 1
rho = 1
[../]
[./vel_y_exact]
type = WedgeFunction
var_num = 1
mu = 1
rho = 1
[../]
[./p_exact]
type = WedgeFunction
var_num = 2
mu = 1
rho = 1
[../]
[]
[Postprocessors]
[./vel_x_L2_error]
type = ElementL2Error
variable = vel_x
function = vel_x_exact
execute_on = 'initial timestep_end'
[../]
[./vel_y_L2_error]
type = ElementL2Error
variable = vel_y
function = vel_y_exact
execute_on = 'initial timestep_end'
[../]
[./p_L2_error]
type = ElementL2Error
variable = p
function = p_exact
execute_on = 'initial timestep_end'
[../]
[]
(modules/contact/test/tests/verification/patch_tests/single_pnt_2d/single_point_2d_frictional.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = single_point_2d.e
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[]
[Functions]
[./appl_disp]
type = PiecewiseLinear
x = '0 0.001 0.101'
y = '0 0.0 -0.10'
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./incslip_x]
type = PenetrationAux
variable = inc_slip_x
quantity = incremental_slip_x
boundary = 3
paired_boundary = 2
[../]
[./incslip_y]
type = PenetrationAux
variable = inc_slip_y
quantity = incremental_slip_y
boundary = 3
paired_boundary = 2
[../]
[./accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[../]
[./accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[]
[BCs]
[./botx]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./boty]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./topx]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = appl_disp
[../]
[./topy]
type = DirichletBC
variable = disp_y
boundary = 4
value = -0.002001
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e9
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputePlaneFiniteStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputePlaneFiniteStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 4
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 4
[../]
[./disp_x]
type = NodalVariableValue
nodeid = 5
variable = disp_x
[../]
[./disp_y]
type = NodalVariableValue
nodeid = 5
variable = disp_y
[../]
[./inc_slip_x]
type = NodalVariableValue
nodeid = 5
variable = inc_slip_x
[../]
[./inc_slip_y]
type = NodalVariableValue
nodeid = 5
variable = inc_slip_y
[../]
[./accum_slip_x]
type = NodalVariableValue
nodeid = 5
variable = accum_slip_x
[../]
[./accum_slip_y]
type = NodalVariableValue
nodeid = 5
variable = accum_slip_y
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
l_max_its = 100
nl_max_its = 200
dt = 0.001
end_time = 0.001
num_steps = 10000
nl_rel_tol = 1e-6
nl_abs_tol = 1e-8
dtmin = 0.001
l_tol = 1e-3
[]
[Outputs]
file_base = single_point_2d_out_frictional_0_2_kin
exodus = true
print_linear_residuals = true
perf_graph = true
csv = true
[./console]
type = Console
max_rows = 5
[../]
[]
[Contact]
[./leftright]
primary = 2
secondary = 3
model = coulomb
formulation = kinematic
penalty = 1e12
normalize_penalty = true
friction_coefficient = '0.2'
tangential_tolerance = 1e-3
[../]
[]
[Dampers]
[./contact_slip]
type = ContactSlipDamper
primary = '2'
secondary = '3'
[../]
[]
(modules/tensor_mechanics/test/tests/interaction_integral/interaction_integral_3d_rot.i)
#This tests the Interaction-Integral evaluation capability.
#This is a 3d extrusion of a 2d plane strain model with 2 elements
#through the thickness, and calculates the Interaction-Integrals using options
#to treat it as 3d.
[GlobalParams]
order = FIRST
# order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[Mesh]
file = crack3d_rot.e
displacements = 'disp_x disp_y disp_z'
[]
[Functions]
[./rampConstant]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = -1e2
[../]
[]
[DomainIntegral]
integrals = 'InteractionIntegralKI InteractionIntegralKII InteractionIntegralKIII'
boundary = 800
crack_direction_method = CrackDirectionVector
crack_direction_vector = '0 0 -1'
radius_inner = '4.0 5.5'
radius_outer = '5.5 7.0'
block = 1
youngs_modulus = 207000
poissons_ratio = 0.3
output_q = false
incremental = true
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
[../]
[]
[BCs]
[./crack_y]
type = DirichletBC
variable = disp_y
boundary = 100
value = 0.0
[../]
[./no_z]
type = DirichletBC
variable = disp_x
boundary = 500
value = 0.0
[../]
[./no_z2]
type = DirichletBC
variable = disp_x
boundary = 510
value = 0.0
[../]
[./no_x]
type = DirichletBC
variable = disp_z
boundary = 700
value = 0.0
[../]
[./Pressure]
[./Side1]
boundary = 400
function = rampConstant
[../]
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_abs_tol = 1e-5
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Outputs]
file_base = interaction_integral_3d_rot_out
exodus = true
csv = true
[]
(test/tests/geomsearch/3d_moving_penetration/pl_test2.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
file = pl_test2.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./normal_z]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./closest_point_z]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[./diff_z]
type = Diffusion
variable = disp_z
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = normal_z
boundary = 11
paired_boundary = 12
quantity = normal_z
[../]
[./penetrate10]
type = PenetrationAux
variable = normal_z
boundary = 12
paired_boundary = 11
quantity = normal_z
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate13]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate14]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate15]
type = PenetrationAux
variable = closest_point_z
boundary = 11
paired_boundary = 12
quantity = closest_point_z
[../]
[./penetrate16]
type = PenetrationAux
variable = closest_point_z
boundary = 12
paired_boundary = 11
quantity = closest_point_z
[../]
[./penetrate17]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate18]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate19]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate20]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b1z]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[./b2z]
type = DirichletBC
variable = disp_z
boundary = 2
value = 0
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 0.7 -0.7 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-9
l_max_its = 10
start_time = 0.0
dt = 0.05
end_time = 1.0
[]
[Outputs]
file_base = pl_test2_out
exodus = true
[]
(modules/richards/test/tests/dirac/bh04.i)
# unsaturated
# production
[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
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1E-2 1E-1 1 1E1 1E2 1E3'
x = '0 1E-1 1 1E1 1E2 1E3'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1000
bulk_mod = 2E9
[../]
[./Seff1VG]
type = RichardsSeff1VG
m = 0.8
al = 1E-5
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0
sum_s_res = 0
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 1E8
[../]
[./borehole_total_outflow_mass]
type = RichardsSumQuantity
[../]
[]
[Variables]
active = 'pressure'
[./pressure]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./p_ic]
type = FunctionIC
variable = pressure
function = initial_pressure
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[Kernels]
active = 'richardsf richardst'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[DiracKernels]
[./bh]
type = RichardsBorehole
bottom_pressure = -1E6
point_file = bh02.bh
SumQuantityUO = borehole_total_outflow_mass
variable = pressure
unit_weight = '0 0 0'
character = 1
[../]
[]
[Postprocessors]
[./bh_report]
type = RichardsPlotQuantity
uo = borehole_total_outflow_mass
[../]
[./fluid_mass0]
type = RichardsMass
variable = pressure
execute_on = timestep_begin
[../]
[./fluid_mass1]
type = RichardsMass
variable = pressure
execute_on = timestep_end
[../]
[./zmass_error]
type = FunctionValuePostprocessor
function = mass_bal_fcn
execute_on = timestep_end
[../]
[./p0]
type = PointValue
variable = pressure
point = '1 1 1'
execute_on = timestep_end
[../]
[]
[Functions]
[./initial_pressure]
type = ParsedFunction
value = 0
[../]
[./mass_bal_fcn]
type = ParsedFunction
value = abs((a-c+d)/2/(a+c))
vars = 'a c d'
vals = 'fluid_mass1 fluid_mass0 bh_report'
[../]
[]
[Materials]
[./all]
type = RichardsMaterial
block = 0
viscosity = 1E-3
mat_porosity = 0.1
mat_permeability = '1E-12 0 0 0 1E-12 0 0 0 1E-12'
density_UO = DensityConstBulk
relperm_UO = RelPermPower
sat_UO = Saturation
seff_UO = Seff1VG
SUPG_UO = SUPGstandard
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = Seff1VG
pressure_vars = pressure
[../]
[]
[Preconditioning]
[./usual]
type = SMP
full = true
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -ksp_max_it'
petsc_options_value = 'bcgs bjacobi 1E-10 1E-10 10000 30'
[../]
[]
[Executioner]
type = Transient
end_time = 1E3
solve_type = NEWTON
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = bh04
exodus = false
csv = true
execute_on = timestep_end
[]
(modules/xfem/test/tests/diffusion_xfem/levelsetcut2d.i)
# 2D: Mesh is cut by level set based cutter
# The level set is a MOOSE variable
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 3
ny = 3
xmin = 0
xmax = 1
ymin = 0
ymax = 1
elem_type = QUAD4
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./level_set_cut_uo]
type = LevelSetCutUserObject
level_set_var = ls
[../]
[]
[Variables]
[./u]
[../]
[./ls]
[../]
[]
[Functions]
[./u_left]
type = PiecewiseLinear
x = '0 2'
y = '3 5'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./diff_ls]
type = Diffusion
variable = ls
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = DirichletBC
variable = u
boundary = 3
value = 3
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./left_ls]
type = DirichletBC
variable = ls
boundary = 3
value = 3
[../]
[./right_ls]
type = DirichletBC
variable = ls
boundary = 1
value = -3
[../]
[]
[Executioner]
type = Transient
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
start_time = 0.0
dt = 1
end_time = 1.0
max_xfem_update = 1
[]
[Outputs]
interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/xfem/test/tests/second_order_elements/diffusion_quad9_levelsetcut.i)
# A simple diffusion problem with quad9 elements
# The mesh is cut using levle set based cutter
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 3
ny = 3
xmin = 0
xmax = 1
ymin = 0
ymax = 1
elem_type = QUAD9
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./level_set_cut_uo]
type = LevelSetCutUserObject
level_set_var = ls
[../]
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./ls]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./ls_function]
type = FunctionAux
variable = ls
function = ls_func
[../]
[]
[Functions]
[./u_left]
type = PiecewiseLinear
x = '0 2'
y = '3 5'
[../]
[./ls_func]
type = ParsedFunction
value = 'x-0.53'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = DirichletBC
variable = u
boundary = 3
value = 3
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Transient
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
start_time = 0.0
dt = 1
end_time = 1.0
max_xfem_update = 1
[]
[Outputs]
interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/porous_flow/test/tests/poro_elasticity/mandel.i)
# Mandel's problem of consolodation of a drained medium
#
# A sample is in plane strain.
# -a <= x <= a
# -b <= y <= b
# It is squashed with constant force by impermeable, frictionless plattens on its top and bottom surfaces (at y=+/-b)
# Fluid is allowed to leak out from its sides (at x=+/-a)
# The porepressure within the sample is monitored.
#
# As is common in the literature, this is simulated by
# considering the quarter-sample, 0<=x<=a and 0<=y<=b, with
# impermeable, roller BCs at x=0 and y=0 and y=b.
# Porepressure is fixed at zero on x=a.
# Porepressure and displacement are initialised to zero.
# Then the top (y=b) is moved downwards with prescribed velocity,
# so that the total force that is inducing this downwards velocity
# is fixed. The velocity is worked out by solving Mandel's problem
# analytically, and the total force is monitored in the simulation
# to check that it indeed remains constant.
#
# Here are the problem's parameters, and their values:
# Soil width. a = 1
# Soil height. b = 0.1
# Soil's Lame lambda. la = 0.5
# Soil's Lame mu, which is also the Soil's shear modulus. mu = G = 0.75
# Soil bulk modulus. K = la + 2*mu/3 = 1
# Drained Poisson ratio. nu = (3K - 2G)/(6K + 2G) = 0.2
# Soil bulk compliance. 1/K = 1
# Fluid bulk modulus. Kf = 8
# Fluid bulk compliance. 1/Kf = 0.125
# Soil initial porosity. phi0 = 0.1
# Biot coefficient. alpha = 0.6
# Biot modulus. M = 1/(phi0/Kf + (alpha - phi0)(1 - alpha)/K) = 4.705882
# Undrained bulk modulus. Ku = K + alpha^2*M = 2.694118
# Undrained Poisson ratio. nuu = (3Ku - 2G)/(6Ku + 2G) = 0.372627
# Skempton coefficient. B = alpha*M/Ku = 1.048035
# Fluid mobility (soil permeability/fluid viscosity). k = 1.5
# Consolidation coefficient. c = 2*k*B^2*G*(1-nu)*(1+nuu)^2/9/(1-nuu)/(nuu-nu) = 3.821656
# Normal stress on top. F = 1
#
# The solution for porepressure and displacements is given in
# AHD Cheng and E Detournay "A direct boundary element method for plane strain poroelasticity" International Journal of Numerical and Analytical Methods in Geomechanics 12 (1988) 551-572.
# The solution involves complicated infinite series, so I shall not write it here
#
# FINAL NOTE: The above solution assumes constant Biot Modulus.
# In porous_flow this is not true. Therefore the solution is
# a little different than in the paper. This test was therefore
# validated against MOOSE's poromechanics, which can choose either
# a constant Biot Modulus (which has been shown to agree with
# the analytic solution), or a non-constant Biot Modulus (which
# gives the same results as porous_flow).
[Mesh]
type = GeneratedMesh
dim = 3
nx = 10
ny = 1
nz = 1
xmin = 0
xmax = 1
ymin = 0
ymax = 0.1
zmin = 0
zmax = 1
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
PorousFlowDictator = dictator
block = 0
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'porepressure disp_x disp_y disp_z'
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureVG
m = 0.8
alpha = 1e-5
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[disp_z]
[]
[porepressure]
[]
[]
[BCs]
[roller_xmin]
type = DirichletBC
variable = disp_x
value = 0
boundary = 'left'
[]
[roller_ymin]
type = DirichletBC
variable = disp_y
value = 0
boundary = 'bottom'
[]
[plane_strain]
type = DirichletBC
variable = disp_z
value = 0
boundary = 'back front'
[]
[xmax_drained]
type = DirichletBC
variable = porepressure
value = 0
boundary = right
[]
[top_velocity]
type = FunctionDirichletBC
variable = disp_y
function = top_velocity
boundary = top
[]
[]
[Functions]
[top_velocity]
type = PiecewiseLinear
x = '0 0.002 0.006 0.014 0.03 0.046 0.062 0.078 0.094 0.11 0.126 0.142 0.158 0.174 0.19 0.206 0.222 0.238 0.254 0.27 0.286 0.302 0.318 0.334 0.35 0.366 0.382 0.398 0.414 0.43 0.446 0.462 0.478 0.494 0.51 0.526 0.542 0.558 0.574 0.59 0.606 0.622 0.638 0.654 0.67 0.686 0.702'
y = '-0.041824842 -0.042730269 -0.043412712 -0.04428867 -0.045509181 -0.04645965 -0.047268246 -0.047974749 -0.048597109 -0.0491467 -0.049632388 -0.050061697 -0.050441198 -0.050776675 -0.051073238 -0.0513354 -0.051567152 -0.051772022 -0.051953128 -0.052113227 -0.052254754 -0.052379865 -0.052490464 -0.052588233 -0.052674662 -0.052751065 -0.052818606 -0.052878312 -0.052931093 -0.052977751 -0.053018997 -0.053055459 -0.053087691 -0.053116185 -0.053141373 -0.05316364 -0.053183324 -0.053200724 -0.053216106 -0.053229704 -0.053241725 -0.053252351 -0.053261745 -0.053270049 -0.053277389 -0.053283879 -0.053289615'
[]
[]
[AuxVariables]
[stress_yy]
order = CONSTANT
family = MONOMIAL
[]
[tot_force]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
[]
[tot_force]
type = ParsedAux
args = 'stress_yy porepressure'
execute_on = timestep_end
variable = tot_force
function = '-stress_yy+0.6*porepressure'
[]
[]
[Kernels]
[grad_stress_x]
type = StressDivergenceTensors
variable = disp_x
component = 0
[]
[grad_stress_y]
type = StressDivergenceTensors
variable = disp_y
component = 1
[]
[grad_stress_z]
type = StressDivergenceTensors
variable = disp_z
component = 2
[]
[poro_x]
type = PorousFlowEffectiveStressCoupling
biot_coefficient = 0.6
variable = disp_x
component = 0
[]
[poro_y]
type = PorousFlowEffectiveStressCoupling
biot_coefficient = 0.6
variable = disp_y
component = 1
[]
[poro_z]
type = PorousFlowEffectiveStressCoupling
biot_coefficient = 0.6
component = 2
variable = disp_z
[]
[poro_vol_exp]
type = PorousFlowMassVolumetricExpansion
variable = porepressure
fluid_component = 0
[]
[mass0]
type = PorousFlowMassTimeDerivative
fluid_component = 0
variable = porepressure
[]
[flux]
type = PorousFlowAdvectiveFlux
variable = porepressure
gravity = '0 0 0'
fluid_component = 0
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 8
density0 = 1
thermal_expansion = 0
viscosity = 1
[]
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[elasticity_tensor]
type = ComputeElasticityTensor
C_ijkl = '0.5 0.75'
# bulk modulus is lambda + 2*mu/3 = 0.5 + 2*0.75/3 = 1
fill_method = symmetric_isotropic
[]
[strain]
type = ComputeSmallStrain
[]
[stress]
type = ComputeLinearElasticStress
[]
[eff_fluid_pressure]
type = PorousFlowEffectiveFluidPressure
[]
[vol_strain]
type = PorousFlowVolumetricStrain
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = porepressure
capillary_pressure = pc
[]
[massfrac]
type = PorousFlowMassFraction
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[porosity]
type = PorousFlowPorosity
fluid = true
mechanical = true
ensure_positive = false
porosity_zero = 0.1
biot_coefficient = 0.6
solid_bulk = 1
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1.5 0 0 0 1.5 0 0 0 1.5'
[]
[relperm]
type = PorousFlowRelativePermeabilityCorey
n = 0 # unimportant in this fully-saturated situation
phase = 0
[]
[]
[Postprocessors]
[p0]
type = PointValue
outputs = csv
point = '0.0 0 0'
variable = porepressure
[]
[p1]
type = PointValue
outputs = csv
point = '0.1 0 0'
variable = porepressure
[]
[p2]
type = PointValue
outputs = csv
point = '0.2 0 0'
variable = porepressure
[]
[p3]
type = PointValue
outputs = csv
point = '0.3 0 0'
variable = porepressure
[]
[p4]
type = PointValue
outputs = csv
point = '0.4 0 0'
variable = porepressure
[]
[p5]
type = PointValue
outputs = csv
point = '0.5 0 0'
variable = porepressure
[]
[p6]
type = PointValue
outputs = csv
point = '0.6 0 0'
variable = porepressure
[]
[p7]
type = PointValue
outputs = csv
point = '0.7 0 0'
variable = porepressure
[]
[p8]
type = PointValue
outputs = csv
point = '0.8 0 0'
variable = porepressure
[]
[p9]
type = PointValue
outputs = csv
point = '0.9 0 0'
variable = porepressure
[]
[p99]
type = PointValue
outputs = csv
point = '1 0 0'
variable = porepressure
[]
[xdisp]
type = PointValue
outputs = csv
point = '1 0.1 0'
variable = disp_x
[]
[ydisp]
type = PointValue
outputs = csv
point = '1 0.1 0'
variable = disp_y
[]
[total_downwards_force]
type = ElementAverageValue
outputs = csv
variable = tot_force
[]
[dt]
type = FunctionValuePostprocessor
outputs = console
function = if(0.15*t<0.01,0.15*t,0.01)
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'gmres asm lu 1E-14 1E-10 10000'
[]
[]
[Executioner]
type = Transient
solve_type = Newton
start_time = 0
end_time = 0.7
[TimeStepper]
type = PostprocessorDT
postprocessor = dt
dt = 0.001
[]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = mandel
[csv]
interval = 3
type = CSV
[]
[]
(modules/tensor_mechanics/test/tests/ad_smeared_cracking/cracking_function.i)
#
# Simple pull test for cracking. This tests the option to prescribe the
# cracking strength using an AuxVariable. In this case, an elemental
# AuxVariable is used, and a function is used to prescribe its value.
# One of the elements is weaker than the others, so the crack localizes
# in that element.
#
[Mesh]
file = plate.e
[]
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[AuxVariables]
[./cracking_stress_fn]
order = CONSTANT
family = MONOMIAL
[../]
[./crack_flags2]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./displ]
type = PiecewiseLinear
x = '0 0.1 0.2 0.3 0.4'
y = '0 0.001 0 -0.001 0'
[../]
[./fstress]
type = ParsedFunction
value = 'if(x > 0.667, 1.1e6, 1.2e6)'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx strain_xx strain_yy strain_xy strain_yz'
use_automatic_differentiation = true
[../]
[]
[AuxKernels]
[./cracking_stress_fn]
type = FunctionAux
variable = cracking_stress_fn
function = fstress
execute_on = initial
[../]
[./crack_flags2]
type = ADMaterialRealVectorValueAux
property = crack_flags
variable = crack_flags2
component = 2
[../]
[]
[BCs]
[./pull]
type = ADFunctionDirichletBC
variable = disp_x
boundary = '3 4'
function = displ
[../]
[./pin_x]
type = ADDirichletBC
variable = disp_x
boundary = '1 2'
value = 0
[../]
[./pin_y]
type = ADDirichletBC
variable = disp_y
boundary = '1 4'
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 200.0e7
poissons_ratio = 0.0
[../]
[./elastic_stress]
type = ADComputeSmearedCrackingStress
cracking_stress = cracking_stress_fn
softening_models = abrupt_softening
[../]
[./abrupt_softening]
type = ADAbruptSoftening
residual_stress = 0.0
[../]
[]
[Postprocessors]
[./elem_stress_xx]
type = ElementalVariableValue
variable = stress_xx
elementid = 2
[../]
[./elem_strain_xx]
type = ElementalVariableValue
variable = strain_xx
elementid = 2
[../]
[./elem_crack_flags_x]
type = ElementalVariableValue
variable = crack_flags2
elementid = 2
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101 '
line_search = 'none'
l_max_its = 100
nl_max_its = 100
nl_rel_tol = 1e-8
nl_abs_tol = 1e-6
l_tol = 1e-5
start_time = 0.0
end_time = 0.2
dt = 0.0025
[]
[Outputs]
exodus = true
csv = true
[]
(modules/tensor_mechanics/test/tests/ad_anisotropic_creep/ad_aniso_creep_z_3d.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
nx = 2
ny = 2
nz = 10
xmin = 0.0
ymin = 0.0
zmin = 0.0
xmax = 1.0
ymax = 1.0
zmax = 10.0
[]
[corner_node]
type = ExtraNodesetGenerator
new_boundary = '100'
nodes = '9 3'
input = gen
[]
[corner_node_2]
type = ExtraNodesetGenerator
new_boundary = '101'
nodes = '12 1'
input = corner_node
[]
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[AuxVariables]
[hydrostatic_stress]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_xx]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_xy]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_zz]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[hydrostatic_stress]
type = ADRankTwoScalarAux
variable = hydrostatic_stress
rank_two_tensor = stress
scalar_type = Hydrostatic
[]
[creep_strain_xx]
type = ADRankTwoAux
rank_two_tensor = creep_strain
variable = creep_strain_xx
index_i = 0
index_j = 0
[]
[creep_strain_xy]
type = ADRankTwoAux
rank_two_tensor = creep_strain
variable = creep_strain_xy
index_i = 0
index_j = 1
[]
[creep_strain_zz]
type = ADRankTwoAux
rank_two_tensor = creep_strain
variable = creep_strain_zz
index_i = 2
index_j = 2
[]
[sigma_zz]
type = ADRankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
[]
[]
[Functions]
[pull]
type = PiecewiseLinear
x = '0 1.0'
y = '-4e1 -4e1'
[]
[]
[Modules/TensorMechanics/Master]
[all]
strain = FINITE
generate_output = 'elastic_strain_zz stress_zz stress_xx stress_yy stress_xy stress_xz stress_yz'
use_automatic_differentiation = true
add_variables = true
[]
[]
[Materials]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 700
poissons_ratio = 0.0
[]
[elastic_strain]
type = ADComputeMultipleInelasticStress
inelastic_models = "trial_creep_two"
max_iterations = 50
absolute_tolerance = 1e-16
[]
[trial_creep_two]
type = ADHillCreepStressUpdate
coefficient = 1e-16
n_exponent = 9
m_exponent = 0
activation_energy = 0
# F G H L M N
hill_constants = "0.5 0.25 0.3866 1.6413 1.6413 1.2731"
max_inelastic_increment = 0.00003
absolute_tolerance = 1e-20
relative_tolerance = 1e-20
# Force it to not use integration error
max_integration_error = 100.0
[]
[]
[BCs]
[no_disp_x]
type = ADDirichletBC
variable = disp_y
boundary = 100
value = 0.0
[]
[no_disp_y]
type = ADDirichletBC
variable = disp_x
boundary = 101
value = 0.0
[]
[no_disp_z]
type = ADDirichletBC
variable = disp_z
boundary = back
value = 0.0
[]
[Pressure]
[Side1]
boundary = front
function = pull
[]
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
nl_rel_tol = 1.0e-13
nl_abs_tol = 1.0e-13
l_max_its = 90
num_steps = 10
dt = 1.0e-4
start_time = 0
automatic_scaling = true
[]
[Postprocessors]
[matl_ts_min]
type = MaterialTimeStepPostprocessor
[]
[max_disp_x]
type = ElementExtremeValue
variable = disp_x
[]
[max_disp_y]
type = ElementExtremeValue
variable = disp_y
[]
[max_hydro]
type = ElementAverageValue
variable = hydrostatic_stress
[]
[dt]
type = TimestepSize
[]
[num_lin]
type = NumLinearIterations
outputs = console
[]
[num_nonlin]
type = NumNonlinearIterations
outputs = console
[]
[creep_strain_zz]
type = ElementalVariableValue
variable = creep_strain_zz
execute_on = 'TIMESTEP_END'
elementid = 39
[]
[elastic_strain_zz]
type = ElementalVariableValue
variable = elastic_strain_zz
execute_on = 'TIMESTEP_END'
elementid = 39
[]
[sigma_zz]
type = ElementalVariableValue
variable = stress_zz
execute_on = 'TIMESTEP_END'
elementid = 39
[]
[]
[Outputs]
csv = true
exodus = true
perf_graph = true
[]
(modules/navier_stokes/test/tests/ins/jeffery_hamel/wedge_natural.i)
# This input file solves the Jeffery-Hamel problem with the exact
# solution's outlet BC replaced by a natural BC. This problem does
# not converge to the analytical solution, although the flow at the
# outlet still "looks" reasonable.
[GlobalParams]
gravity = '0 0 0'
# Params used by the WedgeFunction for computing the exact solution.
# The value of K is only required for comparing the pressure to the
# exact solution, and is computed by the associated jeffery_hamel.py
# script.
alpha_degrees = 15
Re = 30
K = -9.78221333616
f = f_theta
[]
[Mesh]
file = wedge_8x12.e
[]
[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
p = p
[../]
[./x_momentum_time]
type = INSMomentumTimeDerivative
variable = vel_x
[../]
[./x_momentum_space]
type = INSMomentumLaplaceForm
variable = vel_x
u = vel_x
v = vel_y
p = p
component = 0
[../]
[./y_momentum_time]
type = INSMomentumTimeDerivative
variable = vel_y
[../]
[./y_momentum_space]
type = INSMomentumLaplaceForm
variable = vel_y
u = vel_x
v = vel_y
p = p
component = 1
[../]
[]
[BCs]
[./vel_x_no_slip]
type = DirichletBC
variable = vel_x
boundary = 'top_wall bottom_wall'
value = 0.0
[../]
[./vel_y_no_slip]
type = DirichletBC
variable = vel_y
boundary = 'top_wall bottom_wall'
value = 0.0
[../]
[./vel_x_inlet]
type = FunctionDirichletBC
variable = vel_x
boundary = 'inlet'
function = 'vel_x_exact'
[../]
[./vel_y_inlet]
type = FunctionDirichletBC
variable = vel_y
boundary = 'inlet'
function = 'vel_y_exact'
[../]
[]
[Materials]
[./const]
type = GenericConstantMaterial
block = 1
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[]
[Preconditioning]
[./SMP_NEWTON]
type = SMP
full = true
solve_type = NEWTON
[../]
[]
[Executioner]
type = Transient
dt = 1.e-2
dtmin = 1.e-2
num_steps = 5
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-13
nl_abs_tol = 1e-11
nl_max_its = 10
l_tol = 1e-6
l_max_its = 300
[]
[Outputs]
exodus = true
[]
[Functions]
[./f_theta]
# Non-dimensional solution values f(eta), 0 <= eta <= 1 for
# alpha=15deg, Re=30. Note: this introduces an input file
# ordering dependency: this Function must appear *before* the two
# function below which use it since apparently proper dependency
# resolution is not done in this scenario.
type = PiecewiseLinear
data_file = 'f.csv'
format = 'columns'
[../]
[./vel_x_exact]
type = WedgeFunction
var_num = 0
mu = 1
rho = 1
[../]
[./vel_y_exact]
type = WedgeFunction
var_num = 1
mu = 1
rho = 1
[../]
[]
(modules/combined/test/tests/internal_volume/hex8.i)
#
# Internal Volume Test
#
# This test is designed to compute the internal volume of a space considering
# an embedded volume inside.
#
# The mesh is composed of one block (1) with an interior cavity of volume 8.
# Block 2 sits in the cavity and has a volume of 1. Thus, the total volume
# is 7.
#
# The internal volume is then adjusted by a piecewise linear time varying
# function. Thus, the total volume is 7 plus the addition at the particular
# time.
#
# Time | Addition | Total volume
# 0 | 0.0 | 7.0
# 1 | 3.0 | 10.0
# 2 | 7.0 | 14.0
# 3 | -3.0 | 4.0
#
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
file = meshes/hex8.e
[]
[Functions]
[./step]
type = PiecewiseLinear
x = '0. 1. 2. 3.'
y = '0. 0. 1e-2 0.'
scale_factor = 0.5
[../]
[./addition]
type = PiecewiseLinear
x = '0. 1. 2. 3.'
y = '0. 3. 7. -3.'
[../]
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
volumetric_locking_correction = true
incremental = true
strain = FINITE
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 100
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = 100
value = 0.0
[../]
[./prescribed_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 100
function = step
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = '1 2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
start_time = 0.0
dt = 1.0
end_time = 3.0
[]
[Postprocessors]
[./internalVolume]
type = InternalVolume
boundary = 100
addition = addition
execute_on = 'initial timestep_end'
[../]
[./dispZ]
type = ElementAverageValue
block = '1 2'
variable = disp_z
[../]
[]
[Outputs]
exodus = true
csv = true
[]
(modules/tensor_mechanics/test/tests/dynamics/rayleigh_damping/rayleigh_newmark.i)
# Test for rayleigh damping implemented using Newmark time integration
# The test is for an 1D bar element of unit length fixed on one end
# with a ramped pressure boundary condition applied to the other end.
# zeta and eta correspond to the stiffness and mass proportional rayleigh damping
# beta and gamma are Newmark time integration parameters
# The equation of motion in terms of matrices is:
#
# M*accel + eta*M*vel + zeta*K*vel + K*disp = P*Area
#
# Here M is the mass matrix, K is the stiffness matrix, P is the applied pressure
#
# This equation is equivalent to:
#
# density*accel + eta*density*vel + zeta*d/dt(Div stress) + Div stress = P
#
# The first two terms on the left are evaluated using the Inertial force kernel
# The next two terms on the left involving zeta are evaluated using the
# DynamicStressDivergenceTensors Kernel
# The residual due to Pressure is evaluated using Pressure boundary condition
#
# The system will come to steady state slowly after the pressure becomes constant.
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = 0.0
xmax = 0.1
ymin = 0.0
ymax = 1.0
zmin = 0.0
zmax = 0.1
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./vel_x]
[../]
[./accel_x]
[../]
[./vel_y]
[../]
[./accel_y]
[../]
[./vel_z]
[../]
[./accel_z]
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./DynamicTensorMechanics]
displacements = 'disp_x disp_y disp_z'
zeta = 0.1
[../]
[./inertia_x]
type = InertialForce
variable = disp_x
velocity = vel_x
acceleration = accel_x
beta = 0.25
gamma = 0.5
eta=0.1
[../]
[./inertia_y]
type = InertialForce
variable = disp_y
velocity = vel_y
acceleration = accel_y
beta = 0.25
gamma = 0.5
eta=0.1
[../]
[./inertia_z]
type = InertialForce
variable = disp_z
velocity = vel_z
acceleration = accel_z
beta = 0.25
gamma = 0.5
eta = 0.1
[../]
[]
[AuxKernels]
[./accel_x]
type = NewmarkAccelAux
variable = accel_x
displacement = disp_x
velocity = vel_x
beta = 0.25
execute_on = timestep_end
[../]
[./vel_x]
type = NewmarkVelAux
variable = vel_x
acceleration = accel_x
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_y]
type = NewmarkAccelAux
variable = accel_y
displacement = disp_y
velocity = vel_y
beta = 0.25
execute_on = timestep_end
[../]
[./vel_y]
type = NewmarkVelAux
variable = vel_y
acceleration = accel_y
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_z]
type = NewmarkAccelAux
variable = accel_z
displacement = disp_z
velocity = vel_z
beta = 0.25
execute_on = timestep_end
[../]
[./vel_z]
type = NewmarkVelAux
variable = vel_z
acceleration = accel_z
gamma = 0.5
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 0
index_j = 1
[../]
[./strain_yy]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_yy
index_i = 0
index_j = 1
[../]
[]
[BCs]
[./top_y]
type = DirichletBC
variable = disp_y
boundary = top
value=0.0
[../]
[./top_x]
type = DirichletBC
variable = disp_x
boundary = top
value=0.0
[../]
[./top_z]
type = DirichletBC
variable = disp_z
boundary = top
value=0.0
[../]
[./bottom_x]
type = DirichletBC
variable = disp_x
boundary = bottom
value=0.0
[../]
[./bottom_z]
type = DirichletBC
variable = disp_z
boundary = bottom
value=0.0
[../]
[./Pressure]
[./Side1]
boundary = bottom
function = pressure
factor = 1
displacements = 'disp_x disp_y disp_z'
[../]
[../]
[]
[Materials]
[./Elasticity_tensor]
type = ComputeElasticityTensor
block = 0
fill_method = symmetric_isotropic
C_ijkl = '210e9 0'
[../]
[./strain]
type = ComputeSmallStrain
block = 0
displacements = 'disp_x disp_y disp_z'
[../]
[./stress]
type = ComputeLinearElasticStress
block = 0
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = 'density'
prop_values = '7750'
[../]
[]
[Executioner]
type = Transient
start_time = 0
end_time = 2
dt = 0.1
[]
[Functions]
[./pressure]
type = PiecewiseLinear
x = '0.0 0.1 0.2 1.0 2.0 5.0'
y = '0.0 0.1 0.2 1.0 1.0 1.0'
scale_factor = 1e9
[../]
[]
[Postprocessors]
[./_dt]
type = TimestepSize
[../]
[./disp]
type = NodalMaxValue
variable = disp_y
boundary = bottom
[../]
[./vel]
type = NodalMaxValue
variable = vel_y
boundary = bottom
[../]
[./accel]
type = NodalMaxValue
variable = accel_y
boundary = bottom
[../]
[./stress_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./strain_yy]
type = ElementAverageValue
variable = strain_yy
[../]
[]
[Outputs]
exodus = true
perf_graph = true
[]
(modules/tensor_mechanics/test/tests/scalar_material_damage/scalar_material_damage.i)
# This is a basic test of the system for continuum damage mechanics
# materials. It uses ScalarMaterialDamage for the damage model,
# which simply gets its damage index from another material. In this
# case, we prescribe the evolution of the damage index using a
# function. A single element has a fixed prescribed displacement
# on one side that puts the element in tension, and then the
# damage index evolves from 0 to 1 over time, and this verifies
# that the stress correspondingly drops to 0.
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
elem_type = HEX8
[]
[AuxVariables]
[damage_index]
order = CONSTANT
family = MONOMIAL
[]
[]
[Modules/TensorMechanics/Master]
[all]
strain = SMALL
incremental = true
add_variables = true
generate_output = 'stress_xx strain_xx'
[]
[]
[AuxKernels]
[damage_index]
type = MaterialRealAux
variable = damage_index
property = damage_index_prop
execute_on = timestep_end
[]
[]
[BCs]
[symmy]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0
[]
[symmx]
type = DirichletBC
variable = disp_x
boundary = left
value = 0
[]
[symmz]
type = DirichletBC
variable = disp_z
boundary = back
value = 0
[]
[axial_load]
type = DirichletBC
variable = disp_x
boundary = right
value = 0.01
[]
[]
[Functions]
[damage_evolution]
type = PiecewiseLinear
xy_data = '0.0 0.0
0.1 0.0
2.1 2.0'
[]
[]
[Materials]
[damage_index]
type = GenericFunctionMaterial
prop_names = damage_index_prop
prop_values = damage_evolution
[]
[damage]
type = ScalarMaterialDamage
damage_index = damage_index_prop
[]
[stress]
type = ComputeDamageStress
damage_model = damage
[]
[elasticity]
type = ComputeIsotropicElasticityTensor
poissons_ratio = 0.2
youngs_modulus = 10e9
[]
[]
[Postprocessors]
[stress_xx]
type = ElementAverageValue
variable = stress_xx
[]
[strain_xx]
type = ElementAverageValue
variable = strain_xx
[]
[damage_index]
type = ElementAverageValue
variable = damage_index
[]
[]
[Executioner]
type = Transient
l_max_its = 50
l_tol = 1e-8
nl_max_its = 20
nl_rel_tol = 1e-12
nl_abs_tol = 1e-8
dt = 0.1
dtmin = 0.1
end_time = 1.1
[]
[Outputs]
csv=true
[]
(modules/richards/test/tests/gravity_head_2/gh_lumped_08.i)
# unsaturated = true
# gravity = true
# supg = true
# transient = true
# lumped = true
[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'
viscosity = '1E-3 0.5E-3'
gravity = '-1 0 0'
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1E-2 1E-1 1E0 1E1 1E3 1E4 1E5 1E6 1E7'
x = '0 1E-1 1E0 1E1 1E2 1E3 1E4 1E5 1E6'
[../]
[]
[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 = ConstantIC
value = 1
variable = pwater
[../]
[./gas_ic]
type = ConstantIC
value = 2
variable = pgas
[../]
[]
[Kernels]
active = 'richardsfwater richardstwater richardsfgas richardstgas'
[./richardstwater]
type = RichardsLumpedMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFlux
variable = pwater
[../]
[./richardstgas]
type = RichardsLumpedMassChange
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
[../]
[./mass_error_gas]
type = FunctionValuePostprocessor
function = fcn_mass_error_g
[../]
[./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((-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'
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-10 1E-10 10000'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
end_time = 1E6
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = gh_lumped_08
csv = true
[]
(modules/tensor_mechanics/test/tests/smeared_cracking/cracking_function.i)
#
# Simple pull test for cracking. This tests the option to prescribe the
# cracking strength using an AuxVariable. In this case, an elemental
# AuxVariable is used, and a function is used to prescribe its value.
# One of the elements is weaker than the others, so the crack localizes
# in that element.
#
[Mesh]
file = plate.e
[]
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[AuxVariables]
[./cracking_stress_fn]
order = CONSTANT
family = MONOMIAL
[../]
[./crack_flags2]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./displ]
type = PiecewiseLinear
x = '0 0.1 0.2 0.3 0.4'
y = '0 0.001 0 -0.001 0'
[../]
[./fstress]
type = ParsedFunction
value = 'if(x > 0.667, 1.1e6, 1.2e6)'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx strain_xx strain_yy strain_xy strain_yz'
[../]
[]
[AuxKernels]
[./cracking_stress_fn]
type = FunctionAux
variable = cracking_stress_fn
function = fstress
execute_on = initial
[../]
[./crack_flags2]
type = MaterialRealVectorValueAux
property = crack_flags
variable = crack_flags2
component = 2
[../]
[]
[BCs]
[./pull]
type = FunctionDirichletBC
variable = disp_x
boundary = '3 4'
function = displ
[../]
[./pin_x]
type = DirichletBC
variable = disp_x
boundary = '1 2'
value = 0
[../]
[./pin_y]
type = DirichletBC
variable = disp_y
boundary = '1 4'
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 200.0e7
poissons_ratio = 0.0
[../]
[./elastic_stress]
type = ComputeSmearedCrackingStress
cracking_stress = cracking_stress_fn
softening_models = abrupt_softening
[../]
[./abrupt_softening]
type = AbruptSoftening
residual_stress = 0.0
[../]
[]
[Postprocessors]
[./elem_stress_xx]
type = ElementalVariableValue
variable = stress_xx
elementid = 2
[../]
[./elem_strain_xx]
type = ElementalVariableValue
variable = strain_xx
elementid = 2
[../]
[./elem_crack_flags_x]
type = ElementalVariableValue
variable = crack_flags2
elementid = 2
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101 '
line_search = 'none'
l_max_its = 100
nl_max_its = 100
nl_rel_tol = 1e-8
nl_abs_tol = 1e-6
l_tol = 1e-5
start_time = 0.0
end_time = 0.2
dt = 0.0025
[]
[Outputs]
exodus = true
csv = true
[]
(modules/combined/test/tests/phase_field_fracture/crack2d_computeCrackedStress_finitestrain_plastic.i)
#This input uses PhaseField-Nonconserved Action to add phase field fracture bulk rate kernels
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 40
ny = 20
ymax = 0.5
[]
[./noncrack]
type = BoundingBoxNodeSetGenerator
new_boundary = noncrack
bottom_left = '0.5 0 0'
top_right = '1 0 0'
input = gen
[../]
[]
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[AuxVariables]
[./strain_yy]
family = MONOMIAL
order = CONSTANT
[../]
[./elastic_strain_yy]
family = MONOMIAL
order = CONSTANT
[../]
[./plastic_strain_yy]
family = MONOMIAL
order = CONSTANT
[../]
[./uncracked_stress_yy]
family = MONOMIAL
order = CONSTANT
[../]
[]
[Modules]
[./TensorMechanics]
[./Master]
[./All]
add_variables = true
strain = FINITE
planar_formulation = PLANE_STRAIN
additional_generate_output = 'stress_yy vonmises_stress'
strain_base_name = uncracked
[../]
[../]
[../]
[./PhaseField]
[./Nonconserved]
[./c]
free_energy = E_el
kappa = kappa_op
mobility = L
[../]
[../]
[../]
[]
[Kernels]
[./solid_x]
type = PhaseFieldFractureMechanicsOffDiag
variable = disp_x
component = 0
c = c
[../]
[./solid_y]
type = PhaseFieldFractureMechanicsOffDiag
variable = disp_y
component = 1
c = c
[../]
[./off_disp]
type = AllenCahnElasticEnergyOffDiag
variable = c
displacements = 'disp_x disp_y'
mob_name = L
[../]
[]
[AuxKernels]
[./strain_yy]
type = RankTwoAux
variable = strain_yy
rank_two_tensor = uncracked_mechanical_strain
index_i = 1
index_j = 1
execute_on = TIMESTEP_END
[../]
[./elastic_strain_yy]
type = RankTwoAux
variable = elastic_strain_yy
rank_two_tensor = uncracked_elastic_strain
index_i = 1
index_j = 1
execute_on = TIMESTEP_END
[../]
[./plastic_strain_yy]
type = RankTwoAux
variable = plastic_strain_yy
rank_two_tensor = uncracked_plastic_strain
index_i = 1
index_j = 1
execute_on = TIMESTEP_END
[../]
[./uncracked_stress_yy]
type = RankTwoAux
variable = uncracked_stress_yy
rank_two_tensor = uncracked_stress
index_i = 1
index_j = 1
execute_on = TIMESTEP_END
[../]
[]
[BCs]
[./ydisp]
type = FunctionDirichletBC
variable = disp_y
boundary = top
function = 't'
[../]
[./yfix]
type = DirichletBC
variable = disp_y
boundary = noncrack
value = 0
[../]
[./xfix]
type = DirichletBC
variable = disp_x
boundary = right
value = 0
[../]
[]
[Functions]
[./hf]
type = PiecewiseLinear
x = '0 0.001 0.003 0.023'
y = '0.85 1.0 1.25 1.5'
[../]
[]
[Materials]
[./pfbulkmat]
type = GenericConstantMaterial
prop_names = 'gc_prop l visco'
prop_values = '1e-3 0.05 5e-3'
[../]
[./elasticity_tensor]
type = ComputeElasticityTensor
C_ijkl = '120.0 80.0'
fill_method = symmetric_isotropic
base_name = uncracked
[../]
[./isotropic_plasticity]
type = IsotropicPlasticityStressUpdate
yield_stress = 0.85
hardening_function = hf
base_name = uncracked
[../]
[./radial_return_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'isotropic_plasticity'
base_name = uncracked
[../]
[./cracked_stress]
type = ComputeCrackedStress
c = c
F_name = E_el
use_current_history_variable = true
uncracked_base_name = uncracked
finite_strain_model = true
[../]
[]
[Postprocessors]
[./av_stress_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./av_strain_yy]
type = SideAverageValue
variable = disp_y
boundary = top
[../]
[./av_uncracked_stress_yy]
type = ElementAverageValue
variable = uncracked_stress_yy
[../]
[./max_c]
type = ElementExtremeValue
variable = c
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_factor_mat_solving_package'
petsc_options_value = 'lu superlu_dist'
nl_rel_tol = 1e-8
l_tol = 1e-4
l_max_its = 100
nl_max_its = 10
dt = 2.0e-5
num_steps = 2
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/czm/czm_patch_test.i)
# Patch test for cohesive zone modeling to check convergence
[Mesh]
[./msh]
type = FileMeshGenerator
file = patch_mesh.e
[]
[./transform]
type = TransformGenerator
input = msh
transform = TRANSLATE
vector_value = '-0.5 -0.5 -0.5'
[]
[./split]
type = BreakMeshByBlockGenerator
input = transform
[]
[./add_surfaces]
type = SideSetsFromNormalsGenerator
input = split
normals = '0 0 1
0 1 0
1 0 0
0 0 -1
0 -1 0
-1 0 0'
fixed_normal = true
new_boundary = 'front top right back bottom left'
[]
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Modules]
[./TensorMechanics]
[./Master]
[./all]
strain = FINITE
add_variables = true
use_finite_deform_jacobian = true
use_automatic_differentiation = true
[../]
[../]
[../]
[]
[Functions]
[./angles]
type = PiecewiseLinear
x = '0 1'
y = '0 0'
[../]
[./stretch]
type = PiecewiseLinear
x = '0 1'
y = '0 0.01'
[../]
[./move_y]
type = ParsedFunction
value = 'y*cos(theta) - z * (1 + a)*sin(theta) - y'
vars = 'a theta'
vals = 'stretch angles'
[../]
[./move_z]
type = ParsedFunction
value = 'y*sin(theta) + z*(1+a)*cos(theta) - z'
vars = 'a theta'
vals = 'stretch angles'
[../]
[./dt_fun]
type = PiecewiseConstant
x = '0 1'
y = '0.25 0.25'
[]
[]
[BCs]
[./fix]
type = DirichletBC
preset = true
value = 0.0
boundary = left
variable = disp_x
[../]
[./front_y]
type = FunctionDirichletBC
boundary = front
variable = disp_y
function = move_y
preset = true
[../]
[./back_y]
type = FunctionDirichletBC
boundary = back
variable = disp_y
function = move_y
preset = true
[../]
[./front_z]
type = FunctionDirichletBC
boundary = front
variable = disp_z
function = move_z
preset = true
[../]
[./back_z]
type = FunctionDirichletBC
boundary = back
variable = disp_z
function = move_z
preset = true
[../]
[]
[Modules/TensorMechanics/CohesiveZoneMaster]
[./czm_ik]
boundary = 'interface'
[../]
[]
[Materials]
[./stress]
type = ADComputeFiniteStrainElasticStress
[../]
[./elasticity_tensor]
type = ADComputeElasticityTensor
fill_method = symmetric9
C_ijkl = '1.684e5 0.176e5 0.176e5 1.684e5 0.176e5 1.684e5 0.754e5 0.754e5 0.754e5'
[../]
[./czm_mat]
boundary = 'interface'
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = 'newton'
line_search = none
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
l_max_its = 2
l_tol = 1e-14
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 0.25
end_time = 1
[]
[Postprocessors]
[./nonlin]
type = NumNonlinearIterations
[../]
[]
[Outputs]
csv = true
[]
(modules/tensor_mechanics/test/tests/central_difference/lumped/2D/2d_nodalmass_explicit.i)
# One element test to test the central difference time integrator.
[Mesh]
[./generated_mesh]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 2
nx = 1
ny = 2
[../]
[./all_nodes]
type = BoundingBoxNodeSetGenerator
new_boundary = 'all'
input = 'generated_mesh'
top_right = '1 2 0'
bottom_left = '0 0 0'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./accel_x]
[../]
[./vel_x]
[../]
[./accel_y]
[../]
[./vel_y]
[../]
[]
[AuxKernels]
[./accel_x]
type = TestNewmarkTI
variable = accel_x
displacement = disp_x
first = false
[../]
[./vel_x]
type = TestNewmarkTI
variable = vel_x
displacement = disp_x
[../]
[./accel_y]
type = TestNewmarkTI
variable = accel_y
displacement = disp_y
first = false
[../]
[./vel_y]
type = TestNewmarkTI
variable = vel_y
displacement = disp_y
[../]
[]
[Kernels]
[./DynamicTensorMechanics]
displacements = 'disp_x disp_y'
[../]
[]
[BCs]
[./y_bot]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./x_bot]
type = FunctionDirichletBC
boundary = bottom
variable = disp_x
function = disp
preset = false
[../]
[]
[Functions]
[./disp]
type = PiecewiseLinear
x = '0.0 1.0 2.0 3.0 4.0' # time
y = '0.0 1.0 0.0 -1.0 0.0' # displacement
[../]
[]
[NodalKernels]
[./nodal_mass_x]
type = NodalTranslationalInertia
variable = 'disp_x'
nodal_mass_file = 'nodal_mass_file.csv'
boundary = 'all'
[../]
[./nodal_mass_y]
type = NodalTranslationalInertia
variable = 'disp_y'
nodal_mass_file = 'nodal_mass_file.csv'
boundary = 'all'
[../]
[]
[Materials]
[./elasticity_tensor_block]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.25
block = 0
[../]
[./strain_block]
type = ComputeIncrementalSmallStrain
block = 0
displacements = 'disp_x disp_y'
implicit = false
[../]
[./stress_block]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[]
[Executioner]
type = Transient
start_time = 0
end_time = 0.1
dt = 0.005
timestep_tolerance = 1e-6
[./TimeIntegrator]
type = CentralDifference
[../]
[]
[Postprocessors]
[./accel_2x]
type = PointValue
point = '1.0 2.0 0.0'
variable = accel_x
[../]
[]
[Outputs]
exodus = false
csv = true
[]
(modules/richards/test/tests/dirac/bh_lumped_07.i)
[Mesh]
type = FileMesh
file = bh07_input.e
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = DensityConstBulk
relperm_UO = RelPermPower
sat_UO = Saturation
seff_UO = Seff1VG
SUPG_UO = SUPGstandard
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1000 10000'
x = '100 1000'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1000
bulk_mod = 2E9
[../]
[./Seff1VG]
type = RichardsSeff1VG
m = 0.8
al = 1E-5
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0
sum_s_res = 0
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 1E8
[../]
[./borehole_total_outflow_mass]
type = RichardsSumQuantity
[../]
[]
[Variables]
active = 'pressure'
[./pressure]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./p_ic]
type = FunctionIC
variable = pressure
function = initial_pressure
[../]
[]
[BCs]
[./fix_outer]
type = DirichletBC
boundary = perimeter
variable = pressure
value = 1E7
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[Kernels]
active = 'richardsf richardst'
[./richardst]
type = RichardsLumpedMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[DiracKernels]
[./bh]
type = RichardsBorehole
bottom_pressure = 0
point_file = bh07.bh
SumQuantityUO = borehole_total_outflow_mass
variable = pressure
unit_weight = '0 0 0'
re_constant = 0.1594
character = 2
[../]
[]
[Postprocessors]
[./bh_report]
type = RichardsPlotQuantity
uo = borehole_total_outflow_mass
execute_on = 'initial timestep_end'
[../]
[./fluid_mass]
type = RichardsMass
variable = pressure
execute_on = 'initial timestep_end'
[../]
[]
[Functions]
[./initial_pressure]
type = ParsedFunction
value = 1E7
[../]
[]
[Materials]
[./all]
type = RichardsMaterial
block = 1
viscosity = 1E-3
mat_porosity = 0.1
mat_permeability = '1E-11 0 0 0 1E-11 0 0 0 1E-11'
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = Seff1VG
pressure_vars = pressure
[../]
[]
[Preconditioning]
[./usual]
type = SMP
full = true
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -ksp_max_it'
petsc_options_value = 'bcgs bjacobi 1E-10 1E-10 10000 30'
[../]
[]
[Executioner]
type = Transient
end_time = 1000
solve_type = NEWTON
[./TimeStepper]
# get only marginally better results for smaller time steps
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = bh_lumped_07
execute_on = 'initial timestep_end final'
interval = 10000
exodus = true
[]
(modules/tensor_mechanics/test/tests/ad_thermal_expansion_function/small_linear.i)
# This tests the thermal expansion coefficient function using both
# options to specify that function: mean and instantaneous. There
# two blocks, each containing a single element, and these use the
# two variants of the function.
# In this test, the instantaneous CTE function is a linear function
# while the mean CTE function is an analytic function designed to
# give the same response. If \bar{alpha}(T) is the mean CTE function,
# and \alpha(T) is the instantaneous CTE function,
# \bar{\alpha}(T) = 1/(T-Tref) \intA^{T}_{Tsf} \alpha(T) dT
# where Tref is the reference temperature used to define the mean CTE
# function, and Tsf is the stress-free temperature.
# This version of the test uses small deformation theory. The results
# from the two models are identical.
[Mesh]
file = 'blocks.e'
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[AuxVariables]
[./temp]
order = FIRST
family = LAGRANGE
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
add_variables = true
eigenstrain_names = eigenstrain
generate_output = 'strain_xx strain_yy strain_zz'
use_automatic_differentiation = true
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = disp_x
boundary = 3
value = 0.0
[../]
[./bottom]
type = DirichletBC
variable = disp_y
boundary = 2
value = 0.0
[../]
[./back]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0.0
[../]
[]
[AuxKernels]
[./temp]
type = FunctionAux
variable = temp
block = '1 2'
function = temp_func
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./small_stress]
type = ADComputeLinearElasticStress
[../]
[./thermal_expansion_strain1]
type = ADComputeMeanThermalExpansionFunctionEigenstrain
block = 1
thermal_expansion_function = cte_func_mean
thermal_expansion_function_reference_temperature = 0.5
stress_free_temperature = 0.0
temperature = temp
eigenstrain_name = eigenstrain
[../]
[./thermal_expansion_strain2]
type = ADComputeInstantaneousThermalExpansionFunctionEigenstrain
block = 2
thermal_expansion_function = cte_func_inst
stress_free_temperature = 0.0
temperature = temp
eigenstrain_name = eigenstrain
[../]
[]
[Functions]
[./cte_func_mean]
type = ParsedFunction
vars = 'tsf tref scale' #stress free temp, reference temp, scale factor
vals = '0.0 0.5 1e-4'
value = 'scale * (0.5 * t^2 - 0.5 * tsf^2) / (t - tref)'
[../]
[./cte_func_inst]
type = PiecewiseLinear
xy_data = '0 0.0
2 2.0'
scale_factor = 1e-4
[../]
[./temp_func]
type = PiecewiseLinear
xy_data = '0 1
1 2'
[../]
[]
[Postprocessors]
[./disp_1]
type = NodalMaxValue
variable = disp_x
boundary = 101
[../]
[./disp_2]
type = NodalMaxValue
variable = disp_x
boundary = 102
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
l_max_its = 100
l_tol = 1e-4
nl_abs_tol = 1e-8
nl_rel_tol = 1e-12
start_time = 0.0
end_time = 1.0
dt = 0.1
[]
[Outputs]
csv = true
[]
(modules/tensor_mechanics/test/tests/dynamics/prescribed_displacement/3D_QStatic_1_Ramped_Displacement_ti.i)
# One 3D element under ramped displacement loading.
#
# loading:
# time : 0.0 0.1 0.2 0.3
# disp : 0.0 0.0 -0.01 -0.01
# This displacement loading is applied using the PresetDisplacement boundary condition.
# Here, the given displacement time history is converted to an acceleration
# time history using Backward Euler time differentiation. Then, the resulting
# acceleration is integrated using Newmark time integration to obtain a
# displacement time history which is then applied to the boundary.
# This is done because if the displacement is applied using Dirichlet BC, the
# resulting acceleration is very noisy.
# Boundaries:
# x = 0 left
# x = 1 right
# y = 0 bottom
# y = 1 top
# z = 0 back
# z = 1 front
# Result: The displacement at the top node in the z direction should match
# the prescribed displacement. Also, the z acceleration should
# be two triangular pulses, one peaking at 0.1 and another peaking at
# 0.2.
[Mesh]
type = GeneratedMesh
dim = 3 # Dimension of the mesh
nx = 1 # Number of elements in the x direction
ny = 1 # Number of elements in the y direction
nz = 1 # Number of elements in the z direction
xmin = 0.0
xmax = 1
ymin = 0.0
ymax = 1
zmin = 0.0
zmax = 1
allow_renumbering = false # So NodalVariableValue can index by id
[]
[Variables] # variables that are solved
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables] # variables that are calculated for output
[./accel_x]
[../]
[./vel_x]
[../]
[./accel_y]
[../]
[./vel_y]
[../]
[./accel_z]
[../]
[./vel_z]
[../]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./DynamicTensorMechanics] # zeta*K*vel + K * disp
displacements = 'disp_x disp_y disp_z'
zeta = 0.000025
[../]
[./inertia_x] # M*accel + eta*M*vel
type = InertialForce
variable = disp_x
eta = 19.63
[../]
[./inertia_y]
type = InertialForce
variable = disp_y
eta = 19.63
[../]
[./inertia_z]
type = InertialForce
variable = disp_z
eta = 19.63
[../]
[]
[AuxKernels]
[./accel_x] # These auxkernels are only to check output
type = TestNewmarkTI
displacement = disp_x
variable = accel_x
first = false
[../]
[./accel_y]
type = TestNewmarkTI
displacement = disp_y
variable = accel_y
first = false
[../]
[./accel_z]
type = TestNewmarkTI
displacement = disp_z
variable = accel_z
first = false
[../]
[./vel_x]
type = TestNewmarkTI
displacement = disp_x
variable = vel_x
[../]
[./vel_y]
type = TestNewmarkTI
displacement = disp_y
variable = vel_y
[../]
[./vel_z]
type = TestNewmarkTI
displacement = disp_z
variable = vel_z
[../]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
[../]
[./strain_xx]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_xx
index_i = 0
index_j = 0
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
[../]
[./strain_yy]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_yy
index_i = 1
index_j = 1
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
[../]
[./strain_zz]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_zz
index_i = 2
index_j = 2
[../]
[]
[Functions]
[./displacement_front]
type = PiecewiseLinear
data_file = 'displacement.csv'
format = columns
[../]
[]
[BCs]
[./Preset_displacement]
type = PresetDisplacement
variable = disp_z
function = displacement_front
boundary = front
beta = 0.25
velocity = vel_z
acceleration = accel_z
[../]
[./anchor_x]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./anchor_y]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./anchor_z]
type = DirichletBC
variable = disp_z
boundary = back
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
youngs_modulus = 325e6 #Pa
poissons_ratio = 0.3
type = ComputeIsotropicElasticityTensor
block = 0
[../]
[./strain]
#Computes the strain, assuming small strains
type = ComputeSmallStrain
block = 0
displacements = 'disp_x disp_y disp_z'
[../]
[./stress]
#Computes the stress, using linear elasticity
type = ComputeLinearElasticStress
block = 0
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = density
prop_values = 2000 #kg/m3
[../]
[]
[Executioner]
type = Transient
start_time = 0
end_time = 3.0
l_tol = 1e-6
nl_rel_tol = 1e-6
nl_abs_tol = 1e-6
dt = 0.1
timestep_tolerance = 1e-6
# Time integrator scheme
scheme = "newmark-beta"
[]
[Postprocessors] # These quantites are printed to a csv file at every time step
[./_dt]
type = TimestepSize
[../]
[./accel_6x]
type = NodalVariableValue
nodeid = 6
variable = accel_x
[../]
[./accel_6y]
type = NodalVariableValue
nodeid = 6
variable = accel_y
[../]
[./accel_6z]
type = NodalVariableValue
nodeid = 6
variable = accel_z
[../]
[./vel_6x]
type = NodalVariableValue
nodeid = 6
variable = vel_x
[../]
[./vel_6y]
type = NodalVariableValue
nodeid = 6
variable = vel_y
[../]
[./vel_6z]
type = NodalVariableValue
nodeid = 6
variable = vel_z
[../]
[./disp_6x]
type = NodalVariableValue
nodeid = 6
variable = disp_x
[../]
[./disp_6y]
type = NodalVariableValue
nodeid = 6
variable = disp_y
[../]
[./disp_6z]
type = NodalVariableValue
nodeid = 6
variable = disp_z
[../]
[]
[Outputs]
file_base = "3D_QStatic_1_Ramped_Displacement_out"
exodus = true
csv = true
perf_graph = true
[]
(modules/tensor_mechanics/test/tests/dynamics/prescribed_displacement/3D_QStatic_1_Ramped_Displacement.i)
# One 3D element under ramped displacement loading.
#
# loading:
# time : 0.0 0.1 0.2 0.3
# disp : 0.0 0.0 -0.01 -0.01
# This displacement loading is applied using the PresetDisplacement boundary condition.
# Here, the given displacement time history is converted to an acceleration
# time history using Backward Euler time differentiation. Then, the resulting
# acceleration is integrated using Newmark time integration to obtain a
# displacement time history which is then applied to the boundary.
# This is done because if the displacement is applied using Dirichlet BC, the
# resulting acceleration is very noisy.
# Boundaries:
# x = 0 left
# x = 1 right
# y = 0 bottom
# y = 1 top
# z = 0 back
# z = 1 front
# Result: The displacement at the top node in the z direction should match
# the prescribed displacement. Also, the z acceleration should
# be two triangular pulses, one peaking at 0.1 and another peaking at
# 0.2.
[Mesh]
type = GeneratedMesh
dim = 3 # Dimension of the mesh
nx = 1 # Number of elements in the x direction
ny = 1 # Number of elements in the y direction
nz = 1 # Number of elements in the z direction
xmin = 0.0
xmax = 1
ymin = 0.0
ymax = 1
zmin = 0.0
zmax = 1
allow_renumbering = false # So NodalVariableValue can index by id
[]
[Variables] # variables that are solved
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables] # variables that are calculated for output
[./accel_x]
[../]
[./vel_x]
[../]
[./accel_y]
[../]
[./vel_y]
[../]
[./accel_z]
[../]
[./vel_z]
[../]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./DynamicTensorMechanics] # zeta*K*vel + K * disp
displacements = 'disp_x disp_y disp_z'
zeta = 0.000025
[../]
[./inertia_x] # M*accel + eta*M*vel
type = InertialForce
variable = disp_x
velocity = vel_x
acceleration = accel_x
beta = 0.25 # Newmark time integration
gamma = 0.5 # Newmark time integration
eta = 19.63
[../]
[./inertia_y]
type = InertialForce
variable = disp_y
velocity = vel_y
acceleration = accel_y
beta = 0.25
gamma = 0.5
eta = 19.63
[../]
[./inertia_z]
type = InertialForce
variable = disp_z
velocity = vel_z
acceleration = accel_z
beta = 0.25
gamma = 0.5
eta = 19.63
[../]
[]
[AuxKernels]
[./accel_x] # Calculates and stores acceleration at the end of time step
type = NewmarkAccelAux
variable = accel_x
displacement = disp_x
velocity = vel_x
beta = 0.25
execute_on = timestep_end
[../]
[./vel_x] # Calculates and stores velocity at the end of the time step
type = NewmarkVelAux
variable = vel_x
acceleration = accel_x
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_y]
type = NewmarkAccelAux
variable = accel_y
displacement = disp_y
velocity = vel_y
beta = 0.25
execute_on = timestep_end
[../]
[./vel_y]
type = NewmarkVelAux
variable = vel_y
acceleration = accel_y
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_z]
type = NewmarkAccelAux
variable = accel_z
displacement = disp_z
velocity = vel_z
beta = 0.25
execute_on = timestep_end
[../]
[./vel_z]
type = NewmarkVelAux
variable = vel_z
acceleration = accel_z
gamma = 0.5
execute_on = timestep_end
[../]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
[../]
[./strain_xx]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_xx
index_i = 0
index_j = 0
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
[../]
[./strain_yy]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_yy
index_i = 1
index_j = 1
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
[../]
[./strain_zz]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_zz
index_i = 2
index_j = 2
[../]
[]
[Functions]
[./displacement_front]
type = PiecewiseLinear
data_file = 'displacement.csv'
format = columns
[../]
[]
[BCs]
[./Preset_displacement]
type = PresetDisplacement
variable = disp_z
function = displacement_front
boundary = front
beta = 0.25
velocity = vel_z
acceleration = accel_z
[../]
[./anchor_x]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./anchor_y]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./anchor_z]
type = DirichletBC
variable = disp_z
boundary = back
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
youngs_modulus = 325e6 #Pa
poissons_ratio = 0.3
type = ComputeIsotropicElasticityTensor
block = 0
[../]
[./strain]
#Computes the strain, assuming small strains
type = ComputeSmallStrain
block = 0
displacements = 'disp_x disp_y disp_z'
[../]
[./stress]
#Computes the stress, using linear elasticity
type = ComputeLinearElasticStress
block = 0
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = density
prop_values = 2000 #kg/m3
[../]
[]
[Executioner]
type = Transient
start_time = 0
end_time = 3.0
l_tol = 1e-6
nl_rel_tol = 1e-6
nl_abs_tol = 1e-6
dt = 0.1
timestep_tolerance = 1e-6
[]
[Postprocessors] # These quantites are printed to a csv file at every time step
[./_dt]
type = TimestepSize
[../]
[./accel_6x]
type = NodalVariableValue
nodeid = 6
variable = accel_x
[../]
[./accel_6y]
type = NodalVariableValue
nodeid = 6
variable = accel_y
[../]
[./accel_6z]
type = NodalVariableValue
nodeid = 6
variable = accel_z
[../]
[./vel_6x]
type = NodalVariableValue
nodeid = 6
variable = vel_x
[../]
[./vel_6y]
type = NodalVariableValue
nodeid = 6
variable = vel_y
[../]
[./vel_6z]
type = NodalVariableValue
nodeid = 6
variable = vel_z
[../]
[./disp_6x]
type = NodalVariableValue
nodeid = 6
variable = disp_x
[../]
[./disp_6y]
type = NodalVariableValue
nodeid = 6
variable = disp_y
[../]
[./disp_6z]
type = NodalVariableValue
nodeid = 6
variable = disp_z
[../]
[]
[Outputs]
exodus = true
csv = true
perf_graph = true
[]
(modules/richards/test/tests/theis/th22.i)
# two-phase, fully-saturated
# production
[Mesh]
type = FileMesh
file = th02_input.e
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1 2 4 20'
x = '0 1 10 100'
[../]
[]
[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 = 1E-5
[../]
[./SUPGgas]
type = RichardsSUPGstandard
p_SUPG = 1E-5
[../]
[./total_outflow_mass]
type = RichardsSumQuantity
[../]
[]
[Variables]
[./pwater]
order = FIRST
family = LAGRANGE
[../]
[./pgas]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./water_ic]
type = FunctionIC
variable = pwater
function = initial_pressure
[../]
[./gas_ic]
type = FunctionIC
variable = pgas
function = initial_pressure
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[Kernels]
active = 'richardsfwater richardstwater richardsfgas richardstgas'
[./richardstwater]
type = RichardsMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFlux
variable = pwater
[../]
[./richardstgas]
type = RichardsMassChange
variable = pgas
[../]
[./richardsfgas]
type = RichardsFlux
variable = pgas
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = SeffWater
pressure_vars = 'pwater pgas'
[../]
[]
[DiracKernels]
[./bh]
type = RichardsPolyLineSink
pressures = '-1E9 1E9'
fluxes = '200 200'
point_file = th01.points
SumQuantityUO = total_outflow_mass
variable = pwater
[../]
[]
[Postprocessors]
[./flow_report]
type = RichardsPlotQuantity
uo = total_outflow_mass
[../]
[./p50]
type = PointValue
variable = pwater
point = '50 0 0'
execute_on = timestep_end
[../]
[]
[Functions]
[./initial_pressure]
type = ParsedFunction
value = 1E5
[../]
[]
[Materials]
[./all]
type = RichardsMaterial
block = 1
mat_porosity = 0.1
mat_permeability = '1E-10 0 0 0 1E-10 0 0 0 1E-10'
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]
[./usual]
type = SMP
full = true
petsc_options = '-snes_converged_reason -ksp_diagonal_scale -ksp_diagonal_scale_fix -ksp_gmres_modifiedgramschmidt -snes_linesearch_monitor'
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -sub_pc_factor_shift_type -pc_asm_overlap -snes_atol -snes_rtol -snes_max_it -ksp_rtol -ksp_atol'
petsc_options_value = 'gmres asm lu NONZERO 2 1E-7 1E-10 20 1E-10 1E-100'
[../]
[]
[Executioner]
type = Transient
end_time = 100
solve_type = NEWTON
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = th22
exodus = true
csv = true
[]
(modules/combined/test/tests/evolving_mass_density/expand_compress_test_tensors.i)
# Element mass tests
# This series of tests is designed to compute the mass of elements based on
# an evolving mass density calculation. The tests consist of expansion and compression
# of the elastic patch test model along each axis, uniform expansion and compression,
# and shear in each direction. The expansion and compression tests change the volume of
# the elements. The corresponding change in density should compensate for this so the
# mass remains constant. The shear tests should not result in a volume change, and this
# is checked too. The mass calculation is done with the post processor called Mass.
# The tests/file names are as follows:
# Expansion and compression along a single axis
# expand_compress_x_test_out.e
# expand_compress_y_test_out.e
# expand_compress_z_test_out.e
# Volumetric expansion and compression
# uniform_expand_compress_test.i
# Zero volume change shear along each axis
# shear_x_test_out.e
# shear_y_test_out.e
# shear_z_test_out.e
# The resulting mass calculation for these tests should always be = 1.
# This test is a duplicate of the uniform_expand_compress_test.i test for solid mechanics, and the
# output of this tensor mechanics test is compared to the original
# solid mechanics output. The duplication is necessary to test the
# migrated tensor mechanics version while maintaining tests for solid mechanics.
[Mesh]
file = elastic_patch.e
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
order = FIRST
family = LAGRANGE
[]
[Functions]
[./rampConstant1]
type = PiecewiseLinear
x = '0.00 1.00 2.0 3.00'
y = '0.00 0.25 0.0 -0.25'
scale_factor = 1
[../]
[] # Functions
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[Kernels]
[./TensorMechanics]
[../]
[]
[BCs]
[./bot_x]
type = DirichletBC
variable = disp_x
value = 0.0
[../]
[./bot_y]
type = DirichletBC
variable = disp_y
value = 0
[../]
[./bot_z]
type = DirichletBC
variable = disp_z
value = 0
[../]
[./top]
type = FunctionDirichletBC
preset = false
function = rampConstant1
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = '1 2 3 4 5 6 7'
youngs_modulus = 1e6
poissons_ratio = 0.0
[../]
[./small_strain]
type = ComputeSmallStrain
block = ' 1 2 3 4 5 6 7'
[../]
[./elastic_stress]
type = ComputeLinearElasticStress
block = '1 2 3 4 5 6 7'
[../]
[]
[Executioner]
type = Transient
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
nl_abs_tol = 1e-10
l_max_its = 20
start_time = 0.0
dt = 1.0
num_steps = 3
end_time = 3.0
[]
[Outputs]
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[]
[Postprocessors]
[./Mass]
type = Mass
variable = disp_x
execute_on = 'initial timestep_end'
[../]
[]
(modules/tensor_mechanics/test/tests/dynamics/rayleigh_damping/rayleigh_newmark_material_dependent.i)
# Test for rayleigh damping implemented using Newmark time integration
# The test is for an 1D bar element of unit length fixed on one end
# with a ramped pressure boundary condition applied to the other end.
# zeta and eta correspond to the stiffness and mass proportional rayleigh damping
# beta and gamma are Newmark time integration parameters
# The equation of motion in terms of matrices is:
#
# M*accel + eta*M*vel + zeta*K*vel + K*disp = P*Area
#
# Here M is the mass matrix, K is the stiffness matrix, P is the applied pressure
#
# This equation is equivalent to:
#
# density*accel + eta*density*vel + zeta*d/dt(Div stress) + Div stress = P
#
# The first two terms on the left are evaluated using the Inertial force kernel
# The next two terms on the left involving zeta are evaluated using the
# DynamicStressDivergenceTensors Kernel
# The residual due to Pressure is evaluated using Pressure boundary condition
#
# The system will come to steady state slowly after the pressure becomes constant.
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = 0.0
xmax = 0.1
ymin = 0.0
ymax = 1.0
zmin = 0.0
zmax = 0.1
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./vel_x]
[../]
[./accel_x]
[../]
[./vel_y]
[../]
[./accel_y]
[../]
[./vel_z]
[../]
[./accel_z]
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./DynamicTensorMechanics]
displacements = 'disp_x disp_y disp_z'
zeta = 'zeta_rayleigh'
[../]
[./inertia_x]
type = InertialForce
variable = disp_x
velocity = vel_x
acceleration = accel_x
beta = 0.25
gamma = 0.5
eta = 'eta_rayleigh'
[../]
[./inertia_y]
type = InertialForce
variable = disp_y
velocity = vel_y
acceleration = accel_y
beta = 0.25
gamma = 0.5
eta = 'eta_rayleigh'
[../]
[./inertia_z]
type = InertialForce
variable = disp_z
velocity = vel_z
acceleration = accel_z
beta = 0.25
gamma = 0.5
eta = 'eta_rayleigh'
[../]
[]
[AuxKernels]
[./accel_x]
type = NewmarkAccelAux
variable = accel_x
displacement = disp_x
velocity = vel_x
beta = 0.25
execute_on = timestep_end
[../]
[./vel_x]
type = NewmarkVelAux
variable = vel_x
acceleration = accel_x
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_y]
type = NewmarkAccelAux
variable = accel_y
displacement = disp_y
velocity = vel_y
beta = 0.25
execute_on = timestep_end
[../]
[./vel_y]
type = NewmarkVelAux
variable = vel_y
acceleration = accel_y
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_z]
type = NewmarkAccelAux
variable = accel_z
displacement = disp_z
velocity = vel_z
beta = 0.25
execute_on = timestep_end
[../]
[./vel_z]
type = NewmarkVelAux
variable = vel_z
acceleration = accel_z
gamma = 0.5
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 0
index_j = 1
[../]
[./strain_yy]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_yy
index_i = 0
index_j = 1
[../]
[]
[BCs]
[./top_y]
type = DirichletBC
variable = disp_y
boundary = top
value=0.0
[../]
[./top_x]
type = DirichletBC
variable = disp_x
boundary = top
value=0.0
[../]
[./top_z]
type = DirichletBC
variable = disp_z
boundary = top
value=0.0
[../]
[./bottom_x]
type = DirichletBC
variable = disp_x
boundary = bottom
value=0.0
[../]
[./bottom_z]
type = DirichletBC
variable = disp_z
boundary = bottom
value=0.0
[../]
[./Pressure]
[./Side1]
boundary = bottom
function = pressure
displacements = 'disp_x disp_y disp_z'
factor = 1
[../]
[../]
[]
[Materials]
[./Elasticity_tensor]
type = ComputeElasticityTensor
block = 0
fill_method = symmetric_isotropic
C_ijkl = '210e9 0'
[../]
[./strain]
type = ComputeSmallStrain
block = 0
displacements = 'disp_x disp_y disp_z'
[../]
[./stress]
type = ComputeLinearElasticStress
block = 0
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = 'density'
prop_values = '7750'
[../]
[./material_zeta]
type = GenericConstantMaterial
block = 0
prop_names = 'zeta_rayleigh'
prop_values = '0.1'
[../]
[./material_eta]
type = GenericConstantMaterial
block = 0
prop_names = 'eta_rayleigh'
prop_values = '0.1'
[../]
[]
[Executioner]
type = Transient
start_time = 0
end_time = 2
dt = 0.1
[]
[Functions]
[./pressure]
type = PiecewiseLinear
x = '0.0 0.1 0.2 1.0 2.0 5.0'
y = '0.0 0.1 0.2 1.0 1.0 1.0'
scale_factor = 1e9
[../]
[]
[Postprocessors]
[./_dt]
type = TimestepSize
[../]
[./disp]
type = NodalMaxValue
variable = disp_y
boundary = bottom
[../]
[./vel]
type = NodalMaxValue
variable = vel_y
boundary = bottom
[../]
[./accel]
type = NodalMaxValue
variable = accel_y
boundary = bottom
[../]
[./stress_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./strain_yy]
type = ElementAverageValue
variable = strain_yy
[../]
[]
[Outputs]
file_base = 'rayleigh_newmark_out'
exodus = true
perf_graph = true
[]
(modules/xfem/test/tests/second_order_elements/diffusion_2d_quad9.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 3
ny = 4
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD9
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.35 1.0 0.35 0.2'
time_start_cut = 0.0
time_end_cut = 2.0
[../]
[]
[Variables]
[./u]
[../]
[]
[Functions]
[./u_left]
type = PiecewiseLinear
x = '0 2'
y = '0 0.1'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = FunctionDirichletBC
variable = u
boundary = 3
function = u_left
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Transient
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
start_time = 0.0
dt = 1.0
end_time = 2.0
[]
[Outputs]
interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(test/tests/time_steppers/iteration_adaptive/piecewise_linear.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 50
ny = 2
xmax = 5
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
[./temp_spike]
type = PiecewiseLinear
x = '0 1 1.1 1.2 2'
y = '1 1 2 1 1'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./dt]
type = TimeDerivative
variable = u
[../]
[]
[BCs]
[./left]
type = FunctionDirichletBC
variable = u
boundary = left
function = temp_spike
[../]
[./right]
type = NeumannBC
variable = u
boundary = right
value = -1
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
start_time = 0.0
end_time = 2.0
verbose = true
[./TimeStepper]
type = IterationAdaptiveDT
dt = 0.9
optimal_iterations = 10
timestep_limiting_function = temp_spike
max_function_change = 0.5
[../]
[]
[Postprocessors]
[./dt]
type = TimestepSize
[../]
[]
[Outputs]
csv = 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
[]
(test/tests/geomsearch/3d_moving_penetration/pl_test2qtt.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
file = pl_test2qtt.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./normal_z]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./closest_point_z]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[./diff_z]
type = Diffusion
variable = disp_z
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
tangential_tolerance = 0.1
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
tangential_tolerance = 0.1
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = normal_z
boundary = 11
paired_boundary = 12
quantity = normal_z
[../]
[./penetrate10]
type = PenetrationAux
variable = normal_z
boundary = 12
paired_boundary = 11
quantity = normal_z
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate13]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate14]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate15]
type = PenetrationAux
variable = closest_point_z
boundary = 11
paired_boundary = 12
quantity = closest_point_z
[../]
[./penetrate16]
type = PenetrationAux
variable = closest_point_z
boundary = 12
paired_boundary = 11
quantity = closest_point_z
[../]
[./penetrate17]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate18]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate19]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate20]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b1z]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[./b2z]
type = DirichletBC
variable = disp_z
boundary = 2
value = 0
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 0.7 -0.7 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-9
l_max_its = 10
start_time = 0.0
dt = 0.06
end_time = 1.0
[./Quadrature]
order = THIRD
[../]
[]
[Outputs]
file_base = pl_test2qtt_out
exodus = true
[]
(modules/tensor_mechanics/test/tests/truss/truss_3d.i)
[Mesh]
type = FileMesh
file = truss_3d.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./axial_stress]
order = CONSTANT
family = MONOMIAL
[../]
[./e_over_l]
order = CONSTANT
family = MONOMIAL
[../]
[./area]
order = CONSTANT
family = MONOMIAL
# initial_condition = 1.0
[../]
[./react_x]
order = FIRST
family = LAGRANGE
[../]
[./react_y]
order = FIRST
family = LAGRANGE
[../]
[./react_z]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
[./x2]
type = PiecewiseLinear
x = '0 1 2 3'
y = '0 .5 1 1'
[../]
[./y2]
type = PiecewiseLinear
x = '0 1 2 3'
y = '0 0 .5 1'
[../]
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
preset = false
boundary = 1
value = 0.0
[../]
[./fixx2]
type = FunctionDirichletBC
variable = disp_x
preset = false
boundary = 2
function = x2
[../]
[./fixx3]
type = DirichletBC
variable = disp_x
preset = false
boundary = 3
value = 0.0
[../]
[./fixy1]
type = DirichletBC
variable = disp_y
preset = false
boundary = 1
value = 0
[../]
[./fixy2]
type = FunctionDirichletBC
variable = disp_y
preset = false
boundary = 2
function = y2
[../]
[./fixy3]
type = DirichletBC
variable = disp_y
preset = false
boundary = 3
value = 0
[../]
[./fixz1]
type = DirichletBC
variable = disp_z
preset = false
boundary = 1
value = 0
[../]
[./fixz2]
type = DirichletBC
variable = disp_z
preset = false
boundary = 2
value = 0
[../]
[./fixz3]
type = DirichletBC
variable = disp_z
preset = false
boundary = 3
value = 0
[../]
[]
[AuxKernels]
[./axial_stress]
type = MaterialRealAux
block = '1 2'
property = axial_stress
variable = axial_stress
[../]
[./e_over_l]
type = MaterialRealAux
block = '1 2'
property = e_over_l
variable = e_over_l
[../]
[./area]
type = ConstantAux
block = '1 2'
variable = area
value = 1.0
execute_on = 'initial timestep_begin'
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
petsc_options_iname = '-pc_type -ksp_gmres_restart'
petsc_options_value = 'jacobi 101'
line_search = 'none'
nl_max_its = 15
nl_rel_tol = 1e-6
nl_abs_tol = 1e-10
dt = 1
num_steps = 3
end_time = 3
[]
[Kernels]
[./solid_x]
type = StressDivergenceTensorsTruss
block = '1 2'
displacements = 'disp_x disp_y disp_z'
component = 0
variable = disp_x
area = area
save_in = react_x
[../]
[./solid_y]
type = StressDivergenceTensorsTruss
block = '1 2'
displacements = 'disp_x disp_y disp_z'
component = 1
variable = disp_y
area = area
save_in = react_y
[../]
[./solid_z]
type = StressDivergenceTensorsTruss
block = '1 2'
displacements = 'disp_x disp_y disp_z'
component = 2
variable = disp_z
area = area
save_in = react_z
[../]
[]
[Materials]
[./linelast]
type = LinearElasticTruss
block = '1 2'
youngs_modulus = 1e6
displacements = 'disp_x disp_y disp_z'
[../]
[]
[Outputs]
exodus = true
[]
(modules/contact/test/tests/normalized_penalty/normalized_penalty_Q8.i)
[GlobalParams]
order = SECOND
displacements = 'disp_x disp_y'
[]
[Mesh]
file = normalized_penalty_Q8.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Functions]
[./left_x]
type = PiecewiseLinear
x = '0 1 2'
y = '0 0.02 0'
[../]
[]
[AuxVariables]
[./saved_x]
[../]
[./saved_y]
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = FINITE
generate_output = 'stress_xx'
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
[]
[]
[Contact]
[./m3_s2]
primary = 3
secondary = 2
penalty = 1e10
normalize_penalty = true
formulation = penalty
tangential_tolerance = 1e-3
[../]
[]
[BCs]
[./left_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 1
function = left_x
[../]
[./y]
type = DirichletBC
variable = disp_y
boundary = '1 2 3 4'
value = 0.0
[../]
[./right]
type = DirichletBC
variable = disp_x
boundary = '3 4'
value = 0
[../]
[]
[Materials]
[./stiffStuff1]
type = ComputeIsotropicElasticityTensor
block = '1 2 3 4 1000'
youngs_modulus = 3e8
poissons_ratio = 0.0
[../]
[./stiffStuff1_stress]
type = ComputeFiniteStrainElasticStress
block = '1 2 3 4 1000'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -ksp_gmres_restart'
petsc_options_value = 'lu 101'
line_search = 'none'
nl_rel_tol = 1e-12
nl_abs_tol = 5e-8
l_max_its = 100
nl_max_its = 10
dt = 0.5
num_steps = 4
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/1D_axisymmetric/axisymmetric_gps_finite.i)
#
# This test checks the generalized plane strain using finite strain formulation.
# since we constrain all the nodes against movement and the applied thermal strain
# is very small, the results are the same as small and incremental small strain formulations
#
[GlobalParams]
displacements = disp_x
scalar_out_of_plane_strain = scalar_strain_yy
[]
[Problem]
coord_type = RZ
[]
[Mesh]
file = lines.e
[]
[Variables]
[./disp_x]
[../]
[./temp]
initial_condition = 580.0
[../]
[./scalar_strain_yy]
order = FIRST
family = SCALAR
[../]
[]
[Functions]
[./temp100]
type = PiecewiseLinear
x = '0 1'
y = '580 680'
[../]
[./temp300]
type = PiecewiseLinear
x = '0 1'
y = '580 880'
[../]
[]
[Kernels]
[./heat]
type = Diffusion
variable = temp
[../]
[]
[Modules]
[./TensorMechanics]
[./Master]
[./gps]
planar_formulation = GENERALIZED_PLANE_STRAIN
scalar_out_of_plane_strain = scalar_strain_yy
strain = FINITE
generate_output = 'strain_xx strain_yy strain_zz stress_xx stress_yy stress_zz'
eigenstrain_names = eigenstrain
[../]
[../]
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
boundary = 1000
value = 0
variable = disp_x
[../]
[./temp100]
type = FunctionDirichletBC
variable = temp
function = temp100
boundary = 2
[../]
[./temp300]
type = FunctionDirichletBC
variable = temp
function = temp300
boundary = 3
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 3600
poissons_ratio = 0.2
[../]
[./thermal_strain]
type = ComputeThermalExpansionEigenstrain
thermal_expansion_coeff = 1e-8
temperature = temp
stress_free_temperature = 580
eigenstrain_name = eigenstrain
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
line_search = 'none'
l_max_its = 50
l_tol = 1e-08
nl_max_its = 15
nl_abs_tol = 1e-10
start_time = 0
end_time = 1
num_steps = 1
[]
[Outputs]
exodus = true
console = true
[]
(modules/tensor_mechanics/test/tests/beam/dynamic/dyn_euler_small_added_mass_inertia_damping_ti.i)
# Test for small strain euler beam vibration in y direction
# An impulse load is applied at the end of a cantilever beam of length 4m.
# The beam is massless with a lumped mass at the end of the beam. The lumped
# mass also has a moment of inertia associated with it.
# The properties of the cantilever beam are as follows:
# Young's modulus (E) = 1e4
# Shear modulus (G) = 4e7
# Shear coefficient (k) = 1.0
# Cross-section area (A) = 0.01
# Iy = 1e-4 = Iz
# Length (L)= 4 m
# mass (m) = 0.01899772
# Moment of inertia of lumped mass:
# Ixx = 0.2
# Iyy = 0.1
# Izz = 0.1
# mass proportional damping coefficient (eta) = 0.1
# For this beam, the dimensionless parameter alpha = kAGL^2/EI = 6.4e6
# Therefore, the beam behaves like a Euler-Bernoulli beam.
# The displacement time history from this analysis matches with that obtained from Abaqus.
# Values from the first few time steps are as follows:
# time disp_y vel_y accel_y
# 0.0 0.0 0.0 0.0
# 0.1 0.001278249649738 0.025564992994761 0.51129985989521
# 0.2 0.0049813090917644 0.048496195845768 -0.052675802875074
# 0.3 0.0094704658873002 0.041286940064947 -0.091509312741339
# 0.4 0.013082280729802 0.03094935678508 -0.115242352856
# 0.5 0.015588313103503 0.019171290688959 -0.12031896906642
[Mesh]
type = GeneratedMesh
dim = 1
nx = 10
xmin = 0.0
xmax = 4.0
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[./rot_x]
order = FIRST
family = LAGRANGE
[../]
[./rot_y]
order = FIRST
family = LAGRANGE
[../]
[./rot_z]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./vel_x]
order = FIRST
family = LAGRANGE
[../]
[./vel_y]
order = FIRST
family = LAGRANGE
[../]
[./vel_z]
order = FIRST
family = LAGRANGE
[../]
[./accel_x]
order = FIRST
family = LAGRANGE
[../]
[./accel_y]
order = FIRST
family = LAGRANGE
[../]
[./accel_z]
order = FIRST
family = LAGRANGE
[../]
[./rot_vel_x]
order = FIRST
family = LAGRANGE
[../]
[./rot_vel_y]
order = FIRST
family = LAGRANGE
[../]
[./rot_vel_z]
order = FIRST
family = LAGRANGE
[../]
[./rot_accel_x]
order = FIRST
family = LAGRANGE
[../]
[./rot_accel_y]
order = FIRST
family = LAGRANGE
[../]
[./rot_accel_z]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./accel_x] # These auxkernels are only to check output
type = TestNewmarkTI
displacement = disp_x
variable = accel_x
first = false
[../]
[./accel_y]
type = TestNewmarkTI
displacement = disp_y
variable = accel_y
first = false
[../]
[./accel_z]
type = TestNewmarkTI
displacement = disp_z
variable = accel_z
first = false
[../]
[./vel_x]
type = TestNewmarkTI
displacement = disp_x
variable = vel_x
[../]
[./vel_y]
type = TestNewmarkTI
displacement = disp_y
variable = vel_y
[../]
[./vel_z]
type = TestNewmarkTI
displacement = disp_z
variable = vel_z
[../]
[./rot_accel_x]
type = TestNewmarkTI
displacement = rot_x
variable = rot_accel_x
first = false
[../]
[./rot_accel_y]
type = TestNewmarkTI
displacement = rot_y
variable = rot_accel_y
first = false
[../]
[./rot_accel_z]
type = TestNewmarkTI
displacement = rot_z
variable = rot_accel_z
first = false
[../]
[./rot_vel_x]
type = TestNewmarkTI
displacement = rot_x
variable = rot_vel_x
[../]
[./rot_vel_y]
type = TestNewmarkTI
displacement = rot_y
variable = rot_vel_y
[../]
[./rot_vel_z]
type = TestNewmarkTI
displacement = rot_z
variable = rot_vel_z
[../]
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./fixy1]
type = DirichletBC
variable = disp_y
boundary = left
value = 0.0
[../]
[./fixz1]
type = DirichletBC
variable = disp_z
boundary = left
value = 0.0
[../]
[./fixr1]
type = DirichletBC
variable = rot_x
boundary = left
value = 0.0
[../]
[./fixr2]
type = DirichletBC
variable = rot_y
boundary = left
value = 0.0
[../]
[./fixr3]
type = DirichletBC
variable = rot_z
boundary = left
value = 0.0
[../]
[]
[NodalKernels]
[./force_y2]
type = UserForcingFunctionNodalKernel
variable = disp_y
boundary = right
function = force
[../]
[./x_inertial]
type = NodalTranslationalInertia
variable = disp_x
boundary = right
mass = 0.01899772
eta = 0.1
[../]
[./y_inertial]
type = NodalTranslationalInertia
variable = disp_y
boundary = right
mass = 0.01899772
eta = 0.1
[../]
[./z_inertial]
type = NodalTranslationalInertia
variable = disp_z
boundary = right
mass = 0.01899772
eta = 0.1
[../]
[./rot_x_inertial]
type = NodalRotationalInertia
variable = rot_x
rotations = 'rot_x rot_y rot_z'
boundary = right
Ixx = 2e-1
Iyy = 1e-1
Izz = 1e-1
eta = 0.1
component = 0
[../]
[./rot_y_inertial]
type = NodalRotationalInertia
variable = rot_y
rotations = 'rot_x rot_y rot_z'
boundary = right
Ixx = 2e-1
Iyy = 1e-1
Izz = 1e-1
eta = 0.1
component = 1
[../]
[./rot_z_inertial]
type = NodalRotationalInertia
variable = rot_z
rotations = 'rot_x rot_y rot_z'
boundary = right
Ixx = 2e-1
Iyy = 1e-1
Izz = 1e-1
eta = 0.1
component = 2
[../]
[]
[Functions]
[./force]
type = PiecewiseLinear
x = '0.0 0.1 0.2 10.0'
y = '0.0 1e-2 0.0 0.0'
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options_iname = '-ksp_type -pc_type'
petsc_options_value = 'preonly lu'
start_time = 0.0
dt = 0.1
end_time = 5.0
timestep_tolerance = 1e-6
# Time integrator scheme
scheme = "newmark-beta"
[]
[Kernels]
[./solid_disp_x]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 0
variable = disp_x
[../]
[./solid_disp_y]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 1
variable = disp_y
[../]
[./solid_disp_z]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 2
variable = disp_z
[../]
[./solid_rot_x]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 3
variable = rot_x
[../]
[./solid_rot_y]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 4
variable = rot_y
[../]
[./solid_rot_z]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 5
variable = rot_z
[../]
[]
[Materials]
[./elasticity]
type = ComputeElasticityBeam
youngs_modulus = 1.0e4
poissons_ratio = -0.999875
shear_coefficient = 1.0
block = 0
[../]
[./strain]
type = ComputeIncrementalBeamStrain
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
area = 0.01
Ay = 0.0
Az = 0.0
Iy = 1.0e-4
Iz = 1.0e-4
y_orientation = '0.0 1.0 0.0'
[../]
[./stress]
type = ComputeBeamResultants
block = 0
[../]
[]
[Postprocessors]
[./disp_x]
type = PointValue
point = '4.0 0.0 0.0'
variable = disp_x
[../]
[./disp_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = disp_y
[../]
[./vel_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = vel_y
[../]
[./accel_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = accel_y
[../]
[]
[Outputs]
file_base = "dyn_euler_small_added_mass_inertia_damping_out"
exodus = true
csv = true
perf_graph = true
[]
(test/tests/time_integrators/newmark-beta/newmark_beta_default_parameters.i)
###########################################################
# This is a simple test with a time-dependent problem
# demonstrating the use of the TimeIntegrator system.
#
# Testing that the first and second time derivatives
# are calculated correctly using the Newmark-Beta method
#
# @Requirement F1.30
###########################################################
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 1
ny = 1
[]
[Variables]
[./u]
[../]
[]
[Functions]
[./forcing_fn]
type = PiecewiseLinear
x = '0.0 0.1 0.2 0.3 0.4 0.5 0.6'
y = '0.0 0.0 0.0025 0.01 0.0175 0.02 0.02'
[../]
[]
[Kernels]
[./ie]
type = TimeDerivative
variable = u
[../]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = FunctionDirichletBC
variable = u
preset = false
boundary = 'left'
function = forcing_fn
[../]
[./right]
type = FunctionDirichletBC
variable = u
preset = false
boundary = 'right'
function = forcing_fn
[../]
[]
[Executioner]
type = Transient
# Time integrator scheme
scheme = "newmark-beta"
start_time = 0.0
num_steps = 6
dt = 0.1
[]
[Postprocessors]
[./udot]
type = ElementAverageTimeDerivative
variable = u
[../]
[./udotdot]
type = ElementAverageSecondTimeDerivative
variable = u
[../]
[./u]
type = ElementAverageValue
variable = u
[../]
[]
[Outputs]
csv = true
[]
(modules/tensor_mechanics/test/tests/ad_anisotropic_elastoplasticity/ad_aniso_plasticity_x_one.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
nx = 10
ny = 2
nz = 2
xmin = 0.0
ymin = 0.0
zmin = 0.0
xmax = 10.0
ymax = 1.0
zmax = 1.0
[]
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[AuxVariables]
[hydrostatic_stress]
order = CONSTANT
family = MONOMIAL
[]
[plastic_strain_xx]
order = CONSTANT
family = MONOMIAL
[]
[plastic_strain_xy]
order = CONSTANT
family = MONOMIAL
[]
[plastic_strain_yy]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[hydrostatic_stress]
type = ADRankTwoScalarAux
variable = hydrostatic_stress
rank_two_tensor = stress
scalar_type = Hydrostatic
[]
[plasticity_strain_xx]
type = ADRankTwoAux
rank_two_tensor = plastic_strain
variable = plastic_strain_xx
index_i = 0
index_j = 0
[]
[plasticity_strain_xy]
type = ADRankTwoAux
rank_two_tensor = plastic_strain
variable = plastic_strain_xy
index_i = 0
index_j = 1
[]
[plasticity_strain_yy]
type = ADRankTwoAux
rank_two_tensor = plastic_strain
variable = plastic_strain_yy
index_i = 1
index_j = 1
[]
[sigma_xx]
type = ADRankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 1
index_j = 1
[]
[]
[Functions]
[pull]
type = PiecewiseLinear
x = '0 1e1 1e8'
y = '0 -4e2 -4e2'
[]
[]
[Modules/TensorMechanics/Master]
[all]
strain = FINITE
generate_output = 'elastic_strain_xx stress_xx'
use_automatic_differentiation = true
add_variables = true
[]
[]
[Materials]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 70000
poissons_ratio = 0.25
[]
[elastic_strain]
type = ADComputeMultipleInelasticStress
inelastic_models = "trial_plasticity"
max_iterations = 50
absolute_tolerance = 1e-16
[]
[trial_plasticity]
type = ADHillElastoPlasticityStressUpdate
hardening_constant = 2000.0
yield_stress = 0.001 # was 200 for verification
# F G H L M N
hill_constants = "0.5829856 0.364424 0.6342174 2.0691375 2.3492325 1.814589"
absolute_tolerance = 1e-15
relative_tolerance = 1e-13
# internal_solve_full_iteration_history = true
max_inelastic_increment = 2.0e-6
# internal_solve_output_on = on_error
[]
[]
[BCs]
[no_disp_x]
type = ADDirichletBC
variable = disp_x
boundary = left
value = 0.0
[]
[no_disp_y]
type = ADDirichletBC
variable = disp_y
boundary = left
value = 0.0
[]
[no_disp_z]
type = ADDirichletBC
variable = disp_z
boundary = left
value = 0.0
[]
[Pressure]
[Side1]
boundary = right
function = pull
[]
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
nl_rel_tol = 1e-12
nl_abs_tol = 1.0e-14
l_max_its = 90
num_steps = 25
[TimeStepper]
type = IterationAdaptiveDT
optimal_iterations = 30
iteration_window = 9
growth_factor = 1.05
cutback_factor = 0.5
timestep_limiting_postprocessor = matl_ts_min
dt = 1.0e-5
time_t = '0 3.4e-5 10'
time_dt = '1.0e-5 1.0e-7 1.0e-7'
[]
start_time = 0
automatic_scaling = true
[]
[Postprocessors]
[matl_ts_min]
type = MaterialTimeStepPostprocessor
[]
[max_disp_x]
type = ElementExtremeValue
variable = disp_x
[]
[max_hydro]
type = ElementAverageValue
variable = hydrostatic_stress
[]
[dt]
type = TimestepSize
[]
[plasticity_strain_xx]
type = ElementalVariableValue
variable = plastic_strain_xx
execute_on = 'TIMESTEP_END'
elementid = 0
[]
[elastic_strain_xx]
type = ElementalVariableValue
variable = elastic_strain_xx
execute_on = 'TIMESTEP_END'
elementid = 0
[]
[sigma_xx]
type = ElementalVariableValue
variable = stress_xx
execute_on = 'TIMESTEP_END'
elementid = 0
[]
[]
[Outputs]
csv = true
exodus = true
perf_graph = true
[]
(modules/richards/test/tests/buckley_leverett/bl20.i)
# two-phase version
[Mesh]
type = GeneratedMesh
dim = 1
nx = 30
xmin = 0
xmax = 15
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '0.1 0.5 0.5 1 2 4'
x = '0 0.1 1 5 40 42'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = 'pwater pgas'
[../]
[./DensityWater]
type = RichardsDensityConstBulk
dens0 = 1000
bulk_mod = 2E6
[../]
[./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 = 2
[../]
[./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 = 1E-5
[../]
[./SUPGgas]
type = RichardsSUPGstandard
p_SUPG = 1E-5
[../]
[]
[Variables]
[./pwater]
order = FIRST
family = LAGRANGE
[../]
[./pgas]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[./bounds_dummy]
[../]
[]
[Kernels]
active = 'richardsfwater richardstwater richardsfgas richardstgas'
[./richardstwater]
type = RichardsMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFlux
variable = pwater
[../]
[./richardstgas]
type = RichardsMassChange
variable = pgas
[../]
[./richardsfgas]
type = RichardsFlux
variable = pgas
[../]
[./richardsppenalty]
type = RichardsPPenalty
variable = pgas
a = 1E-18
lower_var = pwater
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = SeffWater
pressure_vars = 'pwater pgas'
[../]
[]
[Bounds]
[./pwater_upper_bounds]
type = ConstantBoundsAux
variable = bounds_dummy
bounded_variable = pwater
bound_type = upper
bound_value = 1E7
[../]
[./pwater_lower_bounds]
type = ConstantBoundsAux
variable = bounds_dummy
bounded_variable = pwater
bound_type = lower
bound_value = -310000
[../]
[]
[ICs]
[./water_ic]
type = FunctionIC
variable = pwater
function = initial_water
[../]
[./gas_ic]
type = FunctionIC
variable = pgas
function = initial_gas
[../]
[]
[BCs]
[./left_w]
type = DirichletBC
variable = pwater
boundary = left
value = 1E6
[../]
[./left_g]
type = DirichletBC
variable = pgas
boundary = left
value = 1E6
[../]
[./right_w]
type = DirichletBC
variable = pwater
boundary = right
value = -300000
[../]
[./right_g]
type = DirichletBC
variable = pgas
boundary = right
value = 0
[../]
[]
[Functions]
[./initial_water]
type = ParsedFunction
value = 1000000*(1-min(x/5,1))-300000*(max(x-5,0)/max(abs(x-5),1E-10))
[../]
[./initial_gas]
type = ParsedFunction
value = max(1000000*(1-x/5),0)+1000
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.15
mat_permeability = '1E-10 0 0 0 1E-10 0 0 0 1E-10'
density_UO = 'DensityWater DensityGas'
relperm_UO = 'RelPermWater RelPermGas'
SUPG_UO = 'SUPGwater SUPGgas'
sat_UO = 'SatWater SatGas'
seff_UO = 'SeffWater SeffGas'
viscosity = '1E-3 1E-6'
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
active = 'standard'
[./bounded]
# must use --use-petsc-dm command line argument
type = SMP
full = true
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -snes_type -ksp_rtol -ksp_atol'
petsc_options_value = 'bcgs bjacobi 1E-10 1E-10 50 vinewtonssls 1E-20 1E-20'
[../]
[./standard]
type = SMP
full = true
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -sub_pc_factor_shift_type -snes_atol -snes_rtol -snes_max_it -ksp_rtol -ksp_atol'
petsc_options_value = 'gmres asm lu NONZERO 1E-10 1E-10 20 1E-20 1E-20'
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
end_time = 50
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = bl20
execute_on = 'initial timestep_end final'
interval = 10000
exodus = true
hide = pgas
[]
(modules/contact/test/tests/hertz_spherical/hertz_contact_hex20.i)
# Hertz Contact: Sphere on sphere
# Spheres have the same radius, Young's modulus, and Poisson's ratio.
# Define E:
# 1/E = (1-nu1^2)/E1 + (1-nu2^2)/E2
#
# Effective radius R:
# 1/R = 1/R1 + 1/R2
#
# F is the applied compressive load.
#
# Area of contact a::
# a^3 = 3FR/4E
#
# Depth of indentation d:
# d = a^2/R
#
#
# Let R1 = R2 = 2. Then R = 1.
#
# Let nu1 = nu2 = 0.25, E1 = E2 = 1.40625e7. Then E = 7.5e6.
#
# Let F = 10000. Then a = 0.1, d = 0.01.
#
[GlobalParams]
volumetric_locking_correction = false
displacements = 'disp_x disp_y disp_z'
order = SECOND
[]
[Mesh]#Comment
file = hertz_contact_hex20.e
allow_renumbering = false
[] # Mesh
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Functions]
[./pressure]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 1.'
scale_factor = 795.77471545947674 # 10000/pi/2^2
[../]
[./disp_y]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. -0.01 -0.01'
[../]
[] # Functions
[Variables]
[./disp_x]
order = SECOND
family = LAGRANGE
[../]
[./disp_y]
order = SECOND
family = LAGRANGE
[../]
[./disp_z]
order = SECOND
family = LAGRANGE
[../]
[] # Variables
[AuxVariables]
[./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_zx]
order = CONSTANT
family = MONOMIAL
[../]
[./vonmises]
order = CONSTANT
family = MONOMIAL
[../]
[./hydrostatic]
order = CONSTANT
family = MONOMIAL
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./saved_z]
[../]
[] # AuxVariables
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = SMALL
extra_vector_tags = 'ref'
save_in = 'saved_x saved_y saved_z'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 0
variable = stress_xx
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 1
variable = stress_yy
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 2
variable = stress_zz
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 1
variable = stress_xy
[../]
[./stress_yz]
type = RankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 2
variable = stress_yz
[../]
[./stress_zx]
type = RankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 0
variable = stress_zx
[../]
# [./vonmises]
# type = RankTwoScalarAux
# rank_two_tensor = stress
# variable = vonmises
# scalar_type = VonMisesStress
# [../]
[] # AuxKernels
[BCs]
[./base_x]
type = DirichletBC
variable = disp_x
boundary = 1000
value = 0.0
[../]
[./base_y]
type = DirichletBC
variable = disp_y
boundary = 1000
value = 0.0
[../]
[./base_z]
type = DirichletBC
variable = disp_z
boundary = 1000
value = 0.0
[../]
[./symm_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./symm_z]
type = DirichletBC
variable = disp_z
boundary = 3
value = 0.0
[../]
[./disp_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[] # BCs
[Contact]
[./dummy_name]
primary = 1000
secondary = 100
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+10
[../]
[]
#[Dampers]
# [./contact_slip]
# type = ContactSlipDamper
# primary = 1000
# secondary = 100
# [../]
#[]
[Materials]
[./tensor]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1.40625e7
poissons_ratio = 0.25
[../]
[./stress]
type = ComputeLinearElasticStress
block = '1'
[../]
[./tensor_1000]
type = ComputeIsotropicElasticityTensor
block = '1000'
youngs_modulus = 1e6
poissons_ratio = 0.0
[../]
[./stress_1000]
type = ComputeLinearElasticStress
block = '1000'
[../]
[] # Materials
[Preconditioning]
[./SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-7
l_max_its = 10
start_time = 0.0
dt = 0.05
end_time = 2.0
[./Quadrature]
order = THIRD
[../]
[] # Executioner
[Postprocessors]
[./maxdisp]
type = NodalVariableValue
nodeid = 386 # 387-1 where 387 is the exodus node number of the top-center node
variable = disp_y
[../]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 2
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 2
[../]
[./bot_react_z]
type = NodalSum
variable = saved_z
boundary = 2
[../]
[]
[Outputs]
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[] # Outputs
(modules/richards/test/tests/theis/th_lumped_01.i)
# fully-saturated
# production
# lumped
[Mesh]
type = FileMesh
file = th01_input.e
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = DensityConstBulk
relperm_UO = RelPermPower
sat_UO = Saturation
seff_UO = Seff1VG
SUPG_UO = SUPGstandard
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '0.5 1 2 10'
x = '0 1 10 100'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1000
bulk_mod = 2E9
[../]
[./Seff1VG]
type = RichardsSeff1VG
m = 0.8
al = 1E-5
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0
sum_s_res = 0
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 1E-5
[../]
[./total_outflow_mass]
type = RichardsSumQuantity
[../]
[]
[Variables]
active = 'pressure'
[./pressure]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./p_ic]
type = FunctionIC
variable = pressure
function = initial_pressure
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[Kernels]
active = 'richardsf richardst'
[./richardst]
type = RichardsLumpedMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[DiracKernels]
[./bh]
type = RichardsPolyLineSink
pressures = '-1E9 1E9'
fluxes = '200 200'
point_file = th01.points
SumQuantityUO = total_outflow_mass
variable = pressure
[../]
[]
[Postprocessors]
[./flow_report]
type = RichardsPlotQuantity
uo = total_outflow_mass
[../]
[./p50]
type = PointValue
variable = pressure
point = '50 0 0'
execute_on = timestep_end
[../]
[]
[Functions]
[./initial_pressure]
type = ParsedFunction
value = 1E5
[../]
[]
[Materials]
[./all]
type = RichardsMaterial
block = 1
viscosity = 1E-3
mat_porosity = 0.1
mat_permeability = '1E-10 0 0 0 1E-10 0 0 0 1E-10'
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = Seff1VG
pressure_vars = pressure
[../]
[]
[Preconditioning]
[./usual]
type = SMP
full = true
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -ksp_max_it'
petsc_options_value = 'bcgs bjacobi 1E-6 1E-10 10000 30'
[../]
[]
[Executioner]
type = Transient
end_time = 100
solve_type = NEWTON
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = th_lumped_01
csv = true
[]
(modules/tensor_mechanics/test/tests/volumetric_eigenstrain/volumetric_mechanical.i)
# This test ensures that the reported volumetric strain for a cube with
# mechanically imposed displacements (through Dirichlet BCs) exactly
# matches that from a version of this test that experiences the same
# defomation, but due to imposed eigenstrains.
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./volumetric_strain]
order = CONSTANT
family = MONOMIAL
[../]
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
decomposition_method = EigenSolution #Necessary for exact solution
[../]
[]
[AuxKernels]
[./volumetric_strain]
type = RankTwoScalarAux
scalar_type = VolumetricStrain
rank_two_tensor = total_strain
variable = volumetric_strain
[../]
[]
[Functions]
[pres_disp]
type = PiecewiseLinear
# These values are taken from the displacements in the eigenstrain
# version of this test. The volume of the cube (which starts out as
# a 1x1x1 cube) is (1 + disp)^3. At time 2, this is
# (1.44224957030741)^3, which is 3.0.
xy_data = '0 0
1 0.25992104989487
2 0.44224957030741'
[]
[]
[BCs]
[./left]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./bottom]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./back]
type = DirichletBC
variable = disp_z
boundary = back
value = 0.0
[../]
[./right]
type = FunctionDirichletBC
variable = disp_x
boundary = right
function = pres_disp
[../]
[./top]
type = FunctionDirichletBC
variable = disp_y
boundary = top
function = pres_disp
[../]
[./front]
type = FunctionDirichletBC
variable = disp_z
boundary = front
function = pres_disp
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./finite_strain_stress]
type = ComputeFiniteStrainElasticStress
[../]
[./volumetric_change]
type = GenericFunctionMaterial
prop_names = volumetric_change
prop_values = t
[../]
[]
[Postprocessors]
[./vol]
type = VolumePostprocessor
use_displaced_mesh = true
execute_on = 'initial timestep_end'
[../]
[./volumetric_strain]
type = ElementalVariableValue
variable = volumetric_strain
elementid = 0
[../]
[./disp_right]
type = NodalMaxValue
variable = disp_x
boundary = right
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
l_max_its = 100
l_tol = 1e-4
nl_abs_tol = 1e-8
nl_rel_tol = 1e-12
start_time = 0.0
end_time = 2.0
dt = 1.0
[]
[Outputs]
exodus = true
csv = true
[]
(modules/tensor_mechanics/test/tests/ad_smeared_cracking/cracking_power.i)
#
# Simple test of power law softening law for smeared cracking.
# Upon reaching the failure stress in the x direction, the
# softening model abruptly reduces the stress to a fraction
# of its original value, and re-loading occurs at a reduced
# stiffness. This is repeated multiple times.
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Functions]
[./displ]
type = PiecewiseLinear
x = '0 1 2 3 4'
y = '0 1 0 -1 0'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx'
use_automatic_differentiation = true
[../]
[]
[BCs]
[./pull]
type = ADFunctionDirichletBC
variable = disp_x
boundary = right
function = displ
[../]
[./left]
type = ADDirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./bottom]
type = ADDirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./back]
type = ADDirichletBC
variable = disp_z
boundary = back
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 2.8e7
poissons_ratio = 0
[../]
[./elastic_stress]
type = ADComputeSmearedCrackingStress
cracking_stress = 1.68e6
softening_models = power_law_softening
[../]
[./power_law_softening]
type = ADPowerLawSoftening
stiffness_reduction = 0.3333
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
petsc_options_iname = '-ksp_gmres_restart -pc_type -sub_pc_type'
petsc_options_value = '101 asm lu'
line_search = 'none'
l_max_its = 100
nl_max_its = 100
nl_rel_tol = 1e-8
nl_abs_tol = 1e-8
l_tol = 1e-5
start_time = 0.0
end_time = 1.0
dt = 0.01
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/beam/dynamic/dyn_euler_small_added_mass_gravity.i)
# Test for small strain euler beam vibration in y direction
# Test uses NodalGravity instead of UserForcingFunctionNodalKernel to apply the
# force.
# An impulse load is applied at the end of a cantilever beam of length 4m.
# The beam is massless with a lumped mass at the end of the beam
# The properties of the cantilever beam are as follows:
# Young's modulus (E) = 1e4
# Shear modulus (G) = 4e7
# Shear coefficient (k) = 1.0
# Cross-section area (A) = 0.01
# Iy = 1e-4 = Iz
# Length (L)= 4 m
# mass = 0.01899772 at the cantilever end
# mass = 2.0 at the fixed end (just for file testing purposes does not alter result)
# For this beam, the dimensionless parameter alpha = kAGL^2/EI = 6.4e6
# Therefore, the beam behaves like a Euler-Bernoulli beam.
# The theoretical first frequency of this beam is:
# f1 = 1/(2 pi) * sqrt(3EI/(mL^3)) = 0.25
# This implies that the corresponding time period of this beam is 4s.
# The FEM solution for this beam with 10 element gives time periods of 4s with time step of 0.01s.
# A higher time step of 0.1 s is used in the test to reduce computational time.
# The time history from this analysis matches with that obtained from Abaqus.
# Values from the first few time steps are as follows:
# time disp_y vel_y accel_y
# 0.0 0.0 0.0 0.0
# 0.1 0.0013076435060869 0.026152870121738 0.52305740243477
# 0.2 0.0051984378734383 0.051663017225289 -0.01285446036375
# 0.3 0.010269120909367 0.049750643493289 -0.02539301427625
# 0.4 0.015087433925158 0.046615616822532 -0.037307519138892
# 0.5 0.019534963888307 0.042334982440433 -0.048305168503101
[Mesh]
type = GeneratedMesh
xmin = 0.0
xmax = 4.0
nx = 10
dim = 1
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[./rot_x]
order = FIRST
family = LAGRANGE
[../]
[./rot_y]
order = FIRST
family = LAGRANGE
[../]
[./rot_z]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./vel_x]
order = FIRST
family = LAGRANGE
[../]
[./vel_y]
order = FIRST
family = LAGRANGE
[../]
[./vel_z]
order = FIRST
family = LAGRANGE
[../]
[./accel_x]
order = FIRST
family = LAGRANGE
[../]
[./accel_y]
order = FIRST
family = LAGRANGE
[../]
[./accel_z]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./accel_x]
type = NewmarkAccelAux
variable = accel_x
displacement = disp_x
velocity = vel_x
beta = 0.25
execute_on = timestep_end
[../]
[./vel_x]
type = NewmarkVelAux
variable = vel_x
acceleration = accel_x
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_y]
type = NewmarkAccelAux
variable = accel_y
displacement = disp_y
velocity = vel_y
beta = 0.25
execute_on = timestep_end
[../]
[./vel_y]
type = NewmarkVelAux
variable = vel_y
acceleration = accel_y
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_z]
type = NewmarkAccelAux
variable = accel_z
displacement = disp_z
velocity = vel_z
beta = 0.25
execute_on = timestep_end
[../]
[./vel_z]
type = NewmarkVelAux
variable = vel_z
acceleration = accel_z
gamma = 0.5
execute_on = timestep_end
[../]
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./fixy1]
type = DirichletBC
variable = disp_y
boundary = left
value = 0.0
[../]
[./fixz1]
type = DirichletBC
variable = disp_z
boundary = left
value = 0.0
[../]
[./fixr1]
type = DirichletBC
variable = rot_x
boundary = left
value = 0.0
[../]
[./fixr2]
type = DirichletBC
variable = rot_y
boundary = left
value = 0.0
[../]
[./fixr3]
type = DirichletBC
variable = rot_z
boundary = left
value = 0.0
[../]
[]
[NodalKernels]
[./force_y2]
type = NodalGravity
variable = disp_y
boundary = 'left right'
gravity_value = 52.6378954948 # inverse of nodal mass at cantilever end
function = force
# nodal_mass_file = nodal_mass.csv # commented out for testing purposes
# mass = 0.01899772 # commented out for testing purposes
[../]
[./x_inertial]
type = NodalTranslationalInertia
variable = disp_x
velocity = vel_x
acceleration = accel_x
boundary = right
beta = 0.25
gamma = 0.5
mass = 0.01899772
[../]
[./y_inertial]
type = NodalTranslationalInertia
variable = disp_y
velocity = vel_y
acceleration = accel_y
boundary = right
beta = 0.25
gamma = 0.5
mass = 0.01899772
[../]
[./z_inertial]
type = NodalTranslationalInertia
variable = disp_z
velocity = vel_z
acceleration = accel_z
boundary = right
beta = 0.25
gamma = 0.5
mass = 0.01899772
[../]
[]
[Functions]
[./force]
type = PiecewiseLinear
x = '0.0 0.1 0.2 10.0'
y = '0.0 1e-2 0.0 0.0'
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options_iname = '-ksp_type -pc_type'
petsc_options_value = 'preonly lu'
dt = 0.1
end_time = 5.0
timestep_tolerance = 1e-6
[]
[Kernels]
[./solid_disp_x]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 0
variable = disp_x
[../]
[./solid_disp_y]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 1
variable = disp_y
[../]
[./solid_disp_z]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 2
variable = disp_z
[../]
[./solid_rot_x]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 3
variable = rot_x
[../]
[./solid_rot_y]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 4
variable = rot_y
[../]
[./solid_rot_z]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 5
variable = rot_z
[../]
[]
[Materials]
[./elasticity]
type = ComputeElasticityBeam
youngs_modulus = 1.0e4
poissons_ratio = -0.999875
shear_coefficient = 1.0
block = 0
[../]
[./strain]
type = ComputeIncrementalBeamStrain
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
area = 0.01
Ay = 0.0
Az = 0.0
Iy = 1.0e-4
Iz = 1.0e-4
y_orientation = '0.0 1.0 0.0'
[../]
[./stress]
type = ComputeBeamResultants
block = 0
[../]
[]
[Postprocessors]
[./disp_x]
type = PointValue
point = '4.0 0.0 0.0'
variable = disp_x
[../]
[./disp_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = disp_y
[../]
[./vel_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = vel_y
[../]
[./accel_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = accel_y
[../]
[]
[Outputs]
file_base = dyn_euler_small_added_mass_out
exodus = true
csv = true
perf_graph = true
[]
(modules/tensor_mechanics/test/tests/dynamics/wave_1D/wave_rayleigh_hht.i)
# Wave propogation in 1D using HHT time integration in the presence of Rayleigh damping
#
# The test is for an 1D bar element of length 4m fixed on one end
# with a sinusoidal pulse dirichlet boundary condition applied to the other end.
# alpha, beta and gamma are HHT time integration parameters
# eta and zeta are mass dependent and stiffness dependent Rayleigh damping
# coefficients, respectively.
# The equation of motion in terms of matrices is:
#
# M*accel + (eta*M+zeta*K)*((1+alpha)*vel-alpha*vel_old)
# +(1+alpha)*K*disp-alpha*K*disp_old = 0
#
# Here M is the mass matrix, K is the stiffness matrix
#
# The displacement at the first, second, third and fourth node at t = 0.1 are
# -7.787499960311491942e-02, 1.955566679096475483e-02 and -4.634888180231294501e-03, respectively.
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 4
nz = 1
xmin = 0.0
xmax = 0.1
ymin = 0.0
ymax = 4.0
zmin = 0.0
zmax = 0.1
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./vel_x]
[../]
[./accel_x]
[../]
[./vel_y]
[../]
[./accel_y]
[../]
[./vel_z]
[../]
[./accel_z]
[../]
[]
[Kernels]
[./DynamicTensorMechanics]
displacements = 'disp_x disp_y disp_z'
alpha = -0.3
zeta = 0.1
[../]
[./inertia_x]
type = InertialForce
variable = disp_x
velocity = vel_x
acceleration = accel_x
beta = 0.422
gamma = 0.8
eta=0.1
alpha = -0.3
[../]
[./inertia_y]
type = InertialForce
variable = disp_y
velocity = vel_y
acceleration = accel_y
beta = 0.422
gamma = 0.8
eta=0.1
alpha = -0.3
[../]
[./inertia_z]
type = InertialForce
variable = disp_z
velocity = vel_z
acceleration = accel_z
beta = 0.422
gamma = 0.8
eta = 0.1
alpha = -0.3
[../]
[]
[AuxKernels]
[./accel_x]
type = NewmarkAccelAux
variable = accel_x
displacement = disp_x
velocity = vel_x
beta = 0.422
execute_on = timestep_end
[../]
[./vel_x]
type = NewmarkVelAux
variable = vel_x
acceleration = accel_x
gamma = 0.8
execute_on = timestep_end
[../]
[./accel_y]
type = NewmarkAccelAux
variable = accel_y
displacement = disp_y
velocity = vel_y
beta = 0.422
execute_on = timestep_end
[../]
[./vel_y]
type = NewmarkVelAux
variable = vel_y
acceleration = accel_y
gamma = 0.8
execute_on = timestep_end
[../]
[./accel_z]
type = NewmarkAccelAux
variable = accel_z
displacement = disp_z
velocity = vel_z
beta = 0.422
execute_on = timestep_end
[../]
[./vel_z]
type = NewmarkVelAux
variable = vel_z
acceleration = accel_z
gamma = 0.8
execute_on = timestep_end
[../]
[]
[BCs]
[./top_y]
type = DirichletBC
variable = disp_y
boundary = top
value=0.0
[../]
[./top_x]
type = DirichletBC
variable = disp_x
boundary = top
value=0.0
[../]
[./top_z]
type = DirichletBC
variable = disp_z
boundary = top
value=0.0
[../]
[./right_x]
type = DirichletBC
variable = disp_x
boundary = right
value=0.0
[../]
[./right_z]
type = DirichletBC
variable = disp_z
boundary = right
value=0.0
[../]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = left
value=0.0
[../]
[./left_z]
type = DirichletBC
variable = disp_z
boundary = left
value=0.0
[../]
[./front_x]
type = DirichletBC
variable = disp_x
boundary = front
value=0.0
[../]
[./front_z]
type = DirichletBC
variable = disp_z
boundary = front
value=0.0
[../]
[./back_x]
type = DirichletBC
variable = disp_x
boundary = back
value=0.0
[../]
[./back_z]
type = DirichletBC
variable = disp_z
boundary = back
value=0.0
[../]
[./bottom_x]
type = DirichletBC
variable = disp_x
boundary = bottom
value=0.0
[../]
[./bottom_z]
type = DirichletBC
variable = disp_z
boundary = bottom
value=0.0
[../]
[./bottom_y]
type = FunctionDirichletBC
variable = disp_y
boundary = bottom
function = displacement_bc
[../]
[]
[Materials]
[./Elasticity_tensor]
type = ComputeElasticityTensor
block = 0
fill_method = symmetric_isotropic
C_ijkl = '1 0'
[../]
[./strain]
type = ComputeSmallStrain
block = 0
displacements = 'disp_x disp_y disp_z'
[../]
[./stress]
type = ComputeLinearElasticStress
block = 0
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = 'density'
prop_values = '1'
[../]
[]
[Executioner]
type = Transient
start_time = 0
end_time = 6.0
l_tol = 1e-12
nl_rel_tol = 1e-12
dt = 0.1
[]
[Functions]
[./displacement_bc]
type = PiecewiseLinear
data_file = 'sine_wave.csv'
format = columns
[../]
[]
[Postprocessors]
[./_dt]
type = TimestepSize
[../]
[./disp_1]
type = NodalVariableValue
nodeid = 1
variable = disp_y
[../]
[./disp_2]
type = NodalVariableValue
nodeid = 3
variable = disp_y
[../]
[./disp_3]
type = NodalVariableValue
nodeid = 10
variable = disp_y
[../]
[./disp_4]
type = NodalVariableValue
nodeid = 14
variable = disp_y
[../]
[]
[Outputs]
exodus = true
perf_graph = true
[]
(modules/richards/test/tests/broadbridge_white/bw01.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 200
ny = 1
xmin = -10
xmax = 10
ymin = 0
ymax = 0.05
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1E-5 1E-2 1E-2 1E-1'
x = '0 1E-5 1 10'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 10
bulk_mod = 2E9
[../]
[./SeffBW]
type = RichardsSeff1BWsmall
Sn = 0.0
Ss = 1.0
C = 1.5
las = 2
[../]
[./RelPermBW]
type = RichardsRelPermBW
Sn = 0.0
Ss = 1.0
Kn = 0
Ks = 1
C = 1.5
[../]
[./Saturation]
type = RichardsSat
s_res = 0.0
sum_s_res = 0.0
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 1.0E2
[../]
[]
[Variables]
active = 'pressure'
[./pressure]
order = FIRST
family = LAGRANGE
initial_condition = -9E2
[../]
[]
[Kernels]
active = 'richardsf richardst'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = SeffBW
pressure_vars = pressure
[../]
[]
[BCs]
active = 'recharge'
[./recharge]
type = RichardsPiecewiseLinearSink
variable = pressure
boundary = 'right'
pressures = '-1E10 1E10'
bare_fluxes = '-1.25 -1.25' # corresponds to Rstar being 0.5 because i have to multiply by density*porosity
use_mobility = false
use_relperm = false
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.25
mat_permeability = '1 0 0 0 1 0 0 0 1'
density_UO = DensityConstBulk
relperm_UO = RelPermBW
SUPG_UO = SUPGstandard
sat_UO = Saturation
seff_UO = SeffBW
viscosity = 4
gravity = '-0.1 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
active = 'andy'
[./andy]
type = SMP
full = true
petsc_options = ''
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-10 1E-10 10000'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
petsc_options = '-snes_converged_reason'
end_time = 2
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = bw01
interval = 10000
execute_on = 'timestep_end final'
exodus = true
[]
(modules/combined/test/tests/ad_cavity_pressure/3d.i)
#
# Cavity Pressure Test
#
# This test is designed to compute an internal pressure based on
# p = n * R * T / V
# where
# p is the pressure
# n is the amount of material in the volume (moles)
# R is the universal gas constant
# T is the temperature
# V is the volume
#
# The mesh is composed of one block (1) with an interior cavity of volume 8.
# Block 2 sits in the cavity and has a volume of 1. Thus, the total
# initial volume is 7.
# The test adjusts n, T, and V in the following way:
# n => n0 + alpha * t
# T => T0 + beta * t
# V => V0 + gamma * t
# with
# alpha = n0
# beta = T0 / 2
# gamma = - (0.003322259...) * V0
# T0 = 240.54443866068704
# V0 = 7
# n0 = f(p0)
# p0 = 100
# R = 8.314472 J * K^(-1) * mol^(-1)
#
# So, n0 = p0 * V0 / R / T0 = 100 * 7 / 8.314472 / 240.544439
# = 0.35
#
# The parameters combined at t = 1 gives p = 301.
#
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[Mesh]
file = 3d.e
[]
[Functions]
[./displ_positive]
type = PiecewiseLinear
x = '0 1'
y = '0 0.0029069767441859684'
[../]
[./displ_negative]
type = PiecewiseLinear
x = '0 1'
y = '0 -0.0029069767441859684'
[../]
[./temp1]
type = PiecewiseLinear
x = '0 1'
y = '1 1.5'
scale_factor = 240.54443866068704
[../]
[./material_input_function]
type = PiecewiseLinear
x = '0 1'
y = '0 0.35'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[./temp]
initial_condition = 240.54443866068704
[../]
[./material_input]
[../]
[]
[AuxVariables]
[./pressure_residual_x]
[../]
[./pressure_residual_y]
[../]
[./pressure_residual_z]
[../]
[./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_zx]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
use_automatic_differentiation = true
[../]
[./heat]
type = ADDiffusion
variable = temp
use_displaced_mesh = true
[../]
[./material_input_dummy]
type = ADDiffusion
variable = material_input
use_displaced_mesh = true
[../]
[]
[AuxKernels]
[./stress_xx]
type = ADRankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 0
variable = stress_xx
[../]
[./stress_yy]
type = ADRankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 1
variable = stress_yy
[../]
[./stress_zz]
type = ADRankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 2
variable = stress_zz
[../]
[./stress_xy]
type = ADRankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 1
variable = stress_xy
[../]
[./stress_yz]
type = ADRankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 2
variable = stress_yz
[../]
[./stress_zx]
type = ADRankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 0
variable = stress_zx
[../]
[]
[BCs]
[./no_x_exterior]
type = DirichletBC
variable = disp_x
boundary = '7 8'
value = 0.0
[../]
[./no_y_exterior]
type = DirichletBC
variable = disp_y
boundary = '9 10'
value = 0.0
[../]
[./no_z_exterior]
type = DirichletBC
variable = disp_z
boundary = '11 12'
value = 0.0
[../]
[./prescribed_left]
type = ADFunctionDirichletBC
variable = disp_x
boundary = 13
function = displ_positive
[../]
[./prescribed_right]
type = ADFunctionDirichletBC
variable = disp_x
boundary = 14
function = displ_negative
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = '15 16'
value = 0.0
[../]
[./no_z]
type = DirichletBC
variable = disp_z
boundary = '17 18'
value = 0.0
[../]
[./no_x_interior]
type = DirichletBC
variable = disp_x
boundary = '1 2'
value = 0.0
[../]
[./no_y_interior]
type = DirichletBC
variable = disp_y
boundary = '3 4'
value = 0.0
[../]
[./no_z_interior]
type = DirichletBC
variable = disp_z
boundary = '5 6'
value = 0.0
[../]
[./temperatureInterior]
type = ADFunctionDirichletBC
boundary = 100
function = temp1
variable = temp
[../]
[./MaterialInput]
type = ADFunctionDirichletBC
boundary = '100 13 14 15 16'
function = material_input_function
variable = material_input
[../]
[./CavityPressure]
[./1]
boundary = 100
initial_pressure = 100
material_input = materialInput
R = 8.314472
temperature = aveTempInterior
volume = internalVolume
startup_time = 0.5
output = ppress
save_in = 'pressure_residual_x pressure_residual_y pressure_residual_z'
use_automatic_differentiation = true
[../]
[../]
[]
[Materials]
[./elast_tensor1]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1e1
poissons_ratio = 0
block = 1
[../]
[./strain1]
type = ADComputeFiniteStrain
block = 1
[../]
[./stress1]
type = ADComputeFiniteStrainElasticStress
block = 1
[../]
[./elast_tensor2]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0
block = 2
[../]
[./strain2]
type = ADComputeFiniteStrain
block = 2
[../]
[./stress2]
type = ADComputeFiniteStrainElasticStress
block = 2
[../]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_type'
petsc_options_value = 'asm lu'
nl_rel_tol = 1e-12
l_tol = 1e-12
l_max_its = 20
dt = 0.5
end_time = 1.0
[]
[Postprocessors]
[./internalVolume]
type = InternalVolume
boundary = 100
execute_on = 'initial linear'
[../]
[./aveTempInterior]
type = SideAverageValue
boundary = 100
variable = temp
execute_on = 'initial linear'
[../]
[./materialInput]
type = SideAverageValue
boundary = '7 8 9 10 11 12'
variable = material_input
execute_on = linear
[../]
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/smeared_cracking/cracking.i)
#
# Simple pull test for cracking.
# The stress increases for two steps and then drops to zero.
[Mesh]
file = cracking_test.e
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Functions]
[./displ]
type = PiecewiseLinear
x = '0 1 2 3 4'
y = '0 1 0 -1 0'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx'
[../]
[]
[BCs]
[./pull]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = displ
[../]
[./left]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./bottom]
type = DirichletBC
variable = disp_y
boundary = 2
value = 0.0
[../]
[./back]
type = DirichletBC
variable = disp_z
boundary = 3
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 2.8e7
poissons_ratio = 0
[../]
[./elastic_stress]
type = ComputeSmearedCrackingStress
cracking_stress = 1.68e6
softening_models = abrupt_softening
[../]
[./abrupt_softening]
type = AbruptSoftening
[../]
[]
[Executioner]
type = Transient
petsc_options_iname = '-ksp_gmres_restart -pc_type -sub_pc_type'
petsc_options_value = '101 asm lu'
line_search = 'none'
l_max_its = 100
nl_max_its = 100
nl_rel_tol = 1e-8
nl_abs_tol = 1e-8
l_tol = 1e-5
start_time = 0.0
end_time = 0.1
dt = 0.025
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/ad_smeared_cracking/cracking_deprecated.i)
#
# Simple pull test for cracking.
# The stress increases for two steps and then drops to zero.
[Mesh]
file = cracking_test.e
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Functions]
[./displ]
type = PiecewiseLinear
x = '0 1 2 3 4'
y = '0 1 0 -1 0'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx'
use_automatic_differentiation = true
[../]
[]
[BCs]
[./pull]
type = ADFunctionDirichletBC
variable = disp_x
boundary = 4
function = displ
[../]
[./left]
type = ADDirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./bottom]
type = ADDirichletBC
variable = disp_y
boundary = 2
value = 0.0
[../]
[./back]
type = ADDirichletBC
variable = disp_z
boundary = 3
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 2.8e7
poissons_ratio = 0
[../]
[./elastic_stress]
type = ADComputeSmearedCrackingStress
cracking_stress = 1.68e6
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
petsc_options_iname = '-ksp_gmres_restart -pc_type -sub_pc_type'
petsc_options_value = '101 asm lu'
line_search = 'none'
l_max_its = 100
nl_max_its = 100
nl_rel_tol = 1e-8
nl_abs_tol = 1e-8
l_tol = 1e-5
start_time = 0.0
end_time = 0.1
dt = 0.025
[]
[Outputs]
exodus = true
file_base = cracking_out
[]
(modules/richards/test/tests/buckley_leverett/bl21.i)
# two-phase version
# sharp front version
[Mesh]
type = GeneratedMesh
dim = 1
nx = 150
xmin = 0
xmax = 15
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1E-3 1E-2 3E-2 4E-2 0.5 0.5 1'
x = '0 1E-2 1E-1 1 5 40 41'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = 'pwater pgas'
[../]
[./DensityWater]
type = RichardsDensityConstBulk
dens0 = 1000
bulk_mod = 2E6
[../]
[./DensityGas]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 2E6
[../]
[./SeffWater]
type = RichardsSeff2waterVG
m = 0.8
al = 3E-5
[../]
[./SeffGas]
type = RichardsSeff2gasVG
m = 0.8
al = 3E-5
[../]
[./RelPermWater]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./RelPermGas]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./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 = 1E-5
[../]
[./SUPGgas]
type = RichardsSUPGstandard
p_SUPG = 1E-5
[../]
[]
[Variables]
[./pwater]
order = FIRST
family = LAGRANGE
[../]
[./pgas]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[./bounds_dummy]
[../]
[]
[Kernels]
active = 'richardsfwater richardstwater richardsfgas richardstgas'
[./richardstwater]
type = RichardsMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFlux
variable = pwater
[../]
[./richardstgas]
type = RichardsMassChange
variable = pgas
[../]
[./richardsfgas]
type = RichardsFlux
variable = pgas
[../]
[./richardsppenalty]
type = RichardsPPenalty
variable = pgas
a = 1E-18
lower_var = pwater
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = SeffWater
pressure_vars = 'pwater pgas'
[../]
[]
[Bounds]
[./pwater_upper_bounds]
type = ConstantBoundsAux
variable = bounds_dummy
bounded_variable = pwater
bound_type = upper
bound_value = 1E7
[../]
[./pwater_lower_bounds]
type = ConstantBoundsAux
variable = bounds_dummy
bounded_variable = pwater
bound_type = lower
bound_value = -110000
[../]
[]
[ICs]
[./water_ic]
type = FunctionIC
variable = pwater
function = initial_water
[../]
[./gas_ic]
type = FunctionIC
variable = pgas
function = initial_gas
[../]
[]
[BCs]
[./left_w]
type = DirichletBC
variable = pwater
boundary = left
value = 1E6
[../]
[./left_g]
type = DirichletBC
variable = pgas
boundary = left
value = 1E6+1000
[../]
[./right_w]
type = DirichletBC
variable = pwater
boundary = right
value = -100000
[../]
[./right_g]
type = DirichletBC
variable = pgas
boundary = right
value = 0+1000
[../]
[]
[Functions]
[./initial_water]
type = ParsedFunction
value = 1000000*(1-min(x/5,1))-100000*(max(x-5,0)/max(abs(x-5),1E-10))
[../]
[./initial_gas]
type = ParsedFunction
value = max(1000000*(1-x/5),0)+1000
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.15
mat_permeability = '1E-10 0 0 0 1E-10 0 0 0 1E-10'
density_UO = 'DensityWater DensityGas'
relperm_UO = 'RelPermWater RelPermGas'
SUPG_UO = 'SUPGwater SUPGgas'
sat_UO = 'SatWater SatGas'
seff_UO = 'SeffWater SeffGas'
viscosity = '1E-3 1E-6'
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
active = 'standard'
[./bounded]
# must use --use-petsc-dm command line argument
type = SMP
full = true
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -snes_type -ksp_rtol -ksp_atol'
petsc_options_value = 'bcgs bjacobi 1E-10 1E-10 50 vinewtonssls 1E-20 1E-20'
[../]
[./standard]
type = SMP
full = true
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -ksp_rtol -ksp_atol'
petsc_options_value = 'bcgs bjacobi 1E-10 1E-10 20 1E-20 1E-20'
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
end_time = 50
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = bl21
interval = 10000
exodus = true
[]
(modules/tensor_mechanics/test/tests/j_integral_vtest/j_int_surfbreak_ellip_crack_sym_mm_cm.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[Mesh]
file = ellip_crack_4sym_norad_mm.e
partitioner = centroid
centroid_partitioner_direction = z
[]
[AuxVariables]
[./SED]
order = CONSTANT
family = MONOMIAL
[../]
[./resid_z]
[../]
[]
[Functions]
[./rampConstantUp]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 0.1'
scale_factor = -689.5 #MPa
[../]
[]
[DomainIntegral]
integrals = JIntegral
boundary = 1001
crack_direction_method = CrackMouth
crack_mouth_boundary = 11
crack_end_direction_method = CrackDirectionVector
crack_direction_vector_end_1 = '0.0 1.0 0.0'
crack_direction_vector_end_2 = '1.0 0.0 0.0'
radius_inner = '12.5 25.0 37.5'
radius_outer = '25.0 37.5 50.0'
intersecting_boundary = '1 2'
symmetry_plane = 2
position_type = angle
incremental = true
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
[../]
[]
[AuxKernels]
[./SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[../]
[]
[BCs]
[./crack_y]
type = DirichletBC
variable = disp_z
boundary = 6
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = 12
value = 0.0
[../]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./Pressure]
[./Side1]
boundary = 5
function = rampConstantUp
[../]
[../]
[] # BCs
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 206800
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
# Two sets of linesearch options are for petsc 3.1 and 3.3 respectively
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
# petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 4'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_abs_tol = 1e-5
nl_rel_tol = 1e-11
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Postprocessors]
[./_dt]
type = TimestepSize
[../]
[./nl_its]
type = NumNonlinearIterations
[../]
[./lin_its]
type = NumLinearIterations
[../]
[./react_z]
type = NodalSum
variable = resid_z
boundary = 5
[../]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = j_int_surfbreak_ellip_crack_sym_mm_cm_out
exodus = true
csv = true
[]
(test/tests/time_integrators/newmark-beta/newmark_beta_prescribed_parameters.i)
###########################################################
# This is a simple test with a time-dependent problem
# demonstrating the use of the TimeIntegrator system.
#
# Testing that the first and second time derivatives
# are calculated correctly using the Newmark-Beta method
#
# @Requirement F1.30
###########################################################
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 1
ny = 1
[]
[Variables]
[u]
[]
[]
[Functions]
[forcing_fn]
type = PiecewiseLinear
x = '0.0 0.1 0.2 0.3 0.4 0.5 0.6'
y = '0.0 0.0 0.0025 0.01 0.0175 0.02 0.02'
[]
[]
[Kernels]
[ie]
type = TimeDerivative
variable = u
[]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = FunctionDirichletBC
variable = u
boundary = 'left'
function = forcing_fn
[]
[right]
type = FunctionDirichletBC
variable = u
boundary = 'right'
function = forcing_fn
[]
[]
[Executioner]
type = Transient
start_time = 0.0
num_steps = 6
dt = 0.1
[TimeIntegrator]
type = NewmarkBeta
beta = 0.4225
gamma = 0.8
[]
[]
[Postprocessors]
[udot]
type = ElementAverageTimeDerivative
variable = u
[]
[udotdot]
type = ElementAverageSecondTimeDerivative
variable = u
[]
[u]
type = ElementAverageValue
variable = u
[]
[]
[Outputs]
csv = true
[]
(modules/tensor_mechanics/test/tests/smeared_cracking/cracking_exponential_deprecated.i)
#
# Test to exercise the exponential stress release
#
# Stress vs. strain should show a linear relationship until cracking,
# an exponential stress release, a linear relationship back to zero
# strain, a linear relationship with the original stiffness in
# compression and then back to zero strain, a linear relationship
# back to the exponential curve, and finally further exponential
# stress release.
#
[Mesh]
file = cracking_test.e
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Functions]
[./displx]
type = PiecewiseLinear
x = '0 1 2 3 4 5 6'
y = '0 0.00175 0 -0.0001 0 0.00175 0.0035'
[../]
[./disply]
type = PiecewiseLinear
x = '0 5 6'
y = '0 0 .00175'
[../]
[./displz]
type = PiecewiseLinear
x = '0 2 3'
y = '0 0 .0035'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx'
[../]
[]
[BCs]
[./pullx]
type = FunctionDirichletBC
#type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = displx
[../]
[./left]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./fix_y]
type = DirichletBC
variable = disp_y
boundary = '11 12'
value = 0.0
[../]
[./move_y]
type = FunctionDirichletBC
variable = disp_y
boundary = '15 16'
function = disply
[../]
[./back]
type = DirichletBC
variable = disp_z
boundary = '3'
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 186.5e9
poissons_ratio = .316
[../]
[./elastic_stress]
type = ComputeSmearedCrackingStress
cracking_stress = 119.3e6
cracking_release = exponential
[../]
[]
[Executioner]
type = Transient
petsc_options_iname = '-ksp_gmres_restart -pc_type'
petsc_options_value = '101 lu'
line_search = 'none'
l_max_its = 100
l_tol = 1e-6
nl_max_its = 10
nl_rel_tol = 1e-12
nl_abs_tol = 1.e-4
start_time = 0.0
dt = 0.02
dtmin = 0.02
num_steps = 300
[]
[Outputs]
exodus = true
file_base = cracking_exponential_out
[]
(modules/tensor_mechanics/test/tests/1D_axisymmetric/axisymm_plane_strain_finite.i)
#
# This test checks elastic stress calculations with mechanical and thermal
# strain using finite strain formulation. Young's modulus is 3600, and Poisson's ratio is 0.2.
# The axisymmetric, plane strain 1D mesh is pulled with displacement of 2e-3.
# Thus, the strain is [log(1+1e-3)=9.995e-4, 0, log(1+1e-3)=9.995e-4] (xx, yy, zz). This gives stress of
# [4.9975, 1.999, 4.9975]. After a temperature increase of 100 with alpha of
# 1e-6, the stress becomes [4.3975, 1.399, 4.3975].
#
[GlobalParams]
displacements = disp_x
[]
[Problem]
coord_type = RZ
[]
[Mesh]
file = line.e
[]
[Variables]
[./disp_x]
[../]
[]
[AuxVariables]
[./temp]
initial_condition = 580.0
[../]
[]
[Functions]
[./temp]
type = PiecewiseLinear
x = '0 1 2'
y = '580 580 680'
[../]
[./disp_x]
type = PiecewiseLinear
x = '0 1'
y = '0 2e-3'
[../]
[]
[Modules]
[./TensorMechanics]
[./Master]
[./ps]
planar_formulation = PLANE_STRAIN
strain = FINITE
generate_output = 'strain_xx strain_zz stress_xx stress_yy stress_zz'
eigenstrain_names = eigenstrain
[../]
[../]
[../]
[]
[AuxKernels]
[./temp]
type = FunctionAux
variable = temp
function = temp
execute_on = 'timestep_begin'
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
boundary = 1
value = 0
variable = disp_x
[../]
[./disp_x]
type = FunctionDirichletBC
boundary = 2
function = disp_x
variable = disp_x
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 3600
poissons_ratio = 0.2
[../]
[./thermal_strain]
type = ComputeThermalExpansionEigenstrain
thermal_expansion_coeff = 1e-6
temperature = temp
stress_free_temperature = 580
eigenstrain_name = eigenstrain
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
line_search = 'none'
l_max_its = 50
l_tol = 1e-6
nl_max_its = 15
nl_rel_tol = 1e-8
nl_abs_tol = 1e-10
start_time = 0
end_time = 2
num_steps = 2
[]
[Outputs]
exodus = true
console = true
[]
(modules/tensor_mechanics/test/tests/dynamics/wave_1D/wave_hht.i)
# Wave propogation in 1D using HHT time integration
#
# The test is for an 1D bar element of length 4m fixed on one end
# with a sinusoidal pulse dirichlet boundary condition applied to the other end.
# alpha, beta and gamma are Newmark time integration parameters
# The equation of motion in terms of matrices is:
#
# M*accel + K*((1+alpha)*disp-alpha*disp_old) = 0
#
# Here M is the mass matrix, K is the stiffness matrix
#
# The displacement at the second, third and fourth node at t = 0.1 are
# -8.097405701570538350e-02, 2.113131879547342634e-02 and -5.182787688751439893e-03, respectively.
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 4
nz = 1
xmin = 0.0
xmax = 0.1
ymin = 0.0
ymax = 4.0
zmin = 0.0
zmax = 0.1
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./vel_x]
[../]
[./accel_x]
[../]
[./vel_y]
[../]
[./accel_y]
[../]
[./vel_z]
[../]
[./accel_z]
[../]
[]
[Kernels]
[./DynamicTensorMechanics]
displacements = 'disp_x disp_y disp_z'
alpha = -0.3
[../]
[./inertia_x]
type = InertialForce
variable = disp_x
velocity = vel_x
acceleration = accel_x
beta = 0.3025
gamma = 0.6
alpha = -0.3
[../]
[./inertia_y]
type = InertialForce
variable = disp_y
velocity = vel_y
acceleration = accel_y
beta = 0.3025
gamma = 0.6
alpha = -0.3
[../]
[./inertia_z]
type = InertialForce
variable = disp_z
velocity = vel_z
acceleration = accel_z
beta = 0.3025
gamma = 0.6
alpha = -0.3
[../]
[]
[AuxKernels]
[./accel_x]
type = NewmarkAccelAux
variable = accel_x
displacement = disp_x
velocity = vel_x
beta = 0.3025
execute_on = timestep_end
[../]
[./vel_x]
type = NewmarkVelAux
variable = vel_x
acceleration = accel_x
gamma = 0.6
execute_on = timestep_end
[../]
[./accel_y]
type = NewmarkAccelAux
variable = accel_y
displacement = disp_y
velocity = vel_y
beta = 0.3025
execute_on = timestep_end
[../]
[./vel_y]
type = NewmarkVelAux
variable = vel_y
acceleration = accel_y
gamma = 0.6
execute_on = timestep_end
[../]
[./accel_z]
type = NewmarkAccelAux
variable = accel_z
displacement = disp_z
velocity = vel_z
beta = 0.3025
execute_on = timestep_end
[../]
[./vel_z]
type = NewmarkVelAux
variable = vel_z
acceleration = accel_z
gamma = 0.6
execute_on = timestep_end
[../]
[]
[BCs]
[./top_y]
type = DirichletBC
variable = disp_y
boundary = top
value=0.0
[../]
[./top_x]
type = DirichletBC
variable = disp_x
boundary = top
value=0.0
[../]
[./top_z]
type = DirichletBC
variable = disp_z
boundary = top
value=0.0
[../]
[./right_x]
type = DirichletBC
variable = disp_x
boundary = right
value=0.0
[../]
[./right_z]
type = DirichletBC
variable = disp_z
boundary = right
value=0.0
[../]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = left
value=0.0
[../]
[./left_z]
type = DirichletBC
variable = disp_z
boundary = left
value=0.0
[../]
[./front_x]
type = DirichletBC
variable = disp_x
boundary = front
value=0.0
[../]
[./front_z]
type = DirichletBC
variable = disp_z
boundary = front
value=0.0
[../]
[./back_x]
type = DirichletBC
variable = disp_x
boundary = back
value=0.0
[../]
[./back_z]
type = DirichletBC
variable = disp_z
boundary = back
value=0.0
[../]
[./bottom_x]
type = DirichletBC
variable = disp_x
boundary = bottom
value=0.0
[../]
[./bottom_z]
type = DirichletBC
variable = disp_z
boundary = bottom
value=0.0
[../]
[./bottom_y]
type = FunctionDirichletBC
variable = disp_y
boundary = bottom
function = displacement_bc
[../]
[]
[Materials]
[./Elasticity_tensor]
type = ComputeElasticityTensor
block = 0
fill_method = symmetric_isotropic
C_ijkl = '1 0'
[../]
[./strain]
type = ComputeSmallStrain
block = 0
displacements = 'disp_x disp_y disp_z'
[../]
[./stress]
type = ComputeLinearElasticStress
block = 0
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = 'density'
prop_values = '1'
[../]
[]
[Executioner]
type = Transient
start_time = 0
end_time = 6.0
l_tol = 1e-12
nl_rel_tol = 1e-12
dt = 0.1
[]
[Functions]
[./displacement_bc]
type = PiecewiseLinear
data_file = 'sine_wave.csv'
format = columns
[../]
[]
[Postprocessors]
[./_dt]
type = TimestepSize
[../]
[./disp_1]
type = NodalVariableValue
nodeid = 1
variable = vel_y
[../]
[./disp_2]
type = NodalVariableValue
nodeid = 3
variable = vel_y
[../]
[./disp_3]
type = NodalVariableValue
nodeid = 10
variable = vel_y
[../]
[./disp_4]
type = NodalVariableValue
nodeid = 14
variable = vel_y
[../]
[]
[Outputs]
exodus = true
perf_graph = true
[]
(modules/combined/test/tests/ad_cavity_pressure/negative_volume.i)
#
# Cavity Pressure Test
#
# This test is designed to compute a negative number of moles
# to trigger an error check in the CavityPressureUserObject.
# The negative number of moles is achieved by supplying an
# open volume to the InternalVolume postprocessor, which
# calculates a negative volume.
[Problem]
coord_type = RZ
[]
[GlobalParams]
displacements = 'disp_r disp_z'
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 2
[]
[Functions]
[./temperature]
type = PiecewiseLinear
x = '0 1'
y = '1 2'
scale_factor = 100
[../]
[]
[Variables]
[./temperature]
initial_condition = 100
[../]
[]
[Modules/TensorMechanics/Master]
[./block]
strain = FINITE
add_variables = true
use_automatic_differentiation = true
[../]
[]
[Kernels]
[./heat]
type = Diffusion
variable = temperature
use_displaced_mesh = true
[../]
[]
[BCs]
[./no_x]
type = ADDirichletBC
variable = disp_r
boundary = left
value = 0.0
[../]
[./no_y]
type = ADDirichletBC
variable = disp_z
boundary = bottom
value = 0.0
[../]
[./temperatureInterior]
type = ADFunctionDirichletBC
boundary = 2
function = temperature
variable = temperature
[../]
[./CavityPressure]
[./pressure]
boundary = 'top bottom right'
initial_pressure = 10e5
R = 8.3143
output_initial_moles = initial_moles
temperature = aveTempInterior
volume = internalVolume
startup_time = 0.5
output = ppress
use_automatic_differentiation = true
[../]
[../]
[]
[Materials]
[./elastic_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress1]
type = ADComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_type'
petsc_options_value = 'asm lu'
nl_abs_tol = 1e-10
l_max_its = 20
dt = 0.5
end_time = 1.0
[]
[Postprocessors]
[./internalVolume]
type = InternalVolume
boundary = 'top bottom right'
execute_on = 'initial linear'
[../]
[./aveTempInterior]
type = AxisymmetricCenterlineAverageValue
boundary = left
variable = temperature
execute_on = 'initial linear'
[../]
[]
[Outputs]
exodus = false
[]
(modules/xfem/test/tests/diffusion_xfem/levelsetcut2d_aux.i)
# 2D: Mesh is cut by level set based cutter
# The level set is a MOOSE auxvariable
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 3
ny = 3
xmin = 0
xmax = 1
ymin = 0
ymax = 1
elem_type = QUAD4
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./level_set_cut_uo]
type = LevelSetCutUserObject
level_set_var = ls
[../]
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./ls]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./ls_function]
type = FunctionAux
variable = ls
function = ls_func
[../]
[]
[Functions]
[./u_left]
type = PiecewiseLinear
x = '0 2'
y = '3 5'
[../]
[./ls_func]
type = ParsedFunction
value = 'x-0.5'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = DirichletBC
variable = u
boundary = 3
value = 3
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Transient
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
start_time = 0.0
dt = 1
end_time = 1.0
max_xfem_update = 1
[]
[Outputs]
interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/tensor_mechanics/test/tests/dynamics/time_integration/newmark_test.i)
# Test for Newmark time integration
# The test is for an 1D bar element of unit length fixed on one end
# with a ramped pressure boundary condition applied to the other end.
# beta and gamma are Newmark time integration parameters
# The equation of motion in terms of matrices is:
#
# M*accel + K*disp = P*Area
#
# Here M is the mass matrix, K is the stiffness matrix, P is the applied pressure
#
# This equation is equivalent to:
#
# density*accel + Div Stress = P
#
# The first term on the left is evaluated using the Inertial force kernel
# The last term on the left is evaluated using StressDivergenceTensors
# The residual due to Pressure is evaluated using Pressure boundary condition
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = 0.0
xmax = 0.1
ymin = 0.0
ymax = 1.0
zmin = 0.0
zmax = 0.1
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./vel_x]
[../]
[./accel_x]
[../]
[./vel_y]
[../]
[./accel_y]
[../]
[./vel_z]
[../]
[./accel_z]
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./TensorMechanics]
displacements = 'disp_x disp_y disp_z'
[../]
[./inertia_x]
type = InertialForce
variable = disp_x
velocity = vel_x
acceleration = accel_x
beta = 0.25
gamma = 0.5
[../]
[./inertia_y]
type = InertialForce
variable = disp_y
velocity = vel_y
acceleration = accel_y
beta = 0.25
gamma = 0.5
[../]
[./inertia_z]
type = InertialForce
variable = disp_z
velocity = vel_z
acceleration = accel_z
beta = 0.25
gamma = 0.5
[../]
[]
[AuxKernels]
[./accel_x]
type = NewmarkAccelAux
variable = accel_x
displacement = disp_x
velocity = vel_x
beta = 0.25
execute_on = timestep_end
[../]
[./vel_x]
type = NewmarkVelAux
variable = vel_x
acceleration = accel_x
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_y]
type = NewmarkAccelAux
variable = accel_y
displacement = disp_y
velocity = vel_y
beta = 0.25
execute_on = timestep_end
[../]
[./vel_y]
type = NewmarkVelAux
variable = vel_y
acceleration = accel_y
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_z]
type = NewmarkAccelAux
variable = accel_z
displacement = disp_z
velocity = vel_z
beta = 0.25
execute_on = timestep_end
[../]
[./vel_z]
type = NewmarkVelAux
variable = vel_z
acceleration = accel_z
gamma = 0.5
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 0
index_j = 1
[../]
[./strain_yy]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_yy
index_i = 0
index_j = 1
[../]
[]
[BCs]
[./top_y]
type = DirichletBC
variable = disp_y
boundary = top
value=0.0
[../]
[./top_x]
type = DirichletBC
variable = disp_x
boundary = top
value=0.0
[../]
[./top_z]
type = DirichletBC
variable = disp_z
boundary = top
value=0.0
[../]
[./bottom_x]
type = DirichletBC
variable = disp_x
boundary = bottom
value=0.0
[../]
[./bottom_z]
type = DirichletBC
variable = disp_z
boundary = bottom
value=0.0
[../]
[./Pressure]
[./Side1]
boundary = bottom
function = pressure
factor = 1
displacements = 'disp_x disp_y disp_z'
[../]
[../]
[]
[Materials]
[./Elasticity_tensor]
type = ComputeElasticityTensor
block = 0
fill_method = symmetric_isotropic
C_ijkl = '210e9 0'
[../]
[./strain]
type = ComputeSmallStrain
block = 0
displacements = 'disp_x disp_y disp_z'
[../]
[./stress]
type = ComputeLinearElasticStress
block = 0
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = 'density'
prop_values = '7750'
[../]
[]
[Executioner]
type = Transient
start_time = 0
end_time = 2
dt = 0.1
[]
[Functions]
[./pressure]
type = PiecewiseLinear
x = '0.0 0.1 0.2 1.0 2.0 5.0'
y = '0.0 0.1 0.2 1.0 1.0 1.0'
scale_factor = 1e9
[../]
[]
[Postprocessors]
[./_dt]
type = TimestepSize
[../]
[./disp]
type = NodalMaxValue
variable = disp_y
boundary = bottom
[../]
[./vel]
type = NodalMaxValue
variable = vel_y
boundary = bottom
[../]
[./accel]
type = NodalMaxValue
variable = accel_y
boundary = bottom
[../]
[./stress_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./strain_yy]
type = ElementAverageValue
variable = strain_yy
[../]
[]
[Outputs]
exodus = true
perf_graph = true
[]
(test/tests/geomsearch/2d_moving_penetration/pl_test3qnns.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
file = pl_test3q.e
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
normal_smoothing_method = nodal_normal_based
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate10]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate13]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate14]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate15]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate16]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-10
l_max_its = 10
start_time = 0.0
dt = 0.02
end_time = 1.0
[./Quadrature]
order = THIRD
[../]
[]
[Outputs]
file_base = pl_test3qnns_out
exodus = true
[]
[NodalNormals]
boundary = 11
corner_boundary = 20
[]
(modules/tensor_mechanics/test/tests/ad_viscoplasticity_stress_update/gtn_single.i)
# This test provides an example of an individual GTN viscoplasticity model
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
xmax = 0.002
ymax = 0.002
[]
[Modules/TensorMechanics/Master/All]
strain = FINITE
add_variables = true
base_name = 'total'
generate_output = 'strain_xx strain_yy strain_xy hydrostatic_stress vonmises_stress'
use_automatic_differentiation = true
[]
[Functions]
[./pull]
type = PiecewiseLinear
x = '0 0.1'
y = '0 1e-5'
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1e10
poissons_ratio = 0.3
base_name = 'total'
[../]
[./stress]
type = ADComputeMultipleInelasticStress
inelastic_models = gtn
outputs = all
base_name = 'total'
[../]
[./porosity]
type = ADPorosityFromStrain
initial_porosity = 0.1
inelastic_strain = 'total_combined_inelastic_strain'
outputs = 'all'
[../]
[./gtn]
type = ADViscoplasticityStressUpdate
total_strain_base_name = 'total'
coefficient = 'coef'
power = 3
viscoplasticity_model = GTN
outputs = all
relative_tolerance = 1e-11
[../]
[./coef]
type = ADParsedMaterial
f_name = coef
# Example of creep power law
function = '1e-18 * exp(-4e4 / 1.987 / 1200)'
[../]
[]
[BCs]
[./no_disp_x]
type = ADDirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./no_disp_y]
type = ADDirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./pull_disp_y]
type = ADFunctionDirichletBC
variable = disp_y
boundary = top
function = pull
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
dt = 0.01
end_time = 0.12
[]
[Postprocessors]
[./disp_x]
type = SideAverageValue
variable = disp_x
boundary = right
[../]
[./disp_y]
type = SideAverageValue
variable = disp_y
boundary = top
[../]
[./avg_hydro]
type = ElementAverageValue
variable = total_hydrostatic_stress
[../]
[./avg_vonmises]
type = ElementAverageValue
variable = total_vonmises_stress
[../]
[./dt]
type = TimestepSize
[../]
[./num_lin]
type = NumLinearIterations
outputs = console
[../]
[./num_nonlin]
type = NumNonlinearIterations
outputs = console
[../]
[./eff_creep_strain]
type = ElementAverageValue
variable = effective_viscoplasticity
[../]
[./porosity]
type = ElementAverageValue
variable = porosity
[../]
[]
[Outputs]
csv = true
[]
(modules/tensor_mechanics/test/tests/central_difference/consistent/1D/1d_consistent_explicit.i)
# Test for central difference integration for a 1D element
# Consistent mass matrix
[Mesh]
type = GeneratedMesh
xmin = 0
xmax = 10
nx = 5
dim = 1
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./accel_x]
[../]
[./vel_x]
[../]
[]
[AuxKernels]
[./accel_x]
type = TestNewmarkTI
variable = accel_x
displacement = disp_x
first = false
[../]
[./vel_x]
type = TestNewmarkTI
variable = vel_x
displacement = disp_x
[../]
[]
[Kernels]
[./DynamicTensorMechanics]
displacements = 'disp_x'
[../]
[./inertia_x]
type = InertialForce
variable = disp_x
[../]
[]
[NodalKernels]
[./force_x]
type = UserForcingFunctionNodalKernel
variable = disp_x
boundary = right
function = force_x
[../]
[]
[Functions]
[./force_x]
type = PiecewiseLinear
x = '0.0 1.0 2.0 3.0 4.0' # time
y = '0.0 1.0 0.0 -1.0 0.0' # force
scale_factor = 1e3
[../]
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor_block]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.25
block = 0
[../]
[./strain_block]
type = ComputeIncrementalSmallStrain
block = 0
displacements = 'disp_x'
implicit = false
[../]
[./stress_block]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = density
prop_values = 2500
[../]
[]
[Executioner]
type = Transient
start_time = -0.005
end_time = 0.1
dt = 0.005
timestep_tolerance = 1e-6
l_tol = 1e-10
[./TimeIntegrator]
type = CentralDifference
[../]
[]
[Postprocessors]
[./disp_x]
type = NodalVariableValue
nodeid = 1
variable = disp_x
[../]
[./vel_x]
type = NodalVariableValue
nodeid = 1
variable = vel_x
[../]
[./accel_x]
type = NodalVariableValue
nodeid = 1
variable = accel_x
[../]
[]
[Outputs]
exodus = false
csv = true
perf_graph = false
[]
(modules/contact/test/tests/verification/patch_tests/single_pnt_2d/single_point_2d.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = single_point_2d.e
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[]
[Functions]
[./appl_disp]
type = PiecewiseLinear
x = '0 0.001 0.101'
y = '0 0.0 -0.10'
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./incslip_x]
type = PenetrationAux
variable = inc_slip_x
quantity = incremental_slip_x
boundary = 3
paired_boundary = 2
[../]
[./incslip_y]
type = PenetrationAux
variable = inc_slip_y
quantity = incremental_slip_y
boundary = 3
paired_boundary = 2
[../]
[./accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[../]
[./accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[]
[BCs]
[./botx]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./boty]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./topx]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = appl_disp
[../]
[./topy]
type = DirichletBC
variable = disp_y
boundary = 4
value = -0.002001
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e9
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputePlaneFiniteStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputePlaneFiniteStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 4
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 4
[../]
[./disp_x]
type = NodalVariableValue
nodeid = 5
variable = disp_x
[../]
[./disp_y]
type = NodalVariableValue
nodeid = 5
variable = disp_y
[../]
[./inc_slip_x]
type = NodalVariableValue
nodeid = 5
variable = inc_slip_x
[../]
[./inc_slip_y]
type = NodalVariableValue
nodeid = 5
variable = inc_slip_y
[../]
[./accum_slip_x]
type = NodalVariableValue
nodeid = 5
variable = accum_slip_x
[../]
[./accum_slip_y]
type = NodalVariableValue
nodeid = 5
variable = accum_slip_y
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package -mat_superlu_dist_iterrefine'
petsc_options_value = 'lu superlu_dist 1'
line_search = 'none'
l_max_its = 100
nl_max_its = 200
dt = 0.001
end_time = 0.001
num_steps = 10000
nl_rel_tol = 1e-6
nl_abs_tol = 1e-8
dtmin = 0.001
l_tol = 1e-3
[]
[Outputs]
file_base = single_point_2d_out_glued_kin
exodus = true
print_linear_residuals = true
perf_graph = true
csv = true
[./console]
type = Console
max_rows = 5
[../]
[]
[Contact]
[./leftright]
primary = 2
secondary = 3
model = glued
formulation = kinematic
penalty = 1e12
normalize_penalty = true
tangential_tolerance = 1e-3
[../]
[]
(modules/contact/test/tests/verification/hertz_cyl/half_symm_q8/hertz_cyl_half_1deg_template3.i)
[GlobalParams]
order = SECOND
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Mesh]
file = hertz_cyl_half_1deg.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Functions]
[./disp_ramp_vert]
type = PiecewiseLinear
x = '0. 1. 11.'
y = '0. -0.0020 -0.0020'
[../]
[./disp_ramp_horz]
type = PiecewiseLinear
x = '0. 1. 11.'
y = '0. 0.0 0.0014'
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
[../]
[]
[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_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 2
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 2
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 4
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 4
[../]
[./disp_x639]
type = NodalVariableValue
nodeid = 638
variable = disp_x
[../]
[./disp_y639]
type = NodalVariableValue
nodeid = 638
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./side_x]
type = DirichletBC
variable = disp_y
boundary = '1 2'
value = 0.0
[../]
[./bot_y]
type = DirichletBC
variable = disp_x
boundary = '1 2'
value = 0.0
[../]
[./top_y_disp]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = disp_ramp_vert
[../]
[./top_x_disp]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = disp_ramp_horz
[../]
[]
[Materials]
[./stuff1_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e10
poissons_ratio = 0.0
[../]
[./stuff1_strain]
type = ComputeFiniteStrain
block = '1'
[../]
[./stuff1_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./stuff2_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff2_strain]
type = ComputeFiniteStrain
block = '2'
[../]
[./stuff2_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[./stuff3_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '3'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff3_strain]
type = ComputeFiniteStrain
block = '3'
[../]
[./stuff3_stress]
type = ComputeFiniteStrainElasticStress
block = '3'
[../]
[./stuff4_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '4'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff4_strain]
type = ComputeFiniteStrain
block = '4'
[../]
[./stuff4_stress]
type = ComputeFiniteStrainElasticStress
block = '4'
[../]
[./stuff5_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '5'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff5_strain]
type = ComputeFiniteStrain
block = '5'
[../]
[./stuff5_stress]
type = ComputeFiniteStrainElasticStress
block = '5'
[../]
[./stuff6_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '6'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff6_strain]
type = ComputeFiniteStrain
block = '6'
[../]
[./stuff6_stress]
type = ComputeFiniteStrainElasticStress
block = '6'
[../]
[./stuff7_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '7'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff7_strain]
type = ComputeFiniteStrain
block = '7'
[../]
[./stuff7_stress]
type = ComputeFiniteStrainElasticStress
block = '7'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-7
nl_rel_tol = 1e-6
l_max_its = 100
nl_max_its = 200
start_time = 0.0
end_time = 2.0
l_tol = 5e-4
dt = 0.1
dtmin = 0.1
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '3 4'
sort_by = id
[../]
[./y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '3 4'
sort_by = id
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = id
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'x_disp y_disp cont_press'
start_time = 0.9
execute_vector_postprocessors_on = timestep_end
[../]
[./chkfile2]
type = CSV
show = 'bot_react_x bot_react_y disp_x639 disp_y639 top_react_x top_react_y'
start_time = 0.9
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./interface]
primary = 2
secondary = 3
model = coulomb
friction_coefficient = 0.0
formulation = penalty
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
[../]
[]
[Dampers]
[./contact_slip]
type = ContactSlipDamper
primary = '2'
secondary = '3'
[../]
[]
(modules/tensor_mechanics/test/tests/interaction_integral/interaction_integral_3d_points.i)
#This tests the Interaction-Integral evaluation capability.
#This is a 3d extrusion of a 2d plane strain model with 2 elements
#through the thickness, and calculates the Interaction-Integrals using options
#to treat it as 3d.
[GlobalParams]
order = FIRST
# order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[Mesh]
file = crack3d.e
displacements = 'disp_x disp_y disp_z'
[]
[Functions]
[./rampConstant]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = -1e2
[../]
[]
[DomainIntegral]
integrals = 'InteractionIntegralKI InteractionIntegralKII InteractionIntegralKIII'
crack_front_points = '0 -10 .5
0 -10 0
0 -10 -.5'
closed_loop = false # if user provides 'crack_front_points' instead of 'boundary', 'closed_loop' should be set by user!
crack_direction_method = CrackDirectionVector
crack_direction_vector = '1 0 0'
radius_inner = '4.0 5.5'
radius_outer = '5.5 7.0'
block = 1
youngs_modulus = 207000
poissons_ratio = 0.3
output_q = false
incremental = true
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
[../]
[]
[BCs]
[./crack_y]
type = DirichletBC
variable = disp_y
boundary = 100
value = 0.0
[../]
[./no_z]
type = DirichletBC
variable = disp_z
boundary = 500
value = 0.0
[../]
[./no_z2]
type = DirichletBC
variable = disp_z
boundary = 510
value = 0.0
[../]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 700
value = 0.0
[../]
[./Pressure]
[./Side1]
boundary = 400
function = rampConstant
[../]
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_abs_tol = 1e-7
l_tol = 1e-3
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Outputs]
file_base = interaction_integral_3d_points_out
exodus = true
csv = true
[]
(modules/tensor_mechanics/test/tests/plane_stress/weak_plane_stress_incremental.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
temperature = temp
out_of_plane_strain = strain_zz
[]
[Mesh]
[./square]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 2
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./strain_zz]
[../]
[]
[AuxVariables]
[./temp]
[../]
[./nl_strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Postprocessors]
[./react_z]
type = MaterialTensorIntegral
rank_two_tensor = stress
index_i = 2
index_j = 2
[../]
[./min_strain_zz]
type = NodalExtremeValue
variable = strain_zz
value_type = min
[../]
[./max_strain_zz]
type = NodalExtremeValue
variable = strain_zz
value_type = max
[../]
[]
[Modules/TensorMechanics/Master]
[plane_stress]
planar_formulation = WEAK_PLANE_STRESS
strain = SMALL
incremental = true
generate_output = 'stress_xx stress_xy stress_yy stress_zz strain_xx strain_xy strain_yy'
eigenstrain_names = eigenstrain
[]
[]
[AuxKernels]
[./tempfuncaux]
type = FunctionAux
variable = temp
function = tempfunc
use_displaced_mesh = false
[../]
[./strain_zz]
type = RankTwoAux
rank_two_tensor = total_strain
variable = nl_strain_zz
index_i = 2
index_j = 2
[../]
[]
[Functions]
[./pull]
type = PiecewiseLinear
x='0 1 100'
y='0 0.00 0.00'
[../]
[./tempfunc]
type = ParsedFunction
value = '(1 - x) * t'
[../]
[]
[BCs]
[./bottomx]
type = DirichletBC
boundary = 0
variable = disp_x
value = 0.0
[../]
[./bottomy]
type = DirichletBC
boundary = 0
variable = disp_y
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
poissons_ratio = 0.3
youngs_modulus = 1e6
[../]
[./thermal_strain]
type = ComputeThermalExpansionEigenstrain
thermal_expansion_coeff = 0.02
stress_free_temperature = 0.5
eigenstrain_name = eigenstrain
[../]
[./stress]
type = ComputeStrainIncrementBasedStress
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
line_search = none
# controls for linear iterations
l_max_its = 100
l_tol = 1e-06
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-14
nl_abs_tol = 1e-12
# time control
start_time = 0.0
dt = 1.0
dtmin = 1.0
end_time = 2.0
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/beam/static/euler_finite_rot_y_action.i)
# Large strain/large rotation cantilever beam tese
# A 300 N point load is applied at the end of a 4 m long cantilever beam.
# Young's modulus (E) = 1e4
# Shear modulus (G) = 1e8
# shear coefficient (k) = 1.0
# Area (A) = 1.0
# Iy = Iz = 0.16
# The non-dimensionless parameter alpha = kAGL^2/EI = 1e6
# Since the value of alpha is quite high, the beam behaves like
# a thin beam where shear effects are not significant.
# Beam deflection:
# small strain+rot = 3.998 m (exact 4.0)
# large strain + small rotation = -0.05 m in x and 3.74 m in y
# large rotations + small strain = -0.92 m in x and 2.38 m in y
# large rotations + large strain = -0.954 m in x and 2.37 m in y (exact -1.0 m in x and 2.4 m in y)
# References:
# K. E. Bisshopp and D.C. Drucker, Quaterly of Applied Mathematics, Vol 3, No. 3, 1945.
[Mesh]
type = FileMesh
file = beam_finite_rot_test_2.e
displacements = 'disp_x disp_y disp_z'
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./fixy1]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./fixz1]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0.0
[../]
[./fixr1]
type = DirichletBC
variable = rot_x
boundary = 1
value = 0.0
[../]
[./fixr2]
type = DirichletBC
variable = rot_y
boundary = 1
value = 0.0
[../]
[./fixr3]
type = DirichletBC
variable = rot_z
boundary = 1
value = 0.0
[../]
[]
[NodalKernels]
[./force_y2]
type = UserForcingFunctionNodalKernel
variable = disp_y
boundary = 2
function = force
[../]
[]
[Functions]
[./force]
type = PiecewiseLinear
x = '0.0 2.0 8.0'
y = '0.0 300.0 300.0'
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
line_search = 'none'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 4'
nl_max_its = 50
nl_rel_tol = 1e-9
nl_abs_tol = 1e-7
l_max_its = 50
dt = 0.05
end_time = 2.1
[]
[Modules/TensorMechanics/LineElementMaster]
[./all]
add_variables = true
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
strain_type = FINITE
rotation_type = FINITE
# Geometry parameters
area = 1.0
Iy = 0.16
Iz = 0.16
y_orientation = '0.0 1.0 0.0'
[../]
[]
[Materials]
[./elasticity]
type = ComputeElasticityBeam
youngs_modulus = 1e4
poissons_ratio = -0.99995
shear_coefficient = 1.0
block = 1
[../]
[./stress]
type = ComputeBeamResultants
block = 1
[../]
[]
[Postprocessors]
[./disp_x]
type = PointValue
point = '4.0 0.0 0.0'
variable = disp_x
[../]
[./disp_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = disp_y
[../]
[./rot_z]
type = PointValue
point = '4.0 0.0 0.0'
variable = rot_z
[../]
[]
[Outputs]
file_base = 'euler_finite_rot_y_out'
exodus = true
perf_graph = true
[]
(modules/richards/test/tests/gravity_head_2/gh_fu_17.i)
# unsaturated = false
# gravity = true
# full upwinding = true
# transient = true
[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'
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1E-2 1E-1 1E0 1E1 1E3 1E4 1E5 1E6 1E7'
x = '0 1E-1 1E0 1E1 1E2 1E3 1E4 1E5 1E6'
[../]
[]
[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 = 0.1
[../]
[./SUPGgas]
type = RichardsSUPGstandard
p_SUPG = 0.01
[../]
[]
[Variables]
[./pwater]
order = FIRST
family = LAGRANGE
[../]
[./pgas]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./water_ic]
type = ConstantIC
value = 1
variable = pwater
[../]
[./gas_ic]
type = ConstantIC
value = 1
variable = pgas
[../]
[]
[Kernels]
active = 'richardsfwater richardstwater richardsfgas richardstgas'
[./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
[../]
[./mass_error_gas]
type = FunctionValuePostprocessor
function = fcn_mass_error_g
[../]
[./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
[../]
[]
[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((-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'
[../]
[]
[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 -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-15 10000'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
end_time = 1E6
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = gh_fu_17
csv = true
[]
(modules/tensor_mechanics/test/tests/j_integral/j_integral_3d_mouth_dir_end_dir_vec.i)
#This tests the J-Integral evaluation capability.
#This is a 3d extrusion of a 2d plane strain model with 2 elements
#through the thickness, and calculates the J-Integrals using options
#to treat it as 3d.
#Crack direction is defined using the crack mouth coordinates.
#The analytic solution for J1 is 2.434. This model
#converges to that solution with a refined mesh.
#Reference: National Agency for Finite Element Methods and Standards (U.K.):
#Test 1.1 from NAFEMS publication "Test Cases in Linear Elastic Fracture
#Mechanics" R0020.
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[Mesh]
file = crack3d.e
[]
[AuxVariables]
[./SED]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./rampConstant]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = -1e2
[../]
[]
[DomainIntegral]
integrals = JIntegral
boundary = 800
crack_direction_method = CrackMouth
crack_mouth_boundary = 900
crack_end_direction_method = CrackDirectionVector
crack_direction_vector_end_1 = '1.0 0.0 0.0'
crack_direction_vector_end_2 = '1.0 0.0 0.0'
radius_inner = '4.0 5.5'
radius_outer = '5.5 7.0'
output_variable = 'disp_x'
output_q = false
incremental = true
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
[../]
[]
[AuxKernels]
[./SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[../]
[]
[BCs]
[./crack_y]
type = DirichletBC
variable = disp_y
boundary = 100
value = 0.0
[../]
[./no_z]
type = DirichletBC
variable = disp_z
boundary = 500
value = 0.0
[../]
[./no_z2]
type = DirichletBC
variable = disp_z
boundary = 510
value = 0.0
[../]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 700
value = 0.0
[../]
[./Pressure]
[./Side1]
boundary = 400
function = rampConstant
[../]
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_abs_tol = 1e-5
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Postprocessors]
[./disp_x_centercrack]
type = CrackFrontData
crack_front_definition = crackFrontDefinition
variable = disp_x
crack_front_point_index = 1
[../]
[]
[Outputs]
file_base = j_integral_3d_mouth_dir_end_dir_vec_out
exodus = true
csv = true
[]
(modules/combined/test/tests/evolving_mass_density/shear_test_tensors.i)
# Element mass tests
# This series of tests is designed to compute the mass of elements based on
# an evolving mass density calculation. The tests consist of expansion and compression
# of the elastic patch test model along each axis, uniform expansion and compression,
# and shear in each direction. The expansion and compression tests change the volume of
# the elements. The corresponding change in density should compensate for this so the
# mass remains constant. The shear tests should not result in a volume change, and this
# is checked too. The mass calculation is done with the post processor called Mass.
# The tests/file names are as follows:
# Expansion and compression along a single axis
# expand_compress_x_test_out.e
# expand_compress_y_test_out.e
# expand_compress_z_test_out.e
# Volumetric expansion and compression
# uniform_expand_compress_test.i
# Zero volume change shear along each axis
# shear_x_test_out.e
# shear_y_test_out.e
# shear_z_test_out.e
# The resulting mass calculation for these tests should always be = 1.
# This test is a duplicate of the uniform_expand_compress_test.i test for solid mechanics, and the
# output of this tensor mechanics test is compared to the original
# solid mechanics output. The duplication is necessary to test the
# migrated tensor mechanics version while maintaining tests for solid mechanics.
[Mesh]
file = elastic_patch.e
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Functions]
[./rampConstant1]
type = PiecewiseLinear
x = '0.00 1.00 2.0 3.00'
y = '0.00 0.25 0.0 -0.25'
scale_factor = 1
[../]
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./TensorMechanics]
[../]
[]
[BCs]
[./bot_x]
type = DirichletBC
variable = disp_x
value = 0.0
[../]
[./bot_y]
type = DirichletBC
variable = disp_y
value = 0
[../]
[./bot_z]
type = DirichletBC
variable = disp_z
value = 0
[../]
[./top_x]
variable = disp_x
preset = false
[../]
[./top_y]
variable = disp_y
preset = false
[../]
[./top_z]
variable = disp_z
preset = false
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = '1 2 3 4 5 6 7'
youngs_modulus = 1e6
poissons_ratio = 0.0
[../]
[./small_strain]
type = ComputeSmallStrain
block = ' 1 2 3 4 5 6 7'
[../]
[./elastic_stress]
type = ComputeLinearElasticStress
block = '1 2 3 4 5 6 7'
[../]
[]
[Executioner]
type = Transient
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
nl_abs_tol = 1e-10
l_max_its = 20
start_time = 0.0
dt = 1.0
num_steps = 3
end_time = 3.0
[] # Executioner
[Outputs]
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[] # Outputs
[Postprocessors]
[./Mass]
type = Mass
variable = disp_x
execute_on = 'initial timestep_end'
[../]
[]
(modules/combined/test/tests/cavity_pressure/multiple_postprocessors.i)
#
# Cavity Pressure Test (Volume input as a vector of postprocessors)
#
# This test is designed to compute an internal pressure based on
# p = n * R * T / V
# where
# p is the pressure
# n is the amount of material in the volume (moles)
# R is the universal gas constant
# T is the temperature
# V is the volume
#
# The mesh is composed of one block (1) with an interior cavity of volume 8.
# Block 2 sits in the cavity and has a volume of 1. Thus, the total
# initial volume is 7.
# The test adjusts n, T, and V in the following way:
# n => n0 + alpha * t
# T => T0 + beta * t
# V => V0 + gamma * t
# with
# alpha = n0
# beta = T0 / 2
# gamma = - (0.003322259...) * V0
# T0 = 240.54443866068704
# V0 = 7
# n0 = f(p0)
# p0 = 100
# R = 8.314472 J * K^(-1) * mol^(-1)
#
# So, n0 = p0 * V0 / R / T0 = 100 * 7 / 8.314472 / 240.544439
# = 0.35
#
# In this test the internal volume is calculated as the sum of two Postprocessors
# internalVolumeInterior and internalVolumeExterior. This sum equals the value
# reported by the internalVolume postprocessor.
#
# The parameters combined at t = 1 gives p = 301.
#
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[Mesh]
file = 3d.e
[]
[Functions]
[./displ_positive]
type = PiecewiseLinear
x = '0 1'
y = '0 0.0029069767441859684'
[../]
[./displ_negative]
type = PiecewiseLinear
x = '0 1'
y = '0 -0.0029069767441859684'
[../]
[./temp1]
type = PiecewiseLinear
x = '0 1'
y = '1 1.5'
scale_factor = 240.54443866068704
[../]
[./material_input_function]
type = PiecewiseLinear
x = '0 1'
y = '0 0.35'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[./temp]
initial_condition = 240.54443866068704
[../]
[./material_input]
[../]
[]
[AuxVariables]
[./pressure_residual_x]
[../]
[./pressure_residual_y]
[../]
[./pressure_residual_z]
[../]
[./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_zx]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
[../]
[./heat]
type = Diffusion
variable = temp
use_displaced_mesh = true
[../]
[./material_input_dummy]
type = Diffusion
variable = material_input
use_displaced_mesh = true
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 0
variable = stress_xx
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 1
variable = stress_yy
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 2
variable = stress_zz
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 1
variable = stress_xy
[../]
[./stress_yz]
type = RankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 2
variable = stress_yz
[../]
[./stress_zx]
type = RankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 0
variable = stress_zx
[../]
[]
[BCs]
[./no_x_exterior]
type = DirichletBC
variable = disp_x
boundary = '7 8'
value = 0.0
[../]
[./no_y_exterior]
type = DirichletBC
variable = disp_y
boundary = '9 10'
value = 0.0
[../]
[./no_z_exterior]
type = DirichletBC
variable = disp_z
boundary = '11 12'
value = 0.0
[../]
[./prescribed_left]
type = FunctionDirichletBC
variable = disp_x
boundary = 13
function = displ_positive
[../]
[./prescribed_right]
type = FunctionDirichletBC
variable = disp_x
boundary = 14
function = displ_negative
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = '15 16'
value = 0.0
[../]
[./no_z]
type = DirichletBC
variable = disp_z
boundary = '17 18'
value = 0.0
[../]
[./no_x_interior]
type = DirichletBC
variable = disp_x
boundary = '1 2'
value = 0.0
[../]
[./no_y_interior]
type = DirichletBC
variable = disp_y
boundary = '3 4'
value = 0.0
[../]
[./no_z_interior]
type = DirichletBC
variable = disp_z
boundary = '5 6'
value = 0.0
[../]
[./temperatureInterior]
type = FunctionDirichletBC
boundary = 100
function = temp1
variable = temp
[../]
[./MaterialInput]
type = FunctionDirichletBC
boundary = '100 13 14 15 16'
function = material_input_function
variable = material_input
[../]
[./CavityPressure]
[./1]
boundary = 100
initial_pressure = 100
material_input = materialInput
R = 8.314472
temperature = aveTempInterior
volume = 'internalVolumeInterior internalVolumeExterior'
startup_time = 0.5
output = ppress
save_in = 'pressure_residual_x pressure_residual_y pressure_residual_z'
[../]
[../]
[]
[Materials]
[./elast_tensor1]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e1
poissons_ratio = 0
block = 1
[../]
[./strain1]
type = ComputeFiniteStrain
block = 1
[../]
[./stress1]
type = ComputeFiniteStrainElasticStress
block = 1
[../]
[./elast_tensor2]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0
block = 2
[../]
[./strain2]
type = ComputeFiniteStrain
block = 2
[../]
[./stress2]
type = ComputeFiniteStrainElasticStress
block = 2
[../]
[]
[Executioner]
type = Transient
petsc_options_iname = '-pc_type -sub_pc_type'
petsc_options_value = 'asm lu'
nl_rel_tol = 1e-12
l_tol = 1e-12
l_max_its = 20
dt = 0.5
end_time = 1.0
[]
[Postprocessors]
[./internalVolume]
type = InternalVolume
boundary = 100
execute_on = 'initial linear'
[../]
[./aveTempInterior]
type = SideAverageValue
boundary = 100
variable = temp
execute_on = 'initial linear'
[../]
[./internalVolumeInterior]
type = InternalVolume
boundary = '1 2 3 4 5 6'
execute_on = 'initial linear'
[../]
[./internalVolumeExterior]
type = InternalVolume
boundary = '13 14 15 16 17 18'
execute_on = 'initial linear'
[../]
[./materialInput]
type = SideAverageValue
boundary = '7 8 9 10 11 12'
variable = material_input
execute_on = linear
[../]
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_htonly/gap_heat_transfer_htonly_it_plot_test.i)
#
# 1-D Gap Heat Transfer Test without mechanics
#
# This test exercises 1-D gap heat transfer for a constant conductivity gap.
#
# The mesh consists of two element blocks containing one element each. Each
# element is a unit cube. They sit next to one another with a unit between them.
#
# The conductivity of both blocks is set very large to achieve a uniform temperature
# across each block. The temperature of the far left boundary
# is ramped from 100 to 200 over one time unit, and then held fixed for an additional
# time unit. The temperature of the far right boundary is held fixed at 100.
#
# A simple analytical solution is possible for the heat flux between the blocks:
#
# Flux = (T_left - T_right) * (gapK/gap_width)
#
# The gap conductivity is specified as 1, thus
#
# gapK(Tavg) = 1.0*Tavg
#
#
# The heat flux across the gap at time = 2 is then:
#
# Flux(2) = 100 * (1.0/1.0) = 100
#
# For comparison, see results from the flux post processors
#
[Mesh]
file = gap_heat_transfer_htonly_test.e
[]
[Functions]
[./temp]
type = PiecewiseLinear
x = '0 1 2'
y = '100 200 200'
[../]
[]
[ThermalContact]
[./thermal_contact]
type = GapHeatTransfer
variable = temp
primary = 3
secondary = 2
emissivity_primary = 0
emissivity_secondary = 0
[../]
[]
[Variables]
[./temp]
order = FIRST
family = LAGRANGE
initial_condition = 100
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[]
[BCs]
[./temp_far_left]
type = FunctionDirichletBC
boundary = 1
variable = temp
function = temp
[../]
[./temp_far_right]
type = DirichletBC
boundary = 4
variable = temp
value = 100
[../]
[]
[Materials]
[./heat1]
type = HeatConductionMaterial
block = '1 2'
specific_heat = 1.0
thermal_conductivity = 100000000.0
[../]
[./density]
type = GenericConstantMaterial
block = '1 2'
prop_names = 'density'
prop_values = '1.0'
[../]
[]
[Executioner]
type = Transient
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 4'
line_search = 'none'
nl_abs_tol = 1e-5
nl_rel_tol = 1e-12
l_tol = 1e-10
l_max_its = 100
start_time = 0.0
dt = 1e-1
end_time = 2.0
[]
[Postprocessors]
[./temp_left]
type = SideAverageValue
boundary = 2
variable = temp
[../]
[./temp_right]
type = SideAverageValue
boundary = 3
variable = temp
[../]
[./flux_left]
type = SideFluxIntegral
variable = temp
boundary = 2
diffusivity = thermal_conductivity
[../]
[./flux_right]
type = SideFluxIntegral
variable = temp
boundary = 3
diffusivity = thermal_conductivity
[../]
[]
[Outputs]
file_base = out_it_plot
[./exodus]
type = Exodus
execute_on = 'initial timestep_end nonlinear'
nonlinear_residual_dt_divisor = 100
[../]
[]
(modules/combined/test/tests/gap_heat_transfer_convex/gap_heat_transfer_convex.i)
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
temperature = temp
[]
[Mesh]
file = gap_heat_transfer_convex.e
[]
[Functions]
[./disp]
type = PiecewiseLinear
x = '0 2.0'
y = '0 1.0'
[../]
[./temp]
type = PiecewiseLinear
x = '0 1'
y = '200 200'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[./temp]
initial_condition = 100
[../]
[]
[ThermalContact]
[./thermal_contact]
type = GapHeatTransfer
variable = temp
primary = 2
secondary = 3
emissivity_primary = 0
emissivity_secondary = 0
[../]
[]
[Modules/TensorMechanics/Master/All]
volumetric_locking_correction = true
strain = FINITE
eigenstrain_names = eigenstrain
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[]
[BCs]
[./move_right]
type = FunctionDirichletBC
boundary = '3'
variable = disp_x
function = disp
[../]
[./fixed_x]
type = DirichletBC
boundary = '1'
variable = disp_x
value = 0
[../]
[./fixed_y]
type = DirichletBC
boundary = '1 2 3 4'
variable = disp_y
value = 0
[../]
[./fixed_z]
type = DirichletBC
boundary = '1 2 3 4'
variable = disp_z
value = 0
[../]
[./temp_bottom]
type = FunctionDirichletBC
boundary = 1
variable = temp
function = temp
[../]
[./temp_top]
type = DirichletBC
boundary = 4
variable = temp
value = 100
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = '1 2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./thermal_strain]
type = ComputeThermalExpansionEigenstrain
stress_free_temperature = 100
thermal_expansion_coeff = 0
eigenstrain_name = eigenstrain
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[./heat1]
type = HeatConductionMaterial
block = 1
specific_heat = 1.0
thermal_conductivity = 1.0
[../]
[./heat2]
type = HeatConductionMaterial
block = 2
specific_heat = 1.0
thermal_conductivity = 1.0
[../]
[./density]
type = Density
block = '1 2'
density = 1.0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
start_time = 0.0
dt = 0.1
end_time = 2.0
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/domain_integral_thermal/c_integral_2d.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[Mesh]
file = crack2d.e
[]
[AuxVariables]
[./SERD]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./rampConstantUp]
type = PiecewiseLinear
x = '0. 0.1 100.0'
y = '0. 1 1'
scale_factor = -68.95 #MPa
[../]
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
planar_formulation = PLANE_STRAIN
[../]
[]
[AuxKernels]
[./SERD]
type = MaterialRealAux
variable = SERD
property = strain_energy_rate_density
execute_on = timestep_end
[../]
[]
[BCs]
[./crack_y]
type = DirichletBC
variable = disp_y
boundary = 100
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = 400
value = 0.0
[../]
[./no_x1]
type = DirichletBC
variable = disp_x
boundary = 900
value = 0.0
[../]
[./Pressure]
[./crack_pressure]
boundary = 700
function = rampConstantUp
[../]
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 206800
poissons_ratio = 0.0
[../]
[./radial_return_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'powerlawcrp'
[../]
[./powerlawcrp]
type = PowerLawCreepStressUpdate
coefficient = 3.125e-21 # 7.04e-17 #
n_exponent = 2.0
m_exponent = 0.0
activation_energy = 0.0
[../]
[]
[DomainIntegral]
integrals = CIntegral
boundary = 800
crack_direction_method = CrackDirectionVector
crack_direction_vector = '1 0 0'
2d = true
axis_2d = 2
radius_inner = '60.0 80.0 100.0 120.0'
radius_outer = '80.0 100.0 120.0 140.0'
incremental = true
inelastic_models = 'powerlawcrp'
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_ksp_type -sub_pc_type -pc_asm_overlap'
petsc_options_value = 'asm 31 preonly lu 1'
line_search = 'none'
l_max_its = 50
nl_max_its = 40
nl_rel_step_tol= 1e-10
nl_rel_tol = 1e-10
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Outputs]
exodus = true
[]
[Preconditioning]
[./smp]
type = SMP
pc_side = left
ksp_norm = preconditioned
full = true
[../]
[]
(modules/contact/test/tests/simple_contact/simple_contact_rz_test.i)
#
# The analytic solution is:
# disp_x = -7e-5 * x
# disp_y = 6e-5 * y
# stress_xx = stress_zz = -100
# stress_yy = stress_xy = 0
#
# Note: Run merged_rz.i to generate a solution to compare to that doesn't use contact.
[Mesh]
file = contact_rz.e
# PETSc < 3.5.0 requires the iteration patch_update_strategy to
# avoid PenetrationLocator warnings, which are currently treated as
# errors by the TestHarness.
patch_update_strategy = 'iteration'
[]
[GlobalParams]
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Problem]
coord_type = RZ
[]
[Functions]
[./pressure]
type = PiecewiseLinear
x = '0 1'
y = '0 1'
scale_factor = 100
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
incremental = true
strain = FINITE
generate_output = 'stress_xx stress_xy stress_zx stress_yy stress_zz stress_yz'
[../]
[]
[Contact]
[./dummy_name]
primary = 3
secondary = 2
penalty = 1e5
[../]
[]
[BCs]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./bottom_y]
type = DirichletBC
variable = disp_y
boundary = 10
value = 0.0
[../]
[./Pressure]
[./right_pressure]
boundary = 4
function = pressure
[../]
[../]
[]
[Materials]
[./stiffStuff]
type = ComputeIsotropicElasticityTensor
block = '1 2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stiffStuff_stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type '
petsc_options_value = 'lu '
line_search = 'none'
nl_abs_tol = 1e-9
nl_rel_tol = 1e-9
l_max_its = 20
dt = 1.0
end_time = 1.0
[]
[Outputs]
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[]
(modules/combined/test/tests/cavity_pressure/rz.i)
#
# Cavity Pressure Test
#
# This test is designed to compute an internal pressure based on
# p = n * R * T / V
# where
# p is the pressure
# n is the amount of material in the volume (moles)
# R is the universal gas constant
# T is the temperature
# V is the volume
#
# The mesh is composed of one block (2) with an interior cavity of volume 8.
# Block 1 sits in the cavity and has a volume of 1. Thus, the total
# initial volume is 7.
# The test adjusts T in the following way:
# T => T0 + beta * t
# with
# beta = T0
# T0 = 240.54443866068704
# V0 = 7
# n0 = f(p0)
# p0 = 100
# R = 8.314472 J * K^(-1) * mol^(-1)
#
# So, n0 = p0 * V0 / R / T0 = 100 * 7 / 8.314472 / 240.544439
# = 0.35
#
# At t = 1, p = 200.
[Problem]
coord_type = RZ
[]
[GlobalParams]
displacements = 'disp_r disp_z'
[]
[Mesh]
file = rz.e
[]
[Functions]
[./temperature]
type = PiecewiseLinear
x = '0 1'
y = '1 2'
scale_factor = 240.54443866068704
[../]
[]
[Variables]
[./disp_r]
[../]
[./disp_z]
[../]
[./temp]
initial_condition = 240.54443866068704
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
[../]
[./heat]
type = Diffusion
variable = temp
use_displaced_mesh = true
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
variable = disp_r
boundary = '1 2'
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_z
boundary = '1 2'
value = 0.0
[../]
[./temperatureInterior]
type = FunctionDirichletBC
boundary = 2
function = temperature
variable = temp
[../]
[./CavityPressure]
[./1]
boundary = 2
initial_pressure = 100
R = 8.314472
temperature = aveTempInterior
volume = internalVolume
startup_time = 0.5
output = ppress
[../]
[../]
[]
[Materials]
[./elastic_tensor1]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
block = 1
[../]
[./strain1]
type = ComputeAxisymmetricRZFiniteStrain
block = 1
[../]
[./stress1]
type = ComputeFiniteStrainElasticStress
block = 1
[../]
[./elastic_tensor2]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
block = 2
[../]
[./strain2]
type = ComputeAxisymmetricRZFiniteStrain
block = 2
[../]
[./stress2]
type = ComputeFiniteStrainElasticStress
block = 2
[../]
[]
[Executioner]
type = Transient
petsc_options_iname = '-pc_type -sub_pc_type'
petsc_options_value = 'asm lu'
nl_abs_tol = 1e-10
l_max_its = 20
dt = 0.5
end_time = 1.0
[]
[Postprocessors]
[./internalVolume]
type = InternalVolume
boundary = 2
execute_on = 'initial linear'
[../]
[./aveTempInterior]
type = SideAverageValue
boundary = 2
variable = temp
execute_on = 'initial linear'
[../]
[]
[Outputs]
exodus = true
[./checkpoint]
type = Checkpoint
num_files = 1
[../]
[]
(modules/tensor_mechanics/test/tests/dynamics/rayleigh_damping/rayleigh_hht.i)
# Test for rayleigh damping implemented using HHT time integration
#
# The test is for an 1D bar element of unit length fixed on one end
# with a ramped pressure boundary condition applied to the other end.
# zeta and eta correspond to the stiffness and mass proportional rayleigh damping
# alpha, beta and gamma are HHT time integration parameters
# The equation of motion in terms of matrices is:
#
# M*accel + (eta*M+zeta*K)*[(1+alpha)vel-alpha vel_old]
# + alpha*(K*disp - K*disp_old) + K*disp = P(t+alpha dt)*Area
#
# Here M is the mass matrix, K is the stiffness matrix, P is the applied pressure
#
# This equation is equivalent to:
#
# density*accel + eta*density*[(1+alpha)vel-alpha vel_old]
# + zeta*[(1+alpha)*d/dt(Div stress)- alpha*d/dt(Div stress_old)]
# + alpha *(Div stress - Div stress_old) +Div Stress= P(t+alpha dt)
#
# The first two terms on the left are evaluated using the Inertial force kernel
# The next three terms on the left involving zeta and alpha are evaluated using
# the DynamicStressDivergenceTensors Kernel
# The residual due to Pressure is evaluated using Pressure boundary condition
#
# The system will come to steady state slowly after the pressure becomes constant.
# Alpha equal to zero will result in Newmark integration.
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = 0.0
xmax = 0.1
ymin = 0.0
ymax = 1.0
zmin = 0.0
zmax = 0.1
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./vel_x]
[../]
[./accel_x]
[../]
[./vel_y]
[../]
[./accel_y]
[../]
[./vel_z]
[../]
[./accel_z]
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./DynamicTensorMechanics]
displacements = 'disp_x disp_y disp_z'
zeta = 0.1
alpha = 0.11
[../]
[./inertia_x]
type = InertialForce
variable = disp_x
velocity = vel_x
acceleration = accel_x
beta = 0.25
gamma = 0.5
eta=0.1
alpha = 0.11
[../]
[./inertia_y]
type = InertialForce
variable = disp_y
velocity = vel_y
acceleration = accel_y
beta = 0.25
gamma = 0.5
eta=0.1
alpha = 0.11
[../]
[./inertia_z]
type = InertialForce
variable = disp_z
velocity = vel_z
acceleration = accel_z
beta = 0.25
gamma = 0.5
eta = 0.1
alpha = 0.11
[../]
[]
[AuxKernels]
[./accel_x]
type = NewmarkAccelAux
variable = accel_x
displacement = disp_x
velocity = vel_x
beta = 0.25
execute_on = timestep_end
[../]
[./vel_x]
type = NewmarkVelAux
variable = vel_x
acceleration = accel_x
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_y]
type = NewmarkAccelAux
variable = accel_y
displacement = disp_y
velocity = vel_y
beta = 0.25
execute_on = timestep_end
[../]
[./vel_y]
type = NewmarkVelAux
variable = vel_y
acceleration = accel_y
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_z]
type = NewmarkAccelAux
variable = accel_z
displacement = disp_z
velocity = vel_z
beta = 0.25
execute_on = timestep_end
[../]
[./vel_z]
type = NewmarkVelAux
variable = vel_z
acceleration = accel_z
gamma = 0.5
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 0
index_j = 1
[../]
[./strain_yy]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_yy
index_i = 0
index_j = 1
[../]
[]
[BCs]
[./top_y]
type = DirichletBC
variable = disp_y
boundary = top
value=0.0
[../]
[./top_x]
type = DirichletBC
variable = disp_x
boundary = top
value=0.0
[../]
[./top_z]
type = DirichletBC
variable = disp_z
boundary = top
value=0.0
[../]
[./bottom_x]
type = DirichletBC
variable = disp_x
boundary = bottom
value=0.0
[../]
[./bottom_z]
type = DirichletBC
variable = disp_z
boundary = bottom
value=0.0
[../]
[./Pressure]
[./Side1]
boundary = bottom
function = pressure
factor = 1
alpha = 0.11
displacements = 'disp_x disp_y disp_z'
[../]
[../]
[]
[Materials]
[./Elasticity_tensor]
type = ComputeElasticityTensor
block = 0
fill_method = symmetric_isotropic
C_ijkl = '210e9 0'
[../]
[./strain]
type = ComputeSmallStrain
block = 0
displacements = 'disp_x disp_y disp_z'
[../]
[./stress]
type = ComputeLinearElasticStress
block = 0
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = 'density'
prop_values = '7750'
[../]
[]
[Executioner]
type = Transient
start_time = 0
end_time = 2
dt = 0.1
[]
[Functions]
[./pressure]
type = PiecewiseLinear
x = '0.0 0.1 0.2 1.0 2.0 5.0'
y = '0.0 0.1 0.2 1.0 1.0 1.0'
scale_factor = 1e9
[../]
[]
[Postprocessors]
[./_dt]
type = TimestepSize
[../]
[./disp]
type = NodalMaxValue
variable = disp_y
boundary = bottom
[../]
[./vel]
type = NodalMaxValue
variable = vel_y
boundary = bottom
[../]
[./accel]
type = NodalMaxValue
variable = accel_y
boundary = bottom
[../]
[./stress_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./strain_yy]
type = ElementAverageValue
variable = strain_yy
[../]
[]
[Outputs]
exodus = true
perf_graph = true
[]
(modules/tensor_mechanics/test/tests/ad_thermal_expansion_function/finite_linear.i)
# This tests the thermal expansion coefficient function using both
# options to specify that function: mean and instantaneous. There
# two blocks, each containing a single element, and these use the
# two variants of the function.
# In this test, the instantaneous CTE function is a linear function
# while the mean CTE function is an analytic function designed to
# give the same response. If \bar{alpha}(T) is the mean CTE function,
# and \alpha(T) is the instantaneous CTE function,
# \bar{\alpha}(T) = 1/(T-Tref) \intA^{T}_{Tsf} \alpha(T) dT
# where Tref is the reference temperature used to define the mean CTE
# function, and Tsf is the stress-free temperature.
# This version of the test uses finite deformation theory.
# The two models produce very similar results. There are slight
# differences due to the large deformation treatment.
[Mesh]
file = 'blocks.e'
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[AuxVariables]
[./temp]
order = FIRST
family = LAGRANGE
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
eigenstrain_names = eigenstrain
generate_output = 'strain_xx strain_yy strain_zz'
use_automatic_differentiation = true
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = disp_x
boundary = 3
value = 0.0
[../]
[./bottom]
type = DirichletBC
variable = disp_y
boundary = 2
value = 0.0
[../]
[./back]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0.0
[../]
[]
[AuxKernels]
[./temp]
type = FunctionAux
variable = temp
block = '1 2'
function = temp_func
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./small_stress]
type = ADComputeFiniteStrainElasticStress
[../]
[./thermal_expansion_strain1]
type = ADComputeMeanThermalExpansionFunctionEigenstrain
block = 1
thermal_expansion_function = cte_func_mean
thermal_expansion_function_reference_temperature = 0.5
stress_free_temperature = 0.0
temperature = temp
eigenstrain_name = eigenstrain
[../]
[./thermal_expansion_strain2]
type = ADComputeInstantaneousThermalExpansionFunctionEigenstrain
block = 2
thermal_expansion_function = cte_func_inst
stress_free_temperature = 0.0
temperature = temp
eigenstrain_name = eigenstrain
[../]
[]
[Functions]
[./cte_func_mean]
type = ParsedFunction
vars = 'tsf tref scale' #stress free temp, reference temp, scale factor
vals = '0.0 0.5 1e-4'
value = 'scale * (0.5 * t^2 - 0.5 * tsf^2) / (t - tref)'
[../]
[./cte_func_inst]
type = PiecewiseLinear
xy_data = '0 0.0
2 2.0'
scale_factor = 1e-4
[../]
[./temp_func]
type = PiecewiseLinear
xy_data = '0 1
1 2'
[../]
[]
[Postprocessors]
[./disp_1]
type = NodalMaxValue
variable = disp_x
boundary = 101
[../]
[./disp_2]
type = NodalMaxValue
variable = disp_x
boundary = 102
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
l_max_its = 100
l_tol = 1e-4
nl_abs_tol = 1e-8
nl_rel_tol = 1e-12
start_time = 0.0
end_time = 1.0
dt = 0.1
[]
[Outputs]
csv = true
[]
(test/tests/geomsearch/3d_moving_penetration_smoothing/pl_test3nstt.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
file = pl_test3tt.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./normal_z]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./closest_point_z]
[../]
# [./element_id]
# [../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[./diff_z]
type = Diffusion
variable = disp_z
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
tangential_tolerance = 0.09
normal_smoothing_distance = 0.2
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
tangential_tolerance = 0.09
normal_smoothing_distance = 0.2
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = normal_z
boundary = 11
paired_boundary = 12
quantity = normal_z
[../]
[./penetrate10]
type = PenetrationAux
variable = normal_z
boundary = 12
paired_boundary = 11
quantity = normal_z
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate13]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate14]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate15]
type = PenetrationAux
variable = closest_point_z
boundary = 11
paired_boundary = 12
quantity = closest_point_z
[../]
[./penetrate16]
type = PenetrationAux
variable = closest_point_z
boundary = 12
paired_boundary = 11
quantity = closest_point_z
[../]
# [./penetrate17]
# type = PenetrationAux
# variable = element_id
# boundary = 11
# paired_boundary = 12
# quantity = element_id
# [../]
#
# [./penetrate18]
# type = PenetrationAux
# variable = element_id
# boundary = 12
# paired_boundary = 11
# quantity = element_id
# [../]
[./penetrate19]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate20]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
preset = false
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
preset = false
boundary = 1
value = 0
[../]
[./b1z]
type = DirichletBC
variable = disp_z
preset = false
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
preset = false
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
preset = false
boundary = 2
function = disp_y
[../]
[./b2z]
type = DirichletBC
variable = disp_z
preset = false
boundary = 2
value = 0
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-9
l_max_its = 10
start_time = 0.0
dt = 0.02
end_time = 1.0
[]
[Outputs]
file_base = pl_test3nstt_out
exodus = true
[]
(modules/porous_flow/test/tests/dirackernels/bh04.i)
# fully-saturated
# production
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = -1
xmax = 1
ymin = -1
ymax = 1
zmin = -1
zmax = 1
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Functions]
[dts]
type = PiecewiseLinear
y = '1E-2 1E-1 1 1E1 1E2 1E3'
x = '0 1E-1 1 1E1 1E2 1E3'
[]
[]
[Variables]
[pp]
initial_condition = 0
[]
[]
[Kernels]
[mass0]
type = PorousFlowMassTimeDerivative
fluid_component = 0
variable = pp
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[borehole_total_outflow_mass]
type = PorousFlowSumQuantity
[]
[pc]
type = PorousFlowCapillaryPressureVG
m = 0.8
alpha = 1e-5
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 2e9
viscosity = 1e-3
density0 = 1000
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
[]
[porosity]
type = PorousFlowPorosityConst
porosity = 0.1
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1E-12 0 0 0 1E-12 0 0 0 1E-12'
[]
[relperm]
type = PorousFlowRelativePermeabilityFLAC
m = 2
phase = 0
[]
[]
[DiracKernels]
[bh]
type = PorousFlowPeacemanBorehole
variable = pp
SumQuantityUO = borehole_total_outflow_mass
point_file = bh02.bh
fluid_phase = 0
bottom_p_or_t = -1E6
unit_weight = '0 0 0'
use_mobility = true
character = 1
[]
[]
[Postprocessors]
[bh_report]
type = PorousFlowPlotQuantity
uo = borehole_total_outflow_mass
[]
[fluid_mass0]
type = PorousFlowFluidMass
execute_on = timestep_begin
[]
[fluid_mass1]
type = PorousFlowFluidMass
execute_on = timestep_end
[]
[zmass_error]
type = FunctionValuePostprocessor
function = mass_bal_fcn
execute_on = timestep_end
[]
[p0]
type = PointValue
variable = pp
point = '0 0 0'
execute_on = timestep_end
[]
[]
[Functions]
[mass_bal_fcn]
type = ParsedFunction
value = abs((a-c+d)/2/(a+c))
vars = 'a c d'
vals = 'fluid_mass1 fluid_mass0 bh_report'
[]
[]
[Preconditioning]
[usual]
type = SMP
full = true
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -ksp_max_it'
petsc_options_value = 'bcgs bjacobi 1E-10 1E-10 10000 30'
[]
[]
[Executioner]
type = Transient
end_time = 1E3
solve_type = NEWTON
[TimeStepper]
type = FunctionDT
function = dts
[]
[]
[Outputs]
file_base = bh04
exodus = false
csv = true
execute_on = timestep_end
[]
(modules/porous_flow/test/tests/dirackernels/hfrompps.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 3
ny = 3
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Variables]
[pressure]
[]
[temperature]
scaling = 1E-6
[]
[]
[ICs]
[pressure_ic]
type = ConstantIC
variable = pressure
value = 1e6
[]
[temperature_ic]
type = ConstantIC
variable = temperature
value = 400
[]
[]
[Kernels]
[P_time_deriv]
type = PorousFlowMassTimeDerivative
fluid_component = 0
variable = pressure
[]
[P_flux]
type = PorousFlowAdvectiveFlux
fluid_component = 0
variable = pressure
gravity = '0 -9.8 0'
[]
[energy_dot]
type = PorousFlowEnergyTimeDerivative
variable = temperature
[]
[heat_conduction]
type = PorousFlowHeatConduction
variable = temperature
[]
[heat_advection]
type = PorousFlowHeatAdvection
variable = temperature
gravity = '0 -9.8 0'
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pressure temperature'
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureConst
[]
[]
[Functions]
[mass_flux_in_fn]
type = PiecewiseConstant
direction = left
xy_data = '
0 0
100 0.1
300 0
600 0.1
1400 0
1500 0.2'
[]
[T_in_fn]
type = PiecewiseLinear
xy_data = '
0 400
600 450'
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 2e9
density0 = 1000
thermal_expansion = 0
[]
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
temperature = temperature
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pressure
capillary_pressure = pc
[]
[massfrac]
type = PorousFlowMassFraction
at_nodes = true
[]
[fluid_props]
type = PorousFlowSingleComponentFluid
phase = 0
fp = simple_fluid
[]
[relperm]
type = PorousFlowRelativePermeabilityCorey
n = 1
phase = 0
[]
[fp_mat]
type = FluidPropertiesMaterialPT
pressure = pressure
temperature = temperature
fp = simple_fluid
[]
[rock_heat]
type = PorousFlowMatrixInternalEnergy
specific_heat_capacity = 830.0
density = 2750
[]
[thermal_conductivity]
type = PorousFlowThermalConductivityIdeal
dry_thermal_conductivity = '2.5 0 0 0 2.5 0 0 0 2.5'
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1.0E-15 0 0 0 1.0E-15 0 0 0 1.0E-14'
[]
[porosity]
type = PorousFlowPorosityConst
porosity = 0.1
[]
[]
[DiracKernels]
[source]
type = PorousFlowPointSourceFromPostprocessor
variable = pressure
mass_flux = mass_flux_in
point = '0.5 0.5 0'
[]
[source_h]
type = PorousFlowPointEnthalpySourceFromPostprocessor
variable = temperature
mass_flux = mass_flux_in
point = '0.5 0.5 0'
T_in = T_in
pressure = pressure
fp = simple_fluid
[]
[]
[Preconditioning]
[preferred]
type = SMP
full = true
petsc_options_iname = '-pc_type'
petsc_options_value = ' lu '
[]
[]
[Postprocessors]
[total_mass]
type = PorousFlowFluidMass
execute_on = 'initial timestep_end'
[]
[total_heat]
type = PorousFlowHeatEnergy
[]
[mass_flux_in]
type = FunctionValuePostprocessor
function = mass_flux_in_fn
execute_on = 'initial timestep_end'
[]
[avg_temp]
type = ElementAverageValue
variable = temperature
execute_on = 'initial timestep_end'
[]
[T_in]
type = FunctionValuePostprocessor
function = T_in_fn
execute_on = 'initial timestep_end'
[]
[]
[Executioner]
type = Transient
solve_type = Newton
nl_abs_tol = 1e-14
dt = 100
end_time = 2000
[]
[Outputs]
csv = true
execute_on = 'initial timestep_end'
file_base = hfrompps
[]
(modules/richards/test/tests/gravity_head_2/gh_fu_05.i)
# unsaturated = true
# gravity = false
# supg = false
# transient = true
[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'
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1E-2 1E-1 1E0 1E1 1E3 1E4 1E5 1E6 1E7'
x = '0 1E-1 1E0 1E1 1E2 1E3 1E4 1E5 1E6'
[../]
[]
[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 = 0.2
max = 0.8
variable = pwater
[../]
[./gas_ic]
type = RandomIC
min = 1.2
max = 1.8
variable = pgas
[../]
[]
[Kernels]
active = 'richardsfwater richardstwater richardsfgas richardstgas'
[./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
[../]
[./mass_error_gas]
type = FunctionValuePostprocessor
function = fcn_mass_error_g
[../]
[./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 = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-10 1E-10 10000'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
end_time = 1E6
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = gh_fu_05
csv = true
[]
(modules/richards/test/tests/gravity_head_2/gh08.i)
# unsaturated = true
# gravity = true
# supg = true
# transient = true
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
xmin = 0
xmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1E-2 1E-1 1E0 1E1 1E3 1E4 1E5 1E6 1E7'
x = '0 1E-1 1E0 1E1 1E2 1E3 1E4 1E5 1E6'
[../]
[]
[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 = ConstantIC
value = 1
variable = pwater
[../]
[./gas_ic]
type = ConstantIC
value = 2
variable = pgas
[../]
[]
[Kernels]
active = 'richardsfwater richardstwater richardsfgas richardstgas'
[./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
[../]
[./mass_error_gas]
type = FunctionValuePostprocessor
function = fcn_mass_error_g
[../]
[./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((-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 -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-10 1E-10 10000'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
end_time = 1E6
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = gh08
csv = true
[]
(modules/contact/test/tests/normal-nodal-lm-tan-tolerance/normal-nodal-lm-tan-tolerance.i)
[GlobalParams]
displacements = 'disp_x disp_y'
preset = false
[]
[Mesh]
[file]
type = FileMeshGenerator
file = 2blk-gap_no1000.e
[]
[]
[Modules/TensorMechanics/Master]
[./all]
displacements = 'disp_x disp_y'
strain = FINITE
add_variables = true
block = '1 2'
use_automatic_differentiation = true
scaling = 1e-4
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1e5
poissons_ratio = 0.345
block = '1 2'
[../]
[./_elastic_strain]
type = ADComputeFiniteStrainElasticStress
block = '1 2'
[../]
[]
[Contact]
[mortar]
mesh = file
secondary = 101
primary = 100
model = frictionless
formulation = mortar
c_normal = 1e4
tangential_tolerance = .05
normal_lm_scaling = 1e-3
[]
[]
[Functions]
[./disp_bc]
type = PiecewiseLinear
x = '0 10.0'
y = '0 -0.30'
[../]
[]
[BCs]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = 'left'
value = 0.0
[../]
[./left_y]
type = DirichletBC
variable = disp_y
boundary = 'left'
value = 0.0
[../]
[./right_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 'right'
function = disp_bc # '-30e-3 * t'
[../]
[./right_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 'right'
function = 0
[../]
[]
[Preconditioning]
[./fmp]
type = FDP
full = true
finite_difference_type = standard
[../]
[]
[Executioner]
solve_type = NEWTON
type = Transient
num_steps = 10
dt = 1
dtmin = 1
nl_rel_tol = 1e-12
nl_abs_tol = 1e-13
petsc_options = '-ksp_monitor_true_residual -snes_converged_reason -ksp_converged_reason'
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_shift_type -snes_max_it -ksp_max_it'
petsc_options_value = 'lu basic NONZERO 20 30'
[Predictor]
type = SimplePredictor
scale = 1
[]
[]
[Outputs]
checkpoint = true
exodus = true
print_linear_residuals = false
[dof]
type = DOFMap
execute_on = 'initial'
[]
[]
[Debug]
show_var_residual_norms = true
[]
(modules/tensor_mechanics/test/tests/ad_pressure/pressure_test.i)
#
# Pressure Test
#
# This test is designed to compute pressure loads on three faces of a unit cube.
#
# The mesh is composed of one block with a single element. Symmetry bcs are
# applied to the faces opposite the pressures. Poisson's ratio is zero,
# which makes it trivial to check displacements.
#
[Mesh]
type = FileMesh
file = pressure_test.e
displacements = 'disp_x disp_y disp_z'
[]
[Functions]
[./rampConstant]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 1.'
scale_factor = 1.0
[../]
[./zeroRamp]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 0. 1.'
scale_factor = 1.0
[../]
[./rampUnramp]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 0.'
scale_factor = 10.0
[../]
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./TensorMechanics]
displacements = 'disp_x disp_y disp_z'
use_automatic_differentiation = true
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 4
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = 5
value = 0.0
[../]
[./no_z]
type = DirichletBC
variable = disp_z
boundary = 6
value = 0.0
[../]
[./Pressure]
[./Side1]
boundary = 1
function = rampConstant
displacements = 'disp_x disp_y disp_z'
use_automatic_differentiation = true
[../]
[./Side2]
boundary = 2
function = zeroRamp
displacements = 'disp_x disp_y disp_z'
use_automatic_differentiation = true
factor = 2.0
[../]
[./Side3]
boundary = 3
function = rampUnramp
displacements = 'disp_x disp_y disp_z'
use_automatic_differentiation = true
[../]
[../]
[]
[Materials]
[./Elasticity_tensor]
type = ADComputeElasticityTensor
block = 1
fill_method = symmetric_isotropic
C_ijkl = '0 0.5e6'
[../]
[./strain]
type = ADComputeSmallStrain
displacements = 'disp_x disp_y disp_z'
block = 1
[../]
[./stress]
type = ADComputeLinearElasticStress
block = 1
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
nl_abs_tol = 1e-10
l_max_its = 20
start_time = 0.0
dt = 1.0
num_steps = 2
end_time = 2.0
[]
[Outputs]
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[]
(test/tests/geomsearch/2d_moving_penetration/pl_test1.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
file = pl_test1.e
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate10]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate13]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate14]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate15]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate16]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 0.7 -0.7 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-9
l_max_its = 10
start_time = 0.0
dt = 0.05
end_time = 1.0
[]
[Outputs]
file_base = pl_test1_out
exodus = true
[]
(test/tests/time_steppers/cutback_factor_at_failure/function_dt_cutback.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Functions]
[./dts]
type = PiecewiseLinear
x = '0 0.85 2'
y = '0.2 0.25 0.25'
[../]
[]
[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
[../]
[]
[Problem]
type = FailingProblem
fail_step = 3
[]
[Executioner]
type = Transient
num_steps = 10
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[./TimeStepper]
type = FunctionDT
function = dts
min_dt = 0.01
cutback_factor_at_failure = 0.75
[../]
[]
[Outputs]
exodus = true
[]
(modules/contact/examples/2d_indenter/indenter_rz_nodeface_friction.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Problem]
coord_type = RZ
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
[]
[Mesh]#Comment
file = indenter_rz_fine.e
displacements = 'disp_x disp_y'
# For NodalVariableValue to work with distributed mesh
allow_renumbering = false
[] # Mesh
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0. 1.0 1.8 2. 3.0'
y = '0. -4.5 -5.4 -5.4 -4.0'
[../]
[] # Functions
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[] # Variables
[AuxVariables]
[saved_x]
[]
[saved_y]
[]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = FINITE
block = '1 2'
use_automatic_differentiation = false
generate_output = 'stress_xx stress_xy stress_xz stress_yy stress_zz'
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[] # AuxKernels
[BCs]
# Symmetries of the Problem
[./symm_x_indenter]
type = DirichletBC
variable = disp_x
boundary = 5
value = 0.0
[../]
[./symm_x_material]
type = DirichletBC
variable = disp_x
boundary = 9
value = 0.0
[../]
# Material should not fly away
[./material_base_y]
type = DirichletBC
variable = disp_y
boundary = 8
value = 0.0
[../]
# Drive indenter motion
[./disp_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 1
function = disp_y
[../]
[] # BCs
[Contact]
[./dummy_name]
primary = 6
secondary = 4
model = coulomb
formulation = penalty
normalize_penalty = true
friction_coefficient = 0.5
penalty = 8e6
tangential_tolerance = 0.005
[../]
[]
[Dampers]
[./contact_slip]
type = ContactSlipDamper
secondary = 4
primary = 6
[../]
[]
[Materials]
[./tensor]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1.0e7
poissons_ratio = 0.25
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./tensor_2]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.0
[../]
[./power_law_hardening]
type = IsotropicPowerLawHardeningStressUpdate
strength_coefficient = 1e5 #K
strain_hardening_exponent = 0.5 #n
block = '2'
[../]
[./radial_return_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'power_law_hardening'
tangent_operator = elastic
block = '2'
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_shift_type -pc_factor_shift_amount'
petsc_options_value = 'lu basic NONZERO 1e-15'
line_search = 'none'
automatic_scaling = true
nl_abs_tol = 1.5e-07
nl_rel_tol = 1.5e-07
l_max_its = 40
start_time = 0.0
dt = 0.025
end_time = 3.0
[]
[Postprocessors]
[./maxdisp]
type = NodalVariableValue
nodeid = 39 # 40-1 where 40 is the exodus node number
variable = disp_y
[../]
[resid_y]
type = NodalSum
variable = saved_y
boundary = 1
[]
[]
[Outputs]
[./out]
type = Exodus
elemental_as_nodal = true
[../]
perf_graph = true
csv = true
[]
(modules/tensor_mechanics/test/tests/ad_smeared_cracking/cracking_exponential_deprecated.i)
#
# Test to exercise the exponential stress release
#
# Stress vs. strain should show a linear relationship until cracking,
# an exponential stress release, a linear relationship back to zero
# strain, a linear relationship with the original stiffness in
# compression and then back to zero strain, a linear relationship
# back to the exponential curve, and finally further exponential
# stress release.
#
[Mesh]
file = cracking_test.e
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Functions]
[./displx]
type = PiecewiseLinear
x = '0 1 2 3 4 5 6'
y = '0 0.00175 0 -0.0001 0 0.00175 0.0035'
[../]
[./disply]
type = PiecewiseLinear
x = '0 5 6'
y = '0 0 .00175'
[../]
[./displz]
type = PiecewiseLinear
x = '0 2 3'
y = '0 0 .0035'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx'
use_automatic_differentiation = true
[../]
[]
[BCs]
[./pullx]
type = ADFunctionDirichletBC
#type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = displx
[../]
[./left]
type = ADDirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./fix_y]
type = ADDirichletBC
variable = disp_y
boundary = '11 12'
value = 0.0
[../]
[./move_y]
type = ADFunctionDirichletBC
variable = disp_y
boundary = '15 16'
function = disply
[../]
[./back]
type = ADDirichletBC
variable = disp_z
boundary = '3'
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 186.5e9
poissons_ratio = .316
[../]
[./elastic_stress]
type = ADComputeSmearedCrackingStress
cracking_stress = 119.3e6
cracking_release = exponential
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
petsc_options_iname = '-ksp_gmres_restart -pc_type'
petsc_options_value = '101 lu'
line_search = 'none'
l_max_its = 100
l_tol = 1e-6
nl_max_its = 10
nl_rel_tol = 1e-12
nl_abs_tol = 1.e-4
start_time = 0.0
dt = 0.02
dtmin = 0.02
num_steps = 300
[]
[Outputs]
exodus = true
file_base = cracking_exponential_out
[]
(modules/combined/test/tests/power_law_creep/power_law_creep_smallstrain.i)
# 1x1x1 unit cube with uniform pressure on top face for the case of small strain.
# This test does not have a solid mechanics analog because there is not an equvialent
# small strain with rotations strain calculator material in solid mechanics
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
[]
[Variables]
[./temp]
order = FIRST
family = LAGRANGE
initial_condition = 1000.0
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
incremental = true
add_variables = true
generate_output = 'stress_yy creep_strain_xx creep_strain_yy creep_strain_zz elastic_strain_yy'
[../]
[]
[Functions]
[./top_pull]
type = PiecewiseLinear
x = '0 1'
y = '1 1'
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[./heat_ie]
type = HeatConductionTimeDerivative
variable = temp
[../]
[]
[BCs]
[./u_top_pull]
type = Pressure
variable = disp_y
component = 1
boundary = top
factor = -10.0e6
function = top_pull
[../]
[./u_bottom_fix]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./u_yz_fix]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./u_xy_fix]
type = DirichletBC
variable = disp_z
boundary = back
value = 0.0
[../]
[./temp_fix]
type = DirichletBC
variable = temp
boundary = 'bottom top'
value = 1000.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 2e11
poissons_ratio = 0.3
[../]
[./radial_return_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'power_law_creep'
tangent_operator = elastic
[../]
[./power_law_creep]
type = PowerLawCreepStressUpdate
coefficient = 1.0e-15
n_exponent = 4
activation_energy = 3.0e5
temperature = temp
[../]
[./thermal]
type = HeatConductionMaterial
specific_heat = 1.0
thermal_conductivity = 100.
[../]
[./density]
type = Density
density = 1.0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 20
nl_max_its = 20
nl_rel_tol = 1e-6
nl_abs_tol = 1e-6
l_tol = 1e-5
start_time = 0.0
end_time = 1.0
num_steps = 10
dt = 0.1
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/action/ad_converter_action_multi_eigenstrain.i)
# This tests the thermal expansion coefficient function using both
# options to specify that function: mean and instantaneous. There
# two blocks, each containing a single element, and these use the
# two variants of the function.
# In this test, the instantaneous CTE function has a constant value,
# while the mean CTE function is an analytic function designed to
# give the same response. If \bar{alpha}(T) is the mean CTE function,
# and \alpha(T) is the instantaneous CTE function,
# \bar{\alpha}(T) = 1/(T-Tref) \intA^{T}_{Tsf} \alpha(T) dT
# where Tref is the reference temperature used to define the mean CTE
# function, and Tsf is the stress-free temperature.
# This version of the test uses finite deformation theory.
# The two models produce very similar results. There are slight
# differences due to the large deformation treatment.
[Mesh]
file = 'blocks.e'
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[AuxVariables]
[./temp]
order = FIRST
family = LAGRANGE
[../]
[]
[Problem]
solve = false
[]
[Modules/TensorMechanics/Master]
[./block1]
block = 1
strain = FINITE
add_variables = true
automatic_eigenstrain_names = true
generate_output = 'strain_xx strain_yy strain_zz'
use_automatic_differentiation = true
[../]
[./block2]
block = 2
strain = FINITE
add_variables = true
automatic_eigenstrain_names = true
generate_output = 'strain_xx strain_yy strain_zz'
use_automatic_differentiation = true
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = disp_x
boundary = 3
value = 0.0
[../]
[./bottom]
type = DirichletBC
variable = disp_y
boundary = 2
value = 0.0
[../]
[./back]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0.0
[../]
[]
[AuxKernels]
[./temp]
type = FunctionAux
variable = temp
block = '1 2'
function = temp_func
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./small_stress]
type = ADComputeFiniteStrainElasticStress
[../]
[./thermal_expansion_strain1]
type = ComputeMeanThermalExpansionFunctionEigenstrain
block = 1
thermal_expansion_function = cte_func_mean
thermal_expansion_function_reference_temperature = 0.5
stress_free_temperature = 0.0
temperature = temp
eigenstrain_name = reg_eigenstrain1
[../]
[./converter1]
type = RankTwoTensorMaterialConverter
block = 1
reg_props_in = 'reg_eigenstrain1'
ad_props_out = 'eigenstrain1'
[../]
[./thermal_expansion_strain2]
type = ADComputeInstantaneousThermalExpansionFunctionEigenstrain
block = 2
thermal_expansion_function = cte_func_inst
stress_free_temperature = 0.0
temperature = temp
eigenstrain_name = eigenstrain2
[../]
[]
[Functions]
[./cte_func_mean]
type = ParsedFunction
vars = 'tsf tref scale' #stress free temp, reference temp, scale factor
vals = '0.0 0.5 1e-4'
value = 'scale * (t - tsf) / (t - tref)'
[../]
[./cte_func_inst]
type = PiecewiseLinear
xy_data = '0 1.0
2 1.0'
scale_factor = 1e-4
[../]
[./temp_func]
type = PiecewiseLinear
xy_data = '0 1
1 2'
[../]
[]
[Postprocessors]
[./disp_1]
type = NodalMaxValue
variable = disp_x
boundary = 101
[../]
[./disp_2]
type = NodalMaxValue
variable = disp_x
boundary = 102
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
l_max_its = 100
l_tol = 1e-4
nl_abs_tol = 1e-8
nl_rel_tol = 1e-12
start_time = 0.0
end_time = 1.0
dt = 0.1
[]
[Outputs]
csv = true
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_htonly/gap_heat_transfer_htonly_rz_test.i)
#
# 2-D RZ Gap Heat Transfer Test without mechanics
#
# This test exercises 1-D gap heat transfer for a constant conductivity gap.
#
# The mesh consists of two element blocks containing one element each. Each
# element is a unit cube. They sit next to one another with a unit between them.
#
# The conductivity of both blocks is set very large to achieve a uniform temperature
# across each block. The temperature of the far left boundary
# is ramped from 100 to 200 over one time unit, and then held fixed for an additional
# time unit. The temperature of the far right boundary is held fixed at 100.
#
# A simple analytical solution is possible for the heat flux between the blocks, or cylinders in the case of RZ.:
#
# Flux = (T_left - T_right) * (gapK/(r*ln(r2/r1)))
#
# For gapK = 1 (default value)
#
# The integrated heat flux across the gap at time 2 is then:
#
# 2*pi*h*k*delta_T/(ln(r2/r1))
# 2*pi*1*1*100/(ln(2/1)) = 906.5 watts
#
# For comparison, see results from the flux post processors.
#
# As a second test, use the rectilinear (parallel plate) form of the gap heat transfer.
#
# Flux = (T_left - T_right) * (gapK/gapL)
#
# For gapK = 1 (default value)
#
# The integrated heat flux across the gap at time 2 is then:
#
# 2*pi*h*k*delta_T/(1)
# 2*pi*1*1*100/(1) = 628.3 watts
#
# For comparison, see results from the flux post processors.
#
[Problem]
coord_type = RZ
rz_coord_axis = Y # this is modified through CLI args to test Z-R as opposed to R-Z
[]
[Mesh]
active = 'file'
[file]
type = FileMeshGenerator
file = gap_heat_transfer_htonly_rz_test.e
[]
[rotate]
type = TransformGenerator
transform = ROTATE
vector_value = '90 0 0'
input = file
[]
[]
[Functions]
[./ramp]
type = PiecewiseLinear
x = '0 1 2'
y = '100 200 200'
[../]
[]
[ThermalContact]
[./thermal_contact]
type = GapHeatTransfer
variable = temp
primary = 3
secondary = 2
emissivity_primary = 0
emissivity_secondary = 0
[../]
[./thermal_contact2]
type = GapHeatTransfer
variable = temp2
primary = 3
secondary = 2
emissivity_primary = 0
emissivity_secondary = 0
gap_geometry_type = PLATE
appended_property_name = 2
[../]
[]
[Variables]
[./temp]
order = FIRST
family = LAGRANGE
initial_condition = 100
[../]
[./temp2]
order = FIRST
family = LAGRANGE
initial_condition = 100
[../]
[]
[AuxVariables]
[./gap_cond]
order = CONSTANT
family = MONOMIAL
[../]
[./gap_cond2]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[./heat2]
type = HeatConduction
variable = temp2
[../]
[]
[BCs]
[./temp_far_left]
type = FunctionDirichletBC
boundary = 1
variable = temp
function = ramp
[../]
[./temp_far_right]
type = DirichletBC
boundary = 4
variable = temp
value = 100
[../]
[./temp_far_left2]
type = FunctionDirichletBC
boundary = 1
variable = temp2
function = ramp
[../]
[./temp_far_right2]
type = DirichletBC
boundary = 4
variable = temp2
value = 100
[../]
[]
[AuxKernels]
[./conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_cond
boundary = 2
[../]
[./conductance2]
type = MaterialRealAux
property = gap_conductance
variable = gap_cond2
boundary = 2
[../]
[]
[Materials]
[./heat1]
type = HeatConductionMaterial
block = '1 2'
specific_heat = 1.0
thermal_conductivity = 1e6
[../]
[./density]
type = GenericConstantMaterial
block = '1 2'
prop_names = 'density'
prop_values = '1.0'
[../]
[]
[Executioner]
type = Transient
# petsc_options = '-snes_mf_operator -ksp_monitor -snes_ksp_ew'
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
# petsc_options_iname = '-snes_type -snes_ls -snes_linesearch_type -ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
# petsc_options_value = 'ls basic basic 201 hypre boomeramg 4'
# petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
# petsc_options_value = '201 hypre boomeramg 4'
nl_abs_tol = 1e-3
nl_rel_tol = 1e-8
l_tol = 1e-6
l_max_its = 100
start_time = 0.0
dt = 1e-1
dtmin = 1e-1
end_time = 2.0
[]
[Postprocessors]
[./temp_left]
type = SideAverageValue
boundary = 2
variable = temp
execute_on = 'initial timestep_end'
[../]
[./temp_right]
type = SideAverageValue
boundary = 3
variable = temp
execute_on = 'initial timestep_end'
[../]
[./flux_left]
type = SideFluxIntegral
variable = temp
boundary = 2
diffusivity = thermal_conductivity
[../]
[./flux_right]
type = SideFluxIntegral
variable = temp
boundary = 3
diffusivity = thermal_conductivity
[../]
[./temp_left2]
type = SideAverageValue
boundary = 2
variable = temp2
execute_on = 'initial timestep_end'
[../]
[./temp_right2]
type = SideAverageValue
boundary = 3
variable = temp2
execute_on = 'initial timestep_end'
[../]
[./flux_left2]
type = SideFluxIntegral
variable = temp2
boundary = 2
diffusivity = thermal_conductivity
[../]
[./flux_right2]
type = SideFluxIntegral
variable = temp2
boundary = 3
diffusivity = thermal_conductivity
[../]
[]
[Outputs]
exodus = true
[]
(modules/xfem/test/tests/mechanical_constraint/glued_penalty.i)
[GlobalParams]
displacements = 'disp_x disp_y'
volumetric_locking_correction = false
[]
[XFEM]
geometric_cut_userobjects = 'line_seg_cut_uo'
qrule = volfrac
output_cut_plane = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 11
ny = 11
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '1.0 0.5 0.0 0.5'
time_start_cut = 0.0
time_end_cut = 0.0
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
planar_formulation = plane_strain
add_variables = true
[../]
[]
[Functions]
[./pull]
type = PiecewiseLinear
x='0 50 100'
y='0 0.02 0.1'
[../]
[]
[BCs]
[./bottomx]
type = DirichletBC
boundary = bottom
variable = disp_x
value = 0.0
[../]
[./bottomy]
type = DirichletBC
boundary = bottom
variable = disp_y
value = 0.0
[../]
[./topx]
type = DirichletBC
boundary = top
variable = disp_x
value = 0.0
[../]
[./topy]
type = FunctionDirichletBC
boundary = top
variable = disp_y
function = pull
[../]
[]
[Constraints]
[./disp_x]
type = XFEMSingleVariableConstraint
variable = disp_x
use_penalty = true
alpha = 1.0e8
use_displaced_mesh = true
geometric_cut_userobject = 'line_seg_cut_uo'
[../]
[./disp_y]
type = XFEMSingleVariableConstraint
variable = disp_y
use_penalty = true
alpha = 1.0e8
use_displaced_mesh = true
geometric_cut_userobject = 'line_seg_cut_uo'
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
block = 0
[../]
[./_elastic_strain]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-14
nl_abs_tol = 1e-9
# time control
start_time = 0.0
dt = 1.0
end_time = 2.0
num_steps = 5000
max_xfem_update = 1
[]
[Outputs]
exodus = true
execute_on = timestep_end
[./console]
type = Console
output_linear = true
[../]
[]
(modules/richards/test/tests/gravity_head_2/gh18.i)
# with immobile saturation
# unsaturated = true
# gravity = true
# supg = true
# transient = true
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
xmin = 0
xmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1E-2 1E-1 1E0 0.5E1 0.5E2 0.4E4 1E5 1E6 1E7'
x = '0 1E-1 1E0 1E1 1E2 1E3 1E4 1E5 1E6'
[../]
[]
[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 = 0.4
n = 2
[../]
[./RelPermGas]
type = RichardsRelPermPower
simm = 0.3
n = 2
[../]
[./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-5
[../]
[./SUPGgas]
type = RichardsSUPGstandard
p_SUPG = 1E-5
[../]
[]
[Variables]
[./pwater]
order = FIRST
family = LAGRANGE
[../]
[./pgas]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./water_ic]
type = ConstantIC
value = 1
variable = pwater
[../]
[./gas_ic]
type = ConstantIC
value = 2
variable = pgas
[../]
[]
[Kernels]
active = 'richardsfwater richardstwater richardsfgas richardstgas'
[./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
[../]
[./mass_error_gas]
type = FunctionValuePostprocessor
function = fcn_mass_error_g
[../]
[./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((-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 -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-10 1E-10 10'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
end_time = 1E6
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = gh18
execute_on = 'timestep_end final'
interval = 100000
exodus = true
[./console]
type = Console
interval = 1
[../]
[]
(test/tests/predictors/simple/predictor_test_skip_after_failed_tstep.i)
# The purpose of this test is to test the simple predictor.
# The test is adjusted to produce a failed time step.
# The predictor option 'skip_after_failed_timestep' should suppress a prediction
# after the failed time step.
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 3
ny = 3
[]
[Functions]
[./ramp1]
type = PiecewiseLinear
x = '0 0.5 1'
y = '0 1 4'
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./bot]
type = DirichletBC
variable = u
boundary = bottom
value = 0.0
[../]
[./ss2_x]
type = FunctionDirichletBC
variable = u
boundary = top
function = ramp1
[../]
[]
[Problem]
type = FailingProblem
fail_step = 6
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
nl_max_its = 15
nl_rel_tol = 1e-14
nl_abs_tol = 1e-14
l_tol = 1e-14
start_time = 0.0
end_time = 1.0
[./TimeStepper]
type = ConstantDT
dt = 0.1
cutback_factor_at_failure = 0.5
[../]
[./Predictor]
type = SimplePredictor
scale = 1.0
skip_after_failed_timestep = true
[../]
[]
[Postprocessors]
[./final_residual]
type = Residual
residual_type = final
[../]
[./initial_residual_before]
type = Residual
residual_type = initial_before_preset
[../]
[./initial_residual_after]
type = Residual
residual_type = initial_after_preset
[../]
[]
[Outputs]
csv = true
[]
(modules/richards/test/tests/gravity_head_1/gh23.i)
# investigating validity of immobile saturation
# 50 elements, with SUPG
[Mesh]
type = GeneratedMesh
dim = 1
nx = 50
xmin = -1
xmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1 10 100 1000 10000'
x = '0 10 100 1000 10000'
[../]
[]
[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 = 0.3
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 1.0E-6
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
initial_condition = -1.0
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[Kernels]
active = 'richardsf richardst'
[./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-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 = Transient
solve_type = Newton
dt = 1E0
end_time = 1E5
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = gh23
execute_on = 'timestep_end final'
interval = 10000
exodus = true
[./console]
interval = 1
type = Console
[../]
[]
(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
[]
(test/tests/geomsearch/3d_moving_penetration_smoothing/pl_test4nnstt.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
file = pl_test4tt.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./normal_z]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./closest_point_z]
[../]
# [./element_id]
# [../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[./diff_z]
type = Diffusion
variable = disp_z
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
tangential_tolerance = 0.09
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
tangential_tolerance = 0.09
normal_smoothing_method = nodal_normal_based
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = normal_z
boundary = 11
paired_boundary = 12
quantity = normal_z
[../]
[./penetrate10]
type = PenetrationAux
variable = normal_z
boundary = 12
paired_boundary = 11
quantity = normal_z
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate13]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate14]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate15]
type = PenetrationAux
variable = closest_point_z
boundary = 11
paired_boundary = 12
quantity = closest_point_z
[../]
[./penetrate16]
type = PenetrationAux
variable = closest_point_z
boundary = 12
paired_boundary = 11
quantity = closest_point_z
[../]
# [./penetrate17]
# type = PenetrationAux
# variable = element_id
# boundary = 11
# paired_boundary = 12
# quantity = element_id
# [../]
#
# [./penetrate18]
# type = PenetrationAux
# variable = element_id
# boundary = 12
# paired_boundary = 11
# quantity = element_id
# [../]
[./penetrate19]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate20]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b1z]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[./b2z]
type = DirichletBC
variable = disp_z
boundary = 2
value = 0
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-9
l_max_its = 10
start_time = 0.0
dt = 0.02
end_time = 1.0
[]
[Outputs]
file_base = pl_test4nnstt_out
exodus = true
[]
[NodalNormals]
boundary = 11
corner_boundary = 20
[]
(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
[]
(modules/tensor_mechanics/test/tests/strain_energy_density/nonAD_rate_model_weak_plane.i)
# Single element test to check the strain energy density calculation
[GlobalParams]
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
out_of_plane_strain = strain_zz
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
xmin = 0
xmax = 1
ymin = 0
ymax = 2
[]
[Variables]
[./strain_zz]
[]
[]
[AuxVariables]
[./SERD]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./rampConstantUp]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = -100
[../]
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress strain_xx strain_yy'
planar_formulation = WEAK_PLANE_STRESS
[../]
[]
[AuxKernels]
[./SERD]
type = MaterialRealAux
variable = SERD
property = strain_energy_rate_density
execute_on = timestep_end
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 'left'
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = 'bottom'
value = 0.0
[../]
[./Pressure]
[./top]
boundary = 'top'
function = rampConstantUp
[../]
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 206800
poissons_ratio = 0.0
[../]
[./radial_return_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'powerlawcrp'
[../]
[./powerlawcrp]
type = PowerLawCreepStressUpdate
coefficient = 3.125e-21 # 7.04e-17 #
n_exponent = 4.0
m_exponent = 0.0
activation_energy = 0.0
# max_inelastic_increment = 0.01
[../]
[./strain_energy_rate_density]
type = StrainEnergyRateDensity
inelastic_models = 'powerlawcrp'
[../]
[]
[Executioner]
type = Transient
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 4'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_abs_tol = 3e-7
nl_rel_tol = 1e-12
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Postprocessors]
[./SERD]
type = ElementAverageValue
variable = SERD
[../]
[]
[Outputs]
exodus = true
csv = true
[]
(test/tests/geomsearch/2d_moving_penetration/pl_test3.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
file = pl_test3.e
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate10]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate13]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate14]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate15]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate16]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1.e-10
l_max_its = 10
start_time = 0.0
dt = 0.0125
end_time = 1.0
[]
[Outputs]
file_base = pl_test3_out
exodus = true
[]
(modules/tensor_mechanics/test/tests/j_integral_vtest/j_int_surfbreak_ellip_crack_sym_mm.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[Mesh]
file = ellip_crack_4sym_norad_mm.e
partitioner = centroid
centroid_partitioner_direction = z
[]
[AuxVariables]
[./SED]
order = CONSTANT
family = MONOMIAL
[../]
[./resid_z]
[../]
[]
[Functions]
[./rampConstantUp]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1'
scale_factor = -68.95 #MPa
[../]
[]
[DomainIntegral]
integrals = JIntegral
boundary = 1001
crack_direction_method = CurvedCrackFront
crack_end_direction_method = CrackDirectionVector
crack_direction_vector_end_1 = '0.0 1.0 0.0'
crack_direction_vector_end_2 = '1.0 0.0 0.0'
radius_inner = '12.5 25.0 37.5'
radius_outer = '25.0 37.5 50.0'
intersecting_boundary = '1 2'
symmetry_plane = 2
incremental = true
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
[../]
[]
[AuxKernels]
[./SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[../]
[]
[BCs]
[./crack_y]
type = DirichletBC
variable = disp_z
boundary = 6
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = 12
value = 0.0
[../]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./Pressure]
[./Side1]
boundary = 5
function = rampConstantUp
[../]
[../]
[] # BCs
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 206800
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
# Two sets of linesearch options are for petsc 3.1 and 3.3 respectively
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
# petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 4'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_abs_tol = 1e-5
nl_rel_tol = 1e-11
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Postprocessors]
[./_dt]
type = TimestepSize
[../]
[./nl_its]
type = NumNonlinearIterations
[../]
[./lin_its]
type = NumLinearIterations
[../]
[./react_z]
type = NodalSum
variable = resid_z
boundary = 5
[../]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = j_int_surfbreak_ellip_crack_sym_mm_out
exodus = true
csv = true
[]
(test/tests/geomsearch/2d_moving_penetration/restart.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
file = pl_test1.e
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate10]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate13]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate14]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate15]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate16]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 0.7 -0.7 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-9
l_max_its = 10
start_time = 0.0
dt = 0.05
end_time = 0.5
[]
[Outputs]
exodus = true
checkpoint = true
[]
(modules/tensor_mechanics/test/tests/smeared_cracking/cracking_multiple_softening.i)
# Test of cracking with direction-specific release models in 3
# directions. Block is first pulled in one direction, and then
# held while it is sequentially pulled in the other two
# directions. Poisson's ratio is zero so that the cracking in one
# direction doesn't affect the others.
# Softening in the three directions should follow the laws for the
# prescribed models in the three directions, which are power law (x),
# exponential (y), and abrupt (z).
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Functions]
[./displx]
type = PiecewiseLinear
x = '0 1 2 3'
y = '0 1 1 1'
[../]
[./disply]
type = PiecewiseLinear
x = '0 1 2 3'
y = '0 0 1 1'
[../]
[./displz]
type = PiecewiseLinear
x = '0 1 2 3'
y = '0 0 0 1'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx'
[../]
[]
[BCs]
[./pullx]
type = FunctionDirichletBC
variable = disp_x
boundary = right
function = displx
[../]
[./pully]
type = FunctionDirichletBC
variable = disp_y
boundary = top
function = disply
[../]
[./pullz]
type = FunctionDirichletBC
variable = disp_z
boundary = front
function = displz
[../]
[./left]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./bottom]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./back]
type = DirichletBC
variable = disp_z
boundary = back
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 2.8e7
poissons_ratio = 0
[../]
[./elastic_stress]
type = ComputeSmearedCrackingStress
cracking_stress = 1.68e6
softening_models = 'power_law_softening exponential_softening abrupt_softening'
prescribed_crack_directions = 'x y z'
[../]
[./power_law_softening]
type = PowerLawSoftening
stiffness_reduction = 0.3333
[../]
[./exponential_softening]
type = ExponentialSoftening
[../]
[./abrupt_softening]
type = AbruptSoftening
[../]
[]
[Executioner]
type = Transient
petsc_options_iname = '-ksp_gmres_restart -pc_type -sub_pc_type'
petsc_options_value = '101 asm lu'
line_search = 'none'
l_max_its = 100
nl_max_its = 100
nl_rel_tol = 1e-8
nl_abs_tol = 1e-8
l_tol = 1e-5
start_time = 0.0
end_time = 3.0
dt = 0.01
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/plane_stress/ad_weak_plane_stress_incremental.i)
[GlobalParams]
displacements = 'disp_x disp_y'
temperature = temp
out_of_plane_strain = strain_zz
[]
[Mesh]
[./square]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 2
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./strain_zz]
[../]
[]
[AuxVariables]
[./temp]
[../]
[./nl_strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Postprocessors]
[./react_z]
type = ADMaterialTensorIntegral
rank_two_tensor = stress
index_i = 2
index_j = 2
[../]
[./min_strain_zz]
type = NodalExtremeValue
variable = strain_zz
value_type = min
[../]
[./max_strain_zz]
type = NodalExtremeValue
variable = strain_zz
value_type = max
[../]
[]
[Modules/TensorMechanics/Master]
[./plane_stress]
planar_formulation = WEAK_PLANE_STRESS
strain = SMALL
incremental = true
generate_output = 'stress_xx stress_xy stress_yy stress_zz strain_xx strain_xy strain_yy'
eigenstrain_names = eigenstrain
use_automatic_differentiation = true
[../]
[]
[AuxKernels]
[./tempfuncaux]
type = FunctionAux
variable = temp
function = tempfunc
use_displaced_mesh = false
[../]
[./strain_zz]
type = ADRankTwoAux
rank_two_tensor = total_strain
variable = nl_strain_zz
index_i = 2
index_j = 2
[../]
[]
[Functions]
[./pull]
type = PiecewiseLinear
x='0 1 100'
y='0 0.00 0.00'
[../]
[./tempfunc]
type = ParsedFunction
value = '(1 - x) * t'
[../]
[]
[BCs]
[./bottomx]
type = DirichletBC
boundary = 0
variable = disp_x
value = 0.0
[../]
[./bottomy]
type = DirichletBC
boundary = 0
variable = disp_y
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
poissons_ratio = 0.3
youngs_modulus = 1e6
[../]
[./thermal_strain]
type = ADComputeThermalExpansionEigenstrain
thermal_expansion_coeff = 0.02
stress_free_temperature = 0.5
eigenstrain_name = eigenstrain
[../]
[./stress]
type = ADComputeStrainIncrementBasedStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-14
nl_abs_tol = 1e-12
# time control
start_time = 0.0
dt = 1.0
dtmin = 1.0
end_time = 2.0
[]
[Outputs]
file_base = 'weak_plane_stress_incremental_out'
exodus = true
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_htonly/gap_heat_transfer_htonly_rspherical.i)
#
# 1-D spherical Gap Heat Transfer Test
#
# This test exercises 1-D gap heat transfer for a constant conductivity gap.
#
# The mesh consists of two "blocks" with a mesh biased toward the gap
# between them. Each block is unit length. The gap between them is one
# unit in length.
#
# The conductivity of both blocks is set very large to achieve a uniform temperature
# across each block. The temperature of the far left boundary
# is ramped from 100 to 200 over one time unit, and then held fixed for an additional
# time unit. The temperature of the far right boundary is held fixed at 100.
#
# A simple analytical solution is possible for the heat flux between the blocks, or spheres in the case of RSPHERICAL.:
#
# Flux = (T_left - T_right) * (gapK/(r^2*((1/r1)-(1/r2))))
#
# For gapK = 1 (default value)
#
# The area is taken as the area of the secondary (inner) surface:
#
# Area = 4 * pi * 1 * 1
#
# The integrated heat flux across the gap at time 2 is then:
#
# 4*pi*k*delta_T/((1/r1)-(1/r2))
# 4*pi*1*100/((1/1) - (1/2)) = 2513.3 watts
#
# For comparison, see results from the flux post processors.
#
#
[Problem]
coord_type = RSPHERICAL
[]
[Mesh]
file = gap_heat_transfer_htonly_rspherical.e
construct_side_list_from_node_list = true
[]
[Functions]
[./temp]
type = PiecewiseLinear
x = '0 1 2'
y = '100 200 200'
[../]
[]
[ThermalContact]
[./thermal_contact]
type = GapHeatTransfer
variable = temp
primary = 3
secondary = 2
emissivity_primary = 0
emissivity_secondary = 0
gap_geometry_type = sphere
[../]
[]
[Variables]
[./temp]
order = FIRST
family = LAGRANGE
initial_condition = 100
[../]
[]
[AuxVariables]
[./gap_cond]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[]
[BCs]
[./temp_far_left]
type = FunctionDirichletBC
boundary = 1
variable = temp
function = temp
[../]
[./temp_far_right]
type = DirichletBC
boundary = 4
variable = temp
value = 100
[../]
[]
[AuxKernels]
[./conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_cond
boundary = 2
[../]
[]
[Materials]
[./heat1]
type = HeatConductionMaterial
block = '1 2'
specific_heat = 1.0
thermal_conductivity = 1e6
[../]
[./density]
type = GenericConstantMaterial
block = '1 2'
prop_names = 'density'
prop_values = '1.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
# I don't know enough about this test to say why it needs such a
# loose nl_abs_tol... after timestep 10 the residual basically can't
# be reduced much beyond the initial residual. The test probably
# needs to be revisited to determine why.
nl_abs_tol = 1e-3
nl_rel_tol = 1e-10
l_tol = 1e-6
l_max_its = 100
line_search = 'none'
nl_max_its = 10
dt = 1e-1
dtmin = 1e-1
end_time = 2.0
[]
[Postprocessors]
[./temp_left]
type = SideAverageValue
boundary = 2
variable = temp
execute_on = 'initial timestep_end'
[../]
[./temp_right]
type = SideAverageValue
boundary = 3
variable = temp
execute_on = 'initial timestep_end'
[../]
[./flux_left]
type = SideFluxIntegral
variable = temp
boundary = 2
diffusivity = thermal_conductivity
[../]
[./flux_right]
type = SideFluxIntegral
variable = temp
boundary = 3
diffusivity = thermal_conductivity
[../]
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/central_difference/lumped/1D/1d_nodalmass_explicit.i)
# Test for central difference integration for 1D elements
[Mesh]
[./generated_mesh]
type = GeneratedMeshGenerator
xmin = 0
xmax = 10
nx = 5
dim = 1
[../]
[./all_nodes]
type = BoundingBoxNodeSetGenerator
new_boundary = 'all'
input = 'generated_mesh'
top_right = '10 0 0'
bottom_left = '0 0 0'
[../]
[]
[Variables]
[./disp_x]
[../]
[]
[AuxVariables]
[./accel_x]
[../]
[./vel_x]
[../]
[]
[AuxKernels]
[./accel_x]
type = TestNewmarkTI
variable = accel_x
displacement = disp_x
first = false
[../]
[./vel_x]
type = TestNewmarkTI
variable = vel_x
displacement = disp_x
[../]
[]
[Kernels]
[./DynamicTensorMechanics]
displacements = 'disp_x'
[../]
[]
[NodalKernels]
[./force_x]
type = UserForcingFunctionNodalKernel
variable = disp_x
boundary = right
function = force_x
[../]
[./nodal_masses]
type = NodalTranslationalInertia
nodal_mass_file = 'nodal_mass_file.csv'
variable = 'disp_x'
boundary = 'all'
[../]
[]
[Functions]
[./force_x]
type = PiecewiseLinear
x = '0.0 1.0 2.0 3.0 4.0' # time
y = '0.0 1.0 0.0 -1.0 0.0' # force
scale_factor = 1e3
[../]
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor_block]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.25
block = 0
[../]
[./strain_block]
type = ComputeIncrementalSmallStrain
block = 0
displacements = 'disp_x'
implicit = false
[../]
[./stress_block]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[]
[Executioner]
type = Transient
start_time = -0.01
end_time = 0.1
dt = 0.005
timestep_tolerance = 2e-10
[./TimeIntegrator]
type = CentralDifference
[../]
[]
[Postprocessors]
[./accel_x]
type = PointValue
point = '10.0 0.0 0.0'
variable = accel_x
[../]
[]
[Outputs]
exodus = false
csv = true
[]
(modules/combined/test/tests/inelastic_strain/elas_plas/elas_plas_nl1_cycle.i)
#
# Test for effective strain calculation.
# Boundary conditions from NAFEMS test NL1
#
#
# This is not a verification test. The boundary conditions are applied such
# that the first step generates only elastic stresses. The rest of the load
# steps generate cycles of tension and compression in the axial (i.e., y-axis)
# direction. The axial stresses and strains also cycle, however the effective
# plastic strain increases in value throughout the analysis.
#
[GlobalParams]
order = FIRST
family = LAGRANGE
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = one_elem2.e
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./vonmises]
order = CONSTANT
family = MONOMIAL
[../]
[./pressure]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./plastic_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./plastic_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./plastic_strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./tot_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./tot_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./tot_strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./eff_plastic_strain]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
[../]
[]
[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_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./vonmises]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = vonmises
scalar_type = VonMisesStress
execute_on = timestep_end
[../]
[./pressure]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = pressure
scalar_type = Hydrostatic
execute_on = timestep_end
[../]
[./elastic_strain_xx]
type = RankTwoAux
rank_two_tensor = elastic_strain
variable = elastic_strain_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./elastic_strain_yy]
type = RankTwoAux
rank_two_tensor = elastic_strain
variable = elastic_strain_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./elastic_strain_zz]
type = RankTwoAux
rank_two_tensor = elastic_strain
variable = elastic_strain_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./plastic_strain_xx]
type = RankTwoAux
rank_two_tensor = plastic_strain
variable = plastic_strain_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./plastic_strain_yy]
type = RankTwoAux
rank_two_tensor = plastic_strain
variable = plastic_strain_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./plastic_strain_zz]
type = RankTwoAux
rank_two_tensor = plastic_strain
variable = plastic_strain_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./tot_strain_xx]
type = RankTwoAux
rank_two_tensor = total_strain
variable = tot_strain_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./tot_strain_yy]
type = RankTwoAux
rank_two_tensor = total_strain
variable = tot_strain_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./tot_strain_zz]
type = RankTwoAux
rank_two_tensor = total_strain
variable = tot_strain_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./eff_plastic_strain]
type = MaterialRealAux
property = effective_plastic_strain
variable = eff_plastic_strain
[../]
[]
[Functions]
[./appl_dispy]
type = PiecewiseLinear
x = '0 1.0 2.0 3.0 4.0 5.0 6.0 7.0 8.0 9.0 10.0 11.0 12.0'
y = '0.0 0.208e-4 0.50e-4 1.00e-4 0.784e-4 0.50e-4 0.0 0.216e-4 0.5e-4 1.0e-4 0.785e-4 0.50e-4 0.0'
[../]
[]
[BCs]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 101
value = 0.0
[../]
[./origin_x]
type = DirichletBC
variable = disp_x
boundary = 103
value = 0.0
[../]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 102
value = 0.0
[../]
[./origin_y]
type = DirichletBC
variable = disp_y
boundary = 103
value = 0.0
[../]
[./top_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 1
function = appl_dispy
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = 1
youngs_modulus = 250e9
poissons_ratio = 0.25
[../]
[./strain]
type = ComputePlaneFiniteStrain
block = 1
[../]
[./stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'isoplas'
block = 1
[../]
[./isoplas]
type = IsotropicPlasticityStressUpdate
yield_stress = 5e6
hardening_constant = 0.0
relative_tolerance = 1e-20
absolute_tolerance = 1e-8
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
nl_rel_tol = 1e-10
nl_abs_tol = 1e-12
l_tol = 1e-4
l_max_its = 100
nl_max_its = 20
dt = 1.0
start_time = 0.0
num_steps = 100
end_time = 12.0
[]
[Postprocessors]
[./stress_xx]
type = ElementAverageValue
variable = stress_xx
[../]
[./stress_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./stress_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./stress_xy]
type = ElementAverageValue
variable = stress_xy
[../]
[./vonmises]
type = ElementAverageValue
variable = vonmises
[../]
[./pressure]
type = ElementAverageValue
variable = pressure
[../]
[./el_strain_xx]
type = ElementAverageValue
variable = elastic_strain_xx
[../]
[./el_strain_yy]
type = ElementAverageValue
variable = elastic_strain_yy
[../]
[./el_strain_zz]
type = ElementAverageValue
variable = elastic_strain_zz
[../]
[./pl_strain_xx]
type = ElementAverageValue
variable = plastic_strain_xx
[../]
[./pl_strain_yy]
type = ElementAverageValue
variable = plastic_strain_yy
[../]
[./pl_strain_zz]
type = ElementAverageValue
variable = plastic_strain_zz
[../]
[./eff_plastic_strain]
type = ElementAverageValue
variable = eff_plastic_strain
[../]
[./tot_strain_xx]
type = ElementAverageValue
variable = tot_strain_xx
[../]
[./tot_strain_yy]
type = ElementAverageValue
variable = tot_strain_yy
[../]
[./tot_strain_zz]
type = ElementAverageValue
variable = tot_strain_zz
[../]
[./disp_x1]
type = NodalVariableValue
nodeid = 0
variable = disp_x
[../]
[./disp_x4]
type = NodalVariableValue
nodeid = 3
variable = disp_x
[../]
[./disp_y1]
type = NodalVariableValue
nodeid = 0
variable = disp_y
[../]
[./disp_y4]
type = NodalVariableValue
nodeid = 3
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[]
[Outputs]
exodus = true
csv = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/combined/test/tests/ad_cavity_pressure/multiple_postprocessors.i)
#
# Cavity Pressure Test (Volume input as a vector of postprocessors)
#
# This test is designed to compute an internal pressure based on
# p = n * R * T / V
# where
# p is the pressure
# n is the amount of material in the volume (moles)
# R is the universal gas constant
# T is the temperature
# V is the volume
#
# The mesh is composed of one block (1) with an interior cavity of volume 8.
# Block 2 sits in the cavity and has a volume of 1. Thus, the total
# initial volume is 7.
# The test adjusts n, T, and V in the following way:
# n => n0 + alpha * t
# T => T0 + beta * t
# V => V0 + gamma * t
# with
# alpha = n0
# beta = T0 / 2
# gamma = - (0.003322259...) * V0
# T0 = 240.54443866068704
# V0 = 7
# n0 = f(p0)
# p0 = 100
# R = 8.314472 J * K^(-1) * mol^(-1)
#
# So, n0 = p0 * V0 / R / T0 = 100 * 7 / 8.314472 / 240.544439
# = 0.35
#
# In this test the internal volume is calculated as the sum of two Postprocessors
# internalVolumeInterior and internalVolumeExterior. This sum equals the value
# reported by the internalVolume postprocessor.
#
# The parameters combined at t = 1 gives p = 301.
#
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[Mesh]
file = 3d.e
[]
[Functions]
[./displ_positive]
type = PiecewiseLinear
x = '0 1'
y = '0 0.0029069767441859684'
[../]
[./displ_negative]
type = PiecewiseLinear
x = '0 1'
y = '0 -0.0029069767441859684'
[../]
[./temp1]
type = PiecewiseLinear
x = '0 1'
y = '1 1.5'
scale_factor = 240.54443866068704
[../]
[./material_input_function]
type = PiecewiseLinear
x = '0 1'
y = '0 0.35'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[./temp]
initial_condition = 240.54443866068704
[../]
[./material_input]
[../]
[]
[AuxVariables]
[./pressure_residual_x]
[../]
[./pressure_residual_y]
[../]
[./pressure_residual_z]
[../]
[./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_zx]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
use_automatic_differentiation = true
[../]
[./heat]
type = ADDiffusion
variable = temp
use_displaced_mesh = true
[../]
[./material_input_dummy]
type = ADDiffusion
variable = material_input
use_displaced_mesh = true
[../]
[]
[AuxKernels]
[./stress_xx]
type = ADRankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 0
variable = stress_xx
[../]
[./stress_yy]
type = ADRankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 1
variable = stress_yy
[../]
[./stress_zz]
type = ADRankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 2
variable = stress_zz
[../]
[./stress_xy]
type = ADRankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 1
variable = stress_xy
[../]
[./stress_yz]
type = ADRankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 2
variable = stress_yz
[../]
[./stress_zx]
type = ADRankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 0
variable = stress_zx
[../]
[]
[BCs]
[./no_x_exterior]
type = DirichletBC
variable = disp_x
boundary = '7 8'
value = 0.0
[../]
[./no_y_exterior]
type = DirichletBC
variable = disp_y
boundary = '9 10'
value = 0.0
[../]
[./no_z_exterior]
type = DirichletBC
variable = disp_z
boundary = '11 12'
value = 0.0
[../]
[./prescribed_left]
type = ADFunctionDirichletBC
variable = disp_x
boundary = 13
function = displ_positive
[../]
[./prescribed_right]
type = ADFunctionDirichletBC
variable = disp_x
boundary = 14
function = displ_negative
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = '15 16'
value = 0.0
[../]
[./no_z]
type = DirichletBC
variable = disp_z
boundary = '17 18'
value = 0.0
[../]
[./no_x_interior]
type = DirichletBC
variable = disp_x
boundary = '1 2'
value = 0.0
[../]
[./no_y_interior]
type = DirichletBC
variable = disp_y
boundary = '3 4'
value = 0.0
[../]
[./no_z_interior]
type = DirichletBC
variable = disp_z
boundary = '5 6'
value = 0.0
[../]
[./temperatureInterior]
type = ADFunctionDirichletBC
boundary = 100
function = temp1
variable = temp
[../]
[./MaterialInput]
type = ADFunctionDirichletBC
boundary = '100 13 14 15 16'
function = material_input_function
variable = material_input
[../]
[./CavityPressure]
[./1]
boundary = 100
initial_pressure = 100
material_input = materialInput
R = 8.314472
temperature = aveTempInterior
volume = 'internalVolumeInterior internalVolumeExterior'
startup_time = 0.5
output = ppress
save_in = 'pressure_residual_x pressure_residual_y pressure_residual_z'
use_automatic_differentiation = true
[../]
[../]
[]
[Materials]
[./elast_tensor1]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1e1
poissons_ratio = 0
block = 1
[../]
[./strain1]
type = ADComputeFiniteStrain
block = 1
[../]
[./stress1]
type = ADComputeFiniteStrainElasticStress
block = 1
[../]
[./elast_tensor2]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0
block = 2
[../]
[./strain2]
type = ADComputeFiniteStrain
block = 2
[../]
[./stress2]
type = ADComputeFiniteStrainElasticStress
block = 2
[../]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_type'
petsc_options_value = 'asm lu'
nl_rel_tol = 1e-12
l_tol = 1e-12
l_max_its = 20
dt = 0.5
end_time = 1.0
[]
[Postprocessors]
[./internalVolume]
type = InternalVolume
boundary = 100
execute_on = 'initial linear'
[../]
[./aveTempInterior]
type = SideAverageValue
boundary = 100
variable = temp
execute_on = 'initial linear'
[../]
[./internalVolumeInterior]
type = InternalVolume
boundary = '1 2 3 4 5 6'
execute_on = 'initial linear'
[../]
[./internalVolumeExterior]
type = InternalVolume
boundary = '13 14 15 16 17 18'
execute_on = 'initial linear'
[../]
[./materialInput]
type = SideAverageValue
boundary = '7 8 9 10 11 12'
variable = material_input
execute_on = linear
[../]
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/domain_integral_thermal/j_integral_2d_ctefunc.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[Mesh]
file = crack2d.e
[]
[AuxVariables]
[./SED]
order = CONSTANT
family = MONOMIAL
[../]
[./temp]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
[./tempfunc]
type = ParsedFunction
value = 10.0*(2*x/504)
[../]
[./cte_func]
type = PiecewiseLinear
x = '-10 -6 -2 0 2 6 10'
y = '1.484e-5 1.489e-5 1.494e-5 1.496e-5 1.498e-5 1.502e-5 1.505e-5'
[../]
[]
[DomainIntegral]
integrals = JIntegral
boundary = 800
crack_direction_method = CrackDirectionVector
crack_direction_vector = '1 0 0'
2d = true
axis_2d = 2
radius_inner = '60.0 80.0 100.0 120.0'
radius_outer = '80.0 100.0 120.0 140.0'
temperature = temp
incremental = true
eigenstrain_names = thermal_expansion
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
planar_formulation = PLANE_STRAIN
eigenstrain_names = thermal_expansion
[../]
[]
[AuxKernels]
[./SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[../]
[./tempfuncaux]
type = FunctionAux
variable = temp
function = tempfunc
block = 1
[../]
[]
[BCs]
[./crack_y]
type = DirichletBC
variable = disp_y
boundary = 100
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = 400
value = 0.0
[../]
[./no_x1]
type = DirichletBC
variable = disp_x
boundary = 900
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeFiniteStrainElasticStress
[../]
[./thermal_expansion_strain]
type = ComputeInstantaneousThermalExpansionFunctionEigenstrain
block = 1
thermal_expansion_function = cte_func
stress_free_temperature = 0.0
temperature = temp
eigenstrain_name = thermal_expansion
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_ksp_type -sub_pc_type -pc_asm_overlap'
petsc_options_value = 'asm 31 preonly lu 1'
line_search = 'none'
l_max_its = 50
nl_max_its = 40
nl_rel_step_tol= 1e-10
nl_rel_tol = 1e-10
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Outputs]
csv = true
[]
[Preconditioning]
[./smp]
type = SMP
pc_side = left
ksp_norm = preconditioned
full = true
[../]
[]
(test/tests/geomsearch/2d_moving_penetration/pl_test4qtt.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
file = pl_test4q.e
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
tangential_tolerance = 0.09
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
tangential_tolerance = 0.09
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate10]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate13]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate14]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate15]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate16]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-9
l_max_its = 10
start_time = 0.0
dt = 0.02
end_time = 1.0
[./Quadrature]
order = THIRD
[../]
[]
[Outputs]
file_base = pl_test4qtt_out
exodus = true
[]
(modules/tensor_mechanics/test/tests/1D_axisymmetric/axisymmetric_gps_small.i)
#
# This test checks the generalized plane strain using small strain formulation.
# The model consists of two sets of line elements. One undergoes a temperature rise of 100 with
# the other seeing a temperature rise of 300. Young's modulus is 3600, and
# Poisson's ratio is 0.2. The thermal expansion coefficient is 1e-8. All
# nodes are constrained against movement.
#
# For plane strain case, i.e., without constraining the strain_yy to be uniform,
# the stress solution would be [-6e-3, -6e-3, -6e-3] and [-18e-3, -18e-3, -18e-3] (xx, yy, zz).
# The generalized plane strain kernels work to balance the force in y direction.
#
# With out of plane strain of 3e-6, the stress solution becomes
# [-3e-3, 6e-3, -3e-3] and [-15e-3, -6e-3, -15e-3] (xx, yy, zz). This gives
# a domain integral of out-of-plane stress to be zero.
#
[GlobalParams]
displacements = disp_x
scalar_out_of_plane_strain = scalar_strain_yy
[]
[Problem]
coord_type = RZ
[]
[Mesh]
file = lines.e
[]
[Variables]
[./disp_x]
[../]
[./temp]
initial_condition = 580.0
[../]
[./scalar_strain_yy]
order = FIRST
family = SCALAR
[../]
[]
[Functions]
[./temp100]
type = PiecewiseLinear
x = '0 1'
y = '580 680'
[../]
[./temp300]
type = PiecewiseLinear
x = '0 1'
y = '580 880'
[../]
[]
[Kernels]
[./heat]
type = Diffusion
variable = temp
[../]
[]
[Modules]
[./TensorMechanics]
[./Master]
[./gps]
planar_formulation = GENERALIZED_PLANE_STRAIN
scalar_out_of_plane_strain = scalar_strain_yy
strain = SMALL
generate_output = 'strain_xx strain_yy strain_zz stress_xx stress_yy stress_zz'
eigenstrain_names = eigenstrain
[../]
[../]
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
boundary = 1000
value = 0
variable = disp_x
[../]
[./temp100]
type = FunctionDirichletBC
variable = temp
function = temp100
boundary = 2
[../]
[./temp300]
type = FunctionDirichletBC
variable = temp
function = temp300
boundary = 3
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 3600
poissons_ratio = 0.2
[../]
[./thermal_strain]
type = ComputeThermalExpansionEigenstrain
thermal_expansion_coeff = 1e-8
temperature = temp
stress_free_temperature = 580
eigenstrain_name = eigenstrain
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
line_search = 'none'
l_max_its = 50
l_tol = 1e-08
nl_max_its = 15
nl_abs_tol = 1e-10
start_time = 0
end_time = 1
num_steps = 1
[]
[Outputs]
exodus = true
console = true
[]
(modules/tensor_mechanics/test/tests/shell/dynamics/shell_dynamics_bending_moment.i)
# Test that models bending of a cantilever beam using shell elements
# A cantilever beam of length 10 m (in Y direction) and cross-section
# 1 m x 0.1 m is modeled using 4 shell elements placed along the length
# (Figure 6a from Dvorkin and Bathe, 1984). All displacements and
# X rotations are fixed on the bottom boundary. E = 2100000 and v = 0.0.
# A load of 0.5 N (in the Z direction) is applied at each node on the top
# boundary resulting in a total load of 1 N.
# The analytical solution for displacement at tip using small strain/rotations # is PL^3/3EI + PL/AG = 1.90485714 m
# The FEM solution using 4 shell elements is 1.875095 m with a relative error
# of 1.5%.
# Similarly, the analytical solution for slope at tip is PL^2/2EI = 0.285714286
# The FEM solution is 0.2857143 and the relative error is 5e-6%.
# The stress_yy for the four elements at z = -0.57735 * (t/2) (first qp below mid-surface of shell) are:
# 3031.089 Pa, 2165.064 Pa, 1299.038 Pa and 433.0127 Pa.
# Note the above values are the average stresses in each element.
# Analytically, stress_yy decreases linearly from y = 0 to y = 10 m.
# The maximum value of stress_yy at y = 0 is Mz/I = PL * 0.57735*(t/2)/I = 3464.1 Pa
# Therefore, the analytical value of stress at z = -0.57735 * (t/2) at the mid-point
# of the four elements are:
# 3031.0875 Pa, 2165.0625 Pa, 1299.0375 Pa ,433.0125 Pa
# The relative error in stress_yy is in the order of 5e-5%.
# The stress_yz at z = -0.57735 * (t/2) at all four elements from the simulation is 10 Pa.
# The analytical solution for the shear stress is: V/2/I *((t^2)/4 - z^2), where the shear force (V)
# is 1 N at any y along the length of the beam. Therefore, the analytical shear stress at
# z = -0.57735 * (t/2) is 10 Pa at any location along the length of the beam.
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 4
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 10.0
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[./rot_x]
order = FIRST
family = LAGRANGE
[../]
[./rot_y]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yz]
order = CONSTANT
family = MONOMIAL
[../]
# aux variables for dynamics
[./vel_x]
order = FIRST
family = LAGRANGE
[../]
[./vel_y]
order = FIRST
family = LAGRANGE
[../]
[./vel_z]
order = FIRST
family = LAGRANGE
[../]
[./accel_x]
order = FIRST
family = LAGRANGE
[../]
[./accel_y]
order = FIRST
family = LAGRANGE
[../]
[./accel_z]
order = FIRST
family = LAGRANGE
[../]
[./rot_vel_x]
order = FIRST
family = LAGRANGE
[../]
[./rot_vel_y]
order = FIRST
family = LAGRANGE
[../]
[./rot_accel_x]
order = FIRST
family = LAGRANGE
[../]
[./rot_accel_y]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./stress_yy]
type = RankTwoAux
variable = stress_yy
rank_two_tensor = global_stress_t_points_0
index_i = 1
index_j = 1
[../]
[./stress_yz]
type = RankTwoAux
variable = stress_yz
rank_two_tensor = global_stress_t_points_0
index_i = 1
index_j = 2
[../]
# Kernels for dynamics
[./accel_x]
type = NewmarkAccelAux
variable = accel_x
displacement = disp_x
velocity = vel_x
beta = 0.25
execute_on = timestep_end
[../]
[./vel_x]
type = NewmarkVelAux
variable = vel_x
acceleration = accel_x
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_y]
type = NewmarkAccelAux
variable = accel_y
displacement = disp_y
velocity = vel_y
beta = 0.25
execute_on = timestep_end
[../]
[./vel_y]
type = NewmarkVelAux
variable = vel_y
acceleration = accel_y
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_z]
type = NewmarkAccelAux
variable = accel_z
displacement = disp_z
velocity = vel_z
beta = 0.25
execute_on = timestep_end
[../]
[./vel_z]
type = NewmarkVelAux
variable = vel_z
acceleration = accel_z
gamma = 0.5
execute_on = timestep_end
[../]
[./rot_accel_x]
type = NewmarkAccelAux
variable = rot_accel_x
displacement = rot_x
velocity = rot_vel_x
beta = 0.25
execute_on = timestep_end
[../]
[./rot_vel_x]
type = NewmarkVelAux
variable = rot_vel_x
acceleration = rot_accel_x
gamma = 0.5
execute_on = timestep_end
[../]
[./rot_accel_y]
type = NewmarkAccelAux
variable = rot_accel_y
displacement = rot_y
velocity = rot_vel_y
beta = 0.25
execute_on = timestep_end
[../]
[./rot_vel_y]
type = NewmarkVelAux
variable = rot_vel_y
acceleration = rot_accel_y
gamma = 0.5
execute_on = timestep_end
[../]
[]
[BCs]
[./fixy1]
type = DirichletBC
variable = disp_y
boundary = 'bottom'
value = 0.0
[../]
[./fixz1]
type = DirichletBC
variable = disp_z
boundary = 'bottom'
value = 0.0
[../]
[./fixr1]
type = DirichletBC
variable = rot_x
boundary = 'bottom'
value = 0.0
[../]
[./fixr2]
type = DirichletBC
variable = rot_y
boundary = 'bottom'
value = 0.0
[../]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = 'bottom'
value = 0.0
[../]
[]
[Functions]
[./force_function]
type = PiecewiseLinear
x = '0.0 1.0'
y = '0.0 0.5'
[../]
[]
[NodalKernels]
[./force_y2]
type = UserForcingFunctionNodalKernel
variable = disp_z
boundary = 'top'
function = force_function
[../]
[]
[Kernels]
[./solid_disp_x]
type = ADStressDivergenceShell
block = '0'
component = 0
variable = disp_x
through_thickness_order = SECOND
[../]
[./solid_disp_y]
type = ADStressDivergenceShell
block = '0'
component = 1
variable = disp_y
through_thickness_order = SECOND
[../]
[./solid_disp_z]
type = ADStressDivergenceShell
block = '0'
component = 2
variable = disp_z
through_thickness_order = SECOND
[../]
[./solid_rot_x]
type = ADStressDivergenceShell
block = '0'
component = 3
variable = rot_x
through_thickness_order = SECOND
[../]
[./solid_rot_y]
type = ADStressDivergenceShell
block = '0'
component = 4
variable = rot_y
through_thickness_order = SECOND
[../]
[./inertial_force_x]
type = ADInertialForceShell
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y'
rotational_accelerations = 'rot_accel_x rot_accel_y'
component = 0
variable = disp_x
thickness = 0.1
[../]
[./inertial_force_y]
type = ADInertialForceShell
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y'
rotational_accelerations = 'rot_accel_x rot_accel_y'
component = 1
variable = disp_y
thickness = 0.1
[../]
[./inertial_force_z]
type = ADInertialForceShell
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y'
rotational_accelerations = 'rot_accel_x rot_accel_y'
component = 2
variable = disp_z
thickness = 0.1
[../]
[./inertial_force_rot_x]
type = ADInertialForceShell
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y'
rotational_accelerations = 'rot_accel_x rot_accel_y'
component = 3
variable = rot_x
thickness = 0.1
[../]
[./inertial_force_rot_y]
type = ADInertialForceShell
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y'
rotational_accelerations = 'rot_accel_x rot_accel_y'
component = 4
variable = rot_y
thickness = 0.1
[../]
[]
[Materials]
[./elasticity]
type = ADComputeIsotropicElasticityTensorShell
youngs_modulus = 2100000
poissons_ratio = 0.0
block = 0
through_thickness_order = SECOND
[../]
[./strain]
type = ADComputeIncrementalShellStrain
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y'
thickness = 0.1
through_thickness_order = SECOND
[../]
[./stress]
type = ADComputeShellStress
block = 0
through_thickness_order = SECOND
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = 'density'
prop_values = '1.0'
[../]
[]
[Postprocessors]
[./disp_z_tip]
type = PointValue
point = '1.0 10.0 0.0'
variable = disp_z
[../]
[./rot_x_tip]
type = PointValue
point = '0.0 10.0 0.0'
variable = rot_x
[../]
[./stress_yy_el_0]
type = ElementalVariableValue
elementid = 0
variable = stress_yy
[../]
[./stress_yy_el_1]
type = ElementalVariableValue
elementid = 1
variable = stress_yy
[../]
[./stress_yy_el_2]
type = ElementalVariableValue
elementid = 2
variable = stress_yy
[../]
[./stress_yy_el_3]
type = ElementalVariableValue
elementid = 3
variable = stress_yy
[../]
[./stress_yz_el_0]
type = ElementalVariableValue
elementid = 0
variable = stress_yz
[../]
[./stress_yz_el_1]
type = ElementalVariableValue
elementid = 1
variable = stress_yz
[../]
[./stress_yz_el_2]
type = ElementalVariableValue
elementid = 2
variable = stress_yz
[../]
[./stress_yz_el_3]
type = ElementalVariableValue
elementid = 3
variable = stress_yz
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
nl_max_its = 2
nl_rel_tol = 1e-10
nl_abs_tol = 5e-4
dt = 0.0005
dtmin = 0.0005
end_time = 1
# [./TimeIntegrator]
# type = NewmarkBeta
# beta = 0.25
# gamma = 0.5
# [../]
[]
[Outputs]
exodus = true
[]
(test/tests/geomsearch/3d_moving_penetration/pl_test4.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
file = pl_test4.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./normal_z]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./closest_point_z]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[./diff_z]
type = Diffusion
variable = disp_z
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = normal_z
boundary = 11
paired_boundary = 12
quantity = normal_z
[../]
[./penetrate10]
type = PenetrationAux
variable = normal_z
boundary = 12
paired_boundary = 11
quantity = normal_z
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate13]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate14]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate15]
type = PenetrationAux
variable = closest_point_z
boundary = 11
paired_boundary = 12
quantity = closest_point_z
[../]
[./penetrate16]
type = PenetrationAux
variable = closest_point_z
boundary = 12
paired_boundary = 11
quantity = closest_point_z
[../]
[./penetrate17]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate18]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate19]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate20]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b1z]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[./b2z]
type = DirichletBC
variable = disp_z
boundary = 2
value = 0
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-9
l_max_its = 10
start_time = 0.0
dt = 0.02
end_time = 1.0
[]
[Outputs]
file_base = pl_test4_out
exodus = true
[]
(framework/contrib/hit/test/input.i)
# This tests the thermal expansion coefficient function using both
# options to specify that function: mean and instantaneous. There
# two blocks, each containing a single element, and these use the
# two variants of the function.
# In this test, the instantaneous CTE function has a constant value,
# while the mean CTE function is an analytic function designed to
# give the same response. If \bar{alpha}(T) is the mean CTE function,
# and \alpha(T) is the instantaneous CTE function,
# \bar{\alpha}(T) = 1/(T-Tref) \intA^{T}_{Tsf} \alpha(T) dT
# where Tref is the reference temperature used to define the mean CTE
# function, and Tsf is the stress-free temperature.
# The two models produce very similar results. There are slight
# differences due to the large deformation treatment.
[Mesh]
file = 'blocks.e'
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./temp]
order = FIRST
family = LAGRANGE
[../]
[]
[SolidMechanics]
[./solid]
disp_x = disp_x
disp_y = disp_y
disp_z = disp_z
[../]
[]
[BCs]
[./left]
type = FunctionDirichletBC
variable = disp_x
boundary = 3
function = 0.02*t
[../]
[./bottom]
type = DirichletBC
variable = disp_y
boundary = 2
value = 0.0
[../]
[./back]
type = FunctionDirichletBC
variable = disp_z
boundary = 1
function = 0.01*t
[../]
[]
[AuxKernels]
[./temp]
type = FunctionAux
variable = temp
block = '1 2'
function = temp_func
[../]
[]
[Materials]
[./mean_alpha]
type = Elastic
block = 1
youngs_modulus = 1e6
poissons_ratio = .3
disp_x = disp_x
disp_y = disp_y
disp_z = disp_z
temp = temp
thermal_expansion_function = cte_func_mean
stress_free_temperature = 0.0
thermal_expansion_reference_temperature = 0.5
thermal_expansion_function_type = mean
[../]
[./inst_alpha]
type = Elastic
block = 2
youngs_modulus = 1e6
poissons_ratio = .3
disp_x = disp_x
disp_y = disp_y
disp_z = disp_z
temp = temp
thermal_expansion_function = cte_func_inst
stress_free_temperature = 0.0
thermal_expansion_function_type = instantaneous
[../]
[]
[Functions]
[./cte_func_mean]
type = ParsedFunction
vars = 'tsf tref scale' #stress free temp, reference temp, scale factor
vals = '0.0 0.5 1e-4'
value = 'scale * (t - tsf) / (t - tref)'
[../]
[./cte_func_inst]
type = PiecewiseLinear
xy_data = '0 1.0
2 1.0'
scale_factor = 1e-4
[../]
[./temp_func]
type = PiecewiseLinear
xy_data = '0 1
1 2'
[../]
[]
[Postprocessors]
[./disp_1]
type = NodalMaxValue
variable = disp_x
boundary = 101
[../]
[./disp_2]
type = NodalMaxValue
variable = disp_x
boundary = 102
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
l_max_its = 100
l_tol = 1e-4
nl_abs_tol = 1e-8
nl_rel_tol = 1e-12
start_time = 0.0
end_time = 1.0
dt = 0.1
[]
[Outputs]
file_base = const_alpha_out
exodus = true
csv = true
[]
(modules/combined/test/tests/power_law_creep/power_law_creep_restart2.i)
# 1x1x1 unit cube with uniform pressure on top face
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
[]
[Variables]
[./temp]
order = FIRST
family = LAGRANGE
initial_condition = 1000.0
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
incremental = true
add_variables = true
generate_output = 'stress_yy creep_strain_xx creep_strain_yy creep_strain_zz elastic_strain_yy'
[../]
[]
[Functions]
[./top_pull]
type = PiecewiseLinear
x = '0 1'
y = '1 1'
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[./heat_ie]
type = HeatConductionTimeDerivative
variable = temp
[../]
[]
[BCs]
[./u_top_pull]
type = Pressure
variable = disp_y
component = 1
boundary = top
factor = -10.0e6
function = top_pull
[../]
[./u_bottom_fix]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./u_yz_fix]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./u_xy_fix]
type = DirichletBC
variable = disp_z
boundary = back
value = 0.0
[../]
[./temp_fix]
type = DirichletBC
variable = temp
boundary = 'bottom top'
value = 1000.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 2e11
poissons_ratio = 0.3
[../]
[./radial_return_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'power_law_creep'
tangent_operator = elastic
[../]
[./power_law_creep]
type = PowerLawCreepStressUpdate
coefficient = 1.0e-15
n_exponent = 4
activation_energy = 3.0e5
temperature = temp
[../]
[./thermal]
type = HeatConductionMaterial
specific_heat = 1.0
thermal_conductivity = 100.
[../]
[./density]
type = Density
density = 1.0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 20
nl_max_its = 20
nl_rel_tol = 1e-6
nl_abs_tol = 1e-6
l_tol = 1e-5
start_time = 0.6
end_time = 1.0
num_steps = 12
dt = 0.1
[]
[Outputs]
file_base = power_law_creep_out
exodus = true
[]
[Problem]
restart_file_base = power_law_creep_restart1_out_cp/0006
[]
(modules/tensor_mechanics/test/tests/ad_smeared_cracking/cracking_rz.i)
#
[Mesh]
file = cracking_rz_test.e
[]
[Problem]
coord_type = RZ
[]
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Functions]
[./displ]
type = PiecewiseLinear
x = '0 1 2 3 4'
y = '0 1 0 -1 0'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx'
use_automatic_differentiation = true
[../]
[]
[BCs]
[./pull]
type = ADFunctionDirichletBC
variable = disp_x
boundary = 2
function = displ
[../]
[./left]
type = ADDirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./bottom]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 4.0e7
poissons_ratio = 0.0
[../]
[./elastic_stress]
type = ADComputeSmearedCrackingStress
cracking_stress = 1.68e6
softening_models = abrupt_softening
[../]
[./abrupt_softening]
type = ADAbruptSoftening
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101 '
line_search = 'none'
l_max_its = 100
nl_max_its = 100
nl_rel_tol = 1e-8
nl_abs_tol = 1e-2
l_tol = 1e-5
start_time = 0.0
end_time = 0.1
dt = 0.025
[]
[Outputs]
exodus = true
[]
(modules/combined/test/tests/ad_cavity_pressure/additional_volume.i)
#
# Cavity Pressure Test using using automatic differentiation
#
# This test is designed to compute an internal pressure based on
# p = n * R * / (V_cavity / T_cavity + V_add / T_add)
# where
# p is the pressure
# n is the amount of material in the volume (moles)
# R is the universal gas constant
# T_cavity is the temperature in the cavity
# T_add is the temperature of the additional volume
#
# The mesh is composed of one block (1) with an interior cavity of volume 8.
# Block 2 sits in the cavity and has a volume of 1. Thus, the total
# initial volume is 7. An additional volume of 2 is added.
#
# The test adjusts n, T, and V in the following way:
# n => n0 + alpha * t
# T => T0 + beta * t
# V => V_cavity0 + gamma * t + V_add
# with
# alpha = n0
# beta = T0 / 2
# gamma = -(0.003322259...) * V0
# T0 = 240.54443866068704
# V_cavity0 = 7
# V_add = 2
# T_add = 100
# n0 = f(p0)
# p0 = 100
# R = 8.314472 J * K^(-1) * mol^(-1)
#
# An additional volume of 2 with a temperature of 100.0 is included.
#
# So, n0 = p0 * (V_cavity / T_cavity + V_add / T_add) / R
# = 100 * (7 / 240.544439 + 2 / 100) / 8.314472
# = 0.59054
#
# The parameters combined at t = 1 gives p = 249.647.
#
# This test sets the initial temperature to 500, but the CavityPressure
# is told that that initial temperature is T0. Thus, the final solution
# is unchanged.
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
file = 3d.e
[]
[GlobalParams]
volumetric_locking_correction = true
[]
[Functions]
[./displ_positive]
type = PiecewiseLinear
x = '0 1'
y = '0 0.0029069767441859684'
[../]
[./displ_negative]
type = PiecewiseLinear
x = '0 1'
y = '0 -0.0029069767441859684'
[../]
[./temp1]
type = PiecewiseLinear
x = '0 1'
y = '1 1.5'
scale_factor = 240.54443866068704
[../]
[./material_input_function]
type = PiecewiseLinear
x = '0 1'
y = '0 0.59054'
[../]
[./additional_volume]
type = ConstantFunction
value = 2
[../]
[./temperature_of_additional_volume]
type = ConstantFunction
value = 100
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[./temp]
initial_condition = 500
[../]
[./material_input]
[../]
[]
[AuxVariables]
[./pressure_residual_x]
[../]
[./pressure_residual_y]
[../]
[./pressure_residual_z]
[../]
[./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_zx]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
use_automatic_differentiation = true
[../]
[./heat]
type = ADDiffusion
variable = temp
use_displaced_mesh = true
[../]
[./material_input_dummy]
type = ADDiffusion
variable = material_input
use_displaced_mesh = true
[../]
[]
[AuxKernels]
[./stress_xx]
type = ADRankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 0
variable = stress_xx
[../]
[./stress_yy]
type = ADRankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 1
variable = stress_yy
[../]
[./stress_zz]
type = ADRankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 2
variable = stress_zz
[../]
[./stress_xy]
type = ADRankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 1
variable = stress_xy
[../]
[./stress_yz]
type = ADRankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 2
variable = stress_yz
[../]
[./stress_zx]
type = ADRankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 0
variable = stress_zx
[../]
[]
[BCs]
[./no_x_exterior]
type = DirichletBC
variable = disp_x
boundary = '7 8'
value = 0.0
[../]
[./no_y_exterior]
type = DirichletBC
variable = disp_y
boundary = '9 10'
value = 0.0
[../]
[./no_z_exterior]
type = DirichletBC
variable = disp_z
boundary = '11 12'
value = 0.0
[../]
[./prescribed_left]
type = FunctionDirichletBC
variable = disp_x
boundary = 13
function = displ_positive
[../]
[./prescribed_right]
type = FunctionDirichletBC
variable = disp_x
boundary = 14
function = displ_negative
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = '15 16'
value = 0.0
[../]
[./no_z]
type = DirichletBC
variable = disp_z
boundary = '17 18'
value = 0.0
[../]
[./no_x_interior]
type = DirichletBC
variable = disp_x
boundary = '1 2'
value = 0.0
[../]
[./no_y_interior]
type = DirichletBC
variable = disp_y
boundary = '3 4'
value = 0.0
[../]
[./no_z_interior]
type = DirichletBC
variable = disp_z
boundary = '5 6'
value = 0.0
[../]
[./temperatureInterior]
type = ADFunctionDirichletBC
boundary = 100
function = temp1
variable = temp
[../]
[./MaterialInput]
type = ADFunctionDirichletBC
boundary = '100 13 14 15 16'
function = material_input_function
variable = material_input
[../]
[./CavityPressure]
[./1]
boundary = 100
initial_pressure = 100
material_input = materialInput
R = 8.314472
temperature = aveTempInterior
initial_temperature = 240.54443866068704
volume = internalVolume
startup_time = 0.5
output = ppress
save_in = 'pressure_residual_x pressure_residual_y pressure_residual_z'
additional_volumes = volume1
temperature_of_additional_volumes = temperature1
use_automatic_differentiation = true
[../]
[../]
[]
[Materials]
[./elast_tensor1]
type = ADComputeElasticityTensor
C_ijkl = '0 5'
fill_method = symmetric_isotropic
block = 1
[../]
[./strain1]
type = ADComputeFiniteStrain
block = 1
[../]
[./stress1]
type = ADComputeFiniteStrainElasticStress
block = 1
[../]
[./elast_tensor2]
type = ADComputeElasticityTensor
C_ijkl = '0 5'
fill_method = symmetric_isotropic
block = 2
[../]
[./strain2]
type = ADComputeFiniteStrain
block = 2
[../]
[./stress2]
type = ADComputeFiniteStrainElasticStress
block = 2
[../]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_type'
petsc_options_value = 'asm lu'
nl_rel_tol = 1e-12
l_tol = 1e-12
l_max_its = 20
dt = 0.5
end_time = 1.0
[]
[Postprocessors]
[./internalVolume]
type = InternalVolume
boundary = 100
execute_on = 'initial linear'
[../]
[./aveTempInterior]
type = SideAverageValue
boundary = 100
variable = temp
execute_on = 'initial linear'
[../]
[./materialInput]
type = SideAverageValue
boundary = '7 8 9 10 11 12'
variable = material_input
execute_on = linear
[../]
[./volume1]
type = FunctionValuePostprocessor
function = additional_volume
execute_on = 'initial linear'
[../]
[./temperature1]
type = FunctionValuePostprocessor
function = temperature_of_additional_volume
execute_on = 'initial linear'
[../]
[]
[Outputs]
exodus = true
[]
(test/tests/geomsearch/3d_moving_penetration/pl_test4qtt.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
file = pl_test4qtt.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./normal_z]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./closest_point_z]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[./diff_z]
type = Diffusion
variable = disp_z
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
tangential_tolerance = 0.1
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
tangential_tolerance = 0.1
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = normal_z
boundary = 11
paired_boundary = 12
quantity = normal_z
[../]
[./penetrate10]
type = PenetrationAux
variable = normal_z
boundary = 12
paired_boundary = 11
quantity = normal_z
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate13]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate14]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate15]
type = PenetrationAux
variable = closest_point_z
boundary = 11
paired_boundary = 12
quantity = closest_point_z
[../]
[./penetrate16]
type = PenetrationAux
variable = closest_point_z
boundary = 12
paired_boundary = 11
quantity = closest_point_z
[../]
[./penetrate17]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate18]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate19]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate20]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b1z]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[./b2z]
type = DirichletBC
variable = disp_z
boundary = 2
value = 0
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_abs_tol = 1e-7
l_max_its = 10
start_time = 0.0
dt = 0.0125
end_time = 1.0
[./Quadrature]
order = THIRD
[../]
[]
[Outputs]
file_base = pl_test4qtt_out
exodus = true
[]
(modules/tensor_mechanics/test/tests/t_stress/t_stress_ellip_crack_3d.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[Mesh]
file = ellip_crack_4sym_norad_mm.e
displacements = 'disp_x disp_y disp_z'
partitioner = centroid
centroid_partitioner_direction = z
[]
[AuxVariables]
[./SED]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./rampConstantUp]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = -689.5 #MPa
[../]
[]
[DomainIntegral]
integrals = 'JIntegral InteractionIntegralKI InteractionIntegralT'
boundary = 1001
crack_direction_method = CurvedCrackFront
crack_end_direction_method = CrackDirectionVector
crack_direction_vector_end_1 = '0.0 1.0 0.0'
crack_direction_vector_end_2 = '1.0 0.0 0.0'
radius_inner = '12.5 25.0 37.5'
radius_outer = '25.0 37.5 50.0'
intersecting_boundary = '1 2'
symmetry_plane = 2
youngs_modulus = 206.8e+3 #MPa
poissons_ratio = 0.3
block = 1
incremental = true
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress strain_xx strain_yy strain_zz'
[../]
[]
[AuxKernels]
[./SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[../]
[]
[BCs]
[./crack_y]
type = DirichletBC
variable = disp_z
boundary = 6
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = 12
value = 0.0
[../]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./Pressure]
[./Side1]
boundary = 5
function = rampConstantUp
[../]
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 206.8e+3
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
#petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 4'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_abs_tol = 1e-5
nl_rel_tol = 1e-11
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Outputs]
execute_on = 'timestep_end'
file_base = t_stress_ellip_crack_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/xfem/test/tests/second_order_elements/diffusion_3d_tet10.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 3
ny = 5
nz = 2
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
zmin = 0.0
zmax = 0.2
elem_type = TET10
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./square_planar_cut_uo]
type = RectangleCutUserObject
cut_data = ' 0.35 1.01 -0.001
0.35 0.49 -0.001
0.35 0.49 0.201
0.35 1.01 0.201'
[../]
[]
[Variables]
[./u]
[../]
[]
[Functions]
[./u_left]
type = PiecewiseLinear
x = '0 2'
y = '0 0.1'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = FunctionDirichletBC
variable = u
boundary = left
function = u_left
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 0
[../]
[]
[Executioner]
type = Transient
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
start_time = 0.0
dt = 1.0
end_time = 1.0
[]
[Outputs]
interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_htonly/planar_xy.i)
# 1-D Gap Heat Transfer Test without mechanics
#
# This test exercises 1-D gap heat transfer for a constant conductivity gap.
#
# The mesh consists of two element blocks in the x-y plane. Each element block
# is a square. They sit next to one another with a unit between them.
#
# The conductivity of both blocks is set very large to achieve a uniform temperature
# across each block. The temperature of the far bottom boundary
# is ramped from 100 to 200 over one time unit. The temperature of the far top
# boundary is held fixed at 100.
#
# A simple analytical solution is possible for the heat flux between the blocks:
#
# Flux = (T_left - T_right) * (gapK/gap_width)
#
# The gap conductivity is specified as 1, thus
#
# gapK(Tavg) = 1.0*Tavg
#
# The heat flux across the gap at time = 1 is then:
#
# Flux = 100 * (1.0/1.0) = 100
#
# For comparison, see results from the flux post processors. These results
# are the same as for the unit 1-D gap heat transfer between two unit cubes.
[Mesh]
file = simple_2D.e
[]
[Functions]
[./temp]
type = PiecewiseLinear
x = '0 1 2'
y = '100 200 200'
[../]
[]
[ThermalContact]
[./thermal_contact]
type = GapHeatTransfer
variable = temp
primary = 3
secondary = 2
emissivity_primary = 0
emissivity_secondary = 0
[../]
[]
[Variables]
[./temp]
order = FIRST
family = LAGRANGE
initial_condition = 100
[../]
[]
[AuxVariables]
[./gap_cond]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[]
[BCs]
[./temp_far_bottom]
type = FunctionDirichletBC
boundary = 1
variable = temp
function = temp
[../]
[./temp_far_top]
type = DirichletBC
boundary = 4
variable = temp
value = 100
[../]
[]
[AuxKernels]
[./conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_cond
boundary = 2
[../]
[]
[Materials]
[./heat1]
type = HeatConductionMaterial
block = '1 2'
specific_heat = 1.0
thermal_conductivity = 100000000.0
[../]
[./density]
type = GenericConstantMaterial
block = '1 2'
prop_names = 'density'
prop_values = '1.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 4'
line_search = 'none'
nl_rel_tol = 1e-14
l_tol = 1e-3
l_max_its = 100
dt = 1e-1
end_time = 1.0
[]
[Postprocessors]
[./temp_bottom]
type = SideAverageValue
boundary = 2
variable = temp
execute_on = 'initial timestep_end'
[../]
[./temp_top]
type = SideAverageValue
boundary = 3
variable = temp
execute_on = 'initial timestep_end'
[../]
[./flux_bottom]
type = SideFluxIntegral
variable = temp
boundary = 2
diffusivity = thermal_conductivity
execute_on = 'initial timestep_end'
[../]
[./flux_top]
type = SideFluxIntegral
variable = temp
boundary = 3
diffusivity = thermal_conductivity
execute_on = 'initial timestep_end'
[../]
[]
[Outputs]
exodus = true
[]
(test/tests/geomsearch/3d_moving_penetration/pl_test3tt.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
file = pl_test3tt.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./normal_z]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./closest_point_z]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[./diff_z]
type = Diffusion
variable = disp_z
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
tangential_tolerance = 0.09
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
tangential_tolerance = 0.09
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = normal_z
boundary = 11
paired_boundary = 12
quantity = normal_z
[../]
[./penetrate10]
type = PenetrationAux
variable = normal_z
boundary = 12
paired_boundary = 11
quantity = normal_z
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate13]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate14]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate15]
type = PenetrationAux
variable = closest_point_z
boundary = 11
paired_boundary = 12
quantity = closest_point_z
[../]
[./penetrate16]
type = PenetrationAux
variable = closest_point_z
boundary = 12
paired_boundary = 11
quantity = closest_point_z
[../]
[./penetrate17]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate18]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate19]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate20]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
preset = false
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
preset = false
boundary = 1
value = 0
[../]
[./b1z]
type = DirichletBC
variable = disp_z
preset = false
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
preset = false
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
preset = false
boundary = 2
function = disp_y
[../]
[./b2z]
type = DirichletBC
variable = disp_z
preset = false
boundary = 2
value = 0
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-9
l_max_its = 10
start_time = 0.0
dt = 0.02
end_time = 1.0
[]
[Outputs]
file_base = pl_test3tt_out
exodus = true
[]
(modules/tensor_mechanics/test/tests/1D_axisymmetric/axisymm_plane_strain_small.i)
#
# This test checks elastic stress calculations with mechanical and thermal
# strain using small strain formulation. Young's modulus is 3600, and Poisson's ratio is 0.2.
# The axisymmetric, plane strain 1D mesh is pulled with 1e-6 strain. Thus,
# the strain is [1e-6, 0, 1e-6] (xx, yy, zz). This gives stress of
# [5e-3, 2e-3, 5e-3]. After a temperature increase of 100 with alpha of
# 1e-8, the stress becomes [-1e-3, -4e-3, -1e-3].
#
[GlobalParams]
displacements = disp_x
[]
[Problem]
coord_type = RZ
[]
[Mesh]
file = line.e
[]
[Variables]
[./disp_x]
[../]
[]
[AuxVariables]
[./temp]
initial_condition = 580.0
[../]
[]
[Functions]
[./temp]
type = PiecewiseLinear
x = '0 1 2'
y = '580 580 680'
[../]
[./disp_x]
type = PiecewiseLinear
x = '0 1'
y = '0 2e-6'
[../]
[]
[Modules]
[./TensorMechanics]
[./Master]
[./ps]
planar_formulation = PLANE_STRAIN
strain = SMALL
generate_output = 'strain_xx strain_zz stress_xx stress_yy stress_zz'
eigenstrain_names = eigenstrain
[../]
[../]
[../]
[]
[AuxKernels]
[./temp]
type = FunctionAux
variable = temp
function = temp
execute_on = 'timestep_begin'
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
boundary = 1
value = 0
variable = disp_x
[../]
[./disp_x]
type = FunctionDirichletBC
boundary = 2
function = disp_x
variable = disp_x
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 3600
poissons_ratio = 0.2
[../]
[./thermal_strain]
type = ComputeThermalExpansionEigenstrain
thermal_expansion_coeff = 1e-8
temperature = temp
stress_free_temperature = 580
eigenstrain_name = eigenstrain
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
line_search = 'none'
l_max_its = 50
l_tol = 1e-6
nl_max_its = 15
nl_rel_tol = 1e-8
nl_abs_tol = 1e-10
start_time = 0
end_time = 2
num_steps = 2
[]
[Outputs]
exodus = true
console = true
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_htonly/cyl2D.i)
#
# 2D Cylindrical Gap Heat Transfer Test.
#
# This test exercises 2D gap heat transfer for a constant conductivity gap.
#
# The mesh consists of an inner solid cylinder of radius = 1 unit, and outer
# hollow cylinder with an inner radius of 2 in the x-y plane. In other words,
# the gap between them is 1 radial unit in length.
#
# The conductivity of both cylinders is set very large to achieve a uniform
# temperature in each cylinder. The temperature of the center node of the
# inner cylinder is ramped from 100 to 200 over one time unit. The temperature
# of the outside of the outer, hollow cylinder is held fixed at 100.
#
# A simple analytical solution is possible for the integrated heat flux
# between the inner and outer cylinders:
#
# Integrated Flux = (T_left - T_right) * (gapK/(r*ln(r2/r1))) * Area
#
# For gapK = 1 (default value)
#
# The area is taken as the area of the secondary (inner) surface:
#
# Area = 2 * pi * h * r, where h is the height of the cylinder.
#
# The integrated heat flux across the gap at time 1 is then:
#
# 2*pi*h*k*delta_T/(ln(r2/r1))
# 2*pi*1*1*100/(ln(2/1)) = 906.5 watts
#
# For comparison, see results from the integrated flux post processors.
# This simulation makes use of symmetry, so only 1/4 of the cylinders is meshed
# As such, the integrated flux from the post processors is 1/4 of the total,
# or 226.6 watts.
# The value coming from the post processor is slightly less than this
# but converges as mesh refinement increases.
# Note that the 2D and 3D results are the same.
#
# Simulating contact is challenging. Regression tests that exercise
# contact features can be difficult to solve consistently across multiple
# platforms. While designing these tests, we felt it worth while to note
# some aspects of these tests. The following applies to:
# sphere3D.i, sphere2DRZ.i, cyl2D.i, and cyl3D.i.
# 1. We decided that to perform consistently across multiple platforms we
# would use very small convergence tolerance. In this test we chose an
# nl_rel_tol of 1e-12.
# 2. Due to such a high value for thermal conductivity (used here so that the
# domains come to a uniform temperature) the integrated flux at time = 0
# was relatively large (the value coming from SideIntegralFlux =
# -_diffusion_coef[_qp]*_grad_u[_qp]*_normals[_qp] where the diffusion coefficient
# here is thermal conductivity).
# Even though _grad_u[_qp] is small, in this case the diffusion coefficient
# is large. The result is a number that isn't exactly zero and tends to
# fail exodiff. For this reason the parameter execute_on = initial should not
# be used. That parameter is left to default settings in these regression tests.
#
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
file = cyl2D.e
[]
[Functions]
[./temp]
type = PiecewiseLinear
x = '0 1'
y = '100 200'
[../]
[]
[Variables]
[./temp]
initial_condition = 100
[../]
[]
[AuxVariables]
[./gap_conductance]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./heat_conduction]
type = HeatConduction
variable = temp
[../]
[]
[AuxKernels]
[./gap_cond]
type = MaterialRealAux
property = gap_conductance
variable = gap_conductance
boundary = 2
[../]
[]
[Materials]
[./heat1]
type = HeatConductionMaterial
block = '1 2'
specific_heat = 1.0
thermal_conductivity = 1000000.0
[../]
[]
[ThermalContact]
[./thermal_contact]
type = GapHeatTransfer
variable = temp
primary = 3
secondary = 2
emissivity_primary = 0
emissivity_secondary = 0
gap_conductivity = 1
quadrature = true
gap_geometry_type = CYLINDER
cylinder_axis_point_1 = '0 0 0'
cylinder_axis_point_2 = '0 0 1'
[../]
[]
[BCs]
[./mid]
type = FunctionDirichletBC
boundary = 1
variable = temp
function = temp
[../]
[./temp_far_right]
type = DirichletBC
boundary = 4
variable = temp
value = 100
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
dt = 1
dtmin = 0.01
end_time = 1
nl_rel_tol = 1e-12
nl_abs_tol = 1e-7
[./Quadrature]
order = fifth
side_order = seventh
[../]
[]
[Outputs]
exodus = true
[./Console]
type = Console
[../]
[]
[Postprocessors]
[./temp_left]
type = SideAverageValue
boundary = 2
variable = temp
[../]
[./temp_right]
type = SideAverageValue
boundary = 3
variable = temp
[../]
[./flux_left]
type = SideFluxIntegral
variable = temp
boundary = 2
diffusivity = thermal_conductivity
[../]
[./flux_right]
type = SideFluxIntegral
variable = temp
boundary = 3
diffusivity = thermal_conductivity
[../]
[]
(modules/combined/test/tests/inelastic_strain/elas_plas/elas_plas_nl1.i)
#
# Test for effective strain calculation.
# Boundary conditions from NAFEMS test NL1
#
# This is not a verification test. The boundary conditions are applied such
# that the first step generates only elastic stresses. The second and third
# steps generate plastic deformation and the effective strain should be
# increasing throughout the run.
#
[GlobalParams]
order = FIRST
family = LAGRANGE
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = one_elem2.e
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./vonmises]
order = CONSTANT
family = MONOMIAL
[../]
[./pressure]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./plastic_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./plastic_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./plastic_strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./tot_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./tot_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./tot_strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./eff_plastic_strain]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
[../]
[]
[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_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./vonmises]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = vonmises
scalar_type = VonMisesStress
execute_on = timestep_end
[../]
[./pressure]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = pressure
scalar_type = Hydrostatic
execute_on = timestep_end
[../]
[./elastic_strain_xx]
type = RankTwoAux
rank_two_tensor = elastic_strain
variable = elastic_strain_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./elastic_strain_yy]
type = RankTwoAux
rank_two_tensor = elastic_strain
variable = elastic_strain_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./elastic_strain_zz]
type = RankTwoAux
rank_two_tensor = elastic_strain
variable = elastic_strain_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./plastic_strain_xx]
type = RankTwoAux
rank_two_tensor = plastic_strain
variable = plastic_strain_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./plastic_strain_yy]
type = RankTwoAux
rank_two_tensor = plastic_strain
variable = plastic_strain_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./plastic_strain_zz]
type = RankTwoAux
rank_two_tensor = plastic_strain
variable = plastic_strain_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./tot_strain_xx]
type = RankTwoAux
rank_two_tensor = total_strain
variable = tot_strain_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./tot_strain_yy]
type = RankTwoAux
rank_two_tensor = total_strain
variable = tot_strain_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./tot_strain_zz]
type = RankTwoAux
rank_two_tensor = total_strain
variable = tot_strain_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./eff_plastic_strain]
type = MaterialRealAux
property = effective_plastic_strain
variable = eff_plastic_strain
[../]
[]
[Functions]
[./appl_dispy]
type = PiecewiseLinear
x = '0 1.0 2.0 3.0'
y = '0.0 0.208e-4 0.50e-4 1.00e-4'
[../]
[]
[BCs]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 101
value = 0.0
[../]
[./origin_x]
type = DirichletBC
variable = disp_x
boundary = 103
value = 0.0
[../]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 102
value = 0.0
[../]
[./origin_y]
type = DirichletBC
variable = disp_y
boundary = 103
value = 0.0
[../]
[./top_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 1
function = appl_dispy
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = 1
youngs_modulus = 250e9
poissons_ratio = 0.25
[../]
[./strain]
type = ComputePlaneFiniteStrain
block = 1
[../]
[./stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'isoplas'
block = 1
[../]
[./isoplas]
type = IsotropicPlasticityStressUpdate
yield_stress = 5e6
hardening_constant = 0.0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
nl_rel_tol = 1e-10
nl_abs_tol = 1e-12
l_tol = 1e-4
l_max_its = 100
nl_max_its = 20
dt = 1.0
start_time = 0.0
num_steps = 100
end_time = 3.0
[] # Executioner
[Postprocessors]
[./stress_xx]
type = ElementAverageValue
variable = stress_xx
[../]
[./stress_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./stress_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./stress_xy]
type = ElementAverageValue
variable = stress_xy
[../]
[./vonmises]
type = ElementAverageValue
variable = vonmises
[../]
[./pressure]
type = ElementAverageValue
variable = pressure
[../]
[./el_strain_xx]
type = ElementAverageValue
variable = elastic_strain_xx
[../]
[./el_strain_yy]
type = ElementAverageValue
variable = elastic_strain_yy
[../]
[./el_strain_zz]
type = ElementAverageValue
variable = elastic_strain_zz
[../]
[./pl_strain_xx]
type = ElementAverageValue
variable = plastic_strain_xx
[../]
[./pl_strain_yy]
type = ElementAverageValue
variable = plastic_strain_yy
[../]
[./pl_strain_zz]
type = ElementAverageValue
variable = plastic_strain_zz
[../]
[./eff_plastic_strain]
type = ElementAverageValue
variable = eff_plastic_strain
[../]
[./tot_strain_xx]
type = ElementAverageValue
variable = tot_strain_xx
[../]
[./tot_strain_yy]
type = ElementAverageValue
variable = tot_strain_yy
[../]
[./tot_strain_zz]
type = ElementAverageValue
variable = tot_strain_zz
[../]
[./disp_x1]
type = NodalVariableValue
nodeid = 0
variable = disp_x
[../]
[./disp_x4]
type = NodalVariableValue
nodeid = 3
variable = disp_x
[../]
[./disp_y1]
type = NodalVariableValue
nodeid = 0
variable = disp_y
[../]
[./disp_y4]
type = NodalVariableValue
nodeid = 3
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[]
[Outputs]
exodus = true
csv = true
[./console]
type = Console
output_linear = true
[../]
[] # Outputs
(modules/tensor_mechanics/test/tests/beam/dynamic/dyn_euler_small_added_mass.i)
# Test for small strain euler beam vibration in y direction
# An impulse load is applied at the end of a cantilever beam of length 4m.
# The beam is massless with a lumped mass at the end of the beam
# The properties of the cantilever beam are as follows:
# Young's modulus (E) = 1e4
# Shear modulus (G) = 4e7
# Shear coefficient (k) = 1.0
# Cross-section area (A) = 0.01
# Iy = 1e-4 = Iz
# Length (L)= 4 m
# mass (m) = 0.01899772
# For this beam, the dimensionless parameter alpha = kAGL^2/EI = 6.4e6
# Therefore, the beam behaves like a Euler-Bernoulli beam.
# The theoretical first frequency of this beam is:
# f1 = 1/(2 pi) * sqrt(3EI/(mL^3)) = 0.25
# This implies that the corresponding time period of this beam is 4s.
# The FEM solution for this beam with 10 element gives time periods of 4s with time step of 0.01s.
# A higher time step of 0.1 s is used in the test to reduce computational time.
# The time history from this analysis matches with that obtained from Abaqus.
# Values from the first few time steps are as follows:
# time disp_y vel_y accel_y
# 0.0 0.0 0.0 0.0
# 0.1 0.0013076435060869 0.026152870121738 0.52305740243477
# 0.2 0.0051984378734383 0.051663017225289 -0.01285446036375
# 0.3 0.010269120909367 0.049750643493289 -0.02539301427625
# 0.4 0.015087433925158 0.046615616822532 -0.037307519138892
# 0.5 0.019534963888307 0.042334982440433 -0.048305168503101
[Mesh]
type = GeneratedMesh
xmin = 0.0
xmax = 4.0
nx = 10
dim = 1
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[./rot_x]
order = FIRST
family = LAGRANGE
[../]
[./rot_y]
order = FIRST
family = LAGRANGE
[../]
[./rot_z]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./vel_x]
order = FIRST
family = LAGRANGE
[../]
[./vel_y]
order = FIRST
family = LAGRANGE
[../]
[./vel_z]
order = FIRST
family = LAGRANGE
[../]
[./accel_x]
order = FIRST
family = LAGRANGE
[../]
[./accel_y]
order = FIRST
family = LAGRANGE
[../]
[./accel_z]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./accel_x]
type = NewmarkAccelAux
variable = accel_x
displacement = disp_x
velocity = vel_x
beta = 0.25
execute_on = timestep_end
[../]
[./vel_x]
type = NewmarkVelAux
variable = vel_x
acceleration = accel_x
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_y]
type = NewmarkAccelAux
variable = accel_y
displacement = disp_y
velocity = vel_y
beta = 0.25
execute_on = timestep_end
[../]
[./vel_y]
type = NewmarkVelAux
variable = vel_y
acceleration = accel_y
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_z]
type = NewmarkAccelAux
variable = accel_z
displacement = disp_z
velocity = vel_z
beta = 0.25
execute_on = timestep_end
[../]
[./vel_z]
type = NewmarkVelAux
variable = vel_z
acceleration = accel_z
gamma = 0.5
execute_on = timestep_end
[../]
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./fixy1]
type = DirichletBC
variable = disp_y
boundary = left
value = 0.0
[../]
[./fixz1]
type = DirichletBC
variable = disp_z
boundary = left
value = 0.0
[../]
[./fixr1]
type = DirichletBC
variable = rot_x
boundary = left
value = 0.0
[../]
[./fixr2]
type = DirichletBC
variable = rot_y
boundary = left
value = 0.0
[../]
[./fixr3]
type = DirichletBC
variable = rot_z
boundary = left
value = 0.0
[../]
[]
[NodalKernels]
[./force_y2]
type = UserForcingFunctionNodalKernel
variable = disp_y
boundary = right
function = force
[../]
[./x_inertial]
type = NodalTranslationalInertia
variable = disp_x
velocity = vel_x
acceleration = accel_x
boundary = right
beta = 0.25
gamma = 0.5
mass = 0.01899772
[../]
[./y_inertial]
type = NodalTranslationalInertia
variable = disp_y
velocity = vel_y
acceleration = accel_y
boundary = right
beta = 0.25
gamma = 0.5
mass = 0.01899772
[../]
[./z_inertial]
type = NodalTranslationalInertia
variable = disp_z
velocity = vel_z
acceleration = accel_z
boundary = right
beta = 0.25
gamma = 0.5
mass = 0.01899772
[../]
[]
[Functions]
[./force]
type = PiecewiseLinear
x = '0.0 0.1 0.2 10.0'
y = '0.0 1e-2 0.0 0.0'
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options_iname = '-ksp_type -pc_type'
petsc_options_value = 'preonly lu'
dt = 0.1
end_time = 5.0
timestep_tolerance = 1e-6
[]
[Kernels]
[./solid_disp_x]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 0
variable = disp_x
[../]
[./solid_disp_y]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 1
variable = disp_y
[../]
[./solid_disp_z]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 2
variable = disp_z
[../]
[./solid_rot_x]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 3
variable = rot_x
[../]
[./solid_rot_y]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 4
variable = rot_y
[../]
[./solid_rot_z]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 5
variable = rot_z
[../]
[]
[Materials]
[./elasticity]
type = ComputeElasticityBeam
youngs_modulus = 1.0e4
poissons_ratio = -0.999875
shear_coefficient = 1.0
block = 0
[../]
[./strain]
type = ComputeIncrementalBeamStrain
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
area = 0.01
Ay = 0.0
Az = 0.0
Iy = 1.0e-4
Iz = 1.0e-4
y_orientation = '0.0 1.0 0.0'
[../]
[./stress]
type = ComputeBeamResultants
block = 0
[../]
[]
[Postprocessors]
[./disp_x]
type = PointValue
point = '4.0 0.0 0.0'
variable = disp_x
[../]
[./disp_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = disp_y
[../]
[./vel_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = vel_y
[../]
[./accel_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = accel_y
[../]
[]
[Outputs]
exodus = true
csv = true
perf_graph = true
[]
(modules/richards/test/tests/gravity_head_2/gh_lumped_07.i)
# unsaturated = true
# gravity = false
# supg = true
# transient = true
# lumped = true
[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'
viscosity = '1E-3 0.5E-3'
gravity = '0 0 0'
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1E-2 1E-1 1E0 1E1 1E3 1E4 1E5 1E6 1E7'
x = '0 1E-1 1E0 1E1 1E2 1E3 1E4 1E5 1E6'
[../]
[]
[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 = 0.2
max = 0.8
variable = pwater
[../]
[./gas_ic]
type = RandomIC
min = 1.2
max = 1.8
variable = pgas
[../]
[]
[Kernels]
active = 'richardsfwater richardstwater richardsfgas richardstgas'
[./richardstwater]
type = RichardsLumpedMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFlux
variable = pwater
[../]
[./richardstgas]
type = RichardsLumpedMassChange
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
[../]
[./mass_error_gas]
type = FunctionValuePostprocessor
function = fcn_mass_error_g
[../]
[./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'
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-13 1E-10 10000'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
end_time = 1E6
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = gh_lumped_07
csv = true
[]
(modules/combined/test/tests/power_law_creep/power_law_creep.i)
# 1x1x1 unit cube with uniform pressure on top face
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
[]
[Variables]
[./temp]
order = FIRST
family = LAGRANGE
initial_condition = 1000.0
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
incremental = true
add_variables = true
generate_output = 'stress_yy creep_strain_xx creep_strain_yy creep_strain_zz elastic_strain_yy'
[../]
[]
[Functions]
[./top_pull]
type = PiecewiseLinear
x = '0 1'
y = '1 1'
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[./heat_ie]
type = HeatConductionTimeDerivative
variable = temp
[../]
[]
[BCs]
[./u_top_pull]
type = Pressure
variable = disp_y
component = 1
boundary = top
factor = -10.0e6
function = top_pull
[../]
[./u_bottom_fix]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./u_yz_fix]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./u_xy_fix]
type = DirichletBC
variable = disp_z
boundary = back
value = 0.0
[../]
[./temp_fix]
type = DirichletBC
variable = temp
boundary = 'bottom top'
value = 1000.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 2e11
poissons_ratio = 0.3
[../]
[./radial_return_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'power_law_creep'
tangent_operator = elastic
[../]
[./power_law_creep]
type = PowerLawCreepStressUpdate
coefficient = 1.0e-15
n_exponent = 4
activation_energy = 3.0e5
temperature = temp
[../]
[./thermal]
type = HeatConductionMaterial
specific_heat = 1.0
thermal_conductivity = 100.
[../]
[./density]
type = Density
density = 1.0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 20
nl_max_its = 20
nl_rel_tol = 1e-6
nl_abs_tol = 1e-6
l_tol = 1e-5
start_time = 0.0
end_time = 1.0
num_steps = 10
dt = 0.1
[]
[Outputs]
exodus = 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
[]
(modules/porous_flow/test/tests/dirackernels/bh05.i)
# unsaturated
# injection
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = -1
xmax = 1
ymin = -1
ymax = 1
zmin = -1
zmax = 1
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Functions]
[dts]
type = PiecewiseLinear
y = '500 500 1E1'
x = '4000 5000 6500'
[]
[]
[Variables]
[pp]
initial_condition = -2E5
[]
[]
[Kernels]
[mass0]
type = PorousFlowMassTimeDerivative
fluid_component = 0
variable = pp
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[borehole_total_outflow_mass]
type = PorousFlowSumQuantity
[]
[pc]
type = PorousFlowCapillaryPressureVG
m = 0.8
alpha = 1e-5
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 2e9
viscosity = 1e-3
density0 = 1000
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
[]
[porosity]
type = PorousFlowPorosityConst
porosity = 0.1
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1E-12 0 0 0 1E-12 0 0 0 1E-12'
[]
[relperm]
type = PorousFlowRelativePermeabilityFLAC
m = 2
phase = 0
[]
[]
[DiracKernels]
[bh]
type = PorousFlowPeacemanBorehole
variable = pp
SumQuantityUO = borehole_total_outflow_mass
point_file = bh03.bh
fluid_phase = 0
bottom_p_or_t = 0
unit_weight = '0 0 0'
use_mobility = true
character = -1
[]
[]
[Postprocessors]
[bh_report]
type = PorousFlowPlotQuantity
uo = borehole_total_outflow_mass
[]
[fluid_mass0]
type = PorousFlowFluidMass
execute_on = timestep_begin
[]
[fluid_mass1]
type = PorousFlowFluidMass
execute_on = timestep_end
[]
[zmass_error]
type = FunctionValuePostprocessor
function = mass_bal_fcn
execute_on = timestep_end
[]
[p0]
type = PointValue
variable = pp
point = '0 0 0'
execute_on = timestep_end
[]
[]
[Functions]
[mass_bal_fcn]
type = ParsedFunction
value = abs((a-c+d)/2/(a+c))
vars = 'a c d'
vals = 'fluid_mass1 fluid_mass0 bh_report'
[]
[]
[Preconditioning]
[usual]
type = SMP
full = true
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -ksp_max_it'
petsc_options_value = 'bcgs bjacobi 1E-10 1E-10 10000 30'
[]
[]
[Executioner]
type = Transient
end_time = 6500
solve_type = NEWTON
[TimeStepper]
type = FunctionDT
function = dts
[]
[]
[Outputs]
file_base = bh05
exodus = false
csv = true
execute_on = timestep_end
[]
(modules/richards/test/tests/dirac/bh_fu_04.i)
# unsaturated
# production
# fullyupwind
[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
sat_UO = Saturation
seff_UO = Seff1VG
SUPG_UO = SUPGstandard
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1E-2 1E-1 1 1E1 1E2 1E3'
x = '0 1E-1 1 1E1 1E2 1E3'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1000
bulk_mod = 2E9
[../]
[./Seff1VG]
type = RichardsSeff1VG
m = 0.8
al = 1E-5
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0
sum_s_res = 0
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 1E8
[../]
[./borehole_total_outflow_mass]
type = RichardsSumQuantity
[../]
[]
[Variables]
active = 'pressure'
[./pressure]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./p_ic]
type = FunctionIC
variable = pressure
function = initial_pressure
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[Kernels]
active = 'richardsf richardst'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[DiracKernels]
[./bh]
type = RichardsBorehole
bottom_pressure = -1E6
point_file = bh02.bh
SumQuantityUO = borehole_total_outflow_mass
variable = pressure
unit_weight = '0 0 0'
character = 1
fully_upwind = true
[../]
[]
[Postprocessors]
[./bh_report]
type = RichardsPlotQuantity
uo = borehole_total_outflow_mass
[../]
[./fluid_mass0]
type = RichardsMass
variable = pressure
execute_on = timestep_begin
[../]
[./fluid_mass1]
type = RichardsMass
variable = pressure
execute_on = timestep_end
[../]
[./zmass_error]
type = FunctionValuePostprocessor
function = mass_bal_fcn
execute_on = timestep_end
[../]
[./p0]
type = PointValue
variable = pressure
point = '1 1 1'
execute_on = timestep_end
[../]
[]
[Functions]
[./initial_pressure]
type = ParsedFunction
value = 0
[../]
[./mass_bal_fcn]
type = ParsedFunction
value = abs((a-c+d)/2/(a+c))
vars = 'a c d'
vals = 'fluid_mass1 fluid_mass0 bh_report'
[../]
[]
[Materials]
[./all]
type = RichardsMaterial
block = 0
viscosity = 1E-3
mat_porosity = 0.1
mat_permeability = '1E-12 0 0 0 1E-12 0 0 0 1E-12'
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = Seff1VG
pressure_vars = pressure
[../]
[]
[Preconditioning]
[./usual]
type = SMP
full = true
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -ksp_max_it'
petsc_options_value = 'bcgs bjacobi 1E-10 1E-10 10000 30'
[../]
[]
[Executioner]
type = Transient
end_time = 1E3
solve_type = NEWTON
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = bh_fu_04
exodus = false
execute_on = timestep_end
csv = true
[]
(test/tests/geomsearch/3d_moving_penetration/pl_test1qtt.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
file = pl_test1qtt.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./normal_z]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./closest_point_z]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[./diff_z]
type = Diffusion
variable = disp_z
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
tangential_tolerance = 0.1
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
tangential_tolerance = 0.1
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = normal_z
boundary = 11
paired_boundary = 12
quantity = normal_z
[../]
[./penetrate10]
type = PenetrationAux
variable = normal_z
boundary = 12
paired_boundary = 11
quantity = normal_z
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate13]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate14]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate15]
type = PenetrationAux
variable = closest_point_z
boundary = 11
paired_boundary = 12
quantity = closest_point_z
[../]
[./penetrate16]
type = PenetrationAux
variable = closest_point_z
boundary = 12
paired_boundary = 11
quantity = closest_point_z
[../]
[./penetrate17]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate18]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate19]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate20]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b1z]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[./b2z]
type = DirichletBC
variable = disp_z
boundary = 2
value = 0
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 0.7 -0.7 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-9
l_max_its = 10
start_time = 0.0
dt = 0.06
end_time = 1.0
[./Quadrature]
order = THIRD
[../]
[]
[Outputs]
file_base = pl_test1qtt_out
exodus = true
[]
(modules/tensor_mechanics/test/tests/interaction_integral/interaction_integral_2d.i)
#This tests the Interaction Integral evaluation capability.
#This is a 2d nonlinear plane strain model
[GlobalParams]
order = FIRST
# order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[Mesh]
file = crack2d.e
displacements = 'disp_x disp_y'
[]
[Functions]
[./rampConstant]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = -1e2
[../]
[]
[DomainIntegral]
integrals = 'InteractionIntegralKI InteractionIntegralKII InteractionIntegralKIII'
boundary = 800
crack_direction_method = CrackDirectionVector
crack_direction_vector = '1 0 0'
2d = true
axis_2d = 2
radius_inner = '4.0 4.5 5.0 5.5 6.0'
radius_outer = '4.5 5.0 5.5 6.0 6.5'
block = 1
youngs_modulus = 207000
poissons_ratio = 0.3
output_q = false
incremental = true
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
planar_formulation = PLANE_STRAIN
[../]
[]
[BCs]
[./crack_y]
type = DirichletBC
variable = disp_y
boundary = 100
value = 0.0
[../]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 700
value = 0.0
[../]
[./Pressure]
[./Side1]
boundary = 400
function = rampConstant
[../]
[../]
[] # BCs
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_abs_tol = 1e-5
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Outputs]
file_base = interaction_integral_2d_out
exodus = true
csv = true
[]
(modules/tensor_mechanics/test/tests/1D_axisymmetric/axisymm_gps_finite.i)
# this test checks the asixymmetric 1D generalized plane strain formulation using finite strains
[GlobalParams]
displacements = disp_x
scalar_out_of_plane_strain = scalar_strain_yy
[]
[Problem]
coord_type = RZ
[]
[Mesh]
file = line.e
[]
[Variables]
[./disp_x]
[../]
[./scalar_strain_yy]
order = FIRST
family = SCALAR
[../]
[]
[AuxVariables]
[./strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./temp]
initial_condition = 580.0
[../]
[]
[Functions]
[./temp]
type = PiecewiseLinear
x = '0 1 2'
y = '580 580 680'
[../]
[./disp_x]
type = PiecewiseLinear
x = '0 1'
y = '0 2e-3'
[../]
[]
[Kernels]
[./TensorMechanics]
[../]
[]
[Modules]
[./TensorMechanics]
[./GeneralizedPlaneStrain]
[./gps]
[../]
[../]
[../]
[]
[AuxKernels]
[./strain_xx]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_xx
index_i = 0
index_j = 0
[../]
[./strain_yy]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_yy
index_i = 1
index_j = 1
[../]
[./strain_zz]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_zz
index_i = 2
index_j = 2
[../]
[./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_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./temp]
type = FunctionAux
variable = temp
function = temp
execute_on = 'timestep_begin'
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
boundary = 1
value = 0
variable = disp_x
[../]
[./disp_x]
type = FunctionDirichletBC
boundary = 2
function = disp_x
variable = disp_x
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 3600
poissons_ratio = 0.2
[../]
[./strain]
type = ComputeAxisymmetric1DFiniteStrain
eigenstrain_names = eigenstrain
scalar_out_of_plane_strain = scalar_strain_yy
[../]
[./thermal_strain]
type = ComputeThermalExpansionEigenstrain
thermal_expansion_coeff = 1e-6
temperature = temp
stress_free_temperature = 580
eigenstrain_name = eigenstrain
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
line_search = 'none'
l_max_its = 50
l_tol = 1e-6
nl_max_its = 15
nl_rel_tol = 1e-8
nl_abs_tol = 1e-10
start_time = 0
end_time = 2
num_steps = 2
[]
[Outputs]
exodus = true
console = true
[]
(modules/tensor_mechanics/test/tests/ad_anisotropic_elastoplasticity/ad_aniso_plasticity_x_one_ref.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
nx = 10
ny = 2
nz = 2
xmin = 0.0
ymin = 0.0
zmin = 0.0
xmax = 10.0
ymax = 1.0
zmax = 1.0
[]
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[AuxVariables]
[hydrostatic_stress]
order = CONSTANT
family = MONOMIAL
[]
[plastic_strain_xx]
order = CONSTANT
family = MONOMIAL
[]
[plastic_strain_xy]
order = CONSTANT
family = MONOMIAL
[]
[plastic_strain_yy]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[hydrostatic_stress]
type = ADRankTwoScalarAux
variable = hydrostatic_stress
rank_two_tensor = stress
scalar_type = Hydrostatic
[]
[plasticity_strain_xx]
type = ADRankTwoAux
rank_two_tensor = plastic_strain
variable = plastic_strain_xx
index_i = 0
index_j = 0
[]
[plasticity_strain_xy]
type = ADRankTwoAux
rank_two_tensor = plastic_strain
variable = plastic_strain_xy
index_i = 0
index_j = 1
[]
[plasticity_strain_yy]
type = ADRankTwoAux
rank_two_tensor = plastic_strain
variable = plastic_strain_yy
index_i = 1
index_j = 1
[]
[sigma_xx]
type = ADRankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 1
index_j = 1
[]
[]
[Functions]
[pull]
type = PiecewiseLinear
x = '0 1e1 1e8'
y = '0 -4e2 -4e2'
[]
[]
[Modules/TensorMechanics/Master]
[all]
strain = FINITE
generate_output = 'elastic_strain_xx stress_xx'
use_automatic_differentiation = true
add_variables = true
[]
[]
[Materials]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 70000
poissons_ratio = 0.25
[]
[elastic_strain]
type = ADComputeMultipleInelasticStress
inelastic_models = "trial_plasticity"
max_iterations = 50
absolute_tolerance = 1e-16
[]
[trial_plasticity]
type = ADHillPlasticityStressUpdate
hardening_constant = 2000.0
yield_stress = 0.001 # was 200 for verification
# F G H L M N
hill_constants = "0.5829856 0.364424 0.6342174 2.0691375 2.3492325 1.814589"
absolute_tolerance = 1e-15
relative_tolerance = 1e-13
# internal_solve_full_iteration_history = true
max_inelastic_increment = 2.0e-6
# internal_solve_output_on = on_error
[]
[]
[BCs]
[no_disp_x]
type = ADDirichletBC
variable = disp_x
boundary = left
value = 0.0
[]
[no_disp_y]
type = ADDirichletBC
variable = disp_y
boundary = left
value = 0.0
[]
[no_disp_z]
type = ADDirichletBC
variable = disp_z
boundary = left
value = 0.0
[]
[Pressure]
[Side1]
boundary = right
function = pull
[]
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
nl_rel_tol = 1e-12
nl_abs_tol = 1.0e-14
l_max_its = 90
num_steps = 25
[TimeStepper]
type = IterationAdaptiveDT
optimal_iterations = 30
iteration_window = 9
growth_factor = 1.05
cutback_factor = 0.5
timestep_limiting_postprocessor = matl_ts_min
dt = 1.0e-5
time_t = '0 3.4e-5 10'
time_dt = '1.0e-5 1.0e-7 1.0e-7'
[]
start_time = 0
automatic_scaling = true
[]
[Postprocessors]
[matl_ts_min]
type = MaterialTimeStepPostprocessor
[]
[max_disp_x]
type = ElementExtremeValue
variable = disp_x
[]
[max_hydro]
type = ElementAverageValue
variable = hydrostatic_stress
[]
[dt]
type = TimestepSize
[]
[plasticity_strain_xx]
type = ElementalVariableValue
variable = plastic_strain_xx
execute_on = 'TIMESTEP_END'
elementid = 0
[]
[elastic_strain_xx]
type = ElementalVariableValue
variable = elastic_strain_xx
execute_on = 'TIMESTEP_END'
elementid = 0
[]
[sigma_xx]
type = ElementalVariableValue
variable = stress_xx
execute_on = 'TIMESTEP_END'
elementid = 0
[]
[]
[Outputs]
csv = true
exodus = true
perf_graph = true
[]
(test/tests/multiapps/sub_cycling_failure/master_gold.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Functions]
# These mimic the behavior of the failing solve
[./dts]
type = PiecewiseLinear
x = '0 0.1 0.15'
y = '0.1 0.05 0.1'
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./td]
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 = Transient
num_steps = 4
dt = 0.1
[./TimeStepper]
type = FunctionDT
function = dts
[../]
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
[MultiApps]
[./sub]
type = TransientMultiApp
app_type = MooseTestApp
execute_on = timestep_end
positions = '0 0 0'
input_files = sub_gold.i
sub_cycling = true
[../]
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_htonly/sphere2DRZ.i)
#
# 2DRZ Spherical Gap Heat Transfer Test.
#
# This test exercises 2D gap heat transfer for a constant conductivity gap.
#
# The mesh consists of an inner solid sphere of radius = 1 unit, and outer
# hollow sphere with an inner radius of 2. In other words, the gap between
# them is 1 radial unit in length.
#
# The conductivity of both spheres is set very large to achieve a uniform
# temperature in each sphere. The temperature of the center node of the
# inner sphere is ramped from 100 to 200 over one time unit. The
# temperature of the outside of the outer, hollow sphere is held fixed
# at 100.
#
# A simple analytical solution is possible for the integrated heat flux
# between the inner and outer spheres:
#
# Integrated Flux = (T_left - T_right) * (gapK/(r^2*((1/r1)-(1/r2)))) * Area
#
# For gapK = 1 (default value)
#
# The area is taken as the area of the secondary (inner) surface:
#
# Area = 4 * pi * 1^2 (4*pi*r^2)
#
# The integrated heat flux across the gap at time 1 is then:
#
# 4*pi*k*delta_T/((1/r1)-(1/r2))
# 4*pi*1*100/((1/1) - (1/2)) = 2513.3 watts
#
# For comparison, see results from the integrated flux post processors.
# This simulation makes use of symmetry, so only 1/2 of the spheres is meshed
# As such, the integrated flux from the post processors is 1/2 of the total,
# or 1256.6 watts... i.e. 400*pi.
# The value coming from the post processor is slightly less than this
# but converges as mesh refinement increases.
#
# Simulating contact is challenging. Regression tests that exercise
# contact features can be difficult to solve consistently across multiple
# platforms. While designing these tests, we felt it worth while to note
# some aspects of these tests. The following applies to:
# sphere3D.i, sphere2DRZ.i, cyl2D.i, and cyl3D.i.
# 1. We decided that to perform consistently across multiple platforms we
# would use very small convergence tolerance. In this test we chose an
# nl_rel_tol of 1e-12.
# 2. Due to such a high value for thermal conductivity (used here so that the
# domains come to a uniform temperature) the integrated flux at time = 0
# was relatively large (the value coming from SideIntegralFlux =
# -_diffusion_coef[_qp]*_grad_u[_qp]*_normals[_qp] where the diffusion coefficient
# here is thermal conductivity).
# Even though _grad_u[_qp] is small, in this case the diffusion coefficient
# is large. The result is a number that isn't exactly zero and tends to
# fail exodiff. For this reason the parameter execute_on = initial should not
# be used. That parameter is left to default settings in these regression tests.
#
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Problem]
coord_type = RZ
[]
[Mesh]
file = cyl2D.e
[]
[Functions]
[./temp]
type = PiecewiseLinear
x = '0 1'
y = '100 200'
[../]
[]
[Variables]
[./temp]
initial_condition = 100
[../]
[]
[AuxVariables]
[./gap_conductance]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./heat_conduction]
type = HeatConduction
variable = temp
[../]
[]
[AuxKernels]
[./gap_cond]
type = MaterialRealAux
property = gap_conductance
variable = gap_conductance
boundary = 2
[../]
[]
[Materials]
[./heat1]
type = HeatConductionMaterial
block = '1 2'
specific_heat = 1.0
thermal_conductivity = 1000000.0
[../]
[]
[ThermalContact]
[./thermal_contact]
type = GapHeatTransfer
variable = temp
primary = 3
secondary = 2
emissivity_primary = 0
emissivity_secondary = 0
gap_conductivity = 1
quadrature = true
gap_geometry_type = SPHERE
sphere_origin = '0 0 0'
[../]
[]
[BCs]
[./mid]
type = FunctionDirichletBC
boundary = 1
variable = temp
function = temp
[../]
[./temp_far_right]
type = DirichletBC
boundary = 4
variable = temp
value = 100
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
dt = 1
dtmin = 0.01
end_time = 1
nl_rel_tol = 1e-12
nl_abs_tol = 1e-7
[./Quadrature]
order = fifth
side_order = seventh
[../]
[]
[Outputs]
exodus = true
[./Console]
type = Console
[../]
[]
[Postprocessors]
[./temp_left]
type = SideAverageValue
boundary = 2
variable = temp
[../]
[./temp_right]
type = SideAverageValue
boundary = 3
variable = temp
[../]
[./flux_left]
type = SideFluxIntegral
variable = temp
boundary = 2
diffusivity = thermal_conductivity
[../]
[./flux_right]
type = SideFluxIntegral
variable = temp
boundary = 3
diffusivity = thermal_conductivity
[../]
[]
(modules/tensor_mechanics/test/tests/jacobian_damper/cube_load.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
displacements = 'disp_x disp_y disp_z'
# This test uses ElementalVariableValue postprocessors on specific
# elements, so element numbering needs to stay unchanged
allow_renumbering = false
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./total_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./top_pull]
type = PiecewiseLinear
x = '0 1 2'
y = '0 0.025 0.05'
[../]
[]
[Kernels]
[./TensorMechanics]
displacements = 'disp_x disp_y disp_z'
use_displaced_mesh = true
[../]
[]
[AuxKernels]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
[../]
[./total_strain_yy]
type = RankTwoAux
rank_two_tensor = total_strain
variable = total_strain_yy
index_i = 1
index_j = 1
[../]
[]
[BCs]
[./y_pull_function]
type = FunctionDirichletBC
variable = disp_y
boundary = 3
function = top_pull
[../]
[./x_bot]
type = DirichletBC
variable = disp_x
boundary = 4
value = 0.0
[../]
[./y_bot]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./z_bot]
type = DirichletBC
variable = disp_z
boundary = 0
value = 0.0
[../]
[]
[Postprocessors]
[./stress_yy_el]
type = ElementalVariableValue
variable = stress_yy
elementid = 0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
poissons_ratio = 0.3
youngs_modulus = 2e5
[../]
[./strain]
type = ComputeFiniteStrain
displacements = 'disp_x disp_y disp_z'
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Dampers]
[./disp_x_damp]
type = ElementJacobianDamper
max_increment = 0.002
displacements = 'disp_x disp_y disp_z'
[../]
[]
[Executioner]
type = Transient
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 4'
line_search = 'none'
l_max_its = 100
nl_max_its = 100
nl_rel_tol = 1e-12
nl_abs_tol = 1e-10
l_tol = 1e-9
start_time = 0.0
end_time = 2
dt = 1
[]
[Outputs]
exodus = true
[]
(test/tests/geomsearch/3d_moving_penetration_smoothing/pl_test3nnstt.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
file = pl_test3tt.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./normal_z]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./closest_point_z]
[../]
# [./element_id]
# [../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[./diff_z]
type = Diffusion
variable = disp_z
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
tangential_tolerance = 0.09
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
tangential_tolerance = 0.09
normal_smoothing_method = nodal_normal_based
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = normal_z
boundary = 11
paired_boundary = 12
quantity = normal_z
[../]
[./penetrate10]
type = PenetrationAux
variable = normal_z
boundary = 12
paired_boundary = 11
quantity = normal_z
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate13]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate14]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate15]
type = PenetrationAux
variable = closest_point_z
boundary = 11
paired_boundary = 12
quantity = closest_point_z
[../]
[./penetrate16]
type = PenetrationAux
variable = closest_point_z
boundary = 12
paired_boundary = 11
quantity = closest_point_z
[../]
# [./penetrate17]
# type = PenetrationAux
# variable = element_id
# boundary = 11
# paired_boundary = 12
# quantity = element_id
# [../]
#
# [./penetrate18]
# type = PenetrationAux
# variable = element_id
# boundary = 12
# paired_boundary = 11
# quantity = element_id
# [../]
[./penetrate19]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate20]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
preset = false
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
preset = false
boundary = 1
value = 0
[../]
[./b1z]
type = DirichletBC
variable = disp_z
preset = false
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
preset = false
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
preset = false
boundary = 2
function = disp_y
[../]
[./b2z]
type = DirichletBC
variable = disp_z
preset = false
boundary = 2
value = 0
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-9
l_max_its = 10
start_time = 0.0
dt = 0.02
end_time = 1.0
[]
[Outputs]
file_base = pl_test3nnstt_out
exodus = true
[]
[NodalNormals]
boundary = 11
corner_boundary = 20
[]
(modules/tensor_mechanics/test/tests/central_difference/lumped/2D/2d_nodalmass_implicit.i)
# One element test to test the central difference time integrator.
[Mesh]
[./generated_mesh]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 2
nx = 1
ny = 2
[../]
[./all_nodes]
type = BoundingBoxNodeSetGenerator
new_boundary = 'all'
input = 'generated_mesh'
top_right = '1 2 0'
bottom_left = '0 0 0'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./accel_x]
[../]
[./vel_x]
[../]
[./accel_y]
[../]
[./vel_y]
[../]
[]
[AuxKernels]
[./accel_x]
type = TestNewmarkTI
variable = accel_x
displacement = disp_x
first = false
[../]
[./vel_x]
type = TestNewmarkTI
variable = vel_x
displacement = disp_x
[../]
[./accel_y]
type = TestNewmarkTI
variable = accel_y
displacement = disp_y
first = false
[../]
[./vel_y]
type = TestNewmarkTI
variable = vel_y
displacement = disp_y
[../]
[]
[Kernels]
[./DynamicTensorMechanics]
displacements = 'disp_x disp_y'
[../]
[]
[BCs]
[./y_bot]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./x_bot]
type = PresetDisplacement
boundary = bottom
variable = disp_x
beta = 0.25
velocity = vel_x
acceleration = accel_x
function = disp
[../]
[]
[Functions]
[./disp]
type = PiecewiseLinear
x = '0.0 1.0 2.0 3.0 4.0' # time
y = '0.0 1.0 0.0 -1.0 0.0' # displacement
[../]
[]
[NodalKernels]
[./nodal_mass_x]
type = NodalTranslationalInertia
variable = 'disp_x'
nodal_mass_file = 'nodal_mass_file.csv'
boundary = 'all'
[../]
[./nodal_mass_y]
type = NodalTranslationalInertia
variable = 'disp_y'
nodal_mass_file = 'nodal_mass_file.csv'
boundary = 'all'
[../]
[]
[Materials]
[./elasticity_tensor_block]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.25
block = 0
[../]
[./strain_block]
type = ComputeIncrementalSmallStrain
block = 0
displacements = 'disp_x disp_y'
[../]
[./stress_block]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
nl_abs_tol = 1e-11
nl_rel_tol = 1e-11
start_time = -0.01
end_time = 0.1
dt = 0.005
timestep_tolerance = 1e-6
[./TimeIntegrator]
type = NewmarkBeta
beta = 0.25
gamma = 0.5
[../]
[]
[Postprocessors]
[./accel_2x]
type = PointValue
point = '1.0 2.0 0.0'
variable = accel_x
[../]
[]
[Outputs]
exodus = false
csv = true
[]
(modules/combined/test/tests/reference_residual/reference_residual_perfgraph.i)
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 4
ny = 4
nz = 4
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[./temp]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./saved_x]
[../]
[./saved_y]
[../]
[./saved_z]
[../]
[./saved_t]
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
volumetric_locking_correction = true
incremental = true
save_in = 'saved_x saved_y saved_z'
eigenstrain_names = thermal_expansion
strain = FINITE
decomposition_method = EigenSolution
extra_vector_tags = 'ref'
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
save_in = saved_t
extra_vector_tags = 'ref'
[../]
[]
[Functions]
[./pull]
type = PiecewiseLinear
x = '0 1 2'
y = '0 1 1'
scale_factor = 0.1
[../]
[]
[BCs]
[./bottom_x]
type = DirichletBC
variable = disp_x
boundary = bottom
value = 0.0
[../]
[./bottom_y]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./bottom_z]
type = DirichletBC
variable = disp_z
boundary = bottom
value = 0.0
[../]
[./top_x]
type = DirichletBC
variable = disp_x
boundary = top
value = 0.0
[../]
[./top_y]
type = FunctionDirichletBC
variable = disp_y
boundary = top
function = pull
[../]
[./top_z]
type = DirichletBC
variable = disp_z
boundary = top
value = 0.0
[../]
[./bottom_temp]
type = DirichletBC
variable = temp
boundary = bottom
value = 10.0
[../]
[./top_temp]
type = DirichletBC
variable = temp
boundary = top
value = 20.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = 0
youngs_modulus = 1.0
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[./thermal_expansion]
type = ComputeThermalExpansionEigenstrain
block = 0
eigenstrain_name = thermal_expansion
temperature = temp
thermal_expansion_coeff = 1e-5
stress_free_temperature = 0.0
[../]
[./heat1]
type = HeatConductionMaterial
block = 0
specific_heat = 1.0
thermal_conductivity = 1e-3 #Tuned to give temperature reference resid close to that of solidmech
[../]
[./density]
type = Density
block = 0
density = 1.0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
nl_rel_tol = 1e-10
l_tol = 1e-3
l_max_its = 100
dt = 1.0
end_time = 2.0
[]
[Postprocessors]
[./res_calls]
type = PerfGraphData
section_name = "ReferenceResidualProblem::computeResidualInternal"
data_type = calls
[../]
[./elapsed]
type = PerfGraphData
section_name = "Root"
data_type = total
[../]
[]
[Outputs]
csv = true
[]
(modules/contact/test/tests/nodal_area/nodal_area_Hex27.i)
[Mesh]
file = nodal_area_Hex27.e
[]
[GlobalParams]
order = SECOND
displacements = 'displ_x displ_y displ_z'
[]
[Functions]
[./disp]
type = PiecewiseLinear
x = '0 1'
y = '0 20e-6'
[../]
[]
[Variables]
[./displ_x]
[../]
[./displ_y]
[../]
[./displ_z]
[../]
[]
[AuxVariables]
[./react_x]
[../]
[./react_y]
[../]
[./react_z]
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
incremental = true
save_in = 'react_x react_y react_z'
add_variables = true
strain = FINITE
generate_output = 'stress_xx'
[../]
[]
[BCs]
[./move_right]
type = FunctionDirichletBC
boundary = '1'
variable = displ_x
function = disp
[../]
[./fixed_x]
type = DirichletBC
boundary = '3 4'
variable = displ_x
value = 0
[../]
[./fixed_y]
type = DirichletBC
boundary = 10
variable = displ_y
value = 0
[../]
[./fixed_z]
type = DirichletBC
boundary = 11
variable = displ_z
value = 0
[../]
[]
[Contact]
[./dummy_name]
primary = 3
secondary = 2
penalty = 1e8
tangential_tolerance = 1e-4
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = '1 2'
youngs_modulus = 1e6
poissons_ratio = 0.0
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
#petsc_options_iname = '-snes_type -snes_ls -snes_linesearch_type -ksp_gmres_restart -pc_type'
#petsc_options_value = 'ls basic basic 201 lu'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 4'
line_search = 'none'
nl_abs_tol = 1e-7
nl_rel_tol = 1e-6
l_tol = 1e-4
l_max_its = 40
start_time = 0.0
dt = 1.0
end_time = 1.0
num_steps = 100
[./Quadrature]
order = THIRD
[../]
[]
[Postprocessors]
[./react_x]
type = NodalSum
variable = react_x
boundary = 1
[../]
[./total_area]
type = NodalSum
variable = nodal_area_dummy_name
boundary = 2
[../]
[]
[Outputs]
exodus = true
[]
(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/geomsearch/3d_moving_penetration/pl_test1.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
file = pl_test1.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./normal_z]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./closest_point_z]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[./diff_z]
type = Diffusion
variable = disp_z
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = normal_z
boundary = 11
paired_boundary = 12
quantity = normal_z
[../]
[./penetrate10]
type = PenetrationAux
variable = normal_z
boundary = 12
paired_boundary = 11
quantity = normal_z
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate13]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate14]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate15]
type = PenetrationAux
variable = closest_point_z
boundary = 11
paired_boundary = 12
quantity = closest_point_z
[../]
[./penetrate16]
type = PenetrationAux
variable = closest_point_z
boundary = 12
paired_boundary = 11
quantity = closest_point_z
[../]
[./penetrate17]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate18]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate19]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate20]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b1z]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[./b2z]
type = DirichletBC
variable = disp_z
boundary = 2
value = 0
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 0.7 -0.7 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-9
l_max_its = 10
start_time = 0.0
dt = 0.05
end_time = 1.0
[]
[Outputs]
file_base = pl_test1_out
exodus = 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/tensor_mechanics/test/tests/strain_energy_density/tot_model.i)
# Single element test to check the strain energy density calculation
[GlobalParams]
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
xmin = 0
xmax = 1
ymin = 0
ymax = 2
[]
[AuxVariables]
[./SED]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./rampConstantUp]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = -100
[../]
[]
[Modules/TensorMechanics/Master]
[./master]
strain = SMALL
add_variables = true
incremental = false
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress strain_xx strain_yy strain_zz'
planar_formulation = PLANE_STRAIN
[../]
[]
[AuxKernels]
[./SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 'left'
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = 'bottom'
value = 0.0
[../]
[./Pressure]
[./top]
boundary = 'top'
function = rampConstantUp
[../]
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 30e+6
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeLinearElasticStress
[../]
[./strain_energy_density]
type = StrainEnergyDensity
incremental = false
[../]
[]
[Executioner]
type = Transient
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 4'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_abs_tol = 3e-7
nl_rel_tol = 1e-12
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Postprocessors]
[./epxx]
type = ElementalVariableValue
variable = strain_xx
elementid = 0
[../]
[./epyy]
type = ElementalVariableValue
variable = strain_yy
elementid = 0
[../]
[./epzz]
type = ElementalVariableValue
variable = strain_zz
elementid = 0
[../]
[./sigxx]
type = ElementAverageValue
variable = stress_xx
[../]
[./sigyy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigzz]
type = ElementAverageValue
variable = stress_zz
[../]
[./SED]
type = ElementAverageValue
variable = SED
[../]
[]
[Outputs]
exodus = true
csv = true
[]
(modules/tensor_mechanics/test/tests/beam/dynamic/dyn_timoshenko_small.i)
# Test for small strain Timoshenko beam vibration in y direction
# An impulse load is applied at the end of a cantilever beam of length 4m.
# The properties of the cantilever beam are as follows:
# Young's modulus (E) = 2e4
# Shear modulus (G) = 1e4
# Shear coefficient (k) = 1.0
# Cross-section area (A) = 1.0
# Iy = 1.0 = Iz
# Length (L)= 4 m
# density (rho) = 1.0
# For this beam, the dimensionless parameter alpha = kAGL^2/EI = 8
# Therefore, the beam behaves like a Timoshenko beam.
# The FEM solution for this beam with 100 elements give first natural period of 0.2731s with a time step of 0.005.
# The acceleration, velocity and displacement time histories obtained from MOOSE matches with those obtained from ABAQUS.
# Values from the first few time steps are as follows:
# time disp_y vel_y accel_y
# 0.0 0.0 0.0 0.0
# 0.005 2.5473249455812e-05 0.010189299782325 4.0757199129299
# 0.01 5.3012872677486e-05 0.00082654950634483 -7.8208200233219
# 0.015 5.8611622914354e-05 0.0014129505884026 8.055380456145
# 0.02 6.766113649781e-05 0.0022068548449798 -7.7378187535141
# 0.025 7.8981810558437e-05 0.0023214147792709 7.7836427272305
# Note that the theoretical first frequency of the beam using Euler-Bernoulli theory is:
# f1 = 1/(2 pi) * (3.5156/L^2) * sqrt(EI/rho) = 4.9455
# This implies that the corresponding time period of this beam (under Euler-Bernoulli assumption) is 0.2022s.
# This shows that Euler-Bernoulli beam theory under-predicts the time period of a thick beam. In other words, the Euler-Bernoulli beam theory predicts a more compliant beam than reality for a thick beam.
[Mesh]
type = GeneratedMesh
xmin = 0
xmax = 4.0
nx = 100
dim = 1
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[./rot_x]
order = FIRST
family = LAGRANGE
[../]
[./rot_y]
order = FIRST
family = LAGRANGE
[../]
[./rot_z]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./vel_x]
order = FIRST
family = LAGRANGE
[../]
[./vel_y]
order = FIRST
family = LAGRANGE
[../]
[./vel_z]
order = FIRST
family = LAGRANGE
[../]
[./accel_x]
order = FIRST
family = LAGRANGE
[../]
[./accel_y]
order = FIRST
family = LAGRANGE
[../]
[./accel_z]
order = FIRST
family = LAGRANGE
[../]
[./rot_vel_x]
order = FIRST
family = LAGRANGE
[../]
[./rot_vel_y]
order = FIRST
family = LAGRANGE
[../]
[./rot_vel_z]
order = FIRST
family = LAGRANGE
[../]
[./rot_accel_x]
order = FIRST
family = LAGRANGE
[../]
[./rot_accel_y]
order = FIRST
family = LAGRANGE
[../]
[./rot_accel_z]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./accel_x]
type = NewmarkAccelAux
variable = accel_x
displacement = disp_x
velocity = vel_x
beta = 0.25
execute_on = timestep_end
[../]
[./vel_x]
type = NewmarkVelAux
variable = vel_x
acceleration = accel_x
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_y]
type = NewmarkAccelAux
variable = accel_y
displacement = disp_y
velocity = vel_y
beta = 0.25
execute_on = timestep_end
[../]
[./vel_y]
type = NewmarkVelAux
variable = vel_y
acceleration = accel_y
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_z]
type = NewmarkAccelAux
variable = accel_z
displacement = disp_z
velocity = vel_z
beta = 0.25
execute_on = timestep_end
[../]
[./vel_z]
type = NewmarkVelAux
variable = vel_z
acceleration = accel_z
gamma = 0.5
execute_on = timestep_end
[../]
[./rot_accel_x]
type = NewmarkAccelAux
variable = rot_accel_x
displacement = rot_x
velocity = rot_vel_x
beta = 0.25
execute_on = timestep_end
[../]
[./rot_vel_x]
type = NewmarkVelAux
variable = rot_vel_x
acceleration = rot_accel_x
gamma = 0.5
execute_on = timestep_end
[../]
[./rot_accel_y]
type = NewmarkAccelAux
variable = rot_accel_y
displacement = rot_y
velocity = rot_vel_y
beta = 0.25
execute_on = timestep_end
[../]
[./rot_vel_y]
type = NewmarkVelAux
variable = rot_vel_y
acceleration = rot_accel_y
gamma = 0.5
execute_on = timestep_end
[../]
[./rot_accel_z]
type = NewmarkAccelAux
variable = rot_accel_z
displacement = rot_z
velocity = rot_vel_z
beta = 0.25
execute_on = timestep_end
[../]
[./rot_vel_z]
type = NewmarkVelAux
variable = rot_vel_z
acceleration = rot_accel_z
gamma = 0.5
execute_on = timestep_end
[../]
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./fixy1]
type = DirichletBC
variable = disp_y
boundary = left
value = 0.0
[../]
[./fixz1]
type = DirichletBC
variable = disp_z
boundary = left
value = 0.0
[../]
[./fixr1]
type = DirichletBC
variable = rot_x
boundary = left
value = 0.0
[../]
[./fixr2]
type = DirichletBC
variable = rot_y
boundary = left
value = 0.0
[../]
[./fixr3]
type = DirichletBC
variable = rot_z
boundary = left
value = 0.0
[../]
[]
[NodalKernels]
[./force_y2]
type = UserForcingFunctionNodalKernel
variable = disp_y
boundary = right
function = force
[../]
[]
[Functions]
[./force]
type = PiecewiseLinear
x = '0.0 0.005 0.01 1.0'
y = '0.0 1.0 0.0 0.0'
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
line_search = 'none'
nl_rel_tol = 1e-11
nl_abs_tol = 1e-11
start_time = 0.0
dt = 0.005
end_time = 0.5
timestep_tolerance = 1e-6
[]
[Kernels]
[./solid_disp_x]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 0
variable = disp_x
[../]
[./solid_disp_y]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 1
variable = disp_y
[../]
[./solid_disp_z]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 2
variable = disp_z
[../]
[./solid_rot_x]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 3
variable = rot_x
[../]
[./solid_rot_y]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 4
variable = rot_y
[../]
[./solid_rot_z]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 5
variable = rot_z
[../]
[./inertial_force_x]
type = InertialForceBeam
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y rot_vel_z'
rotational_accelerations = 'rot_accel_x rot_accel_y rot_accel_z'
beta = 0.25
gamma = 0.5
area = 1.0
Iy = 1.0
Iz = 1.0
Ay = 0.0
Az = 0.0
component = 0
variable = disp_x
[../]
[./inertial_force_y]
type = InertialForceBeam
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y rot_vel_z'
rotational_accelerations = 'rot_accel_x rot_accel_y rot_accel_z'
beta = 0.25
gamma = 0.5
area = 1.0
Iy = 1.0
Iz = 1.0
Ay = 0.0
Az = 0.0
component = 1
variable = disp_y
[../]
[./inertial_force_z]
type = InertialForceBeam
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y rot_vel_z'
rotational_accelerations = 'rot_accel_x rot_accel_y rot_accel_z'
beta = 0.25
gamma = 0.5
area = 1.0
Iy = 1.0
Iz = 1.0
Ay = 0.0
Az = 0.0
component = 2
variable = disp_z
[../]
[./inertial_force_rot_x]
type = InertialForceBeam
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y rot_vel_z'
rotational_accelerations = 'rot_accel_x rot_accel_y rot_accel_z'
beta = 0.25
gamma = 0.5
area = 1.0
Iy = 1.0
Iz = 1.0
Ay = 0.0
Az = 0.0
component = 3
variable = rot_x
[../]
[./inertial_force_rot_y]
type = InertialForceBeam
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y rot_vel_z'
rotational_accelerations = 'rot_accel_x rot_accel_y rot_accel_z'
beta = 0.25
gamma = 0.5
area = 1.0
Iy = 1.0
Iz = 1.0
Ay = 0.0
Az = 0.0
component = 4
variable = rot_y
[../]
[./inertial_force_rot_z]
type = InertialForceBeam
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y rot_vel_z'
rotational_accelerations = 'rot_accel_x rot_accel_y rot_accel_z'
beta = 0.25
gamma = 0.5
area = 1.0
Iy = 1.0
Iz = 1.0
Ay = 0.0
Az = 0.0
component = 5
variable = rot_z
[../]
[]
[Materials]
[./elasticity]
type = ComputeElasticityBeam
youngs_modulus = 2e4
poissons_ratio = 0.0
shear_coefficient = 1.0
block = 0
[../]
[./strain]
type = ComputeIncrementalBeamStrain
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
area = 1.0
Ay = 0.0
Az = 0.0
Iy = 1.0
Iz = 1.0
y_orientation = '0.0 1.0 0.0'
[../]
[./stress]
type = ComputeBeamResultants
block = 0
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = 'density'
prop_values = '1.0'
[../]
[]
[Postprocessors]
[./disp_x]
type = PointValue
point = '4.0 0.0 0.0'
variable = disp_x
[../]
[./disp_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = disp_y
[../]
[./vel_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = vel_y
[../]
[./accel_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = accel_y
[../]
[]
[Outputs]
exodus = true
csv = true
perf_graph = true
[]
(modules/tensor_mechanics/test/tests/truss/truss_3d_action.i)
[Mesh]
type = FileMesh
file = truss_3d.e
displacements = 'disp_x disp_y disp_z'
[]
[AuxVariables]
[./axial_stress]
order = CONSTANT
family = MONOMIAL
[../]
[./e_over_l]
order = CONSTANT
family = MONOMIAL
[../]
[./area]
order = CONSTANT
family = MONOMIAL
[../]
[./react_x]
order = FIRST
family = LAGRANGE
[../]
[./react_y]
order = FIRST
family = LAGRANGE
[../]
[./react_z]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
[./x2]
type = PiecewiseLinear
x = '0 1 2 3'
y = '0 .5 1 1'
[../]
[./y2]
type = PiecewiseLinear
x = '0 1 2 3'
y = '0 0 .5 1'
[../]
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
preset = false
boundary = 1
value = 0.0
[../]
[./fixx2]
type = FunctionDirichletBC
variable = disp_x
preset = false
boundary = 2
function = x2
[../]
[./fixx3]
type = DirichletBC
variable = disp_x
preset = false
boundary = 3
value = 0.0
[../]
[./fixy1]
type = DirichletBC
variable = disp_y
preset = false
boundary = 1
value = 0
[../]
[./fixy2]
type = FunctionDirichletBC
variable = disp_y
preset = false
boundary = 2
function = y2
[../]
[./fixy3]
type = DirichletBC
variable = disp_y
preset = false
boundary = 3
value = 0
[../]
[./fixz1]
type = DirichletBC
variable = disp_z
preset = false
boundary = 1
value = 0
[../]
[./fixz2]
type = DirichletBC
variable = disp_z
preset = false
boundary = 2
value = 0
[../]
[./fixz3]
type = DirichletBC
variable = disp_z
preset = false
boundary = 3
value = 0
[../]
[]
[AuxKernels]
[./axial_stress]
type = MaterialRealAux
block = '1 2'
property = axial_stress
variable = axial_stress
[../]
[./e_over_l]
type = MaterialRealAux
block = '1 2'
property = e_over_l
variable = e_over_l
[../]
[./area]
type = ConstantAux
block = '1 2'
variable = area
value = 1.0
execute_on = 'initial timestep_begin'
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
petsc_options_iname = '-pc_type -ksp_gmres_restart'
petsc_options_value = 'jacobi 101'
line_search = 'none'
nl_max_its = 15
nl_rel_tol = 1e-6
nl_abs_tol = 1e-10
dt = 1
num_steps = 3
end_time = 3
[]
[Modules/TensorMechanics/LineElementMaster]
[./block]
truss = true
add_variables = true
displacements = 'disp_x disp_y disp_z'
area = area
block = '1 2'
save_in = 'react_x react_y react_z'
[../]
[]
[Materials]
[./linelast]
type = LinearElasticTruss
block = '1 2'
youngs_modulus = 1e6
displacements = 'disp_x disp_y disp_z'
[../]
[]
[Outputs]
file_base = 'truss_3d_out'
exodus = true
[]
(modules/tensor_mechanics/test/tests/truss/truss_plastic.i)
[Mesh]
type = GeneratedMesh
dim = 1
elem_type = EDGE
nx = 1
[]
[GlobalParams]
displacements = 'disp_x'
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./axial_stress]
order = CONSTANT
family = MONOMIAL
[../]
[./e_over_l]
order = CONSTANT
family = MONOMIAL
[../]
[./area]
order = CONSTANT
family = MONOMIAL
[../]
[./react_x]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
[./hf]
type = PiecewiseLinear
x = '0 0.0001 0.0003 0.0023'
y = '50e6 52e6 54e6 56e6'
[../]
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./load]
type = FunctionDirichletBC
variable = disp_x
boundary = right
function = 't'
[../]
[]
[AuxKernels]
[./axial_stress]
type = MaterialRealAux
property = axial_stress
variable = axial_stress
[../]
[./e_over_l]
type = MaterialRealAux
property = e_over_l
variable = e_over_l
[../]
[./area]
type = ConstantAux
variable = area
value = 1.0
execute_on = 'initial timestep_begin'
[../]
[]
[Postprocessors]
[./s_xx]
type = ElementIntegralMaterialProperty
mat_prop = axial_stress
[../]
[./e_xx]
type = ElementIntegralMaterialProperty
mat_prop = total_stretch
[../]
[./ee_xx]
type = ElementIntegralMaterialProperty
mat_prop = elastic_stretch
[../]
[./ep_xx]
type = ElementIntegralMaterialProperty
mat_prop = plastic_stretch
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
nl_abs_tol = 1e-11
l_max_its = 20
dt = 5e-5
num_steps = 10
[]
[Kernels]
[./solid]
type = StressDivergenceTensorsTruss
component = 0
variable = disp_x
area = area
save_in = react_x
[../]
[]
[Materials]
[./truss]
type = PlasticTruss
youngs_modulus = 2.0e11
yield_stress = 500e5
outputs = exodus
[../]
[]
[Outputs]
exodus = true
csv = true
[]
(modules/tensor_mechanics/test/tests/j_integral/j_integral_2d.i)
#This tests the J-Integral evaluation capability.
#This is a 2d plane strain model
#The analytic solution for J1 is 2.434. This model
#converges to that solution with a refined mesh.
#Reference: National Agency for Finite Element Methods and Standards (U.K.):
#Test 1.1 from NAFEMS publication "Test Cases in Linear Elastic Fracture
#Mechanics" R0020.
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[Mesh]
file = crack2d.e
[]
[AuxVariables]
[./SED]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./rampConstant]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = -1e2
[../]
[]
[DomainIntegral]
integrals = JIntegral
boundary = 800
crack_direction_method = CrackDirectionVector
crack_direction_vector = '1 0 0'
2d = true
axis_2d = 2
radius_inner = '4.0 4.5 5.0 5.5 6.0'
radius_outer = '4.5 5.0 5.5 6.0 6.5'
output_q = false
incremental = true
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
planar_formulation = PLANE_STRAIN
[../]
[]
[AuxKernels]
[./SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[../]
[]
[BCs]
[./crack_y]
type = DirichletBC
variable = disp_y
boundary = 100
value = 0.0
[../]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 700
value = 0.0
[../]
[./Pressure]
[./Side1]
boundary = 400
function = rampConstant
[../]
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_rel_tol = 1e-12
nl_abs_tol = 1e-5
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Outputs]
file_base = j_integral_2d_out
exodus = true
csv = true
[]
(modules/contact/test/tests/nodal_area/nodal_area_Hex20.i)
[Mesh]
file = nodal_area_Hex20.e
[]
[GlobalParams]
order = SECOND
displacements = 'displ_x displ_y displ_z'
[]
[Functions]
[./disp]
type = PiecewiseLinear
x = '0 1'
y = '0 20e-6'
[../]
[]
[Variables]
[./displ_x]
[../]
[./displ_y]
[../]
[./displ_z]
[../]
[]
[AuxVariables]
[./react_x]
[../]
[./react_y]
[../]
[./react_z]
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
incremental = true
save_in = 'react_x react_y react_z'
add_variables = true
strain = FINITE
generate_output = 'stress_xx'
[../]
[]
[BCs]
[./move_right]
type = FunctionDirichletBC
boundary = '1'
variable = displ_x
function = disp
[../]
[./fixed_x]
type = DirichletBC
boundary = '3 4'
variable = displ_x
value = 0
[../]
[./fixed_y]
type = DirichletBC
boundary = 10
variable = displ_y
value = 0
[../]
[./fixed_z]
type = DirichletBC
boundary = 11
variable = displ_z
value = 0
[../]
[]
[Contact]
[./dummy_name]
primary = 3
secondary = 2
penalty = 1e7
tangential_tolerance = 1e-5
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = '1 2'
youngs_modulus = 1e6
poissons_ratio = 0.0
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 4'
line_search = 'none'
nl_rel_tol = 1e-9
l_tol = 1e-4
l_max_its = 40
start_time = 0.0
dt = 1.0
end_time = 1.0
[./Quadrature]
order = THIRD
[../]
[]
[Postprocessors]
[./react_x]
type = NodalSum
variable = react_x
boundary = 1
execute_on = 'initial timestep_end'
[../]
[./total_area]
type = NodalSum
variable = nodal_area_dummy_name
boundary = 2
execute_on = 'initial timestep_end'
[../]
[]
[Outputs]
exodus = true
[]
(modules/richards/test/tests/theis/th_lumped_02.i)
# fully-saturated
# production
# lumped
[Mesh]
type = FileMesh
file = th02_input.e
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = DensityConstBulk
relperm_UO = RelPermPower
sat_UO = Saturation
seff_UO = Seff1VG
SUPG_UO = SUPGstandard
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1 2 4 20'
x = '0 1 10 100'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1000
bulk_mod = 2E9
[../]
[./Seff1VG]
type = RichardsSeff1VG
m = 0.8
al = 1E-5
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0
sum_s_res = 0
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 1E-5
[../]
[./total_outflow_mass]
type = RichardsSumQuantity
[../]
[]
[Variables]
active = 'pressure'
[./pressure]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./p_ic]
type = FunctionIC
variable = pressure
function = initial_pressure
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[Kernels]
active = 'richardsf richardst'
[./richardst]
type = RichardsLumpedMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[DiracKernels]
[./bh]
type = RichardsPolyLineSink
pressures = '-1E9 1E9'
fluxes = '200 200'
point_file = th01.points
SumQuantityUO = total_outflow_mass
variable = pressure
[../]
[]
[Postprocessors]
[./flow_report]
type = RichardsPlotQuantity
uo = total_outflow_mass
[../]
[./p50]
type = PointValue
variable = pressure
point = '50 0 0'
execute_on = 'initial timestep_end'
[../]
[]
[Functions]
[./initial_pressure]
type = ParsedFunction
value = 1E5
[../]
[]
[Materials]
[./all]
type = RichardsMaterial
block = 1
viscosity = 1E-3
mat_porosity = 0.1
mat_permeability = '1E-10 0 0 0 1E-10 0 0 0 1E-10'
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = Seff1VG
pressure_vars = pressure
[../]
[]
[Preconditioning]
[./usual]
type = SMP
full = true
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -ksp_max_it'
petsc_options_value = 'bcgs bjacobi 1E-6 1E-10 10000 30'
[../]
[]
[Executioner]
type = Transient
end_time = 100
solve_type = NEWTON
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = th_lumped_02
csv = true
[]
(modules/contact/test/tests/normalized_penalty/normalized_penalty.i)
[GlobalParams]
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Mesh]
file = normalized_penalty.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Functions]
[./left_x]
type = PiecewiseLinear
x = '0 1 2'
y = '0 0.02 0'
[../]
[]
[AuxVariables]
[./saved_x]
[../]
[./saved_y]
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = FINITE
generate_output = 'stress_xx'
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
[]
[]
[Contact]
[./m3_s2]
primary = 3
secondary = 2
penalty = 1e10
normalize_penalty = true
formulation = penalty
tangential_tolerance = 1e-3
[../]
[]
[BCs]
[./left_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 1
function = left_x
[../]
[./y]
type = DirichletBC
variable = disp_y
boundary = '1 2 3 4'
value = 0.0
[../]
[./right]
type = DirichletBC
variable = disp_x
boundary = '3 4'
value = 0
[../]
[]
[Materials]
[./stiffStuff1]
type = ComputeIsotropicElasticityTensor
block = '1 2 3 4 1000'
youngs_modulus = 3e8
poissons_ratio = 0.0
[../]
[./stiffStuff1_stress]
type = ComputeFiniteStrainElasticStress
block = '1 2 3 4 1000'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -ksp_gmres_restart'
petsc_options_value = 'lu 101'
line_search = 'none'
nl_rel_tol = 1e-12
nl_abs_tol = 5e-8
l_max_its = 100
nl_max_its = 10
dt = 0.5
num_steps = 4
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/j_integral/j_integral_2d_topo_q_func.i)
#This tests the J-Integral evaluation capability.
#This is a 2d plane strain model
#The analytic solution for J1 is 2.434. This model
#converges to that solution with a refined mesh.
#Reference: National Agency for Finite Element Methods and Standards (U.K.):
#Test 1.1 from NAFEMS publication "Test Cases in Linear Elastic Fracture
#Mechanics" R0020.
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[Mesh]
file = crack2d.e
[]
[AuxVariables]
[./SED]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./rampConstant]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = -1e2
[../]
[]
[DomainIntegral]
integrals = JIntegral
boundary = 800
crack_direction_method = CrackDirectionVector
crack_direction_vector = '1 0 0'
2d = true
axis_2d = 2
q_function_type = Topology
ring_first = 1
ring_last = 4
output_q = false
incremental = true
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
planar_formulation = PLANE_STRAIN
[../]
[]
[AuxKernels]
[./SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[../]
[]
[BCs]
[./crack_y]
type = DirichletBC
variable = disp_y
boundary = 100
value = 0.0
[../]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 700
value = 0.0
[../]
[./Pressure]
[./Side1]
boundary = 400
function = rampConstant
[../]
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_rel_tol = 1e-12
nl_abs_tol = 1e-5
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Outputs]
file_base = j_integral_2d_topo_q_func_out
exodus = true
csv = true
[]
(modules/tensor_mechanics/test/tests/beam/dynamic/dyn_euler_small_rayleigh_hht.i)
# Test for damped small strain euler beam vibration in y direction
# An impulse load is applied at the end of a cantilever beam of length 4m.
# The properties of the cantilever beam are as follows:
# Young's modulus (E) = 1e4
# Shear modulus (G) = 4e7
# Shear coefficient (k) = 1.0
# Cross-section area (A) = 0.01
# Iy = 1e-4 = Iz
# Length (L)= 4 m
# density (rho) = 1.0
# mass proportional rayleigh damping(eta) = 0.1
# stiffness proportional rayleigh damping(eta) = 0.1
# HHT time integration parameter (alpha) = -0.3
# Corresponding Newmark beta time integration parameters beta = 0.4225 and gamma = 0.8
# For this beam, the dimensionless parameter alpha = kAGL^2/EI = 6.4e6
# Therefore, the behaves like a Euler-Bernoulli beam.
# The displacement time history from this analysis matches with that obtained from Abaqus.
# Values from the first few time steps are as follows:
# time disp_y vel_y accel_y
# 0.0 0.0 0.0 0.0
# 0.2 0.019898364318588 0.18838688112273 1.1774180070171
# 0.4 0.045577003505278 0.087329917525455 -0.92596052423724
# 0.6 0.063767907208218 0.084330765885995 0.21274543331268
# 0.8 0.073602908614573 0.020029576220975 -0.45506879373455
# 1.0 0.06841704414745 -0.071840076837194 -0.46041813317992
[Mesh]
type = GeneratedMesh
nx = 10
dim = 1
xmin = 0.0
xmax = 4.0
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[./rot_x]
order = FIRST
family = LAGRANGE
[../]
[./rot_y]
order = FIRST
family = LAGRANGE
[../]
[./rot_z]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./vel_x]
order = FIRST
family = LAGRANGE
[../]
[./vel_y]
order = FIRST
family = LAGRANGE
[../]
[./vel_z]
order = FIRST
family = LAGRANGE
[../]
[./accel_x]
order = FIRST
family = LAGRANGE
[../]
[./accel_y]
order = FIRST
family = LAGRANGE
[../]
[./accel_z]
order = FIRST
family = LAGRANGE
[../]
[./rot_vel_x]
order = FIRST
family = LAGRANGE
[../]
[./rot_vel_y]
order = FIRST
family = LAGRANGE
[../]
[./rot_vel_z]
order = FIRST
family = LAGRANGE
[../]
[./rot_accel_x]
order = FIRST
family = LAGRANGE
[../]
[./rot_accel_y]
order = FIRST
family = LAGRANGE
[../]
[./rot_accel_z]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./accel_x]
type = NewmarkAccelAux
variable = accel_x
displacement = disp_x
velocity = vel_x
beta = 0.4225
execute_on = timestep_end
[../]
[./vel_x]
type = NewmarkVelAux
variable = vel_x
acceleration = accel_x
gamma = 0.8
execute_on = timestep_end
[../]
[./accel_y]
type = NewmarkAccelAux
variable = accel_y
displacement = disp_y
velocity = vel_y
beta = 0.4225
execute_on = timestep_end
[../]
[./vel_y]
type = NewmarkVelAux
variable = vel_y
acceleration = accel_y
gamma = 0.8
execute_on = timestep_end
[../]
[./accel_z]
type = NewmarkAccelAux
variable = accel_z
displacement = disp_z
velocity = vel_z
beta = 0.4225
execute_on = timestep_end
[../]
[./vel_z]
type = NewmarkVelAux
variable = vel_z
acceleration = accel_z
gamma = 0.8
execute_on = timestep_end
[../]
[./rot_accel_x]
type = NewmarkAccelAux
variable = rot_accel_x
displacement = rot_x
velocity = rot_vel_x
beta = 0.4225
execute_on = timestep_end
[../]
[./rot_vel_x]
type = NewmarkVelAux
variable = rot_vel_x
acceleration = rot_accel_x
gamma = 0.8
execute_on = timestep_end
[../]
[./rot_accel_y]
type = NewmarkAccelAux
variable = rot_accel_y
displacement = rot_y
velocity = rot_vel_y
beta = 0.4225
execute_on = timestep_end
[../]
[./rot_vel_y]
type = NewmarkVelAux
variable = rot_vel_y
acceleration = rot_accel_y
gamma = 0.8
execute_on = timestep_end
[../]
[./rot_accel_z]
type = NewmarkAccelAux
variable = rot_accel_z
displacement = rot_z
velocity = rot_vel_z
beta = 0.4225
execute_on = timestep_end
[../]
[./rot_vel_z]
type = NewmarkVelAux
variable = rot_vel_z
acceleration = rot_accel_z
gamma = 0.8
execute_on = timestep_end
[../]
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./fixy1]
type = DirichletBC
variable = disp_y
boundary = left
value = 0.0
[../]
[./fixz1]
type = DirichletBC
variable = disp_z
boundary = left
value = 0.0
[../]
[./fixr1]
type = DirichletBC
variable = rot_x
boundary = left
value = 0.0
[../]
[./fixr2]
type = DirichletBC
variable = rot_y
boundary = left
value = 0.0
[../]
[./fixr3]
type = DirichletBC
variable = rot_z
boundary = left
value = 0.0
[../]
[]
[NodalKernels]
[./force_y2]
type = UserForcingFunctionNodalKernel
variable = disp_y
boundary = right
function = force
[../]
[]
[Functions]
[./force]
type = PiecewiseLinear
x = '0.0 0.2 0.4 10.0'
y = '0.0 0.01 0.0 0.0'
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
l_tol = 1e-11
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 0.2
end_time = 5.0
timestep_tolerance = 1e-6
[]
[Kernels]
[./solid_disp_x]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 0
variable = disp_x
zeta = 0.1
alpha = -0.3
[../]
[./solid_disp_y]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 1
variable = disp_y
zeta = 0.1
alpha = -0.3
[../]
[./solid_disp_z]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 2
variable = disp_z
zeta = 0.1
alpha = -0.3
[../]
[./solid_rot_x]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 3
variable = rot_x
zeta = 0.1
alpha = -0.3
[../]
[./solid_rot_y]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 4
variable = rot_y
zeta = 0.1
alpha = -0.3
[../]
[./solid_rot_z]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 5
variable = rot_z
zeta = 0.1
alpha = -0.3
[../]
[./inertial_force_x]
type = InertialForceBeam
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y rot_vel_z'
rotational_accelerations = 'rot_accel_x rot_accel_y rot_accel_z'
beta = 0.4225
gamma = 0.8
eta = 0.1
area = 0.01
Iy = 1e-4
Iz = 1e-4
Ay = 0.0
Az = 0.0
component = 0
variable = disp_x
alpha = -0.3
[../]
[./inertial_force_y]
type = InertialForceBeam
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y rot_vel_z'
rotational_accelerations = 'rot_accel_x rot_accel_y rot_accel_z'
beta = 0.4225
gamma = 0.8
eta = 0.1
area = 0.01
Iy = 1e-4
Iz = 1e-4
Ay = 0.0
Az = 0.0
component = 1
variable = disp_y
alpha = -0.3
[../]
[./inertial_force_z]
type = InertialForceBeam
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y rot_vel_z'
rotational_accelerations = 'rot_accel_x rot_accel_y rot_accel_z'
beta = 0.4225
gamma = 0.8
eta = 0.1
area = 0.01
Iy = 1e-4
Iz = 1e-4
Ay = 0.0
Az = 0.0
component = 2
variable = disp_z
alpha = -0.3
[../]
[./inertial_force_rot_x]
type = InertialForceBeam
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y rot_vel_z'
rotational_accelerations = 'rot_accel_x rot_accel_y rot_accel_z'
beta = 0.4225
gamma = 0.8
eta = 0.1
area = 0.01
Iy = 1e-4
Iz = 1e-4
Ay = 0.0
Az = 0.0
component = 3
variable = rot_x
alpha = -0.3
[../]
[./inertial_force_rot_y]
type = InertialForceBeam
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y rot_vel_z'
rotational_accelerations = 'rot_accel_x rot_accel_y rot_accel_z'
beta = 0.4225
gamma = 0.8
eta = 0.1
area = 0.01
Iy = 1e-4
Iz = 1e-4
Ay = 0.0
Az = 0.0
component = 4
variable = rot_y
alpha = -0.3
[../]
[./inertial_force_rot_z]
type = InertialForceBeam
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y rot_vel_z'
rotational_accelerations = 'rot_accel_x rot_accel_y rot_accel_z'
beta = 0.4225
gamma = 0.8
eta = 0.1
area = 0.01
Iy = 1e-4
Iz = 1e-4
Ay = 0.0
Az = 0.0
component = 5
variable = rot_z
alpha = -0.3
[../]
[]
[Materials]
[./elasticity]
type = ComputeElasticityBeam
youngs_modulus = 1.0e4
poissons_ratio = -0.999875
shear_coefficient = 1.0
block = 0
[../]
[./strain]
type = ComputeIncrementalBeamStrain
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
area = 0.01
Ay = 0.0
Az = 0.0
Iy = 1.0e-4
Iz = 1.0e-4
y_orientation = '0.0 1.0 0.0'
[../]
[./stress]
type = ComputeBeamResultants
block = 0
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = 'density'
prop_values = '1.0'
[../]
[]
[Postprocessors]
[./disp_x]
type = PointValue
point = '4.0 0.0 0.0'
variable = disp_x
[../]
[./disp_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = disp_y
[../]
[./vel_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = vel_y
[../]
[./accel_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = accel_y
[../]
[]
[Outputs]
exodus = true
csv = true
perf_graph = true
[]
(modules/combined/test/tests/internal_volume/rz_quad8.i)
#
# Internal Volume Test
#
# This test is designed to compute the internal volume of a space considering
# an embedded volume inside.
#
# The mesh is composed of one block (1) with an interior cavity of volume 8.
# Block 2 sits in the cavity and has a volume of 1. Thus, the total volume
# is 7.
#
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Problem]
coord_type = RZ
[]
[Mesh]
file = meshes/rz_quad8.e
[]
[Functions]
[./pressure]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = 1e4
[../]
[]
[Variables]
[./disp_x]
order = SECOND
family = LAGRANGE
[../]
[./disp_y]
order = SECOND
family = LAGRANGE
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
incremental = true
strain = FINITE
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = '1 2'
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = '1 2'
value = 0.0
[../]
[./Pressure]
[./the_pressure]
boundary = 3
function = pressure
[../]
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = '1 2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
start_time = 0.0
dt = 1.0
end_time = 1.0
[./Quadrature]
order = THIRD
[../]
[]
[Postprocessors]
[./internalVolume]
type = InternalVolume
boundary = 2
execute_on = 'initial timestep_end'
[../]
[]
[Outputs]
exodus = true
csv = true
[]
(modules/contact/test/tests/verification/hertz_cyl/quart_symm_q4/hertz_cyl_qsym_1deg_template1.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = hertz_cyl_qsym_1deg_q4.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Functions]
[./disp_ramp_vert]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. -0.0020 -0.0020'
[../]
[./disp_ramp_zero]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 0.0 0.0'
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
[../]
[]
[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_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 4
paired_boundary = 3
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 4
paired_boundary = 3
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 4
paired_boundary = 3
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./disp_x281]
type = NodalVariableValue
nodeid = 280
variable = disp_x
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./side_x]
type = DirichletBC
variable = disp_y
boundary = '1 3'
value = 0.0
[../]
[./bot_y]
type = DirichletBC
variable = disp_x
boundary = '1 2 3'
value = 0.0
[../]
[./top_y_disp]
type = FunctionDirichletBC
variable = disp_y
boundary = 5
function = disp_ramp_vert
[../]
[]
[Materials]
[./stuff1_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e10
poissons_ratio = 0.0
[../]
[./stuff1_strain]
type = ComputeFiniteStrain
block = '1'
[../]
[./stuff1_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./stuff2_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff2_strain]
type = ComputeFiniteStrain
block = '2'
[../]
[./stuff2_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[./stuff3_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '3'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff3_strain]
type = ComputeFiniteStrain
block = '3'
[../]
[./stuff3_stress]
type = ComputeFiniteStrainElasticStress
block = '3'
[../]
[./stuff4_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '4'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff4_strain]
type = ComputeFiniteStrain
block = '4'
[../]
[./stuff4_stress]
type = ComputeFiniteStrainElasticStress
block = '4'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-6
nl_rel_tol = 1e-5
l_max_its = 50
nl_max_its = 100
start_time = 0.0
dt = 0.1
dtmin = 0.1
num_steps = 10
end_time = 1.0
l_tol = 1e-3
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '3 4 5'
sort_by = id
[../]
[./y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '3 4 5'
sort_by = id
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '4'
sort_by = id
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x281 top_react_x top_react_y x_disp y_disp cont_press'
start_time = 0.9
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./interface]
primary = 3
secondary = 4
model = glued
formulation = kinematic
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
[../]
[]
(modules/xfem/test/tests/diffusion_xfem/levelsetcut3d.i)
# 3D: Mesh is cut by level set based cutter
# The level set is a MOOSE auxvariable
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 5
ny = 5
nz = 5
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
zmin = 0.0
zmax = 1.0
elem_type = HEX8
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./level_set_cut_uo]
type = LevelSetCutUserObject
level_set_var = ls
[../]
[]
[Variables]
[./u]
[../]
[]
[Functions]
[./u_left]
type = PiecewiseLinear
x = '0 2'
y = '0 0.1'
[../]
[./ls_func]
type = ParsedFunction
value = 'sqrt(x*x + y*y + z*z) - 0.5'
[../]
[]
[AuxVariables]
[./ls]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./ls_function]
type = FunctionAux
variable = ls
function = ls_func
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = DirichletBC
variable = u
boundary = left
value = 2
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Transient
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
start_time = 0.0
dt = 1
end_time = 1.0
max_xfem_update = 1
[]
[Outputs]
interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/porous_flow/test/tests/poro_elasticity/mandel_fully_saturated_volume.i)
# Mandel's problem of consolodation of a drained medium
# Using the FullySaturatedDarcyBase and FullySaturatedFullySaturatedMassTimeDerivative kernels
# with multiply_by_density = false, so that this problem becomes linear
# Note the use of consistent_with_displaced_mesh = false in the calculation of volumetric strain
#
# A sample is in plane strain.
# -a <= x <= a
# -b <= y <= b
# It is squashed with constant force by impermeable, frictionless plattens on its top and bottom surfaces (at y=+/-b)
# Fluid is allowed to leak out from its sides (at x=+/-a)
# The porepressure within the sample is monitored.
#
# As is common in the literature, this is simulated by
# considering the quarter-sample, 0<=x<=a and 0<=y<=b, with
# impermeable, roller BCs at x=0 and y=0 and y=b.
# Porepressure is fixed at zero on x=a.
# Porepressure and displacement are initialised to zero.
# Then the top (y=b) is moved downwards with prescribed velocity,
# so that the total force that is inducing this downwards velocity
# is fixed. The velocity is worked out by solving Mandel's problem
# analytically, and the total force is monitored in the simulation
# to check that it indeed remains constant.
#
# Here are the problem's parameters, and their values:
# Soil width. a = 1
# Soil height. b = 0.1
# Soil's Lame lambda. la = 0.5
# Soil's Lame mu, which is also the Soil's shear modulus. mu = G = 0.75
# Soil bulk modulus. K = la + 2*mu/3 = 1
# Drained Poisson ratio. nu = (3K - 2G)/(6K + 2G) = 0.2
# Soil bulk compliance. 1/K = 1
# Fluid bulk modulus. Kf = 8
# Fluid bulk compliance. 1/Kf = 0.125
# Soil initial porosity. phi0 = 0.1
# Biot coefficient. alpha = 0.6
# Biot modulus. M = 1/(phi0/Kf + (alpha - phi0)(1 - alpha)/K) = 4.705882
# Undrained bulk modulus. Ku = K + alpha^2*M = 2.694118
# Undrained Poisson ratio. nuu = (3Ku - 2G)/(6Ku + 2G) = 0.372627
# Skempton coefficient. B = alpha*M/Ku = 1.048035
# Fluid mobility (soil permeability/fluid viscosity). k = 1.5
# Consolidation coefficient. c = 2*k*B^2*G*(1-nu)*(1+nuu)^2/9/(1-nuu)/(nuu-nu) = 3.821656
# Normal stress on top. F = 1
#
# The solution for porepressure and displacements is given in
# AHD Cheng and E Detournay "A direct boundary element method for plane strain poroelasticity" International Journal of Numerical and Analytical Methods in Geomechanics 12 (1988) 551-572.
# The solution involves complicated infinite series, so I shall not write it here
[Mesh]
type = GeneratedMesh
dim = 3
nx = 10
ny = 1
nz = 1
xmin = 0
xmax = 1
ymin = 0
ymax = 0.1
zmin = 0
zmax = 1
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
PorousFlowDictator = dictator
block = 0
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'porepressure disp_x disp_y disp_z'
number_fluid_phases = 1
number_fluid_components = 1
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[disp_z]
[]
[porepressure]
[]
[]
[BCs]
[roller_xmin]
type = DirichletBC
variable = disp_x
value = 0
boundary = 'left'
[]
[roller_ymin]
type = DirichletBC
variable = disp_y
value = 0
boundary = 'bottom'
[]
[plane_strain]
type = DirichletBC
variable = disp_z
value = 0
boundary = 'back front'
[]
[xmax_drained]
type = DirichletBC
variable = porepressure
value = 0
boundary = right
[]
[top_velocity]
type = FunctionDirichletBC
variable = disp_y
function = top_velocity
boundary = top
[]
[]
[Functions]
[top_velocity]
type = PiecewiseLinear
x = '0 0.002 0.006 0.014 0.03 0.046 0.062 0.078 0.094 0.11 0.126 0.142 0.158 0.174 0.19 0.206 0.222 0.238 0.254 0.27 0.286 0.302 0.318 0.334 0.35 0.366 0.382 0.398 0.414 0.43 0.446 0.462 0.478 0.494 0.51 0.526 0.542 0.558 0.574 0.59 0.606 0.622 0.638 0.654 0.67 0.686 0.702'
y = '-0.041824842 -0.042730269 -0.043412712 -0.04428867 -0.045509181 -0.04645965 -0.047268246 -0.047974749 -0.048597109 -0.0491467 -0.049632388 -0.050061697 -0.050441198 -0.050776675 -0.051073238 -0.0513354 -0.051567152 -0.051772022 -0.051953128 -0.052113227 -0.052254754 -0.052379865 -0.052490464 -0.052588233 -0.052674662 -0.052751065 -0.052818606 -0.052878312 -0.052931093 -0.052977751 -0.053018997 -0.053055459 -0.053087691 -0.053116185 -0.053141373 -0.05316364 -0.053183324 -0.053200724 -0.053216106 -0.053229704 -0.053241725 -0.053252351 -0.053261745 -0.053270049 -0.053277389 -0.053283879 -0.053289615'
[]
[]
[AuxVariables]
[stress_yy]
order = CONSTANT
family = MONOMIAL
[]
[tot_force]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
[]
[tot_force]
type = ParsedAux
args = 'stress_yy porepressure'
execute_on = timestep_end
variable = tot_force
function = '-stress_yy+0.6*porepressure'
[]
[]
[Kernels]
[grad_stress_x]
type = StressDivergenceTensors
variable = disp_x
component = 0
[]
[grad_stress_y]
type = StressDivergenceTensors
variable = disp_y
component = 1
[]
[grad_stress_z]
type = StressDivergenceTensors
variable = disp_z
component = 2
[]
[poro_x]
type = PorousFlowEffectiveStressCoupling
biot_coefficient = 0.6
variable = disp_x
component = 0
[]
[poro_y]
type = PorousFlowEffectiveStressCoupling
biot_coefficient = 0.6
variable = disp_y
component = 1
[]
[poro_z]
type = PorousFlowEffectiveStressCoupling
biot_coefficient = 0.6
component = 2
variable = disp_z
[]
[mass0]
type = PorousFlowFullySaturatedMassTimeDerivative
biot_coefficient = 0.6
multiply_by_density = false
coupling_type = HydroMechanical
variable = porepressure
[]
[flux]
type = PorousFlowFullySaturatedDarcyBase
multiply_by_density = false
variable = porepressure
gravity = '0 0 0'
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 8
density0 = 1
thermal_expansion = 0
viscosity = 1
[]
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[elasticity_tensor]
type = ComputeElasticityTensor
C_ijkl = '0.5 0.75'
# bulk modulus is lambda + 2*mu/3 = 0.5 + 2*0.75/3 = 1
fill_method = symmetric_isotropic
[]
[strain]
type = ComputeSmallStrain
[]
[stress]
type = ComputeLinearElasticStress
[]
[eff_fluid_pressure_qp]
type = PorousFlowEffectiveFluidPressure
[]
[vol_strain]
type = PorousFlowVolumetricStrain
consistent_with_displaced_mesh = false
[]
[ppss]
type = PorousFlow1PhaseFullySaturated
porepressure = porepressure
[]
[massfrac]
type = PorousFlowMassFraction
[]
[simple_fluid_qp]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[porosity]
type = PorousFlowPorosityConst # only the initial value of this is ever used
porosity = 0.1
[]
[biot_modulus]
type = PorousFlowConstantBiotModulus
biot_coefficient = 0.6
solid_bulk_compliance = 1
fluid_bulk_modulus = 8
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1.5 0 0 0 1.5 0 0 0 1.5'
[]
[]
[Postprocessors]
[p0]
type = PointValue
outputs = csv
point = '0.0 0 0'
variable = porepressure
[]
[p1]
type = PointValue
outputs = csv
point = '0.1 0 0'
variable = porepressure
[]
[p2]
type = PointValue
outputs = csv
point = '0.2 0 0'
variable = porepressure
[]
[p3]
type = PointValue
outputs = csv
point = '0.3 0 0'
variable = porepressure
[]
[p4]
type = PointValue
outputs = csv
point = '0.4 0 0'
variable = porepressure
[]
[p5]
type = PointValue
outputs = csv
point = '0.5 0 0'
variable = porepressure
[]
[p6]
type = PointValue
outputs = csv
point = '0.6 0 0'
variable = porepressure
[]
[p7]
type = PointValue
outputs = csv
point = '0.7 0 0'
variable = porepressure
[]
[p8]
type = PointValue
outputs = csv
point = '0.8 0 0'
variable = porepressure
[]
[p9]
type = PointValue
outputs = csv
point = '0.9 0 0'
variable = porepressure
[]
[p99]
type = PointValue
outputs = csv
point = '1 0 0'
variable = porepressure
[]
[xdisp]
type = PointValue
outputs = csv
point = '1 0.1 0'
variable = disp_x
[]
[ydisp]
type = PointValue
outputs = csv
point = '1 0.1 0'
variable = disp_y
[]
[total_downwards_force]
type = ElementAverageValue
outputs = csv
variable = tot_force
[]
[dt]
type = FunctionValuePostprocessor
outputs = console
function = if(0.15*t<0.01,0.15*t,0.01)
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'gmres asm lu 1E-14 1E-10 10000'
[]
[]
[Executioner]
type = Transient
solve_type = Newton
start_time = 0
end_time = 0.7
[TimeStepper]
type = PostprocessorDT
postprocessor = dt
dt = 0.001
[]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = mandel_fully_saturated_volume
[csv]
interval = 3
type = CSV
[]
[]
(test/tests/geomsearch/2d_moving_penetration/pl_test1tt.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
file = pl_test1.e
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
tangential_tolerance = 0.1
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
tangential_tolerance = 0.1
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate10]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate13]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate14]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate15]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate16]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 0.7 -0.7 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-9
l_max_its = 10
start_time = 0.0
dt = 0.05
end_time = 1.0
[]
[Outputs]
file_base = pl_test1tt_out
exodus = 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
[]
(modules/tensor_mechanics/test/tests/ad_anisotropic_plasticity/anis_plasticity_test.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[AuxVariables]
[hydrostatic_stress]
order = CONSTANT
family = MONOMIAL
[]
[plasticity_strain_xx]
order = CONSTANT
family = MONOMIAL
[]
[plasticity_strain_xy]
order = CONSTANT
family = MONOMIAL
[]
[plasticity_strain_yy]
order = CONSTANT
family = MONOMIAL
[]
[]
[Variables]
[disp_x]
scaling = 1e-10
[]
[disp_y]
scaling = 1e-10
[]
[disp_z]
scaling = 1e-10
[]
[]
[AuxKernels]
[hydrostatic_stress]
type = ADRankTwoScalarAux
variable = hydrostatic_stress
rank_two_tensor = stress
scalar_type = Hydrostatic
[]
[plasticity_strain_xx]
type = ADRankTwoAux
rank_two_tensor = trial_plasticity_plastic_strain
variable = plasticity_strain_xx
index_i = 0
index_j = 0
[]
[plasticity_strain_xy]
type = ADRankTwoAux
rank_two_tensor = trial_plasticity_plastic_strain
variable = plasticity_strain_xy
index_i = 0
index_j = 1
[]
[plasticity_strain_yy]
type = ADRankTwoAux
rank_two_tensor = trial_plasticity_plastic_strain
variable = plasticity_strain_yy
index_i = 1
index_j = 1
[]
[]
[Functions]
[pull]
type = PiecewiseLinear
x = '0 1e3 1e8'
y = '0 1e2 1e2'
[]
[]
[Modules/TensorMechanics/Master]
[all]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'elastic_strain_xx elastic_strain_yy elastic_strain_xy stress_xx stress_xy stress_yy'
use_automatic_differentiation = true
[]
[]
[Materials]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 206800
poissons_ratio = 0.0
[]
[elastic_strain]
type = ADComputeMultipleInelasticStress
inelastic_models = "trial_plasticity"
max_iterations = 500
absolute_tolerance = 1e-05
[]
[trial_plasticity]
type = ADHillPlasticityStressUpdate
# internal_solve_output_on = always
# F G H L M N
hardening_constant = 5000
yield_stress = 20000000000000
hill_constants = "1.0 4.0 5.0 0.5 0.5 0.5"
base_name = trial_plasticity
[]
[]
[BCs]
[no_disp_x]
type = ADDirichletBC
variable = disp_x
boundary = bottom
value = 0.0
[]
[no_disp_y]
type = ADDirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[]
[no_disp_z]
type = ADDirichletBC
variable = disp_z
boundary = bottom
value = 0.0
[]
[Pressure]
[Side1]
boundary = top
function = pull
[]
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options_iname = '-ksp_gmres_restart -pc_type -sub_pc_type'
petsc_options_value = '101 asm lu'
line_search = 'none'
nl_rel_tol = 1e-07
nl_abs_tol = 1.0e-15
l_max_its = 90
num_steps = 40
dt = 5.0e1
start_time = 0
automatic_scaling = true
[]
[Postprocessors]
[max_disp_x]
type = ElementExtremeValue
variable = disp_x
[]
[max_disp_y]
type = ElementExtremeValue
variable = disp_y
[]
[max_hydro]
type = ElementAverageValue
variable = hydrostatic_stress
[]
[dt]
type = TimestepSize
[]
[num_lin]
type = NumLinearIterations
outputs = console
[]
[num_nonlin]
type = NumNonlinearIterations
outputs = console
[]
[]
[Outputs]
csv = true
exodus = true
perf_graph = true
[]
(modules/richards/test/tests/broadbridge_white/bw_lumped_02.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 200
ny = 1
xmin = -10
xmax = 10
ymin = 0
ymax = 0.05
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = DensityConstBulk
relperm_UO = RelPermBW
SUPG_UO = SUPGstandard
sat_UO = Saturation
seff_UO = SeffBW
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1E-1 5E-1 5E-1'
x = '0 1 10'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 10
bulk_mod = 2E9
[../]
[./SeffBW]
type = RichardsSeff1BWsmall
Sn = 0.0
Ss = 1.0
C = 1.5
las = 2
[../]
[./RelPermBW]
type = RichardsRelPermBW
Sn = 0.0
Ss = 1.0
Kn = 0
Ks = 1
C = 1.5
[../]
[./Saturation]
type = RichardsSat
s_res = 0.0
sum_s_res = 0.0
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 1.0E2
[../]
[]
[Variables]
active = 'pressure'
[./pressure]
order = FIRST
family = LAGRANGE
initial_condition = -9E2
[../]
[]
[Kernels]
active = 'richardsf richardst'
[./richardst]
type = RichardsLumpedMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = SeffBW
pressure_vars = pressure
[../]
[]
[BCs]
active = 'recharge'
[./recharge]
type = RichardsPiecewiseLinearSink
variable = pressure
boundary = 'right'
pressures = '-1E10 1E10'
bare_fluxes = '-1.25 -1.25' # corresponds to Rstar being 0.5 because i have to multiply by density*porosity
use_mobility = false
use_relperm = false
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.25
mat_permeability = '1 0 0 0 1 0 0 0 1'
viscosity = 4
gravity = '-0.1 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
active = 'andy'
[./andy]
type = SMP
full = true
petsc_options = ''
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-10 1E-10 10000'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
petsc_options = '-snes_converged_reason'
end_time = 2
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = bw_lumped_02
interval = 10000
execute_on = 'timestep_end final'
exodus = true
[]
(modules/tensor_mechanics/test/tests/j_integral/j_integral_2d_points.i)
#This tests the J-Integral evaluation capability.
#This is a 2d plane strain model
#The analytic solution for J1 is 2.434. This model
#converges to that solution with a refined mesh.
#Reference: National Agency for Finite Element Methods and Standards (U.K.):
#Test 1.1 from NAFEMS publication "Test Cases in Linear Elastic Fracture
#Mechanics" R0020.
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[Mesh]
file = crack2d.e
[]
[AuxVariables]
[./SED]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./rampConstant]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = -1e2
[../]
[]
[DomainIntegral]
integrals = JIntegral
crack_front_points = '0 -10 0'
crack_direction_method = CrackDirectionVector
crack_direction_vector = '1 0 0'
2d = true
axis_2d = 2
radius_inner = '4.0 4.5 5.0 5.5 6.0'
radius_outer = '4.5 5.0 5.5 6.0 6.5'
output_q = false
incremental = true
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
planar_formulation = PLANE_STRAIN
[../]
[]
[AuxKernels]
[./SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[../]
[]
[BCs]
[./crack_y]
type = DirichletBC
variable = disp_y
boundary = 100
value = 0.0
[../]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 700
value = 0.0
[../]
[./Pressure]
[./Side1]
boundary = 400
function = rampConstant
[../]
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_rel_tol = 1e-12
nl_abs_tol = 1e-5
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Outputs]
file_base = j_integral_2d_points_out
exodus = true
csv = true
[]
(modules/combined/test/tests/internal_volume/hex20.i)
#
# Internal Volume Test
#
# This test is designed to compute the internal volume of a space considering
# an embedded volume inside.
#
# The mesh is composed of one block (1) with an interior cavity of volume 8.
# Block 2 sits in the cavity and has a volume of 1. Thus, the total volume
# is 7.
#
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
file = meshes/hex20.e
[]
[Functions]
[./step]
type = PiecewiseLinear
x = '0. 1. 2. 3.'
y = '0. 0. 1e-2 0.'
scale_factor = 0.5
[../]
[]
[Variables]
[./disp_x]
order = SECOND
family = LAGRANGE
[../]
[./disp_y]
order = SECOND
family = LAGRANGE
[../]
[./disp_z]
order = SECOND
family = LAGRANGE
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
incremental = true
strain = FINITE
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 100
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = 100
value = 0.0
[../]
[./prescribed_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 100
function = step
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = '1 2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = PJFNK
start_time = 0.0
dt = 1.0
end_time = 3.0
[./Quadrature]
order = THIRD
[../]
[]
[Postprocessors]
[./internalVolume]
type = InternalVolume
boundary = 100
execute_on = 'initial timestep_end'
[../]
[./dispZ]
type = ElementAverageValue
block = '1 2'
variable = disp_z
[../]
[]
[Outputs]
exodus = true
csv = true
[]
(modules/tensor_mechanics/test/tests/ad_anisotropic_plasticity/anis_elasticity_test.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[AuxVariables]
[hydrostatic_stress]
order = CONSTANT
family = MONOMIAL
[]
[]
[Variables]
[disp_x]
scaling = 1e-10
[]
[disp_y]
scaling = 1e-10
[]
[disp_z]
scaling = 1e-10
[]
[]
[AuxKernels]
[hydrostatic_stress]
type = ADRankTwoScalarAux
variable = hydrostatic_stress
rank_two_tensor = stress
scalar_type = Hydrostatic
[]
[]
[Functions]
[pull]
type = PiecewiseLinear
x = '0 1e3 1e8'
y = '0 1e2 1e2'
[]
[]
[Modules/TensorMechanics/Master]
[all]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'elastic_strain_xx elastic_strain_yy elastic_strain_xy stress_xx stress_xy stress_yy'
use_automatic_differentiation = true
[]
[]
[Materials]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 206800
poissons_ratio = 0.0
[]
[stress_]
type = ADComputeFiniteStrainElasticStress
[]
[]
[BCs]
[no_disp_x]
type = ADDirichletBC
variable = disp_x
boundary = bottom
value = 0.0
[]
[no_disp_y]
type = ADDirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[]
[no_disp_z]
type = ADDirichletBC
variable = disp_z
boundary = bottom
value = 0.0
[]
[Pressure]
[Side1]
boundary = top
function = pull
[]
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options_iname = '-ksp_gmres_restart -pc_type -sub_pc_type'
petsc_options_value = '101 asm lu'
line_search = 'none'
nl_rel_tol = 1e-07
nl_abs_tol = 1.0e-15
l_max_its = 90
num_steps = 40
dt = 5.0e1
start_time = 0
automatic_scaling = true
[]
[Postprocessors]
[max_disp_x]
type = ElementExtremeValue
variable = disp_x
[]
[max_disp_y]
type = ElementExtremeValue
variable = disp_y
[]
[max_hydro]
type = ElementAverageValue
variable = hydrostatic_stress
[]
[dt]
type = TimestepSize
[]
[num_lin]
type = NumLinearIterations
outputs = console
[]
[num_nonlin]
type = NumNonlinearIterations
outputs = console
[]
[]
[Outputs]
csv = true
exodus = true
perf_graph = true
[]
(modules/porous_flow/test/tests/infiltration_and_drainage/rd03.i)
[Mesh]
file = gold/rd02.e
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Functions]
[dts]
type = PiecewiseLinear
y = '2E4 1E6'
x = '0 1E6'
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = pressure
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureVG
m = 0.336
alpha = 1.43e-4
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 2e7
viscosity = 1.01e-3
density0 = 1000
thermal_expansion = 0
[]
[]
[]
[Materials]
[massfrac]
type = PorousFlowMassFraction
[]
[temperature]
type = PorousFlowTemperature
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pressure
capillary_pressure = pc
[]
[relperm]
type = PorousFlowRelativePermeabilityVG
m = 0.336
seff_turnover = 0.99
phase = 0
[]
[porosity]
type = PorousFlowPorosityConst
porosity = 0.33
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '0.295E-12 0 0 0 0.295E-12 0 0 0 0.295E-12'
[]
[]
[Variables]
[pressure]
initial_from_file_timestep = LATEST
initial_from_file_var = pressure
[]
[]
[Kernels]
[mass0]
type = PorousFlowMassTimeDerivative
fluid_component = 0
variable = pressure
[]
[flux0]
type = PorousFlowAdvectiveFlux
fluid_component = 0
variable = pressure
gravity = '-10 0 0'
[]
[]
[AuxVariables]
[SWater]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[SWater]
type = MaterialStdVectorAux
property = PorousFlow_saturation_qp
index = 0
variable = SWater
[]
[]
[BCs]
[base]
type = DirichletBC
boundary = left
value = 0.0
variable = pressure
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
petsc_options = '-snes_converged_reason -ksp_diagonal_scale -ksp_diagonal_scale_fix -ksp_gmres_modifiedgramschmidt -snes_linesearch_monitor'
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -sub_pc_factor_shift_type -pc_asm_overlap -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'gmres asm lu NONZERO 2 1E-10 1E-10 10'
[]
[]
[VectorPostprocessors]
[swater]
type = LineValueSampler
variable = SWater
start_point = '0 0 0'
end_point = '6 0 0'
sort_by = x
num_points = 121
execute_on = timestep_end
[]
[]
[Executioner]
type = Transient
solve_type = Newton
petsc_options = '-snes_converged_reason'
end_time = 8.2944E6
[TimeStepper]
type = FunctionDT
function = dts
[]
[]
[Outputs]
file_base = rd03
[exodus]
type = Exodus
execute_on = 'initial final'
[]
[along_line]
type = CSV
execute_on = final
[]
[]
(modules/tensor_mechanics/test/tests/dynamics/acceleration_bc/AccelerationBC_test.i)
# Test for Acceleration boundary condition
# This test contains one brick element which is fixed in the y and z direction.
# Base acceleration is applied in the x direction to all nodes on the bottom surface (y=0).
# The PresetAcceleration converts the given acceleration to a displacement
# using Newmark time integration. This displacement is then prescribed on the boundary.
#
# Result: The acceleration at the bottom node should be same as the input acceleration
# which is a triangular function with peak at t = 0.2 in this case. Width of the triangular function
# is 0.2 s.
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = 0.0
xmax = 0.1
ymin = 0.0
ymax = 1.0
zmin = 0.0
zmax = 0.1
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./vel_x]
[../]
[./accel_x]
[../]
[./vel_y]
[../]
[./accel_y]
[../]
[./vel_z]
[../]
[./accel_z]
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./TensorMechanics]
[../]
[./inertia_x]
type = InertialForce
variable = disp_x
velocity = vel_x
acceleration = accel_x
beta = 0.25
gamma = 0.5
[../]
[./inertia_y]
type = InertialForce
variable = disp_y
velocity = vel_y
acceleration = accel_y
beta = 0.25
gamma = 0.5
[../]
[./inertia_z]
type = InertialForce
variable = disp_z
velocity = vel_z
acceleration = accel_z
beta = 0.25
gamma = 0.5
[../]
[]
[AuxKernels]
[./accel_x]
type = NewmarkAccelAux
variable = accel_x
displacement = disp_x
velocity = vel_x
beta = 0.25
execute_on = timestep_end
[../]
[./vel_x]
type = NewmarkVelAux
variable = vel_x
acceleration = accel_x
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_y]
type = NewmarkAccelAux
variable = accel_y
displacement = disp_y
velocity = vel_y
beta = 0.25
execute_on = timestep_end
[../]
[./vel_y]
type = NewmarkVelAux
variable = vel_y
acceleration = accel_y
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_z]
type = NewmarkAccelAux
variable = accel_z
displacement = disp_z
velocity = vel_z
beta = 0.25
execute_on = timestep_end
[../]
[./vel_z]
type = NewmarkVelAux
variable = vel_z
acceleration = accel_z
gamma = 0.5
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 0
index_j = 1
[../]
[./strain_yy]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_yy
index_i = 0
index_j = 1
[../]
[]
[Functions]
[./acceleration_bottom]
type = PiecewiseLinear
data_file = acceleration.csv
format = columns
[../]
[]
[BCs]
[./top_y]
type = DirichletBC
variable = disp_y
boundary = top
value=0.0
[../]
[./top_z]
type = DirichletBC
variable = disp_z
boundary = top
value=0.0
[../]
[./bottom_y]
type = DirichletBC
variable = disp_y
boundary = bottom
value=0.0
[../]
[./bottom_z]
type = DirichletBC
variable = disp_z
boundary = bottom
value=0.0
[../]
[./preset_accelertion]
type = PresetAcceleration
boundary = bottom
function = acceleration_bottom
variable = disp_x
beta = 0.25
acceleration = accel_x
velocity = vel_x
[../]
[]
[Materials]
[./Elasticity_tensor]
type = ComputeElasticityTensor
fill_method = symmetric_isotropic
C_ijkl = '210e9 0'
[../]
[./strain]
type = ComputeSmallStrain
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[./density]
type = GenericConstantMaterial
prop_names = 'density'
prop_values = '7750'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart'
petsc_options_value = 'hypre boomeramg 101'
start_time = 0
end_time = 2.0
dt = 0.01
dtmin = 0.01
nl_abs_tol = 1e-8
nl_rel_tol = 1e-8
l_tol = 1e-8
timestep_tolerance = 1e-8
[]
[Postprocessors]
[./_dt]
type = TimestepSize
[../]
[./disp]
type = NodalVariableValue
variable = disp_x
nodeid = 1
[../]
[./vel]
type = NodalVariableValue
variable = vel_x
nodeid = 1
[../]
[./accel]
type = NodalVariableValue
variable = accel_x
nodeid = 1
[../]
[]
[Outputs]
csv = true
exodus = true
perf_graph = true
[]
(modules/richards/test/tests/rogers_stallybrass_clements/rsc_fu_01.i)
# RSC test with high-res time and spatial resolution
[Mesh]
type = GeneratedMesh
dim = 2
nx = 600
ny = 1
xmin = 0
xmax = 10 # x is the depth variable, called zeta in RSC
ymin = 0
ymax = 0.05
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = 'DensityWater DensityOil'
relperm_UO = 'RelPerm RelPerm'
SUPG_UO = 'SUPGstandard SUPGstandard'
sat_UO = 'Saturation Saturation'
seff_UO = 'SeffWater SeffOil'
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '3E-3 3E-2 0.05'
x = '0 1 5'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = 'pwater poil'
[../]
[./DensityWater]
type = RichardsDensityConstBulk
dens0 = 10
bulk_mod = 2E9
[../]
[./DensityOil]
type = RichardsDensityConstBulk
dens0 = 20
bulk_mod = 2E9
[../]
[./SeffWater]
type = RichardsSeff2waterRSC
oil_viscosity = 2E-3
scale_ratio = 2E3
shift = 10
[../]
[./SeffOil]
type = RichardsSeff2gasRSC
oil_viscosity = 2E-3
scale_ratio = 2E3
shift = 10
[../]
[./RelPerm]
type = RichardsRelPermMonomial
simm = 0
n = 1
[../]
[./Saturation]
type = RichardsSat
s_res = 0.0
sum_s_res = 0.0
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 1.0E-2
[../]
[]
[Variables]
[./pwater]
[../]
[./poil]
[../]
[]
[ICs]
[./water_init]
type = ConstantIC
variable = pwater
value = 0
[../]
[./oil_init]
type = ConstantIC
variable = poil
value = 15
[../]
[]
[Kernels]
[./richardstwater]
type = RichardsMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFullyUpwindFlux
variable = pwater
[../]
[./richardstoil]
type = RichardsMassChange
variable = poil
[../]
[./richardsfoil]
type = RichardsFullyUpwindFlux
variable = poil
[../]
[]
[AuxVariables]
[./SWater]
[../]
[./SOil]
[../]
[]
[AuxKernels]
[./Seff1VGwater_AuxK]
type = RichardsSeffAux
variable = SWater
seff_UO = SeffWater
pressure_vars = 'pwater poil'
[../]
[./Seff1VGoil_AuxK]
type = RichardsSeffAux
variable = SOil
seff_UO = SeffOil
pressure_vars = 'pwater poil'
[../]
[]
[BCs]
# we are pumping water into a system that has virtually incompressible fluids, hence the pressures rise enormously. this adversely affects convergence because of almost-overflows and precision-loss problems. The fixed things help keep pressures low and so prevent these awful behaviours. the movement of the saturation front is the same regardless of the fixed things.
active = 'recharge fixedoil fixedwater'
[./recharge]
type = RichardsPiecewiseLinearSink
variable = pwater
boundary = 'left'
pressures = '-1E10 1E10'
bare_fluxes = '-1 -1'
use_mobility = false
use_relperm = false
[../]
[./fixedwater]
type = DirichletBC
variable = pwater
boundary = 'right'
value = 0
[../]
[./fixedoil]
type = DirichletBC
variable = poil
boundary = 'right'
value = 15
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.25
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
viscosity = '1E-3 2E-3'
gravity = '0E-0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
active = 'andy'
[./andy]
type = SMP
full = true
petsc_options = ''
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-10 1E-10 10000'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
petsc_options = '-snes_converged_reason'
end_time = 5
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = rsc_fu_01
interval = 100000
execute_on = 'initial timestep_end final'
exodus = true
[]
(modules/tensor_mechanics/test/tests/strain_energy_density/rate_model_small.i)
# Single element test to check the strain energy density calculation
[GlobalParams]
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
xmin = 0
xmax = 1
ymin = 0
ymax = 2
[]
[AuxVariables]
[./SERD]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./rampConstantUp]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = -100
[../]
[./ramp_disp_y]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 6.8e-6 1.36e-5'
[../]
[]
[Modules/TensorMechanics/Master]
[./master]
strain = SMALL
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress elastic_strain_xx elastic_strain_yy elastic_strain_zz strain_xx strain_yy strain_zz'
planar_formulation = PLANE_STRAIN
[../]
[]
[AuxKernels]
[./SERD]
type = MaterialRealAux
variable = SERD
property = strain_energy_rate_density
execute_on = timestep_end
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
variable = disp_x
preset = false
boundary = 'left'
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_y
preset = false
boundary = 'bottom'
value = 0.0
[../]
[./top_disp]
type = FunctionDirichletBC
variable = disp_y
preset = false
boundary = 'top'
function = ramp_disp_y
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 206800
poissons_ratio = 0.0
[../]
[./radial_return_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'powerlawcrp'
[../]
[./powerlawcrp]
type = PowerLawCreepStressUpdate
coefficient = 3.125e-21 # 7.04e-17 #
n_exponent = 4.0
m_exponent = 0.0
activation_energy = 0.0
# max_inelastic_increment = 0.01
[../]
[./strain_energy_rate_density]
type = StrainEnergyRateDensity
inelastic_models = 'powerlawcrp'
[../]
[]
[Executioner]
type = Transient
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 4'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_abs_tol = 3e-7
nl_rel_tol = 1e-12
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 2
num_steps = 2
[]
[Postprocessors]
[./etxx]
type = ElementalVariableValue
variable = strain_xx
elementid = 0
[../]
[./etyy]
type = ElementalVariableValue
variable = strain_yy
elementid = 0
[../]
[./etzz]
type = ElementalVariableValue
variable = strain_zz
elementid = 0
[../]
[./sigxx]
type = ElementAverageValue
variable = stress_xx
[../]
[./sigyy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigzz]
type = ElementAverageValue
variable = stress_zz
[../]
[./SERD]
type = ElementAverageValue
variable = SERD
[../]
[]
[Outputs]
exodus = true
csv = true
[]
(modules/combined/test/tests/thermo_mech/youngs_modulus_function_temp.i)
# ---------------------------------------------------------------------------
# This test is designed to verify the variable elasticity tensor functionality in the
# ComputeFiniteStrainElasticStress class with the elasticity_tensor_has_changed flag
# by varying the young's modulus with temperature. A constant strain is applied
# to the mesh in this case, and the stress varies with the changing elastic constants.
#
# Geometry: A single element cube in symmetry boundary conditions and pulled
# at a constant displacement to create a constant strain in the x-direction.
#
# Temperature: The temperature varies from 400K to 700K in this simulation by
# 100K each time step. The temperature is held constant in the last
# timestep to ensure that the elasticity tensor components are constant
# under constant temperature.
#
# Results: Because Poisson's ratio is set to zero, only the stress along the x
# axis is non-zero. The stress changes with temperature.
#
# Temperature(K) strain_{xx}(m/m) Young's Modulus(Pa) stress_{xx}(Pa)
# 400 0.001 10.0e6 1.0e4
# 500 0.001 10.0e6 1.0e4
# 600 0.001 9.94e6 9.94e3
# 700 0.001 9.93e6 9.93e3
#
# The tensor mechanics results align exactly with the analytical results above
# when this test is run with ComputeIncrementalSmallStrain. When the test is
# run with ComputeFiniteStrain, a 0.05% discrepancy between the analytical
# strains and the simulation strain results is observed, and this discrepancy
# is carried over into the calculation of the elastic stress.
#-------------------------------------------------------------------------
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[./temp]
initial_condition = 400
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./temperature_function]
type = PiecewiseLinear
x = '1 4'
y = '400 700'
[../]
[]
[Kernels]
[./heat]
type = Diffusion
variable = temp
[../]
[./TensorMechanics]
use_displaced_mesh = true
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
[../]
[./elastic_strain_xx]
type = RankTwoAux
rank_two_tensor = elastic_strain
variable = elastic_strain_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[]
[BCs]
[./u_left_fix]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./u_bottom_fix]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./u_back_fix]
type = DirichletBC
variable = disp_z
boundary = back
value = 0.0
[../]
[./u_pull_right]
type = DirichletBC
variable = disp_x
boundary = right
value = 0.001
[../]
[./temp_bc_1]
type = FunctionDirichletBC
variable = temp
preset = false
boundary = '1 2 3 4'
function = temperature_function
[../]
[]
[Materials]
[./youngs_modulus]
type = PiecewiseLinearInterpolationMaterial
xy_data = '0 10e+6
599.9999 10e+6
600 9.94e+6
99900 10e3'
property = youngs_modulus
variable = temp
[../]
[./elasticity_tensor]
type = ComputeVariableIsotropicElasticityTensor
args = temp
youngs_modulus = youngs_modulus
poissons_ratio = 0.0
[../]
[./strain]
type = ComputeIncrementalSmallStrain
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
end_time = 5
[]
[Postprocessors]
[./elastic_strain_xx]
type = ElementAverageValue
variable = elastic_strain_xx
[../]
[./elastic_stress_xx]
type = ElementAverageValue
variable = stress_xx
[../]
[./temp]
type = AverageNodalVariableValue
variable = temp
[../]
[]
[Outputs]
exodus = true
[]
(modules/combined/test/tests/internal_volume/rz.i)
#
# Internal Volume Test
#
# This test is designed to compute the internal volume of a space considering
# an embedded volume inside.
#
# The mesh is composed of one block (1) with an interior cavity of volume 8.
# Block 2 sits in the cavity and has a volume of 1. Thus, the total volume
# is 7.
#
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Problem]
coord_type = RZ
[]
[Mesh]
file = meshes/rz.e
[]
[Functions]
[./pressure]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = 1e4
[../]
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
volumetric_locking_correction = true
incremental = true
strain = FINITE
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = '1 2'
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = '1 2'
value = 0.0
[../]
[./Pressure]
[./fred]
boundary = 3
function = pressure
[../]
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = '1 2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
start_time = 0.0
dt = 1.0
end_time = 1.0
[]
[Postprocessors]
[./internalVolume]
type = InternalVolume
boundary = 2
execute_on = 'initial timestep_end'
[../]
[]
[Outputs]
exodus = true
csv = true
[]
(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
[]
(modules/tensor_mechanics/test/tests/scalar_material_damage/combined_scalar_damage.i)
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
elem_type = HEX8
[]
[AuxVariables]
[damage_index]
order = CONSTANT
family = MONOMIAL
[]
[damage_index_a]
order = CONSTANT
family = MONOMIAL
[]
[damage_index_b]
order = CONSTANT
family = MONOMIAL
[]
[]
[Modules/TensorMechanics/Master]
[all]
strain = SMALL
incremental = true
add_variables = true
generate_output = 'stress_xx strain_xx'
[]
[]
[AuxKernels]
[damage_index]
type = MaterialRealAux
variable = damage_index
property = damage_index
execute_on = timestep_end
[]
[damage_index_a]
type = MaterialRealAux
variable = damage_index_a
property = damage_index_a
execute_on = timestep_end
[]
[damage_index_b]
type = MaterialRealAux
variable = damage_index_b
property = damage_index_b
execute_on = timestep_end
[]
[]
[BCs]
[symmy]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0
[]
[symmx]
type = DirichletBC
variable = disp_x
boundary = left
value = 0
[]
[symmz]
type = DirichletBC
variable = disp_z
boundary = back
value = 0
[]
[axial_load]
type = DirichletBC
variable = disp_x
boundary = right
value = 0.01
[]
[]
[Functions]
[damage_evolution_a]
type = PiecewiseLinear
xy_data = '0.0 0.0
0.1 0.0
2.1 2.0'
[]
[damage_evolution_b]
type = PiecewiseLinear
xy_data = '0.0 0.2
0.1 0.2
2.1 0.7'
[]
[]
[Materials]
[damage_index_a]
type = GenericFunctionMaterial
prop_names = damage_index_prop_a
prop_values = damage_evolution_a
[]
[damage_index_b]
type = GenericFunctionMaterial
prop_names = damage_index_prop_b
prop_values = damage_evolution_b
[]
[damage_a]
type = ScalarMaterialDamage
damage_index = damage_index_prop_a
damage_index_name = damage_index_a
[]
[damage_b]
type = ScalarMaterialDamage
damage_index = damage_index_prop_b
damage_index_name = damage_index_b
[]
[damage]
type = CombinedScalarDamage
damage_models = 'damage_a damage_b'
[]
[stress]
type = ComputeDamageStress
damage_model = damage
[]
[elasticity]
type = ComputeIsotropicElasticityTensor
poissons_ratio = 0.2
youngs_modulus = 10e9
[]
[]
[Postprocessors]
[stress_xx]
type = ElementAverageValue
variable = stress_xx
[]
[strain_xx]
type = ElementAverageValue
variable = strain_xx
[]
[damage_index]
type = ElementAverageValue
variable = damage_index
[]
[damage_index_a]
type = ElementAverageValue
variable = damage_index_a
[]
[damage_index_b]
type = ElementAverageValue
variable = damage_index_b
[]
[]
[Executioner]
type = Transient
l_max_its = 50
l_tol = 1e-8
nl_max_its = 20
nl_rel_tol = 1e-12
nl_abs_tol = 1e-8
dt = 0.1
dtmin = 0.1
end_time = 1.1
[]
[Outputs]
csv=true
[]
(test/tests/geomsearch/3d_moving_penetration_smoothing/pl_test4ns.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
file = pl_test4.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./normal_z]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./closest_point_z]
[../]
# [./element_id]
# [../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[./diff_z]
type = Diffusion
variable = disp_z
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
normal_smoothing_distance = 0.2
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
normal_smoothing_distance = 0.2
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = normal_z
boundary = 11
paired_boundary = 12
quantity = normal_z
[../]
[./penetrate10]
type = PenetrationAux
variable = normal_z
boundary = 12
paired_boundary = 11
quantity = normal_z
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate13]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate14]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate15]
type = PenetrationAux
variable = closest_point_z
boundary = 11
paired_boundary = 12
quantity = closest_point_z
[../]
[./penetrate16]
type = PenetrationAux
variable = closest_point_z
boundary = 12
paired_boundary = 11
quantity = closest_point_z
[../]
# [./penetrate17]
# type = PenetrationAux
# variable = element_id
# boundary = 11
# paired_boundary = 12
# quantity = element_id
# [../]
#
# [./penetrate18]
# type = PenetrationAux
# variable = element_id
# boundary = 12
# paired_boundary = 11
# quantity = element_id
# [../]
[./penetrate19]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate20]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
preset = false
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
preset = false
boundary = 1
value = 0
[../]
[./b1z]
type = DirichletBC
variable = disp_z
preset = false
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
preset = false
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
preset = false
boundary = 2
function = disp_y
[../]
[./b2z]
type = DirichletBC
variable = disp_z
preset = false
boundary = 2
value = 0
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-9
l_max_its = 10
start_time = 0.0
dt = 0.02
end_time = 1.0
[]
[Outputs]
file_base = pl_test4ns_out
exodus = true
[]
(modules/richards/test/tests/recharge_discharge/rd03.i)
[Mesh]
file = gold/rd02.e
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '2E4 1E6'
x = '0 1E6'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1E3
bulk_mod = 2E7
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.336
al = 1.43E-4
[../]
[./RelPermPower]
type = RichardsRelPermVG1
scut = 0.99
simm = 0.0
m = 0.336
[../]
[./Saturation]
type = RichardsSat
s_res = 0.0
sum_s_res = 0.0
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 1.0E+0
[../]
[]
[Variables]
active = 'pressure'
[./pressure]
order = FIRST
family = LAGRANGE
initial_from_file_timestep = 2
initial_from_file_var = pressure
[../]
[]
[Kernels]
active = 'richardsf richardst'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = SeffVG
pressure_vars = pressure
[../]
[]
[BCs]
active = 'fix_bot'
[./fix_bot]
type = DirichletBC
variable = pressure
boundary = 'left'
value = 0.0
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.33
mat_permeability = '0.295E-12 0 0 0 0.295E-12 0 0 0 0.295E-12'
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGstandard
sat_UO = Saturation
seff_UO = SeffVG
viscosity = 1.01E-3
gravity = '-10 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
active = 'andy'
[./andy]
type = SMP
full = true
petsc_options = ''
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-13 1E-15 10000'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
petsc_options = '-snes_converged_reason'
end_time = 8.2944E6
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = rd03
interval = 100000
execute_on = 'initial timestep_end final'
exodus = true
[]
(modules/porous_flow/test/tests/gravity/grav02c.i)
# Checking that gravity head is established in the transient situation when 0<=saturation<=1 (note the less-than-or-equal-to).
# 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
[]
[Functions]
[dts]
type = PiecewiseLinear
y = '1E-3 1E-2 1E-1'
x = '1E-3 1E-2 1E-1'
[]
[]
[Variables]
[ppwater]
initial_condition = -0.1
[]
[ppgas]
initial_condition = 0
[]
[]
[AuxVariables]
[massfrac_ph0_sp0]
initial_condition = 1
[]
[massfrac_ph1_sp0]
initial_condition = 0
[]
[]
[Kernels]
[mass0]
type = PorousFlowMassTimeDerivative
fluid_component = 0
variable = ppwater
[]
[flux0]
type = PorousFlowAdvectiveFlux
fluid_component = 0
variable = ppwater
gravity = '-1 0 0'
[]
[mass1]
type = PorousFlowMassTimeDerivative
fluid_component = 1
variable = ppgas
[]
[flux1]
type = PorousFlowAdvectiveFlux
fluid_component = 1
variable = ppgas
gravity = '-1 0 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
[]
[]
[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
[]
[porosity]
type = PorousFlowPorosityConst
porosity = 0.1
[]
[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'
[]
[mass_ph0]
type = PorousFlowFluidMass
fluid_component = 0
execute_on = 'initial timestep_end'
[]
[mass_ph1]
type = PorousFlowFluidMass
fluid_component = 1
execute_on = 'initial timestep_end'
[]
[]
[Preconditioning]
active = andy
[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-12 1E-10 10000'
[]
[check]
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-12 1E-10 10000 test'
[]
[]
[Executioner]
type = Transient
solve_type = Newton
[TimeStepper]
type = FunctionDT
function = dts
[]
end_time = 1.0
[]
[Outputs]
execute_on = 'initial timestep_end'
file_base = grav02c
[csv]
type = CSV
[]
exodus = true
[]
(modules/tensor_mechanics/test/tests/ad_viscoplasticity_stress_update/lps_single_split.i)
# This test provides an example of combining two LPS viscoplasticity model.
# The answer should be close, but not exactly the same, as lps_single.i
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
xmax = 0.002
ymax = 0.002
[]
[Modules/TensorMechanics/Master/All]
strain = FINITE
add_variables = true
generate_output = 'strain_xx strain_yy strain_xy hydrostatic_stress vonmises_stress'
use_automatic_differentiation = true
[]
[Functions]
[./pull]
type = PiecewiseLinear
x = '0 0.1'
y = '0 1e-5'
[../]
[./tot_effective_viscoplasticity]
type = ParsedFunction
vals = 'lps_1_eff_creep_strain lps_2_eff_creep_strain'
vars = 'lps_1_eff_creep_strain lps_2_eff_creep_strain'
value = 'lps_1_eff_creep_strain+lps_2_eff_creep_strain'
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1e10
poissons_ratio = 0.3
[../]
[./stress]
type = ADComputeMultipleInelasticStress
inelastic_models = 'one two'
outputs = all
[../]
[./porosity]
type = ADPorosityFromStrain
initial_porosity = 0.1
inelastic_strain = 'combined_inelastic_strain'
outputs = 'all'
[../]
[./one]
type = ADViscoplasticityStressUpdate
coefficient = 'coef'
power = 3
base_name = 'lps_first'
outputs = all
relative_tolerance = 1e-11
[../]
[./two]
type = ADViscoplasticityStressUpdate
coefficient = 'coef'
power = 3
base_name = 'lps_second'
outputs = all
relative_tolerance = 1e-11
[../]
[./coef]
type = ADParsedMaterial
f_name = coef
# Example of creep power law
function = '0.5e-18 * exp(-4e4 / 1.987 / 1200)'
[../]
[]
[BCs]
[./no_disp_x]
type = ADDirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./no_disp_y]
type = ADDirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./pull_disp_y]
type = ADFunctionDirichletBC
variable = disp_y
boundary = top
function = pull
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
dt = 0.01
end_time = 0.12
[]
[Postprocessors]
[./disp_x]
type = SideAverageValue
variable = disp_x
boundary = right
[../]
[./disp_y]
type = SideAverageValue
variable = disp_y
boundary = top
[../]
[./avg_hydro]
type = ElementAverageValue
variable = hydrostatic_stress
[../]
[./avg_vonmises]
type = ElementAverageValue
variable = vonmises_stress
[../]
[./dt]
type = TimestepSize
[../]
[./num_lin]
type = NumLinearIterations
outputs = console
[../]
[./num_nonlin]
type = NumNonlinearIterations
outputs = console
[../]
[./lps_1_eff_creep_strain]
type = ElementAverageValue
variable = lps_first_effective_viscoplasticity
outputs = none
[../]
[./lps_2_eff_creep_strain]
type = ElementAverageValue
variable = lps_second_effective_viscoplasticity
outputs = none
[../]
[./eff_creep_strain_tot]
type = FunctionValuePostprocessor
function = tot_effective_viscoplasticity
[../]
[./porosity]
type = ElementAverageValue
variable = porosity
[../]
[]
[Outputs]
csv = true
[]
(test/tests/geomsearch/3d_moving_penetration/pl_test3.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
file = pl_test3.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./normal_z]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./closest_point_z]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[./diff_z]
type = Diffusion
variable = disp_z
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = normal_z
boundary = 11
paired_boundary = 12
quantity = normal_z
[../]
[./penetrate10]
type = PenetrationAux
variable = normal_z
boundary = 12
paired_boundary = 11
quantity = normal_z
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate13]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate14]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate15]
type = PenetrationAux
variable = closest_point_z
boundary = 11
paired_boundary = 12
quantity = closest_point_z
[../]
[./penetrate16]
type = PenetrationAux
variable = closest_point_z
boundary = 12
paired_boundary = 11
quantity = closest_point_z
[../]
[./penetrate17]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate18]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate19]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate20]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
preset = false
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
preset = false
boundary = 1
value = 0
[../]
[./b1z]
type = DirichletBC
variable = disp_z
preset = false
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
preset = false
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
preset = false
boundary = 2
function = disp_y
[../]
[./b2z]
type = DirichletBC
variable = disp_z
preset = false
boundary = 2
value = 0
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-9
l_max_its = 10
start_time = 0.0
dt = 0.02
end_time = 1.0
[]
[Outputs]
file_base = pl_test3_out
exodus = true
[]
(modules/richards/test/tests/theis/th01.i)
# fully-saturated
# production
[Mesh]
type = FileMesh
file = th01_input.e
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '0.5 1 2 10'
x = '0 1 10 100'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1000
bulk_mod = 2E9
[../]
[./Seff1VG]
type = RichardsSeff1VG
m = 0.8
al = 1E-5
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0
sum_s_res = 0
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 1E-5
[../]
[./total_outflow_mass]
type = RichardsSumQuantity
[../]
[]
[Variables]
active = 'pressure'
[./pressure]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./p_ic]
type = FunctionIC
variable = pressure
function = initial_pressure
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[Kernels]
active = 'richardsf richardst'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[DiracKernels]
[./bh]
type = RichardsPolyLineSink
pressures = '-1E9 1E9'
fluxes = '200 200'
point_file = th01.points
SumQuantityUO = total_outflow_mass
variable = pressure
[../]
[]
[Postprocessors]
[./flow_report]
type = RichardsPlotQuantity
uo = total_outflow_mass
[../]
[./p50]
type = PointValue
variable = pressure
point = '50 0 0'
execute_on = timestep_end
[../]
[]
[Functions]
[./initial_pressure]
type = ParsedFunction
value = 1E5
[../]
[]
[Materials]
[./all]
type = RichardsMaterial
block = 1
viscosity = 1E-3
mat_porosity = 0.1
mat_permeability = '1E-10 0 0 0 1E-10 0 0 0 1E-10'
density_UO = DensityConstBulk
relperm_UO = RelPermPower
sat_UO = Saturation
seff_UO = Seff1VG
SUPG_UO = SUPGstandard
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = Seff1VG
pressure_vars = pressure
[../]
[]
[Preconditioning]
[./usual]
type = SMP
full = true
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -ksp_max_it'
petsc_options_value = 'bcgs bjacobi 1E-6 1E-10 10000 30'
[../]
[]
[Executioner]
type = Transient
end_time = 100
solve_type = NEWTON
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = th01
csv = true
[]
(modules/tensor_mechanics/test/tests/strain_energy_density/ad_rate_model_weak_plane.i)
# Single element test to check the strain energy density calculation
[GlobalParams]
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
out_of_plane_strain = strain_zz
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
xmin = 0
xmax = 1
ymin = 0
ymax = 2
[]
[AuxVariables]
[./SERD]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Variables]
[./strain_zz]
[]
[]
[Functions]
[./rampConstantUp]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = -100
[../]
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress strain_xx strain_yy'
planar_formulation = WEAK_PLANE_STRESS
use_automatic_differentiation = true
[../]
[]
[AuxKernels]
[./SERD]
type = ADMaterialRealAux
variable = SERD
property = strain_energy_rate_density
execute_on = timestep_end
[../]
[]
[BCs]
[./no_x]
type = ADDirichletBC
variable = disp_x
boundary = 'left'
value = 0.0
[../]
[./no_y]
type = ADDirichletBC
variable = disp_y
boundary = 'bottom'
value = 0.0
[../]
[./Pressure]
[./top]
boundary = 'top'
function = rampConstantUp
[../]
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 206800
poissons_ratio = 0.0
[../]
[./radial_return_stress]
type = ADComputeMultipleInelasticStress
inelastic_models = 'powerlawcrp'
[../]
[./powerlawcrp]
type = ADPowerLawCreepStressUpdate
coefficient = 3.125e-21 # 7.04e-17 #
n_exponent = 4.0
m_exponent = 0.0
activation_energy = 0.0
# max_inelastic_increment = 0.01
[../]
[./strain_energy_rate_density]
type = ADStrainEnergyRateDensity
inelastic_models = 'powerlawcrp'
[../]
[]
[Executioner]
type = Transient
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 4'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_abs_tol = 3e-7
nl_rel_tol = 1e-12
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Postprocessors]
[./SERD]
type = ElementAverageValue
variable = SERD
[../]
[]
[Outputs]
exodus = true
csv = true
[]
(modules/richards/test/tests/gravity_head_2/gh05.i)
# unsaturated = true
# gravity = false
# supg = false
# transient = true
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
xmin = 0
xmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1E-2 1E-1 1E0 1E1 1E3 1E4 1E5 1E6 1E7'
x = '0 1E-1 1E0 1E1 1E2 1E3 1E4 1E5 1E6'
[../]
[]
[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 = 0.2
max = 0.8
variable = pwater
[../]
[./gas_ic]
type = RandomIC
min = 1.2
max = 1.8
variable = pgas
[../]
[]
[Kernels]
active = 'richardsfwater richardstwater richardsfgas richardstgas'
[./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
[../]
[./mass_error_gas]
type = FunctionValuePostprocessor
function = fcn_mass_error_g
[../]
[./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 -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-10 1E-10 10000'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
end_time = 1E6
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = gh05
csv = true
[]
(modules/richards/test/tests/gravity_head_2/gh_fu_06.i)
# unsaturated = true
# gravity = true
# supg = false
# transient = true
[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'
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1E-2 1E-1 1E0 1E1 1E3 1E4 1E5 1E6 1E7'
x = '0 1E-1 1E0 1E1 1E2 1E3 1E4 1E5 1E6'
[../]
[]
[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 = ConstantIC
value = 1
variable = pwater
[../]
[./gas_ic]
type = ConstantIC
value = 2
variable = pgas
[../]
[]
[Kernels]
active = 'richardsfwater richardstwater richardsfgas richardstgas'
[./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
[../]
[./mass_error_gas]
type = FunctionValuePostprocessor
function = fcn_mass_error_g
[../]
[./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((-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 -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-13 1E-10 10000'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
end_time = 1E6
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = gh_fu_06
csv = true
[]
(modules/porous_flow/test/tests/functions/mpf1.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 15
ny = 15
xmin = 0
xmax = 10
ymin = 0
ymax = 10
[]
[Variables]
[u]
[]
[]
[Kernels]
[dummy]
type = TimeDerivative
variable = u
[]
[]
[Functions]
[dist]
type = PiecewiseLinear
x = '1 10' # time
y = '0 9' # distance
[]
[moving_planar_front]
type = MovingPlanarFront
start_posn = '1 1 0'
end_posn = '2 2 0' # it does not matter that dist exceeds this
active_length = 5
activation_time = 1
deactivation_time = 9
distance = dist
[]
[]
[AuxVariables]
[mpf]
[]
[]
[AuxKernels]
[mpf]
type = FunctionAux
variable = mpf
function = moving_planar_front
[]
[]
[Executioner]
type = Transient
dt = 0.5
end_time = 10
[]
[Outputs]
file_base = mpf1
exodus = true
[]
(modules/tensor_mechanics/test/tests/ad_viscoplasticity_stress_update/lps_single.i)
# This test provides an example of an individual LPS viscoplasticity model
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
xmax = 0.002
ymax = 0.002
[]
[Modules/TensorMechanics/Master/All]
strain = FINITE
add_variables = true
generate_output = 'strain_xx strain_yy strain_xy hydrostatic_stress vonmises_stress'
use_automatic_differentiation = true
[]
[Functions]
[./pull]
type = PiecewiseLinear
x = '0 0.1'
y = '0 1e-5'
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1e10
poissons_ratio = 0.3
[../]
[./stress]
type = ADComputeMultipleInelasticStress
inelastic_models = lps
outputs = all
[../]
[./porosity]
type = ADPorosityFromStrain
initial_porosity = 0.1
inelastic_strain = 'combined_inelastic_strain'
outputs = 'all'
[../]
[./lps]
type = ADViscoplasticityStressUpdate
coefficient = 'coef'
power = 3
outputs = all
relative_tolerance = 1e-11
[../]
[./coef]
type = ADParsedMaterial
f_name = coef
# Example of creep power law
function = '1e-18 * exp(-4e4 / 1.987 / 1200)'
[../]
[]
[BCs]
[./no_disp_x]
type = ADDirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./no_disp_y]
type = ADDirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./pull_disp_y]
type = ADFunctionDirichletBC
variable = disp_y
boundary = top
function = pull
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
dt = 0.01
end_time = 0.12
[]
[Postprocessors]
[./disp_x]
type = SideAverageValue
variable = disp_x
boundary = right
[../]
[./disp_y]
type = SideAverageValue
variable = disp_y
boundary = top
[../]
[./avg_hydro]
type = ElementAverageValue
variable = hydrostatic_stress
[../]
[./avg_vonmises]
type = ElementAverageValue
variable = vonmises_stress
[../]
[./dt]
type = TimestepSize
[../]
[./num_lin]
type = NumLinearIterations
outputs = console
[../]
[./num_nonlin]
type = NumNonlinearIterations
outputs = console
[../]
[./eff_creep_strain]
type = ElementAverageValue
variable = effective_viscoplasticity
[../]
[./porosity]
type = ElementAverageValue
variable = porosity
[../]
[]
[Outputs]
csv = true
[]
(modules/tensor_mechanics/test/tests/anisotropic_patch/anisotropic_patch_test.i)
# Patch Test
# This test is designed to compute constant xx, yy, zz, xy, yz, and zx
# stress on a set of irregular hexes. The mesh is composed of one
# block with seven elements. The elements form a unit cube with one
# internal element. There is a nodeset for each exterior node.
# The cube is displaced by 1e-6 units in x, 2e-6 in y, and 3e-6 in z.
# The faces are sheared as well (1e-6, 2e-6, and 3e-6 for xy, yz, and
# zx). This gives a uniform strain/stress state for all six unique
# tensor components.
# With Young's modulus at 1e6 and Poisson's ratio at 0, the shear
# modulus is 5e5 (G=E/2/(1+nu)). Therefore,
#
# stress xx = 1e6 * 1e-6 = 1
# stress yy = 1e6 * 2e-6 = 2
# stress zz = 1e6 * 3e-6 = 3
# stress xy = 2 * 5e5 * 1e-6 / 2 = 0.5
# (2 * G * gamma_xy / 2 = 2 * G * epsilon_xy)
# stress yz = 2 * 5e5 * 2e-6 / 2 = 1
# stress zx = 2 * 5e5 * 3e-6 / 2 = 1.5
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
block = '1 2 3 4 5 6 7'
[]
[Mesh]#Comment
file = anisotropic_patch_test.e
[] # Mesh
[Functions]
[./rampConstant1]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 1.'
scale_factor = 1e-6
[../]
[./rampConstant2]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 1.'
scale_factor = 2e-6
[../]
[./rampConstant3]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 1.'
scale_factor = 3e-6
[../]
[./rampConstant4]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 1.'
scale_factor = 4e-6
[../]
[./rampConstant6]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 1.'
scale_factor = 6e-6
[../]
[] # Functions
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[] # Variables
[AuxVariables]
[./elastic_energy]
order = CONSTANT
family = MONOMIAL
[../]
[] # AuxVariables
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx vonmises_stress hydrostatic_stress firstinv_stress secondinv_stress thirdinv_stress'
[../]
[]
[AuxKernels]
[./elastic_energy]
type = ElasticEnergyAux
variable = elastic_energy
[../]
[] # AuxKernels
[BCs]
[./node1_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./node1_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 1
function = rampConstant2
[../]
[./node1_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 1
function = rampConstant3
[../]
[./node2_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 2
function = rampConstant1
[../]
[./node2_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = rampConstant2
[../]
[./node2_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 2
function = rampConstant6
[../]
[./node3_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 3
function = rampConstant1
[../]
[./node3_y]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.0
[../]
[./node3_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 3
function = rampConstant3
[../]
[./node4_x]
type = DirichletBC
variable = disp_x
boundary = 4
value = 0.0
[../]
[./node4_y]
type = DirichletBC
variable = disp_y
boundary = 4
value = 0.0
[../]
[./node4_z]
type = DirichletBC
variable = disp_z
boundary = 4
value = 0.0
[../]
[./node5_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 5
function = rampConstant1
[../]
[./node5_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 5
function = rampConstant4
[../]
[./node5_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 5
function = rampConstant3
[../]
[./node6_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 6
function = rampConstant2
[../]
[./node6_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 6
function = rampConstant4
[../]
[./node6_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 6
function = rampConstant6
[../]
[./node7_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 7
function = rampConstant2
[../]
[./node7_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 7
function = rampConstant2
[../]
[./node7_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 7
function = rampConstant3
[../]
[./node8_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 8
function = rampConstant1
[../]
[./node8_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 8
function = rampConstant2
[../]
[./node8_z]
type = DirichletBC
variable = disp_z
boundary = 8
value = 0.0
[../]
[] # BCs
[Materials]
[./elastic_tensor]
type = ComputeElasticityTensor
C_ijkl = '1e6 0.0 0.0 1e6 0.0 1e6 0.5e6 0.5e6 0.5e6'
fill_method = symmetric9
euler_angle_1 = 18.0
euler_angle_2 = 43.0
euler_angle_3 = 177.0
# Isotropic material constants
# The three euler angles do not matter
# youngs_modulus = 1e6
# poissons_ratio = 0.0
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[] # Materials
[Executioner]
type = Transient
nl_abs_tol = 1e-10
l_max_its = 20
start_time = 0.0
dt = 1.0
num_steps = 2
end_time = 2.0
[] # Executioner
[Outputs]
file_base = anisotropic_patch_test_out
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[] # Outputs
(modules/tensor_mechanics/test/tests/strain_energy_density/incr_model_elas_plas.i)
# Single element test to check the strain energy density calculation
[GlobalParams]
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
xmin = 0
xmax = 1
ymin = 0
ymax = 2
[]
[AuxVariables]
[./SED]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./rampConstantUp]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = -100
[../]
[./ramp_disp_y]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 6.8e-6 1.36e-5'
[../]
[]
[Modules/TensorMechanics/Master]
[./master]
strain = SMALL
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress elastic_strain_xx elastic_strain_yy elastic_strain_zz plastic_strain_xx plastic_strain_yy plastic_strain_zz strain_xx strain_yy strain_zz'
planar_formulation = PLANE_STRAIN
[../]
[]
[AuxKernels]
[./SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
variable = disp_x
preset = false
boundary = 'left'
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_y
preset = false
boundary = 'bottom'
value = 0.0
[../]
[./top_disp]
type = FunctionDirichletBC
variable = disp_y
preset = false
boundary = 'top'
function = ramp_disp_y
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 30e+6
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'isoplas'
[../]
[./isoplas]
type = IsotropicPlasticityStressUpdate
yield_stress = 1e2
hardening_constant = 0.0
[../]
[./strain_energy_density]
type = StrainEnergyDensity
incremental = true
[../]
[]
[Executioner]
type = Transient
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 4'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_abs_tol = 3e-7
nl_rel_tol = 1e-12
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 2
num_steps = 2
[]
[Postprocessors]
[./epxx]
type = ElementalVariableValue
variable = elastic_strain_xx
elementid = 0
[../]
[./epyy]
type = ElementalVariableValue
variable = elastic_strain_yy
elementid = 0
[../]
[./epzz]
type = ElementalVariableValue
variable = elastic_strain_zz
elementid = 0
[../]
[./eplxx]
type = ElementalVariableValue
variable = plastic_strain_xx
elementid = 0
[../]
[./eplyy]
type = ElementalVariableValue
variable = plastic_strain_yy
elementid = 0
[../]
[./eplzz]
type = ElementalVariableValue
variable = plastic_strain_zz
elementid = 0
[../]
[./etxx]
type = ElementalVariableValue
variable = strain_xx
elementid = 0
[../]
[./etyy]
type = ElementalVariableValue
variable = strain_yy
elementid = 0
[../]
[./etzz]
type = ElementalVariableValue
variable = strain_zz
elementid = 0
[../]
[./sigxx]
type = ElementAverageValue
variable = stress_xx
[../]
[./sigyy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigzz]
type = ElementAverageValue
variable = stress_zz
[../]
[./SED]
type = ElementAverageValue
variable = SED
[../]
[]
[Outputs]
exodus = true
csv = true
[]
(modules/xfem/test/tests/moment_fitting/diffusion_moment_fitting_six_points.i)
# Test for a diffusion problem which uses six points moment_fitting approach.
# To use six points rule, add Quadrature block with order = FOURTH and type = MONOMIAL.
# See this paper (https://doi.org/10.1007/s00466-018-1544-2) for more details about moment_fitting approach.
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 6
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[XFEM]
geometric_cut_userobjects = 'line_seg_cut_uo'
qrule = moment_fitting
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.5 1.0 0.5 0.5'
time_start_cut = 0.0
time_end_cut = 0.0
[../]
[]
[Variables]
[./u]
[../]
[]
[Functions]
[./u_left]
type = PiecewiseLinear
x = '0 2'
y = '0 0.1'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = FunctionDirichletBC
variable = u
boundary = 3
function = u_left
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
[./Quadrature]
order = FOURTH
type = MONOMIAL
[../]
l_tol = 1e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 1.0
end_time = 2.0
[]
[Outputs]
interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/tensor_mechanics/test/tests/ad_thermal_expansion_function/dilatation.i)
# This test checks the thermal expansion calculated via an dilatation function.
# The coefficient is selected so as to result in a 1e-4 strain in the x-axis, and to cross over
# from positive to negative strain.
[Mesh]
[./gen]
type = GeneratedMeshGenerator
dim = 3
[../]
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[AuxVariables]
[./temp]
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
add_variables = true
eigenstrain_names = eigenstrain
generate_output = 'strain_xx strain_yy strain_zz'
use_automatic_differentiation = true
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./bottom]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./back]
type = DirichletBC
variable = disp_z
boundary = back
value = 0.0
[../]
[]
[AuxKernels]
[./temp]
type = FunctionAux
variable = temp
function = '1 + t'
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1
poissons_ratio = 0.3
[../]
[./stress]
type = ADComputeLinearElasticStress
[../]
[./thermal_expansion_strain]
type = ADComputeDilatationThermalExpansionFunctionEigenstrain
dilatation_function = cte_dilatation
stress_free_temperature = 1.5
temperature = temp
eigenstrain_name = eigenstrain
[../]
[]
[Functions]
[./cte_dilatation]
type = PiecewiseLinear
x = '1 2'
y = '-1e-4 1e-4'
[../]
[]
[Postprocessors]
[./disp_x_max]
type = SideAverageValue
variable = disp_x
boundary = right
[../]
[./temp_avg]
type = ElementAverageValue
variable = temp
[../]
[]
[Executioner]
type = Transient
end_time = 1.0
dt = 0.1
[]
[Outputs]
csv = true
[]
(modules/xfem/test/tests/solid_mechanics_basic/square_branch_tri_2d.i)
[GlobalParams]
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = TRI3
[]
[UserObjects]
[./line_seg_cut_uo0]
type = LineSegmentCutUserObject
cut_data = '-1.0000e-10 6.6340e-01 6.6340e-01 -1.0000e-10'
time_start_cut = 0.0
time_end_cut = 1.0
[../]
[./line_seg_cut_uo1]
type = LineSegmentCutUserObject
cut_data = '3.3120e-01 3.3200e-01 1.0001e+00 3.3200e-01'
time_start_cut = 1.0
time_end_cut = 2.0
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
planar_formulation = PLANE_STRAIN
add_variables = true
[../]
[]
[Functions]
[./right_disp_x]
type = PiecewiseLinear
x = '0 1.0 2.0 3.0'
y = '0 0.005 0.01 0.01'
[../]
[./top_disp_y]
type = PiecewiseLinear
x = '0 1.0 2.0 3.0'
y = '0 0.005 0.01 0.01'
[../]
[]
[BCs]
[./right_x]
type = FunctionDirichletBC
boundary = 1
variable = disp_x
function = right_disp_x
[../]
[./top_y]
type = FunctionDirichletBC
boundary = 2
variable = disp_y
function = top_disp_y
[../]
[./bottom_y]
type = DirichletBC
boundary = 0
variable = disp_y
value = 0.0
[../]
[./left_x]
type = DirichletBC
boundary = 3
variable = disp_x
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-16
nl_abs_tol = 1e-10
# time control
start_time = 0.0
dt = 1.0
end_time = 2.2
num_steps = 5000
[]
[Outputs]
file_base = square_branch_tri_2d_out
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/contact/test/tests/ring_contact/ring_contact.i)
#
# A test of contact with quadratic (Hex20) elements
#
# A stiff ring is pushed into a soft base. The base shows a circular impression.
#
[GlobalParams]
order = SECOND
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = false
[]
[Mesh]
file = ring_contact.e
[]
[Functions]
[./ring_y]
type = PiecewiseLinear
x = '0 1'
y = '0 1'
scale_factor = -0.2
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = FINITE
[../]
[]
[Contact]
[./dummy_name]
primary = 3
secondary = 2
penalty = 1e3
tension_release = -1
[../]
[]
[BCs]
[./plane]
type = DirichletBC
variable = disp_z
boundary = 10
value = 0.0
[../]
[./bottom_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./bottom_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./bottom_z]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0.0
[../]
[./ring_x]
type = DirichletBC
variable = disp_x
boundary = 4
value = 0.0
[../]
[./ring_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = ring_y
[../]
[]
[Materials]
[./stiffStuff1]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stiffStuff2]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e3
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[../]
[] # Materials
[Preconditioning]
[./SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -ksp_gmres_restart'
petsc_options_value = 'lu 101'
line_search = 'none'
nl_rel_tol = 1.e-10
l_max_its = 100
nl_max_its = 10
dt = 0.1
end_time = 0.5
[./Quadrature]
order = THIRD
[../]
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/thermal_expansion_function/finite_linear.i)
# This tests the thermal expansion coefficient function using both
# options to specify that function: mean and instantaneous. There
# two blocks, each containing a single element, and these use the
# two variants of the function.
# In this test, the instantaneous CTE function is a linear function
# while the mean CTE function is an analytic function designed to
# give the same response. If \bar{alpha}(T) is the mean CTE function,
# and \alpha(T) is the instantaneous CTE function,
# \bar{\alpha}(T) = 1/(T-Tref) \intA^{T}_{Tsf} \alpha(T) dT
# where Tref is the reference temperature used to define the mean CTE
# function, and Tsf is the stress-free temperature.
# This version of the test uses finite deformation theory.
# The two models produce very similar results. There are slight
# differences due to the large deformation treatment.
[Mesh]
file = 'blocks.e'
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[AuxVariables]
[./temp]
order = FIRST
family = LAGRANGE
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
eigenstrain_names = eigenstrain
generate_output = 'strain_xx strain_yy strain_zz'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = disp_x
boundary = 3
value = 0.0
[../]
[./bottom]
type = DirichletBC
variable = disp_y
boundary = 2
value = 0.0
[../]
[./back]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0.0
[../]
[]
[AuxKernels]
[./temp]
type = FunctionAux
variable = temp
block = '1 2'
function = temp_func
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./small_stress]
type = ComputeFiniteStrainElasticStress
[../]
[./thermal_expansion_strain1]
type = ComputeMeanThermalExpansionFunctionEigenstrain
block = 1
thermal_expansion_function = cte_func_mean
thermal_expansion_function_reference_temperature = 0.5
stress_free_temperature = 0.0
temperature = temp
eigenstrain_name = eigenstrain
[../]
[./thermal_expansion_strain2]
type = ComputeInstantaneousThermalExpansionFunctionEigenstrain
block = 2
thermal_expansion_function = cte_func_inst
stress_free_temperature = 0.0
temperature = temp
eigenstrain_name = eigenstrain
[../]
[]
[Functions]
[./cte_func_mean]
type = ParsedFunction
vars = 'tsf tref scale' #stress free temp, reference temp, scale factor
vals = '0.0 0.5 1e-4'
value = 'scale * (0.5 * t^2 - 0.5 * tsf^2) / (t - tref)'
[../]
[./cte_func_inst]
type = PiecewiseLinear
xy_data = '0 0.0
2 2.0'
scale_factor = 1e-4
[../]
[./temp_func]
type = PiecewiseLinear
xy_data = '0 1
1 2'
[../]
[]
[Postprocessors]
[./disp_1]
type = NodalMaxValue
variable = disp_x
boundary = 101
[../]
[./disp_2]
type = NodalMaxValue
variable = disp_x
boundary = 102
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
l_max_its = 100
l_tol = 1e-4
nl_abs_tol = 1e-8
nl_rel_tol = 1e-12
start_time = 0.0
end_time = 1.0
dt = 0.1
[]
[Outputs]
csv = true
[]
(modules/tensor_mechanics/test/tests/ad_smeared_cracking/cracking_rz_exponential.i)
#
# Test to exercise the exponential stress release
#
# Stress vs. strain should show a linear relationship until cracking,
# an exponential stress release, a linear relationship back to zero
# strain, a linear relationship with the original stiffness in
# compression and then back to zero strain, a linear relationship
# back to the exponential curve, and finally further exponential
# stress release.
[Mesh]
file = cracking_rz_test.e
[]
[Problem]
coord_type = RZ
[]
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Functions]
[./disply]
type = PiecewiseLinear
x = '0 1 2 3 4 5 6'
y = '0 0.00175 0 -0.0001 0 0.00175 0.0035'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx'
use_automatic_differentiation = true
[../]
[]
[BCs]
[./pully]
type = ADFunctionDirichletBC
variable = disp_y
boundary = 4
function = disply
[../]
[./bottom]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.0
[../]
[./sides]
type = ADDirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 186.5e9
poissons_ratio = 0.316
[../]
[./elastic_stress]
type = ADComputeSmearedCrackingStress
cracking_stress = 119.3e6
softening_models = exponential_softening
[../]
[./exponential_softening]
type = ADExponentialSoftening
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
petsc_options_iname = '-ksp_gmres_restart -pc_type'
petsc_options_value = '101 lu'
line_search = 'none'
l_max_its = 100
l_tol = 1e-5
nl_max_its = 10
nl_rel_tol = 1e-8
nl_abs_tol = 1e-4
start_time = 0.0
end_time = 6.0
dt = 0.005
dtmin = 0.005
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/dynamics/wave_1D/wave_newmark.i)
# Wave propogation in 1D using Newmark time integration
#
# The test is for an 1D bar element of length 4m fixed on one end
# with a sinusoidal pulse dirichlet boundary condition applied to the other end.
# beta and gamma are Newmark time integration parameters
# The equation of motion in terms of matrices is:
#
# M*accel + K*disp = 0
#
# Here M is the mass matrix, K is the stiffness matrix
#
# This equation is equivalent to:
#
# density*accel + Div Stress= 0
#
# The first term on the left is evaluated using the Inertial force kernel
# The last term on the left is evaluated using StressDivergenceTensors
#
# The displacement at the second, third and fourth node at t = 0.1 are
# -8.021501116638234119e-02, 2.073994362053969628e-02 and -5.045094181261772920e-03, respectively
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 4
nz = 1
xmin = 0.0
xmax = 0.1
ymin = 0.0
ymax = 4.0
zmin = 0.0
zmax = 0.1
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./vel_x]
[../]
[./accel_x]
[../]
[./vel_y]
[../]
[./accel_y]
[../]
[./vel_z]
[../]
[./accel_z]
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./TensorMechanics]
displacements = 'disp_x disp_y disp_z'
[../]
[./inertia_x]
type = InertialForce
variable = disp_x
velocity = vel_x
acceleration = accel_x
beta = 0.3025
gamma = 0.6
eta=0.0
[../]
[./inertia_y]
type = InertialForce
variable = disp_y
velocity = vel_y
acceleration = accel_y
beta = 0.3025
gamma = 0.6
eta=0.0
[../]
[./inertia_z]
type = InertialForce
variable = disp_z
velocity = vel_z
acceleration = accel_z
beta = 0.3025
gamma = 0.6
eta = 0.0
[../]
[]
[AuxKernels]
[./accel_x]
type = NewmarkAccelAux
variable = accel_x
displacement = disp_x
velocity = vel_x
beta = 0.3025
execute_on = timestep_end
[../]
[./vel_x]
type = NewmarkVelAux
variable = vel_x
acceleration = accel_x
gamma = 0.6
execute_on = timestep_end
[../]
[./accel_y]
type = NewmarkAccelAux
variable = accel_y
displacement = disp_y
velocity = vel_y
beta = 0.3025
execute_on = timestep_end
[../]
[./vel_y]
type = NewmarkVelAux
variable = vel_y
acceleration = accel_y
gamma = 0.6
execute_on = timestep_end
[../]
[./accel_z]
type = NewmarkAccelAux
variable = accel_z
displacement = disp_z
velocity = vel_z
beta = 0.3025
execute_on = timestep_end
[../]
[./vel_z]
type = NewmarkVelAux
variable = vel_z
acceleration = accel_z
gamma = 0.6
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 0
index_j = 1
[../]
[./strain_yy]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_yy
index_i = 0
index_j = 1
[../]
[]
[BCs]
[./top_y]
type = DirichletBC
variable = disp_y
boundary = top
value=0.0
[../]
[./top_x]
type = DirichletBC
variable = disp_x
boundary = top
value=0.0
[../]
[./top_z]
type = DirichletBC
variable = disp_z
boundary = top
value=0.0
[../]
[./right_x]
type = DirichletBC
variable = disp_x
boundary = right
value=0.0
[../]
[./right_z]
type = DirichletBC
variable = disp_z
boundary = right
value=0.0
[../]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = left
value=0.0
[../]
[./left_z]
type = DirichletBC
variable = disp_z
boundary = left
value=0.0
[../]
[./front_x]
type = DirichletBC
variable = disp_x
boundary = front
value=0.0
[../]
[./front_z]
type = DirichletBC
variable = disp_z
boundary = front
value=0.0
[../]
[./back_x]
type = DirichletBC
variable = disp_x
boundary = back
value=0.0
[../]
[./back_z]
type = DirichletBC
variable = disp_z
boundary = back
value=0.0
[../]
[./bottom_x]
type = DirichletBC
variable = disp_x
boundary = bottom
value=0.0
[../]
[./bottom_z]
type = DirichletBC
variable = disp_z
boundary = bottom
value=0.0
[../]
[./bottom_y]
type = FunctionDirichletBC
variable = disp_y
boundary = bottom
function = displacement_bc
[../]
[]
[Materials]
[./Elasticity_tensor]
type = ComputeElasticityTensor
block = 0
fill_method = symmetric_isotropic
C_ijkl = '1 0'
[../]
[./strain]
type = ComputeSmallStrain
block = 0
displacements = 'disp_x disp_y disp_z'
[../]
[./stress]
type = ComputeLinearElasticStress
block = 0
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = 'density'
prop_values = '1'
[../]
[]
[Executioner]
type = Transient
start_time = 0
end_time = 6.0
l_tol = 1e-12
nl_rel_tol = 1e-12
dt = 0.1
[]
[Functions]
[./displacement_bc]
type = PiecewiseLinear
data_file = 'sine_wave.csv'
format = columns
[../]
[]
[Postprocessors]
[./_dt]
type = TimestepSize
[../]
[./disp_1]
type = NodalVariableValue
nodeid = 1
variable = disp_y
[../]
[./disp_2]
type = NodalVariableValue
nodeid = 3
variable = disp_y
[../]
[./disp_3]
type = NodalVariableValue
nodeid = 10
variable = disp_y
[../]
[./disp_4]
type = NodalVariableValue
nodeid = 14
variable = disp_y
[../]
[]
[Outputs]
exodus = true
perf_graph = true
[]
(modules/richards/test/tests/theis/th02.i)
# fully-saturated
# production
[Mesh]
type = FileMesh
file = th02_input.e
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1 2 4 20'
x = '0 1 10 100'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1000
bulk_mod = 2E9
[../]
[./Seff1VG]
type = RichardsSeff1VG
m = 0.8
al = 1E-5
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0
sum_s_res = 0
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 1E-5
[../]
[./total_outflow_mass]
type = RichardsSumQuantity
[../]
[]
[Variables]
active = 'pressure'
[./pressure]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./p_ic]
type = FunctionIC
variable = pressure
function = initial_pressure
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[Kernels]
active = 'richardsf richardst'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[DiracKernels]
[./bh]
type = RichardsPolyLineSink
pressures = '-1E9 1E9'
fluxes = '200 200'
point_file = th01.points
SumQuantityUO = total_outflow_mass
variable = pressure
[../]
[]
[Postprocessors]
[./flow_report]
type = RichardsPlotQuantity
uo = total_outflow_mass
[../]
[./p50]
type = PointValue
variable = pressure
point = '50 0 0'
execute_on = 'initial timestep_end'
[../]
[]
[Functions]
[./initial_pressure]
type = ParsedFunction
value = 1E5
[../]
[]
[Materials]
[./all]
type = RichardsMaterial
block = 1
viscosity = 1E-3
mat_porosity = 0.1
mat_permeability = '1E-10 0 0 0 1E-10 0 0 0 1E-10'
density_UO = DensityConstBulk
relperm_UO = RelPermPower
sat_UO = Saturation
seff_UO = Seff1VG
SUPG_UO = SUPGstandard
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = Seff1VG
pressure_vars = pressure
[../]
[]
[Preconditioning]
[./usual]
type = SMP
full = true
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -ksp_max_it'
petsc_options_value = 'bcgs bjacobi 1E-6 1E-10 10000 30'
[../]
[]
[Executioner]
type = Transient
end_time = 100
solve_type = NEWTON
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = th02
csv = true
[]
(modules/tensor_mechanics/test/tests/ad_anisotropic_creep/ad_aniso_creep_x_3d.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
nx = 10
ny = 2
nz = 2
xmin = 0.0
ymin = 0.0
zmin = 0.0
xmax = 10.0
ymax = 1.0
zmax = 1.0
[]
[corner_node]
type = ExtraNodesetGenerator
new_boundary = '100'
nodes = '3 69'
input = gen
[]
[corner_node_2]
type = ExtraNodesetGenerator
new_boundary = '101'
nodes = '4 47'
input = corner_node
[]
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[AuxVariables]
[hydrostatic_stress]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_xx]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_xy]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_yy]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[hydrostatic_stress]
type = ADRankTwoScalarAux
variable = hydrostatic_stress
rank_two_tensor = stress
scalar_type = Hydrostatic
[]
[creep_strain_xx]
type = ADRankTwoAux
rank_two_tensor = creep_strain
variable = creep_strain_xx
index_i = 0
index_j = 0
[]
[creep_strain_xy]
type = ADRankTwoAux
rank_two_tensor = creep_strain
variable = creep_strain_xy
index_i = 0
index_j = 1
[]
[creep_strain_yy]
type = ADRankTwoAux
rank_two_tensor = creep_strain
variable = creep_strain_yy
index_i = 1
index_j = 1
[]
[sigma_xx]
type = ADRankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 1
index_j = 1
[]
[]
[Functions]
[pull]
type = PiecewiseLinear
x = '0 1.0e-9 1.0'
y = '0 -4e1 -4e1'
[]
[]
[Modules/TensorMechanics/Master]
[all]
strain = FINITE
generate_output = 'elastic_strain_xx stress_xx'
use_automatic_differentiation = true
add_variables = true
[]
[]
[Materials]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 700
poissons_ratio = 0.0
[]
[elastic_strain]
type = ADComputeMultipleInelasticStress
inelastic_models = "trial_creep_two"
max_iterations = 50
absolute_tolerance = 1e-16
[]
[trial_creep_two]
type = ADHillCreepStressUpdate
coefficient = 1e-16
n_exponent = 9
m_exponent = 0
activation_energy = 0
# F G H L M N
hill_constants = "0.5 0.25 0.3866 1.6413 1.6413 1.2731"
max_inelastic_increment = 0.00003
absolute_tolerance = 1e-20
relative_tolerance = 1e-20
# Force it to not use integration error
max_integration_error = 100.0
[]
[]
[BCs]
[no_disp_x]
type = ADDirichletBC
variable = disp_x
boundary = left
value = 0.0
[]
[no_disp_y]
type = ADDirichletBC
variable = disp_y
boundary = 100
value = 0.0
[]
[no_disp_z]
type = ADDirichletBC
variable = disp_z
boundary = 101
value = 0.0
[]
[Pressure]
[Side1]
boundary = right
function = pull
[]
[]
[]
[Executioner]
type = Transient
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
nl_rel_tol = 1.0e-14
nl_abs_tol = 1.0e-14
l_max_its = 10
num_steps = 10
dt = 1.0e-4
start_time = 0
automatic_scaling = true
[]
[Postprocessors]
[matl_ts_min]
type = MaterialTimeStepPostprocessor
[]
[max_disp_x]
type = ElementExtremeValue
variable = disp_x
[]
[max_disp_y]
type = ElementExtremeValue
variable = disp_y
[]
[max_hydro]
type = ElementAverageValue
variable = hydrostatic_stress
[]
[dt]
type = TimestepSize
[]
[num_lin]
type = NumLinearIterations
outputs = console
[]
[num_nonlin]
type = NumNonlinearIterations
outputs = console
[]
[creep_strain_xx]
type = ElementalVariableValue
variable = creep_strain_xx
execute_on = 'TIMESTEP_END'
elementid = 39
[]
[elastic_strain_xx]
type = ElementalVariableValue
variable = elastic_strain_xx
execute_on = 'TIMESTEP_END'
elementid = 39
[]
[sigma_xx]
type = ElementalVariableValue
variable = stress_xx
execute_on = 'TIMESTEP_END'
elementid = 39
[]
[]
[Outputs]
csv = true
exodus = true
perf_graph = true
[]
(modules/tensor_mechanics/test/tests/dynamics/wave_1D/wave_rayleigh_hht_ti.i)
# Wave propogation in 1D using HHT time integration in the presence of Rayleigh damping
#
# The test is for an 1D bar element of length 4m fixed on one end
# with a sinusoidal pulse dirichlet boundary condition applied to the other end.
# alpha, beta and gamma are HHT time integration parameters
# eta and zeta are mass dependent and stiffness dependent Rayleigh damping
# coefficients, respectively.
# The equation of motion in terms of matrices is:
#
# M*accel + (eta*M+zeta*K)*((1+alpha)*vel-alpha*vel_old)
# +(1+alpha)*K*disp-alpha*K*disp_old = 0
#
# Here M is the mass matrix, K is the stiffness matrix
#
# The displacement at the first, second, third and fourth node at t = 0.1 are
# -7.787499960311491942e-02, 1.955566679096475483e-02 and -4.634888180231294501e-03, respectively.
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 4
nz = 1
xmin = 0.0
xmax = 0.1
ymin = 0.0
ymax = 4.0
zmin = 0.0
zmax = 0.1
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./vel_x]
[../]
[./accel_x]
[../]
[./vel_y]
[../]
[./accel_y]
[../]
[./vel_z]
[../]
[./accel_z]
[../]
[]
[Kernels]
[./DynamicTensorMechanics]
displacements = 'disp_x disp_y disp_z'
alpha = -0.3
zeta = 0.1
[../]
[./inertia_x]
type = InertialForce
variable = disp_x
eta=0.1
alpha = -0.3
[../]
[./inertia_y]
type = InertialForce
variable = disp_y
eta=0.1
alpha = -0.3
[../]
[./inertia_z]
type = InertialForce
variable = disp_z
eta = 0.1
alpha = -0.3
[../]
[]
[AuxKernels]
[./accel_x] # These auxkernels are only to check output
type = TestNewmarkTI
displacement = disp_x
variable = accel_x
first = false
[../]
[./accel_y]
type = TestNewmarkTI
displacement = disp_y
variable = accel_y
first = false
[../]
[./accel_z]
type = TestNewmarkTI
displacement = disp_z
variable = accel_z
first = false
[../]
[./vel_x]
type = TestNewmarkTI
displacement = disp_x
variable = vel_x
[../]
[./vel_y]
type = TestNewmarkTI
displacement = disp_y
variable = vel_y
[../]
[./vel_z]
type = TestNewmarkTI
displacement = disp_z
variable = vel_z
[../]
[]
[BCs]
[./top_y]
type = DirichletBC
variable = disp_y
boundary = top
value=0.0
[../]
[./top_x]
type = DirichletBC
variable = disp_x
boundary = top
value=0.0
[../]
[./top_z]
type = DirichletBC
variable = disp_z
boundary = top
value=0.0
[../]
[./right_x]
type = DirichletBC
variable = disp_x
boundary = right
value=0.0
[../]
[./right_z]
type = DirichletBC
variable = disp_z
boundary = right
value=0.0
[../]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = left
value=0.0
[../]
[./left_z]
type = DirichletBC
variable = disp_z
boundary = left
value=0.0
[../]
[./front_x]
type = DirichletBC
variable = disp_x
boundary = front
value=0.0
[../]
[./front_z]
type = DirichletBC
variable = disp_z
boundary = front
value=0.0
[../]
[./back_x]
type = DirichletBC
variable = disp_x
boundary = back
value=0.0
[../]
[./back_z]
type = DirichletBC
variable = disp_z
boundary = back
value=0.0
[../]
[./bottom_x]
type = DirichletBC
variable = disp_x
boundary = bottom
value=0.0
[../]
[./bottom_z]
type = DirichletBC
variable = disp_z
boundary = bottom
value=0.0
[../]
[./bottom_y]
type = FunctionDirichletBC
variable = disp_y
boundary = bottom
function = displacement_bc
[../]
[]
[Materials]
[./Elasticity_tensor]
type = ComputeElasticityTensor
block = 0
fill_method = symmetric_isotropic
C_ijkl = '1 0'
[../]
[./strain]
type = ComputeSmallStrain
block = 0
displacements = 'disp_x disp_y disp_z'
[../]
[./stress]
type = ComputeLinearElasticStress
block = 0
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = 'density'
prop_values = '1'
[../]
[]
[Executioner]
type = Transient
start_time = 0
end_time = 6.0
l_tol = 1e-12
nl_rel_tol = 1e-12
dt = 0.1
[./TimeIntegrator]
type = NewmarkBeta
beta = 0.422
gamma = 0.8
[../]
[]
[Functions]
[./displacement_bc]
type = PiecewiseLinear
data_file = 'sine_wave.csv'
format = columns
[../]
[]
[Postprocessors]
[./_dt]
type = TimestepSize
[../]
[./disp_1]
type = NodalVariableValue
nodeid = 1
variable = disp_y
[../]
[./disp_2]
type = NodalVariableValue
nodeid = 3
variable = disp_y
[../]
[./disp_3]
type = NodalVariableValue
nodeid = 10
variable = disp_y
[../]
[./disp_4]
type = NodalVariableValue
nodeid = 14
variable = disp_y
[../]
[]
[Outputs]
file_base = 'wave_rayleigh_hht_out'
exodus = true
perf_graph = true
[]
(modules/tensor_mechanics/test/tests/beam/dynamic/dyn_euler_small_added_mass_file.i)
# Test for small strain euler beam vibration in y direction
# An impulse load is applied at the end of a cantilever beam of length 4m.
# The beam is massless with a lumped masses at the ends of the beam.
# The properties of the cantilever beam are as follows:
# Young's modulus (E) = 1e4
# Shear modulus (G) = 4e7
# Shear coefficient (k) = 1.0
# Cross-section area (A) = 0.01
# Iy = 1e-4 = Iz
# Length (L)= 4 m
# mass = 0.01899772 at the cantilever end
# mass = 2.0 at the fixed end (just for file testing purposes does not alter result)
# For this beam, the dimensionless parameter alpha = kAGL^2/EI = 6.4e6
# Therefore, the beam behaves like a Euler-Bernoulli beam.
# The theoretical first frequency of this beam is:
# f1 = 1/(2 pi) * sqrt(3EI/(mL^3)) = 0.25
# This implies that the corresponding time period of this beam is 4s.
# The FEM solution for this beam with 10 element gives time periods of 4s with time step of 0.01s.
# A higher time step of 0.1 s is used in the test to reduce computational time.
# The time history from this analysis matches with that obtained from Abaqus.
# Values from the first few time steps are as follows:
# time disp_y vel_y accel_y
# 0.0 0.0 0.0 0.0
# 0.1 0.0013076435060869 0.026152870121738 0.52305740243477
# 0.2 0.0051984378734383 0.051663017225289 -0.01285446036375
# 0.3 0.010269120909367 0.049750643493289 -0.02539301427625
# 0.4 0.015087433925158 0.046615616822532 -0.037307519138892
# 0.5 0.019534963888307 0.042334982440433 -0.048305168503101
[Mesh]
type = GeneratedMesh
xmin = 0.0
xmax = 4.0
nx = 10
dim = 1
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[./rot_x]
order = FIRST
family = LAGRANGE
[../]
[./rot_y]
order = FIRST
family = LAGRANGE
[../]
[./rot_z]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./vel_x]
order = FIRST
family = LAGRANGE
[../]
[./vel_y]
order = FIRST
family = LAGRANGE
[../]
[./vel_z]
order = FIRST
family = LAGRANGE
[../]
[./accel_x]
order = FIRST
family = LAGRANGE
[../]
[./accel_y]
order = FIRST
family = LAGRANGE
[../]
[./accel_z]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./accel_x]
type = NewmarkAccelAux
variable = accel_x
displacement = disp_x
velocity = vel_x
beta = 0.25
execute_on = timestep_end
[../]
[./vel_x]
type = NewmarkVelAux
variable = vel_x
acceleration = accel_x
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_y]
type = NewmarkAccelAux
variable = accel_y
displacement = disp_y
velocity = vel_y
beta = 0.25
execute_on = timestep_end
[../]
[./vel_y]
type = NewmarkVelAux
variable = vel_y
acceleration = accel_y
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_z]
type = NewmarkAccelAux
variable = accel_z
displacement = disp_z
velocity = vel_z
beta = 0.25
execute_on = timestep_end
[../]
[./vel_z]
type = NewmarkVelAux
variable = vel_z
acceleration = accel_z
gamma = 0.5
execute_on = timestep_end
[../]
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./fixy1]
type = DirichletBC
variable = disp_y
boundary = left
value = 0.0
[../]
[./fixz1]
type = DirichletBC
variable = disp_z
boundary = left
value = 0.0
[../]
[./fixr1]
type = DirichletBC
variable = rot_x
boundary = left
value = 0.0
[../]
[./fixr2]
type = DirichletBC
variable = rot_y
boundary = left
value = 0.0
[../]
[./fixr3]
type = DirichletBC
variable = rot_z
boundary = left
value = 0.0
[../]
[]
[NodalKernels]
[./force_y2]
type = UserForcingFunctionNodalKernel
variable = disp_y
boundary = right
function = force
[../]
[./x_inertial]
type = NodalTranslationalInertia
variable = disp_x
velocity = vel_x
acceleration = accel_x
boundary = 'left right'
beta = 0.25
gamma = 0.5
# nodal_mass_file = nodal_mass.csv # commented out for testing error message
[../]
[./y_inertial]
type = NodalTranslationalInertia
variable = disp_y
velocity = vel_y
acceleration = accel_y
boundary = 'left right'
beta = 0.25
gamma = 0.5
nodal_mass_file = nodal_mass.csv
[../]
[./z_inertial]
type = NodalTranslationalInertia
variable = disp_z
velocity = vel_z
acceleration = accel_z
boundary = 'left right'
beta = 0.25
gamma = 0.5
nodal_mass_file = nodal_mass.csv
[../]
[]
[Functions]
[./force]
type = PiecewiseLinear
x = '0.0 0.1 0.2 10.0'
y = '0.0 1e-2 0.0 0.0'
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options_iname = '-ksp_type -pc_type'
petsc_options_value = 'preonly lu'
dt = 0.1
end_time = 5.0
timestep_tolerance = 1e-6
[]
[Kernels]
[./solid_disp_x]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 0
variable = disp_x
[../]
[./solid_disp_y]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 1
variable = disp_y
[../]
[./solid_disp_z]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 2
variable = disp_z
[../]
[./solid_rot_x]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 3
variable = rot_x
[../]
[./solid_rot_y]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 4
variable = rot_y
[../]
[./solid_rot_z]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 5
variable = rot_z
[../]
[]
[Materials]
[./elasticity]
type = ComputeElasticityBeam
youngs_modulus = 1.0e4
poissons_ratio = -0.999875
shear_coefficient = 1.0
block = 0
[../]
[./strain]
type = ComputeIncrementalBeamStrain
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
area = 0.01
Ay = 0.0
Az = 0.0
Iy = 1.0e-4
Iz = 1.0e-4
y_orientation = '0.0 1.0 0.0'
[../]
[./stress]
type = ComputeBeamResultants
block = 0
[../]
[]
[Postprocessors]
[./disp_x]
type = PointValue
point = '4.0 0.0 0.0'
variable = disp_x
[../]
[./disp_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = disp_y
[../]
[./vel_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = vel_y
[../]
[./accel_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = accel_y
[../]
[]
[Outputs]
file_base = dyn_euler_small_added_mass_out
exodus = true
csv = true
perf_graph = true
[]
(modules/tensor_mechanics/test/tests/smeared_cracking/cracking_rz.i)
#
[Mesh]
file = cracking_rz_test.e
[]
[Problem]
coord_type = RZ
[]
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Functions]
[./displ]
type = PiecewiseLinear
x = '0 1 2 3 4'
y = '0 1 0 -1 0'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx'
[../]
[]
[BCs]
[./pull]
type = FunctionDirichletBC
variable = disp_x
boundary = 2
function = displ
[../]
[./left]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./bottom]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 4.0e7
poissons_ratio = 0.0
[../]
[./elastic_stress]
type = ComputeSmearedCrackingStress
cracking_stress = 1.68e6
softening_models = abrupt_softening
[../]
[./abrupt_softening]
type = AbruptSoftening
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101 '
line_search = 'none'
l_max_its = 100
nl_max_its = 100
nl_rel_tol = 1e-8
nl_abs_tol = 1e-2
l_tol = 1e-5
start_time = 0.0
end_time = 0.1
dt = 0.025
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_htonly/cyl2D_yz.i)
#
# 2D Cylindrical Gap Heat Transfer Test.
#
# This test exercises 2D gap heat transfer for a constant conductivity gap.
#
# The mesh consists of an inner solid cylinder of radius = 1 unit, and outer
# hollow cylinder with an inner radius of 2 in the y-z plane. In other words,
# the gap between them is 1 radial unit in length.
#
# The calculated results are the same as for the cyl2D.i case in the x-y plane.
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
[file]
type = FileMeshGenerator
file = cyl2D.e
[]
[./rotate]
type = TransformGenerator
transform = ROTATE
vector_value = '0 90 90'
input = file
[../]
[]
[Functions]
[./temp]
type = PiecewiseLinear
x = '0 1'
y = '100 200'
[../]
[]
[Variables]
[./temp]
initial_condition = 100
[../]
[]
[AuxVariables]
[./gap_conductance]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./heat_conduction]
type = HeatConduction
variable = temp
[../]
[]
[AuxKernels]
[./gap_cond]
type = MaterialRealAux
property = gap_conductance
variable = gap_conductance
boundary = 2
[../]
[]
[Materials]
[./heat1]
type = HeatConductionMaterial
block = '1 2'
specific_heat = 1.0
thermal_conductivity = 1000000.0
[../]
[]
[ThermalContact]
[./thermal_contact]
type = GapHeatTransfer
variable = temp
primary = 3
secondary = 2
emissivity_primary = 0
emissivity_secondary = 0
gap_conductivity = 1
quadrature = true
gap_geometry_type = CYLINDER
cylinder_axis_point_1 = '0 0 0'
cylinder_axis_point_2 = '1 0 0'
[../]
[]
[BCs]
[./mid]
type = FunctionDirichletBC
boundary = 1
variable = temp
function = temp
[../]
[./temp_far_right]
type = DirichletBC
boundary = 4
variable = temp
value = 100
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
dt = 1
dtmin = 0.01
end_time = 1
nl_rel_tol = 1e-12
nl_abs_tol = 1e-7
[./Quadrature]
order = fifth
side_order = seventh
[../]
[]
[Outputs]
exodus = true
[]
[Postprocessors]
[./temp_left]
type = SideAverageValue
boundary = 2
variable = temp
[../]
[./temp_right]
type = SideAverageValue
boundary = 3
variable = temp
[../]
[./flux_left]
type = SideFluxIntegral
variable = temp
boundary = 2
diffusivity = thermal_conductivity
[../]
[./flux_right]
type = SideFluxIntegral
variable = temp
boundary = 3
diffusivity = thermal_conductivity
[../]
[]
(modules/combined/test/tests/combined_plasticity_temperature/ad_plasticity_temperature_dep_yield.i)
#
# This is a test of the piece-wise linear strain hardening model using the
# small strain formulation. This test exercises the temperature-dependent
# yield stress.
#
# Test procedure:
# 1. The element is pulled to and then beyond the yield stress for a given
# temperature.
# 2. The displacement is then constant while the temperature increases and
# the yield stress decreases. This results in a lower stress with more
# plastic strain.
# 3. The temperature decreases beyond its original value giving a higher
# yield stress. The displacement increases, causing increases stress to
# the new yield stress.
# 4. The temperature and yield stress are constant with increasing
# displacement giving a constant stress and more plastic strain.
#
# Plotting total_strain_yy on the x axis and stress_yy on the y axis shows
# the stress history in a clear way.
#
# s |
# t | *****
# r | *
# e | ***** *
# s | * * *
# s | * *
# |*
# +------------------
# total strain
#
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
incremental = true
add_variables = true
generate_output = 'stress_yy plastic_strain_xx plastic_strain_yy plastic_strain_zz'
use_automatic_differentiation = true
[../]
[]
[Variables]
[./temp]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
[./top_pull]
type = PiecewiseLinear
x = '0 1 2 4 5 6'
y = '0 0.025 0.05 0.05 0.06 0.085'
[../]
[./yield]
type = PiecewiseLinear
x = '400 500 600'
y = '6e3 5e3 4e3'
[../]
[./temp]
type = PiecewiseLinear
x = '0 1 2 3 4'
y = '500 500 500 600 400'
[../]
[]
[Kernels]
[./heat]
type = ADHeatConduction
variable = temp
[../]
[]
[BCs]
[./y_pull_function]
type = FunctionDirichletBC
variable = disp_y
boundary = top
function = top_pull
[../]
[./x_bot]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./y_bot]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./z_bot]
type = DirichletBC
variable = disp_z
boundary = back
value = 0.0
[../]
[./temp]
type = FunctionDirichletBC
variable = temp
function = temp
boundary = left
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
block = 0
youngs_modulus = 2.0e5
poissons_ratio = 0.3
[../]
[./creep_plas]
type = ADComputeMultipleInelasticStress
block = 0
inelastic_models = 'plasticity'
max_iterations = 50
absolute_tolerance = 1e-05
[../]
[./plasticity]
type = ADIsotropicPlasticityStressUpdate
block = 0
hardening_constant = 0
yield_stress_function = yield
temperature = temp
[../]
[./heat_conduction]
type = ADHeatConductionMaterial
block = 0
specific_heat = 1
thermal_conductivity = 1
[../]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
line_search = 'none'
l_max_its = 100
nl_max_its = 100
nl_rel_tol = 1e-12
nl_abs_tol = 1e-10
l_tol = 1e-9
start_time = 0.0
end_time = 6
dt = 0.1
[]
[Outputs]
exodus = true
[]
(modules/combined/test/tests/internal_volume/rz_displaced.i)
#
# Volume Test
#
# This test is designed to compute the volume of a space when displacements
# are imposed.
#
# The mesh is composed of one block (1) with two elements. The mesh is
# such that the initial volume is 1. One element face is displaced to
# produce a final volume of 2.
#
# r1
# +----+ -
# | | |
# +----+ h V1 = pi * h * r1^2
# | | |
# +----+ -
#
# becomes
#
# +----+
# | \
# +------+ v2 = pi * h/2 * ( r2^2 + 1/3 * ( r2^2 + r2*r1 + r1^2 ) )
# | |
# +------+
# r2
#
# r1 = 1
# r2 = 1.5380168369562588
# h = 1/pi
#
# Note: Because the InternalVolume PP computes cavity volumes as positive,
# the volumes reported are negative.
#
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Problem]
coord_type = RZ
[]
[Mesh]
file = meshes/rz_displaced.e
# This test uses ElementalVariableValue postprocessors on specific
# elements, so element numbering needs to stay unchanged
allow_renumbering = false
[]
[Functions]
[./disp_x]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 0.5380168369562588'
[../]
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./volumetric_strain]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
volumetric_locking_correction = false
decomposition_method = EigenSolution
incremental = true
strain = FINITE
[../]
[]
[AuxKernels]
[./fred]
type = RankTwoScalarAux
rank_two_tensor = total_strain
variable = volumetric_strain
scalar_type = VolumetricStrain
execute_on = timestep_end
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = 2
value = 0.0
[../]
[./x]
type = FunctionDirichletBC
boundary = 3
variable = disp_x
function = disp_x
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
start_time = 0.0
dt = 1.0
end_time = 1.0
[]
[Postprocessors]
[./internalVolume]
type = InternalVolume
boundary = 2
execute_on = 'initial timestep_end'
[../]
[./volStrain0]
type = ElementalVariableValue
elementid = 0
variable = volumetric_strain
[../]
[./volStrain1]
type = ElementalVariableValue
elementid = 1
variable = volumetric_strain
[../]
[]
[Outputs]
exodus = true
csv = true
[]
(modules/richards/test/tests/rogers_stallybrass_clements/rsc_lumped_01.i)
# RSC test with high-res time and spatial resolution
[Mesh]
type = GeneratedMesh
dim = 2
nx = 600
ny = 1
xmin = 0
xmax = 10 # x is the depth variable, called zeta in RSC
ymin = 0
ymax = 0.05
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = 'DensityWater DensityOil'
relperm_UO = 'RelPerm RelPerm'
SUPG_UO = 'SUPGstandard SUPGstandard'
sat_UO = 'Saturation Saturation'
seff_UO = 'SeffWater SeffOil'
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '3E-3 3E-2 0.05'
x = '0 1 5'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = 'pwater poil'
[../]
[./DensityWater]
type = RichardsDensityConstBulk
dens0 = 10
bulk_mod = 2E9
[../]
[./DensityOil]
type = RichardsDensityConstBulk
dens0 = 20
bulk_mod = 2E9
[../]
[./SeffWater]
type = RichardsSeff2waterRSC
oil_viscosity = 2E-3
scale_ratio = 2E3
shift = 10
[../]
[./SeffOil]
type = RichardsSeff2gasRSC
oil_viscosity = 2E-3
scale_ratio = 2E3
shift = 10
[../]
[./RelPerm]
type = RichardsRelPermMonomial
simm = 0
n = 1
[../]
[./Saturation]
type = RichardsSat
s_res = 0.0
sum_s_res = 0.0
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 1.0E-2
[../]
[]
[Variables]
[./pwater]
[../]
[./poil]
[../]
[]
[ICs]
[./water_init]
type = ConstantIC
variable = pwater
value = 0
[../]
[./oil_init]
type = ConstantIC
variable = poil
value = 15
[../]
[]
[Kernels]
[./richardstwater]
type = RichardsLumpedMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFlux
variable = pwater
[../]
[./richardstoil]
type = RichardsLumpedMassChange
variable = poil
[../]
[./richardsfoil]
type = RichardsFlux
variable = poil
[../]
[]
[AuxVariables]
[./SWater]
[../]
[./SOil]
[../]
[]
[AuxKernels]
[./Seff1VGwater_AuxK]
type = RichardsSeffAux
variable = SWater
seff_UO = SeffWater
pressure_vars = 'pwater poil'
[../]
[./Seff1VGoil_AuxK]
type = RichardsSeffAux
variable = SOil
seff_UO = SeffOil
pressure_vars = 'pwater poil'
[../]
[]
[BCs]
# we are pumping water into a system that has virtually incompressible fluids, hence the pressures rise enormously. this adversely affects convergence because of almost-overflows and precision-loss problems. The fixed things help keep pressures low and so prevent these awful behaviours. the movement of the saturation front is the same regardless of the fixed things.
active = 'recharge fixedoil fixedwater'
[./recharge]
type = RichardsPiecewiseLinearSink
variable = pwater
boundary = 'left'
pressures = '-1E10 1E10'
bare_fluxes = '-1 -1'
use_mobility = false
use_relperm = false
[../]
[./fixedwater]
type = DirichletBC
variable = pwater
boundary = 'right'
value = 0
[../]
[./fixedoil]
type = DirichletBC
variable = poil
boundary = 'right'
value = 15
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.25
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
viscosity = '1E-3 2E-3'
gravity = '0E-0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
active = 'andy'
[./andy]
type = SMP
full = true
petsc_options = ''
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-10 1E-10 10000'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
petsc_options = '-snes_converged_reason'
end_time = 5
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = rsc_lumped_01
interval = 100000
execute_on = 'initial final'
exodus = true
[]
(test/tests/time_integrators/central-difference/central_difference.i)
###########################################################
# This is a simple test with a time-dependent problem
# demonstrating the use of the TimeIntegrator system.
#
# Testing that the first and second time derivatives
# are calculated correctly using the Newmark-Beta method
#
# @Requirement F1.30
###########################################################
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 1
ny = 1
[]
[Variables]
[./u]
[../]
[]
[Functions]
[./forcing_fn]
type = PiecewiseLinear
x = '0.0 0.1 0.2 0.3 0.4 0.5 0.6'
y = '0.0 0.0 0.0025 0.01 0.0175 0.02 0.02'
[../]
[]
[Kernels]
[./ie]
type = TimeDerivative
variable = u
[../]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = FunctionDirichletBC
variable = u
boundary = 'left'
function = forcing_fn
preset = false
[../]
[./right]
type = FunctionDirichletBC
variable = u
boundary = 'right'
function = forcing_fn
preset = false
[../]
[]
[Executioner]
type = Transient
[./TimeIntegrator]
type = CentralDifference
[]
start_time = 0.0
num_steps = 6
dt = 0.1
[]
[Postprocessors]
[./udot]
type = ElementAverageTimeDerivative
variable = u
[../]
[./udotdot]
type = ElementAverageSecondTimeDerivative
variable = u
[../]
[./u]
type = ElementAverageValue
variable = u
[../]
[]
[Outputs]
csv = true
[]
(modules/porous_flow/test/tests/infiltration_and_drainage/rsc02.i)
# RSC test with low-res time and spatial resolution
[Mesh]
type = GeneratedMesh
dim = 2
nx = 200
ny = 1
xmin = 0
xmax = 10 # x is the depth variable, called zeta in RSC
ymin = 0
ymax = 0.05
[]
[GlobalParams]
PorousFlowDictator = dictator
gravity = '0 0 0'
[]
[Functions]
[dts]
type = PiecewiseLinear
y = '3E-2 5E-1 8E-1'
x = '0 1 5'
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pwater poil'
number_fluid_phases = 2
number_fluid_components = 2
[]
[pc]
type = PorousFlowCapillaryPressureRSC
oil_viscosity = 2E-3
scale_ratio = 2E3
shift = 10
[]
[]
[Modules]
[FluidProperties]
[water]
type = SimpleFluidProperties
bulk_modulus = 2e9
density0 = 10
thermal_expansion = 0
viscosity = 1e-3
[]
[oil]
type = SimpleFluidProperties
bulk_modulus = 2e9
density0 = 20
thermal_expansion = 0
viscosity = 2e-3
[]
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow2PhasePP
phase0_porepressure = pwater
phase1_porepressure = poil
capillary_pressure = pc
[]
[massfrac]
type = PorousFlowMassFraction
mass_fraction_vars = 'massfrac_ph0_sp0 massfrac_ph1_sp0'
[]
[water]
type = PorousFlowSingleComponentFluid
fp = water
phase = 0
compute_enthalpy = false
compute_internal_energy = false
[]
[oil]
type = PorousFlowSingleComponentFluid
fp = oil
phase = 1
compute_enthalpy = false
compute_internal_energy = false
[]
[relperm_water]
type = PorousFlowRelativePermeabilityCorey
n = 1
phase = 0
[]
[relperm_oil]
type = PorousFlowRelativePermeabilityCorey
n = 1
phase = 1
[]
[porosity]
type = PorousFlowPorosityConst
porosity = 0.25
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
[]
[]
[Variables]
[pwater]
[]
[poil]
[]
[]
[ICs]
[water_init]
type = ConstantIC
variable = pwater
value = 0
[]
[oil_init]
type = ConstantIC
variable = poil
value = 15
[]
[]
[Kernels]
[mass0]
type = PorousFlowMassTimeDerivative
fluid_component = 0
variable = pwater
[]
[flux0]
type = PorousFlowAdvectiveFlux
fluid_component = 0
variable = pwater
[]
[mass1]
type = PorousFlowMassTimeDerivative
fluid_component = 1
variable = poil
[]
[flux1]
type = PorousFlowAdvectiveFlux
fluid_component = 1
variable = poil
[]
[]
[AuxVariables]
[SWater]
family = MONOMIAL
order = CONSTANT
[]
[SOil]
family = MONOMIAL
order = CONSTANT
[]
[massfrac_ph0_sp0]
initial_condition = 1
[]
[massfrac_ph1_sp0]
initial_condition = 0
[]
[]
[AuxKernels]
[SWater]
type = MaterialStdVectorAux
property = PorousFlow_saturation_qp
index = 0
variable = SWater
[]
[SOil]
type = MaterialStdVectorAux
property = PorousFlow_saturation_qp
index = 1
variable = SOil
[]
[]
[BCs]
# we are pumping water into a system that has virtually incompressible fluids, hence the pressures rise enormously. this adversely affects convergence because of almost-overflows and precision-loss problems. The fixed things help keep pressures low and so prevent these awful behaviours. the movement of the saturation front is the same regardless of the fixed things.
active = 'recharge fixedoil fixedwater'
[recharge]
type = PorousFlowSink
variable = pwater
boundary = 'left'
flux_function = -1.0
[]
[fixedwater]
type = DirichletBC
variable = pwater
boundary = 'right'
value = 0
[]
[fixedoil]
type = DirichletBC
variable = poil
boundary = 'right'
value = 15
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
petsc_options = '-snes_converged_reason -ksp_diagonal_scale -ksp_diagonal_scale_fix -ksp_gmres_modifiedgramschmidt -snes_linesearch_monitor'
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -sub_pc_factor_shift_type -pc_asm_overlap -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'gmres asm lu NONZERO 2 1E-10 1E-10 10000'
[]
[]
[VectorPostprocessors]
[swater]
type = LineValueSampler
variable = SWater
start_point = '0 0 0'
end_point = '7 0 0'
sort_by = x
num_points = 21
execute_on = timestep_end
[]
[]
[Executioner]
type = Transient
solve_type = Newton
petsc_options = '-snes_converged_reason'
end_time = 5
[TimeStepper]
type = FunctionDT
function = dts
[]
[]
[Outputs]
file_base = rsc02
[along_line]
type = CSV
execute_vector_postprocessors_on = final
[]
[exodus]
type = Exodus
execute_on = 'initial final'
[]
[]
(modules/contact/examples/2d_indenter/indenter_rz_fine.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Problem]
coord_type = RZ
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
[]
[Mesh]
patch_update_strategy = auto
patch_size = 2
partitioner = centroid
centroid_partitioner_direction = y
[simple_mesh]
type = FileMeshGenerator
file = indenter_rz_fine_bigsideset.e
[]
[secondary]
type = LowerDBlockFromSidesetGenerator
sidesets = '4'
new_block_id = '10001'
new_block_name = 'secondary_lower'
input = simple_mesh
[]
[primary]
type = LowerDBlockFromSidesetGenerator
sidesets = '6'
new_block_id = '10000'
new_block_name = 'primary_lower'
input = secondary
[]
# For NodalVariableValue to work with distributed mesh
allow_renumbering = false
[../]
[Functions]
[disp_y]
type = PiecewiseLinear
x = '0. 1.0 2.0 2.6 3.0'
y = '0. -4.5 -5.7 -5.7 -4.0'
[]
[]
[Variables]
[disp_x]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[disp_y]
order = FIRST
family = LAGRANGE
block = '1 2'
[]
[frictionless_normal_lm]
block = 'secondary_lower'
[]
[]
[AuxVariables]
[saved_x]
[]
[saved_y]
[]
[]
[Modules/TensorMechanics/Master]
[all]
add_variables = true
strain = FINITE
block = '1 2'
use_automatic_differentiation = false
generate_output = 'stress_xx stress_xy stress_xz stress_yy stress_zz'
save_in = 'saved_x saved_y'
[]
[]
[BCs]
# Symmetries of the Problem
[symm_x_indenter]
type = DirichletBC
variable = disp_x
boundary = 5
value = 0.0
[]
[symm_x_material]
type = DirichletBC
variable = disp_x
boundary = 9
value = 0.0
[]
# Material should not fly away
[material_base_y]
type = DirichletBC
variable = disp_y
boundary = 8
value = 0.0
[]
# Drive indenter motion
[disp_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 1
function = disp_y
[]
[]
[Constraints]
# All constraints below for mechanical contact (Mortar)
[lm]
type = NormalNodalLMMechanicalContact
secondary = '4'
primary = 6
variable = frictionless_normal_lm
primary_variable = disp_x
disp_y = disp_y
use_displaced_mesh = true
tangential_tolerance = 0.01
[]
[x]
type = NormalMortarMechanicalContact
primary_boundary = '6'
secondary_boundary = '4'
primary_subdomain = '10000'
secondary_subdomain = '10001'
variable = frictionless_normal_lm
secondary_variable = disp_x
component = x
use_displaced_mesh = true
compute_lm_residuals = true
[]
[y]
type = NormalMortarMechanicalContact
primary_boundary = '6'
secondary_boundary = '4'
primary_subdomain = '10000'
secondary_subdomain = '10001'
variable = frictionless_normal_lm
secondary_variable = disp_y
component = y
use_displaced_mesh = true
compute_lm_residuals = true
[]
[../]
[UserObjects]
[slip_rate_gss]
type = CrystalPlasticitySlipRateGSS
variable_size = 48
slip_sys_file_name = input_slip_sys_bcc48.txt
num_slip_sys_flowrate_props = 2
flowprops = '1 48 0.0001 0.01'
uo_state_var_name = state_var_gss
slip_incr_tol = 10.0
block = 2
[]
[slip_resistance_gss]
type = CrystalPlasticitySlipResistanceGSS
variable_size = 48
uo_state_var_name = state_var_gss
block = 2
[]
[state_var_gss]
type = CrystalPlasticityStateVariable
variable_size = 48
groups = '0 24 48'
group_values = '900 1000' #120
uo_state_var_evol_rate_comp_name = state_var_evol_rate_comp_gss
scale_factor = 1.0
block = 2
[]
[state_var_evol_rate_comp_gss]
type = CrystalPlasticityStateVarRateComponentGSS
variable_size = 48
hprops = '1.4 1000 1200 2.5'
uo_slip_rate_name = slip_rate_gss
uo_state_var_name = state_var_gss
block = 2
[]
[]
[Materials]
[tensor]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1.0e7
poissons_ratio = 0.25
[]
[stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[]
[crysp]
type = FiniteStrainUObasedCP
block = 2
stol = 1e-2
tan_mod_type = exact
uo_slip_rates = 'slip_rate_gss'
uo_slip_resistances = 'slip_resistance_gss'
uo_state_vars = 'state_var_gss'
uo_state_var_evol_rate_comps = 'state_var_evol_rate_comp_gss'
maximum_substep_iteration = 20
[]
[elasticity_tensor]
type = ComputeElasticityTensorCP
block = 2
C_ijkl = '265190 113650 113650 265190 113650 265190 75769 75769 75760'
fill_method = symmetric9
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_shift_type '
'-pc_factor_shift_amount'
petsc_options_value = 'lu basic NONZERO 1e-15'
line_search = 'none'
automatic_scaling = true
nl_abs_tol = 1.5e-07
nl_rel_tol = 1.5e-07
l_max_its = 40
l_abs_tol = 1e-08
l_tol = 1e-08
start_time = 0.0
dt = 0.01
end_time = 3.0 # Executioner
[]
[Postprocessors]
[maxdisp]
type = NodalVariableValue
nodeid = 39
variable = disp_y
[]
[resid_y]
type = NodalSum
variable = saved_y
boundary = 1
[]
[]
[Outputs]
[out]
type = Exodus
elemental_as_nodal = true
[]
perf_graph = true
csv = true
[]
(modules/porous_flow/test/tests/gravity/grav02d.i)
# Checking that gravity head is established in the transient situation when 0<=saturation<=1 (note the less-than-or-equal-to).
# 2phase (PP), 2components, vanGenuchten, constant fluid bulk-moduli for each phase, constant viscosity, constant permeability, Corey relative perm.
# A boundary condition enforces porepressures at the right boundary
# 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
[]
[Functions]
[dts]
type = PiecewiseLinear
x = '1E-3 1E-2 1E-1 2E-1'
y = '1E-3 1E-2 0.2E-1 1E-1'
[]
[]
[Variables]
[ppwater]
initial_condition = 0
[]
[ppgas]
initial_condition = 0.5
[]
[]
[AuxVariables]
[massfrac_ph0_sp0]
initial_condition = 1
[]
[massfrac_ph1_sp0]
initial_condition = 0
[]
[]
[BCs]
[ppwater]
type = DirichletBC
boundary = right
variable = ppwater
value = 0
[]
[ppgas]
type = DirichletBC
boundary = right
variable = ppgas
value = 0.5
[]
[]
[Kernels]
[mass0]
type = PorousFlowMassTimeDerivative
fluid_component = 0
variable = ppwater
[]
[flux0]
type = PorousFlowAdvectiveFlux
fluid_component = 0
variable = ppwater
gravity = '-1 0 0'
[]
[mass1]
type = PorousFlowMassTimeDerivative
fluid_component = 1
variable = ppgas
[]
[flux1]
type = PorousFlowAdvectiveFlux
fluid_component = 1
variable = ppgas
gravity = '-1 0 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
[]
[]
[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 = 1.2
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
[]
[porosity]
type = PorousFlowPorosityConst
porosity = 0.1
[]
[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'
[]
[ppwater_00]
type = PointValue
variable = ppwater
point = '0 0 0'
[]
[ppwater_01]
type = PointValue
variable = ppwater
point = '-0.1 0 0'
[]
[ppwater_02]
type = PointValue
variable = ppwater
point = '-0.2 0 0'
[]
[ppwater_03]
type = PointValue
variable = ppwater
point = '-0.3 0 0'
[]
[ppwater_04]
type = PointValue
variable = ppwater
point = '-0.4 0 0'
[]
[ppwater_05]
type = PointValue
variable = ppwater
point = '-0.5 0 0'
[]
[ppwater_06]
type = PointValue
variable = ppwater
point = '-0.6 0 0'
[]
[ppwater_07]
type = PointValue
variable = ppwater
point = '-0.7 0 0'
[]
[ppwater_08]
type = PointValue
variable = ppwater
point = '-0.8 0 0'
[]
[ppwater_09]
type = PointValue
variable = ppwater
point = '-0.9 0 0'
[]
[ppwater_10]
type = PointValue
variable = ppwater
point = '-1 0 0'
[]
[ppgas_00]
type = PointValue
variable = ppgas
point = '0 0 0'
[]
[ppgas_01]
type = PointValue
variable = ppgas
point = '-0.1 0 0'
[]
[ppgas_02]
type = PointValue
variable = ppgas
point = '-0.2 0 0'
[]
[ppgas_03]
type = PointValue
variable = ppgas
point = '-0.3 0 0'
[]
[ppgas_04]
type = PointValue
variable = ppgas
point = '-0.4 0 0'
[]
[ppgas_05]
type = PointValue
variable = ppgas
point = '-0.5 0 0'
[]
[ppgas_06]
type = PointValue
variable = ppgas
point = '-0.6 0 0'
[]
[ppgas_07]
type = PointValue
variable = ppgas
point = '-0.7 0 0'
[]
[ppgas_08]
type = PointValue
variable = ppgas
point = '-0.8 0 0'
[]
[ppgas_09]
type = PointValue
variable = ppgas
point = '-0.9 0 0'
[]
[ppgas_10]
type = PointValue
variable = ppgas
point = '-1 0 0'
[]
[]
[Preconditioning]
active = andy
[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-12 1E-10 10000'
[]
[check]
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-12 1E-10 10000 test'
[]
[]
[Executioner]
type = Transient
solve_type = Newton
[TimeStepper]
type = FunctionDT
function = dts
[]
end_time = 1.0
[]
[Outputs]
[csv]
type = CSV
execute_on = 'initial final'
file_base = grav02d
[]
[]
(modules/contact/test/tests/verification/patch_tests/single_pnt_2d/single_point_2d_contact_line_search.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = single_point_2d.e
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[]
[Functions]
[./appl_disp]
type = PiecewiseLinear
x = '0 0.001 0.101'
y = '0 0.0 -0.10'
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./incslip_x]
type = PenetrationAux
variable = inc_slip_x
quantity = incremental_slip_x
boundary = 3
paired_boundary = 2
[../]
[./incslip_y]
type = PenetrationAux
variable = inc_slip_y
quantity = incremental_slip_y
boundary = 3
paired_boundary = 2
[../]
[./accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[../]
[./accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[]
[BCs]
[./botx]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./boty]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./topx]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = appl_disp
[../]
[./topy]
type = DirichletBC
variable = disp_y
boundary = 4
value = -0.002001
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e9
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputePlaneFiniteStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputePlaneFiniteStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Postprocessors]
[./disp_x]
type = NodalVariableValue
nodeid = 5
variable = disp_x
[../]
[./disp_y]
type = NodalVariableValue
nodeid = 5
variable = disp_y
[../]
[./inc_slip_x]
type = NodalVariableValue
nodeid = 5
variable = inc_slip_x
[../]
[./inc_slip_y]
type = NodalVariableValue
nodeid = 5
variable = inc_slip_y
[../]
[./accum_slip_x]
type = NodalVariableValue
nodeid = 5
variable = accum_slip_x
[../]
[./accum_slip_y]
type = NodalVariableValue
nodeid = 5
variable = accum_slip_y
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package -mat_superlu_dist_iterrefine'
petsc_options_value = 'lu superlu_dist 1'
line_search = 'contact'
contact_line_search_allowed_lambda_cuts = 0
contact_line_search_ltol = 0.5
l_max_its = 15
nl_max_its = 10
dt = 0.001
end_time = 0.002
num_steps = 10000
nl_rel_tol = 1e-6
nl_abs_tol = 1e-8
dtmin = 0.001
l_tol = 1e-3
[]
[Outputs]
exodus = true
print_linear_residuals = true
perf_graph = true
csv = true
[./console]
type = Console
max_rows = 5
[../]
[]
[Contact]
[./leftright]
primary = 2
secondary = 3
model = frictionless
formulation = kinematic
penalty = 1e12
normalize_penalty = true
tangential_tolerance = 1e-3
[../]
[]
(modules/contact/test/tests/tension_release/4ElemTensionRelease.i)
[Mesh]
file = 4ElemTensionRelease.e
[]
[GlobalParams]
displacements = 'disp_x disp_y'
volumetric_locking_correction = false
[]
[Functions]
[./up]
type = PiecewiseLinear
x = '0 1 2 3'
y = '0 0.0001 0 -.0001'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = FINITE
[]
[]
[Contact]
[./dummy_name]
primary = 2
secondary = 3
penalty = 1e6
model = frictionless
tangential_tolerance = 0.01
[../]
[]
[BCs]
[./lateral]
type = DirichletBC
variable = disp_x
boundary = '1 4'
value = 0
[../]
[./bottom_up]
type = FunctionDirichletBC
variable = disp_y
boundary = 1
function = up
[../]
[./top]
type = DirichletBC
variable = disp_y
boundary = 4
value = 0.0
[../]
[]
[Materials]
[./stiffStuff1]
type = ComputeIsotropicElasticityTensor
block = '1 2'
youngs_modulus = 1.0e6
poissons_ratio = 0.3
[../]
[./stiffStuff1_stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart'
petsc_options_value = 'hypre boomeramg 101'
line_search = 'none'
nl_rel_tol = 1e-8
nl_abs_tol = 1e-8
l_tol = 1e-4
l_max_its = 100
nl_max_its = 10
dt = 0.2
dtmin = 0.2
end_time = 3
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
[]
[Outputs]
exodus = true
[]
(modules/richards/test/tests/gravity_head_2/gh06.i)
# unsaturated = true
# gravity = true
# supg = false
# transient = true
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
xmin = 0
xmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1E-2 1E-1 1E0 1E1 1E3 1E4 1E5 1E6 1E7'
x = '0 1E-1 1E0 1E1 1E2 1E3 1E4 1E5 1E6'
[../]
[]
[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 = ConstantIC
value = 1
variable = pwater
[../]
[./gas_ic]
type = ConstantIC
value = 2
variable = pgas
[../]
[]
[Kernels]
active = 'richardsfwater richardstwater richardsfgas richardstgas'
[./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
[../]
[./mass_error_gas]
type = FunctionValuePostprocessor
function = fcn_mass_error_g
[../]
[./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((-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 -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-13 1E-10 10000'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
end_time = 1E6
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = gh06
csv = true
[]
(modules/tensor_mechanics/test/tests/shell/dynamics/shell_dynamics_bending_moment_free_orientation_inclined_hht.i)
# Test to verify the fundamental natural frequency of a one element ADComputeShellStress
# BCs: Clamped on one end, free on others.
# Initial perturbation applied to edge of the beam. After that, the shell vibrates freely.
#
# Results have been compared for various thicknesses with the following approximate Results
# (Moose results were obtained with 8 elements along the length)
# Thickness = 0.1. Reference freq: 10.785 Hz, Moose freq: 10.612 Hz
# Thickness = 0.05. Reference freq: 5.393 Hz, Moose freq: 5.335 Hz
# Thickness = 0.025. Reference freq: 2.696 Hz, Moose freq: 2.660 Hz
#
# Reference values have been obtained from Robert Blevins, "Formulas for Dynamics, Acoustics and Vibration",
# Table 5.3 case 11. Formula looks like: f = lambda^2/(2*pi*a^2) * sqrt(E*h^2/(12*(1-nu*nu))), where lambda
# changes as a function of shell dimensions.
# This test uses one single element for speed reasons.
# Here, the shell, instead of being on the XY plane, is oriented at a 45 deg. angle
# with respect to the Y axis.
[Mesh]
type = FileMesh
file = shell_inclined.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[./rot_x]
[../]
[./rot_y]
[../]
[]
[AuxVariables]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yz]
order = CONSTANT
family = MONOMIAL
[../]
# aux variables for dynamics
[./vel_x]
[../]
[./vel_y]
[../]
[./vel_z]
[../]
[./accel_x]
[../]
[./accel_y]
[../]
[./accel_z]
[../]
[./rot_vel_x]
[../]
[./rot_vel_y]
[../]
[./rot_accel_x]
[../]
[./rot_accel_y]
[../]
[]
[AuxKernels]
[./stress_yy]
type = RankTwoAux
variable = stress_yy
rank_two_tensor = global_stress_t_points_0
index_i = 1
index_j = 1
[../]
[./stress_yz]
type = RankTwoAux
variable = stress_yz
rank_two_tensor = global_stress_t_points_0
index_i = 1
index_j = 2
[../]
# Kernels for dynamics
[./accel_x]
type = NewmarkAccelAux
variable = accel_x
displacement = disp_x
velocity = vel_x
beta = 0.25
execute_on = timestep_end
[../]
[./vel_x]
type = NewmarkVelAux
variable = vel_x
acceleration = accel_x
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_y]
type = NewmarkAccelAux
variable = accel_y
displacement = disp_y
velocity = vel_y
beta = 0.25
execute_on = timestep_end
[../]
[./vel_y]
type = NewmarkVelAux
variable = vel_y
acceleration = accel_y
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_z]
type = NewmarkAccelAux
variable = accel_z
displacement = disp_z
velocity = vel_z
beta = 0.25
execute_on = timestep_end
[../]
[./vel_z]
type = NewmarkVelAux
variable = vel_z
acceleration = accel_z
gamma = 0.5
execute_on = timestep_end
[../]
[./rot_accel_x]
type = NewmarkAccelAux
variable = rot_accel_x
displacement = rot_x
velocity = rot_vel_x
beta = 0.25
execute_on = timestep_end
[../]
[./rot_vel_x]
type = NewmarkVelAux
variable = rot_vel_x
acceleration = rot_accel_x
gamma = 0.5
execute_on = timestep_end
[../]
[./rot_accel_y]
type = NewmarkAccelAux
variable = rot_accel_y
displacement = rot_y
velocity = rot_vel_y
beta = 0.25
execute_on = timestep_end
[../]
[./rot_vel_y]
type = NewmarkVelAux
variable = rot_vel_y
acceleration = rot_accel_y
gamma = 0.5
execute_on = timestep_end
[../]
[]
[BCs]
[./fixy1]
type = DirichletBC
variable = disp_y
boundary = '0'
value = 0.0
[../]
[./fixz1]
type = DirichletBC
variable = disp_z
boundary = '0'
value = 0.0
[../]
[./fixr1]
type = DirichletBC
variable = rot_x
boundary = '0'
value = 0.0
[../]
[./fixr2]
type = DirichletBC
variable = rot_y
boundary = '0'
value = 0.0
[../]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = '0'
value = 0.0
[../]
[]
[Functions]
[./force_function]
type = PiecewiseLinear
x = '0.0 0.01 0.15 10.0'
y = '0.0 0.01 0.0 0.0'
[../]
[]
[NodalKernels]
[./force_y2]
type = UserForcingFunctionNodalKernel
variable = disp_z
boundary = '2'
function = force_function
[../]
[]
[Kernels]
[./solid_disp_x]
type = ADStressDivergenceShell
block = '0'
component = 0
variable = disp_x
through_thickness_order = SECOND
[../]
[./solid_disp_y]
type = ADStressDivergenceShell
block = '0'
component = 1
variable = disp_y
through_thickness_order = SECOND
[../]
[./solid_disp_z]
type = ADStressDivergenceShell
block = '0'
component = 2
variable = disp_z
through_thickness_order = SECOND
[../]
[./solid_rot_x]
type = ADStressDivergenceShell
block = '0'
component = 3
variable = rot_x
through_thickness_order = SECOND
[../]
[./solid_rot_y]
type = ADStressDivergenceShell
block = '0'
component = 4
variable = rot_y
through_thickness_order = SECOND
[../]
[./inertial_force_x]
type = ADInertialForceShell
use_displaced_mesh = true
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y'
rotational_accelerations = 'rot_accel_x rot_accel_y'
component = 0
variable = disp_x
thickness = 0.1
eta = 0.0
alpha = 0.0
[../]
[./inertial_force_y]
type = ADInertialForceShell
use_displaced_mesh = true
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y'
rotational_accelerations = 'rot_accel_x rot_accel_y'
component = 1
variable = disp_y
thickness = 0.1
eta = 0.0
alpha = 0.0
[../]
[./inertial_force_z]
type = ADInertialForceShell
use_displaced_mesh = true
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y'
rotational_accelerations = 'rot_accel_x rot_accel_y'
component = 2
variable = disp_z
thickness = 0.1
eta = 0.0
alpha = 0.0
[../]
[./inertial_force_rot_x]
type = ADInertialForceShell
use_displaced_mesh = true
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y'
rotational_accelerations = 'rot_accel_x rot_accel_y'
component = 3
variable = rot_x
thickness = 0.1
eta = 0.0
alpha = 0.0
[../]
[./inertial_force_rot_y]
type = ADInertialForceShell
use_displaced_mesh = true
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y'
rotational_accelerations = 'rot_accel_x rot_accel_y'
component = 4
variable = rot_y
thickness = 0.1
eta = 0.0
alpha = 0.0
[../]
[]
[Materials]
[./elasticity]
type = ADComputeIsotropicElasticityTensorShell
youngs_modulus = 2100000
poissons_ratio = 0.3
block = 0
through_thickness_order = SECOND
[../]
[./strain]
type = ADComputeIncrementalShellStrain
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y'
thickness = 0.1
through_thickness_order = SECOND
[../]
[./stress]
type = ADComputeShellStress
block = 0
through_thickness_order = SECOND
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = 'density'
prop_values = '1.0'
[../]
[]
[Postprocessors]
[./disp_z_tip]
type = PointValue
point = '0.0 1.06 1.06'
variable = disp_z
[../]
[./rot_x_tip]
type = PointValue
point = '0.0 1.06 1.06'
variable = rot_x
[../]
[./stress_yy_el_0]
type = ElementalVariableValue
elementid = 0
variable = stress_yy
[../]
[./stress_yy_el_1]
type = ElementalVariableValue
elementid = 1
variable = stress_yy
[../]
[./stress_yy_el_2]
type = ElementalVariableValue
elementid = 2
variable = stress_yy
[../]
[./stress_yy_el_3]
type = ElementalVariableValue
elementid = 3
variable = stress_yy
[../]
[./stress_yz_el_0]
type = ElementalVariableValue
elementid = 0
variable = stress_yz
[../]
[./stress_yz_el_1]
type = ElementalVariableValue
elementid = 1
variable = stress_yz
[../]
[./stress_yz_el_2]
type = ElementalVariableValue
elementid = 2
variable = stress_yz
[../]
[./stress_yz_el_3]
type = ElementalVariableValue
elementid = 3
variable = stress_yz
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
l_tol = 1e-11
nl_max_its = 15
nl_rel_tol = 1e-11
nl_abs_tol = 1e-10
l_max_its = 20
dt = 0.005
dtmin = 0.005
timestep_tolerance = 2e-13
end_time = 0.5
[./TimeIntegrator]
type = NewmarkBeta
beta = 0.25
gamma = 0.5
[../]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[]
(modules/richards/test/tests/gravity_head_2/gh_lumped_17.i)
# unsaturated = false
# gravity = true
# supg = true
# transient = true
# lumped = true
[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'
viscosity = '1E-3 0.5E-3'
gravity = '-1 0 0'
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1E-2 1E-1 1E0 1E1 1E3 1E4 1E5 1E6 1E7'
x = '0 1E-1 1E0 1E1 1E2 1E3 1E4 1E5 1E6'
[../]
[]
[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 = 0.1
[../]
[./SUPGgas]
type = RichardsSUPGstandard
p_SUPG = 0.01
[../]
[]
[Variables]
[./pwater]
order = FIRST
family = LAGRANGE
[../]
[./pgas]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./water_ic]
type = ConstantIC
value = 1
variable = pwater
[../]
[./gas_ic]
type = ConstantIC
value = 1
variable = pgas
[../]
[]
[Kernels]
active = 'richardsfwater richardstwater richardsfgas richardstgas'
[./richardstwater]
type = RichardsLumpedMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFlux
variable = pwater
[../]
[./richardstgas]
type = RichardsLumpedMassChange
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
[../]
[./mass_error_gas]
type = FunctionValuePostprocessor
function = fcn_mass_error_g
[../]
[./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
[../]
[]
[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((-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'
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
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-15 10000'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
end_time = 1E6
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = gh_lumped_17
csv = true
[]
(modules/xfem/test/tests/init_solution_propagation/init_solution_propagation.i)
# The purpose of this test is to verify that the procedures for initializing
# the solution on nodes/elements affected by XFEM works correctly in both
# serial and parallel.
# The crack cuts near to domain boundaries in parallel, and the displacement
# solution will be wrong in parallel if this is not done correctly. This
# test also has multiple aux variables of various types that are only computed
# on initialization, and which will be wrong if the XFEM initializtion
# is not done correctly.
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[XFEM]
output_cut_plane = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 7
ny = 7
xmin = 0.0
xmax = 25.0
ymin = -12.5
ymax = 12.5
elem_type = QUAD4
[]
[UserObjects]
[./line_seg_cut_set_uo]
type = LineSegmentCutSetUserObject
cut_data ='0.0000e+000 0.0000e+000 5.5000e+000 0.0000e+000 0.0 0.0
5.5000e+000 0.0000e+000 2.5500e+001 0.0000e+000 0.05 1.05'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./const_monomial]
order = CONSTANT
family = MONOMIAL
[../]
[./first_monomial]
order = FIRST
family = MONOMIAL
[../]
[./first_linear]
order = FIRST
family = LAGRANGE
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
planar_formulation = PLANE_STRAIN
[../]
[]
[AuxKernels]
[./const_monomial]
type = FunctionAux
function = 'dummy'
variable = const_monomial
execute_on = 'initial'
[../]
[./first_monomial]
type = FunctionAux
function = 'dummy'
variable = first_monomial
execute_on = 'initial'
[../]
[./first_linear]
type = FunctionAux
function = 'dummy'
variable = first_linear
execute_on = 'initial'
[../]
[]
[Functions]
[./dummy]
type = ParsedFunction
value = 'x*x+y*y'
[../]
[./disp_top_y]
type = PiecewiseLinear
x = '0 1'
y = '0 0.1'
[../]
[]
[BCs]
[./top_y]
type = FunctionDirichletBC
boundary = 2
variable = disp_y
function = disp_top_y
[../]
[./bottom_y]
type = DirichletBC
boundary = 0
variable = disp_y
value = 0.0
[../]
[./right_x]
type = DirichletBC
boundary = 1
variable = disp_x
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
petsc_options = '-snes_ksp_ew'
l_max_its = 100
nl_max_its = 25
nl_rel_tol = 1e-6
nl_abs_tol = 1e-8
start_time = 0.0
dt = 0.1
end_time = 1.0
max_xfem_update = 1
[]
[Outputs]
exodus = true
csv = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/tensor_mechanics/test/tests/domain_integral_thermal/interaction_integral_2d_c.i)
#This problem from [Wilson 1979] tests the thermal strain term in the
#interaction integral
#
#theta_e = 10 degrees C; a = 252; E = 207000; nu = 0.3; alpha = 1.35e-5
#
#With uniform_refine = 3, KI converges to
#KI = 5.602461e+02 (interaction integral)
#KI = 5.655005e+02 (J-integral)
#
#Both are in good agreement with [Shih 1986]:
#average_value = 0.4857 = KI / (sigma_theta * sqrt(pi * a))
#sigma_theta = E * alpha * theta_e / (1 - nu)
# = 207000 * 1.35e-5 * 10 / (1 - 0.3) = 39.9214
#KI = average_value * sigma_theta * sqrt(pi * a) = 5.656e+02
#
#References:
#W.K. Wilson, I.-W. Yu, Int J Fract 15 (1979) 377-387
#C.F. Shih, B. Moran, T. Nakamura, Int J Fract 30 (1986) 79-102
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
volumetric_locking_correction = False
[]
[Mesh]
file = crack2d.e
displacements = 'disp_x disp_y'
# uniform_refine = 3
[]
[AuxVariables]
[./SED]
order = CONSTANT
family = MONOMIAL
[../]
[./SERD]
order = CONSTANT
family = MONOMIAL
[../]
[./temp]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
[./rampConstantUp]
type = PiecewiseLinear
x = '0. 0.1 100.0'
y = '0. 1 1'
scale_factor = -68.95 #MPa
[../]
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
planar_formulation = PLANE_STRAIN
[../]
[]
[AuxKernels]
[./SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[../]
[./SERD]
type = MaterialRealAux
variable = SERD
property = strain_energy_rate_density
execute_on = timestep_end
[../]
[]
[BCs]
[./crack_y]
type = DirichletBC
variable = disp_y
boundary = 100
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = 400
value = 0.0
[../]
[./no_x1]
type = DirichletBC
variable = disp_x
boundary = 900
value = 0.0
[../]
[./Pressure]
[./crack_pressure]
boundary = 700
function = rampConstantUp
[../]
[../]
[] # BCs
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 206800
poissons_ratio = 0.0
[../]
[./radial_return_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'powerlawcrp'
[../]
[./powerlawcrp]
type = PowerLawCreepStressUpdate
coefficient = 3.125e-21 # 7.04e-17 #
n_exponent = 3.0
m_exponent = 0.0
activation_energy = 0.0
[../]
[]
[DomainIntegral]
integrals = 'CIntegral InteractionIntegralKI'
boundary = 800
crack_direction_method = CrackDirectionVector
crack_direction_vector = '1 0 0'
2d = true
axis_2d = 2
radius_inner = '60.0 80.0 100.0 120.0'
radius_outer = '80.0 100.0 120.0 140.0'
symmetry_plane = 1
incremental = true
# interaction integral parameters
block = 1
youngs_modulus = 207000
poissons_ratio = 0.3
inelastic_models = 'powerlawcrp'
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_ksp_type -sub_pc_type -pc_asm_overlap'
petsc_options_value = 'asm 31 preonly lu 1'
line_search = 'none'
l_max_its = 50
nl_max_its = 40
nl_rel_step_tol= 1e-10
nl_rel_tol = 1e-10
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Outputs]
exodus = true
csv = true
[]
[Preconditioning]
active = 'smp'
[./smp]
type = SMP
pc_side = left
ksp_norm = preconditioned
full = true
[../]
[]
(modules/tensor_mechanics/test/tests/generalized_plane_strain/out_of_plane_pressure.i)
# Tests for application of out-of-plane pressure in generalized plane strain.
[Mesh]
[./square]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 2
[../]
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./scalar_strain_zz]
order = FIRST
family = SCALAR
[../]
[]
[AuxVariables]
[./saved_x]
order = FIRST
family = LAGRANGE
[../]
[./saved_y]
order = FIRST
family = LAGRANGE
[../]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Postprocessors]
[./react_z]
type = MaterialTensorIntegral
rank_two_tensor = stress
index_i = 2
index_j = 2
[../]
[]
[Modules]
[./TensorMechanics]
[./GeneralizedPlaneStrain]
[./gps]
use_displaced_mesh = true
displacements = 'disp_x disp_y'
scalar_out_of_plane_strain = scalar_strain_zz
out_of_plane_pressure_function = traction_function
pressure_factor = 1e5
[../]
[../]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = false
displacements = 'disp_x disp_y'
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
[../]
[./strain_xx]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_xx
index_i = 0
index_j = 0
[../]
[./strain_xy]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_xy
index_i = 0
index_j = 1
[../]
[./strain_yy]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_yy
index_i = 1
index_j = 1
[../]
[./strain_zz]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_zz
index_i = 2
index_j = 2
[../]
[]
[Functions]
[./traction_function]
type = PiecewiseLinear
x = '0 2'
y = '0 1'
[../]
[]
[BCs]
[./leftx]
type = DirichletBC
boundary = 3
variable = disp_x
value = 0.0
[../]
[./bottomy]
type = DirichletBC
boundary = 0
variable = disp_y
value = 0.0
[../]
[]
[Materials]
[./elastic_tensor]
type = ComputeIsotropicElasticityTensor
poissons_ratio = 0.3
youngs_modulus = 1e6
[../]
[./strain]
type = ComputePlaneSmallStrain
displacements = 'disp_x disp_y'
scalar_out_of_plane_strain = scalar_strain_zz
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
# This material is not used for anything in the base verison of this test,
# but is used in a variant of the test with cli_args
[./traction_material]
type = GenericFunctionMaterial
prop_names = traction_material
prop_values = traction_function
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
line_search = none
# controls for linear iterations
l_max_its = 100
l_tol = 1e-4
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-14
nl_abs_tol = 1e-11
# time control
start_time = 0.0
dt = 1.0
dtmin = 1.0
end_time = 2.0
num_steps = 5000
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/ad_anisotropic_plasticity/ad_aniso_plasticity_y.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
# Original verification nx = 2, ny = 10, nz = 2
nx = 2
ny = 10
nz = 2
xmin = 0.0
ymin = 0.0
zmin = 0.0
xmax = 1.0
ymax = 10.0
zmax = 1.0
[]
[corner_node]
type = ExtraNodesetGenerator
new_boundary = '100'
nodes = '4 10'
input = gen
[]
[corner_node_2]
type = ExtraNodesetGenerator
new_boundary = '101'
nodes = '1 67'
input = corner_node
[]
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[AuxVariables]
[hydrostatic_stress]
order = CONSTANT
family = MONOMIAL
[]
[plastic_strain_xx]
order = CONSTANT
family = MONOMIAL
[]
[plastic_strain_xy]
order = CONSTANT
family = MONOMIAL
[]
[plastic_strain_yy]
order = CONSTANT
family = MONOMIAL
[]
[stress_yy]
order = CONSTANT
family = MONOMIAL
[]
[elastic_strain_yy]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[hydrostatic_stress]
type = ADRankTwoScalarAux
variable = hydrostatic_stress
rank_two_tensor = stress
scalar_type = Hydrostatic
[]
[plasticity_strain_xx]
type = ADRankTwoAux
rank_two_tensor = trial_plasticity_plastic_strain
variable = plastic_strain_xx
index_i = 0
index_j = 0
[]
[plasticity_strain_xy]
type = ADRankTwoAux
rank_two_tensor = trial_plasticity_plastic_strain
variable = plastic_strain_xy
index_i = 0
index_j = 1
[]
[plasticity_strain_yy]
type = ADRankTwoAux
rank_two_tensor = trial_plasticity_plastic_strain
variable = plastic_strain_yy
index_i = 1
index_j = 1
[]
[elastic_strain_yy]
type = ADRankTwoAux
rank_two_tensor = elastic_strain
variable = elastic_strain_yy
index_i = 1
index_j = 1
[]
[sigma_yy]
type = ADRankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
[]
[]
[Functions]
[pull]
type = PiecewiseLinear
x = '0 1e1 1e8'
y = '0 -4e2 -4e2'
[]
[]
[Modules/TensorMechanics/Master]
[all]
strain = FINITE
use_automatic_differentiation = true
add_variables = true
[]
[]
[Materials]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 70000
poissons_ratio = 0.25
[]
[elastic_strain]
type = ADComputeMultipleInelasticStress
inelastic_models = "trial_plasticity"
max_iterations = 50
absolute_tolerance = 1e-16
[]
[trial_plasticity]
type = ADHillPlasticityStressUpdate
hardening_constant = 2000.0
yield_stress = 0.001
# F G H L M N
hill_constants = "0.5829856 0.364424 0.6342174 2.0691375 2.3492325 1.814589"
absolute_tolerance = 1e-14
relative_tolerance = 1e-12
base_name = trial_plasticity
internal_solve_full_iteration_history = true
max_inelastic_increment = 2.0e-6
internal_solve_output_on = on_error
[]
[]
[BCs]
[no_disp_x]
type = ADDirichletBC
variable = disp_x
boundary = 101
value = 0.0
[]
[no_disp_y]
type = ADDirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[]
[no_disp_z]
type = ADDirichletBC
variable = disp_z
boundary = 100
value = 0.0
[]
[Pressure]
[Side1]
boundary = top
function = pull
[]
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
nl_rel_tol = 1e-11
nl_abs_tol = 1.0e-14
l_max_its = 90
num_steps = 25
[TimeStepper]
type = IterationAdaptiveDT
optimal_iterations = 30
iteration_window = 9
growth_factor = 1.05
cutback_factor = 0.5
timestep_limiting_postprocessor = matl_ts_min
dt = 1e-5
time_t = '0 3.2e-5 10'
time_dt = '1e-5 1.0e-7 1.0e-7'
[]
start_time = 0
automatic_scaling = true
[]
[Postprocessors]
[matl_ts_min]
type = MaterialTimeStepPostprocessor
[]
[max_disp_x]
type = ElementExtremeValue
variable = disp_x
[]
[max_disp_y]
type = ElementExtremeValue
variable = disp_y
[]
[max_hydro]
type = ElementAverageValue
variable = hydrostatic_stress
[]
[dt]
type = TimestepSize
[]
[num_lin]
type = NumLinearIterations
outputs = console
[]
[num_nonlin]
type = NumNonlinearIterations
outputs = console
[]
[plasticity_strain_yy]
type = ElementalVariableValue
variable = plastic_strain_yy
execute_on = 'TIMESTEP_END'
elementid = 39
[]
[elastic_strain_yy]
type = ElementalVariableValue
variable = elastic_strain_yy
execute_on = 'TIMESTEP_END'
elementid = 39
[]
[sigma_yy]
type = ElementalVariableValue
variable = stress_yy
execute_on = 'TIMESTEP_END'
elementid = 39
[]
[]
[Outputs]
csv = true
exodus = true
perf_graph = true
[]
(modules/tensor_mechanics/test/tests/central_difference/lumped/2D/2d_lumped_explicit.i)
# Tests for the central difference time integrator for 2D elements
[Mesh]
[./generated_mesh]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 2
nx = 1
ny = 2
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./accel_x]
[../]
[./vel_x]
[../]
[./accel_y]
[../]
[./vel_y]
[../]
[]
[AuxKernels]
[./accel_x]
type = TestNewmarkTI
variable = accel_x
displacement = disp_x
first = false
[../]
[./vel_x]
type = TestNewmarkTI
variable = vel_x
displacement = disp_x
[../]
[./accel_y]
type = TestNewmarkTI
variable = accel_y
displacement = disp_y
first = false
[../]
[./vel_y]
type = TestNewmarkTI
variable = vel_y
displacement = disp_y
[../]
[]
[Kernels]
[./DynamicTensorMechanics]
displacements = 'disp_x disp_y'
[../]
[./inertia_x]
type = InertialForce
variable = disp_x
[../]
[./inertia_y]
type = InertialForce
variable = disp_y
[../]
[]
[BCs]
[./y_bot]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./x_bot]
type = FunctionDirichletBC
boundary = bottom
variable = disp_x
function = disp
preset = false
[../]
[]
[Functions]
[./disp]
type = PiecewiseLinear
x = '0.0 1.0 2.0 3.0 4.0' # time
y = '0.0 1.0 0.0 -1.0 0.0' # displacement
[../]
[]
[Materials]
[./elasticity_tensor_block]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.25
block = 0
[../]
[./strain_block]
type = ComputeIncrementalSmallStrain
block = 0
displacements = 'disp_x disp_y'
implicit = false
[../]
[./stress_block]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = density
prop_values = 1e4
[../]
[]
[Executioner]
type = Transient
start_time = 0
end_time = 0.1
dt = 0.005
timestep_tolerance = 1e-6
[./TimeIntegrator]
type = CentralDifference
solve_type = lumped
[../]
[]
[Postprocessors]
[./accel_2x]
type = PointValue
point = '1.0 2.0 0.0'
variable = accel_x
[../]
[]
[Outputs]
exodus = false
csv = true
[]
(modules/tensor_mechanics/test/tests/combined_creep_plasticity/combined_stress_prescribed.i)
#
# 1x1x1 unit cube with time-varying pressure on top face
#
# The problem is a one-dimensional creep analysis. The top face has a
# pressure load that is a function of time. The creep strain can be
# calculated analytically. There is no practical active linear
# isotropic plasticity because the yield stress for the plasticity
# model is set to 1e30 MPa, which will not be reached in this
# regression test.
#
# The analytic solution to this problem is:
#
# d ec
# ---- = a*S^b with S = c*t^d
# dt
#
# d ec = a*c^b*t^(b*d) dt
#
# a*c^b
# ec = ----- t^(b*d+1)
# b*d+1
#
# where S = stress
# ec = creep strain
# t = time
# a = constant
# b = constant
# c = constant
# d = constant
#
# With a = 3e-24,
# b = 4,
# c = 1,
# d = 1/2, and
# t = 32400
# we have
#
# S = t^(1/2) = 180
#
# ec = 1e-24*t^3 = 3.4012224e-11
#
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
incremental = true
add_variables = true
generate_output = 'stress_yy creep_strain_yy'
[../]
[]
[Functions]
[./pressure]
type = ParsedFunction
value = 'sqrt(t)'
[../]
[./dts]
type = PiecewiseLinear
y = '1e-2 1e-1 1e0 1e1 1e2'
x = '0 7e-1 7e0 7e1 1e2'
[../]
[]
[BCs]
[./top_pressure]
type = Pressure
variable = disp_y
component = 1
boundary = top
function = pressure
[../]
[./u_bottom_fix]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./u_yz_fix]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./u_xy_fix]
type = DirichletBC
variable = disp_z
boundary = back
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 2.8e7
poissons_ratio = 0.3
[../]
[./creep_plas]
type = ComputeMultipleInelasticStress
inelastic_models = 'creep plas'
tangent_operator = elastic
[../]
[./creep]
type = PowerLawCreepStressUpdate
coefficient = 3.0e-24
n_exponent = 4
m_exponent = 0
activation_energy = 0
[../]
[./plas]
type = IsotropicPlasticityStressUpdate
hardening_constant = 1
yield_stress = 1e30
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
nl_max_its = 100
nl_rel_tol = 1e-10
nl_abs_tol = 1e-7
l_tol = 1e-6
start_time = 0.0
end_time = 32400
dt = 1e-2
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Postprocessors]
[./timestep]
type = TimestepSize
[../]
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_htonly/sphere3D.i)
#
# 3D Spherical Gap Heat Transfer Test.
#
# This test exercises 3D gap heat transfer for a constant conductivity gap.
#
# The mesh consists of an inner solid sphere of radius = 1 unit, and outer
# hollow sphere with an inner radius of 2. In other words, the gap between
# them is 1 radial unit in length.
#
# The conductivity of both spheres is set very large to achieve a uniform
# temperature in each sphere. The temperature of the center node of the
# inner sphere is ramped from 100 to 200 over one time unit. The
# temperature of the outside of the outer, hollow sphere is held fixed
# at 100.
#
# A simple analytical solution is possible for the integrated heat flux
# between the inner and outer spheres:
#
# Integrated Flux = (T_left - T_right) * (gapK/(r^2*((1/r1)-(1/r2)))) * Area
#
# For gapK = 1 (default value)
#
# The area is taken as the area of the secondary (inner) surface:
#
# Area = 4 * pi * 1^2 (4*pi*r^2)
#
# The integrated heat flux across the gap at time 1 is then:
#
# 4*pi*k*delta_T/((1/r1)-(1/r2))
# 4*pi*1*100/((1/1) - (1/2)) = 2513.3 watts
#
# For comparison, see results from the integrated flux post processors.
# This simulation makes use of symmetry, so only 1/8 of the spheres is meshed
# As such, the integrated flux from the post processors is 1/8 of the total,
# or 314.159 watts... i.e. 100*pi.
# The value coming from the post processor is slightly less than this
# but converges as mesh refinement increases.
#
# Simulating contact is challenging. Regression tests that exercise
# contact features can be difficult to solve consistently across multiple
# platforms. While designing these tests, we felt it worth while to note
# some aspects of these tests. The following applies to:
# sphere3D.i, sphere2DRZ.i, cyl2D.i, and cyl3D.i.
# 1. We decided that to perform consistently across multiple platforms we
# would use very small convergence tolerance. In this test we chose an
# nl_rel_tol of 1e-12.
# 2. Due to such a high value for thermal conductivity (used here so that the
# domains come to a uniform temperature) the integrated flux at time = 0
# was relatively large (the value coming from SideIntegralFlux =
# -_diffusion_coef[_qp]*_grad_u[_qp]*_normals[_qp] where the diffusion coefficient
# here is thermal conductivity).
# Even though _grad_u[_qp] is small, in this case the diffusion coefficient
# is large. The result is a number that isn't exactly zero and tends to
# fail exodiff. For this reason the parameter execute_on = initial should not
# be used. That parameter is left to default settings in these regression tests.
#
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
file = sphere3D.e
[]
[Functions]
[./temp]
type = PiecewiseLinear
x = '0 1'
y = '100 200'
[../]
[]
[Variables]
[./temp]
initial_condition = 100
[../]
[]
[AuxVariables]
[./gap_conductance]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./heat_conduction]
type = HeatConduction
variable = temp
[../]
[]
[AuxKernels]
[./gap_cond]
type = MaterialRealAux
property = gap_conductance
variable = gap_conductance
boundary = 2
[../]
[]
[Materials]
[./heat1]
type = HeatConductionMaterial
block = '1 2'
specific_heat = 1.0
thermal_conductivity = 100000000.0
[../]
[]
[ThermalContact]
[./thermal_contact]
type = GapHeatTransfer
variable = temp
primary = 3
secondary = 2
emissivity_primary = 0
emissivity_secondary = 0
gap_conductivity = 1
quadrature = true
gap_geometry_type = SPHERE
sphere_origin = '0 0 0'
[../]
[]
[BCs]
[./mid]
type = FunctionDirichletBC
boundary = 5
variable = temp
function = temp
[../]
[./temp_far_right]
type = DirichletBC
boundary = 4
variable = temp
value = 100
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
dt = 1
dtmin = 0.01
end_time = 1
nl_rel_tol = 1e-12
nl_abs_tol = 1e-7
[./Quadrature]
order = fifth
side_order = seventh
[../]
[]
[Outputs]
exodus = true
[./Console]
type = Console
[../]
[]
[Postprocessors]
[./temp_left]
type = SideAverageValue
boundary = 2
variable = temp
[../]
[./temp_right]
type = SideAverageValue
boundary = 3
variable = temp
[../]
[./flux_left]
type = SideFluxIntegral
variable = temp
boundary = 2
diffusivity = thermal_conductivity
[../]
[./flux_right]
type = SideFluxIntegral
variable = temp
boundary = 3
diffusivity = thermal_conductivity
[../]
[]
(test/tests/geomsearch/2d_moving_penetration/pl_test2qtt.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
file = pl_test2q.e
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
tangential_tolerance = 0.1
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
tangential_tolerance = 0.1
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate10]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate13]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate14]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate15]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate16]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 0.7 -0.7 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1.e-9
l_max_its = 10
start_time = 0.0
dt = 0.05
end_time = 1.0
[./Quadrature]
order = THIRD
[../]
[]
[Outputs]
file_base = pl_test2qtt_out
exodus = true
[]
(modules/combined/test/tests/cavity_pressure/negative_volume.i)
#
# Cavity Pressure Test
#
# This test is designed to compute a negative number of moles
# to trigger an error check in the CavityPressureUserObject.
# The negative number of moles is achieved by supplying an
# open volume to the InternalVolume postprocessor, which
# calculates a negative volume.
[Problem]
coord_type = RZ
[]
[GlobalParams]
displacements = 'disp_r disp_z'
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 2
[]
[Functions]
[./temperature]
type = PiecewiseLinear
x = '0 1'
y = '1 2'
scale_factor = 100
[../]
[]
[Variables]
[./temperature]
initial_condition = 100
[../]
[]
[Modules/TensorMechanics/Master]
[./block]
strain = FINITE
add_variables = true
[../]
[]
[Kernels]
[./heat]
type = Diffusion
variable = temperature
use_displaced_mesh = true
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
variable = disp_r
boundary = left
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_z
boundary = bottom
value = 0.0
[../]
[./temperatureInterior]
type = FunctionDirichletBC
boundary = 2
function = temperature
variable = temperature
[../]
[./CavityPressure]
[./pressure]
boundary = 'top bottom right'
initial_pressure = 10e5
R = 8.3143
output_initial_moles = initial_moles
temperature = aveTempInterior
volume = internalVolume
startup_time = 0.5
output = ppress
[../]
[../]
[]
[Materials]
[./elastic_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress1]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
petsc_options_iname = '-pc_type -sub_pc_type'
petsc_options_value = 'asm lu'
nl_abs_tol = 1e-10
l_max_its = 20
dt = 0.5
end_time = 1.0
[]
[Postprocessors]
[./internalVolume]
type = InternalVolume
boundary = 'top bottom right'
execute_on = 'initial linear'
[../]
[./aveTempInterior]
type = AxisymmetricCenterlineAverageValue
boundary = left
variable = temperature
execute_on = 'initial linear'
[../]
[]
[Outputs]
exodus = false
[]
(modules/tensor_mechanics/test/tests/substepping/ad_power_law_creep.i)
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
nx = 2
ny = 2
nz = 2
[../]
[]
[AuxVariables]
[./temp]
initial_condition = 1000.0
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_zz elastic_strain_zz creep_strain_zz'
use_automatic_differentiation = true
[../]
[]
[Functions]
[./front_pull]
type = PiecewiseLinear
x = '0 1'
y = '0 1'
scale_factor = 0.5
[../]
[]
[BCs]
[./u_front_pull]
type = ADFunctionDirichletBC
variable = disp_z
boundary = front
function = front_pull
[../]
[./uz_back_fix]
type = ADDirichletBC
variable = disp_z
boundary = back
value = 0.0
[../]
[./u_yz_fix]
type = ADDirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./u_xz_fix]
type = ADDirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 2e11
poissons_ratio = 0.3
[../]
[./radial_return_stress]
type = ADComputeMultipleInelasticStress
inelastic_models = 'power_law_creep'
[../]
[./power_law_creep]
type = ADPowerLawCreepStressUpdate
coefficient = 1.0e-15
n_exponent = 4
activation_energy = 0.0
temperature = temp
# options for using substepping
use_substep = true
substep_strain_tolerance = 0.1
max_inelastic_increment = 0.01
[../]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type '
petsc_options_value = 'lu '
line_search = 'none'
nl_max_its = 10
nl_rel_tol = 1e-6
nl_abs_tol = 1e-10
end_time = 0.1
dt = 0.1
[]
[Outputs]
exodus = true
[]
(test/tests/geomsearch/2d_moving_penetration/pl_test4q.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
file = pl_test4q.e
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate10]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate13]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate14]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate15]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate16]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1.e-9
l_max_its = 10
start_time = 0.0
dt = 0.02
end_time = 1.0
[./Quadrature]
order = THIRD
[../]
[]
[Outputs]
file_base = pl_test4q_out
exodus = true
[]
(modules/tensor_mechanics/test/tests/truss/truss_hex_action.i)
# This test is designed to check
# whether truss element works well with other multi-dimensional element
# e.g. the hex element in this case, by assigning different block number
# to different types of elements.
[Mesh]
type = FileMesh
file = truss_hex.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./axial_stress]
order = CONSTANT
family = MONOMIAL
[../]
[./e_over_l]
order = CONSTANT
family = MONOMIAL
[../]
[./area]
order = CONSTANT
family = MONOMIAL
[../]
[./react_x]
order = FIRST
family = LAGRANGE
[../]
[./react_y]
order = FIRST
family = LAGRANGE
[../]
[./react_z]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
[./x2]
type = PiecewiseLinear
x = '0 1 2 3'
y = '0 .5 1 1'
[../]
[./y2]
type = PiecewiseLinear
x = '0 1 2 3'
y = '0 0 .5 1'
[../]
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./fixy1]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./fixz1]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0
[../]
[./fixx2]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./fixz2]
type = DirichletBC
variable = disp_z
boundary = 2
value = 0
[../]
[./fixDummyHex_x]
type = DirichletBC
variable = disp_x
boundary = 1000
value = 0
[../]
[./fixDummyHex_y]
type = DirichletBC
variable = disp_y
boundary = 1000
value = 0
[../]
[./fixDummyHex_z]
type = DirichletBC
variable = disp_z
boundary = 1000
value = 0
[../]
[]
[DiracKernels]
[./pull]
type = ConstantPointSource
value = -25
point = '0 -2 0'
variable = disp_y
[../]
[]
[AuxKernels]
[./axial_stress]
type = MaterialRealAux
block = '1 2'
property = axial_stress
variable = axial_stress
[../]
[./e_over_l]
type = MaterialRealAux
block = '1 2'
property = e_over_l
variable = e_over_l
[../]
[./area1]
type = ConstantAux
block = 1
variable = area
value = 1.0
execute_on = 'initial timestep_begin'
[../]
[./area2]
type = ConstantAux
block = 2
variable = area
value = 0.25
execute_on = 'initial timestep_begin'
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
petsc_options_iname = '-pc_type -ksp_gmres_restart'
petsc_options_value = 'jacobi 101'
nl_max_its = 15
nl_rel_tol = 1e-8
nl_abs_tol = 1e-10
dt = 1
num_steps = 1
end_time = 1
[]
[Kernels]
[./TensorMechanics]
block = 1000
displacements = 'disp_x disp_y disp_z'
[../]
[]
[Modules/TensorMechanics/LineElementMaster]
[./block]
truss = true
displacements = 'disp_x disp_y disp_z'
area = area
block = '1 2'
save_in = 'react_x react_y react_z'
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = 1000
youngs_modulus = 1e6
poissons_ratio = 0
[../]
[./strain]
type = ComputeSmallStrain
block = 1000
displacements = 'disp_x disp_y disp_z'
[../]
[./stress]
type = ComputeLinearElasticStress
block = 1000
[../]
[./linelast]
type = LinearElasticTruss
block = '1 2'
displacements = 'disp_x disp_y disp_z'
youngs_modulus = 1e6
[../]
[]
[Outputs]
file_base = 'truss_hex_out'
exodus = true
[]
(modules/xfem/test/tests/second_order_elements/diffusion_2d_quad8.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 3
ny = 4
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD8
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.35 1.0 0.35 0.2'
time_start_cut = 0.0
time_end_cut = 2.0
[../]
[]
[Variables]
[./u]
[../]
[]
[Functions]
[./u_left]
type = PiecewiseLinear
x = '0 2'
y = '0 0.1'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = FunctionDirichletBC
variable = u
boundary = 3
function = u_left
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Transient
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
start_time = 0.0
dt = 1.0
end_time = 2.0
[]
[Outputs]
interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/combined/test/tests/cavity_pressure/initial_temperature.i)
#
# Cavity Pressure Test
#
# This test is designed to compute an internal pressure based on
# p = n * R * T / V
# where
# p is the pressure
# n is the amount of material in the volume (moles)
# R is the universal gas constant
# T is the temperature
# V is the volume
#
# The mesh is composed of one block (1) with an interior cavity of volume 8.
# Block 2 sits in the cavity and has a volume of 1. Thus, the total
# initial volume is 7.
# The test adjusts n, T, and V in the following way:
# n => n0 + alpha * t
# T => T0 + beta * t
# V => V0 + gamma * t
# with
# alpha = n0
# beta = T0 / 2
# gamma = -(0.003322259...) * V0
# T0 = 240.54443866068704
# V0 = 7
# n0 = f(p0)
# p0 = 100
# R = 8.314472 J * K^(-1) * mol^(-1)
#
# So, n0 = p0 * V0 / R / T0 = 100 * 7 / 8.314472 / 240.544439
# = 0.35
#
# The parameters combined at t = 1 gives p = 301.
#
# This test sets the initial temperature to 500, but the CavityPressure
# is told that that initial temperature is T0. Thus, the final solution
# is unchanged.
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
file = 3d.e
[]
[GlobalParams]
volumetric_locking_correction = true
[]
[Functions]
[./displ_positive]
type = PiecewiseLinear
x = '0 1'
y = '0 0.0029069767441859684'
[../]
[./displ_negative]
type = PiecewiseLinear
x = '0 1'
y = '0 -0.0029069767441859684'
[../]
[./temp1]
type = PiecewiseLinear
x = '0 1'
y = '1 1.5'
scale_factor = 240.54443866068704
[../]
[./material_input_function]
type = PiecewiseLinear
x = '0 1'
y = '0 0.35'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[./temp]
initial_condition = 500
[../]
[./material_input]
[../]
[]
[AuxVariables]
[./pressure_residual_x]
[../]
[./pressure_residual_y]
[../]
[./pressure_residual_z]
[../]
[./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_zx]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
[../]
[./heat]
type = Diffusion
variable = temp
use_displaced_mesh = true
[../]
[./material_input_dummy]
type = Diffusion
variable = material_input
use_displaced_mesh = true
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 0
variable = stress_xx
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 1
variable = stress_yy
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 2
variable = stress_zz
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 1
variable = stress_xy
[../]
[./stress_yz]
type = RankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 2
variable = stress_yz
[../]
[./stress_zx]
type = RankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 0
variable = stress_zx
[../]
[]
[BCs]
[./no_x_exterior]
type = DirichletBC
variable = disp_x
boundary = '7 8'
value = 0.0
[../]
[./no_y_exterior]
type = DirichletBC
variable = disp_y
boundary = '9 10'
value = 0.0
[../]
[./no_z_exterior]
type = DirichletBC
variable = disp_z
boundary = '11 12'
value = 0.0
[../]
[./prescribed_left]
type = FunctionDirichletBC
variable = disp_x
boundary = 13
function = displ_positive
[../]
[./prescribed_right]
type = FunctionDirichletBC
variable = disp_x
boundary = 14
function = displ_negative
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = '15 16'
value = 0.0
[../]
[./no_z]
type = DirichletBC
variable = disp_z
boundary = '17 18'
value = 0.0
[../]
[./no_x_interior]
type = DirichletBC
variable = disp_x
boundary = '1 2'
value = 0.0
[../]
[./no_y_interior]
type = DirichletBC
variable = disp_y
boundary = '3 4'
value = 0.0
[../]
[./no_z_interior]
type = DirichletBC
variable = disp_z
boundary = '5 6'
value = 0.0
[../]
[./temperatureInterior]
type = FunctionDirichletBC
boundary = 100
function = temp1
variable = temp
[../]
[./MaterialInput]
type = FunctionDirichletBC
boundary = '100 13 14 15 16'
function = material_input_function
variable = material_input
[../]
[./CavityPressure]
[./1]
boundary = 100
initial_pressure = 100
material_input = materialInput
R = 8.314472
temperature = aveTempInterior
initial_temperature = 240.54443866068704
volume = internalVolume
startup_time = 0.5
output = ppress
save_in = 'pressure_residual_x pressure_residual_y pressure_residual_z'
[../]
[../]
[]
[Materials]
[./elast_tensor1]
type = ComputeElasticityTensor
C_ijkl = '0 5'
fill_method = symmetric_isotropic
block = 1
[../]
[./strain1]
type = ComputeFiniteStrain
block = 1
[../]
[./stress1]
type = ComputeFiniteStrainElasticStress
block = 1
[../]
[./elast_tensor2]
type = ComputeElasticityTensor
C_ijkl = '0 5'
fill_method = symmetric_isotropic
block = 2
[../]
[./strain2]
type = ComputeFiniteStrain
block = 2
[../]
[./stress2]
type = ComputeFiniteStrainElasticStress
block = 2
[../]
[]
[Executioner]
type = Transient
petsc_options_iname = '-pc_type -sub_pc_type'
petsc_options_value = 'asm lu'
nl_rel_tol = 1e-12
l_tol = 1e-12
l_max_its = 20
dt = 0.5
end_time = 1.0
[]
[Postprocessors]
[./internalVolume]
type = InternalVolume
boundary = 100
execute_on = 'initial linear'
[../]
[./aveTempInterior]
type = SideAverageValue
boundary = 100
variable = temp
execute_on = 'initial linear'
[../]
[./materialInput]
type = SideAverageValue
boundary = '7 8 9 10 11 12'
variable = material_input
execute_on = linear
[../]
[]
[Outputs]
exodus = true
[]
(modules/richards/test/tests/buckley_leverett/bl22_lumped.i)
# two-phase version
# super-sharp front version
[Mesh]
type = GeneratedMesh
dim = 1
nx = 150
xmin = 0
xmax = 15
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = 'DensityWater DensityGas'
relperm_UO = 'RelPermWater RelPermGas'
SUPG_UO = 'SUPGwater SUPGgas'
sat_UO = 'SatWater SatGas'
seff_UO = 'SeffWater SeffGas'
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1E-4 1E-3 1E-2 2E-2 5E-2 6E-2 0.1 0.2'
x = '0 1E-2 1E-1 1 5 20 40 41'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = 'pwater pgas'
[../]
[./DensityWater]
type = RichardsDensityConstBulk
dens0 = 1000
bulk_mod = 2E6
[../]
[./DensityGas]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 2E6
[../]
[./SeffWater]
type = RichardsSeff2waterVG
m = 0.8
al = 1E-4
[../]
[./SeffGas]
type = RichardsSeff2gasVG
m = 0.8
al = 1E-4
[../]
[./RelPermWater]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./RelPermGas]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./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 = 1E-5
[../]
[./SUPGgas]
type = RichardsSUPGstandard
p_SUPG = 1E-5
[../]
[]
[Variables]
[./pwater]
order = FIRST
family = LAGRANGE
[../]
[./pgas]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[./bounds_dummy]
[../]
[]
[Kernels]
active = 'richardsfwater richardstwater richardsfgas richardstgas'
[./richardstwater]
type = RichardsLumpedMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFlux
variable = pwater
[../]
[./richardstgas]
type = RichardsLumpedMassChange
variable = pgas
[../]
[./richardsfgas]
type = RichardsFlux
variable = pgas
[../]
[./richardsppenalty]
type = RichardsPPenalty
variable = pgas
a = 1E-18
lower_var = pwater
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = SeffWater
pressure_vars = 'pwater pgas'
[../]
[]
[ICs]
[./water_ic]
type = FunctionIC
variable = pwater
function = initial_water
[../]
[./gas_ic]
type = FunctionIC
variable = pgas
function = initial_gas
[../]
[]
[BCs]
[./left_w]
type = DirichletBC
variable = pwater
boundary = left
value = 1E6
[../]
[./left_g]
type = DirichletBC
variable = pgas
boundary = left
value = 1000
[../]
[./right_w]
type = DirichletBC
variable = pwater
boundary = right
value = -100000
[../]
[./right_g]
type = DirichletBC
variable = pgas
boundary = right
value = 0
[../]
[]
[Functions]
[./initial_water]
type = ParsedFunction
value = 1000000*(1-min(x/5,1))-if(x<5,0,100000)
[../]
[./initial_gas]
type = ParsedFunction
value = 1000
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.15
mat_permeability = '1E-10 0 0 0 1E-10 0 0 0 1E-10'
viscosity = '1E-3 1E-6'
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./standard]
type = SMP
full = true
petsc_options = '-snes_converged_reason -ksp_diagonal_scale -ksp_diagonal_scale_fix -ksp_gmres_modifiedgramschmidt'
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -sub_pc_factor_shift_type -pc_asm_overlap -snes_atol -snes_rtol -snes_max_it -ksp_rtol -ksp_atol'
petsc_options_value = 'gmres asm lu NONZERO 2 1E-10 1E-10 20 1E-10 1E-100'
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
end_time = 50
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = bl22_lumped
[./exodus]
type = Exodus
interval = 100000
hide = 'pgas bounds_dummy'
execute_on = 'initial final timestep_end'
[../]
[]
(modules/combined/examples/xfem/xfem_mechanics_prescribed_growth.i)
# This is a demonstration of a simple mechanics simulation using XFEM
# to represent a single crack that is prescribed to propagate along
# a line over time.
[GlobalParams]
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 11
ny = 11
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[XFEM]
geometric_cut_userobjects = 'line_seg_cut_uo'
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '1.0 0.5 0.1 0.5'
time_start_cut = 0.0
time_end_cut = 8.0
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
planar_formulation = plane_strain
add_variables = true
[../]
[]
[Functions]
[./pull]
type = PiecewiseLinear
x='0 50'
y='0 0.02'
[../]
[]
[BCs]
[./bottomx]
type = DirichletBC
boundary = bottom
variable = disp_x
value = 0.0
[../]
[./bottomy]
type = DirichletBC
boundary = bottom
variable = disp_y
value = 0.0
[../]
[./topx]
type = DirichletBC
boundary = top
variable = disp_x
value = 0.0
[../]
[./topy]
type = FunctionDirichletBC
boundary = top
variable = disp_y
function = pull
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./_elastic_strain]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-14
nl_abs_tol = 1e-9
# time control
start_time = 0.0
dt = 1.0
end_time = 10.0
max_xfem_update = 5
[]
[Outputs]
exodus = true
execute_on = timestep_end
[./console]
type = Console
output_linear = true
[../]
[]
(modules/contact/test/tests/hertz_spherical/hertz_contact.i)
# Hertz Contact: Sphere on sphere
# Spheres have the same radius, Young's modulus, and Poisson's ratio.
# Define E:
# 1/E = (1-nu1^2)/E1 + (1-nu2^2)/E2
#
# Effective radius R:
# 1/R = 1/R1 + 1/R2
#
# F is the applied compressive load.
#
# Area of contact a::
# a^3 = 3FR/4E
#
# Depth of indentation d:
# d = a^2/R
#
#
# Let R1 = R2 = 2. Then R = 1.
#
# Let nu1 = nu2 = 0.25, E1 = E2 = 1.40625e7. Then E = 7.5e6.
#
# Let F = 10000. Then a = 0.1, d = 0.01.
#
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[Mesh]#Comment
file = hertz_contact.e
[] # Mesh
[Functions]
[./pressure]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 1.'
scale_factor = 795.77471545947674 # 10000/pi/2^2
[../]
[./disp_y]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. -0.01 -0.01'
[../]
[] # Functions
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[] # Variables
[AuxVariables]
[./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_zx]
order = CONSTANT
family = MONOMIAL
[../]
[./vonmises]
order = CONSTANT
family = MONOMIAL
[../]
[./hydrostatic]
order = CONSTANT
family = MONOMIAL
[../]
[] # AuxVariables
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = SMALL
# extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 0
variable = stress_xx
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 1
variable = stress_yy
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 2
variable = stress_zz
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 1
variable = stress_xy
[../]
[./stress_yz]
type = RankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 2
variable = stress_yz
[../]
[./stress_zx]
type = RankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 0
variable = stress_zx
[../]
[] # AuxKernels
[BCs]
[./base_x]
type = DirichletBC
variable = disp_x
boundary = 1000
value = 0.0
[../]
[./base_y]
type = DirichletBC
variable = disp_y
boundary = 1000
value = 0.0
[../]
[./base_z]
type = DirichletBC
variable = disp_z
boundary = 1000
value = 0.0
[../]
[./symm_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./symm_z]
type = DirichletBC
variable = disp_z
boundary = 3
value = 0.0
[../]
[./disp_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[] # BCs
[Contact]
[./dummy_name]
primary = 1000
secondary = 100
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+10
[../]
[]
[Materials]
[./tensor]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1.40625e7
poissons_ratio = 0.25
[../]
[./stress]
type = ComputeLinearElasticStress
block = '1'
[../]
[./tensor_1000]
type = ComputeIsotropicElasticityTensor
block = '1000'
youngs_modulus = 1e6
poissons_ratio = 0.0
[../]
[./stress_1000]
type = ComputeLinearElasticStress
block = '1000'
[../]
[] # Materials
[Preconditioning]
[./SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-7
l_max_its = 200
start_time = 0.0
dt = 0.5
end_time = 2.0
[] # Executioner
[Postprocessors]
[./maxdisp]
type = NodalVariableValue
nodeid = 122 # 123-1 where 123 is the exodus node number of the top-center node
variable = disp_y
[../]
[]
[Outputs]
[./out]
type = Exodus
[../]
[] # Outputs
(modules/richards/test/tests/dirac/bh_fu_05.i)
# unsaturated
# injection
# fullyupwind
[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
sat_UO = Saturation
seff_UO = Seff1VG
SUPG_UO = SUPGstandard
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '500 500 1E1'
x = '4000 5000 6500'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1000
bulk_mod = 2E9
[../]
[./Seff1VG]
type = RichardsSeff1VG
m = 0.8
al = 1E-5
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0
sum_s_res = 0
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 1E8
[../]
[./borehole_total_outflow_mass]
type = RichardsSumQuantity
[../]
[]
[Variables]
active = 'pressure'
[./pressure]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./p_ic]
type = FunctionIC
variable = pressure
function = initial_pressure
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[Kernels]
active = 'richardsf richardst'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[DiracKernels]
[./bh]
type = RichardsBorehole
bottom_pressure = 0
point_file = bh03.bh
SumQuantityUO = borehole_total_outflow_mass
variable = pressure
unit_weight = '0 0 0'
character = -1
fully_upwind = true
[../]
[]
[Postprocessors]
[./bh_report]
type = RichardsPlotQuantity
uo = borehole_total_outflow_mass
[../]
[./fluid_mass0]
type = RichardsMass
variable = pressure
execute_on = timestep_begin
[../]
[./fluid_mass1]
type = RichardsMass
variable = pressure
execute_on = timestep_end
[../]
[./zmass_error]
type = FunctionValuePostprocessor
function = mass_bal_fcn
execute_on = timestep_end
[../]
[./p0]
type = PointValue
variable = pressure
point = '1 1 1'
execute_on = timestep_end
[../]
[]
[Functions]
[./initial_pressure]
type = ParsedFunction
value = -2E5
[../]
[./mass_bal_fcn]
type = ParsedFunction
value = abs((a-c+d)/2/(a+c))
vars = 'a c d'
vals = 'fluid_mass1 fluid_mass0 bh_report'
[../]
[]
[Materials]
[./all]
type = RichardsMaterial
block = 0
viscosity = 1E-3
mat_porosity = 0.1
mat_permeability = '1E-12 0 0 0 1E-12 0 0 0 1E-12'
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = Seff1VG
pressure_vars = pressure
[../]
[]
[Preconditioning]
[./usual]
type = SMP
full = true
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -ksp_max_it'
petsc_options_value = 'bcgs bjacobi 1E-10 1E-10 10000 30'
[../]
[]
[Executioner]
type = Transient
end_time = 6500
solve_type = NEWTON
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = bh_fu_05
exodus = false
csv = true
execute_on = timestep_end
[]
(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
[]
(modules/xfem/test/tests/second_order_elements/diffusion_3d_hex27.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 3
ny = 4
nz = 2
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
zmin = 0.0
zmax = 0.2
elem_type = HEX27
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./square_planar_cut_uo]
type = RectangleCutUserObject
cut_data = ' 0.35 1.01 -0.001
0.35 0.49 -0.001
0.35 0.49 0.201
0.35 1.01 0.201'
[../]
[]
[Variables]
[./u]
[../]
[]
[Functions]
[./u_left]
type = PiecewiseLinear
x = '0 2'
y = '0 0.1'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = FunctionDirichletBC
variable = u
boundary = left
function = u_left
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 0
[../]
[]
[Executioner]
type = Transient
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
start_time = 0.0
dt = 1.0
end_time = 1.0
[]
[Outputs]
interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/xfem/test/tests/moving_interface/moving_level_set.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
xmin = 0
xmax = 1
ymin = 0
ymax = 1
elem_type = QUAD4
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutSetUserObject
cut_data = '0.3 1.0 0.3 0.2 0 3'
heal_always = false
[../]
[./level_set_cut_uo]
type = LevelSetCutUserObject
level_set_var = ls
heal_always = true
[../]
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./ls]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./ls_function]
type = FunctionAux
variable = ls
function = ls_func
[../]
[]
[Functions]
[./u_left]
type = PiecewiseLinear
x = '0 2'
y = '3 5'
[../]
[./ls_func]
type = ParsedFunction
value = 'x-0.7-0.07*(t-1)'
[../]
[]
[Constraints]
[./u_constraint]
type = XFEMSingleVariableConstraint
geometric_cut_userobject = 'level_set_cut_uo'
use_displaced_mesh = false
variable = u
use_penalty = true
alpha = 1e5
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = DirichletBC
variable = u
boundary = 3
value = 3
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
# petsc_options_iname = '-pc_type -pc_hypre_type'
# petsc_options_value = 'hypre boomeramg'
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
line_search = 'none'
l_tol = 1e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-9
start_time = 0.0
dt = 1
end_time = 3.0
max_xfem_update = 1
[]
[Outputs]
interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/tensor_mechanics/test/tests/truss/truss_2d_action.i)
#
# Truss in two dimensional space
#
# The truss is made of five equilateral triangles supported at each end.
# The truss starts at (0,0). At (1,0), there is a point load of 25.
# The reactions are therefore
# Ryleft = 2/3 * 25 = 16.7
# Ryright = 1/3 * 25 = 8.33
# The area of each member is 0.8.
# Statics gives the stress in each member. For example, for element 6 (from
# (0,0) to (1/2,sqrt(3)/2)), the force is
# f = 2/3 * 25 * 2/sqrt(3) = 100/3/sqrt(3) (compressive)
# and the stress is
# s = -100/3/sqrt(3)/0.8 = -24.06
#
[Mesh]
type = FileMesh
file = truss_2d.e
displacements = 'disp_x disp_y'
[]
[AuxVariables]
[./axial_stress]
order = CONSTANT
family = MONOMIAL
[../]
[./e_over_l]
order = CONSTANT
family = MONOMIAL
[../]
[./area]
order = CONSTANT
family = MONOMIAL
[../]
[./react_x]
order = FIRST
family = LAGRANGE
[../]
[./react_y]
order = FIRST
family = LAGRANGE
[../]
[./react_z]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
[./x2]
type = PiecewiseLinear
x = '0 1 2 3'
y = '0 .5 1 1'
[../]
[./y2]
type = PiecewiseLinear
x = '0 1 2 3'
y = '0 0 .5 1'
[../]
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./fixy1]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./fixy4]
type = DirichletBC
variable = disp_y
boundary = 4
value = 0
[../]
[]
[DiracKernels]
[./pull]
type = ConstantPointSource
value = -25
point = '1 0 0'
variable = disp_y
[../]
[]
[AuxKernels]
[./axial_stress]
type = MaterialRealAux
block = 1
property = axial_stress
variable = axial_stress
[../]
[./e_over_l]
type = MaterialRealAux
block = 1
property = e_over_l
variable = e_over_l
[../]
[./area]
type = ConstantAux
block = 1
variable = area
value = 0.8
execute_on = 'initial timestep_begin'
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
petsc_options_iname = '-pc_type -ksp_gmres_restart'
petsc_options_value = 'jacobi 101'
nl_max_its = 15
nl_rel_tol = 1e-8
nl_abs_tol = 1e-10
dt = 1
num_steps = 1
end_time = 1
[]
[Modules/TensorMechanics/LineElementMaster]
[./block]
truss = true
add_variables = true
displacements = 'disp_x disp_y'
# area = area # commented out for error check
block = 1
save_in = 'react_x react_y'
[../]
[]
[Materials]
[./linelast]
type = LinearElasticTruss
block = 1
youngs_modulus = 1e6
displacements = 'disp_x disp_y'
[../]
[]
[Outputs]
file_base = 'truss_2d_out'
exodus = true
[]
(modules/xfem/test/tests/solid_mechanics_basic/crack_propagation_2d.i)
[GlobalParams]
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
use_crack_growth_increment = true
crack_growth_increment = 0.2
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 11
ny = 11
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '1.0 0.5 0.7 0.5'
time_start_cut = 0.0
time_end_cut = 0.0
[../]
[./xfem_marker_uo]
type = XFEMRankTwoTensorMarkerUserObject
execute_on = timestep_end
tensor = stress
scalar_type = MaxPrincipal
threshold = 5e+1
average = true
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
planar_formulation = plane_strain
add_variables = true
[../]
[]
[Functions]
[./pull]
type = PiecewiseLinear
x='0 50 100'
y='0 0.02 0.1'
[../]
[]
[BCs]
[./bottomx]
type = DirichletBC
boundary = bottom
variable = disp_x
value = 0.0
[../]
[./bottomy]
type = DirichletBC
boundary = bottom
variable = disp_y
value = 0.0
[../]
[./topx]
type = DirichletBC
boundary = top
variable = disp_x
value = 0.0
[../]
[./topy]
type = FunctionDirichletBC
boundary = top
variable = disp_y
function = pull
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
block = 0
[../]
[./_elastic_strain]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-14
nl_abs_tol = 1e-9
# time control
start_time = 0.0
dt = 1.0
end_time = 2.0
num_steps = 5000
max_xfem_update = 1
[]
[Outputs]
file_base = crack_propagation_2d_out
exodus = true
execute_on = timestep_end
[./console]
type = Console
output_linear = true
[../]
[]
(modules/combined/test/tests/internal_volume/rz_displaced_quad8.i)
#
# Volume Test
#
# This test is designed to compute the volume of a space when displacements
# are imposed.
#
# The mesh is composed of one block (1) with two elements. The mesh is
# such that the initial volume is 1. One element face is displaced to
# produce a final volume of 2.
#
# r1
# +----+ -
# | | |
# +----+ h V1 = pi * h * r1^2
# | | |
# +----+ -
#
# becomes
#
# +----+
# | \
# +------+ v2 = pi * h/2 * ( r2^2 + 1/3 * ( r2^2 + r2*r1 + r1^2 ) )
# | |
# +------+
# r2
#
# r1 = 1
# r2 = 1.5380168369562588
# h = 1/pi
#
# Note: Because the InternalVolume PP computes cavity volumes as positive,
# the volumes reported are negative.
#
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Problem]
coord_type = RZ
[]
[Mesh]
file = meshes/rz_displaced_quad8.e
displacements = 'disp_x disp_y'
[]
[Functions]
[./disp_x]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 0.5380168369562588'
[../]
[./disp_x2]
type = PiecewiseLinear
scale_factor = 0.5
x = '0. 1.'
y = '0. 0.5380168369562588'
[../]
[]
[Variables]
[./disp_x]
order = SECOND
family = LAGRANGE
[../]
[./disp_y]
order = SECOND
family = LAGRANGE
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
volumetric_locking_correction = false
decomposition_method = EigenSolution
incremental = true
strain = FINITE
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = 2
value = 0.0
[../]
[./x]
type = FunctionDirichletBC
boundary = 3
variable = disp_x
function = disp_x
[../]
[./x2]
type = FunctionDirichletBC
boundary = 4
variable = disp_x
function = disp_x2
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
start_time = 0.0
dt = 1.0
end_time = 1.0
[./Quadrature]
order = THIRD
[../]
[]
[Postprocessors]
[./internalVolume]
type = InternalVolume
boundary = 2
execute_on = 'initial timestep_end'
[../]
[]
[Outputs]
exodus = true
csv = true
[]
(modules/geochemistry/test/tests/kinetics/quartz_dissolution.i)
# Example of quartz dissolution.
[TimeDependentReactionSolver]
model_definition = definition
geochemistry_reactor_name = reactor
charge_balance_species = "Cl-"
constraint_species = "H2O H+ Cl- SiO2(aq)"
constraint_value = " 1.0 1E-10 1E-10 1E-9"
constraint_meaning = "kg_solvent_water bulk_composition bulk_composition free_concentration"
constraint_unit = " kg moles moles molal"
initial_temperature = 100.0
temperature = 100.0
kinetic_species_name = Quartz
kinetic_species_initial_value = 5
kinetic_species_unit = kg
ramp_max_ionic_strength_initial = 0 # max_ionic_strength in such a simple problem does not need ramping
stoichiometric_ionic_str_using_Cl_only = true # for comparison with GWB
execute_console_output_on = '' # only CSV output for this example
[]
[UserObjects]
[rate_quartz]
type = GeochemistryKineticRate
kinetic_species_name = Quartz
intrinsic_rate_constant = 1.728E-10 # 2.0E-15mol/s/cm^2 = 1.728E-10mol/day/cm^2
multiply_by_mass = true
area_quantity = 1000
[]
[definition]
type = GeochemicalModelDefinition
database_file = "../../../database/moose_geochemdb.json"
basis_species = "H2O SiO2(aq) H+ Cl-"
kinetic_minerals = "Quartz"
kinetic_rate_descriptions = "rate_quartz"
piecewise_linear_interpolation = true # for comparison with GWB
[]
[]
[Functions]
[timestepper]
type = PiecewiseLinear
x = '0 0.5 3'
y = '0.01 0.05 0.1'
[]
[]
[Executioner]
type = Transient
[TimeStepper]
type = FunctionDT
function = timestepper
[]
end_time = 5.0
[]
[AuxVariables]
[diss]
[]
[]
[AuxKernels]
[diss]
type = ParsedAux
args = moles_Quartz
function = '83.216414271 - moles_Quartz'
variable = diss
[]
[]
[Postprocessors]
[dissolved_moles]
type = PointValue
point = '0 0 0'
variable = diss
[]
[]
[Outputs]
csv = true
[]
(modules/richards/test/tests/dirac/bh_fu_07.i)
#fullyupwind
[Mesh]
type = FileMesh
file = bh07_input.e
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = DensityConstBulk
relperm_UO = RelPermPower
sat_UO = Saturation
seff_UO = Seff1VG
SUPG_UO = SUPGstandard
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1000 10000'
x = '100 1000'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1000
bulk_mod = 2E9
[../]
[./Seff1VG]
type = RichardsSeff1VG
m = 0.8
al = 1E-5
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0
sum_s_res = 0
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 1E8
[../]
[./borehole_total_outflow_mass]
type = RichardsSumQuantity
[../]
[]
[Variables]
active = 'pressure'
[./pressure]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./p_ic]
type = FunctionIC
variable = pressure
function = initial_pressure
[../]
[]
[BCs]
[./fix_outer]
type = DirichletBC
boundary = perimeter
variable = pressure
value = 1E7
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[Kernels]
active = 'richardsf richardst'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFullyUpwindFlux
variable = pressure
[../]
[]
[DiracKernels]
[./bh]
type = RichardsBorehole
bottom_pressure = 0
point_file = bh07.bh
SumQuantityUO = borehole_total_outflow_mass
variable = pressure
unit_weight = '0 0 0'
re_constant = 0.1594
character = 2
fully_upwind = true
[../]
[]
[Postprocessors]
[./bh_report]
type = RichardsPlotQuantity
uo = borehole_total_outflow_mass
execute_on = 'initial timestep_end'
[../]
[./fluid_mass]
type = RichardsMass
variable = pressure
execute_on = 'initial timestep_end'
[../]
[]
[Functions]
[./initial_pressure]
type = ParsedFunction
value = 1E7
[../]
[]
[Materials]
[./all]
type = RichardsMaterial
block = 1
viscosity = 1E-3
mat_porosity = 0.1
mat_permeability = '1E-11 0 0 0 1E-11 0 0 0 1E-11'
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = Seff1VG
pressure_vars = pressure
[../]
[]
[Preconditioning]
[./usual]
type = SMP
full = true
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -ksp_max_it'
petsc_options_value = 'bcgs bjacobi 1E-10 1E-10 10000 30'
[../]
[]
[Executioner]
type = Transient
end_time = 1000
solve_type = NEWTON
[./TimeStepper]
# get only marginally better results for smaller time steps
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = bh_fu_07
execute_on = 'initial timestep_end final'
interval = 10000
exodus = true
[]
(modules/richards/test/tests/gravity_head_1/gh_fu_20.i)
# investigating validity of immobile saturation
# 5 elements, full upwinding
[Mesh]
type = GeneratedMesh
dim = 1
nx = 5
xmin = -1
xmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGnone
sat_UO = Saturation
seff_UO = SeffVG
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1 10 100 1000 10000'
x = '0 10 100 1000 10000'
[../]
[]
[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 = 0.3
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGnone]
type = RichardsSUPGnone
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
initial_condition = -1.0
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[Kernels]
active = 'richardsf richardst'
[./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-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 = Transient
solve_type = Newton
dt = 1E0
end_time = 1E5
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = gh_fu_20
execute_on = 'timestep_end final'
interval = 10000
exodus = true
[]
(modules/tensor_mechanics/test/tests/combined_creep_plasticity/combined_stress_relaxation.i)
#
# 1x1x1 unit cube with constant displacement on top face
#
# This problem was taken from "Finite element three-dimensional elastic-plastic
# creep analysis" by A. Levy, Eng. Struct., 1981, Vol. 3, January, pp. 9-16.
#
# The problem is a one-dimensional creep analysis. The top face is displaced 0.01
# units and held there. The stress relaxes in time according to the creep law.
#
# The analytic solution to this problem is (contrary to what is shown in the paper):
#
# / (E*ef)^3 \^(1/3)
# stress_yy = |---------------------|
# \ 3*a*E^4*ef^3*t + 1 /
#
# where E = 2.0e11 (Young's modulus)
# a = 3e-26 (creep coefficient)
# ef = 0.01 (displacement)
# t = 2160.0 (time)
#
# such that the analytical solution is computed to be 2.9518e3 Pa
#
# Averaged over the single element block, MOOSE calculates the stress in the yy direction to be
# to be 3.046e3 Pa, which is a 3.2% error from the analytical solution.
#
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1e-2 1e-1 1e0 1e1 1e2'
x = '0 7e-1 7e0 7e1 1e2'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
incremental = true
add_variables = true
generate_output = 'stress_yy creep_strain_xx creep_strain_yy creep_strain_zz elastic_strain_yy'
[../]
[]
[BCs]
[./u_top_pull]
type = DirichletBC
variable = disp_y
boundary = top
value = 0.01
[../]
[./u_bottom_fix]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./u_yz_fix]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./u_xy_fix]
type = DirichletBC
variable = disp_z
boundary = back
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 2.0e11
poissons_ratio = 0.3
[../]
[./radial_return_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'power_law_creep'
[../]
[./power_law_creep]
type = PowerLawCreepStressUpdate
coefficient = 3.0e-26
n_exponent = 4
activation_energy = 0.0
relative_tolerance = 1e-14
absolute_tolerance = 1e-14
[../]
[]
[Postprocessors]
[./stress_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 100
nl_max_its = 100
nl_rel_tol = 1e-5
nl_abs_tol = 1e-8
l_tol = 1e-5
start_time = 0.0
end_time = 2160
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
exodus = true
[]
(modules/porous_flow/test/tests/poro_elasticity/mandel_fully_saturated.i)
# Mandel's problem of consolodation of a drained medium
# Using the FullySaturatedDarcyBase and FullySaturatedMassTimeDerivative kernels
# Note the use of consistent_with_displaced_mesh = false in the calculation of volumetric strain
#
# A sample is in plane strain.
# -a <= x <= a
# -b <= y <= b
# It is squashed with constant force by impermeable, frictionless plattens on its top and bottom surfaces (at y=+/-b)
# Fluid is allowed to leak out from its sides (at x=+/-a)
# The porepressure within the sample is monitored.
#
# As is common in the literature, this is simulated by
# considering the quarter-sample, 0<=x<=a and 0<=y<=b, with
# impermeable, roller BCs at x=0 and y=0 and y=b.
# Porepressure is fixed at zero on x=a.
# Porepressure and displacement are initialised to zero.
# Then the top (y=b) is moved downwards with prescribed velocity,
# so that the total force that is inducing this downwards velocity
# is fixed. The velocity is worked out by solving Mandel's problem
# analytically, and the total force is monitored in the simulation
# to check that it indeed remains constant.
#
# Here are the problem's parameters, and their values:
# Soil width. a = 1
# Soil height. b = 0.1
# Soil's Lame lambda. la = 0.5
# Soil's Lame mu, which is also the Soil's shear modulus. mu = G = 0.75
# Soil bulk modulus. K = la + 2*mu/3 = 1
# Drained Poisson ratio. nu = (3K - 2G)/(6K + 2G) = 0.2
# Soil bulk compliance. 1/K = 1
# Fluid bulk modulus. Kf = 8
# Fluid bulk compliance. 1/Kf = 0.125
# Soil initial porosity. phi0 = 0.1
# Biot coefficient. alpha = 0.6
# Biot modulus. M = 1/(phi0/Kf + (alpha - phi0)(1 - alpha)/K) = 4.705882
# Undrained bulk modulus. Ku = K + alpha^2*M = 2.694118
# Undrained Poisson ratio. nuu = (3Ku - 2G)/(6Ku + 2G) = 0.372627
# Skempton coefficient. B = alpha*M/Ku = 1.048035
# Fluid mobility (soil permeability/fluid viscosity). k = 1.5
# Consolidation coefficient. c = 2*k*B^2*G*(1-nu)*(1+nuu)^2/9/(1-nuu)/(nuu-nu) = 3.821656
# Normal stress on top. F = 1
#
# The solution for porepressure and displacements is given in
# AHD Cheng and E Detournay "A direct boundary element method for plane strain poroelasticity" International Journal of Numerical and Analytical Methods in Geomechanics 12 (1988) 551-572.
# The solution involves complicated infinite series, so I shall not write it here
[Mesh]
type = GeneratedMesh
dim = 3
nx = 10
ny = 1
nz = 1
xmin = 0
xmax = 1
ymin = 0
ymax = 0.1
zmin = 0
zmax = 1
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
PorousFlowDictator = dictator
block = 0
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'porepressure disp_x disp_y disp_z'
number_fluid_phases = 1
number_fluid_components = 1
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[disp_z]
[]
[porepressure]
[]
[]
[BCs]
[roller_xmin]
type = DirichletBC
variable = disp_x
value = 0
boundary = 'left'
[]
[roller_ymin]
type = DirichletBC
variable = disp_y
value = 0
boundary = 'bottom'
[]
[plane_strain]
type = DirichletBC
variable = disp_z
value = 0
boundary = 'back front'
[]
[xmax_drained]
type = DirichletBC
variable = porepressure
value = 0
boundary = right
[]
[top_velocity]
type = FunctionDirichletBC
variable = disp_y
function = top_velocity
boundary = top
[]
[]
[Functions]
[top_velocity]
type = PiecewiseLinear
x = '0 0.002 0.006 0.014 0.03 0.046 0.062 0.078 0.094 0.11 0.126 0.142 0.158 0.174 0.19 0.206 0.222 0.238 0.254 0.27 0.286 0.302 0.318 0.334 0.35 0.366 0.382 0.398 0.414 0.43 0.446 0.462 0.478 0.494 0.51 0.526 0.542 0.558 0.574 0.59 0.606 0.622 0.638 0.654 0.67 0.686 0.702'
y = '-0.041824842 -0.042730269 -0.043412712 -0.04428867 -0.045509181 -0.04645965 -0.047268246 -0.047974749 -0.048597109 -0.0491467 -0.049632388 -0.050061697 -0.050441198 -0.050776675 -0.051073238 -0.0513354 -0.051567152 -0.051772022 -0.051953128 -0.052113227 -0.052254754 -0.052379865 -0.052490464 -0.052588233 -0.052674662 -0.052751065 -0.052818606 -0.052878312 -0.052931093 -0.052977751 -0.053018997 -0.053055459 -0.053087691 -0.053116185 -0.053141373 -0.05316364 -0.053183324 -0.053200724 -0.053216106 -0.053229704 -0.053241725 -0.053252351 -0.053261745 -0.053270049 -0.053277389 -0.053283879 -0.053289615'
[]
[]
[AuxVariables]
[stress_yy]
order = CONSTANT
family = MONOMIAL
[]
[tot_force]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
[]
[tot_force]
type = ParsedAux
args = 'stress_yy porepressure'
execute_on = timestep_end
variable = tot_force
function = '-stress_yy+0.6*porepressure'
[]
[]
[Kernels]
[grad_stress_x]
type = StressDivergenceTensors
variable = disp_x
component = 0
[]
[grad_stress_y]
type = StressDivergenceTensors
variable = disp_y
component = 1
[]
[grad_stress_z]
type = StressDivergenceTensors
variable = disp_z
component = 2
[]
[poro_x]
type = PorousFlowEffectiveStressCoupling
biot_coefficient = 0.6
variable = disp_x
component = 0
[]
[poro_y]
type = PorousFlowEffectiveStressCoupling
biot_coefficient = 0.6
variable = disp_y
component = 1
[]
[poro_z]
type = PorousFlowEffectiveStressCoupling
biot_coefficient = 0.6
component = 2
variable = disp_z
[]
[mass0]
type = PorousFlowFullySaturatedMassTimeDerivative
biot_coefficient = 0.6
coupling_type = HydroMechanical
variable = porepressure
[]
[flux]
type = PorousFlowFullySaturatedDarcyBase
variable = porepressure
gravity = '0 0 0'
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 8
density0 = 1
thermal_expansion = 0
viscosity = 1
[]
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[elasticity_tensor]
type = ComputeElasticityTensor
C_ijkl = '0.5 0.75'
# bulk modulus is lambda + 2*mu/3 = 0.5 + 2*0.75/3 = 1
fill_method = symmetric_isotropic
[]
[strain]
type = ComputeSmallStrain
[]
[stress]
type = ComputeLinearElasticStress
[]
[eff_fluid_pressure_qp]
type = PorousFlowEffectiveFluidPressure
[]
[vol_strain]
type = PorousFlowVolumetricStrain
consistent_with_displaced_mesh = false
[]
[ppss]
type = PorousFlow1PhaseFullySaturated
porepressure = porepressure
[]
[massfrac]
type = PorousFlowMassFraction
[]
[simple_fluid_qp]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[porosity]
type = PorousFlowPorosityConst # only the initial value of this is ever used
porosity = 0.1
[]
[biot_modulus]
type = PorousFlowConstantBiotModulus
biot_coefficient = 0.6
solid_bulk_compliance = 1
fluid_bulk_modulus = 8
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1.5 0 0 0 1.5 0 0 0 1.5'
[]
[]
[Postprocessors]
[p0]
type = PointValue
outputs = csv
point = '0.0 0 0'
variable = porepressure
[]
[p1]
type = PointValue
outputs = csv
point = '0.1 0 0'
variable = porepressure
[]
[p2]
type = PointValue
outputs = csv
point = '0.2 0 0'
variable = porepressure
[]
[p3]
type = PointValue
outputs = csv
point = '0.3 0 0'
variable = porepressure
[]
[p4]
type = PointValue
outputs = csv
point = '0.4 0 0'
variable = porepressure
[]
[p5]
type = PointValue
outputs = csv
point = '0.5 0 0'
variable = porepressure
[]
[p6]
type = PointValue
outputs = csv
point = '0.6 0 0'
variable = porepressure
[]
[p7]
type = PointValue
outputs = csv
point = '0.7 0 0'
variable = porepressure
[]
[p8]
type = PointValue
outputs = csv
point = '0.8 0 0'
variable = porepressure
[]
[p9]
type = PointValue
outputs = csv
point = '0.9 0 0'
variable = porepressure
[]
[p99]
type = PointValue
outputs = csv
point = '1 0 0'
variable = porepressure
[]
[xdisp]
type = PointValue
outputs = csv
point = '1 0.1 0'
variable = disp_x
[]
[ydisp]
type = PointValue
outputs = csv
point = '1 0.1 0'
variable = disp_y
[]
[total_downwards_force]
type = ElementAverageValue
outputs = csv
variable = tot_force
[]
[dt]
type = FunctionValuePostprocessor
outputs = console
function = if(0.15*t<0.01,0.15*t,0.01)
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'gmres asm lu 1E-14 1E-10 10000'
[]
[]
[Executioner]
type = Transient
solve_type = Newton
start_time = 0
end_time = 0.7
[TimeStepper]
type = PostprocessorDT
postprocessor = dt
dt = 0.001
[]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = mandel_fully_saturated
[csv]
interval = 3
type = CSV
[]
[]
(modules/combined/test/tests/inelastic_strain/creep/creep_nl1.i)
#
# Test for effective strain calculation.
# Boundary conditions from NAFEMS test NL1
#
# This is not a verification test. This is the creep analog of the same test
# in the elas_plas directory. Instead of using the IsotropicPlasticity
# material model this test uses the PowerLawCreep material model.
#
[GlobalParams]
temperature = temp
order = FIRST
family = LAGRANGE
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = one_elem2.e
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./temp]
initial_condition = 600.0
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./vonmises]
order = CONSTANT
family = MONOMIAL
[../]
[./pressure]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./creep_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./creep_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./creep_strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./tot_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./tot_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./tot_strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./eff_creep_strain]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
decomposition_method = EigenSolution
[../]
[./heat]
type = HeatConduction
variable = temp
[../]
[./heat_ie]
type = HeatConductionTimeDerivative
variable = temp
[../]
[]
[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_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./vonmises]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = vonmises
scalar_type = VonMisesStress
execute_on = timestep_end
[../]
[./pressure]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = pressure
scalar_type = Hydrostatic
execute_on = timestep_end
[../]
[./elastic_strain_xx]
type = RankTwoAux
rank_two_tensor = elastic_strain
variable = elastic_strain_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./elastic_strain_yy]
type = RankTwoAux
rank_two_tensor = elastic_strain
variable = elastic_strain_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./elastic_strain_zz]
type = RankTwoAux
rank_two_tensor = elastic_strain
variable = elastic_strain_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./creep_strain_xx]
type = RankTwoAux
rank_two_tensor = creep_strain
variable = creep_strain_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./creep_strain_yy]
type = RankTwoAux
rank_two_tensor = creep_strain
variable = creep_strain_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./creep_strain_zz]
type = RankTwoAux
rank_two_tensor = creep_strain
variable = creep_strain_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./tot_strain_xx]
type = RankTwoAux
rank_two_tensor = total_strain
variable = tot_strain_xx
index_i = 0
index_j = 0
[../]
[./tot_strain_yy]
type = RankTwoAux
rank_two_tensor = total_strain
variable = tot_strain_yy
index_i = 1
index_j = 1
[../]
[./tot_strain_zz]
type = RankTwoAux
rank_two_tensor = total_strain
variable = tot_strain_zz
index_i = 2
index_j = 2
[../]
[./eff_creep_strain]
type = MaterialRealAux
property = effective_creep_strain
variable = eff_creep_strain
[../]
[]
[Functions]
[./appl_dispy]
type = PiecewiseLinear
x = '0 1.0 2.0'
y = '0.0 0.25e-4 0.50e-4'
[../]
[]
[BCs]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 101
value = 0.0
[../]
[./origin_x]
type = DirichletBC
variable = disp_x
boundary = 103
value = 0.0
[../]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 102
value = 0.0
[../]
[./origin_y]
type = DirichletBC
variable = disp_y
boundary = 103
value = 0.0
[../]
[./top_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 1
function = appl_dispy
[../]
[./temp_fix]
type = DirichletBC
variable = temp
boundary = '1 2'
value = 600.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = 1
youngs_modulus = 250e9
poissons_ratio = 0.25
[../]
[./strain]
type = ComputePlaneFiniteStrain
block = 1
[../]
[./radial_return_stress]
type = ComputeMultipleInelasticStress
block = 1
inelastic_models = 'powerlawcrp'
[../]
[./powerlawcrp]
type = PowerLawCreepStressUpdate
block = 1
coefficient = 3.125e-14
n_exponent = 5.0
m_exponent = 0.0
activation_energy = 0.0
[../]
[./thermal]
type = HeatConductionMaterial
block = 1
specific_heat = 1.0
thermal_conductivity = 100.
[../]
[./density]
type = Density
block = 1
density = 1.0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
nl_rel_tol = 1e-10
nl_abs_tol = 1e-12
l_tol = 1e-6
l_max_its = 100
nl_max_its = 20
dt = 1.0
start_time = 0.0
num_steps = 100
end_time = 2.0
[]
[Postprocessors]
[./stress_xx]
type = ElementAverageValue
variable = stress_xx
[../]
[./stress_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./stress_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./stress_xy]
type = ElementAverageValue
variable = stress_xy
[../]
[./vonmises]
type = ElementAverageValue
variable = vonmises
[../]
[./pressure]
type = ElementAverageValue
variable = pressure
[../]
[./el_strain_xx]
type = ElementAverageValue
variable = elastic_strain_xx
[../]
[./el_strain_yy]
type = ElementAverageValue
variable = elastic_strain_yy
[../]
[./el_strain_zz]
type = ElementAverageValue
variable = elastic_strain_zz
[../]
[./crp_strain_xx]
type = ElementAverageValue
variable = creep_strain_xx
[../]
[./crp_strain_yy]
type = ElementAverageValue
variable = creep_strain_yy
[../]
[./crp_strain_zz]
type = ElementAverageValue
variable = creep_strain_zz
[../]
[./eff_creep_strain]
type = ElementAverageValue
variable = eff_creep_strain
[../]
[./tot_strain_xx]
type = ElementAverageValue
variable = tot_strain_xx
[../]
[./tot_strain_yy]
type = ElementAverageValue
variable = tot_strain_yy
[../]
[./tot_strain_zz]
type = ElementAverageValue
variable = tot_strain_zz
[../]
[./disp_x1]
type = NodalVariableValue
nodeid = 0
variable = disp_x
[../]
[./disp_x4]
type = NodalVariableValue
nodeid = 3
variable = disp_x
[../]
[./disp_y1]
type = NodalVariableValue
nodeid = 0
variable = disp_y
[../]
[./disp_y4]
type = NodalVariableValue
nodeid = 3
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[]
[Outputs]
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/combined/test/tests/adaptive_timestepping/adapt_tstep_function_change_restart2.i)
# This is a test designed to evaluate the cabability of the
# IterationAdaptiveDT TimeStepper to adjust time step size according to
# a function. For example, if the power input function for a BISON
# simulation rapidly increases or decreases, the IterationAdaptiveDT
# TimeStepper should take time steps small enough to capture the
# oscillation.
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
order = FIRST
family = LAGRANGE
block = 1
[]
[Mesh]
file = 1hex8_10mm_cube.e
[]
[Functions]
[./Fiss_Function]
type = PiecewiseLinear
x = '0 1e6 2e6 2.001e6 2.002e6'
y = '0 3e8 3e8 12e8 0'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[./temp]
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
volumetric_locking_correction = true
incremental = true
eigenstrain_names = thermal_expansion
decomposition_method = EigenSolution
add_variables = true
generate_output = 'vonmises_stress'
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[./heat_ie]
type = HeatConductionTimeDerivative
variable = temp
[../]
[./heat_source]
type = HeatSource
variable = temp
value = 1.0
function = Fiss_Function
[../]
[]
[BCs]
[./bottom_temp]
type = DirichletBC
variable = temp
boundary = 1
value = 300
[../]
[./top_bottom_disp_x]
type = DirichletBC
variable = disp_x
boundary = '1'
value = 0
[../]
[./top_bottom_disp_y]
type = DirichletBC
variable = disp_y
boundary = '1'
value = 0
[../]
[./top_bottom_disp_z]
type = DirichletBC
variable = disp_z
boundary = '1'
value = 0
[../]
[]
[Materials]
[./thermal]
type = HeatConductionMaterial
temp = temp
specific_heat = 1.0
thermal_conductivity = 1.0
[../]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 300e6
poissons_ratio = .3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[./thermal_expansion]
type = ComputeThermalExpansionEigenstrain
thermal_expansion_coeff = 5e-6
stress_free_temperature = 300.0
temperature = temp
eigenstrain_name = thermal_expansion
[../]
[./density]
type = Density
density = 10963.0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
verbose = true
nl_abs_tol = 1e-10
num_steps = 50000
end_time = 2.002e6
[./TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_function = Fiss_Function
max_function_change = 3e7
dt = 1e6
[../]
[]
[Postprocessors]
[./Temperature_of_Block]
type = ElementAverageValue
variable = temp
execute_on = 'timestep_end'
[../]
[./vonMises]
type = ElementAverageValue
variable = vonmises_stress
execute_on = 'timestep_end'
[../]
[]
[Outputs]
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 10
[../]
[]
[Problem]
restart_file_base = adapt_tstep_function_change_restart1_checkpoint_cp/0065
[]
(modules/tensor_mechanics/test/tests/ad_viscoplasticity_stress_update/creep.i)
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
xmax = 0.002
ymax = 0.002
[]
[Modules/TensorMechanics/Master/All]
strain = FINITE
add_variables = true
base_name = 'total'
generate_output = 'strain_xx strain_yy strain_xy hydrostatic_stress vonmises_stress'
use_automatic_differentiation = true
[]
[Functions]
[./pull]
type = PiecewiseLinear
x = '0 0.1'
y = '0 1e-5'
[../]
[]
[Materials]
active='elasticity_tensor porous_stress porosity creep'
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1e10
poissons_ratio = 0.3
base_name = 'total'
[../]
[./porous_stress]
type = ADComputeMultipleInelasticStress
inelastic_models = creep
outputs = all
base_name = 'total'
[../]
[./regular_stress]
type = ADComputeMultipleInelasticStress
inelastic_models = creep
outputs = all
base_name = 'total'
[../]
[./porosity]
type = ADGenericConstantMaterial
prop_names = porosity
prop_values = 0.1
outputs = all
[../]
[./creep]
type = ADPowerLawCreepStressUpdate
activation_energy = 4e4
temperature = 1200
coefficient = 1e-18
gas_constant = 1.987
n_exponent = 3
base_name = 'creep'
outputs = all
[../]
[]
[BCs]
[./no_disp_x]
type = ADDirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./no_disp_y]
type = ADDirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./pull_disp_y]
type = ADFunctionDirichletBC
variable = disp_y
boundary = top
function = pull
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
dt = 0.01
end_time = 0.12
[]
[Postprocessors]
[./disp_x]
type = SideAverageValue
variable = disp_x
boundary = right
[../]
[./disp_y]
type = SideAverageValue
variable = disp_y
boundary = top
[../]
[./avg_hydro]
type = ElementAverageValue
variable = total_hydrostatic_stress
[../]
[./avg_vonmises]
type = ElementAverageValue
variable = total_vonmises_stress
[../]
[./dt]
type = TimestepSize
[../]
[./num_lin]
type = NumLinearIterations
outputs = console
[../]
[./num_nonlin]
type = NumNonlinearIterations
outputs = console
[../]
[./eff_creep_strain]
type = ElementAverageValue
variable = creep_effective_creep_strain
[../]
[./porosity]
type = ElementAverageValue
variable = porosity
[../]
[]
[Outputs]
csv = true
[]
(test/tests/geomsearch/2d_moving_penetration/pl_test4qns.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
file = pl_test4q.e
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
normal_smoothing_distance = 0.2
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
normal_smoothing_distance = 0.2
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate10]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate13]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate14]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate15]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate16]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1.e-9
l_max_its = 10
start_time = 0.0
dt = 0.02
end_time = 1.0
[./Quadrature]
order = THIRD
[../]
[]
[Outputs]
file_base = pl_test4qns_out
exodus = true
[]
(modules/combined/test/tests/evolving_mass_density/uniform_expand_compress_test_tensors.i)
# Element mass tests
# This series of tests is designed to compute the mass of elements based on
# an evolving mass density calculation. The tests consist of expansion and compression
# of the elastic patch test model along each axis, uniform expansion and compression,
# and shear in each direction. The expansion and compression tests change the volume of
# the elements. The corresponding change in density should compensate for this so the
# mass remains constant. The shear tests should not result in a volume change, and this
# is checked too. The mass calculation is done with the post processor called Mass.
# The tests/file names are as follows:
# Expansion and compression along a single axis
# expand_compress_x_test_out.e
# expand_compress_y_test_out.e
# expand_compress_z_test_out.e
# Volumetric expansion and compression
# uniform_expand_compress_test.i
# Zero volume change shear along each axis
# shear_x_test_out.e
# shear_y_test_out.e
# shear_z_test_out.e
# The resulting mass calculation for these tests should always be = 1.
# This test is a duplicate of the uniform_expand_compress_test.i test for solid mechanics, and the
# output of this tensor mechanics test is compared to the original
# solid mechanics output. The duplication is necessary to test the
# migrated tensor mechanics version while maintaining tests for solid mechanics.
[Mesh]
file = elastic_patch.e
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Functions]
[./rampConstant2]
type = PiecewiseLinear
x = '0.00 1.00 2.0 3.00'
y = '0.00 0.25 0.0 -0.25'
scale_factor = 1
[../]
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./TensorMechanics]
[../]
[]
[BCs]
[./9_y]
type = DirichletBC
variable = disp_y
boundary = 9
value = 0
[../]
[./10_y]
type = DirichletBC
variable = disp_x
boundary = 10
value = 0
[../]
[./14_y]
type = DirichletBC
variable = disp_z
boundary = 14
value = 0
[../]
[./top]
type = FunctionDirichletBC
variable = disp_y
preset = false
boundary = 11
function = rampConstant2
[../]
[./front]
type = FunctionDirichletBC
variable = disp_z
preset = false
boundary = 13
function = rampConstant2
[../]
[./side]
type = FunctionDirichletBC
variable = disp_x
preset = false
boundary = 12
function = rampConstant2
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = '1 2 3 4 5 6 7'
youngs_modulus = 1e6
poissons_ratio = 0.0
[../]
[./small_strain]
type = ComputeSmallStrain
block = ' 1 2 3 4 5 6 7'
[../]
[./elastic_stress]
type = ComputeLinearElasticStress
block = '1 2 3 4 5 6 7'
[../]
[]
[Executioner]
type = Transient
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
nl_abs_tol = 1e-10
l_max_its = 20
start_time = 0.0
dt = 1.0
num_steps = 3
end_time =3.0
[]
[Outputs]
[./out]
type = Exodus
elemental_as_nodal = true
file_base = uniform_expand_compress_test_out
[../]
[]
[Postprocessors]
[./Mass]
type = Mass
variable = disp_x
execute_on = 'initial timestep_end'
[../]
[]
(modules/richards/test/tests/gravity_head_2/gh_fu_18.i)
# with immobile saturation - this illustrates a perfect case of fullyupwind working very well
# unsaturated = true
# gravity = true
# full upwinding = true
# transient = true
[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'
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1E-2 1E-1 1E0 0.5E1 0.5E2 0.4E4 1E5 1E6 1E7'
x = '0 1E-1 1E0 1E1 1E2 1E3 1E4 1E5 1E6'
[../]
[]
[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 = 0.4
n = 2
[../]
[./RelPermGas]
type = RichardsRelPermPower
simm = 0.3
n = 2
[../]
[./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-5
[../]
[./SUPGgas]
type = RichardsSUPGstandard
p_SUPG = 1E-5
[../]
[]
[Variables]
[./pwater]
order = FIRST
family = LAGRANGE
[../]
[./pgas]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./water_ic]
type = ConstantIC
value = 1
variable = pwater
[../]
[./gas_ic]
type = ConstantIC
value = 2
variable = pgas
[../]
[]
[Kernels]
active = 'richardsfwater richardstwater richardsfgas richardstgas'
[./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
[../]
[./mass_error_gas]
type = FunctionValuePostprocessor
function = fcn_mass_error_g
[../]
[./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((-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 -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-10 1E-10 10'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
end_time = 1E6
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = gh_fu_18
execute_on = 'timestep_end final'
interval = 100000
exodus = true
[]
(modules/tensor_mechanics/test/tests/beam/dynamic/dyn_euler_small_added_mass2.i)
# Test for small strain euler beam vibration in y direction
# An impulse load is applied at the end of a cantilever beam of length 5ft (60 in).
# The beam is massless with a lumped mass at the end of the beam of 5000 lb
# The properties of the cantilever beam are as follows:
# E = 1e7 and I = 120 in^4
# Assuming a square cross section A = sqrt(12 * I) = 37.95
# Shear modulus (G) = 3.846e6
# Shear coefficient (k) = 1.0
# Cross-section area (A) = 1.0
# mass (m) = 5000 lb / 386 = 12.95
# The theoretical first frequency of this beam is:
# f1 = 1/(2 pi) * sqrt(3EI/(mL^3)) = 5.71 cps
# This implies that the corresponding time period of this beam is 0.175 s.
# The FEM solution for this beam with 10 elements gives
# a time period of 0.175 s with time step of 0.005 s.
# Reference: Strength of Materials by Marin ans Sauer, 2nd Ed.
# Example Problem 11-50, pg. 375
[Mesh]
type = GeneratedMesh
dim = 1
nx = 10
xmin = 0.0
xmax = 60.0
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[./rot_x]
order = FIRST
family = LAGRANGE
[../]
[./rot_y]
order = FIRST
family = LAGRANGE
[../]
[./rot_z]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./vel_x]
order = FIRST
family = LAGRANGE
[../]
[./vel_y]
order = FIRST
family = LAGRANGE
[../]
[./vel_z]
order = FIRST
family = LAGRANGE
[../]
[./accel_x]
order = FIRST
family = LAGRANGE
[../]
[./accel_y]
order = FIRST
family = LAGRANGE
[../]
[./accel_z]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./accel_x]
type = NewmarkAccelAux
variable = accel_x
displacement = disp_x
velocity = vel_x
beta = 0.25
execute_on = timestep_end
[../]
[./vel_x]
type = NewmarkVelAux
variable = vel_x
acceleration = accel_x
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_y]
type = NewmarkAccelAux
variable = accel_y
displacement = disp_y
velocity = vel_y
beta = 0.25
execute_on = timestep_end
[../]
[./vel_y]
type = NewmarkVelAux
variable = vel_y
acceleration = accel_y
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_z]
type = NewmarkAccelAux
variable = accel_z
displacement = disp_z
velocity = vel_z
beta = 0.25
execute_on = timestep_end
[../]
[./vel_z]
type = NewmarkVelAux
variable = vel_z
acceleration = accel_z
gamma = 0.5
execute_on = timestep_end
[../]
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./fixy1]
type = DirichletBC
variable = disp_y
boundary = left
value = 0.0
[../]
[./fixz1]
type = DirichletBC
variable = disp_z
boundary = left
value = 0.0
[../]
[./fixr1]
type = DirichletBC
variable = rot_x
boundary = left
value = 0.0
[../]
[./fixr2]
type = DirichletBC
variable = rot_y
boundary = left
value = 0.0
[../]
[./fixr3]
type = DirichletBC
variable = rot_z
boundary = left
value = 0.0
[../]
[]
[NodalKernels]
[./force_y2]
type = UserForcingFunctionNodalKernel
variable = disp_y
boundary = right
function = force
[../]
[./x_inertial]
type = NodalTranslationalInertia
variable = disp_x
velocity = vel_x
acceleration = accel_x
boundary = right
beta = 0.25
gamma = 0.5
mass = 12.95
[../]
[./y_inertial]
type = NodalTranslationalInertia
variable = disp_y
velocity = vel_y
acceleration = accel_y
boundary = right
beta = 0.25
gamma = 0.5
mass = 12.95
[../]
[./z_inertial]
type = NodalTranslationalInertia
variable = disp_z
velocity = vel_z
acceleration = accel_z
boundary = right
beta = 0.25
gamma = 0.5
mass = 12.95
[../]
[]
[Functions]
[./force]
type = PiecewiseLinear
x = '0.0 0.1 0.2 10.0'
y = '0.0 1e2 0.0 0.0'
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
line_search = 'none'
l_tol = 1e-8
l_max_its = 50
nl_max_its = 15
nl_rel_tol = 1e-8
nl_abs_tol = 1e-8
start_time = 0.0
dt = 0.005
end_time = 1.5
timestep_tolerance = 1e-6
[]
[Kernels]
[./solid_disp_x]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 0
variable = disp_x
[../]
[./solid_disp_y]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 1
variable = disp_y
[../]
[./solid_disp_z]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 2
variable = disp_z
[../]
[./solid_rot_x]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 3
variable = rot_x
[../]
[./solid_rot_y]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 4
variable = rot_y
[../]
[./solid_rot_z]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 5
variable = rot_z
[../]
[]
[Materials]
[./elasticity]
type = ComputeElasticityBeam
youngs_modulus = 1.0e7
poissons_ratio = 0.30005200208
shear_coefficient = 1.0
block = 0
[../]
[./strain]
type = ComputeIncrementalBeamStrain
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
area = 37.95
Ay = 0.0
Az = 0.0
Iy = 120.0
Iz = 120.0
y_orientation = '0.0 1.0 0.0'
[../]
[./stress]
type = ComputeBeamResultants
block = 0
[../]
[]
[Postprocessors]
[./disp_x]
type = PointValue
point = '60.0 0.0 0.0'
variable = disp_x
[../]
[./disp_y]
type = PointValue
point = '60.0 0.0 0.0'
variable = disp_y
[../]
[./vel_y]
type = PointValue
point = '60.0 0.0 0.0'
variable = vel_y
[../]
[./accel_y]
type = PointValue
point = '60.0 0.0 0.0'
variable = accel_y
[../]
[]
[Outputs]
exodus = true
csv = true
perf_graph = true
[]
(modules/tensor_mechanics/test/tests/j_integral/j_integral_2d_mouth_dir.i)
#This tests the J-Integral evaluation capability.
#This is a 2d plane strain model
#Crack direction is defined using the crack mouth coordinates.
#The analytic solution for J1 is 2.434. This model
#converges to that solution with a refined mesh.
#Reference: National Agency for Finite Element Methods and Standards (U.K.):
#Test 1.1 from NAFEMS publication "Test Cases in Linear Elastic Fracture
#Mechanics" R0020.
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[Mesh]
file = crack2d.e
[]
[AuxVariables]
[./SED]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./rampConstant]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = -1e2
[../]
[]
[DomainIntegral]
integrals = JIntegral
boundary = 800
crack_direction_method = CrackMouth
crack_mouth_boundary = 900
2d = true
axis_2d = 2
radius_inner = '4.0 4.5 5.0 5.5 6.0'
radius_outer = '4.5 5.0 5.5 6.0 6.5'
output_q = false
incremental = true
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
planar_formulation = PLANE_STRAIN
[../]
[]
[AuxKernels]
[./SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[../]
[]
[BCs]
[./crack_y]
type = DirichletBC
variable = disp_y
boundary = 100
value = 0.0
[../]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 700
value = 0.0
[../]
[./Pressure]
[./Side1]
boundary = 400
function = rampConstant
[../]
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_rel_tol = 1e-12
nl_abs_tol = 1e-5
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Outputs]
file_base = j_integral_2d_mouth_dir_out
exodus = true
csv = true
[]
(modules/xfem/test/tests/second_order_elements/square_branch_quad9_2d.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
volumetric_locking_correction = false
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD9
[]
[UserObjects]
[./line_seg_cut_set_uo]
type = LineSegmentCutSetUserObject
cut_data = '-1.0000e-10 6.6340e-01 6.6340e-01 -1.0000e-10 0.0 1.0
3.3120e-01 3.3200e-01 1.0001e+00 3.3200e-01 1.0 2.0'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
[../]
[]
[Functions]
[./right_disp_x]
type = PiecewiseLinear
x = '0 1.0 2.0 3.0'
y = '0 0.005 0.01 0.01'
[../]
[./top_disp_y]
type = PiecewiseLinear
x = '0 1.0 2.0 3.0'
y = '0 0.005 0.01 0.01'
[../]
[]
[BCs]
[./right_x]
type = FunctionDirichletBC
boundary = 1
variable = disp_x
function = right_disp_x
[../]
[./top_y]
type = FunctionDirichletBC
boundary = 2
variable = disp_y
function = top_disp_y
[../]
[./bottom_y]
type = DirichletBC
boundary = 0
variable = disp_y
value = 0.0
[../]
[./left_x]
type = DirichletBC
boundary = 3
variable = disp_x
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-16
nl_abs_tol = 1e-10
# time control
start_time = 0.0
dt = 1.0
end_time = 2.2
num_steps = 5000
[]
[Outputs]
exodus = true
[./console]
type = Console
output_linear = 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'
[]
(test/tests/geomsearch/2d_moving_penetration/pl_test1qtt.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
file = pl_test1q.e
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
tangential_tolerance = 0.1
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
tangential_tolerance = 0.1
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate10]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate13]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate14]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate15]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate16]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 0.7 -0.7 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1.e-9
l_max_its = 10
start_time = 0.0
dt = 0.05
end_time = 1.0
[./Quadrature]
order = THIRD
[../]
[]
[Outputs]
file_base = pl_test1qtt_out
exodus = true
[]
(modules/tensor_mechanics/test/tests/ad_anisotropic_creep/ad_aniso_creep_integration_error.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
nx = 10
ny = 2
nz = 2
xmin = 0.0
ymin = 0.0
zmin = 0.0
xmax = 10.0
ymax = 1.0
zmax = 1.0
[]
[corner_node]
type = ExtraNodesetGenerator
new_boundary = '100'
nodes = '3 69'
input = gen
[]
[corner_node_2]
type = ExtraNodesetGenerator
new_boundary = '101'
nodes = '4 47'
input = corner_node
[]
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[AuxVariables]
[hydrostatic_stress]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_xx]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_xy]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_yy]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[hydrostatic_stress]
type = ADRankTwoScalarAux
variable = hydrostatic_stress
rank_two_tensor = stress
scalar_type = Hydrostatic
[]
[creep_strain_xx]
type = ADRankTwoAux
rank_two_tensor = creep_strain
variable = creep_strain_xx
index_i = 0
index_j = 0
[]
[creep_strain_xy]
type = ADRankTwoAux
rank_two_tensor = creep_strain
variable = creep_strain_xy
index_i = 0
index_j = 1
[]
[creep_strain_yy]
type = ADRankTwoAux
rank_two_tensor = creep_strain
variable = creep_strain_yy
index_i = 1
index_j = 1
[]
[sigma_xx]
type = ADRankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 1
index_j = 1
[]
[]
[Functions]
[pull]
type = PiecewiseLinear
x = '0 1.0'
y = '0 -4e1'
[]
[]
[Modules/TensorMechanics/Master]
[all]
strain = FINITE
generate_output = 'elastic_strain_xx stress_xx'
use_automatic_differentiation = true
add_variables = true
[]
[]
[Materials]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 7000
poissons_ratio = 0.0
[]
[elastic_strain]
type = ADComputeMultipleInelasticStress
inelastic_models = "trial_creep_two"
max_iterations = 50
absolute_tolerance = 1e-16
[]
[trial_creep_two]
type = ADHillCreepStressUpdate
coefficient = 1e-16
n_exponent = 9
m_exponent = 0
activation_energy = 0
# F G H L M N
hill_constants = "0.5 0.25 0.3866 1.6413 1.6413 1.2731"
# hill_constants = "0.5 0.25 0.3866 1.6413 1.6413 1.2731"
max_inelastic_increment = 1.0e-4
absolute_tolerance = 1e-20
relative_tolerance = 1e-20
max_integration_error = 1.0e-5
[]
[]
[BCs]
[no_disp_x]
type = ADDirichletBC
variable = disp_x
boundary = left
value = 0.0
[]
[no_disp_y]
type = ADDirichletBC
variable = disp_y
boundary = 100
value = 0.0
[]
[no_disp_z]
type = ADDirichletBC
variable = disp_z
boundary = 101
value = 0.0
[]
[Pressure]
[Side1]
boundary = right
function = pull
[]
[]
[]
[UserObjects]
[terminator_creep]
type = Terminator
expression = 'time_step_size > matl_ts_min'
fail_mode = SOFT
execute_on = TIMESTEP_END
[]
[]
[Executioner]
type = Transient
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
nl_rel_tol = 1.0e-13
nl_abs_tol = 1.0e-13
l_max_its = 10
end_time = 1.65e-1
dt = 2.5e-2
start_time = 0
automatic_scaling = true
[./TimeStepper]
type = IterationAdaptiveDT
dt = 2.5e-2
time_t = '0.0 10.0'
time_dt = '2.5e-2 2.5e-2 '
optimal_iterations = 30
iteration_window = 9
growth_factor = 1.5
cutback_factor = 0.5
timestep_limiting_postprocessor = matl_ts_min
[../]
[]
[Postprocessors]
[time_step_size]
type = TimestepSize
[]
[matl_ts_min]
type = MaterialTimeStepPostprocessor
[]
[max_disp_x]
type = ElementExtremeValue
variable = disp_x
[]
[max_disp_y]
type = ElementExtremeValue
variable = disp_y
[]
[max_hydro]
type = ElementAverageValue
variable = hydrostatic_stress
[]
[dt]
type = TimestepSize
[]
[num_lin]
type = NumLinearIterations
outputs = console
[]
[num_nonlin]
type = NumNonlinearIterations
outputs = console
[]
[creep_strain_xx]
type = ElementalVariableValue
variable = creep_strain_xx
execute_on = 'TIMESTEP_END'
elementid = 39
[]
[elastic_strain_xx]
type = ElementalVariableValue
variable = elastic_strain_xx
execute_on = 'TIMESTEP_END'
elementid = 39
[]
[sigma_xx]
type = ElementalVariableValue
variable = stress_xx
execute_on = 'TIMESTEP_END'
elementid = 39
[]
[]
[Outputs]
csv = true
exodus = true
perf_graph = true
[]
(modules/xfem/test/tests/solid_mechanics_basic/test_crack_counter.i)
# This test is used to verify that the pure test object (TestCrackCounter)
# is correctly using the API for extracting the crack_tip_origin_direction_map
# from XFEM. The map contains information of the location of all the crack tips
# computed by XFEM. The TestCrackCounter postprocessor simply returns the
# number of elements in the map which corresponds to the number of cracks.
#
# In this test case 4 prescribed cracks are applied. Therefore, the
# TestCrackCounter postprocessor returns a value of 4.
[GlobalParams]
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 11
ny = 11
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '1.0 0.5 0.7 0.5'
time_start_cut = 0.0
time_end_cut = 0.0
[../]
[./line_seg_cut_uo2]
type = LineSegmentCutUserObject
cut_data = '0.0 0.5 0.3 0.5'
time_start_cut = 0.0
time_end_cut = 0.0
[../]
[./line_seg_cut_uo3]
type = LineSegmentCutUserObject
cut_data = '0.5 0.0 0.5 0.3'
time_start_cut = 0.0
time_end_cut = 0.0
[../]
[./line_seg_cut_uo4]
type = LineSegmentCutUserObject
cut_data = '0.5 1.0 0.5 0.7'
time_start_cut = 0.0
time_end_cut = 0.0
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
planar_formulation = plane_strain
add_variables = true
[../]
[]
[Functions]
[./pull]
type = PiecewiseLinear
x='0 50 100'
y='0 0.02 0.1'
[../]
[]
[BCs]
[./bottomx]
type = DirichletBC
boundary = bottom
variable = disp_x
value = 0.0
[../]
[./bottomy]
type = DirichletBC
boundary = bottom
variable = disp_y
value = 0.0
[../]
[./topx]
type = DirichletBC
boundary = top
variable = disp_x
value = 0.0
[../]
[./topy]
type = FunctionDirichletBC
boundary = top
variable = disp_y
function = pull
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
block = 0
[../]
[./_elastic_strain]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[]
[Postprocessors]
[./number_of_cracks]
type = TestCrackCounter
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-14
nl_abs_tol = 1e-9
# time control
start_time = 0.0
dt = 1.0
end_time = 1.0
num_steps = 5000
max_xfem_update = 1
[]
[Outputs]
csv = true
[]
(modules/tensor_mechanics/test/tests/plane_stress/weak_plane_stress_small.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
temperature = temp
out_of_plane_strain = strain_zz
[]
[Mesh]
[./square]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 2
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./strain_zz]
[../]
[]
[AuxVariables]
[./temp]
[../]
[./nl_strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Postprocessors]
[./react_z]
type = MaterialTensorIntegral
rank_two_tensor = stress
index_i = 2
index_j = 2
[../]
[./min_strain_zz]
type = NodalExtremeValue
variable = strain_zz
value_type = min
[../]
[./max_strain_zz]
type = NodalExtremeValue
variable = strain_zz
value_type = max
[../]
[]
[Modules/TensorMechanics/Master]
[plane_stress]
planar_formulation = WEAK_PLANE_STRESS
strain = SMALL
generate_output = 'stress_xx stress_xy stress_yy stress_zz strain_xx strain_xy strain_yy'
eigenstrain_names = eigenstrain
[]
[]
[AuxKernels]
[./tempfuncaux]
type = FunctionAux
variable = temp
function = tempfunc
use_displaced_mesh = false
[../]
[./strain_zz]
type = RankTwoAux
rank_two_tensor = total_strain
variable = nl_strain_zz
index_i = 2
index_j = 2
[../]
[]
[Functions]
[./pull]
type = PiecewiseLinear
x='0 1 100'
y='0 0.00 0.00'
[../]
[./tempfunc]
type = ParsedFunction
value = '(1 - x) * t'
[../]
[]
[BCs]
[./bottomx]
type = DirichletBC
boundary = 0
variable = disp_x
value = 0.0
[../]
[./bottomy]
type = DirichletBC
boundary = 0
variable = disp_y
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
poissons_ratio = 0.3
youngs_modulus = 1e6
[../]
[./thermal_strain]
type = ComputeThermalExpansionEigenstrain
thermal_expansion_coeff = 0.02
stress_free_temperature = 0.5
eigenstrain_name = eigenstrain
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
line_search = none
# controls for linear iterations
l_max_its = 100
l_tol = 1e-06
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-14
nl_abs_tol = 1e-12
# time control
start_time = 0.0
dt = 1.0
dtmin = 1.0
end_time = 2.0
[]
[Outputs]
exodus = true
[]
(modules/richards/test/tests/dirac/bh27.i)
#2-phase version of bh07 (go to steadystate with borehole)
[Mesh]
type = FileMesh
file = bh07_input.e
[]
[GlobalParams]
richardsVarNames_UO = PPNames
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'
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1000 10000'
x = '100 1000'
[../]
[]
[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 = 0.6
al = 1E-5
[../]
[./SeffGas]
type = RichardsSeff2gasVG
m = 0.6
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 = RichardsSUPGnone
[../]
[./SUPGgas]
type = RichardsSUPGnone
[../]
[./borehole_total_outflow_mass]
type = RichardsSumQuantity
[../]
[]
[Variables]
[./pwater]
order = FIRST
family = LAGRANGE
[../]
[./pgas]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./water_ic]
type = FunctionIC
variable = pwater
function = 1E7
[../]
[./gas_ic]
type = FunctionIC
variable = pgas
function = 1E7
[../]
[]
[BCs]
[./fix_outer_w]
type = DirichletBC
boundary = perimeter
variable = pwater
value = 1E7
[../]
[./fix_outer_g]
type = DirichletBC
boundary = perimeter
variable = pgas
value = 1E7
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[Kernels]
active = 'richardsfwater richardstwater richardsfgas richardstgas'
[./richardstwater]
type = RichardsMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFullyUpwindFlux
variable = pwater
[../]
[./richardstgas]
type = RichardsMassChange
variable = pgas
[../]
[./richardsfgas]
type = RichardsFullyUpwindFlux
variable = pgas
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = SeffWater
pressure_vars = 'pwater pgas'
[../]
[]
[DiracKernels]
[./bh]
type = RichardsBorehole
bottom_pressure = 0
point_file = bh07.bh
SumQuantityUO = borehole_total_outflow_mass
fully_upwind = true
variable = pwater
unit_weight = '0 0 0'
re_constant = 0.1594
character = 2 # this is to make the length 1m borehole fill the entire 2m height
[../]
[./bh_gas_dummy]
type = RichardsBorehole
bottom_pressure = 0
point_file = bh07.bh
SumQuantityUO = borehole_total_outflow_mass
fully_upwind = true
variable = pgas
unit_weight = '0 0 0'
re_constant = 0.1594
character = 2 # this is to make the length 1m borehole fill the entire 2m height
[../]
[]
[Postprocessors]
[./bh_report]
type = RichardsPlotQuantity
uo = borehole_total_outflow_mass
execute_on = 'initial timestep_end'
[../]
[./water_mass]
type = RichardsMass
variable = pwater
execute_on = 'initial timestep_end'
[../]
[./gas_mass]
type = RichardsMass
variable = pgas
execute_on = 'initial timestep_end'
[../]
[]
[Materials]
[./all]
type = RichardsMaterial
block = 1
mat_porosity = 0.1
mat_permeability = '1E-11 0 0 0 1E-11 0 0 0 1E-11'
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./usual]
type = SMP
full = true
petsc_options = '-snes_converged_reason -ksp_diagonal_scale -ksp_diagonal_scale_fix -ksp_gmres_modifiedgramschmidt'
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -sub_pc_factor_shift_type -pc_asm_overlap -snes_atol -snes_rtol -snes_max_it -ksp_rtol -ksp_atol'
petsc_options_value = 'gmres asm lu NONZERO 2 1E-10 1E-10 20 1E-10 1E-100'
[../]
[]
[Executioner]
type = Transient
end_time = 1000
solve_type = NEWTON
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = bh27
execute_on = 'initial timestep_end final'
interval = 1000000
exodus = true
[]
(test/tests/geomsearch/2d_moving_penetration/restart2.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
file = pl_test1.e
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate10]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate13]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate14]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate15]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate16]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 0.7 -0.7 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-9
l_max_its = 10
dt = 0.05
end_time = 1.0
[]
[Outputs]
exodus = true
[]
[Problem]
restart_file_base = restart_out_cp/0010
[]
(modules/richards/test/tests/buckley_leverett/bl22_lumped_fu.i)
# two-phase version
# super-sharp front version
[Mesh]
type = GeneratedMesh
dim = 1
nx = 150
xmin = 0
xmax = 15
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = 'DensityWater DensityGas'
relperm_UO = 'RelPermWater RelPermGas'
SUPG_UO = 'SUPGwater SUPGgas'
sat_UO = 'SatWater SatGas'
seff_UO = 'SeffWater SeffGas'
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1E-4 1E-3 1E-2 2E-2 5E-2 6E-2 0.1 0.2'
x = '0 1E-2 1E-1 1 5 20 40 41'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = 'pwater pgas'
[../]
[./DensityWater]
type = RichardsDensityConstBulk
dens0 = 1000
bulk_mod = 2E6
[../]
[./DensityGas]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 2E6
[../]
[./SeffWater]
type = RichardsSeff2waterVG
m = 0.8
al = 1E-4
[../]
[./SeffGas]
type = RichardsSeff2gasVG
m = 0.8
al = 1E-4
[../]
[./RelPermWater]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./RelPermGas]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./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 = 1E-5
[../]
[./SUPGgas]
type = RichardsSUPGstandard
p_SUPG = 1E-5
[../]
[]
[Variables]
[./pwater]
order = FIRST
family = LAGRANGE
[../]
[./pgas]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[./bounds_dummy]
[../]
[]
[Kernels]
active = 'richardsfwater richardstwater richardsfgas richardstgas'
[./richardstwater]
type = RichardsLumpedMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFullyUpwindFlux
variable = pwater
[../]
[./richardstgas]
type = RichardsLumpedMassChange
variable = pgas
[../]
[./richardsfgas]
type = RichardsFullyUpwindFlux
variable = pgas
[../]
[./richardsppenalty]
type = RichardsPPenalty
variable = pgas
a = 1E-18
lower_var = pwater
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = SeffWater
pressure_vars = 'pwater pgas'
[../]
[]
[ICs]
[./water_ic]
type = FunctionIC
variable = pwater
function = initial_water
[../]
[./gas_ic]
type = FunctionIC
variable = pgas
function = initial_gas
[../]
[]
[BCs]
[./left_w]
type = DirichletBC
variable = pwater
boundary = left
value = 1E6
[../]
[./left_g]
type = DirichletBC
variable = pgas
boundary = left
value = 1000
[../]
[./right_w]
type = DirichletBC
variable = pwater
boundary = right
value = -100000
[../]
[./right_g]
type = DirichletBC
variable = pgas
boundary = right
value = 0
[../]
[]
[Functions]
[./initial_water]
type = ParsedFunction
value = 1000000*(1-min(x/5,1))-if(x<5,0,100000)
[../]
[./initial_gas]
type = ParsedFunction
value = 1000
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.15
mat_permeability = '1E-10 0 0 0 1E-10 0 0 0 1E-10'
viscosity = '1E-3 1E-6'
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./standard]
type = SMP
full = true
petsc_options = '-snes_converged_reason -ksp_diagonal_scale -ksp_diagonal_scale_fix -ksp_gmres_modifiedgramschmidt'
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -sub_pc_factor_shift_type -pc_asm_overlap -snes_atol -snes_rtol -snes_max_it -ksp_rtol -ksp_atol'
petsc_options_value = 'gmres asm lu NONZERO 2 1E-10 1E-10 20 1E-10 1E-100'
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
end_time = 50
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = bl22_lumped_fu
[./exodus]
type = Exodus
interval = 100000
hide = 'pgas bounds_dummy'
execute_on = 'initial final timestep_end'
[../]
[]
(modules/xfem/test/tests/moment_fitting/diffusion_moment_fitting_four_points.i)
# Test for a diffusion problem which uses four points moment_fitting approach.
# See this paper (https://doi.org/10.1007/s00466-018-1544-2) for more details about moment_fitting approach.
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 6
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[XFEM]
geometric_cut_userobjects = 'line_seg_cut_uo'
qrule = moment_fitting
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.5 1.0 0.5 0.5'
time_start_cut = 0.0
time_end_cut = 0.0
[../]
[]
[Variables]
[./u]
[../]
[]
[Functions]
[./u_left]
type = PiecewiseLinear
x = '0 2'
y = '0 0.1'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = FunctionDirichletBC
variable = u
boundary = 3
function = u_left
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Transient
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
start_time = 0.0
dt = 1.0
end_time = 2.0
[]
[Outputs]
interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/tensor_mechanics/test/tests/j_integral_vtest/c_int_surfbreak_ellip_crack_sym_mm.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[Mesh]
file = c_integral_coarse.e
partitioner = centroid
centroid_partitioner_direction = z
[]
[AuxVariables]
[./SED]
order = CONSTANT
family = MONOMIAL
[../]
[./resid_z]
[../]
[]
[Functions]
[./rampConstantUp]
type = PiecewiseLinear
x = '0. 0.1 100.0'
y = '0. 1 1'
scale_factor = -68.95 #MPa
[../]
[./dts]
type = PiecewiseLinear
x = '0 1'
y = '1 400000'
[../]
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
[../]
[]
[AuxKernels]
[./SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[../]
[]
[BCs]
[./crack_y]
type = DirichletBC
variable = disp_z
boundary = 6
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = 12
value = 0.0
[../]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./Pressure]
[./Side1]
boundary = 5
function = rampConstantUp
[../]
[../]
[] # BCs
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 206800
poissons_ratio = 0.0
[../]
[./radial_return_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'powerlawcrp'
[../]
[./powerlawcrp]
type = PowerLawCreepStressUpdate
coefficient = 3.125e-21 # 7.04e-17 #
n_exponent = 4.0
m_exponent = 0.0
activation_energy = 0.0
# max_inelastic_increment = 0.01
[../]
[]
[DomainIntegral]
integrals = CIntegral
boundary = 1001
crack_direction_method = CurvedCrackFront
crack_end_direction_method = CrackDirectionVector
crack_direction_vector_end_1 = '0.0 1.0 0.0'
crack_direction_vector_end_2 = '1.0 0.0 0.0'
radius_inner = '12.5 25.0 37.5'
radius_outer = '25.0 37.5 50.0'
intersecting_boundary = '1 2'
symmetry_plane = 2
incremental = true
inelastic_models = 'powerlawcrp'
[]
[Executioner]
type = Transient
# Two sets of linesearch options are for petsc 3.1 and 3.3 respectively
#Preconditioned JFNK (default)
solve_type = 'NEWTON'
# petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 4'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_abs_tol = 1e-3
nl_rel_tol = 1e-11
l_tol = 1e-2
start_time = 0.0
end_time = 401
[./TimeStepper]
type = FunctionDT
function = dts
min_dt = 1.0
[../]
[]
[Postprocessors]
[./_dt]
type = TimestepSize
[../]
[./nl_its]
type = NumNonlinearIterations
[../]
[./lin_its]
type = NumLinearIterations
[../]
[./react_z]
type = NodalSum
variable = resid_z
boundary = 5
[../]
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
csv = true
[]
(modules/richards/test/tests/buckley_leverett/bl22.i)
# two-phase version
# super-sharp front version
[Mesh]
type = GeneratedMesh
dim = 1
nx = 150
xmin = 0
xmax = 15
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1E-4 1E-3 1E-2 2E-2 5E-2 6E-2 0.1 0.2'
x = '0 1E-2 1E-1 1 5 20 40 41'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = 'pwater pgas'
[../]
[./DensityWater]
type = RichardsDensityConstBulk
dens0 = 1000
bulk_mod = 2E6
[../]
[./DensityGas]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 2E6
[../]
[./SeffWater]
type = RichardsSeff2waterVG
m = 0.8
al = 1E-4
[../]
[./SeffGas]
type = RichardsSeff2gasVG
m = 0.8
al = 1E-4
[../]
[./RelPermWater]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./RelPermGas]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./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 = 1E-5
[../]
[./SUPGgas]
type = RichardsSUPGstandard
p_SUPG = 1E-5
[../]
[]
[Variables]
[./pwater]
order = FIRST
family = LAGRANGE
[../]
[./pgas]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[./bounds_dummy]
[../]
[]
[Kernels]
active = 'richardsfwater richardstwater richardsfgas richardstgas'
[./richardstwater]
type = RichardsMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFlux
variable = pwater
[../]
[./richardstgas]
type = RichardsMassChange
variable = pgas
[../]
[./richardsfgas]
type = RichardsFlux
variable = pgas
[../]
[./richardsppenalty]
type = RichardsPPenalty
variable = pgas
a = 1E-18
lower_var = pwater
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = SeffWater
pressure_vars = 'pwater pgas'
[../]
[]
[ICs]
[./water_ic]
type = FunctionIC
variable = pwater
function = initial_water
[../]
[./gas_ic]
type = FunctionIC
variable = pgas
function = initial_gas
[../]
[]
[BCs]
[./left_w]
type = DirichletBC
variable = pwater
boundary = left
value = 1E6
[../]
[./left_g]
type = DirichletBC
variable = pgas
boundary = left
value = 1E6
[../]
[./right_w]
type = DirichletBC
variable = pwater
boundary = right
value = -100000
[../]
[./right_g]
type = DirichletBC
variable = pgas
boundary = right
value = 0
[../]
[]
[Functions]
[./initial_water]
type = ParsedFunction
value = 1000000*(1-min(x/5,1))-100000*(max(x-5,0)/max(abs(x-5),1E-10))
[../]
[./initial_gas]
type = ParsedFunction
value = max(1000000*(1-x/5),0)+1000
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.15
mat_permeability = '1E-10 0 0 0 1E-10 0 0 0 1E-10'
density_UO = 'DensityWater DensityGas'
relperm_UO = 'RelPermWater RelPermGas'
SUPG_UO = 'SUPGwater SUPGgas'
sat_UO = 'SatWater SatGas'
seff_UO = 'SeffWater SeffGas'
viscosity = '1E-3 1E-6'
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./standard]
type = SMP
full = true
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -ksp_rtol -ksp_atol'
petsc_options_value = 'bcgs bjacobi 1E-10 1E-10 20 1E-20 1E-20'
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
end_time = 50
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = bl22
print_linear_converged_reason = false
print_nonlinear_converged_reason = false
[./exodus]
type = Exodus
interval = 100000
hide = pgas
execute_on = 'initial final timestep_end'
[../]
[]
(modules/combined/test/tests/gap_heat_transfer_convex/gap_heat_transfer_convex_gap_offsets.i)
#The two blocks were moved apart by the value of 0.005 in the y-direction, respectively.
#This value was compensated by the gap offsets from both secondary and primary sides
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
temperature = temp
[]
[Mesh]
file = gap_heat_transfer_convex_gap_offsets.e
[]
[Functions]
[./disp]
type = PiecewiseLinear
x = '0 2.0'
y = '0 1.0'
[../]
[./temp]
type = PiecewiseLinear
x = '0 1'
y = '200 200'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[./temp]
initial_condition = 100
[../]
[]
[AuxVariables]
[./primary_gap_offset]
[../]
[./secondary_gap_offset]
[../]
[./mapped_primary_gap_offset]
[../]
[]
[AuxKernels]
[./primary_gap_offset]
type = ConstantAux
variable = primary_gap_offset
value = -0.005
boundary = 2
[../]
[./mapped_primary_gap_offset]
type = GapValueAux
variable = mapped_primary_gap_offset
paired_variable = primary_gap_offset
boundary = 3
paired_boundary = 2
[../]
[./secondary_gap_offset]
type = ConstantAux
variable = secondary_gap_offset
value = -0.005
boundary = 3
[../]
[]
[ThermalContact]
[./thermal_contact]
type = GapHeatTransfer
variable = temp
primary = 2
secondary = 3
emissivity_primary = 0
emissivity_secondary = 0
secondary_gap_offset = secondary_gap_offset
mapped_primary_gap_offset = mapped_primary_gap_offset
[../]
[]
[Modules/TensorMechanics/Master/All]
volumetric_locking_correction = true
strain = FINITE
eigenstrain_names = eigenstrain
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[]
[BCs]
[./move_right]
type = FunctionDirichletBC
boundary = '3'
variable = disp_x
function = disp
[../]
[./fixed_x]
type = DirichletBC
boundary = '1'
variable = disp_x
value = 0
[../]
[./fixed_y]
type = DirichletBC
boundary = '1 2 3 4'
variable = disp_y
value = 0
[../]
[./fixed_z]
type = DirichletBC
boundary = '1 2 3 4'
variable = disp_z
value = 0
[../]
[./temp_bottom]
type = FunctionDirichletBC
boundary = 1
variable = temp
function = temp
[../]
[./temp_top]
type = DirichletBC
boundary = 4
variable = temp
value = 100
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = '1 2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./thermal_strain]
type = ComputeThermalExpansionEigenstrain
stress_free_temperature = 100
thermal_expansion_coeff = 0
eigenstrain_name = eigenstrain
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[./heat1]
type = HeatConductionMaterial
block = 1
specific_heat = 1.0
thermal_conductivity = 1.0
[../]
[./heat2]
type = HeatConductionMaterial
block = 2
specific_heat = 1.0
thermal_conductivity = 1.0
[../]
[./density]
type = Density
block = '1 2'
density = 1.0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
start_time = 0.0
dt = 0.1
end_time = 2.0
[]
[Outputs]
exodus = true
[]
(modules/richards/test/tests/gravity_head_1/gh21.i)
# investigating validity of immobile saturation
# 5 elements, with SUPG
[Mesh]
type = GeneratedMesh
dim = 1
nx = 5
xmin = -1
xmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1 10 100 1000 10000'
x = '0 10 100 1000 10000'
[../]
[]
[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 = 0.3
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 1.0E-6
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
initial_condition = -1.0
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[Kernels]
active = 'richardsf richardst'
[./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-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 = Transient
solve_type = Newton
dt = 1E0
end_time = 1E5
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = gh21
execute_on = 'timestep_end final'
interval = 10000
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
[]
(test/tests/geomsearch/3d_moving_penetration/pl_test3q.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
file = pl_test3q.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./normal_z]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./closest_point_z]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[./diff_z]
type = Diffusion
variable = disp_z
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = normal_z
boundary = 11
paired_boundary = 12
quantity = normal_z
[../]
[./penetrate10]
type = PenetrationAux
variable = normal_z
boundary = 12
paired_boundary = 11
quantity = normal_z
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate13]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate14]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate15]
type = PenetrationAux
variable = closest_point_z
boundary = 11
paired_boundary = 12
quantity = closest_point_z
[../]
[./penetrate16]
type = PenetrationAux
variable = closest_point_z
boundary = 12
paired_boundary = 11
quantity = closest_point_z
[../]
[./penetrate17]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate18]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate19]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate20]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
preset = false
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
preset = false
boundary = 1
value = 0
[../]
[./b1z]
type = DirichletBC
variable = disp_z
preset = false
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
preset = false
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
preset = false
boundary = 2
function = disp_y
[../]
[./b2z]
type = DirichletBC
variable = disp_z
preset = false
boundary = 2
value = 0
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-9
l_max_its = 10
start_time = 0.0
dt = 0.025
end_time = 1.0
[./Quadrature]
order = THIRD
[../]
[]
[Outputs]
file_base = pl_test3q_out
exodus = true
[]
(modules/tensor_mechanics/test/tests/line_material_rank_two_sampler/rank_two_sampler.i)
[GlobalParams]
displacements = 'x_disp y_disp z_disp'
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 3
ny = 3
nz = 3
elem_type = HEX
[]
[Functions]
[./rampConstant]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = 1e-6
[../]
[]
[Variables]
[./x_disp]
order = FIRST
family = LAGRANGE
[../]
[./y_disp]
order = FIRST
family = LAGRANGE
[../]
[./z_disp]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
[../]
[]
[VectorPostprocessors]
[./stress_xx]
type = LineMaterialRankTwoSampler
start = '0.1667 0.4 0.45'
end = '0.8333 0.6 0.55'
property = stress
index_i = 0
index_j = 0
sort_by = id
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
[../]
[]
[BCs]
[./front]
type = FunctionDirichletBC
variable = z_disp
boundary = 5
function = rampConstant
[../]
[./back_x]
type = DirichletBC
variable = x_disp
boundary = 0
value = 0.0
[../]
[./back_y]
type = DirichletBC
variable = y_disp
boundary = 0
value = 0.0
[../]
[./back_z]
type = DirichletBC
variable = z_disp
boundary = 0
value = 0.0
[../]
[]
[Materials]
[./elast_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = .3
[../]
[./strain]
type = ComputeSmallStrain
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
l_max_its = 100
start_time = 0.0
num_steps = 99999
end_time = 1.0
dt = 0.1
[]
[Outputs]
file_base = rank_two_sampler_out
exodus = true
csv = true
[]
(modules/combined/test/tests/cavity_pressure/additional_volume.i)
#
# Cavity Pressure Test
#
# This test is designed to compute an internal pressure based on
# p = n * R * / (V_cavity / T_cavity + V_add / T_add)
# where
# p is the pressure
# n is the amount of material in the volume (moles)
# R is the universal gas constant
# T_cavity is the temperature in the cavity
# T_add is the temperature of the additional volume
#
# The mesh is composed of one block (1) with an interior cavity of volume 8.
# Block 2 sits in the cavity and has a volume of 1. Thus, the total
# initial volume is 7. An additional volume of 2 is added.
#
# The test adjusts n, T, and V in the following way:
# n => n0 + alpha * t
# T => T0 + beta * t
# V => V_cavity0 + gamma * t + V_add
# with
# alpha = n0
# beta = T0 / 2
# gamma = -(0.003322259...) * V0
# T0 = 240.54443866068704
# V_cavity0 = 7
# V_add = 2
# T_add = 100
# n0 = f(p0)
# p0 = 100
# R = 8.314472 J * K^(-1) * mol^(-1)
#
# An additional volume of 2 with a temperature of 100.0 is included.
#
# So, n0 = p0 * (V_cavity / T_cavity + V_add / T_add) / R
# = 100 * (7 / 240.544439 + 2 / 100) / 8.314472
# = 0.59054
#
# The parameters combined at t = 1 gives p = 249.647.
#
# This test sets the initial temperature to 500, but the CavityPressure
# is told that that initial temperature is T0. Thus, the final solution
# is unchanged.
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
file = 3d.e
[]
[GlobalParams]
volumetric_locking_correction = true
[]
[Functions]
[./displ_positive]
type = PiecewiseLinear
x = '0 1'
y = '0 0.0029069767441859684'
[../]
[./displ_negative]
type = PiecewiseLinear
x = '0 1'
y = '0 -0.0029069767441859684'
[../]
[./temp1]
type = PiecewiseLinear
x = '0 1'
y = '1 1.5'
scale_factor = 240.54443866068704
[../]
[./material_input_function]
type = PiecewiseLinear
x = '0 1'
y = '0 0.59054'
[../]
[./additional_volume]
type = ConstantFunction
value = 2
[../]
[./temperature_of_additional_volume]
type = ConstantFunction
value = 100
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[./temp]
initial_condition = 500
[../]
[./material_input]
[../]
[]
[AuxVariables]
[./pressure_residual_x]
[../]
[./pressure_residual_y]
[../]
[./pressure_residual_z]
[../]
[./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_zx]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
[../]
[./heat]
type = Diffusion
variable = temp
use_displaced_mesh = true
[../]
[./material_input_dummy]
type = Diffusion
variable = material_input
use_displaced_mesh = true
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 0
variable = stress_xx
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 1
variable = stress_yy
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 2
variable = stress_zz
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 1
variable = stress_xy
[../]
[./stress_yz]
type = RankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 2
variable = stress_yz
[../]
[./stress_zx]
type = RankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 0
variable = stress_zx
[../]
[]
[BCs]
[./no_x_exterior]
type = DirichletBC
variable = disp_x
boundary = '7 8'
value = 0.0
[../]
[./no_y_exterior]
type = DirichletBC
variable = disp_y
boundary = '9 10'
value = 0.0
[../]
[./no_z_exterior]
type = DirichletBC
variable = disp_z
boundary = '11 12'
value = 0.0
[../]
[./prescribed_left]
type = FunctionDirichletBC
variable = disp_x
boundary = 13
function = displ_positive
[../]
[./prescribed_right]
type = FunctionDirichletBC
variable = disp_x
boundary = 14
function = displ_negative
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = '15 16'
value = 0.0
[../]
[./no_z]
type = DirichletBC
variable = disp_z
boundary = '17 18'
value = 0.0
[../]
[./no_x_interior]
type = DirichletBC
variable = disp_x
boundary = '1 2'
value = 0.0
[../]
[./no_y_interior]
type = DirichletBC
variable = disp_y
boundary = '3 4'
value = 0.0
[../]
[./no_z_interior]
type = DirichletBC
variable = disp_z
boundary = '5 6'
value = 0.0
[../]
[./temperatureInterior]
type = FunctionDirichletBC
boundary = 100
function = temp1
variable = temp
[../]
[./MaterialInput]
type = FunctionDirichletBC
boundary = '100 13 14 15 16'
function = material_input_function
variable = material_input
[../]
[./CavityPressure]
[./1]
boundary = 100
initial_pressure = 100
material_input = materialInput
R = 8.314472
temperature = aveTempInterior
initial_temperature = 240.54443866068704
volume = internalVolume
startup_time = 0.5
output = ppress
save_in = 'pressure_residual_x pressure_residual_y pressure_residual_z'
additional_volumes = volume1
temperature_of_additional_volumes = temperature1
[../]
[../]
[]
[Materials]
[./elast_tensor1]
type = ComputeElasticityTensor
C_ijkl = '0 5'
fill_method = symmetric_isotropic
block = 1
[../]
[./strain1]
type = ComputeFiniteStrain
block = 1
[../]
[./stress1]
type = ComputeFiniteStrainElasticStress
block = 1
[../]
[./elast_tensor2]
type = ComputeElasticityTensor
C_ijkl = '0 5'
fill_method = symmetric_isotropic
block = 2
[../]
[./strain2]
type = ComputeFiniteStrain
block = 2
[../]
[./stress2]
type = ComputeFiniteStrainElasticStress
block = 2
[../]
[]
[Executioner]
type = Transient
petsc_options_iname = '-pc_type -sub_pc_type'
petsc_options_value = 'asm lu'
nl_rel_tol = 1e-12
l_tol = 1e-12
l_max_its = 20
dt = 0.5
end_time = 1.0
snesmf_reuse_base = false
[]
[Postprocessors]
[./internalVolume]
type = InternalVolume
boundary = 100
execute_on = 'initial linear'
[../]
[./aveTempInterior]
type = SideAverageValue
boundary = 100
variable = temp
execute_on = 'initial linear'
[../]
[./materialInput]
type = SideAverageValue
boundary = '7 8 9 10 11 12'
variable = material_input
execute_on = linear
[../]
[./volume1]
type = FunctionValuePostprocessor
function = additional_volume
execute_on = 'initial linear'
[../]
[./temperature1]
type = FunctionValuePostprocessor
function = temperature_of_additional_volume
execute_on = 'initial linear'
[../]
[]
[Outputs]
exodus = true
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_radiation/gap_heat_transfer_radiation_test.i)
#
# 1-D Gap Heat Transfer Test without mechanics
#
# This test exercises 1-D gap heat transfer for a helium-filled gap including radiation.
#
# The mesh consists of two element blocks containing one element each. Each
# element is a unit cube. They sit next to one another with a unit between them.
#
# The conductivity of both blocks is set very large to achieve a uniform temperature
# across each block. The temperature of the far left boundary
# is ramped from 100 to 200 over one time unit, and then held fixed for an additional
# time unit. The temperature of the far right boundary is held fixed at 100.
#
# A simple analytical solution is possible for the heat flux between the blocks:
#
# Flux = (T_left - T_right) * h_gap
#
# where h_gap = h_gas + h_cont + h_rad
#
# By setting the contact pressure, roughnesses, and jump distances to zero, the gap
# conductance simplifies to:
#
# h_gap = gapK/d_gap + sigma*Fe*(T_left^2 + T_right^2)*(T_left + T_right)
#
# where Fe = 1/(1/eps_left + 1/eps_right - 1)
# eps = emissivity
#
# For pure helium, BISON computes the gas conductivity as:
#
# gapK(Tavg) = 2.639e-3*Tavg^0.7085
#
# For the test, the final (t=2) average gas temperature is (200 +100)/2 = 150,
# giving gapK(150) = 0.09187557
#
# Assuming ems_left = ems_right = 0.5, Fe = 1/3
#
# The heat flux across the gap at that time is then:
#
# Flux(2) = 100 * ((0.09187557/1.0) + (5.669e-8/3)*(200^2 + 100^2)*(200 + 100))
# = 37.532557
#
# The flux post processors give 37.53255
#
[Mesh]
file = gap_heat_transfer_radiation_test.e
[]
[Functions]
[./temp]
type = PiecewiseLinear
x = '0 1'
y = '200 200'
[../]
[]
[Variables]
[./temp]
order = FIRST
family = LAGRANGE
initial_condition = 100
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[]
[BCs]
[./temp_far_left]
type = FunctionDirichletBC
boundary = 1
variable = temp
function = temp
[../]
[./temp_far_right]
type = DirichletBC
boundary = 4
variable = temp
value = 100
[../]
[]
[ThermalContact]
[./gap]
type = GapHeatTransfer
variable = temp
primary = 3
secondary = 2
gap_conductivity = 0.09187557
emissivity_primary = 0.5
emissivity_secondary = 0.5
[../]
[]
[Materials]
[./heat1]
type = HeatConductionMaterial
block = '1 2'
specific_heat = 1.0
thermal_conductivity = 10000000.0
[../]
[./density]
type = GenericConstantMaterial
block = '1 2'
prop_names = 'density'
prop_values = '1.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 4'
line_search = 'none'
nl_abs_tol = 1e-6
nl_rel_tol = 1e-10
l_tol = 1e-3
l_max_its = 100
start_time = 0.0
dt = 1
end_time = 1.0
[]
[Postprocessors]
[./temp_left]
type = SideAverageValue
boundary = 2
variable = temp
execute_on = 'initial timestep_end'
[../]
[./temp_right]
type = SideAverageValue
boundary = 3
variable = temp
execute_on = 'initial timestep_end'
[../]
[./flux_left]
type = SideFluxIntegral
variable = temp
boundary = 2
diffusivity = thermal_conductivity
[../]
[./flux_right]
type = SideFluxIntegral
variable = temp
boundary = 3
diffusivity = thermal_conductivity
[../]
[]
[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/geomsearch/3d_moving_penetration_smoothing/pl_test3qnstt.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
file = pl_test3qtt.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./normal_z]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./closest_point_z]
[../]
# [./element_id]
# [../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[./diff_z]
type = Diffusion
variable = disp_z
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
tangential_tolerance = 0.09
normal_smoothing_distance = 0.2
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
tangential_tolerance = 0.09
normal_smoothing_distance = 0.2
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = normal_z
boundary = 11
paired_boundary = 12
quantity = normal_z
[../]
[./penetrate10]
type = PenetrationAux
variable = normal_z
boundary = 12
paired_boundary = 11
quantity = normal_z
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate13]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate14]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate15]
type = PenetrationAux
variable = closest_point_z
boundary = 11
paired_boundary = 12
quantity = closest_point_z
[../]
[./penetrate16]
type = PenetrationAux
variable = closest_point_z
boundary = 12
paired_boundary = 11
quantity = closest_point_z
[../]
# [./penetrate17]
# type = PenetrationAux
# variable = element_id
# boundary = 11
# paired_boundary = 12
# quantity = element_id
# [../]
#
# [./penetrate18]
# type = PenetrationAux
# variable = element_id
# boundary = 12
# paired_boundary = 11
# quantity = element_id
# [../]
[./penetrate19]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate20]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
preset = false
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
preset = false
boundary = 1
value = 0
[../]
[./b1z]
type = DirichletBC
variable = disp_z
preset = false
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
preset = false
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
preset = false
boundary = 2
function = disp_y
[../]
[./b2z]
type = DirichletBC
variable = disp_z
preset = false
boundary = 2
value = 0
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_abs_tol = 1e-7
l_max_its = 10
start_time = 0.0
dt = 0.02
end_time = 1.0
[./Quadrature]
order = THIRD
[../]
[]
[Outputs]
file_base = pl_test3qnstt_out
exodus = true
[]
(modules/tensor_mechanics/test/tests/thermal_expansion_function/small_linear.i)
# This tests the thermal expansion coefficient function using both
# options to specify that function: mean and instantaneous. There
# two blocks, each containing a single element, and these use the
# two variants of the function.
# In this test, the instantaneous CTE function is a linear function
# while the mean CTE function is an analytic function designed to
# give the same response. If \bar{alpha}(T) is the mean CTE function,
# and \alpha(T) is the instantaneous CTE function,
# \bar{\alpha}(T) = 1/(T-Tref) \intA^{T}_{Tsf} \alpha(T) dT
# where Tref is the reference temperature used to define the mean CTE
# function, and Tsf is the stress-free temperature.
# This version of the test uses small deformation theory. The results
# from the two models are identical.
[Mesh]
file = 'blocks.e'
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[AuxVariables]
[./temp]
order = FIRST
family = LAGRANGE
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
add_variables = true
eigenstrain_names = eigenstrain
generate_output = 'strain_xx strain_yy strain_zz'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = disp_x
boundary = 3
value = 0.0
[../]
[./bottom]
type = DirichletBC
variable = disp_y
boundary = 2
value = 0.0
[../]
[./back]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0.0
[../]
[]
[AuxKernels]
[./temp]
type = FunctionAux
variable = temp
block = '1 2'
function = temp_func
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./small_stress]
type = ComputeLinearElasticStress
[../]
[./thermal_expansion_strain1]
type = ComputeMeanThermalExpansionFunctionEigenstrain
block = 1
thermal_expansion_function = cte_func_mean
thermal_expansion_function_reference_temperature = 0.5
stress_free_temperature = 0.0
temperature = temp
eigenstrain_name = eigenstrain
[../]
[./thermal_expansion_strain2]
type = ComputeInstantaneousThermalExpansionFunctionEigenstrain
block = 2
thermal_expansion_function = cte_func_inst
stress_free_temperature = 0.0
temperature = temp
eigenstrain_name = eigenstrain
[../]
[]
[Functions]
[./cte_func_mean]
type = ParsedFunction
vars = 'tsf tref scale' #stress free temp, reference temp, scale factor
vals = '0.0 0.5 1e-4'
value = 'scale * (0.5 * t^2 - 0.5 * tsf^2) / (t - tref)'
[../]
[./cte_func_inst]
type = PiecewiseLinear
xy_data = '0 0.0
2 2.0'
scale_factor = 1e-4
[../]
[./temp_func]
type = PiecewiseLinear
xy_data = '0 1
1 2'
[../]
[]
[Postprocessors]
[./disp_1]
type = NodalMaxValue
variable = disp_x
boundary = 101
[../]
[./disp_2]
type = NodalMaxValue
variable = disp_x
boundary = 102
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
l_max_its = 100
l_tol = 1e-4
nl_abs_tol = 1e-8
nl_rel_tol = 1e-12
start_time = 0.0
end_time = 1.0
dt = 0.1
[]
[Outputs]
csv = true
[]
(modules/combined/test/tests/evolving_mass_density/rz_tensors.i)
# Constant mass in RZ using Tensor Mechanics
#
# This test forces an RZ mesh to move through a series of displacements
# in order to test whether the mass is constant. The density is chosen
# such that the mass is 2.5.
# This test is a duplicate of the rz.i test for solid mechanics, and the
# output of this tensor mechanics test is compared to the original
# solid mechanics output. The duplication is necessary to test the
# migrated tensor mechanics version while maintaining tests for solid mechanics.
[Mesh]
file = elastic_patch_rz.e
[]
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Problem]
coord_type = RZ
[]
[Functions]
[./x101]
type = PiecewiseLinear
x = '0 5 6'
y = '0 0 0.24'
[../]
[./y101]
type = PiecewiseLinear
x = '0 6'
y = '0 0'
[../]
[./x102]
type = PiecewiseLinear
x = '0 4 5'
y = '0 0 0.24'
[../]
[./y102]
type = PiecewiseLinear
x = '0 1 2 3'
y = '0 0 0.12 0'
[../]
[./x103]
type = PiecewiseLinear
x = '0 4 5'
y = '0 0 0.24'
[../]
[./y103]
type = PiecewiseLinear
x = '0 1 3 4'
y = '0 0.12 0.12 0'
[../]
[./x104]
type = PiecewiseLinear
x = '0 5 6'
y = '0 0 0.24'
[../]
[./y104]
type = PiecewiseLinear
x = '0 2 3 4'
y = '0 0 0.12 0'
[../]
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
[../]
[]
[BCs]
[./101x]
type = FunctionDirichletBC
variable = disp_x
boundary = 101
function = x101
[../]
[./101y]
type = FunctionDirichletBC
variable = disp_y
boundary = 101
function = y101
[../]
[./102x]
type = FunctionDirichletBC
variable = disp_x
boundary = 102
function = x102
[../]
[./102y]
type = FunctionDirichletBC
variable = disp_y
boundary = 102
function = y102
[../]
[./103x]
type = FunctionDirichletBC
variable = disp_x
boundary = 103
function = x103
[../]
[./103y]
type = FunctionDirichletBC
variable = disp_y
boundary = 103
function = y103
[../]
[./104x]
type = FunctionDirichletBC
variable = disp_x
boundary = 104
function = x104
[../]
[./104y]
type = FunctionDirichletBC
variable = disp_y
boundary = 104
function = y104
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = PATCH
youngs_modulus = 1e6
poissons_ratio = 0.0
[../]
[./small_strain_rz]
type = ComputeAxisymmetricRZSmallStrain
block = PATCH
[../]
[./elastic_stress]
type = ComputeLinearElasticStress
block = PATCH
[../]
[]
[Executioner]
type = Transient
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
# Two sets of linesearch options are for petsc 3.1 and 3.3 respectively
petsc_options_iname = '-pc_type -ksp_gmres_restart'
petsc_options_value = 'lu 101'
line_search = 'none'
nl_abs_tol = 1e-10
l_max_its = 20
start_time = 0.0
dt = 1
num_steps = 6
end_time = 6.0
[]
[Outputs]
[./out]
type = Exodus
elemental_as_nodal = true
file_base = rz_out
[../]
[]
[Postprocessors]
[./mass]
type = Mass
variable = disp_x
execute_on = 'initial timestep_end'
[../]
[]
(modules/tensor_mechanics/test/tests/beam/fric_constraint/2_block_common_cross.i)
# Test for LineElementAction on multiple blocks by placing parameters
# common to all blocks outside of the individual action blocks
# 2 beams of length 1m are fixed at one end and a force of 1e-4 N
# is applied at the other end of the beams. Beam 1 is in block 1
# and beam 2 is in block 2. All the material properties for the two
# beams are identical. The moment of inertia of beam 2 is twice that
# of beam 1.
# Since the end displacement of a cantilever beam is inversely proportional
# to the moment of inertia, the y displacement at the end of beam 1 should be twice
# that of beam 2.
[Mesh]
type = FileMesh
file = test_fric_cross.e
#displacements = 'disp_x disp_y disp_z'
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = '1 2 3'
value = 0.0
[../]
[./fixy1]
type = DirichletBC
variable = disp_y
boundary = '1 2 3'
value = 0.0
[../]
[./fixz1]
type = DirichletBC
variable = disp_z
boundary = '1 3'
value = 0.0
[../]
[./fixr1]
type = DirichletBC
variable = rot_x
boundary = '1 2 3'
value = 0.0
[../]
[./fixr2]
type = DirichletBC
variable = rot_y
boundary = '1 2 3'
value = 0.0
[../]
[./fixr3]
type = DirichletBC
variable = rot_z
boundary = '1 2 3'
value = 0.0
[../]
[./move_z4]
type = FunctionDirichletBC
variable = disp_z
boundary = 2
function = pull
[../]
[]
[Functions]
[./pull]
type = PiecewiseLinear
x = '0.0 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'
y = '0.0 0.0 -0.2 -0.4 -0.6 -0.8 -0.6 -0.4 -0.2 0.0 0.2 0.4 0.6 0.8'
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
line_search = 'none'
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 5e-5
l_max_its = 10
dt = 1
dtmin = 1
end_time = 13
[]
[Modules/TensorMechanics/LineElementMaster]
# parameters common to all blocks
add_variables = true
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
# Geometry parameters
area = 0.5
y_orientation = '0.0 1.0 0.0'
[./block_1]
Iy = 1e-5
Iz = 1e-5
block = 1
[../]
[./block_2]
Iy = 8e-4
Iz = 8e-4
block = '2 3'
[../]
[]
[Materials]
[./stress]
type = ComputeBeamResultants
block = '1 2 3'
[../]
[./elasticity_1]
type = ComputeElasticityBeam
youngs_modulus = 2.0
poissons_ratio = 0.3
shear_coefficient = 1.0
block = '1 2 3'
[../]
[]
[Constraints]
[./tie_z]
type = NodalFrictionalConstraint
normal_force = 0.006
tangential_penalty = 100
friction_coefficient = 0.5
boundary = 6
secondary = 4
variable = disp_z
[../]
[./tie_z2]
type = NodalFrictionalConstraint
normal_force = 0.006
tangential_penalty = 100
friction_coefficient = 0.2
boundary = 6
secondary = 5
variable = disp_z
[../]
[]
[Postprocessors]
[./disp_x_1]
type = NodalVariableValue
nodeid = 1
variable = disp_x
[../]
[./disp_x_2]
type = NodalVariableValue
nodeid = 2
variable = disp_x
[../]
[./disp_z_1]
type = NodalVariableValue
nodeid = 1
variable = disp_z
[../]
[./disp_z_2]
type = NodalVariableValue
nodeid = 2
variable = disp_z
[../]
[]
[Outputs]
#file_base = '2_block_out'
exodus = true
[]
(modules/tensor_mechanics/test/tests/central_difference/consistent/3D/3d_consistent_explicit.i)
# One element test to test the central difference time integrator in 3D.
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 2
xmin = 0.0
xmax = 1
ymin = 0.0
ymax = 1
zmin = 0.0
zmax = 2
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./vel_x]
[../]
[./accel_x]
[../]
[./vel_y]
[../]
[./accel_y]
[../]
[./vel_z]
[../]
[./accel_z]
[../]
[]
[AuxKernels]
[./accel_x]
type = TestNewmarkTI
variable = accel_x
displacement = disp_x
first = false
[../]
[./vel_x]
type = TestNewmarkTI
variable = vel_x
displacement = disp_x
[../]
[./accel_y]
type = TestNewmarkTI
variable = accel_y
displacement = disp_y
first = false
[../]
[./vel_y]
type = TestNewmarkTI
variable = vel_y
displacement = disp_x
[../]
[./accel_z]
type = TestNewmarkTI
variable = accel_z
displacement = disp_z
first = false
[../]
[./vel_z]
type = TestNewmarkTI
variable = vel_z
displacement = disp_z
[../]
[]
[Kernels]
[./DynamicTensorMechanics]
displacements = 'disp_x disp_y disp_z'
[../]
[./inertia_x]
type = InertialForce
variable = disp_x
[../]
[./inertia_y]
type = InertialForce
variable = disp_y
[../]
[./inertia_z]
type = InertialForce
variable = disp_z
[../]
[]
[BCs]
[./x_bot]
type = FunctionDirichletBC
variable = disp_x
boundary = 'back'
function = dispx
preset = false
[../]
[./y_bot]
type = FunctionDirichletBC
variable = disp_y
boundary = 'back'
function = dispy
preset = false
[../]
[./z_bot]
type = FunctionDirichletBC
variable = disp_z
boundary = 'back'
function = dispz
preset = false
[../]
[./Periodic]
[./x_dir]
variable = 'disp_x disp_y disp_z'
primary = 'left'
secondary = 'right'
translation = '1.0 0.0 0.0'
[../]
[./y_dir]
variable = 'disp_x disp_y disp_z'
primary = 'bottom'
secondary = 'top'
translation = '0.0 1.0 0.0'
[../]
[../]
[]
[Functions]
[./dispx]
type = PiecewiseLinear
x = '0.0 1.0 2.0 3.0 4.0' # time
y = '0.0 1.0 0.0 -1.0 0.0' # displacement
[../]
[./dispy]
type = ParsedFunction
value = 0.1*t*t*sin(10*t)
[../]
[./dispz]
type = ParsedFunction
value = 0.1*t*t*sin(20*t)
[../]
[]
[Materials]
[./elasticity_tensor_block]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.25
block = 0
[../]
[./strain_block]
type = ComputeIncrementalSmallStrain
block = 0
displacements = 'disp_x disp_y disp_z'
implicit = false
[../]
[./stress_block]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = density
prop_values = 1e4
[../]
[]
[Executioner]
type = Transient
start_time = -0.01
end_time = 0.1
dt = 0.005
timestep_tolerance = 1e-6
[./TimeIntegrator]
type = CentralDifference
[../]
[]
[Postprocessors]
[./accel_6x]
type = NodalVariableValue
nodeid = 6
variable = accel_x
[../]
[]
[Outputs]
exodus = false
csv = true
[]
(modules/richards/test/tests/rogers_stallybrass_clements/rsc01.i)
# RSC test with high-res time and spatial resolution
[Mesh]
type = GeneratedMesh
dim = 2
nx = 600
ny = 1
xmin = 0
xmax = 10 # x is the depth variable, called zeta in RSC
ymin = 0
ymax = 0.05
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '3E-3 3E-2 0.05'
x = '0 1 5'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = 'pwater poil'
[../]
[./DensityWater]
type = RichardsDensityConstBulk
dens0 = 10
bulk_mod = 2E9
[../]
[./DensityOil]
type = RichardsDensityConstBulk
dens0 = 20
bulk_mod = 2E9
[../]
[./SeffWater]
type = RichardsSeff2waterRSC
oil_viscosity = 2E-3
scale_ratio = 2E3
shift = 10
[../]
[./SeffOil]
type = RichardsSeff2gasRSC
oil_viscosity = 2E-3
scale_ratio = 2E3
shift = 10
[../]
[./RelPerm]
type = RichardsRelPermMonomial
simm = 0
n = 1
[../]
[./Saturation]
type = RichardsSat
s_res = 0.0
sum_s_res = 0.0
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 1.0E-2
[../]
[]
[Variables]
[./pwater]
[../]
[./poil]
[../]
[]
[ICs]
[./water_init]
type = ConstantIC
variable = pwater
value = 0
[../]
[./oil_init]
type = ConstantIC
variable = poil
value = 15
[../]
[]
[Kernels]
[./richardstwater]
type = RichardsMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFlux
variable = pwater
[../]
[./richardstoil]
type = RichardsMassChange
variable = poil
[../]
[./richardsfoil]
type = RichardsFlux
variable = poil
[../]
[]
[AuxVariables]
[./SWater]
[../]
[./SOil]
[../]
[]
[AuxKernels]
[./Seff1VGwater_AuxK]
type = RichardsSeffAux
variable = SWater
seff_UO = SeffWater
pressure_vars = 'pwater poil'
[../]
[./Seff1VGoil_AuxK]
type = RichardsSeffAux
variable = SOil
seff_UO = SeffOil
pressure_vars = 'pwater poil'
[../]
[]
[BCs]
# we are pumping water into a system that has virtually incompressible fluids, hence the pressures rise enormously. this adversely affects convergence because of almost-overflows and precision-loss problems. The fixed things help keep pressures low and so prevent these awful behaviours. the movement of the saturation front is the same regardless of the fixed things.
active = 'recharge fixedoil fixedwater'
[./recharge]
type = RichardsPiecewiseLinearSink
variable = pwater
boundary = 'left'
pressures = '-1E10 1E10'
bare_fluxes = '-1 -1'
use_mobility = false
use_relperm = false
[../]
[./fixedwater]
type = DirichletBC
variable = pwater
boundary = 'right'
value = 0
[../]
[./fixedoil]
type = DirichletBC
variable = poil
boundary = 'right'
value = 15
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.25
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
density_UO = 'DensityWater DensityOil'
relperm_UO = 'RelPerm RelPerm'
SUPG_UO = 'SUPGstandard SUPGstandard'
sat_UO = 'Saturation Saturation'
seff_UO = 'SeffWater SeffOil'
viscosity = '1E-3 2E-3'
gravity = '0E-0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
active = 'andy'
[./andy]
type = SMP
full = true
petsc_options = ''
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-10 1E-10 10000'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
petsc_options = '-snes_converged_reason'
end_time = 5
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = rsc01
interval = 100000
execute_on = 'initial final'
exodus = true
[]
(modules/richards/test/tests/rogers_stallybrass_clements/rsc_fu_02.i)
# RSC test with low-res time and spatial resolution
[Mesh]
type = GeneratedMesh
dim = 2
nx = 200
ny = 1
xmin = 0
xmax = 10 # x is the depth variable, called zeta in RSC
ymin = 0
ymax = 0.05
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = 'DensityWater DensityOil'
relperm_UO = 'RelPerm RelPerm'
SUPG_UO = 'SUPGstandard SUPGstandard'
sat_UO = 'Saturation Saturation'
seff_UO = 'SeffWater SeffOil'
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '3E-2 5E-1 8E-1'
x = '0 1 5'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = 'pwater poil'
[../]
[./DensityWater]
type = RichardsDensityConstBulk
dens0 = 10
bulk_mod = 2E9
[../]
[./DensityOil]
type = RichardsDensityConstBulk
dens0 = 20
bulk_mod = 2E9
[../]
[./SeffWater]
type = RichardsSeff2waterRSC
oil_viscosity = 2E-3
scale_ratio = 2E3
shift = 10
[../]
[./SeffOil]
type = RichardsSeff2gasRSC
oil_viscosity = 2E-3
scale_ratio = 2E3
shift = 10
[../]
[./RelPerm]
type = RichardsRelPermMonomial
simm = 0
n = 1
[../]
[./Saturation]
type = RichardsSat
s_res = 0.0
sum_s_res = 0.0
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 1.0E-2
[../]
[]
[Variables]
[./pwater]
[../]
[./poil]
[../]
[]
[ICs]
[./water_init]
type = ConstantIC
variable = pwater
value = 0
[../]
[./oil_init]
type = ConstantIC
variable = poil
value = 15
[../]
[]
[Kernels]
[./richardstwater]
type = RichardsMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFullyUpwindFlux
variable = pwater
[../]
[./richardstoil]
type = RichardsMassChange
variable = poil
[../]
[./richardsfoil]
type = RichardsFullyUpwindFlux
variable = poil
[../]
[]
[AuxVariables]
[./SWater]
[../]
[./SOil]
[../]
[]
[AuxKernels]
[./Seff1VGwater_AuxK]
type = RichardsSeffAux
variable = SWater
seff_UO = SeffWater
pressure_vars = 'pwater poil'
[../]
[./Seff1VGoil_AuxK]
type = RichardsSeffAux
variable = SOil
seff_UO = SeffOil
pressure_vars = 'pwater poil'
[../]
[]
[BCs]
# we are pumping water into a system that has virtually incompressible fluids, hence the pressures rise enormously. this adversely affects convergence because of almost-overflows and precision-loss problems. The fixed things help keep pressures low and so prevent these awful behaviours. the movement of the saturation front is the same regardless of the fixed things.
active = 'recharge fixedoil fixedwater'
[./recharge]
type = RichardsPiecewiseLinearSink
variable = pwater
boundary = 'left'
pressures = '-1E10 1E10'
bare_fluxes = '-1 -1'
use_mobility = false
use_relperm = false
[../]
[./fixedwater]
type = DirichletBC
variable = pwater
boundary = 'right'
value = 0
[../]
[./fixedoil]
type = DirichletBC
variable = poil
boundary = 'right'
value = 15
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.25
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
viscosity = '1E-3 2E-3'
gravity = '0E-0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
active = 'andy'
[./andy]
type = SMP
full = true
petsc_options = ''
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-10 1E-10 10000'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
petsc_options = '-snes_converged_reason'
end_time = 5
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = rsc_fu_02
interval = 100000
execute_on = 'initial timestep_end final'
exodus = true
[]
(test/tests/functions/vector_postprocessor_function/vector_postprocessor_function.i)
#This function linearly interpolates the data generated by a vector post
#processor. The purpose is to have a function take points and a field variable
#(aux or primary) as arguments.
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 4
xmin = 0.0
xmax = 0.004
ymin = 0.0
ymax = 0.008
[]
[Variables]
[./u]
initial_condition = 0
[../]
[]
[AuxVariables]
[./v]
initial_condition = 1
[../]
[]
[Functions]
[./ramp_u]
type = ParsedFunction
value = 't'
[../]
[./point_value_function_u]
type = VectorPostprocessorFunction
component = y
argument_column = y
value_column = u
vectorpostprocessor_name = point_value_vector_postprocessor_u
[../]
[./line_value_function_v]
type = VectorPostprocessorFunction
component = y
argument_column = y
value_column = v
vectorpostprocessor_name = line_value_vector_postprocessor_v
[../]
[./function_v]
type = PiecewiseLinear
x = '0 0.008'
y = '1 2'
axis = y
[../]
[]
[Kernels]
[./diffusion_u]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./aux_v]
type = FunctionAux
variable = v
function = function_v
[../]
[]
[BCs]
[./top_u]
type = FunctionDirichletBC
boundary = top
variable = u
function = ramp_u
[../]
[./bottom_u]
type = DirichletBC
boundary = bottom
variable = u
value = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package -ksp_gmres_restart'
petsc_options_value = ' lu superlu_dist 51'
line_search = 'none'
l_max_its = 50
l_tol = 1e-3
nl_max_its = 20
nl_rel_tol = 1e-4
nl_abs_tol = 1e-6
start_time = 0
num_steps = 1
dt = 1
[]
[Postprocessors]
[./point_value_postprocessor_u]
type = FunctionValuePostprocessor
function = point_value_function_u
point = '0.002 0.004 0'
[../]
[./line_value_postprocessor_v]
type = FunctionValuePostprocessor
function = line_value_function_v
point = '0.002 0.004 0'
[../]
[./postprocessor_average_u]
type = ElementAverageValue
variable = u
[../]
[./postprocessor_average_v]
type = ElementAverageValue
variable = v
[../]
[]
[VectorPostprocessors]
[./point_value_vector_postprocessor_u]
type = PointValueSampler
variable = u
points = '0 0.001 0 0 0.004 0 0 0.008 0'
#points = '0.001 0 0 0.002 0 0'
sort_by = y
execute_on = linear
[../]
[./line_value_vector_postprocessor_v]
type = LineValueSampler
variable = v
start_point = '0 0.001 0'
end_point = '0 0.008 0'
num_points = 5
sort_by = y
execute_on = linear
[../]
[]
[Outputs]
interval = 1
csv = false
exodus = true
file_base = out
[./console]
type = Console
output_linear = true
max_rows = 10
[../]
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_htonly/gap_heat_transfer_htonly_test.i)
#
# 1-D Gap Heat Transfer Test without mechanics
#
# This test exercises 1-D gap heat transfer for a constant conductivity gap.
#
# The mesh consists of two element blocks containing one element each. Each
# element is a unit cube. They sit next to one another with a unit between them.
#
# The conductivity of both blocks is set very large to achieve a uniform temperature
# across each block. The temperature of the far left boundary
# is ramped from 100 to 200 over one time unit. The temperature of the far right
# boundary is held fixed at 100.
#
# A simple analytical solution is possible for the heat flux between the blocks:
#
# Flux = (T_left - T_right) * (gapK/gap_width)
#
# The gap conductivity is specified as 1, thus
#
# gapK(Tavg) = 1.0*Tavg
#
#
# The heat flux across the gap at time = 1 is then:
#
# Flux(2) = 100 * (1.0/1.0) = 100
#
# For comparison, see results from the flux post processors
#
# This test has been augmented with a second scalar field that solves nearly
# the same problem. The conductivity has been changed to 10. Thus, the
# flux for the second field is 1000.
#
[Mesh]
file = gap_heat_transfer_htonly_test.e
[]
[Functions]
[./temp]
type = PiecewiseLinear
x = '0 1 2'
y = '100 200 200'
[../]
[]
[ThermalContact]
[./thermal_contact]
type = GapHeatTransfer
variable = temp
primary = 3
secondary = 2
emissivity_primary = 0
emissivity_secondary = 0
[../]
[./awesomium_contact]
type = GapHeatTransfer
variable = awesomium
primary = 3
secondary = 2
emissivity_primary = 0
emissivity_secondary = 0
gap_conductivity = 10
appended_property_name = _awesomium
[../]
[]
[Variables]
[./temp]
order = FIRST
family = LAGRANGE
initial_condition = 100
[../]
[./awesomium]
order = FIRST
family = LAGRANGE
initial_condition = 100
[../]
[]
[AuxVariables]
[./gap_cond]
order = CONSTANT
family = MONOMIAL
[../]
[./gap_cond_awesomium]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[./awe]
type = HeatConduction
variable = awesomium
[../]
[]
[BCs]
[./temp_far_left]
type = FunctionDirichletBC
boundary = 1
variable = temp
function = temp
[../]
[./temp_far_right]
type = DirichletBC
boundary = 4
variable = temp
value = 100
[../]
[./awesomium_far_left]
type = FunctionDirichletBC
boundary = 1
variable = awesomium
function = temp
[../]
[./awesomium_far_right]
type = DirichletBC
boundary = 4
variable = awesomium
value = 100
[../]
[]
[AuxKernels]
[./conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_cond
boundary = 2
[../]
[./conductance_awe]
type = MaterialRealAux
property = gap_conductance_awesomium
variable = gap_cond_awesomium
boundary = 2
[../]
[]
[Materials]
[./heat1]
type = HeatConductionMaterial
block = '1 2'
specific_heat = 1.0
thermal_conductivity = 100000000.0
[../]
[./density]
type = GenericConstantMaterial
block = '1 2'
prop_names = 'density'
prop_values = '1.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 4'
line_search = 'none'
nl_rel_tol = 1e-12
l_tol = 1e-3
l_max_its = 100
dt = 1e-1
end_time = 1.0
[]
[Postprocessors]
[./temp_left]
type = SideAverageValue
boundary = 2
variable = temp
execute_on = 'initial timestep_end'
[../]
[./temp_right]
type = SideAverageValue
boundary = 3
variable = temp
execute_on = 'initial timestep_end'
[../]
[./flux_left]
type = SideFluxIntegral
variable = temp
boundary = 2
diffusivity = thermal_conductivity
execute_on = 'initial timestep_end'
[../]
[./flux_right]
type = SideFluxIntegral
variable = temp
boundary = 3
diffusivity = thermal_conductivity
execute_on = 'initial timestep_end'
[../]
[./awe_left]
type = SideAverageValue
boundary = 2
variable = awesomium
execute_on = 'initial timestep_end'
[../]
[./awe_right]
type = SideAverageValue
boundary = 3
variable = awesomium
execute_on = 'initial timestep_end'
[../]
[./awe_flux_left]
type = SideFluxIntegral
variable = awesomium
boundary = 2
diffusivity = thermal_conductivity
execute_on = 'initial timestep_end'
[../]
[./awe_flux_right]
type = SideFluxIntegral
variable = awesomium
boundary = 3
diffusivity = thermal_conductivity
execute_on = 'initial timestep_end'
[../]
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/dynamics/wave_1D/wave_rayleigh_newmark.i)
# Wave propogation in 1D using Newmark time integration in the presence of Rayleigh damping
#
# The test is for an 1D bar element of length 4m fixed on one end
# with a sinusoidal pulse dirichlet boundary condition applied to the other end.
# beta and gamma are Newmark time integration parameters
# eta and zeta are mass dependent and stiffness dependent Rayleigh damping
# coefficients, respectively.
# The equation of motion in terms of matrices is:
#
# M*accel + (eta*M+zeta*K)*vel +K*disp = 0
#
# Here M is the mass matrix, K is the stiffness matrix
#
# The displacement at the second, third and fourth node at t = 0.1 are
# -7.776268399030435152e-02, 1.949967184623528985e-02 and -4.615737877580032046e-03, respectively
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 4
nz = 1
xmin = 0.0
xmax = 0.1
ymin = 0.0
ymax = 4.0
zmin = 0.0
zmax = 0.1
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./vel_x]
[../]
[./accel_x]
[../]
[./vel_y]
[../]
[./accel_y]
[../]
[./vel_z]
[../]
[./accel_z]
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./DynamicTensorMechanics]
displacements = 'disp_x disp_y disp_z'
zeta = 0.1
[../]
[./inertia_x]
type = InertialForce
variable = disp_x
velocity = vel_x
acceleration = accel_x
beta = 0.3025
gamma = 0.6
eta=0.1
[../]
[./inertia_y]
type = InertialForce
variable = disp_y
velocity = vel_y
acceleration = accel_y
beta = 0.3025
gamma = 0.6
eta=0.1
[../]
[./inertia_z]
type = InertialForce
variable = disp_z
velocity = vel_z
acceleration = accel_z
beta = 0.3025
gamma = 0.6
eta = 0.1
[../]
[]
[AuxKernels]
[./accel_x]
type = NewmarkAccelAux
variable = accel_x
displacement = disp_x
velocity = vel_x
beta = 0.3025
execute_on = timestep_end
[../]
[./vel_x]
type = NewmarkVelAux
variable = vel_x
acceleration = accel_x
gamma = 0.6
execute_on = timestep_end
[../]
[./accel_y]
type = NewmarkAccelAux
variable = accel_y
displacement = disp_y
velocity = vel_y
beta = 0.3025
execute_on = timestep_end
[../]
[./vel_y]
type = NewmarkVelAux
variable = vel_y
acceleration = accel_y
gamma = 0.6
execute_on = timestep_end
[../]
[./accel_z]
type = NewmarkAccelAux
variable = accel_z
displacement = disp_z
velocity = vel_z
beta = 0.3025
execute_on = timestep_end
[../]
[./vel_z]
type = NewmarkVelAux
variable = vel_z
acceleration = accel_z
gamma = 0.6
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 0
index_j = 1
[../]
[./strain_yy]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_yy
index_i = 0
index_j = 1
[../]
[]
[BCs]
[./top_y]
type = DirichletBC
variable = disp_y
boundary = top
value=0.0
[../]
[./top_x]
type = DirichletBC
variable = disp_x
boundary = top
value=0.0
[../]
[./top_z]
type = DirichletBC
variable = disp_z
boundary = top
value=0.0
[../]
[./right_x]
type = DirichletBC
variable = disp_x
boundary = right
value=0.0
[../]
[./right_z]
type = DirichletBC
variable = disp_z
boundary = right
value=0.0
[../]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = left
value=0.0
[../]
[./left_z]
type = DirichletBC
variable = disp_z
boundary = left
value=0.0
[../]
[./front_x]
type = DirichletBC
variable = disp_x
boundary = front
value=0.0
[../]
[./front_z]
type = DirichletBC
variable = disp_z
boundary = front
value=0.0
[../]
[./back_x]
type = DirichletBC
variable = disp_x
boundary = back
value=0.0
[../]
[./back_z]
type = DirichletBC
variable = disp_z
boundary = back
value=0.0
[../]
[./bottom_x]
type = DirichletBC
variable = disp_x
boundary = bottom
value=0.0
[../]
[./bottom_z]
type = DirichletBC
variable = disp_z
boundary = bottom
value=0.0
[../]
[./bottom_y]
type = FunctionDirichletBC
variable = disp_y
boundary = bottom
function = displacement_bc
[../]
[]
[Materials]
[./Elasticity_tensor]
type = ComputeElasticityTensor
block = 0
fill_method = symmetric_isotropic
C_ijkl = '1 0'
[../]
[./strain]
type = ComputeSmallStrain
block = 0
displacements = 'disp_x disp_y disp_z'
[../]
[./stress]
type = ComputeLinearElasticStress
block = 0
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = 'density'
prop_values = '1'
[../]
[]
[Executioner]
type = Transient
start_time = 0
end_time = 6.0
l_tol = 1e-12
nl_rel_tol = 1e-12
dt = 0.1
[]
[Functions]
[./displacement_bc]
type = PiecewiseLinear
data_file = 'sine_wave.csv'
format = columns
[../]
[]
[Postprocessors]
[./_dt]
type = TimestepSize
[../]
[./disp_1]
type = NodalVariableValue
nodeid = 1
variable = disp_y
[../]
[./disp_2]
type = NodalVariableValue
nodeid = 3
variable = disp_y
[../]
[./disp_3]
type = NodalVariableValue
nodeid = 10
variable = disp_y
[../]
[./disp_4]
type = NodalVariableValue
nodeid = 14
variable = disp_y
[../]
[]
[Outputs]
exodus = true
perf_graph = true
[]
(modules/richards/test/tests/dirac/bh07.i)
[Mesh]
type = FileMesh
file = bh07_input.e
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1000 10000'
x = '100 1000'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1000
bulk_mod = 2E9
[../]
[./Seff1VG]
type = RichardsSeff1VG
m = 0.8
al = 1E-5
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0
sum_s_res = 0
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 1E8
[../]
[./borehole_total_outflow_mass]
type = RichardsSumQuantity
[../]
[]
[Variables]
active = 'pressure'
[./pressure]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./p_ic]
type = FunctionIC
variable = pressure
function = initial_pressure
[../]
[]
[BCs]
[./fix_outer]
type = DirichletBC
boundary = perimeter
variable = pressure
value = 1E7
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[Kernels]
active = 'richardsf richardst'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[DiracKernels]
[./bh]
type = RichardsBorehole
bottom_pressure = 0
point_file = bh07.bh
SumQuantityUO = borehole_total_outflow_mass
variable = pressure
unit_weight = '0 0 0'
re_constant = 0.1594
character = 2
[../]
[]
[Postprocessors]
[./bh_report]
type = RichardsPlotQuantity
uo = borehole_total_outflow_mass
execute_on = 'initial timestep_end'
[../]
[./fluid_mass]
type = RichardsMass
variable = pressure
execute_on = 'initial timestep_end'
[../]
[]
[Functions]
[./initial_pressure]
type = ParsedFunction
value = 1E7
[../]
[]
[Materials]
[./all]
type = RichardsMaterial
block = 1
viscosity = 1E-3
mat_porosity = 0.1
mat_permeability = '1E-11 0 0 0 1E-11 0 0 0 1E-11'
density_UO = DensityConstBulk
relperm_UO = RelPermPower
sat_UO = Saturation
seff_UO = Seff1VG
SUPG_UO = SUPGstandard
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = Seff1VG
pressure_vars = pressure
[../]
[]
[Preconditioning]
[./usual]
type = SMP
full = true
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -ksp_max_it'
petsc_options_value = 'bcgs bjacobi 1E-10 1E-10 10000 30'
[../]
[]
[Executioner]
type = Transient
end_time = 1000
solve_type = NEWTON
[./TimeStepper]
# get only marginally better results for smaller time steps
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = bh07
execute_on = 'initial timestep_end final'
interval = 10000
exodus = true
[]
(modules/tensor_mechanics/test/tests/thermal_expansion_function/small_const.i)
# This tests the thermal expansion coefficient function using both
# options to specify that function: mean and instantaneous. There
# two blocks, each containing a single element, and these use the
# two variants of the function.
# In this test, the instantaneous CTE function has a constant value,
# while the mean CTE function is an analytic function designed to
# give the same response. If \bar{alpha}(T) is the mean CTE function,
# and \alpha(T) is the instantaneous CTE function,
# \bar{\alpha}(T) = 1/(T-Tref) \intA^{T}_{Tsf} \alpha(T) dT
# where Tref is the reference temperature used to define the mean CTE
# function, and Tsf is the stress-free temperature.
# This version of the test uses small deformation theory. The results
# from the two models are identical.
[Mesh]
file = 'blocks.e'
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[AuxVariables]
[./temp]
order = FIRST
family = LAGRANGE
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
add_variables = true
eigenstrain_names = eigenstrain
generate_output = 'strain_xx strain_yy strain_zz'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = disp_x
boundary = 3
value = 0.0
[../]
[./bottom]
type = DirichletBC
variable = disp_y
boundary = 2
value = 0.0
[../]
[./back]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0.0
[../]
[]
[AuxKernels]
[./temp]
type = FunctionAux
variable = temp
block = '1 2'
function = temp_func
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./small_stress]
type = ComputeLinearElasticStress
[../]
[./thermal_expansion_strain1]
type = ComputeMeanThermalExpansionFunctionEigenstrain
block = 1
thermal_expansion_function = cte_func_mean
thermal_expansion_function_reference_temperature = 0.5
stress_free_temperature = 0.0
temperature = temp
eigenstrain_name = eigenstrain
[../]
[./thermal_expansion_strain2]
type = ComputeInstantaneousThermalExpansionFunctionEigenstrain
block = 2
thermal_expansion_function = cte_func_inst
stress_free_temperature = 0.0
temperature = temp
eigenstrain_name = eigenstrain
[../]
[]
[Functions]
[./cte_func_mean]
type = ParsedFunction
vars = 'tsf tref scale' #stress free temp, reference temp, scale factor
vals = '0.0 0.5 1e-4'
value = 'scale * (t - tsf) / (t - tref)'
[../]
[./cte_func_inst]
type = PiecewiseLinear
xy_data = '0 1.0
2 1.0'
scale_factor = 1e-4
[../]
[./temp_func]
type = PiecewiseLinear
xy_data = '0 1
1 2'
[../]
[]
[Postprocessors]
[./disp_1]
type = NodalMaxValue
variable = disp_x
boundary = 101
[../]
[./disp_2]
type = NodalMaxValue
variable = disp_x
boundary = 102
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
l_max_its = 100
l_tol = 1e-4
nl_abs_tol = 1e-8
nl_rel_tol = 1e-12
start_time = 0.0
end_time = 1.0
dt = 0.1
[]
[Outputs]
csv = true
[]
(test/tests/test_harness/csv_validation_tester_01.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 3
xmax = 3
[]
[Functions]
[./fn]
type = PiecewiseLinear
axis = x
x = '0 2'
y = '1.01 2.99'
[../]
[]
[AuxVariables]
[./a]
[../]
[]
[AuxKernels]
[./a_ak]
type = FunctionAux
variable = a
function = fn
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./time]
type = TimeDerivative
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Postprocessors]
[./value1]
type = PointValue
variable = a
point = '0 0 0'
[../]
[./value2]
type = PointValue
variable = a
point = '1 0 0'
[../]
[./value3]
type = PointValue
variable = a
point = '2 0 0'
[../]
[]
[Executioner]
type = Transient
num_steps = 1
dt = 0.1
solve_type = NEWTON
[]
[Outputs]
[./csv]
type = CSV
file_base = csv_validation_tester_01
execute_on = 'final'
[../]
[]
(modules/tensor_mechanics/test/tests/interaction_integral/interaction_integral_3d_as_2d.i)
#This tests the Interaction-Integral evaluation capability.
#This is a 3d extrusion of a 2d plane strain model with one element
#through the thickness, and calculates the Interaction-Integrals using options
#to treat it as 2d.
[GlobalParams]
order = FIRST
# order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[Mesh]
file = crack_3d_as_2d.e
displacements = 'disp_x disp_y disp_z'
partitioner = centroid
centroid_partitioner_direction = z
[]
[Functions]
[./rampConstant]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = -1e2
[../]
[]
[DomainIntegral]
integrals = 'InteractionIntegralKI InteractionIntegralKII InteractionIntegralKIII'
boundary = 800
crack_direction_method = CrackDirectionVector
crack_direction_vector = '1 0 0'
2d = true
axis_2d = 2
radius_inner = '4.0 4.5 5.0 5.5 6.0'
radius_outer = '4.5 5.0 5.5 6.0 6.5'
block = 1
youngs_modulus = 207000
poissons_ratio = 0.3
output_q = false
incremental = true
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
[../]
[]
[BCs]
[./crack_y]
type = DirichletBC
variable = disp_y
boundary = 100
value = 0.0
[../]
[./no_z]
type = DirichletBC
variable = disp_z
boundary = 500
value = 0.0
[../]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 700
value = 0.0
[../]
[./Pressure]
[./Side1]
boundary = 400
function = rampConstant
[../]
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_abs_tol = 1e-5
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Outputs]
file_base = interaction_integral_3d_as_2d_out
exodus = true
csv = true
[]
(modules/porous_flow/test/tests/poro_elasticity/mandel_constM.i)
# Mandel's problem of consolodation of a drained medium
#
# A sample is in plane strain.
# -a <= x <= a
# -b <= y <= b
# It is squashed with constant force by impermeable, frictionless plattens on its top and bottom surfaces (at y=+/-b)
# Fluid is allowed to leak out from its sides (at x=+/-a)
# The porepressure within the sample is monitored.
#
# As is common in the literature, this is simulated by
# considering the quarter-sample, 0<=x<=a and 0<=y<=b, with
# impermeable, roller BCs at x=0 and y=0 and y=b.
# Porepressure is fixed at zero on x=a.
# Porepressure and displacement are initialised to zero.
# Then the top (y=b) is moved downwards with prescribed velocity,
# so that the total force that is inducing this downwards velocity
# is fixed. The velocity is worked out by solving Mandel's problem
# analytically, and the total force is monitored in the simulation
# to check that it indeed remains constant.
#
# Here are the problem's parameters, and their values:
# Soil width. a = 1
# Soil height. b = 0.1
# Soil's Lame lambda. la = 0.5
# Soil's Lame mu, which is also the Soil's shear modulus. mu = G = 0.75
# Soil bulk modulus. K = la + 2*mu/3 = 1
# Drained Poisson ratio. nu = (3K - 2G)/(6K + 2G) = 0.2
# Soil bulk compliance. 1/K = 1
# Fluid bulk modulus. Kf = 8
# Fluid bulk compliance. 1/Kf = 0.125
# Soil initial porosity. phi0 = 0.1
# Biot coefficient. alpha = 0.6
# Biot modulus. M = 1/(phi0/Kf + (alpha - phi0)(1 - alpha)/K) = 4.705882
# Undrained bulk modulus. Ku = K + alpha^2*M = 2.694118
# Undrained Poisson ratio. nuu = (3Ku - 2G)/(6Ku + 2G) = 0.372627
# Skempton coefficient. B = alpha*M/Ku = 1.048035
# Fluid mobility (soil permeability/fluid viscosity). k = 1.5
# Consolidation coefficient. c = 2*k*B^2*G*(1-nu)*(1+nuu)^2/9/(1-nuu)/(nuu-nu) = 3.821656
# Normal stress on top. F = 1
#
# The solution for porepressure and displacements is given in
# AHD Cheng and E Detournay "A direct boundary element method for plane strain poroelasticity" International Journal of Numerical and Analytical Methods in Geomechanics 12 (1988) 551-572.
# The solution involves complicated infinite series, so I shall not write it here
[Mesh]
type = GeneratedMesh
dim = 3
nx = 10
ny = 1
nz = 1
xmin = 0
xmax = 1
ymin = 0
ymax = 0.1
zmin = 0
zmax = 1
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
PorousFlowDictator = dictator
block = 0
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'porepressure disp_x disp_y disp_z'
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureVG
m = 0.8
alpha = 1e-5
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[disp_z]
[]
[porepressure]
[]
[]
[BCs]
[roller_xmin]
type = DirichletBC
variable = disp_x
value = 0
boundary = 'left'
[]
[roller_ymin]
type = DirichletBC
variable = disp_y
value = 0
boundary = 'bottom'
[]
[plane_strain]
type = DirichletBC
variable = disp_z
value = 0
boundary = 'back front'
[]
[xmax_drained]
type = DirichletBC
variable = porepressure
value = 0
boundary = right
[]
[top_velocity]
type = FunctionDirichletBC
variable = disp_y
function = top_velocity
boundary = top
[]
[]
[Functions]
[top_velocity]
type = PiecewiseLinear
x = '0 0.002 0.006 0.014 0.03 0.046 0.062 0.078 0.094 0.11 0.126 0.142 0.158 0.174 0.19 0.206 0.222 0.238 0.254 0.27 0.286 0.302 0.318 0.334 0.35 0.366 0.382 0.398 0.414 0.43 0.446 0.462 0.478 0.494 0.51 0.526 0.542 0.558 0.574 0.59 0.606 0.622 0.638 0.654 0.67 0.686 0.702'
y = '-0.041824842 -0.042730269 -0.043412712 -0.04428867 -0.045509181 -0.04645965 -0.047268246 -0.047974749 -0.048597109 -0.0491467 -0.049632388 -0.050061697 -0.050441198 -0.050776675 -0.051073238 -0.0513354 -0.051567152 -0.051772022 -0.051953128 -0.052113227 -0.052254754 -0.052379865 -0.052490464 -0.052588233 -0.052674662 -0.052751065 -0.052818606 -0.052878312 -0.052931093 -0.052977751 -0.053018997 -0.053055459 -0.053087691 -0.053116185 -0.053141373 -0.05316364 -0.053183324 -0.053200724 -0.053216106 -0.053229704 -0.053241725 -0.053252351 -0.053261745 -0.053270049 -0.053277389 -0.053283879 -0.053289615'
[]
[]
[AuxVariables]
[stress_yy]
order = CONSTANT
family = MONOMIAL
[]
[tot_force]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
[]
[tot_force]
type = ParsedAux
args = 'stress_yy porepressure'
execute_on = timestep_end
variable = tot_force
function = '-stress_yy+0.6*porepressure'
[]
[]
[Kernels]
[grad_stress_x]
type = StressDivergenceTensors
variable = disp_x
component = 0
[]
[grad_stress_y]
type = StressDivergenceTensors
variable = disp_y
component = 1
[]
[grad_stress_z]
type = StressDivergenceTensors
variable = disp_z
component = 2
[]
[poro_x]
type = PorousFlowEffectiveStressCoupling
biot_coefficient = 0.6
variable = disp_x
component = 0
[]
[poro_y]
type = PorousFlowEffectiveStressCoupling
biot_coefficient = 0.6
variable = disp_y
component = 1
[]
[poro_z]
type = PorousFlowEffectiveStressCoupling
biot_coefficient = 0.6
component = 2
variable = disp_z
[]
[poro_vol_exp]
type = PorousFlowMassVolumetricExpansion
variable = porepressure
fluid_component = 0
[]
[mass0]
type = PorousFlowMassTimeDerivative
fluid_component = 0
variable = porepressure
[]
[flux]
type = PorousFlowAdvectiveFlux
variable = porepressure
gravity = '0 0 0'
fluid_component = 0
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 8
density0 = 1
thermal_expansion = 0
viscosity = 1
[]
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[elasticity_tensor]
type = ComputeElasticityTensor
C_ijkl = '0.5 0.75'
# bulk modulus is lambda + 2*mu/3 = 0.5 + 2*0.75/3 = 1
fill_method = symmetric_isotropic
[]
[strain]
type = ComputeSmallStrain
[]
[stress]
type = ComputeLinearElasticStress
[]
[eff_fluid_pressure]
type = PorousFlowEffectiveFluidPressure
[]
[vol_strain]
type = PorousFlowVolumetricStrain
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = porepressure
capillary_pressure = pc
[]
[massfrac]
type = PorousFlowMassFraction
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[porosity]
type = PorousFlowPorosityHMBiotModulus
porosity_zero = 0.1
biot_coefficient = 0.6
solid_bulk = 1
constant_fluid_bulk_modulus = 8
constant_biot_modulus = 4.7058823529
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1.5 0 0 0 1.5 0 0 0 1.5'
[]
[relperm]
type = PorousFlowRelativePermeabilityCorey
n = 0 # unimportant in this fully-saturated situation
phase = 0
[]
[]
[Postprocessors]
[p0]
type = PointValue
outputs = csv
point = '0.0 0 0'
variable = porepressure
[]
[p1]
type = PointValue
outputs = csv
point = '0.1 0 0'
variable = porepressure
[]
[p2]
type = PointValue
outputs = csv
point = '0.2 0 0'
variable = porepressure
[]
[p3]
type = PointValue
outputs = csv
point = '0.3 0 0'
variable = porepressure
[]
[p4]
type = PointValue
outputs = csv
point = '0.4 0 0'
variable = porepressure
[]
[p5]
type = PointValue
outputs = csv
point = '0.5 0 0'
variable = porepressure
[]
[p6]
type = PointValue
outputs = csv
point = '0.6 0 0'
variable = porepressure
[]
[p7]
type = PointValue
outputs = csv
point = '0.7 0 0'
variable = porepressure
[]
[p8]
type = PointValue
outputs = csv
point = '0.8 0 0'
variable = porepressure
[]
[p9]
type = PointValue
outputs = csv
point = '0.9 0 0'
variable = porepressure
[]
[p99]
type = PointValue
outputs = csv
point = '1 0 0'
variable = porepressure
[]
[xdisp]
type = PointValue
outputs = csv
point = '1 0.1 0'
variable = disp_x
[]
[ydisp]
type = PointValue
outputs = csv
point = '1 0.1 0'
variable = disp_y
[]
[total_downwards_force]
type = ElementAverageValue
outputs = csv
variable = tot_force
[]
[dt]
type = FunctionValuePostprocessor
outputs = console
function = if(0.15*t<0.01,0.15*t,0.01)
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'gmres asm lu 1E-14 1E-10 10000'
[]
[]
[Executioner]
type = Transient
solve_type = Newton
start_time = 0
end_time = 0.7
[TimeStepper]
type = PostprocessorDT
postprocessor = dt
dt = 0.001
[]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = mandel_constM
[csv]
interval = 3
type = CSV
[]
[]
(modules/tensor_mechanics/test/tests/strain_energy_density/incr_model.i)
# Single element test to check the strain energy density calculation
[GlobalParams]
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
xmin = 0
xmax = 1
ymin = 0
ymax = 2
[]
[AuxVariables]
[./SED]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./rampConstantUp]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = -100
[../]
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress strain_xx strain_yy strain_zz'
planar_formulation = PLANE_STRAIN
[../]
[]
[AuxKernels]
[./SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 'left'
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = 'bottom'
value = 0.0
[../]
[./Pressure]
[./top]
boundary = 'top'
function = rampConstantUp
[../]
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 30e+6
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeFiniteStrainElasticStress
[../]
[./strain_energy_density]
type = StrainEnergyDensity
incremental = true
[../]
[]
[Executioner]
type = Transient
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 4'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_abs_tol = 3e-7
nl_rel_tol = 1e-12
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Postprocessors]
[./epxx]
type = ElementalVariableValue
variable = strain_xx
elementid = 0
[../]
[./epyy]
type = ElementalVariableValue
variable = strain_yy
elementid = 0
[../]
[./epzz]
type = ElementalVariableValue
variable = strain_zz
elementid = 0
[../]
[./sigxx]
type = ElementAverageValue
variable = stress_xx
[../]
[./sigyy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigzz]
type = ElementAverageValue
variable = stress_zz
[../]
[./SED]
type = ElementAverageValue
variable = SED
[../]
[]
[Outputs]
exodus = true
csv = true
[]
(modules/peridynamics/test/tests/generalized_plane_strain/out_of_plane_pressure_OSPD.i)
[GlobalParams]
displacements = 'disp_x disp_y'
scalar_out_of_plane_strain = scalar_strain_zz
[]
[Mesh]
type = PeridynamicsMesh
horizon_number = 3
[./gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 4
ny = 4
[../]
[./gpd]
type = MeshGeneratorPD
input = gmg
retain_fe_mesh = false
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./scalar_strain_zz]
order = FIRST
family = SCALAR
[../]
[]
[AuxVariables]
[./stress_zz]
order = FIRST
family = LAGRANGE
[../]
[]
[Modules]
[./Peridynamics/Mechanics]
[./Master]
[./all]
formulation = ORDINARY_STATE
[../]
[../]
[./GeneralizedPlaneStrain]
[./all]
formulation = ORDINARY_STATE
out_of_plane_stress_variable = stress_zz
out_of_plane_pressure = pressure_function
factor = 1e5
[../]
[../]
[../]
[]
[AuxKernels]
[./stress_zz]
type = NodalRankTwoPD
variable = stress_zz
poissons_ratio = 0.3
youngs_modulus = 1e6
rank_two_tensor = stress
output_type = component
index_i = 2
index_j = 2
[../]
[]
[Postprocessors]
[./react_z]
type = NodalVariableIntegralPD
variable = stress_zz
[../]
[]
[Functions]
[./pressure_function]
type = PiecewiseLinear
x = '0 1'
y = '0 1'
[../]
[]
[BCs]
[./left_x]
type = DirichletBC
boundary = 1003
variable = disp_x
value = 0.0
[../]
[./bottom_y]
type = DirichletBC
boundary = 1000
variable = disp_y
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
poissons_ratio = 0.3
youngs_modulus = 1e6
[../]
[./force_density]
type = ComputeSmallStrainConstantHorizonMaterialOSPD
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
line_search = none
start_time = 0.0
end_time = 1.0
[]
[Outputs]
exodus = true
file_base = out_of_plane_pressure_OSPD
[]
(modules/tensor_mechanics/test/tests/beam/dynamic/dyn_euler_small.i)
# Test for small strain euler beam vibration in y direction
# An impulse load is applied at the end of a cantilever beam of length 4m.
# The properties of the cantilever beam are as follows:
# Young's modulus (E) = 1e4
# Shear modulus (G) = 4e7
# Shear coefficient (k) = 1.0
# Cross-section area (A) = 0.01
# Iy = 1e-4 = Iz
# Length (L)= 4 m
# density (rho) = 1.0
# For this beam, the dimensionless parameter alpha = kAGL^2/EI = 6.4e6
# Therefore, the beam behaves like a Euler-Bernoulli beam.
# The theoretical first and third frequencies of this beam are:
# f1 = 1/(2 pi) * (3.5156/L^2) * sqrt(EI/rho)
# f2 = 6.268 f1
# This implies that the corresponding time period of this beam are 2.858 s and 0.455s
# The FEM solution for this beam with 10 element gives time periods of 2.856 s and 0.4505s with a time step of 0.01.
# A smaller time step is required to obtain a closer match for the lower time periods/higher frequencies.
# A higher time step of 0.05 is used in this test to reduce testing time.
# The time history from this analysis matches with that obtained from Abaqus.
# Values from the first few time steps are as follows:
# time disp_y vel_y accel_y
# 0 0.0 0.0 0.0
# 0.05 0.0016523559162602 0.066094236650407 2.6437694660163
# 0.1 0.0051691308901533 0.07457676230532 -2.3044684398197
# 0.15 0.0078956772343372 0.03448509146203 4.7008016060883
# 0.2 0.0096592517031463 0.03605788729033 -0.63788977295649
# 0.25 0.011069233444348 0.020341382357756 0.0092295756535376
[Mesh]
type = GeneratedMesh
xmin = 0.0
xmax = 4.0
dim = 1
nx = 10
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[./rot_x]
order = FIRST
family = LAGRANGE
[../]
[./rot_y]
order = FIRST
family = LAGRANGE
[../]
[./rot_z]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./vel_x]
order = FIRST
family = LAGRANGE
[../]
[./vel_y]
order = FIRST
family = LAGRANGE
[../]
[./vel_z]
order = FIRST
family = LAGRANGE
[../]
[./accel_x]
order = FIRST
family = LAGRANGE
[../]
[./accel_y]
order = FIRST
family = LAGRANGE
[../]
[./accel_z]
order = FIRST
family = LAGRANGE
[../]
[./rot_vel_x]
order = FIRST
family = LAGRANGE
[../]
[./rot_vel_y]
order = FIRST
family = LAGRANGE
[../]
[./rot_vel_z]
order = FIRST
family = LAGRANGE
[../]
[./rot_accel_x]
order = FIRST
family = LAGRANGE
[../]
[./rot_accel_y]
order = FIRST
family = LAGRANGE
[../]
[./rot_accel_z]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./accel_x]
type = NewmarkAccelAux
variable = accel_x
displacement = disp_x
velocity = vel_x
beta = 0.25
execute_on = timestep_end
[../]
[./vel_x]
type = NewmarkVelAux
variable = vel_x
acceleration = accel_x
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_y]
type = NewmarkAccelAux
variable = accel_y
displacement = disp_y
velocity = vel_y
beta = 0.25
execute_on = timestep_end
[../]
[./vel_y]
type = NewmarkVelAux
variable = vel_y
acceleration = accel_y
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_z]
type = NewmarkAccelAux
variable = accel_z
displacement = disp_z
velocity = vel_z
beta = 0.25
execute_on = timestep_end
[../]
[./vel_z]
type = NewmarkVelAux
variable = vel_z
acceleration = accel_z
gamma = 0.5
execute_on = timestep_end
[../]
[./rot_accel_x]
type = NewmarkAccelAux
variable = rot_accel_x
displacement = rot_x
velocity = rot_vel_x
beta = 0.25
execute_on = timestep_end
[../]
[./rot_vel_x]
type = NewmarkVelAux
variable = rot_vel_x
acceleration = rot_accel_x
gamma = 0.5
execute_on = timestep_end
[../]
[./rot_accel_y]
type = NewmarkAccelAux
variable = rot_accel_y
displacement = rot_y
velocity = rot_vel_y
beta = 0.25
execute_on = timestep_end
[../]
[./rot_vel_y]
type = NewmarkVelAux
variable = rot_vel_y
acceleration = rot_accel_y
gamma = 0.5
execute_on = timestep_end
[../]
[./rot_accel_z]
type = NewmarkAccelAux
variable = rot_accel_z
displacement = rot_z
velocity = rot_vel_z
beta = 0.25
execute_on = timestep_end
[../]
[./rot_vel_z]
type = NewmarkVelAux
variable = rot_vel_z
acceleration = rot_accel_z
gamma = 0.5
execute_on = timestep_end
[../]
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./fixy1]
type = DirichletBC
variable = disp_y
boundary = left
value = 0.0
[../]
[./fixz1]
type = DirichletBC
variable = disp_z
boundary = left
value = 0.0
[../]
[./fixr1]
type = DirichletBC
variable = rot_x
boundary = left
value = 0.0
[../]
[./fixr2]
type = DirichletBC
variable = rot_y
boundary = left
value = 0.0
[../]
[./fixr3]
type = DirichletBC
variable = rot_z
boundary = left
value = 0.0
[../]
[]
[NodalKernels]
[./force_y2]
type = UserForcingFunctionNodalKernel
variable = disp_y
boundary = right
function = force
[../]
[]
[Functions]
[./force]
type = PiecewiseLinear
x = '0.0 0.05 0.1 10.0'
y = '0.0 0.01 0.0 0.0'
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
dt = 0.05
end_time = 5.0
timestep_tolerance = 1e-6
[]
[Kernels]
[./solid_disp_x]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 0
variable = disp_x
[../]
[./solid_disp_y]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 1
variable = disp_y
[../]
[./solid_disp_z]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 2
variable = disp_z
[../]
[./solid_rot_x]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 3
variable = rot_x
[../]
[./solid_rot_y]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 4
variable = rot_y
[../]
[./solid_rot_z]
type = StressDivergenceBeam
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 5
variable = rot_z
[../]
[./inertial_force_x]
type = InertialForceBeam
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y rot_vel_z'
rotational_accelerations = 'rot_accel_x rot_accel_y rot_accel_z'
beta = 0.25
gamma = 0.5
area = 0.01
Iy = 1e-4
Iz = 1e-4
Ay = 0.0
Az = 0.0
component = 0
variable = disp_x
[../]
[./inertial_force_y]
type = InertialForceBeam
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y rot_vel_z'
rotational_accelerations = 'rot_accel_x rot_accel_y rot_accel_z'
beta = 0.25
gamma = 0.5
area = 0.01
Iy = 1e-4
Iz = 1e-4
Ay = 0.0
Az = 0.0
component = 1
variable = disp_y
[../]
[./inertial_force_z]
type = InertialForceBeam
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y rot_vel_z'
rotational_accelerations = 'rot_accel_x rot_accel_y rot_accel_z'
beta = 0.25
gamma = 0.5
area = 0.01
Iy = 1e-4
Iz = 1e-4
Ay = 0.0
Az = 0.0
component = 2
variable = disp_z
[../]
[./inertial_force_rot_x]
type = InertialForceBeam
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y rot_vel_z'
rotational_accelerations = 'rot_accel_x rot_accel_y rot_accel_z'
beta = 0.25
gamma = 0.5
area = 0.01
Iy = 1e-4
Iz = 1e-4
Ay = 0.0
Az = 0.0
component = 3
variable = rot_x
[../]
[./inertial_force_rot_y]
type = InertialForceBeam
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y rot_vel_z'
rotational_accelerations = 'rot_accel_x rot_accel_y rot_accel_z'
beta = 0.25
gamma = 0.5
area = 0.01
Iy = 1e-4
Iz = 1e-4
Ay = 0.0
Az = 0.0
component = 4
variable = rot_y
[../]
[./inertial_force_rot_z]
type = InertialForceBeam
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y rot_vel_z'
rotational_accelerations = 'rot_accel_x rot_accel_y rot_accel_z'
beta = 0.25
gamma = 0.5
area = 0.01
Iy = 1e-4
Iz = 1e-4
Ay = 0.0
Az = 0.0
component = 5
variable = rot_z
[../]
[]
[Materials]
[./elasticity]
type = ComputeElasticityBeam
youngs_modulus = 1.0e4
poissons_ratio = -0.999875
shear_coefficient = 1.0
block = 0
[../]
[./strain]
type = ComputeIncrementalBeamStrain
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
area = 0.01
Ay = 0.0
Az = 0.0
Iy = 1.0e-4
Iz = 1.0e-4
y_orientation = '0.0 1.0 0.0'
[../]
[./stress]
type = ComputeBeamResultants
block = 0
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = 'density'
prop_values = '1.0'
[../]
[]
[Postprocessors]
[./disp_x]
type = PointValue
point = '4.0 0.0 0.0'
variable = disp_x
[../]
[./disp_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = disp_y
[../]
[./vel_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = vel_y
[../]
[./accel_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = accel_y
[../]
[]
[Outputs]
exodus = true
csv = true
perf_graph = true
[]
(modules/tensor_mechanics/test/tests/ad_anisotropic_creep/ad_aniso_creep_y_3d.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
nx = 2
ny = 10
nz = 2
xmin = 0.0
ymin = 0.0
zmin = 0.0
xmax = 1.0
ymax = 10.0
zmax = 1.0
[]
[corner_node]
type = ExtraNodesetGenerator
new_boundary = '100'
nodes = '4 10'
input = gen
[]
[corner_node_2]
type = ExtraNodesetGenerator
new_boundary = '101'
nodes = '1 67'
input = corner_node
[]
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[AuxVariables]
[hydrostatic_stress]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_xx]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_xy]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_yy]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[hydrostatic_stress]
type = ADRankTwoScalarAux
variable = hydrostatic_stress
rank_two_tensor = stress
scalar_type = Hydrostatic
[]
[creep_strain_xx]
type = ADRankTwoAux
rank_two_tensor = creep_strain
variable = creep_strain_xx
index_i = 0
index_j = 0
[]
[creep_strain_xy]
type = ADRankTwoAux
rank_two_tensor = creep_strain
variable = creep_strain_xy
index_i = 0
index_j = 1
[]
[creep_strain_yy]
type = ADRankTwoAux
rank_two_tensor = creep_strain
variable = creep_strain_yy
index_i = 1
index_j = 1
[]
[sigma_yy]
type = ADRankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
[]
[]
[Functions]
[pull]
type = PiecewiseLinear
x = '0 1.0e-11 1.0'
y = '0 -4e1 -4e1'
[]
[]
[Modules/TensorMechanics/Master]
[all]
strain = FINITE
generate_output = 'elastic_strain_yy stress_yy'
use_automatic_differentiation = true
add_variables = true
[]
[]
[Materials]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 700
poissons_ratio = 0.0
[]
[elastic_strain]
type = ADComputeMultipleInelasticStress
inelastic_models = "trial_creep_two"
max_iterations = 50
absolute_tolerance = 1e-16
[]
[trial_creep_two]
type = ADHillCreepStressUpdate
coefficient = 1e-16
n_exponent = 9
m_exponent = 0
activation_energy = 0
# F G H L M N
hill_constants = "0.5 0.25 0.3866 1.6413 1.6413 1.2731"
max_inelastic_increment = 0.00003
absolute_tolerance = 1e-20
relative_tolerance = 1e-20
# Force it to not use integration error
max_integration_error = 100.0
[]
[]
[BCs]
[no_disp_x]
type = ADDirichletBC
variable = disp_x
boundary = 101
value = 0.0
[]
[no_disp_y]
type = ADDirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[]
[no_disp_z]
type = ADDirichletBC
variable = disp_z
boundary = 100
value = 0.0
[]
[Pressure]
[Side1]
boundary = top
function = pull
[]
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
nl_rel_tol = 1.0e-13
nl_abs_tol = 1.0e-13
l_max_its = 90
num_steps = 10
dt = 1.0e-4
start_time = 0
automatic_scaling = true
[]
[Postprocessors]
[matl_ts_min]
type = MaterialTimeStepPostprocessor
[]
[max_disp_x]
type = ElementExtremeValue
variable = disp_x
[]
[max_disp_y]
type = ElementExtremeValue
variable = disp_y
[]
[max_hydro]
type = ElementAverageValue
variable = hydrostatic_stress
[]
[dt]
type = TimestepSize
[]
[num_lin]
type = NumLinearIterations
outputs = console
[]
[num_nonlin]
type = NumNonlinearIterations
outputs = console
[]
[creep_strain_yy]
type = ElementalVariableValue
variable = creep_strain_yy
execute_on = 'TIMESTEP_END'
elementid = 39
[]
[elastic_strain_yy]
type = ElementalVariableValue
variable = elastic_strain_yy
execute_on = 'TIMESTEP_END'
elementid = 39
[]
[sigma_yy]
type = ElementalVariableValue
variable = stress_yy
execute_on = 'TIMESTEP_END'
elementid = 39
[]
[]
[Outputs]
csv = true
exodus = true
perf_graph = true
[]
(modules/tensor_mechanics/test/tests/j_integral/j_integral_2d_small_strain.i)
#This tests the J-Integral evaluation capability.
#This is a 2d plane strain model
#The analytic solution for J1 is 2.434. This model
#converges to that solution with a refined mesh.
#Reference: National Agency for Finite Element Methods and Standards (U.K.):
#Test 1.1 from NAFEMS publication "Test Cases in Linear Elastic Fracture
#Mechanics" R0020.
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[Mesh]
file = crack2d.e
[]
[AuxVariables]
[./SED]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./rampConstant]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = -1e2
[../]
[]
[DomainIntegral]
integrals = JIntegral
boundary = 800
crack_direction_method = CrackDirectionVector
crack_direction_vector = '1 0 0'
2d = true
axis_2d = 2
radius_inner = '4.0 4.5 5.0 5.5 6.0'
radius_outer = '4.5 5.0 5.5 6.0 6.5'
output_q = false
incremental = false
[]
[Modules/TensorMechanics/Master]
[./master]
strain = SMALL
add_variables = true
incremental = false
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
planar_formulation = PLANE_STRAIN
[../]
[]
[AuxKernels]
[./SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[../]
[]
[BCs]
[./crack_y]
type = DirichletBC
variable = disp_y
boundary = 100
value = 0.0
[../]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 700
value = 0.0
[../]
[./Pressure]
[./Side1]
boundary = 400
function = rampConstant
[../]
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeLinearElasticStress
[../]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_rel_tol = 1e-12
nl_abs_tol = 1e-5
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Outputs]
file_base = j_integral_2d_small_strain_out
exodus = true
csv = true
[]
(modules/combined/test/tests/additive_manufacturing/check_element_addition_by_variable.i)
[Problem]
kernel_coverage_check = false
[]
[Mesh]
[./gen]
type = GeneratedMeshGenerator
dim = 3
xmin =0
xmax =2.0
ymin =0
ymax =2.0
zmin =0
zmax =2.0
nx=10
ny=10
nz=10
[../]
[./left_domain]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '0 0 0'
top_right = '2 2 1'
block_id = 1
[../]
[./right_domain]
input = left_domain
type = SubdomainBoundingBoxGenerator
bottom_left = '0 0 1'
top_right = '2 2 2'
block_id = 2
[../]
[./sidesets]
input = right_domain
type = SideSetsAroundSubdomainGenerator
normal = '0 0 1'
block = 1
new_boundary = 'moving_interface'
[]
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
block = '1 2'
[]
[Modules/TensorMechanics/Master]
[./all]
# strain = FINITE
add_variables = true
generate_output = 'stress_zz strain_zz'
block = '1 2'
use_automatic_differentiation = true
[../]
[]
[Materials]
[./elasticity]
type = ADComputeVariableIsotropicElasticityTensor
poissons_ratio = 0.3
youngs_modulus = 1e3
block = '1 2'
[../]
[./stress]
type = ADComputeLinearElasticStress
block = '1 2'
[../]
[]
[Functions]
[./front_pull]
type = PiecewiseLinear
x = '0 1'
y = '0 1'
scale_factor = 0.5
[../]
[]
[BCs]
[./disp_front_pull]
type = ADFunctionDirichletBC
variable = disp_z
boundary = front
function = front_pull
[../]
[./uz_back_fix]
type = ADDirichletBC
variable = disp_z
boundary = back
value = 0.0
[../]
[./u_yz_fix]
type = ADDirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./u_xz_fix]
type = ADDirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
automatic_scaling = true
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
line_search = 'none'
l_max_its = 10
nl_max_its = 20
nl_rel_tol = 1e-4
start_time = 0.0
end_time = 1.0
dt = 1e-1
dtmin = 1e-4
[]
[UserObjects]
[./activated_elem_uo]
type = ActivateElementsCoupled
execute_on = timestep_begin
coupled_var = strain_zz
activate_value = 0.05
active_subdomain_id = 1
expand_boundary_name = 'moving_interface'
[../]
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/action/action_multi_eigenstrain_same_conditions.i)
# This tests a thermal expansion coefficient function using defined on both
# blocks. There two blocks, each containing a single element, and these use
# automatic_eigenstrain_names function of the TensorMechanicsAction to ensure
# the names are passed correctly.
# In this test, the instantaneous CTE function has a constant value,
# while the mean CTE function is an analytic function designed to
# give the same response. If \bar{alpha}(T) is the mean CTE function,
# and \alpha(T) is the instantaneous CTE function,
# \bar{\alpha}(T) = 1/(T-Tref) \intA^{T}_{Tsf} \alpha(T) dT
# where Tref is the reference temperature used to define the mean CTE
# function, and Tsf is the stress-free temperature.
# This version of the test uses finite deformation theory.
# The two models produce very similar results. There are slight
# differences due to the large deformation treatment.
[Mesh]
file = 'blocks.e'
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[AuxVariables]
[./temp]
order = FIRST
family = LAGRANGE
[../]
[]
[Problem]
solve = false
[]
[Modules/TensorMechanics/Master]
[./block1]
block = 1
strain = FINITE
add_variables = true
automatic_eigenstrain_names = true
generate_output = 'strain_xx strain_yy strain_zz'
[../]
[./block2]
block = 2
strain = FINITE
add_variables = true
automatic_eigenstrain_names = true
generate_output = 'strain_xx strain_yy strain_zz'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = disp_x
boundary = 3
value = 0.0
[../]
[./bottom]
type = DirichletBC
variable = disp_y
boundary = 2
value = 0.0
[../]
[./back]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0.0
[../]
[]
[AuxKernels]
[./temp]
type = FunctionAux
variable = temp
block = '1 2'
function = temp_func
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./small_stress]
type = ComputeFiniteStrainElasticStress
[../]
[./thermal_expansion_strain1]
type = ComputeMeanThermalExpansionFunctionEigenstrain
block = '1 2'
thermal_expansion_function = cte_func_mean
thermal_expansion_function_reference_temperature = 0.5
stress_free_temperature = 0.0
temperature = temp
eigenstrain_name = eigenstrain
[../]
[]
[Functions]
[./cte_func_mean]
type = ParsedFunction
vars = 'tsf tref scale' #stress free temp, reference temp, scale factor
vals = '0.0 0.5 1e-4'
value = 'scale * (t - tsf) / (t - tref)'
[../]
[./cte_func_inst]
type = PiecewiseLinear
xy_data = '0 1.0
2 1.0'
scale_factor = 1e-4
[../]
[./temp_func]
type = PiecewiseLinear
xy_data = '0 1
1 2'
[../]
[]
[Postprocessors]
[./disp_1]
type = NodalMaxValue
variable = disp_x
boundary = 101
[../]
[./disp_2]
type = NodalMaxValue
variable = disp_x
boundary = 102
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
l_max_its = 100
l_tol = 1e-4
nl_abs_tol = 1e-8
nl_rel_tol = 1e-12
start_time = 0.0
end_time = 1.0
dt = 0.1
[]
[Outputs]
csv = true
[]
(modules/contact/test/tests/tension_release/8ElemTensionRelease.i)
[Mesh]
file = 8ElemTensionRelease.e
partitioner = centroid
centroid_partitioner_direction = x
[]
[GlobalParams]
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Functions]
[./up]
type = PiecewiseLinear
x = '0 1 2 3'
y = '0 0.0001 0 -.0001'
[../]
[]
[AuxVariables]
[./status]
[../]
[./pid]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = FINITE
[]
[]
[Contact]
[./dummy_name]
primary = 2
secondary = 3
penalty = 1e6
model = frictionless
tangential_tolerance = 0.01
[../]
[]
[AuxKernels]
[./pid]
type = ProcessorIDAux
variable = pid
execute_on = 'initial timestep_end'
[../]
[./status]
type = PenetrationAux
quantity = mechanical_status
variable = status
boundary = 3
paired_boundary = 2
execute_on = timestep_end
[../]
[]
[BCs]
[./lateral]
type = DirichletBC
variable = disp_x
boundary = '1 4'
value = 0
[../]
[./bottom_up]
type = FunctionDirichletBC
variable = disp_y
boundary = 1
function = up
[../]
[./top]
type = DirichletBC
variable = disp_y
boundary = 4
value = 0.0
[../]
[]
[Materials]
[./stiffStuff1]
type = ComputeIsotropicElasticityTensor
block = '1 2'
youngs_modulus = 1.0e6
poissons_ratio = 0.3
[../]
[./stiffStuff1_stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart'
petsc_options_value = 'hypre boomeramg 101'
line_search = 'none'
nl_rel_tol = 1e-8
nl_abs_tol = 1e-9
l_tol = 1e-4
l_max_its = 100
nl_max_its = 10
dt = 0.1
num_steps = 30
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
[]
[Outputs]
exodus = true
[]
(test/tests/geomsearch/2d_moving_penetration/pl_test3qtt.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
file = pl_test3q.e
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
tangential_tolerance = 0.09
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
tangential_tolerance = 0.09
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate10]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate13]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate14]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate15]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate16]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-9
l_max_its = 10
start_time = 0.0
dt = 0.02
end_time = 1.0
[./Quadrature]
order = THIRD
[../]
[]
[Outputs]
file_base = pl_test3qtt_out
exodus = true
[]
(modules/tensor_mechanics/test/tests/generalized_plane_strain/plane_strain_prescribed.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
scalar_out_of_plane_strain = scalar_strain_zz
block = 0
[]
[Mesh]
[./square]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 2
[../]
[]
[AuxVariables]
[./temp]
[../]
[./scalar_strain_zz]
order = FIRST
family = SCALAR
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[]
[AuxKernels]
[./tempfuncaux]
type = FunctionAux
variable = temp
function = tempfunc
use_displaced_mesh = false
[../]
[]
[AuxScalarKernels]
[./strain_zz]
type = FunctionScalarAux
variable = scalar_strain_zz
function = scalar_strain_zz_func
[../]
[]
[Functions]
[./tempfunc]
type = ParsedFunction
value = '(1-x)*t'
[../]
[./scalar_strain_zz_func]
type = PiecewiseLinear
xy_data = '0 0
1 7.901e-5
2 1.103021e-2'
[../]
[]
[BCs]
[./bottomx]
type = DirichletBC
boundary = 0
variable = disp_x
value = 0.0
[../]
[./bottomy]
type = DirichletBC
boundary = 0
variable = disp_y
value = 0.0
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
add_variables = true
temperature = temp
generate_output = 'stress_xx stress_xy stress_yy stress_zz strain_xx strain_xy strain_yy strain_zz'
planar_formulation = PLANE_STRAIN
eigenstrain_names = eigenstrain
save_in = 'saved_x saved_y'
[../]
[]
[Materials]
[./elastic_tensor]
type = ComputeIsotropicElasticityTensor
poissons_ratio = 0.3
youngs_modulus = 1e6
[../]
[./thermal_strain]
type = ComputeThermalExpansionEigenstrain
temperature = temp
thermal_expansion_coeff = 0.02
stress_free_temperature = 0.5
eigenstrain_name = eigenstrain
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[Postprocessors]
[./react_z]
type = MaterialTensorIntegral
rank_two_tensor = stress
index_i = 2
index_j = 2
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
line_search = none
# controls for linear iterations
l_max_its = 100
l_tol = 1e-4
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-5
# time control
start_time = 0.0
dt = 1.0
dtmin = 1.0
end_time = 2.0
num_steps = 5000
[]
[Outputs]
exodus = true
[]
(test/tests/geomsearch/3d_moving_penetration/pl_test1tt.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
file = pl_test1tt.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./normal_z]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./closest_point_z]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[./diff_z]
type = Diffusion
variable = disp_z
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
tangential_tolerance = 0.1
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
tangential_tolerance = 0.1
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = normal_z
boundary = 11
paired_boundary = 12
quantity = normal_z
[../]
[./penetrate10]
type = PenetrationAux
variable = normal_z
boundary = 12
paired_boundary = 11
quantity = normal_z
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate13]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate14]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate15]
type = PenetrationAux
variable = closest_point_z
boundary = 11
paired_boundary = 12
quantity = closest_point_z
[../]
[./penetrate16]
type = PenetrationAux
variable = closest_point_z
boundary = 12
paired_boundary = 11
quantity = closest_point_z
[../]
[./penetrate17]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate18]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate19]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate20]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b1z]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[./b2z]
type = DirichletBC
variable = disp_z
boundary = 2
value = 0
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 0.7 -0.7 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-9
l_max_its = 10
start_time = 0.0
dt = 0.05
end_time = 1.0
[]
[Outputs]
file_base = pl_test1tt_out
exodus = true
[]
(modules/tensor_mechanics/test/tests/j_integral/j_integral_3d_topo_q_func.i)
#This tests the J-Integral evaluation capability.
#This is a 3d extrusion of a 2d plane strain model with 2 elements
#through the thickness, and calculates the J-Integrals using options
#to treat it as 3d.
#The analytic solution for J1 is 2.434. This model
#converges to that solution with a refined mesh.
#Reference: National Agency for Finite Element Methods and Standards (U.K.):
#Test 1.1 from NAFEMS publication "Test Cases in Linear Elastic Fracture
#Mechanics" R0020.
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[Mesh]
file = crack3d.e
[]
[AuxVariables]
[./SED]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./rampConstant]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = -1e2
[../]
[]
[DomainIntegral]
integrals = JIntegral
boundary = 800
crack_direction_method = CrackDirectionVector
crack_direction_vector = '1 0 0'
q_function_type = Topology
ring_first = 1
ring_last = 3
output_q = false
incremental = true
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
[../]
[]
[AuxKernels]
[./SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[../]
[]
[BCs]
[./crack_y]
type = DirichletBC
variable = disp_y
boundary = 100
value = 0.0
[../]
[./no_z]
type = DirichletBC
variable = disp_z
boundary = 500
value = 0.0
[../]
[./no_z2]
type = DirichletBC
variable = disp_z
boundary = 510
value = 0.0
[../]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 700
value = 0.0
[../]
[./Pressure]
[./Side1]
boundary = 400
function = rampConstant
[../]
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_abs_tol = 1e-5
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Outputs]
file_base = j_integral_3d_topo_q_func_out
exodus = true
csv = true
[]
(modules/xfem/test/tests/second_order_elements/diffusion_2d_tri6.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 3
ny = 4
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = TRI6
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.35 1.0 0.35 0.2'
time_start_cut = 0.0
time_end_cut = 2.0
[../]
[]
[Variables]
[./u]
[../]
[]
[Functions]
[./u_left]
type = PiecewiseLinear
x = '0 2'
y = '0 0.1'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = FunctionDirichletBC
variable = u
boundary = 3
function = u_left
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Transient
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
start_time = 0.0
dt = 1.0
end_time = 2.0
[]
[Outputs]
interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/tensor_mechanics/test/tests/line_material_rank_two_sampler/rank_two_scalar_sampler.i)
[GlobalParams]
displacements = 'x_disp y_disp z_disp'
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 3
ny = 3
nz = 3
elem_type = HEX
[]
[Functions]
[./rampConstant]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = 1e-6
[../]
[]
[Variables]
[./x_disp]
order = FIRST
family = LAGRANGE
[../]
[./y_disp]
order = FIRST
family = LAGRANGE
[../]
[./z_disp]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./vonmises]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./vonmises]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = vonmises
scalar_type = VonMisesStress
[../]
[]
[VectorPostprocessors]
[./vonmises]
type = LineMaterialRankTwoScalarSampler
start = '0.1667 0.4 0.45'
end = '0.8333 0.6 0.55'
property = stress
scalar_type = VonMisesStress
sort_by = id
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
[../]
[]
[BCs]
[./front]
type = FunctionDirichletBC
variable = z_disp
boundary = 5
function = rampConstant
[../]
[./back_x]
type = DirichletBC
variable = x_disp
boundary = 0
value = 0.0
[../]
[./back_y]
type = DirichletBC
variable = y_disp
boundary = 0
value = 0.0
[../]
[./back_z]
type = DirichletBC
variable = z_disp
boundary = 0
value = 0.0
[../]
[]
[Materials]
[./elast_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = .3
[../]
[./strain]
type = ComputeSmallStrain
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
l_max_its = 100
start_time = 0.0
num_steps = 99999
end_time = 1.0
dt = 0.1
[]
[Outputs]
file_base = rank_two_scalar_sampler_out
exodus = true
csv = true
[]
(modules/richards/test/tests/gravity_head_2/gh16.i)
# unsaturated = true
# gravity = true
# supg = true
# transient = true
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
xmin = 0
xmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1E-2 1E-1 1E0 1E1 1E3 1E4 1E5 1E6 1E7'
x = '0 1E-1 1E0 1E1 1E2 1E3 1E4 1E5 1E6'
[../]
[]
[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 = 0.1
[../]
[./SUPGgas]
type = RichardsSUPGstandard
p_SUPG = 0.01
[../]
[]
[Variables]
[./pwater]
order = FIRST
family = LAGRANGE
[../]
[./pgas]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./water_ic]
type = ConstantIC
value = 1
variable = pwater
[../]
[./gas_ic]
type = ConstantIC
value = 2
variable = pgas
[../]
[]
[Kernels]
active = 'richardsfwater richardstwater richardsfgas richardstgas'
[./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
output = none
[../]
[./mgas_init]
type = RichardsMass
variable = pgas
execute_on = timestep_begin
output = none
[../]
[./mwater_fin]
type = RichardsMass
variable = pwater
execute_on = timestep_end
output = none
[../]
[./mgas_fin]
type = RichardsMass
variable = pgas
execute_on = timestep_end
output = none
[../]
[./mass_error_water]
type = FunctionValuePostprocessor
function = fcn_mass_error_w
[../]
[./mass_error_gas]
type = FunctionValuePostprocessor
function = fcn_mass_error_g
[../]
[./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((-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 -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-10 1E-10 10000'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
end_time = 1E6
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = gh16
execute_on = 'timestep_end final'
interval = 100000
exodus = true
csv = true
[]
(modules/tensor_mechanics/test/tests/beam/constraints/frictional_constraint.i)
# Test for frictional beam constraint.
#
# Using a simple L-shaped geometry with a frictional constraint at the
# corner between the two beams. The longer beam properties and loading is
# taken from an earlier beam regression test for static loading. The maximum
# applied load of 50000 lb should result in a displacement of 3.537e-3. Since
# the constraint is frictional with a low normal force (1.0) and coefficient
# of friction (0.05) and the short beam is much less stiff, the
# y-dir displacement of the long beam is still 3.537e-3. However, the y-dir
# displacement of the short beam increases until the force exceeds the
# frictional capacity which in this case is 0.05 and then remains constant
# after that point.
[Mesh]
file = beam_cons_patch.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[./rot_x]
order = FIRST
family = LAGRANGE
[../]
[./rot_y]
order = FIRST
family = LAGRANGE
[../]
[./rot_z]
order = FIRST
family = LAGRANGE
[../]
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = '1001 1003'
value = 0.0
[../]
[./fixy1]
type = DirichletBC
variable = disp_y
boundary = '1001 1003'
value = 0.0
[../]
[./fixz1]
type = DirichletBC
variable = disp_z
boundary = '1001 1003'
value = 0.0
[../]
[./fixr1]
type = DirichletBC
variable = rot_x
boundary = '1001 1003'
value = 0.0
[../]
[./fixr2]
type = DirichletBC
variable = rot_y
boundary = '1001 1003'
value = 0.0
[../]
[./fixr3]
type = DirichletBC
variable = rot_z
boundary = '1001 1003'
value = 0.0
[../]
[]
[Constraints]
[./tie_y_fuel]
type = NodalFrictionalConstraint
normal_force = 1.0
tangential_penalty = 1.2e5
friction_coefficient = 0.05
boundary = 1005
secondary = 1004
variable = disp_y
[../]
[./tie_x_fuel]
type = NodalStickConstraint
penalty = 1.2e14
boundary = 1005
secondary = 1004
variable = disp_x
[../]
[./tie_z_fuel]
type = NodalStickConstraint
penalty = 1.2e14
boundary = 1005
secondary = 1004
variable = disp_z
[../]
[./tie_rot_y_fuel]
type = NodalStickConstraint
penalty = 1.2e14
boundary = 1005
secondary = 1004
variable = rot_y
[../]
[./tie_rot_x_fuel]
type = NodalStickConstraint
penalty = 1.2e14
boundary = 1005
secondary = 1004
variable = rot_x
[../]
[./tie_rot_z_fuel]
type = NodalStickConstraint
penalty = 1.2e14
boundary = 1005
secondary = 1004
variable = rot_z
[../]
[]
[Functions]
[./force_loading]
type = PiecewiseLinear
x = '0.0 5.0'
y = '0.0 50000.0'
[../]
[]
[NodalKernels]
[./force_x2]
type = UserForcingFunctionNodalKernel
variable = disp_y
boundary = '1004'
function = force_loading
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
line_search = 'none'
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-8
dt = 1
dtmin = 1
end_time = 5
[]
[Kernels]
[./solid_disp_x]
type = StressDivergenceBeam
block = '1 2'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 0
variable = disp_x
[../]
[./solid_disp_y]
type = StressDivergenceBeam
block = '1 2'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 1
variable = disp_y
[../]
[./solid_disp_z]
type = StressDivergenceBeam
block = '1 2'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 2
variable = disp_z
[../]
[./solid_rot_x]
type = StressDivergenceBeam
block = '1 2'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 3
variable = rot_x
[../]
[./solid_rot_y]
type = StressDivergenceBeam
block = '1 2'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 4
variable = rot_y
[../]
[./solid_rot_z]
type = StressDivergenceBeam
block = '1 2'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 5
variable = rot_z
[../]
[]
[Materials]
[./elasticity_pipe]
type = ComputeElasticityBeam
shear_coefficient = 1.0
youngs_modulus = 30e6
poissons_ratio = 0.3
block = 1
outputs = exodus
output_properties = 'material_stiffness material_flexure'
[../]
[./strain_pipe]
type = ComputeIncrementalBeamStrain
block = '1'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
area = 28.274
Ay = 0.0
Az = 0.0
Iy = 1.0
Iz = 1.0
y_orientation = '0.0 0.0 1.0'
[../]
[./stress_pipe]
type = ComputeBeamResultants
block = 1
outputs = exodus
output_properties = 'forces moments'
[../]
[./elasticity_cons]
type = ComputeElasticityBeam
shear_coefficient = 1.0
youngs_modulus = 10e2
poissons_ratio = 0.3
block = 2
outputs = exodus
output_properties = 'material_stiffness material_flexure'
[../]
[./strain_cons]
type = ComputeIncrementalBeamStrain
block = '2'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
area = 1.0
Ay = 0.0
Az = 0.0
Iy = 1.0
Iz = 1.0
y_orientation = '0.0 0.0 1.0'
[../]
[./stress_cons]
type = ComputeBeamResultants
block = 2
outputs = exodus
output_properties = 'forces moments'
[../]
[]
[Postprocessors]
[./disp_y_n4]
type = NodalVariableValue
variable = disp_y
nodeid = 3
[../]
[./disp_y_n2]
type = NodalVariableValue
variable = disp_y
nodeid = 1
[../]
[./horz_forces_y]
type = PointValue
point = '9.9 60.0 0.0'
variable = forces_y
[../]
[./forces_y]
type = PointValue
point = '10.0 59.9 0.0'
variable = forces_y
[../]
[]
[Outputs]
csv = true
exodus = true
[]
(test/tests/geomsearch/3d_moving_penetration_smoothing/pl_test4nns.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
file = pl_test4.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./normal_z]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./closest_point_z]
[../]
# [./element_id]
# [../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[./diff_z]
type = Diffusion
variable = disp_z
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
normal_smoothing_method = nodal_normal_based
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = normal_z
boundary = 11
paired_boundary = 12
quantity = normal_z
[../]
[./penetrate10]
type = PenetrationAux
variable = normal_z
boundary = 12
paired_boundary = 11
quantity = normal_z
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate13]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate14]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate15]
type = PenetrationAux
variable = closest_point_z
boundary = 11
paired_boundary = 12
quantity = closest_point_z
[../]
[./penetrate16]
type = PenetrationAux
variable = closest_point_z
boundary = 12
paired_boundary = 11
quantity = closest_point_z
[../]
# [./penetrate17]
# type = PenetrationAux
# variable = element_id
# boundary = 11
# paired_boundary = 12
# quantity = element_id
# [../]
#
# [./penetrate18]
# type = PenetrationAux
# variable = element_id
# boundary = 12
# paired_boundary = 11
# quantity = element_id
# [../]
[./penetrate19]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate20]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b1z]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[./b2z]
type = DirichletBC
variable = disp_z
boundary = 2
value = 0
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-9
l_max_its = 10
start_time = 0.0
dt = 0.02
end_time = 1.0
[]
[Outputs]
file_base = pl_test4nns_out
exodus = true
[]
[NodalNormals]
boundary = 11
corner_boundary = 20
[]
(test/tests/geomsearch/2d_moving_penetration/pl_test1q.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
file = pl_test1q.e
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate10]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate13]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate14]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate15]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate16]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 0.7 -0.7 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1.e-9
l_max_its = 10
start_time = 0.0
dt = 0.05
end_time = 1.0
[./Quadrature]
order = THIRD
[../]
[]
[Outputs]
file_base = pl_test1q_out
exodus = true
[]
(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/geomsearch/3d_moving_penetration_smoothing/pl_test3qns.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
file = pl_test3q.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./normal_z]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./closest_point_z]
[../]
# [./element_id]
# [../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[./diff_z]
type = Diffusion
variable = disp_z
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
normal_smoothing_distance = 0.2
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
normal_smoothing_distance = 0.2
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = normal_z
boundary = 11
paired_boundary = 12
quantity = normal_z
[../]
[./penetrate10]
type = PenetrationAux
variable = normal_z
boundary = 12
paired_boundary = 11
quantity = normal_z
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate13]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate14]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate15]
type = PenetrationAux
variable = closest_point_z
boundary = 11
paired_boundary = 12
quantity = closest_point_z
[../]
[./penetrate16]
type = PenetrationAux
variable = closest_point_z
boundary = 12
paired_boundary = 11
quantity = closest_point_z
[../]
# [./penetrate17]
# type = PenetrationAux
# variable = element_id
# boundary = 11
# paired_boundary = 12
# quantity = element_id
# [../]
#
# [./penetrate18]
# type = PenetrationAux
# variable = element_id
# boundary = 12
# paired_boundary = 11
# quantity = element_id
# [../]
[./penetrate19]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate20]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
preset = false
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
preset = false
boundary = 1
value = 0
[../]
[./b1z]
type = DirichletBC
variable = disp_z
preset = false
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
preset = false
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
preset = false
boundary = 2
function = disp_y
[../]
[./b2z]
type = DirichletBC
variable = disp_z
preset = false
boundary = 2
value = 0
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-9
l_max_its = 10
start_time = 0.0
dt = 0.025
end_time = 1.0
[./Quadrature]
order = THIRD
[../]
[]
[Outputs]
file_base = pl_test3qns_out
exodus = true
[]
(modules/combined/test/tests/power_law_creep/power_law_creep_restart1.i)
# 1x1x1 unit cube with uniform pressure on top face
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
[]
[Variables]
[./temp]
order = FIRST
family = LAGRANGE
initial_condition = 1000.0
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
incremental = true
add_variables = true
generate_output = 'stress_yy creep_strain_xx creep_strain_yy creep_strain_zz elastic_strain_yy'
[../]
[]
[Functions]
[./top_pull]
type = PiecewiseLinear
x = '0 1'
y = '1 1'
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[./heat_ie]
type = HeatConductionTimeDerivative
variable = temp
[../]
[]
[BCs]
[./u_top_pull]
type = Pressure
variable = disp_y
component = 1
boundary = top
factor = -10.0e6
function = top_pull
[../]
[./u_bottom_fix]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./u_yz_fix]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./u_xy_fix]
type = DirichletBC
variable = disp_z
boundary = back
value = 0.0
[../]
[./temp_fix]
type = DirichletBC
variable = temp
boundary = 'bottom top'
value = 1000.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 2e11
poissons_ratio = 0.3
[../]
[./radial_return_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'power_law_creep'
[../]
[./power_law_creep]
type = PowerLawCreepStressUpdate
coefficient = 1.0e-15
n_exponent = 4
activation_energy = 3.0e5
temperature = temp
[../]
[./thermal]
type = HeatConductionMaterial
specific_heat = 1.0
thermal_conductivity = 100.
[../]
[./density]
type = Density
density = 1.0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 20
nl_max_its = 20
nl_rel_tol = 1e-6
nl_abs_tol = 1e-6
l_tol = 1e-5
start_time = 0.0
end_time = 1.0
num_steps = 6
dt = 0.1
[]
[Outputs]
exodus = true
csv = true
[./out]
type = Checkpoint
num_files = 1
[../]
[]
(modules/tensor_mechanics/test/tests/torque_reaction/disp_about_axis_errors.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
[]
[Functions]
[./rampConstant]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = 1.
[../]
[]
[Modules/TensorMechanics/Master]
[master]
strain = FINITE
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
add_variables = true
[]
[]
[BCs]
[./bottom_x]
type = DirichletBC
variable = disp_x
boundary = bottom
value = 0.0
[../]
[./bottom_y]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./bottom_z]
type = DirichletBC
variable = disp_z
boundary = bottom
value = 0.0
[../]
[./top_x]
type = DisplacementAboutAxis
boundary = top
function = rampConstant
angle_units = degrees
axis_origin = '0. 0. 0.'
axis_direction = '0. 0. 1.'
component = 0
variable = disp_x
[../]
[./top_y]
type = DisplacementAboutAxis
boundary = top
function = rampConstant
angle_units = degrees
axis_origin = '0. 0. 0.'
variable = disp_y
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = 0
youngs_modulus = 207000
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 30
nl_max_its = 20
nl_rel_tol = 1e-10
nl_abs_tol = 1e-12
l_tol = 1e-8
start_time = 0.0
dt = 0.1
dtmin = 0.1 # die instead of cutting the timestep
end_time = 0.5
[]
[Outputs]
exodus = true
[]
(modules/combined/test/tests/internal_volume/rz_cone.i)
#
# Internal Volume Test
#
# This test is designed to compute the internal volume of a cone.
#
# The mesh is composed of one block (1). The height is 3/pi, and the radius
# is 1. Thus, the volume is 1/3*pi*r^2*h = 1.
#
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Problem]
coord_type = RZ
[]
[Mesh]
file = meshes/rz_cone.e
[]
[Functions]
[./pressure]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = 1e4
[../]
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
volumetric_locking_correction = true
incremental = true
strain = FINITE
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./Pressure]
[./fred]
boundary = 1
function = pressure
[../]
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
nl_abs_tol = 1e-9
start_time = 0.0
dt = 1.0
end_time = 1.0
[]
[Postprocessors]
[./internalVolume]
type = InternalVolume
boundary = 1
execute_on = 'initial timestep_end'
[../]
[]
[Outputs]
exodus = true
csv = true
[]
(modules/richards/test/tests/recharge_discharge/rd01.i)
[Mesh]
type = GeneratedMesh
dim = 2
# very little mesh dependence here
nx = 120
ny = 1
xmin = 0
xmax = 6
ymin = 0
ymax = 0.05
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1E-2 1 10 500 5000 5000'
x = '0 10 100 1000 10000 100000'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1E3
bulk_mod = 2E7
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.336
al = 1.43E-4
[../]
[./RelPermPower]
type = RichardsRelPermVG1
scut = 0.99
simm = 0.0
m = 0.336
[../]
[./Saturation]
type = RichardsSat
s_res = 0.0
sum_s_res = 0.0
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 1.0E+2
[../]
[]
[Variables]
active = 'pressure'
[./pressure]
order = FIRST
family = LAGRANGE
initial_condition = -72620.4
[../]
[]
[Kernels]
active = 'richardsf richardst'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = SeffVG
pressure_vars = pressure
[../]
[]
[BCs]
active = 'recharge'
[./recharge]
type = RichardsPiecewiseLinearSink
variable = pressure
boundary = 'right'
pressures = '0 1E9'
bare_fluxes = '-2.315E-3 -2.315E-3'
use_relperm = false
use_mobility = false
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.33
mat_permeability = '0.295E-12 0 0 0 0.295E-12 0 0 0 0.295E-12'
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGstandard
sat_UO = Saturation
seff_UO = SeffVG
viscosity = 1.01E-3
gravity = '-10 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
active = 'andy'
[./andy]
type = SMP
full = true
petsc_options = ''
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-13 1E-15 10000'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
petsc_options = '-snes_converged_reason'
end_time = 359424
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = rd01
interval = 100000
execute_on = 'initial final'
exodus = true
[]
(modules/tensor_mechanics/test/tests/ad_anisotropic_plasticity/ad_aniso_plasticity_x.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
nx = 10
ny = 2
nz = 2
xmin = 0.0
ymin = 0.0
zmin = 0.0
xmax = 10.0
ymax = 1.0
zmax = 1.0
[]
[corner_node]
type = ExtraNodesetGenerator
new_boundary = '100'
nodes = '3 69'
input = gen
[]
[corner_node_2]
type = ExtraNodesetGenerator
new_boundary = '101'
nodes = '4 47'
input = corner_node
[]
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[AuxVariables]
[hydrostatic_stress]
order = CONSTANT
family = MONOMIAL
[]
[plastic_strain_xx]
order = CONSTANT
family = MONOMIAL
[]
[plastic_strain_xy]
order = CONSTANT
family = MONOMIAL
[]
[plastic_strain_yy]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[hydrostatic_stress]
type = ADRankTwoScalarAux
variable = hydrostatic_stress
rank_two_tensor = stress
scalar_type = Hydrostatic
[]
[plasticity_strain_xx]
type = ADRankTwoAux
rank_two_tensor = trial_plasticity_plastic_strain
variable = plastic_strain_xx
index_i = 0
index_j = 0
[]
[plasticity_strain_xy]
type = ADRankTwoAux
rank_two_tensor = trial_plasticity_plastic_strain
variable = plastic_strain_xy
index_i = 0
index_j = 1
[]
[plasticity_strain_yy]
type = ADRankTwoAux
rank_two_tensor = trial_plasticity_plastic_strain
variable = plastic_strain_yy
index_i = 1
index_j = 1
[]
[sigma_xx]
type = ADRankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 1
index_j = 1
[]
[]
[Functions]
[pull]
type = PiecewiseLinear
x = '0 1e1 1e8'
y = '0 -4e2 -4e2'
[]
[]
[Modules/TensorMechanics/Master]
[all]
strain = FINITE
generate_output = 'elastic_strain_xx stress_xx'
use_automatic_differentiation = true
add_variables = true
[]
[]
[Materials]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 70000
poissons_ratio = 0.25
[]
[elastic_strain]
type = ADComputeMultipleInelasticStress
inelastic_models = "trial_plasticity"
max_iterations = 50
absolute_tolerance = 1e-16
[]
[trial_plasticity]
type = ADHillPlasticityStressUpdate
hardening_constant = 2000.0
yield_stress = 0.001 # was 200 for verification
# F G H L M N
hill_constants = "0.5829856 0.364424 0.6342174 2.0691375 2.3492325 1.814589"
absolute_tolerance = 1e-14
relative_tolerance = 1e-12
base_name = trial_plasticity
internal_solve_full_iteration_history = true
max_inelastic_increment = 2.0e-6
internal_solve_output_on = on_error
[]
[]
[BCs]
[no_disp_x]
type = ADDirichletBC
variable = disp_x
boundary = left
value = 0.0
[]
[no_disp_y]
type = ADDirichletBC
variable = disp_y
boundary = 100
value = 0.0
[]
[no_disp_z]
type = ADDirichletBC
variable = disp_z
boundary = 101
value = 0.0
[]
[Pressure]
[Side1]
boundary = right
function = pull
[]
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
nl_rel_tol = 1e-11
nl_abs_tol = 1.0e-14
l_max_its = 90
num_steps = 25
[TimeStepper]
type = IterationAdaptiveDT
optimal_iterations = 30
iteration_window = 9
growth_factor = 1.05
cutback_factor = 0.5
timestep_limiting_postprocessor = matl_ts_min
dt = 1.0e-5
time_t = '0 3.4e-5 10'
time_dt = '1.0e-5 1.0e-7 1.0e-7'
[]
start_time = 0
automatic_scaling = true
[]
[Postprocessors]
[matl_ts_min]
type = MaterialTimeStepPostprocessor
[]
[max_disp_x]
type = ElementExtremeValue
variable = disp_x
[]
[max_disp_y]
type = ElementExtremeValue
variable = disp_y
[]
[max_hydro]
type = ElementAverageValue
variable = hydrostatic_stress
[]
[dt]
type = TimestepSize
[]
[num_lin]
type = NumLinearIterations
outputs = console
[]
[num_nonlin]
type = NumNonlinearIterations
outputs = console
[]
[plasticity_strain_xx]
type = ElementalVariableValue
variable = plastic_strain_xx
execute_on = 'TIMESTEP_END'
elementid = 39
[]
[elastic_strain_xx]
type = ElementalVariableValue
variable = elastic_strain_xx
execute_on = 'TIMESTEP_END'
elementid = 39
[]
[sigma_xx]
type = ElementalVariableValue
variable = stress_xx
execute_on = 'TIMESTEP_END'
elementid = 39
[]
[]
[Outputs]
csv = true
exodus = true
perf_graph = true
[]
(modules/contact/test/tests/normalized_penalty/normalized_penalty_kin_Q8.i)
[GlobalParams]
order = SECOND
displacements = 'disp_x disp_y'
[]
[Mesh]
file = normalized_penalty_Q8.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[AuxVariables]
[./saved_x]
[../]
[./saved_y]
[../]
[]
[Functions]
[./left_x]
type = PiecewiseLinear
x = '0 1 2'
y = '0 0.02 0'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = FINITE
generate_output = 'stress_xx'
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
[]
[]
[Contact]
[./m3_s2]
primary = 3
secondary = 2
penalty = 1e10
normalize_penalty = true
tangential_tolerance = 1e-3
[../]
[]
[BCs]
[./left_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 1
function = left_x
[../]
[./y]
type = DirichletBC
variable = disp_y
boundary = '1 2 3 4'
value = 0.0
[../]
[./right]
type = DirichletBC
variable = disp_x
boundary = '3 4'
value = 0
[../]
[]
[Materials]
[./stiffStuff1]
type = ComputeIsotropicElasticityTensor
block = '1 2 3 4 1000'
youngs_modulus = 3e8
poissons_ratio = 0.0
[../]
[./stiffStuff1_stress]
type = ComputeFiniteStrainElasticStress
block = '1 2 3 4 1000'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -ksp_gmres_restart'
petsc_options_value = 'lu 101'
line_search = 'none'
nl_rel_tol = 1e-12
nl_abs_tol = 5e-8
l_max_its = 100
nl_max_its = 20
dt = 0.5
num_steps = 4
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/plane_stress/weak_plane_stress_finite.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
temperature = temp
out_of_plane_strain = strain_zz
[]
[Mesh]
[./square]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 2
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./strain_zz]
[../]
[]
[AuxVariables]
[./temp]
[../]
[./nl_strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Postprocessors]
[./react_z]
type = MaterialTensorIntegral
rank_two_tensor = stress
index_i = 2
index_j = 2
[../]
[./min_strain_zz]
type = NodalExtremeValue
variable = strain_zz
value_type = min
[../]
[./max_strain_zz]
type = NodalExtremeValue
variable = strain_zz
value_type = max
[../]
[]
[Modules/TensorMechanics/Master]
[plane_stress]
planar_formulation = WEAK_PLANE_STRESS
strain = FINITE
generate_output = 'stress_xx stress_xy stress_yy stress_zz strain_xx strain_xy strain_yy'
eigenstrain_names = eigenstrain
[]
[]
[AuxKernels]
[./tempfuncaux]
type = FunctionAux
variable = temp
function = tempfunc
use_displaced_mesh = false
[../]
[./strain_zz]
type = RankTwoAux
rank_two_tensor = total_strain
variable = nl_strain_zz
index_i = 2
index_j = 2
[../]
[]
[Functions]
[./pull]
type = PiecewiseLinear
x='0 1 100'
y='0 0.00 0.00'
[../]
[./tempfunc]
type = ParsedFunction
value = '(1 - x) * t'
[../]
[]
[BCs]
[./bottomx]
type = DirichletBC
boundary = 0
variable = disp_x
value = 0.0
[../]
[./bottomy]
type = DirichletBC
boundary = 0
variable = disp_y
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
poissons_ratio = 0.3
youngs_modulus = 1e6
[../]
[./thermal_strain]
type = ComputeThermalExpansionEigenstrain
thermal_expansion_coeff = 0.02
stress_free_temperature = 0.5
eigenstrain_name = eigenstrain
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
line_search = none
# controls for linear iterations
l_max_its = 100
l_tol = 1e-06
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-12
nl_abs_tol = 1e-10
# time control
start_time = 0.0
dt = 1.0
dtmin = 1.0
end_time = 2.0
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/creep_tangent_operator/creep.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
second_order = true
[]
[GlobalParams]
displacements = 'disp_x disp_y'
volumetric_locking_correction = false
[]
[Functions]
[./pull]
type = PiecewiseLinear
x = '0 10'
y = '0 1e-3'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
use_finite_deform_jacobian = true
generate_output = 'hydrostatic_stress'
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e10
poissons_ratio = 0.3
[../]
[./elastic_strain]
type = ComputeMultipleInelasticStress
# inelastic_models = ''
tangent_operator = nonlinear
[../]
[./creep_ten]
type = PowerLawCreepStressUpdate
coefficient = 10e-24
n_exponent = 4
activation_energy = 0
base_name = creep_ten
[../]
[./creep_ten2]
type = PowerLawCreepStressUpdate
coefficient = 10e-24
n_exponent = 4
activation_energy = 0
base_name = creep_ten2
[../]
[./creep_one]
type = PowerLawCreepStressUpdate
coefficient = 1e-24
n_exponent = 4
activation_energy = 0
base_name = creep_one
[../]
[./creep_nine]
type = PowerLawCreepStressUpdate
coefficient = 9e-24
n_exponent = 4
activation_energy = 0
base_name = creep_nine
[../]
[./creep_zero]
type = PowerLawCreepStressUpdate
coefficient = 0e-24
n_exponent = 4
activation_energy = 0
base_name = creep_zero
[../]
[]
[BCs]
[./no_disp_x]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./no_disp_y]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./pull_disp_y]
type = FunctionDirichletBC
variable = disp_y
boundary = top
function = pull
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
line_search = 'none'
nl_rel_tol = 1e-5
num_steps = 5
dt = 1e-1
[]
[Postprocessors]
[./max_disp_x]
type = ElementExtremeValue
variable = disp_x
[../]
[./max_disp_y]
type = ElementExtremeValue
variable = disp_y
[../]
[./max_hydro]
type = ElementAverageValue
variable = hydrostatic_stress
[../]
[./dt]
type = TimestepSize
[../]
[./num_lin]
type = NumLinearIterations
outputs = console
[../]
[./num_nonlin]
type = NumNonlinearIterations
outputs = console
[../]
[]
[Outputs]
csv = true
perf_graph = true
[]
[Debug]
show_var_residual_norms = true
[]
(modules/combined/test/tests/elastic_thermal_patch/elastic_thermal_patch.i)
# Patch Test
# This test is designed to compute constant xx, yy, zz, xy, yz, and zx
# stress on a set of irregular hexes. The mesh is composed of one
# block with seven elements. The elements form a unit cube with one
# internal element. There is a nodeset for each exterior node.
# The cube is displaced by 1e-6 units in x, 2e-6 in y, and 3e-6 in z.
# The faces are sheared as well (1e-6, 2e-6, and 3e-6 for xy, yz, and
# zx). This gives a uniform strain/stress state for all six unique
# tensor components.
# With Young's modulus at 1e6 and Poisson's ratio at 0, the shear
# modulus is 5e5 (G=E/2/(1+nu)). Therefore, for the mechanical strain,
#
# stress xx = 1e6 * 1e-6 = 1
# stress yy = 1e6 * 2e-6 = 2
# stress zz = 1e6 * 3e-6 = 3
# stress xy = 2 * 5e5 * 1e-6 / 2 = 0.5
# (2 * G * gamma_xy / 2 = 2 * G * epsilon_xy)
# stress yz = 2 * 5e5 * 2e-6 / 2 = 1
# stress zx = 2 * 5e5 * 3e-6 / 2 = 1.5
# However, we must also consider the thermal strain.
# The temperature moves 100 degrees, and the coefficient of thermal
# expansion is 1e-8. Therefore, the thermal strain (and the displacement
# since this is a unit cube) is 1e-6.
# Therefore, the overall effect is (at time 1, with a 50 degree delta):
#
# stress xx = 1e6 * (1e-6-0.5e-6) = 0.5
# stress yy = 1e6 * (2e-6-0.5e-6) = 1.5
# stress zz = 1e6 * (3e-6-0.5e-6) = 2.5
# stress xy = 2 * 5e5 * 1e-6 / 2 = 0.5
# (2 * G * gamma_xy / 2 = 2 * G * epsilon_xy)
# stress yz = 2 * 5e5 * 2e-6 / 2 = 1
# stress zx = 2 * 5e5 * 3e-6 / 2 = 1.5
#
# At time 2:
#
# stress xx = 1e6 * (1e-6-1e-6) = 0
# stress yy = 1e6 * (2e-6-1e-6) = 1
# stress zz = 1e6 * (3e-6-1e-6) = 2
# stress xy = 2 * 5e5 * 1e-6 / 2 = 0.5
# (2 * G * gamma_xy / 2 = 2 * G * epsilon_xy)
# stress yz = 2 * 5e5 * 2e-6 / 2 = 1
# stress zx = 2 * 5e5 * 3e-6 / 2 = 1.5
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
temperature = temp
[]
[Mesh]
file = elastic_thermal_patch_test.e
[]
[Functions]
[./rampConstant1]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 1.'
scale_factor = 1e-6
[../]
[./rampConstant2]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 1.'
scale_factor = 2e-6
[../]
[./rampConstant3]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 1.'
scale_factor = 3e-6
[../]
[./rampConstant4]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 1.'
scale_factor = 4e-6
[../]
[./rampConstant6]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 1.'
scale_factor = 6e-6
[../]
[./tempFunc]
type = PiecewiseLinear
x = '0. 2.'
y = '117.56 217.56'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[./temp]
initial_condition = 117.56
[../]
[]
[Modules/TensorMechanics/Master/All]
add_variables = true
strain = FINITE
eigenstrain_names = eigenstrain
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx'
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[]
[BCs]
[./node1_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./node1_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 1
function = rampConstant2
[../]
[./node1_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 1
function = rampConstant3
[../]
[./node2_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 2
function = rampConstant1
[../]
[./node2_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = rampConstant2
[../]
[./node2_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 2
function = rampConstant6
[../]
[./node3_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 3
function = rampConstant1
[../]
[./node3_y]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.0
[../]
[./node3_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 3
function = rampConstant3
[../]
[./node4_x]
type = DirichletBC
variable = disp_x
boundary = 4
value = 0.0
[../]
[./node4_y]
type = DirichletBC
variable = disp_y
boundary = 4
value = 0.0
[../]
[./node4_z]
type = DirichletBC
variable = disp_z
boundary = 4
value = 0.0
[../]
[./node5_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 5
function = rampConstant1
[../]
[./node5_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 5
function = rampConstant4
[../]
[./node5_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 5
function = rampConstant3
[../]
[./node6_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 6
function = rampConstant2
[../]
[./node6_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 6
function = rampConstant4
[../]
[./node6_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 6
function = rampConstant6
[../]
[./node7_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 7
function = rampConstant2
[../]
[./node7_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 7
function = rampConstant2
[../]
[./node7_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 7
function = rampConstant3
[../]
[./node8_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 8
function = rampConstant1
[../]
[./node8_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 8
function = rampConstant2
[../]
[./node8_z]
type = DirichletBC
variable = disp_z
boundary = 8
value = 0.0
[../]
[./temp]
type = FunctionDirichletBC
variable = temp
boundary = '10 12'
function = tempFunc
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
bulk_modulus = 0.333333333333333e6
shear_modulus = 0.5e6
[../]
[./thermal_strain]
type = ComputeThermalExpansionEigenstrain
stress_free_temperature = 117.56
thermal_expansion_coeff = 1e-8
eigenstrain_name = eigenstrain
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[./heat]
type = HeatConductionMaterial
specific_heat = 1.0
thermal_conductivity = 1.0
[../]
[./density]
type = Density
density = 1.0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
nl_rel_tol = 1e-12
l_max_its = 20
start_time = 0.0
dt = 1.0
num_steps = 2
end_time = 2.0
[]
[Outputs]
exodus = true
[]
(modules/combined/test/tests/thermal_elastic/thermal_elastic.i)
# Patch Test
# This test is designed to compute constant xx, yy, zz, xy, yz, and xz
# stress on a set of irregular hexes. The mesh is composed of one
# block with seven elements. The elements form a unit cube with one
# internal element. There is a nodeset for each exterior node.
# The cube is displaced by 1e-6 units in x, 2e-6 in y, and 3e-6 in z.
# The faces are sheared as well (1e-6, 2e-6, and 3e-6 for xy, yz, and
# zx). This gives a uniform strain/stress state for all six unique
# tensor components. This displacement is again applied in the second
# step.
# With Young's modulus at 1e6 and Poisson's ratio at 0, the shear
# modulus is 5e5 (G=E/2/(1+nu)). Therefore, for the mechanical strain,
#
# stress xx = 1e6 * 1e-6 = 1
# stress yy = 1e6 * 2e-6 = 2
# stress zz = 1e6 * 3e-6 = 3
# stress xy = 2 * 5e5 * 1e-6 / 2 = 0.5
# (2 * G * gamma_xy / 2 = 2 * G * epsilon_xy)
# stress yz = 2 * 5e5 * 2e-6 / 2 = 1
# stress zx = 2 * 5e5 * 3e-6 / 2 = 1.5
# Young's modulus is a function of temperature for this test. The
# temperature changes from 100 to 500. The Young's modulus drops
# due to that temperature change from 1e6 to 6e5.
# Poisson's ratio also is a function of temperature and changes from
# 0 to 0.25.
# At the end of the temperature ramp, E=6e5 and nu=0.25. This gives
# G=2.4e=5. lambda=E*nu/(1+nu)/(1-2*nu)=2.4E5. The final stress
# is therefore
# stress xx = 2.4e5 * 12e-6 + 2*2.4e5*2e-6 = 3.84
# stress yy = 2.4e5 * 12e-6 + 2*2.4e5*4e-6 = 4.80
# stress zz = 2.4e5 * 12e-6 + 2*2.4e5*6e-6 = 5.76
# stress xy = 2 * 2.4e5 * 2e-6 / 2 = 0.48
# (2 * G * gamma_xy / 2 = 2 * G * epsilon_xy)
# stress yz = 2 * 2.4e5 * 4e-6 / 2 = 0.96
# stress xz = 2 * 2.4e5 * 6e-6 / 2 = 1.44
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
file = thermal_elastic.e
[]
[Functions]
[./ramp1]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 2.'
scale_factor = 1e-6
[../]
[./ramp2]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 2.'
scale_factor = 2e-6
[../]
[./ramp3]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 2.'
scale_factor = 3e-6
[../]
[./ramp4]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 2.'
scale_factor = 4e-6
[../]
[./ramp6]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 2.'
scale_factor = 6e-6
[../]
[./tempFunc]
type = PiecewiseLinear
x = '0 1 2'
y = '100.0 100.0 500.0'
[../]
[]
[Variables]
[./temp]
initial_condition = 100.0
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_xz stress_yz'
strain = FINITE
[../]
[]
[Kernels]
[./heat]
type = Diffusion
variable = temp
[../]
[]
[BCs]
[./node1_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./node1_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 1
function = ramp2
[../]
[./node1_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 1
function = ramp3
[../]
[./node2_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 2
function = ramp1
[../]
[./node2_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = ramp2
[../]
[./node2_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 2
function = ramp6
[../]
[./node3_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 3
function = ramp1
[../]
[./node3_y]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.0
[../]
[./node3_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 3
function = ramp3
[../]
[./node4_x]
type = DirichletBC
variable = disp_x
boundary = 4
value = 0.0
[../]
[./node4_y]
type = DirichletBC
variable = disp_y
boundary = 4
value = 0.0
[../]
[./node4_z]
type = DirichletBC
variable = disp_z
boundary = 4
value = 0.0
[../]
[./node5_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 5
function = ramp1
[../]
[./node5_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 5
function = ramp4
[../]
[./node5_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 5
function = ramp3
[../]
[./node6_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 6
function = ramp2
[../]
[./node6_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 6
function = ramp4
[../]
[./node6_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 6
function = ramp6
[../]
[./node7_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 7
function = ramp2
[../]
[./node7_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 7
function = ramp2
[../]
[./node7_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 7
function = ramp3
[../]
[./node8_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 8
function = ramp1
[../]
[./node8_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 8
function = ramp2
[../]
[./node8_z]
type = DirichletBC
variable = disp_z
boundary = 8
value = 0.0
[../]
[./temp]
type = FunctionDirichletBC
variable = temp
boundary = '10 12'
function = tempFunc
[../]
[]
[Materials]
[./youngs_modulus]
type = PiecewiseLinearInterpolationMaterial
x = '100 500'
y = '1e6 6e5'
property = youngs_modulus
variable = temp
[../]
[./poissons_ratio]
type = PiecewiseLinearInterpolationMaterial
x = '100 500'
y = '0 0.25'
property = poissons_ratio
variable = temp
[../]
[./elasticity_tensor]
type = ComputeVariableIsotropicElasticityTensor
args = temp
youngs_modulus = youngs_modulus
poissons_ratio = poissons_ratio
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
nl_rel_tol = 1e-9
nl_abs_tol = 1e-9
l_max_its = 20
start_time = 0.0
dt = 1.0
end_time = 2.0
[]
[Outputs]
exodus = true
[]
(modules/contact/test/tests/hertz_spherical/hertz_contact_rz.i)
# Hertz Contact: Sphere on sphere
# Spheres have the same radius, Young's modulus, and Poisson's ratio.
# Define E:
# 1/E = (1-nu1^2)/E1 + (1-nu2^2)/E2
#
# Effective radius R:
# 1/R = 1/R1 + 1/R2
#
# F is the applied compressive load.
#
# Area of contact a::
# a^3 = 3FR/4E
#
# Depth of indentation d:
# d = a^2/R
#
#
# Let R1 = R2 = 2. Then R = 1.
#
# Let nu1 = nu2 = 0.25, E1 = E2 = 1.40625e7. Then E = 7.5e6.
#
# Let F = 10000. Then a = 0.1, d = 0.01.
#
## Note: There is not a good way to check the result. The standard approach is
## to map contact pressure as a function of radius, but we don't have the
## contact pressure available. See the description on Wikipedia for details of
## analytic equations, and the Abaqus Benchmarks Manual, 1.1.11, for a plot of
## contact pressure vs. radius.
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Problem]
coord_type = RZ
[]
[Mesh]#Comment
file = hertz_contact_rz.e
displacements = 'disp_x disp_y'
allow_renumbering = false
[] # Mesh
[Functions]
[./pressure]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 1.'
scale_factor = 795.77471545947674 # 10000/pi/2^2
[../]
[./disp_y]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. -0.01 -0.01'
[../]
[] # Functions
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[] # Variables
[AuxVariables]
[./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_zx]
order = CONSTANT
family = MONOMIAL
[../]
[./vonmises]
order = CONSTANT
family = MONOMIAL
[../]
[./hydrostatic]
order = CONSTANT
family = MONOMIAL
[../]
[] # AuxVariables
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = SMALL
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 0
variable = stress_xx
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 1
variable = stress_yy
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 2
variable = stress_zz
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 1
variable = stress_xy
[../]
[./stress_yz]
type = RankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 2
variable = stress_yz
[../]
[./stress_zx]
type = RankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 0
variable = stress_zx
[../]
[] # AuxKernels
[BCs]
[./base_y]
type = DirichletBC
variable = disp_y
boundary = 1000
value = 0.0
[../]
[./symm_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./disp_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[] # BCs
[Contact]
[./dummy_name]
primary = 1000
secondary = 100
model = coulomb
formulation = penalty
normalize_penalty = true
friction_coefficient = 0.4
penalty = 8e7
tangential_tolerance = 0.005
[../]
[]
[Materials]
[./tensor]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1.40625e7
poissons_ratio = 0.25
[../]
[./stress]
type = ComputeLinearElasticStress
block = '1'
[../]
[./tensor_1000]
type = ComputeIsotropicElasticityTensor
block = '1000'
youngs_modulus = 1e6
poissons_ratio = 0.0
[../]
[./stress_1000]
type = ComputeLinearElasticStress
block = '1000'
[../]
[] # Materials
[Preconditioning]
[./SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart'
petsc_options_value = 'hypre boomeramg 101'
line_search = 'none'
nl_abs_tol = 1e-7
l_max_its = 200
start_time = 0.0
dt = 0.5
end_time = 2.0
[] # Executioner
[Postprocessors]
[./maxdisp]
type = NodalVariableValue
nodeid = 39 # 40-1 where 40 is the exodus node number of the top-left node
variable = disp_y
[../]
[]
[Outputs]
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[] # Outputs
(test/tests/geomsearch/2d_moving_penetration/pl_test3nns.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
file = pl_test3.e
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
normal_smoothing_method = nodal_normal_based
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate10]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate13]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate14]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate15]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate16]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-10
l_max_its = 10
start_time = 0.0
dt = 0.0125
end_time = 1.0
[]
[Outputs]
file_base = pl_test3nns_out
exodus = true
[]
[NodalNormals]
boundary = 11
corner_boundary = 20
[]
(modules/geochemistry/test/tests/time_dependent_reactions/mixing.i)
# Seawater at temperature=4degC is slowly mixed with this fluid initially at temperature=273degC until a 10:1 ratio is achieved
[TimeDependentReactionSolver]
model_definition = definition
geochemistry_reactor_name = reactor
swap_into_basis = "H2S(aq)"
swap_out_of_basis = "O2(aq)"
charge_balance_species = "Cl-"
constraint_species = "H2O H+ Cl- Na+ Mg++ SO4-- Ca++ K+ HCO3- Ba++ SiO2(aq) Sr++ Zn++ Cu+ Al+++ Fe++ Mn++ H2S(aq)"
constraint_value = " 1.0 6.309573E-5 600E-3 529E-3 0.01E-6 0.01E-6 21.6E-3 26.7E-3 2.0E-3 15E-6 20.2E-3 100.5E-6 41E-6 0.02E-6 4.1E-6 903E-6 1039E-6 6.81E-3"
constraint_meaning = "kg_solvent_water activity bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition bulk_composition 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 moles moles moles moles moles moles moles"
close_system_at_time = -0.01
remove_fixed_activity_name = 'H+'
remove_fixed_activity_time = -0.01
initial_temperature = 273
temperature = T
# The following source species and rates are taken from the Geochemists Workbench (see output from mixing.rea)
# An alternative is to run the seawater_mixing MOOSE input files and extract the source species and rates
source_species_names = "H2O Al+++ Ba++ Ca++ Cl- Cu+ Fe++ H+ HCO3- K+ Mg++ Mn++ Na+ O2(aq) SO4-- SiO2(aq) Sr++ Zn++"
source_species_rates = "H2O_rate Al+++_rate Ba++_rate Ca++_rate Cl-_rate Cu+_rate Fe++_rate H+_rate HCO3-_rate K+_rate Mg++_rate Mn++_rate Na+_rate O2aq_rate SO4--_rate SiO2aq_rate Sr++_rate Zn++_rate"
mode = mode
execute_console_output_on = '' # only CSV output needed for this example
stoichiometric_ionic_str_using_Cl_only = true # for comparison with GWB
[]
[AuxVariables]
[T]
[]
[mode]
[]
[H2O_rate]
[]
[Al+++_rate]
[]
[Ba++_rate]
[]
[Ca++_rate]
[]
[Cl-_rate]
[]
[Cu+_rate]
[]
[Fe++_rate]
[]
[H+_rate]
[]
[HCO3-_rate]
[]
[K+_rate]
[]
[Mg++_rate]
[]
[Mn++_rate]
[]
[Na+_rate]
[]
[O2aq_rate]
[]
[SO4--_rate]
[]
[SiO2aq_rate]
[]
[Sr++_rate]
[]
[Zn++_rate]
[]
[]
[AuxKernels]
[mode_auxk]
type = FunctionAux
variable = mode
function = 'if(t<=0, 1, 0)' # dump at start of first timestep
execute_on = timestep_begin
[]
[T_auxk]
type = FunctionAux
variable = T
function = 'if(t<=0, 273, 4)' # during initialisation and dumping, T=273, while during adding T=temperature of reactants
execute_on = timestep_begin
[]
[H2O_rate_auxk]
type = FunctionAux
variable = H2O_rate
execute_on = timestep_begin
function = 'if(t<=0, 0, 55.510000000000005)'
[]
[Al+++_rate]
type = FunctionAux
variable = Al+++_rate
execute_on = timestep_begin
function = 'if(t<=0, 0, 3.643e-10)'
[]
[Ba++_rate]
type = FunctionAux
variable = Ba++_rate
execute_on = timestep_begin
function = 'if(t<=0, 0, 8.831e-08)'
[]
[Ca++_rate]
type = FunctionAux
variable = Ca++_rate
execute_on = timestep_begin
function = 'if(t<=0, 0, 0.0104)'
[]
[Cl-_rate]
type = FunctionAux
variable = Cl-_rate
execute_on = timestep_begin
function = 'if(t<=0, 0, 0.559)'
[]
[Cu+_rate]
type = FunctionAux
variable = Cu+_rate
execute_on = timestep_begin
function = 'if(t<=0, 0, 7.000000000000001e-09)'
[]
[Fe++_rate]
type = FunctionAux
variable = Fe++_rate
execute_on = timestep_begin
function = 'if(t<=0, 0, 4.746e-15)'
[]
[H+_rate]
type = FunctionAux
variable = H+_rate
execute_on = timestep_begin
function = 'if(t<=0, 0, 0.0002005)'
[]
[HCO3-_rate]
type = FunctionAux
variable = HCO3-_rate
execute_on = timestep_begin
function = 'if(t<=0, 0, 0.002153)'
[]
[K+_rate]
type = FunctionAux
variable = K+_rate
execute_on = timestep_begin
function = 'if(t<=0, 0, 0.010100000000000001)'
[]
[Mg++_rate]
type = FunctionAux
variable = Mg++_rate
execute_on = timestep_begin
function = 'if(t<=0, 0, 0.054400000000000004)'
[]
[Mn++_rate]
type = FunctionAux
variable = Mn++_rate
execute_on = timestep_begin
function = 'if(t<=0, 0, 6.79e-14)'
[]
[Na+_rate]
type = FunctionAux
variable = Na+_rate
execute_on = timestep_begin
function = 'if(t<=0, 0, 0.48019999999999996)'
[]
[O2aq_rate]
type = FunctionAux
variable = O2aq_rate
execute_on = timestep_begin
function = 'if(t<=0, 0, 0.000123)'
[]
[SO4--_rate]
type = FunctionAux
variable = SO4--_rate
execute_on = timestep_begin
function = 'if(t<=0, 0, 0.0295)'
[]
[SiO2aq_rate]
type = FunctionAux
variable = SiO2aq_rate
execute_on = timestep_begin
function = 'if(t<=0, 0, 0.00017)'
[]
[Sr++_rate]
type = FunctionAux
variable = Sr++_rate
execute_on = timestep_begin
function = 'if(t<=0, 0, 3.8350000000000004e-05)'
[]
[Zn++_rate]
type = FunctionAux
variable = Zn++_rate
execute_on = timestep_begin
function = 'if(t<=0, 0, 1e-08)'
[]
[]
[Postprocessors]
[temperature]
type = PointValue
point = '0 0 0'
variable = "solution_temperature"
[]
[fugactity_O2]
type = PointValue
point = '0 0 0'
variable = "activity_O2(g)"
[]
[molal_SO4--]
type = PointValue
point = '0 0 0'
variable = "molal_SO4--"
[]
[molal_NaSO4]
type = PointValue
point = '0 0 0'
variable = "molal_NaSO4-"
[]
[molal_H2Saq]
type = PointValue
point = '0 0 0'
variable = "molal_H2S(aq)"
[]
[molal_HSO4-]
type = PointValue
point = '0 0 0'
variable = "molal_HSO4-"
[]
[cm3_Anhydrite]
type = PointValue
point = '0 0 0'
variable = "free_cm3_Anhydrite"
[]
[cm3_Pyrite]
type = PointValue
point = '0 0 0'
variable = "free_cm3_Pyrite"
[]
[cm3_Talc]
type = PointValue
point = '0 0 0'
variable = "free_cm3_Talc"
[]
[cm3_AmSil]
type = PointValue
point = '0 0 0'
variable = "free_cm3_Amrph^silica"
[]
[]
[Functions]
[timestepper]
type = PiecewiseLinear
x = '0 0.1 1 10'
y = '0.01 0.01 0.5 10'
[]
[]
[Executioner]
type = Transient
start_time = -0.01 # to allow initial dump to occur
[TimeStepper]
type = FunctionDT
function = timestepper
[]
end_time = 10
[]
[UserObjects]
[definition]
type = GeochemicalModelDefinition
database_file = "../../../database/moose_geochemdb.json"
basis_species = "H2O H+ Cl- Na+ Mg++ SO4-- Ca++ K+ HCO3- Ba++ SiO2(aq) Sr++ Zn++ Cu+ Al+++ Fe++ Mn++ O2(aq)"
equilibrium_minerals = "Anhydrite Pyrite Talc Amrph^silica Barite Dolomite-ord Muscovite Nontronit-Na Pyrolusite Strontianite"
equilibrium_gases = "O2(g)"
[]
[]
[Outputs]
csv = true
[]
(modules/tensor_mechanics/test/tests/1D_axisymmetric/axisymm_gps_incremental.i)
# this test checks the asixymmetric 1D generalized plane strain formulation using incremental small strains
[GlobalParams]
displacements = disp_x
scalar_out_of_plane_strain = scalar_strain_yy
[]
[Problem]
coord_type = RZ
[]
[Mesh]
file = line.e
[]
[Variables]
[./disp_x]
[../]
[./scalar_strain_yy]
order = FIRST
family = SCALAR
[../]
[]
[AuxVariables]
[./strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./temp]
initial_condition = 580.0
[../]
[]
[Functions]
[./temp]
type = PiecewiseLinear
x = '0 1 2'
y = '580 580 680'
[../]
[./disp_x]
type = PiecewiseLinear
x = '0 1'
y = '0 2e-6'
[../]
[]
[Kernels]
[./TensorMechanics]
[../]
[]
[Modules]
[./TensorMechanics]
[./GeneralizedPlaneStrain]
[./gps]
[../]
[../]
[../]
[]
[AuxKernels]
[./strain_xx]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_xx
index_i = 0
index_j = 0
[../]
[./strain_yy]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_yy
index_i = 1
index_j = 1
[../]
[./strain_zz]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_zz
index_i = 2
index_j = 2
[../]
[./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_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./temp]
type = FunctionAux
variable = temp
function = temp
execute_on = 'timestep_begin'
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
boundary = 1
value = 0
variable = disp_x
[../]
[./disp_x]
type = FunctionDirichletBC
boundary = 2
function = disp_x
variable = disp_x
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 3600
poissons_ratio = 0.2
[../]
[./strain]
type = ComputeAxisymmetric1DIncrementalStrain
eigenstrain_names = eigenstrain
scalar_out_of_plane_strain = scalar_strain_yy
[../]
[./thermal_strain]
type = ComputeThermalExpansionEigenstrain
thermal_expansion_coeff = 1e-8
temperature = temp
stress_free_temperature = 580
eigenstrain_name = eigenstrain
[../]
[./stress]
type = ComputeStrainIncrementBasedStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
line_search = 'none'
l_max_its = 50
l_tol = 1e-6
nl_max_its = 15
nl_rel_tol = 1e-8
nl_abs_tol = 1e-10
start_time = 0
end_time = 2
num_steps = 2
[]
[Outputs]
exodus = true
console = true
[]
(modules/richards/test/tests/user_objects/uo3.i)
# Seff User objects give the correct value
# Sat User objects give the correct value
#
# If you want to add another test for another UserObject
# then add the UserObject, add a Function defining the expected result,
# add an AuxVariable and AuxKernel that will record the UserObjects value
# and finally add a NodalL2Error that compares this with the Function
#
# Here pressure is x where x runs between -5E6 and 5E6
[UserObjects]
[./Seff1VG]
type = RichardsSeff1VG
m = 0.8
al = 1E-6
[../]
[./Seff1BWsmall]
type = RichardsSeff1BWsmall
Sn = 0.0
Ss = 1.0
C = 1.01
las = 1E5
[../]
[./Seff1RSC]
type = RichardsSeff1RSC
oil_viscosity = 4.0
scale_ratio = 1E6
shift = -2E6
[../]
[./Seff1VGcut]
type = RichardsSeff1VGcut
m = 0.8
al = 1E-6
p_cut = -1E6
[../]
# following are unimportant in this test
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1000
bulk_mod = 2E6
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.10101
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.054321
sum_s_res = 0.054321
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 1E5
[../]
[]
[Functions]
[./initial_pressure]
type = ParsedFunction
value = x
[../]
[./answer_Seff1VG]
type = ParsedFunction
value = (1+max((-x)*al,0)^(1/(1-m)))^(-m)
vars = 'al m'
vals = '1E-6 0.8'
[../]
[./answer_dSeff1VG]
type = GradParsedFunction
direction = '1 0 0'
value = (1+max((-x)*al,0)^(1/(1-m)))^(-m)
vars = 'al m'
vals = '1E-6 0.8'
[../]
[./answer_d2Seff1VG]
type = Grad2ParsedFunction
direction = '1 0 0'
value = (1+max((-x)*al,0)^(1/(1-m)))^(-m)
vars = 'al m'
vals = '1E-6 0.8'
[../]
[./answer_Seff1BW]
type = PiecewiseLinear
format = columns
data_file = satBW.csv
axis = x
[../]
[./answer_Seff1BWprime]
type = PiecewiseLinear
format = columns
data_file = satBWprime.csv
axis = x
[../]
[./answer_Seff1BW2prime]
type = PiecewiseLinear
format = columns
data_file = satBW2prime.csv
axis = x
[../]
[./answer_Seff1RSC]
type = ParsedFunction
value = (1+exp((-x-shift)/scale))^(-0.5)
vars = 'shift scale'
vals = '-2E6 1E6'
[../]
[./answer_dSeff1RSC]
type = GradParsedFunction
direction = '1 0 0'
value = (1+exp((-x-shift)/scale))^(-0.5)
vars = 'shift scale'
vals = '-2E6 1E6'
[../]
[./answer_d2Seff1RSC]
type = Grad2ParsedFunction
direction = '1 0 0'
value = (1+exp((-x-shift)/scale))^(-0.5)
vars = 'shift scale'
vals = '-2E6 1E6'
[../]
[./answer_Seff1VGcut]
type = ParsedFunction
value = if(x<pcut,scut+dscut*(x-pcut),(1+max((-x)*al,0)^(1/(1-m)))^(-m))
vars = 'al m pcut scut dscut'
vals = '1E-6 0.8 -1E6 0.574349177498517 1.14869835499703e-06'
[../]
[./answer_dSeff1VGcut]
type = GradParsedFunction
direction = '1 0 0'
value = if(x<pcut,scut+dscut*(x-pcut),(1+max((-x)*al,0)^(1/(1-m)))^(-m))
vars = 'al m pcut scut dscut'
vals = '1E-6 0.8 -1E6 0.574349177498517 1.14869835499703e-06'
[../]
[./answer_d2Seff1VGcut]
type = Grad2ParsedFunction
direction = '1 0 0'
value = if(x<pcut,scut+dscut*(x-pcut),(1+max((-x)*al,0)^(1/(1-m)))^(-m))
vars = 'al m pcut scut dscut'
vals = '1E-6 0.8 -1E6 0.574349177498517 1.14869835499703e-06'
[../]
[./answer_Sat]
type = ParsedFunction
value = sres+((1-sumsres)*((1+max((-x)*al,0)^(1/(1-m)))^(-m)))
vars = 'al m sres sumsres'
vals = '1E-6 0.8 0.054321 0.054321'
[../]
[./answer_dSat]
type = ParsedFunction
value = 1-sumsres
vars = 'sumsres'
vals = '0.054321'
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[./dSeff1VG_Aux]
[../]
[./d2Seff1VG_Aux]
[../]
[./Seff1BWsmall_Aux]
[../]
[./dSeff1BWsmall_Aux]
[../]
[./d2Seff1BWsmall_Aux]
[../]
[./Seff1RSC_Aux]
[../]
[./dSeff1RSC_Aux]
[../]
[./d2Seff1RSC_Aux]
[../]
[./Seff1VGcut_Aux]
[../]
[./dSeff1VGcut_Aux]
[../]
[./d2Seff1VGcut_Aux]
[../]
[./Sat_Aux]
[../]
[./dSat_Aux]
[../]
[./check_Aux]
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = Seff1VG
pressure_vars = pressure
[../]
[./dSeff1VG_AuxK]
type = RichardsSeffPrimeAux
variable = dSeff1VG_Aux
seff_UO = Seff1VG
pressure_vars = pressure
wrtnum = 0
[../]
[./d2Seff1VG_AuxK]
type = RichardsSeffPrimePrimeAux
variable = d2Seff1VG_Aux
seff_UO = Seff1VG
pressure_vars = pressure
wrtnum1 = 0
wrtnum2 = 0
[../]
[./Seff1BWsmall_AuxK]
type = RichardsSeffAux
variable = Seff1BWsmall_Aux
seff_UO = Seff1BWsmall
pressure_vars = pressure
[../]
[./dSeff1BWsmall_AuxK]
type = RichardsSeffPrimeAux
variable = dSeff1BWsmall_Aux
seff_UO = Seff1BWsmall
pressure_vars = pressure
wrtnum = 0
[../]
[./d2Seff1BWsmall_AuxK]
type = RichardsSeffPrimePrimeAux
variable = d2Seff1BWsmall_Aux
seff_UO = Seff1BWsmall
pressure_vars = pressure
wrtnum1 = 0
wrtnum2 = 0
[../]
[./Seff1RSC_AuxK]
type = RichardsSeffAux
variable = Seff1RSC_Aux
seff_UO = Seff1RSC
pressure_vars = pressure
[../]
[./dSeff1RSC_AuxK]
type = RichardsSeffPrimeAux
variable = dSeff1RSC_Aux
seff_UO = Seff1RSC
pressure_vars = pressure
wrtnum = 0
[../]
[./d2Seff1RSC_AuxK]
type = RichardsSeffPrimePrimeAux
variable = d2Seff1RSC_Aux
seff_UO = Seff1RSC
pressure_vars = pressure
wrtnum1 = 0
wrtnum2 = 0
[../]
[./Seff1VGcut_AuxK]
type = RichardsSeffAux
variable = Seff1VGcut_Aux
seff_UO = Seff1VGcut
pressure_vars = pressure
[../]
[./dSeff1VGcut_AuxK]
type = RichardsSeffPrimeAux
variable = dSeff1VGcut_Aux
seff_UO = Seff1VGcut
pressure_vars = pressure
wrtnum = 0
[../]
[./d2Seff1VGcut_AuxK]
type = RichardsSeffPrimePrimeAux
variable = d2Seff1VGcut_Aux
seff_UO = Seff1VGcut
pressure_vars = pressure
wrtnum1 = 0
wrtnum2 = 0
[../]
[./Sat_AuxK]
type = RichardsSatAux
sat_UO = Saturation
seff_var = Seff1VG_Aux
variable = Sat_Aux
[../]
[./dSat_AuxK]
type = RichardsSatPrimeAux
sat_UO = Saturation
seff_var = Seff1VG_Aux
variable = dSat_Aux
[../]
[./check_AuxK]
type = FunctionAux
variable = check_Aux
function = answer_Seff1VGcut
[../]
[]
[Postprocessors]
[./cf_Seff1VG]
type = NodalL2Error
function = answer_Seff1VG
variable = Seff1VG_Aux
[../]
[./cf_dSeff1VG]
type = NodalL2Error
function = answer_dSeff1VG
variable = dSeff1VG_Aux
[../]
[./cf_d2Seff1VG]
type = NodalL2Error
function = answer_d2Seff1VG
variable = d2Seff1VG_Aux
[../]
[./cf_Seff1BW]
type = NodalL2Error
function = answer_Seff1BW
variable = Seff1BWsmall_Aux
[../]
[./cf_Seff1BWprime]
type = NodalL2Error
function = answer_Seff1BWprime
variable = dSeff1BWsmall_Aux
[../]
[./cf_Seff1BW2prime]
type = NodalL2Error
function = answer_Seff1BW2prime
variable = d2Seff1BWsmall_Aux
[../]
[./cf_Seff1RSC]
type = NodalL2Error
function = answer_Seff1RSC
variable = Seff1RSC_Aux
[../]
[./cf_dSeff1RSC]
type = NodalL2Error
function = answer_dSeff1RSC
variable = dSeff1RSC_Aux
[../]
[./cf_d2Seff1RSC]
type = NodalL2Error
function = answer_d2Seff1RSC
variable = d2Seff1RSC_Aux
[../]
[./cf_Seff1VGcut]
type = NodalL2Error
function = answer_Seff1VGcut
variable = Seff1VGcut_Aux
[../]
[./cf_dSeff1VGcut]
type = NodalL2Error
function = answer_dSeff1VGcut
variable = dSeff1VGcut_Aux
[../]
[./cf_d2Seff1VGcut]
type = NodalL2Error
function = answer_d2Seff1VGcut
variable = d2Seff1VGcut_Aux
[../]
[./cf_Sat]
type = NodalL2Error
function = answer_Sat
variable = Sat_Aux
[../]
[./cf_dSat]
type = NodalL2Error
function = answer_dSat
variable = dSat_Aux
[../]
[]
#############################################################################
#
# Following is largely unimportant as we are not running an actual similation
#
#############################################################################
[Mesh]
type = GeneratedMesh
dim = 1
nx = 100
xmin = -5E6
xmax = 5E6
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = initial_pressure
[../]
[../]
[]
[Kernels]
active = 'richardsf richardst'
[./richardst]
type = RichardsMassChange
richardsVarNames_UO = PPNames
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
richardsVarNames_UO = PPNames
variable = pressure
[../]
[]
[Materials]
[./unimportant_material]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-20 0 0 0 1E-20 0 0 0 1E-20'
richardsVarNames_UO = PPNames
density_UO = DensityConstBulk
relperm_UO = RelPermPower
sat_UO = Saturation
seff_UO = Seff1VG
SUPG_UO = SUPGstandard
viscosity = 1E-3
gravity = '0 0 -10'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./does_nothing]
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 1E50 1E50 10000'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
num_steps = 1
dt = 1E-100
[]
[Outputs]
execute_on = 'timestep_end'
active = 'csv'
file_base = uo3
[./csv]
type = CSV
[../]
[./exodus]
type = Exodus
hide = pressure
[../]
[]
(modules/tensor_mechanics/test/tests/truss/truss_2d.i)
#
# Truss in two dimensional space
#
# The truss is made of five equilateral triangles supported at each end.
# The truss starts at (0,0). At (1,0), there is a point load of 25.
# The reactions are therefore
# Ryleft = 2/3 * 25 = 16.7
# Ryright = 1/3 * 25 = 8.33
# The area of each member is 0.8.
# Statics gives the stress in each member. For example, for element 6 (from
# (0,0) to (1/2,sqrt(3)/2)), the force is
# f = 2/3 * 25 * 2/sqrt(3) = 100/3/sqrt(3) (compressive)
# and the stress is
# s = -100/3/sqrt(3)/0.8 = -24.06
#
[Mesh]
type = FileMesh
file = truss_2d.e
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./axial_stress]
order = CONSTANT
family = MONOMIAL
[../]
[./e_over_l]
order = CONSTANT
family = MONOMIAL
[../]
[./area]
order = CONSTANT
family = MONOMIAL
# initial_condition = 1.0
[../]
[./react_x]
order = FIRST
family = LAGRANGE
[../]
[./react_y]
order = FIRST
family = LAGRANGE
[../]
[./react_z]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
[./x2]
type = PiecewiseLinear
x = '0 1 2 3'
y = '0 .5 1 1'
[../]
[./y2]
type = PiecewiseLinear
x = '0 1 2 3'
y = '0 0 .5 1'
[../]
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./fixy1]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./fixy4]
type = DirichletBC
variable = disp_y
boundary = 4
value = 0
[../]
[]
[DiracKernels]
[./pull]
type = ConstantPointSource
value = -25
point = '1 0 0'
variable = disp_y
[../]
[]
[AuxKernels]
[./axial_stress]
type = MaterialRealAux
block = 1
property = axial_stress
variable = axial_stress
[../]
[./e_over_l]
type = MaterialRealAux
block = 1
property = e_over_l
variable = e_over_l
[../]
[./area]
type = ConstantAux
block = 1
variable = area
value = 0.8
execute_on = 'initial timestep_begin'
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
petsc_options_iname = '-pc_type -ksp_gmres_restart'
petsc_options_value = 'jacobi 101'
nl_max_its = 15
nl_rel_tol = 1e-8
nl_abs_tol = 1e-10
dt = 1
num_steps = 1
end_time = 1
[]
[Kernels]
[./solid_x]
type = StressDivergenceTensorsTruss
block = 1
displacements = 'disp_x disp_y'
component = 0
variable = disp_x
area = area
save_in = react_x
[../]
[./solid_y]
type = StressDivergenceTensorsTruss
block = 1
displacements = 'disp_x disp_y'
component = 1
variable = disp_y
area = area
save_in = react_y
[../]
[]
[Materials]
[./linelast]
type = LinearElasticTruss
block = 1
youngs_modulus = 1e6
displacements = 'disp_x disp_y'
[../]
[]
[Outputs]
exodus = true
[]
(modules/xfem/test/tests/pressure_bc/edge_3d_pressure.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = false
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 2
ny = 9
nz = 10
xmin = -0.1
xmax = 0.1
ymin = -0.5
ymax = 0.5
zmin = -0.5
zmax = 0.5
elem_type = HEX8
[]
[UserObjects]
[./square_planar_cut_uo]
type = RectangleCutUserObject
cut_data = '-0.2 0.0 -0.5
-0.2 0.0 0.0
0.2 0.0 0.0
0.2 0.0 -0.5'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz'
[../]
[]
[Functions]
[./pressure]
type = PiecewiseLinear
x = '0 2.0 4.0 6.0 8.0'
y = '0 1000 0 1000 0'
[../]
[]
[DiracKernels]
[./p_x]
type = XFEMPressure
variable = disp_x
component = 0
function = pressure
[../]
[./p_y]
type = XFEMPressure
variable = disp_y
component = 1
function = pressure
[../]
[./p_z]
type = XFEMPressure
variable = disp_z
component = 2
function = pressure
[../]
[]
[BCs]
[./bottom_x]
type = DirichletBC
boundary = 'bottom top'
variable = disp_x
value = 0.0
[../]
[./bottom_y]
type = DirichletBC
boundary = 'bottom top'
variable = disp_y
value = 0.0
[../]
[./bottom_z]
type = DirichletBC
boundary = 'bottom top'
variable = disp_z
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-12
# time control
start_time = 0.0
dt = 1.0
end_time = 2.0
[]
[Outputs]
file_base = edge_3d_pressure_out
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/combined/test/tests/internal_volume/rspherical.i)
#
# Internal Volume Test
#
# This test is designed to compute the internal volume of a space considering
# an embedded volume inside.
#
# The mesh is composed of two blocks with an interior cavity of volume 3.
# The volume of each of the blocks is also 3. The volume of the entire sphere
# is 9.
#
[GlobalParams]
displacements = 'disp_x'
[]
[Problem]
coord_type = RSPHERICAL
[]
[Mesh]
file = meshes/rspherical.e
construct_side_list_from_node_list = true
[]
[Functions]
[./pressure]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = 1e4
[../]
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
incremental = true
strain = FINITE
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = '1 2 3 4'
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = '1 3'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = '1 3'
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
start_time = 0.0
dt = 1.0
end_time = 1.0
[]
[Postprocessors]
[./internalVolume]
type = InternalVolume
boundary = 10
component = 0
execute_on = 'initial timestep_end'
[../]
[./intVol1]
type = InternalVolume
boundary = 2
component = 0
execute_on = 'initial timestep_end'
[../]
[./intVol1Again]
type = InternalVolume
boundary = 9
component = 0
execute_on = 'initial timestep_end'
[../]
[./intVol2]
type = InternalVolume
boundary = 11
component = 0
execute_on = 'initial timestep_end'
[../]
[./intVolTotal]
type = InternalVolume
boundary = 4
component = 0
execute_on = 'initial timestep_end'
[../]
[]
[Outputs]
exodus = true
csv = true
[]
(modules/tensor_mechanics/test/tests/smeared_cracking/cracking_deprecated.i)
#
# Simple pull test for cracking.
# The stress increases for two steps and then drops to zero.
[Mesh]
file = cracking_test.e
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Functions]
[./displ]
type = PiecewiseLinear
x = '0 1 2 3 4'
y = '0 1 0 -1 0'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx'
[../]
[]
[BCs]
[./pull]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = displ
[../]
[./left]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./bottom]
type = DirichletBC
variable = disp_y
boundary = 2
value = 0.0
[../]
[./back]
type = DirichletBC
variable = disp_z
boundary = 3
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 2.8e7
poissons_ratio = 0
[../]
[./elastic_stress]
type = ComputeSmearedCrackingStress
cracking_stress = 1.68e6
[../]
[]
[Executioner]
type = Transient
petsc_options_iname = '-ksp_gmres_restart -pc_type -sub_pc_type'
petsc_options_value = '101 asm lu'
line_search = 'none'
l_max_its = 100
nl_max_its = 100
nl_rel_tol = 1e-8
nl_abs_tol = 1e-8
l_tol = 1e-5
start_time = 0.0
end_time = 0.1
dt = 0.025
[]
[Outputs]
exodus = true
file_base = cracking_out
[]
(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/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/geomsearch/2d_moving_penetration/pl_test3q.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
file = pl_test3q.e
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate10]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate13]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate14]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate15]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate16]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1.e-10
l_max_its = 10
start_time = 0.0
dt = 0.02
end_time = 1.0
[./Quadrature]
order = THIRD
[../]
[]
[Outputs]
file_base = pl_test3q_out
exodus = true
[]
(test/tests/geomsearch/2d_moving_penetration/pl_test4nns.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
file = pl_test4.e
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
normal_smoothing_method = nodal_normal_based
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate10]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate13]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate14]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate15]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate16]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-10
l_max_its = 10
start_time = 0.0
dt = 0.0125
end_time = 1.0
[]
[Outputs]
file_base = pl_test4nns_out
exodus = true
[]
[NodalNormals]
boundary = 11
corner_boundary = 20
[]
(modules/porous_flow/test/tests/dirackernels/bh07.i)
# Comparison with analytical solution for cylindrically-symmetric situation
[Mesh]
type = FileMesh
file = bh07_input.e
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Functions]
[dts]
type = PiecewiseLinear
y = '1000 10000'
x = '100 1000'
[]
[]
[Variables]
[pp]
initial_condition = 1E7
[]
[]
[Kernels]
[mass0]
type = PorousFlowMassTimeDerivative
fluid_component = 0
variable = pp
[]
[fflux]
type = PorousFlowAdvectiveFlux
fluid_component = 0
variable = pp
gravity = '0 0 0'
[]
[]
[BCs]
[fix_outer]
type = DirichletBC
boundary = perimeter
variable = pp
value = 1E7
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[borehole_total_outflow_mass]
type = PorousFlowSumQuantity
[]
[pc]
type = PorousFlowCapillaryPressureVG
m = 0.8
alpha = 1e-5
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 2e9
viscosity = 1e-3
density0 = 1000
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
[]
[porosity]
type = PorousFlowPorosityConst
porosity = 0.1
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1E-11 0 0 0 1E-11 0 0 0 1E-11'
[]
[relperm]
type = PorousFlowRelativePermeabilityFLAC
m = 2
phase = 0
[]
[]
[DiracKernels]
[bh]
type = PorousFlowPeacemanBorehole
variable = pp
SumQuantityUO = borehole_total_outflow_mass
point_file = bh07.bh
fluid_phase = 0
bottom_p_or_t = 0
unit_weight = '0 0 0'
use_mobility = true
re_constant = 0.1594 # use Chen and Zhang version
character = 2 # double the strength because bh07.bh only fills half the mesh
[]
[]
[Postprocessors]
[bh_report]
type = PorousFlowPlotQuantity
uo = borehole_total_outflow_mass
execute_on = 'initial timestep_end'
[]
[fluid_mass]
type = PorousFlowFluidMass
execute_on = 'initial timestep_end'
[]
[]
[VectorPostprocessors]
[pp]
type = LineValueSampler
variable = pp
start_point = '0 0 0'
end_point = '300 0 0'
sort_by = x
num_points = 300
execute_on = timestep_end
[]
[]
[Preconditioning]
[usual]
type = SMP
full = true
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -ksp_max_it'
petsc_options_value = 'bcgs bjacobi 1E-10 1E-10 10000 30'
[]
[]
[Executioner]
type = Transient
end_time = 1E3
solve_type = NEWTON
[TimeStepper]
# get only marginally better results for smaller time steps
type = FunctionDT
function = dts
[]
[]
[Outputs]
file_base = bh07
[along_line]
type = CSV
execute_on = final
[]
[exodus]
type = Exodus
execute_on = 'initial final'
[]
[]
(modules/richards/test/tests/theis/th21.i)
# two-phase, fully-saturated
# production
[Mesh]
type = FileMesh
file = th01_input.e
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '0.5 1 2 10'
x = '0 1 10 100'
[../]
[]
[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 = 1E-5
[../]
[./SUPGgas]
type = RichardsSUPGstandard
p_SUPG = 1E-5
[../]
[./total_outflow_mass]
type = RichardsSumQuantity
[../]
[]
[Variables]
[./pwater]
order = FIRST
family = LAGRANGE
[../]
[./pgas]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./water_ic]
type = FunctionIC
variable = pwater
function = initial_pressure
[../]
[./gas_ic]
type = FunctionIC
variable = pgas
function = initial_pressure
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[Kernels]
active = 'richardsfwater richardstwater richardsfgas richardstgas'
[./richardstwater]
type = RichardsMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFlux
variable = pwater
[../]
[./richardstgas]
type = RichardsMassChange
variable = pgas
[../]
[./richardsfgas]
type = RichardsFlux
variable = pgas
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = SeffWater
pressure_vars = 'pwater pgas'
[../]
[]
[DiracKernels]
[./bh]
type = RichardsPolyLineSink
pressures = '-1E9 1E9'
fluxes = '200 200'
point_file = th01.points
SumQuantityUO = total_outflow_mass
variable = pwater
[../]
[]
[Postprocessors]
[./flow_report]
type = RichardsPlotQuantity
uo = total_outflow_mass
[../]
[./p50]
type = PointValue
variable = pwater
point = '50 0 0'
execute_on = timestep_end
[../]
[]
[Functions]
[./initial_pressure]
type = ParsedFunction
value = 1E5
[../]
[]
[Materials]
[./all]
type = RichardsMaterial
block = 1
mat_porosity = 0.1
mat_permeability = '1E-10 0 0 0 1E-10 0 0 0 1E-10'
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]
[./usual]
type = SMP
full = true
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -ksp_max_it'
petsc_options_value = 'bcgs bjacobi 1E-6 1E-10 10000 30'
[../]
[]
[Executioner]
type = Transient
end_time = 100
solve_type = NEWTON
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = th21
csv = true
[]
(modules/tensor_mechanics/test/tests/truss/truss_hex.i)
# This test is designed to check
# whether truss element works well with other multi-dimensional element
# e.g. the hex element in this case, by assigning different brock number
# to different types of elements.
[Mesh]
type = FileMesh
file = truss_hex.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./axial_stress]
order = CONSTANT
family = MONOMIAL
[../]
[./e_over_l]
order = CONSTANT
family = MONOMIAL
[../]
[./area]
order = CONSTANT
family = MONOMIAL
# initial_condition = 1.0
[../]
[./react_x]
order = FIRST
family = LAGRANGE
[../]
[./react_y]
order = FIRST
family = LAGRANGE
[../]
[./react_z]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
[./x2]
type = PiecewiseLinear
x = '0 1 2 3'
y = '0 .5 1 1'
[../]
[./y2]
type = PiecewiseLinear
x = '0 1 2 3'
y = '0 0 .5 1'
[../]
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./fixy1]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./fixz1]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0
[../]
[./fixx2]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./fixz2]
type = DirichletBC
variable = disp_z
boundary = 2
value = 0
[../]
[./fixDummyHex_x]
type = DirichletBC
variable = disp_x
boundary = 1000
value = 0
[../]
[./fixDummyHex_y]
type = DirichletBC
variable = disp_y
boundary = 1000
value = 0
[../]
[./fixDummyHex_z]
type = DirichletBC
variable = disp_z
boundary = 1000
value = 0
[../]
[]
[DiracKernels]
[./pull]
type = ConstantPointSource
value = -25
point = '0 -2 0'
variable = disp_y
[../]
[]
[AuxKernels]
[./axial_stress]
type = MaterialRealAux
block = '1 2'
property = axial_stress
variable = axial_stress
[../]
[./e_over_l]
type = MaterialRealAux
block = '1 2'
property = e_over_l
variable = e_over_l
[../]
[./area1]
type = ConstantAux
block = 1
variable = area
value = 1.0
execute_on = 'initial timestep_begin'
[../]
[./area2]
type = ConstantAux
block = 2
variable = area
value = 0.25
execute_on = 'initial timestep_begin'
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
petsc_options_iname = '-pc_type -ksp_gmres_restart'
petsc_options_value = 'jacobi 101'
nl_max_its = 15
nl_rel_tol = 1e-8
nl_abs_tol = 1e-10
dt = 1
num_steps = 1
end_time = 1
[]
[Kernels]
[./truss_x]
type = StressDivergenceTensorsTruss
block = '1 2'
variable = disp_x
displacements = 'disp_x disp_y disp_z'
component = 0
area = area
save_in = react_x
[../]
[./truss_y]
type = StressDivergenceTensorsTruss
block = '1 2'
variable = disp_y
component = 1
displacements = 'disp_x disp_y disp_z'
area = area
save_in = react_y
[../]
[./truss_z]
type = StressDivergenceTensorsTruss
block = '1 2'
variable = disp_z
component = 2
displacements = 'disp_x disp_y disp_z'
area = area
save_in = react_z
[../]
[./TensorMechanics]
block = 1000
displacements = 'disp_x disp_y disp_z'
[../]
# [./hex_x]
# type = StressDivergenceTensors
# block = 1000
# variable = disp_x
# component = 0
# displacements = 'disp_x disp_y disp_z'
# [../]
# [./hex_y]
# type = StressDivergenceTensors
# block = 1000
# variable = disp_y
# component = 1
# displacements = 'disp_x disp_y disp_z'
# [../]
# [./hex_z]
# type = StressDivergenceTensors
# block = 1000
# variable = disp_z
# component = 2
# displacements = 'disp_x disp_y disp_z'
# [../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = 1000
youngs_modulus = 1e6
poissons_ratio = 0
[../]
[./strain]
type = ComputeSmallStrain
block = 1000
displacements = 'disp_x disp_y disp_z'
[../]
[./stress]
type = ComputeLinearElasticStress
block = 1000
[../]
[./linelast]
type = LinearElasticTruss
block = '1 2'
displacements = 'disp_x disp_y disp_z'
youngs_modulus = 1e6
[../]
[]
[Outputs]
exodus = true
[]
(test/tests/functions/function_file_format/function_file_format_test.i)
# This tests the capability of the code to read input files in csv or space separated format.
# There are four variables and four functions of the same name; a,b,c, and d. The diffusion equation is "solved"
# for each of these variables with a boundary condition of type FunctionDirchletBC applied to a boundary
# (i.e. node set) that includes every node in the element, so the solution is the boundary condition defined by the function.
# Each boundary condition uses a function of type PiecewiseLinear that gets its value from a file,
# which could be in comma separated or space separated format. The input file can also contain comments.
#
# The files could have the form
# 0,1,2,3 # time
# 0,4,5,6 # bc value
# for format = row
# or
# 0,0
# 1,4
# 2,5
# 3,6
# for format = column
# Values in files could be separated by white space. See the .csv and .dat files for format examples.
#
# The value of the variables should correspond to the function.
# At time = 0, the variable = 0, at time = 1, variable = 4 and so on.
[Mesh]
file = cube.e
# 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
[]
[Variables]
[./a]
[../]
[./b]
[../]
[./c]
[../]
[./d]
[../]
[./e]
[../]
[./f]
[../]
[]
[Functions]
[./a]
type = PiecewiseLinear
data_file = rows.csv
format = rows
[../]
[./b]
type = PiecewiseLinear
data_file = columns.csv
format = columns
[../]
[./c]
type = PiecewiseLinear
data_file = rows_space.dat
format = rows
[../]
[./d]
type = PiecewiseLinear
data_file = columns_space.dat
format = columns
[../]
[./e_func]
type = PiecewiseLinear
data_file = rows_more_data.csv
format = rows
xy_in_file_only = false
x_index_in_file = 2
y_index_in_file = 0
[../]
[./f]
type = PiecewiseLinear
data_file = columns_more_data.csv
format = columns
xy_in_file_only = false
x_index_in_file = 2
y_index_in_file = 0
[../]
[]
[Kernels]
[./diffa]
type = Diffusion
variable = a
[../]
[./diffb]
type = Diffusion
variable = b
[../]
[./diffc]
type = Diffusion
variable = c
[../]
[./diffd]
type = Diffusion
variable = d
[../]
[./diffe]
type = Diffusion
variable = e
[../]
[./difff]
type = Diffusion
variable = f
[../]
[]
[BCs]
[./a]
type = FunctionDirichletBC
variable = a
boundary = '1'
function = a
[../]
[./b]
type = FunctionDirichletBC
variable = b
boundary = '1'
function = b
[../]
[./c]
type = FunctionDirichletBC
variable = c
boundary = '1'
function = c
[../]
[./d]
type = FunctionDirichletBC
variable = d
boundary = '1'
function = d
[../]
[./e]
type = FunctionDirichletBC
variable = e
boundary = '1'
function = e_func
[../]
[./f]
type = FunctionDirichletBC
variable = f
boundary = '1'
function = f
[../]
[]
[Executioner]
type = Transient
dt = 0.5
end_time = 3
nl_rel_tol = 1e-12
[]
[Outputs]
file_base = out
exodus = true
[]
(modules/richards/test/tests/buckley_leverett/bl20_lumped_fu.i)
# two-phase version
[Mesh]
type = GeneratedMesh
dim = 1
nx = 30
xmin = 0
xmax = 15
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = 'DensityWater DensityGas'
relperm_UO = 'RelPermWater RelPermGas'
SUPG_UO = 'SUPGwater SUPGgas'
sat_UO = 'SatWater SatGas'
seff_UO = 'SeffWater SeffGas'
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '0.1 0.5 0.5 1 2 4'
x = '0 0.1 1 5 40 42'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = 'pwater pgas'
[../]
[./DensityWater]
type = RichardsDensityConstBulk
dens0 = 1000
bulk_mod = 2E6
[../]
[./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 = 2
[../]
[./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 = 1E-5
[../]
[./SUPGgas]
type = RichardsSUPGstandard
p_SUPG = 1E-5
[../]
[]
[Variables]
[./pwater]
order = FIRST
family = LAGRANGE
[../]
[./pgas]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./w_aux_seff]
[../]
[]
[Kernels]
[./richardstwater]
type = RichardsLumpedMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFullyUpwindFlux
variable = pwater
[../]
[./richardstgas]
type = RichardsLumpedMassChange
variable = pgas
[../]
[./richardsfgas]
type = RichardsFullyUpwindFlux
variable = pgas
[../]
[]
[AuxKernels]
[./w_aux_seff_auxk]
type = RichardsSeffAux
seff_UO = SeffWater
pressure_vars = 'pwater pgas'
variable = w_aux_seff
[../]
[]
[ICs]
[./water_ic]
type = FunctionIC
variable = pwater
function = initial_water
[../]
[./gas_ic]
type = FunctionIC
variable = pgas
function = initial_gas
[../]
[]
[BCs]
[./left_w]
type = DirichletBC
variable = pwater
boundary = left
value = 1E6
[../]
[./left_g]
type = DirichletBC
variable = pgas
boundary = left
value = 1000
[../]
[./right_w]
type = DirichletBC
variable = pwater
boundary = right
value = -300000
[../]
[./right_g]
type = DirichletBC
variable = pgas
boundary = right
value = 0
[../]
[]
[Functions]
[./initial_water]
type = ParsedFunction
value = 1000000*(1-min(x/5,1))-if(x<5,0,300000)
[../]
[./initial_gas]
type = ParsedFunction
value = 1000
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.15
mat_permeability = '1E-10 0 0 0 1E-10 0 0 0 1E-10'
viscosity = '1E-3 1E-6'
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
active = 'standard'
[./bounded]
# must use --use-petsc-dm command line argument
type = SMP
full = true
petsc_options_iname = '-snes_type -pc_factor_shift_type'
petsc_options_value = 'vinewtonssls nonzero'
[../]
[./standard]
type = SMP
full = true
petsc_options_iname = '-pc_factor_shift_type'
petsc_options_value = 'nonzero'
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
end_time = 50
nl_rel_tol = 1.e-9
nl_max_its = 10
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = bl20_lumped_fu
execute_on = 'initial timestep_end final'
interval = 100000
exodus = true
hide = pgas
[./console_out]
type = Console
interval = 1
[../]
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_htonly/cyl3D.i)
#
# 3D Cylindrical Gap Heat Transfer Test.
#
# This test exercises 3D gap heat transfer for a constant conductivity gap.
#
# The mesh consists of an inner solid cylinder of radius = 1 unit, and outer
# hollow cylinder with an inner radius of 2. In other words, the gap between
# them is 1 radial unit in length.
#
# The conductivity of both cylinders is set very large to achieve a uniform
# temperature in each cylinder. The temperature of the center node of the
# inner cylinder is ramped from 100 to 200 over one time unit. The temperature
# of the outside of the outer, hollow cylinder is held fixed at 100.
#
# A simple analytical solution is possible for the integrated heat flux
# between the inner and outer cylinders:
#
# Integrated Flux = (T_left - T_right) * (gapK/(r*ln(r2/r1))) * Area
#
# For gapK = 1 (default value)
#
# The area is taken as the area of the secondary (inner) surface:
#
# Area = 2 * pi * h * r, where h is the height of the cylinder.
#
# The integrated heat flux across the gap at time 1 is then:
#
# 2*pi*h*k*delta_T/(ln(r2/r1))
# 2*pi*1*1*100/(ln(2/1)) = 906.5 watts
#
# For comparison, see results from the integrated flux post processors.
# This simulation makes use of symmetry, so only 1/4 of the cylinders is meshed
# As such, the integrated flux from the post processors is 1/4 of the total,
# or 226.6 watts.
# The value coming from the post processor is slightly less than this
# but converges as mesh refinement increases.
#
# Simulating contact is challenging. Regression tests that exercise
# contact features can be difficult to solve consistently across multiple
# platforms. While designing these tests, we felt it worth while to note
# some aspects of these tests. The following applies to:
# sphere3D.i, sphere2DRZ.i, cyl2D.i, and cyl3D.i.
# 1. We decided that to perform consistently across multiple platforms we
# would use very small convergence tolerance. In this test we chose an
# nl_rel_tol of 1e-12.
# 2. Due to such a high value for thermal conductivity (used here so that the
# domains come to a uniform temperature) the integrated flux at time = 0
# was relatively large (the value coming from SideIntegralFlux =
# -_diffusion_coef[_qp]*_grad_u[_qp]*_normals[_qp] where the diffusion coefficient
# here is thermal conductivity).
# Even though _grad_u[_qp] is small, in this case the diffusion coefficient
# is large. The result is a number that isn't exactly zero and tends to
# fail exodiff. For this reason the parameter execute_on = initial should not
# be used. That parameter is left to default settings in these regression tests.
#
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
file = cyl3D.e
[]
[Functions]
[./temp]
type = PiecewiseLinear
x = '0 1'
y = '100 200'
[../]
[]
[Variables]
[./temp]
initial_condition = 100
[../]
[]
[AuxVariables]
[./gap_conductance]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./heat_conduction]
type = HeatConduction
variable = temp
[../]
[]
[AuxKernels]
[./gap_cond]
type = MaterialRealAux
property = gap_conductance
variable = gap_conductance
boundary = 2
[../]
[]
[Materials]
[./heat1]
type = HeatConductionMaterial
block = '1 2'
specific_heat = 1.0
thermal_conductivity = 1000000.0
[../]
[]
[ThermalContact]
[./thermal_contact]
type = GapHeatTransfer
variable = temp
primary = 3
secondary = 2
emissivity_primary = 0
emissivity_secondary = 0
gap_conductivity = 1
quadrature = true
gap_geometry_type = CYLINDER
cylinder_axis_point_1 = '0 0 0'
cylinder_axis_point_2 = '0 1 0'
[../]
[]
[BCs]
[./mid]
type = FunctionDirichletBC
boundary = 5
variable = temp
function = temp
[../]
[./temp_far_right]
type = DirichletBC
boundary = 4
variable = temp
value = 100
[../]
[]
[Executioner]
type = Transient
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
dt = 1
dtmin = 0.01
end_time = 1
nl_rel_tol = 1e-12
nl_abs_tol = 1e-7
[./Quadrature]
order = fifth
side_order = seventh
[../]
[]
[Outputs]
exodus = true
[./Console]
type = Console
[../]
[]
[Postprocessors]
[./temp_left]
type = SideAverageValue
boundary = 2
variable = temp
[../]
[./temp_right]
type = SideAverageValue
boundary = 3
variable = temp
[../]
[./flux_left]
type = SideFluxIntegral
variable = temp
boundary = 2
diffusivity = thermal_conductivity
[../]
[./flux_right]
type = SideFluxIntegral
variable = temp
boundary = 3
diffusivity = thermal_conductivity
[../]
[]
(modules/contact/test/tests/nodal_area/nodal_area_Hex20_3.i)
[Mesh]
file = nodal_area_Hex20.e
[]
[GlobalParams]
order = SECOND
displacements = 'displ_x displ_y displ_z'
[]
[Functions]
[./disp]
type = PiecewiseLinear
x = '0 1'
y = '0 20e-6'
[../]
[]
[Variables]
[./displ_x]
[../]
[./displ_y]
[../]
[./displ_z]
[../]
[]
[AuxVariables]
[./react_x]
[../]
[./react_y]
[../]
[./react_z]
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
incremental = true
save_in = 'react_x react_y react_z'
add_variables = true
strain = FINITE
generate_output = 'stress_xx'
[../]
[]
[BCs]
[./move_right]
type = FunctionDirichletBC
boundary = '1'
variable = displ_x
function = disp
[../]
[./fixed_x]
type = DirichletBC
boundary = '3 4'
variable = displ_x
value = 0
[../]
[./fixed_y]
type = DirichletBC
boundary = 10
variable = displ_y
value = 0
[../]
[./fixed_z]
type = DirichletBC
boundary = 11
variable = displ_z
value = 0
[../]
[]
[Contact]
[./dummy_name]
primary = 3
secondary = 2
formulation = penalty
penalty = 1e9
tangential_tolerance = 1e-5
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = '1 2'
youngs_modulus = 1e6
poissons_ratio = 0.0
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 4'
line_search = 'none'
nl_rel_tol = 1e-7
l_tol = 1e-4
l_max_its = 40
nl_max_its = 10
start_time = 0.0
dt = 1.0
dtmin = 1.0
end_time = 1.0
[./Quadrature]
order = THIRD
[../]
[]
[Postprocessors]
[./react_x]
type = NodalSum
variable = react_x
boundary = 1
[../]
[./total_area]
type = NodalSum
variable = nodal_area_dummy_name
boundary = 2
[../]
[]
[Outputs]
exodus = true
[]
(modules/richards/test/tests/dirac/bh_fu_08.i)
#fullyupwind
[Mesh]
type = FileMesh
file = bh07_input.e
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = DensityConstBulk
relperm_UO = RelPermPower
sat_UO = Saturation
seff_UO = Seff1VG
SUPG_UO = SUPGstandard
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1000 10000'
x = '100 1000'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1000
bulk_mod = 2E9
[../]
[./Seff1VG]
type = RichardsSeff1VG
m = 0.8
al = 1E-5
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0
sum_s_res = 0
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 1E8
[../]
[./borehole_total_outflow_mass]
type = RichardsSumQuantity
[../]
[]
[Variables]
active = 'pressure'
[./pressure]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./p_ic]
type = FunctionIC
variable = pressure
function = initial_pressure
[../]
[]
[BCs]
[./fix_outer]
type = DirichletBC
boundary = perimeter
variable = pressure
value = 1E7
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[Kernels]
active = 'richardsf richardst'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFullyUpwindFlux
variable = pressure
[../]
[]
[DiracKernels]
[./bh]
type = RichardsBorehole
bottom_pressure = 0
point_file = bh08.bh
borehole_length = 1
borehole_direction = '0 0 1'
SumQuantityUO = borehole_total_outflow_mass
variable = pressure
unit_weight = '0 0 0'
re_constant = 0.1594
character = 2
fully_upwind = true
[../]
[]
[Postprocessors]
[./bh_report]
type = RichardsPlotQuantity
uo = borehole_total_outflow_mass
execute_on = 'initial timestep_end'
[../]
[./fluid_mass]
type = RichardsMass
variable = pressure
execute_on = 'initial timestep_end'
[../]
[]
[Functions]
[./initial_pressure]
type = ParsedFunction
value = 1E7
[../]
[]
[Materials]
[./all]
type = RichardsMaterial
block = 1
viscosity = 1E-3
mat_porosity = 0.1
mat_permeability = '1E-11 0 0 0 1E-11 0 0 0 1E-11'
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = Seff1VG
pressure_vars = pressure
[../]
[]
[Preconditioning]
[./usual]
type = SMP
full = true
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -ksp_max_it'
petsc_options_value = 'bcgs bjacobi 1E-10 1E-10 10000 30'
[../]
[]
[Executioner]
type = Transient
end_time = 1000
solve_type = NEWTON
[./TimeStepper]
# get only marginally better results for smaller time steps
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = bh_fu_08
execute_on = 'initial timestep_end final'
interval = 10000
exodus = true
[]
(test/tests/geomsearch/2d_moving_penetration/pl_test4tt.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
file = pl_test4.e
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
tangential_tolerance = 0.1
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
tangential_tolerance = 0.1
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate10]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate13]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate14]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate15]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate16]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-10
l_max_its = 10
start_time = 0.0
dt = 0.0125
end_time = 1.0
[]
[Outputs]
file_base = pl_test4tt_out
exodus = true
[]
(modules/xfem/test/tests/diffusion_xfem/diffusion.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 6
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 0.5'
time_start_cut = 0.0
time_end_cut = 0.0
[../]
[]
[Variables]
[./u]
[../]
[]
[Functions]
[./u_left]
type = PiecewiseLinear
x = '0 2'
y = '0 0.1'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = FunctionDirichletBC
variable = u
boundary = 3
function = u_left
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Transient
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
start_time = 0.0
dt = 1.0
end_time = 2.0
[]
[Outputs]
interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/tensor_mechanics/test/tests/beam/static/euler_finite_rot_y.i)
# Large strain/large rotation cantilever beam test
# A 300 N point load is applied at the end of a 4 m long cantilever beam.
# Young's modulus (E) = 1e4
# Shear modulus (G) = 1e8
# shear coefficient (k) = 1.0
# Poisson's ratio (nu) = -0.99995
# Area (A) = 1.0
# Iy = Iz = 0.16
# The dimensionless parameter alpha = kAGL^2/EI = 1e6
# Since the value of alpha is quite high, the beam behaves like
# a thin beam where shear effects are not significant.
# Beam deflection:
# small strain+rot = 3.998 m (exact 4.0)
# large strain + small rotation = -0.05 m in x and 3.74 m in y
# large rotations + small strain = -0.92 m in x and 2.38 m in y
# large rotations + large strain = -0.954 m in x and 2.37 m in y (exact -1.0 m in x and 2.4 m in y)
# References:
# K. E. Bisshopp and D.C. Drucker, Quaterly of Applied Mathematics, Vol 3, No. 3, 1945.
[Mesh]
type = FileMesh
file = beam_finite_rot_test_2.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[./rot_x]
order = FIRST
family = LAGRANGE
[../]
[./rot_y]
order = FIRST
family = LAGRANGE
[../]
[./rot_z]
order = FIRST
family = LAGRANGE
[../]
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./fixy1]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./fixz1]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0.0
[../]
[./fixr1]
type = DirichletBC
variable = rot_x
boundary = 1
value = 0.0
[../]
[./fixr2]
type = DirichletBC
variable = rot_y
boundary = 1
value = 0.0
[../]
[./fixr3]
type = DirichletBC
variable = rot_z
boundary = 1
value = 0.0
[../]
[]
[NodalKernels]
[./force_y2]
type = UserForcingFunctionNodalKernel
variable = disp_y
boundary = 2
function = force
[../]
[]
[Functions]
[./force]
type = PiecewiseLinear
x = '0.0 2.0 8.0'
y = '0.0 300.0 300.0'
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
line_search = 'none'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 4'
nl_max_its = 50
nl_rel_tol = 1e-9
nl_abs_tol = 1e-7
l_max_its = 50
dt = 0.05
end_time = 2.1
[]
[Kernels]
[./solid_disp_x]
type = StressDivergenceBeam
block = '1'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 0
variable = disp_x
[../]
[./solid_disp_y]
type = StressDivergenceBeam
block = '1'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 1
variable = disp_y
[../]
[./solid_disp_z]
type = StressDivergenceBeam
block = '1'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 2
variable = disp_z
[../]
[./solid_rot_x]
type = StressDivergenceBeam
block = '1'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 3
variable = rot_x
[../]
[./solid_rot_y]
type = StressDivergenceBeam
block = '1'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 4
variable = rot_y
[../]
[./solid_rot_z]
type = StressDivergenceBeam
block = '1'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 5
variable = rot_z
[../]
[]
[Materials]
[./elasticity]
type = ComputeElasticityBeam
youngs_modulus = 1e4
poissons_ratio = -0.99995
shear_coefficient = 1.0
block = 1
[../]
[./strain]
type = ComputeFiniteBeamStrain
block = '1'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
area = 1.0
Ay = 0.0
Az = 0.0
Iy = 0.16
Iz = 0.16
y_orientation = '0.0 1.0 0.0'
large_strain = true
[../]
[./stress]
type = ComputeBeamResultants
block = 1
[../]
[]
[Postprocessors]
[./disp_x]
type = PointValue
point = '4.0 0.0 0.0'
variable = disp_x
[../]
[./disp_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = disp_y
[../]
[./rot_z]
type = PointValue
point = '4.0 0.0 0.0'
variable = rot_z
[../]
[]
[Outputs]
exodus = true
perf_graph = true
[]
(modules/xfem/test/tests/second_order_elements/square_branch_tri6_2d.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
volumetric_locking_correction = false
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = TRI6
[]
[UserObjects]
[./line_seg_cut_set_uo]
type = LineSegmentCutSetUserObject
cut_data = '-1.0000e-10 6.6340e-01 6.6340e-01 -1.0000e-10 0.0 1.0
3.3120e-01 3.3200e-01 1.0001e+00 3.3200e-01 1.0 2.0'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
[../]
[]
[Functions]
[./right_disp_x]
type = PiecewiseLinear
x = '0 1.0 2.0 3.0'
y = '0 0.005 0.01 0.01'
[../]
[./top_disp_y]
type = PiecewiseLinear
x = '0 1.0 2.0 3.0'
y = '0 0.005 0.01 0.01'
[../]
[]
[BCs]
[./right_x]
type = FunctionDirichletBC
boundary = 1
variable = disp_x
function = right_disp_x
[../]
[./top_y]
type = FunctionDirichletBC
boundary = 2
variable = disp_y
function = top_disp_y
[../]
[./bottom_y]
type = DirichletBC
boundary = 0
variable = disp_y
value = 0.0
[../]
[./left_x]
type = DirichletBC
boundary = 3
variable = disp_x
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-16
nl_abs_tol = 1e-10
# time control
start_time = 0.0
dt = 1.0
end_time = 2.2
num_steps = 5000
[]
[Outputs]
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/tensor_mechanics/test/tests/recompute_radial_return/affine_plasticity.i)
# Affine Plasticity Test for Transient Stress Eigenvalues with Stationary Eigenvectors
# This test is taken from K. Jamojjala, R. Brannon, A. Sadeghirad, J. Guilkey,
# "Verification tests in solid mechanics," Engineering with Computers, Vol 31.,
# p. 193-213.
# The test involves applying particular strains and expecting particular stresses.
# The material properties are:
# Yield in shear 165 MPa
# Shear modulus 79 GPa
# Poisson's ratio 1/3
# The strains are:
# Time e11 e22 e33
# 0 0 0 0
# 1 -0.003 -0.003 0.006
# 2 -0.0103923 0 0.0103923
# The expected stresses are:
# sigma11:
# -474*t 0 < t <= 0.201
# -95.26 0.201 < t <= 1
# (189.4+0.1704*sqrt(a)-0.003242*a)
# --------------------------------- 1 < t <= 2
# 1+0.00001712*a
# -189.4 t > 2 (paper erroneously gives a positive value)
#
# sigma22:
# -474*t 0 < t <= 0.201
# -95.26 0.201 < t <= 1
# -(76.87+1.443*sqrt(a)-0.001316*a)
# --------------------------------- 1 < t <= 2 (paper gives opposite sign)
# 1+0.00001712*a
# 76.87 t > 2
#
# sigma33:
# 948*t 0 < t <= 0.201
# 190.5 0.201 < t <= 1
# -(112.5-1.272*sqrt(a)-0.001926*a)
# --------------------------------- 1 < t <= 2 (paper has two sign errors here)
# 1+0.00001712*a
# 112.5 t > 2
#
# where a = exp(12.33*t).
#
# Note: If planning to run this case with strain type ComputeFiniteStrain, the
# displacement function must be adjusted. Instead of
# strain = (l - l0)/l0 = (u+l0 - l0)/l0 = u/l0
# with l0=1.0, we would have
# strain = log(l/l0) = log((u+l0)/l0)
# with l0=1.0. So, for strain = -0.003,
# -0.003 = log((u+l0)/l0) ->
# u = exp(-0.003)*l0 - l0 = -0.0029955044966269995.
#
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
block = '0'
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
# This test uses ElementalVariableValue postprocessors on specific
# elements, so element numbering needs to stay unchanged
allow_renumbering = false
[]
[Functions]
[./disp_x]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. -0.003 -0.0103923'
[../]
[./disp_y]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. -0.003 0.'
[../]
[./disp_z]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 0.006 0.0103923'
[../]
[./stress_xx]
type = ParsedFunction
# The paper gives 0.201 as the time at initial yield, but 0.20097635952803425 is the exact value.
# The paper gives -95.26 MPa as the stress at yield, but -95.26279441628823 is the exact value.
# The paper gives 12.33 as the factor in the exponential, but 12.332921390339125 is the exact value.
# 189.409039923814000, 0.170423791206825, -0.003242011311945, 1.711645501845780E-05 - exact values
vars = 'timeAtYield stressAtYield expFac a b c d'
vals = '0.20097635952803425 -95.26279441628823 12.332921390339125 189.409039923814000 0.170423791206825 -0.003242011311945 1.711645501845780E-05'
value = '1e6*
if(t<=timeAtYield, -474*t,
if(t<=1, stressAtYield,
(a+b*sqrt(exp(expFac*t))+c*exp(expFac*t))/(1.0+d*exp(expFac*t))))' # tends to -a
[../]
[./stress_yy]
type = ParsedFunction
# The paper gives 0.201 as the time at initial yield, but 0.20097635952803425 is the exact value.
# the paper gives -95.26 MPa as the stress at yield, but -95.26279441628823 is the exact value.
# The paper gives 12.33 as the factor in the exponential, but 12.332921390339125 is the exact value.
# -76.867432297315000, -1.442488120272900, 0.001315697947301, 1.711645501845780E-05 - exact values
vars = 'timeAtYield stressAtYield expFac a b c d'
vals = '0.20097635952803425 -95.26279441628823 12.332921390339125 -76.867432297315000 -1.442488120272900 0.001315697947301 1.711645501845780E-05'
value = '1e6*
if(t<=timeAtYield, -474*t,
if(t<=1, stressAtYield,
(a+b*sqrt(exp(expFac*t))+c*exp(expFac*t))/(1.0+d*exp(expFac*t))))' # tends to -a
[../]
[./stress_zz]
type = ParsedFunction
# The paper gives 0.201 as the time at initial yield, but 0.20097635952803425 is the exact value.
# the paper gives 190.5 MPa as the stress at yield, but 190.52558883257645 is the exact value.
# The paper gives 12.33 as the factor in the exponential, but 12.332921390339125 is the exact value.
# -112.541607626499000, 1.272064329066080, 0.001926313364644, 1.711645501845780E-05 - exact values
vars = 'timeAtYield stressAtYield expFac a b c d'
vals = '0.20097635952803425 190.52558883257645 12.332921390339125 -112.541607626499000 1.272064329066080 0.001926313364644 1.711645501845780E-05'
value = '1e6*
if(t<=timeAtYield, 948*t,
if(t<=1, stressAtYield,
(a+b*sqrt(exp(expFac*t))+c*exp(expFac*t))/(1.0+d*exp(expFac*t))))' # tends to -a
[../]
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./vonmises]
order = CONSTANT
family = MONOMIAL
[../]
[./plastic_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./plastic_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./plastic_strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./TensorMechanics]
[../]
[]
[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_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = 'timestep_end'
[../]
[./vonmises]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = vonmises
scalar_type = vonmisesStress
execute_on = 'timestep_end'
[../]
[./plastic_strain_xx]
type = RankTwoAux
rank_two_tensor = plastic_strain
variable = plastic_strain_xx
index_i = 0
index_j = 0
execute_on = 'timestep_end'
[../]
[./plastic_strain_yy]
type = RankTwoAux
rank_two_tensor = plastic_strain
variable = plastic_strain_yy
index_i = 1
index_j = 1
execute_on = 'timestep_end'
[../]
[./plastic_strain_zz]
type = RankTwoAux
rank_two_tensor = plastic_strain
variable = plastic_strain_zz
index_i = 2
index_j = 2
execute_on = 'timestep_end'
[../]
[]
[BCs]
[./fixed_x]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./fixed_y]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./fixed_z]
type = DirichletBC
variable = disp_z
boundary = back
value = 0.0
[../]
[./disp_x]
type = FunctionDirichletBC
variable = disp_x
boundary = right
function = disp_x
[../]
[./disp_y]
type = FunctionDirichletBC
variable = disp_y
boundary = top
function = disp_y
[../]
[./disp_z]
type = FunctionDirichletBC
variable = disp_z
boundary = front
function = disp_z
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 210666666666.666667
poissons_ratio = 0.3333333333333333
[../]
[./strain]
type = ComputeIncrementalSmallStrain
[../]
[./isotropic_plasticity]
type = IsotropicPlasticityStressUpdate
yield_stress = 285788383.2488647 # = sqrt(3)*165e6 = sqrt(3) * yield in shear
hardening_constant = 0.0
[../]
[./radial_return_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'isotropic_plasticity'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
nl_abs_tol = 1e-10
l_max_its = 20
start_time = 0.0
dt = 0.01 # use 0.0001 for a nearly exact match
end_time = 2.0
[]
[Postprocessors]
[./analytic_xx]
type = FunctionValuePostprocessor
function = stress_xx
[../]
[./analytic_yy]
type = FunctionValuePostprocessor
function = stress_yy
[../]
[./analytic_zz]
type = FunctionValuePostprocessor
function = stress_zz
[../]
[./stress_xx]
type = ElementalVariableValue
variable = stress_xx
elementid = 0
[../]
[./stress_yy]
type = ElementalVariableValue
variable = stress_yy
elementid = 0
[../]
[./stress_zz]
type = ElementalVariableValue
variable = stress_zz
elementid = 0
[../]
[./stress_xx_l2_error]
type = ElementL2Error
variable = stress_xx
function = stress_xx
[../]
[./stress_yy_l2_error]
type = ElementL2Error
variable = stress_yy
function = stress_yy
[../]
[./stress_zz_l2_error]
type = ElementL2Error
variable = stress_zz
function = stress_zz
[../]
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/central_difference/consistent/1D/1d_consistent_implicit.i)
# Test for Newmark Beta integration for a 1D element
# Consistent mass matrix
[Mesh]
type = GeneratedMesh
xmin = 0
xmax = 10
nx = 5
dim = 1
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./accel_x]
[../]
[./vel_x]
[../]
[]
[AuxKernels]
[./accel_x]
type = TestNewmarkTI
variable = accel_x
displacement = disp_x
first = false
[../]
[./vel_x]
type = TestNewmarkTI
variable = vel_x
displacement = disp_x
[../]
[]
[Kernels]
[./DynamicTensorMechanics]
displacements = 'disp_x'
[../]
[./inertia_x]
type = InertialForce
variable = disp_x
[../]
[]
[NodalKernels]
[./force_x]
type = UserForcingFunctionNodalKernel
variable = disp_x
boundary = right
function = force_x
[../]
[]
[Functions]
[./force_x]
type = PiecewiseLinear
x = '0.0 1.0 2.0 3.0 4.0' # time
y = '0.0 1.0 0.0 -1.0 0.0' # force
scale_factor = 1e3
[../]
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor_block]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.25
block = 0
[../]
[./strain_block]
type = ComputeIncrementalSmallStrain
block = 0
displacements = 'disp_x'
[../]
[./stress_block]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = density
prop_values = 2500
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
nl_rel_tol = 1e-8
nl_abs_tol = 1e-8
dtmin = 1e-4
timestep_tolerance = 1e-6
start_time = -0.005
end_time = 0.1
dt = 0.005
[./TimeIntegrator]
type = NewmarkBeta
beta = 0.25
gamma = 0.5
[../]
[]
[Postprocessors]
[./disp_x]
type = NodalVariableValue
nodeid = 1
variable = disp_x
[../]
[./vel_x]
type = NodalVariableValue
nodeid = 1
variable = vel_x
[../]
[./accel_x]
type = NodalVariableValue
nodeid = 1
variable = accel_x
[../]
[]
[Outputs]
exodus = false
csv = true
perf_graph = false
[]
(modules/tensor_mechanics/test/tests/t_stress/t_stress_crack_infinite_plate_2d.i)
# T-stress test for a through crack in a wide ("infinite") plate.
# For a finer mesh this problem converges to the solution T = -sigma.
# Ref: T.L. Anderson, Fracture Mechanics: Fundamentals and Applications
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[Mesh]
file = crack_infinite_plate.e
displacements = 'disp_x disp_y'
partitioner = centroid
centroid_partitioner_direction = z
[]
[AuxVariables]
[./SED]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./rampConstantUp]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = -100
[../]
[]
[DomainIntegral]
integrals = 'JIntegral InteractionIntegralKI InteractionIntegralT'
boundary = 1001
crack_direction_method = CrackDirectionVector
crack_direction_vector = '1 0 0'
radius_inner = '0.06 0.08 0.10'
radius_outer = '0.08 0.10 0.12'
block = 1
youngs_modulus = 30e+6
poissons_ratio = 0.3
2d = true
axis_2d = 2
symmetry_plane = 1
incremental = true
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
planar_formulation = PLANE_STRAIN
[../]
[]
[AuxKernels]
[./SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 300
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = 100
value = 0.0
[../]
[./Pressure]
[./top]
boundary = 200
function = rampConstantUp
[../]
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 30e+6
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
# petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 4'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_abs_tol = 3e-7
nl_rel_tol = 1e-12
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Outputs]
file_base = t_stress_crack_infinite_plate_out
exodus = true
csv = true
[]
(modules/peridynamics/test/tests/simple_tests/2D_regularD_constH_BPD.i)
# Test for bond-based peridynamic formulation
# for regular grid from generated mesh with const bond constants
# Square plate with Dirichlet boundary conditions applied
# at the left, top and bottom edges
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
type = PeridynamicsMesh
horizon_number = 3
[./gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 4
ny = 4
[../]
[./gpd]
type = MeshGeneratorPD
input = gmg
retain_fe_mesh = false
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[BCs]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = 1003
value = 0.0
[../]
[./top_y]
type = DirichletBC
variable = disp_y
boundary = 1002
value = 0.0
[../]
[./bottom_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 1000
function = '-0.001*t'
[../]
[]
[Modules/Peridynamics/Mechanics/Master]
[./all]
formulation = BOND
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 2e5
poissons_ratio = 0.33
[../]
[./force_density]
type = ComputeSmallStrainConstantHorizonMaterialBPD
[../]
[]
[Functions]
[./disp_x_anal]
type = PiecewiseLinear
axis = x
x = '0 1'
y = '0 -0.00033'
[../]
[./disp_y_anal]
type = PiecewiseLinear
axis = y
x = '0 1'
y = '-0.001 0'
[../]
[]
[Postprocessors]
[./anal_disp_L2]
type = NodalFunctionsL2NormPD
functions = 'disp_x_anal disp_y_anal'
[../]
[./disp_diff_L2]
type = NodalDisplacementDifferenceL2NormPD
analytic_functions = 'disp_x_anal disp_y_anal'
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
line_search = none
start_time = 0
end_time = 1
[]
[Outputs]
file_base = 2D_regularD_constH_BPD
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/tensor_mechanics/test/tests/1D_axisymmetric/axisymm_plane_strain_incremental.i)
#
# This test checks elastic stress calculations with mechanical and thermal
# strain using incremental small strain formulation. Young's modulus is 3600, and Poisson's ratio is 0.2.
# The axisymmetric, plane strain 1D mesh is pulled with 1e-6 strain. Thus,
# the strain is [1e-6, 0, 1e-6] (xx, yy, zz). This gives stress of
# [5e-3, 2e-3, 5e-3]. After a temperature increase of 100 with alpha of
# 1e-8, the stress becomes [-1e-3, -4e-3, -1e-3].
#
[GlobalParams]
displacements = disp_x
[]
[Problem]
coord_type = RZ
[]
[Mesh]
file = line.e
[]
[Variables]
[./disp_x]
[../]
[]
[AuxVariables]
[./temp]
initial_condition = 580.0
[../]
[]
[Functions]
[./temp]
type = PiecewiseLinear
x = '0 1 2'
y = '580 580 680'
[../]
[./disp_x]
type = PiecewiseLinear
x = '0 1'
y = '0 2e-6'
[../]
[]
[Modules]
[./TensorMechanics]
[./Master]
[./ps]
planar_formulation = PLANE_STRAIN
strain = SMALL
incremental = true
generate_output = 'strain_xx strain_zz stress_xx stress_yy stress_zz'
eigenstrain_names = eigenstrain
[../]
[../]
[../]
[]
[AuxKernels]
[./temp]
type = FunctionAux
variable = temp
function = temp
execute_on = 'timestep_begin'
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
boundary = 1
value = 0
variable = disp_x
[../]
[./disp_x]
type = FunctionDirichletBC
boundary = 2
function = disp_x
variable = disp_x
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 3600
poissons_ratio = 0.2
[../]
[./thermal_strain]
type = ComputeThermalExpansionEigenstrain
thermal_expansion_coeff = 1e-8
temperature = temp
stress_free_temperature = 580
eigenstrain_name = eigenstrain
[../]
[./stress]
type = ComputeStrainIncrementBasedStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
line_search = 'none'
l_max_its = 50
l_tol = 1e-6
nl_max_its = 15
nl_rel_tol = 1e-8
nl_abs_tol = 1e-10
start_time = 0
end_time = 2
num_steps = 2
[]
[Outputs]
exodus = true
console = true
[]
(modules/combined/test/tests/thermal_strain/thermal_strain.i)
# Patch Test
# This test is designed to compute displacements from a thermal strain.
# The cube is displaced by 1e-6 units in x, 2e-6 in y, and 3e-6 in z.
# The faces are sheared as well (1e-6, 2e-6, and 3e-6 for xy, yz, and
# zx). This gives a uniform strain/stress state for all six unique
# tensor components.
# The temperature moves 100 degrees, and the coefficient of thermal
# expansion is 1e-6. Therefore, the strain (and the displacement
# since this is a unit cube) is 1e-4.
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
file = thermal_strain_test.e
[]
[Functions]
[./tempFunc]
type = PiecewiseLinear
x = '0. 1.'
y = '117.56 217.56'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[./temp]
initial_condition = 117.56
[../]
[]
[Modules/TensorMechanics/Master]
add_variables = true
strain = SMALL
incremental = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx'
[./block1]
eigenstrain_names = eigenstrain1
block = 1
[../]
[./block2]
eigenstrain_names = eigenstrain2
block = 2
[../]
[./block3]
eigenstrain_names = eigenstrain3
block = 3
[../]
[./block4]
eigenstrain_names = eigenstrain4
block = 4
[../]
[./block5]
eigenstrain_names = eigenstrain5
block = 5
[../]
[./block6]
eigenstrain_names = eigenstrain6
block = 6
[../]
[./block7]
eigenstrain_names = eigenstrain7
block = 7
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 10
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = 9
value = 0.0
[../]
[./no_z]
type = DirichletBC
variable = disp_z
boundary = 14
value = 0
[../]
[./temp]
type = FunctionDirichletBC
variable = temp
boundary = '10 12'
function = tempFunc
[../]
[]
[Materials]
[./elasticity_tensor1]
type = ComputeIsotropicElasticityTensor
block = 1
bulk_modulus = 0.333333333333e6
poissons_ratio = 0.0
[../]
[./thermal_strain1]
type = ComputeThermalExpansionEigenstrain
block = 1
temperature = temp
stress_free_temperature = 117.56
thermal_expansion_coeff = 1e-6
eigenstrain_name = eigenstrain1
[../]
[./stress1]
type = ComputeStrainIncrementBasedStress
block = 1
[../]
[./elasticity_tensor2]
type = ComputeIsotropicElasticityTensor
block = 2
bulk_modulus = 0.333333333333e6
lambda = 0.0
[../]
[./thermal_strain2]
type = ComputeThermalExpansionEigenstrain
block = 2
temperature = temp
stress_free_temperature = 117.56
thermal_expansion_coeff = 1e-6
eigenstrain_name = eigenstrain2
[../]
[./stress2]
type = ComputeStrainIncrementBasedStress
block = 2
[../]
[./elasticity_tensor3]
type = ComputeIsotropicElasticityTensor
block = 3
youngs_modulus = 1e6
poissons_ratio = 0.0
[../]
[./thermal_strain3]
type = ComputeThermalExpansionEigenstrain
block = 3
temperature = temp
stress_free_temperature = 117.56
thermal_expansion_coeff = 1e-6
eigenstrain_name = eigenstrain3
[../]
[./stress3]
type = ComputeStrainIncrementBasedStress
block = 3
[../]
[./elasticity_tensor4]
type = ComputeIsotropicElasticityTensor
block = 4
youngs_modulus = 1e6
poissons_ratio = 0.0
[../]
[./thermal_strain4]
type = ComputeThermalExpansionEigenstrain
block = 4
temperature = temp
stress_free_temperature = 117.56
thermal_expansion_coeff = 1e-6
eigenstrain_name = eigenstrain4
[../]
[./stress4]
type = ComputeStrainIncrementBasedStress
block = 4
[../]
[./elasticity_tensor5]
type = ComputeIsotropicElasticityTensor
block = 5
youngs_modulus = 1e6
lambda = 0.0
[../]
[./thermal_strain5]
type = ComputeThermalExpansionEigenstrain
block = 5
temperature = temp
stress_free_temperature = 117.56
thermal_expansion_coeff = 1e-6
eigenstrain_name = eigenstrain5
[../]
[./stress5]
type = ComputeStrainIncrementBasedStress
block = 5
[../]
[./elasticity_tensor6]
type = ComputeIsotropicElasticityTensor
block = 6
youngs_modulus = 1e6
shear_modulus = 5e5
[../]
[./thermal_strain6]
type = ComputeThermalExpansionEigenstrain
block = 6
temperature = temp
stress_free_temperature = 117.56
thermal_expansion_coeff = 1e-6
eigenstrain_name = eigenstrain6
[../]
[./stress6]
type = ComputeStrainIncrementBasedStress
block = 6
[../]
[./elasticity_tensor7]
type = ComputeIsotropicElasticityTensor
block = 7
shear_modulus = 5e5
poissons_ratio = 0.0
[../]
[./thermal_strain7]
type = ComputeThermalExpansionEigenstrain
block = 7
temperature = temp
stress_free_temperature = 117.56
thermal_expansion_coeff = 1e-6
eigenstrain_name = eigenstrain7
[../]
[./stress7]
type = ComputeStrainIncrementBasedStress
block = 7
[../]
[./heat]
type = HeatConductionMaterial
block = '1 2 3 4 5 6 7'
specific_heat = 1.0
thermal_conductivity = 1.0
[../]
[./density]
type = Density
block = '1 2 3 4 5 6 7'
density = 1.0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
nl_abs_tol = 1e-10
l_max_its = 20
start_time = 0.0
dt = 0.5
num_steps = 2
end_time = 1.0
[]
[Outputs]
exodus = true
[]
(modules/combined/test/tests/adaptive_timestepping/adapt_tstep_function_force_step.i)
# This is a test designed to evaluate the cabability of the
# IterationAdaptiveDT TimeStepper to adjust time step size according to
# a function. For example, if the power input function for a BISON
# simulation rapidly increases or decreases, the IterationAdaptiveDT
# TimeStepper should take time steps small enough to capture the
# oscillation.
[GlobalParams]
order = FIRST
family = LAGRANGE
block = 1
volumetric_locking_correction = true
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
file = 1hex8_10mm_cube.e
[]
[Functions]
[./Fiss_Function]
type = PiecewiseLinear
data_file = blip.csv
format = columns
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[./temp]
initial_condition = 300.0
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
incremental = true
eigenstrain_names = thermal_expansion
add_variables = true
generate_output = 'vonmises_stress'
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[./heat_ie]
type = HeatConductionTimeDerivative
variable = temp
[../]
[./heat_source]
type = HeatSource
variable = temp
value = 1.0
function = Fiss_Function
[../]
[]
[BCs]
[./bottom_temp]
type = DirichletBC
variable = temp
boundary = 1
value = 300
[../]
[./top_bottom_disp_x]
type = DirichletBC
variable = disp_x
boundary = '1'
value = 0
[../]
[./top_bottom_disp_y]
type = DirichletBC
variable = disp_y
boundary = '1'
value = 0
[../]
[./top_bottom_disp_z]
type = DirichletBC
variable = disp_z
boundary = '1'
value = 0
[../]
[]
[Materials]
[./thermal]
type = HeatConductionMaterial
temp = temp
specific_heat = 1.0
thermal_conductivity = 1.0
[../]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 300e6
poissons_ratio = .3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[./thermal_expansion]
type = ComputeThermalExpansionEigenstrain
thermal_expansion_coeff = 5e-6
stress_free_temperature = 300.0
temperature = temp
eigenstrain_name = thermal_expansion
[../]
[./density]
type = Density
density = 10963.0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
verbose = true
nl_abs_tol = 1e-10
start_time = 0.0
num_steps = 50000
end_time = 5.1e3
[./TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_function = Fiss_Function
max_function_change = 3e20
force_step_every_function_point = true
dt = 1e2
[../]
[]
[Postprocessors]
[./Temperature_of_Block]
type = ElementAverageValue
variable = temp
execute_on = 'initial timestep_end'
[../]
[./vonMises]
type = ElementAverageValue
variable = vonmises_stress
execute_on = 'initial timestep_end'
[../]
[]
[Outputs]
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 10
[../]
[]
(modules/tensor_mechanics/test/tests/central_difference/lumped/3D/3d_lumped_explicit.i)
# Test for the central difference time integrator in 3D.
[Mesh]
[./generated_mesh]
type = GeneratedMeshGenerator
dim = 3
nx = 1
ny = 1
nz = 2
xmin = 0.0
xmax = 1
ymin = 0.0
ymax = 1
zmin = 0.0
zmax = 2
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./vel_x]
[../]
[./accel_x]
[../]
[./vel_y]
[../]
[./accel_y]
[../]
[./vel_z]
[../]
[./accel_z]
[../]
[]
[AuxKernels]
[./accel_x]
type = TestNewmarkTI
variable = accel_x
displacement = disp_x
first = false
[../]
[./vel_x]
type = TestNewmarkTI
variable = vel_x
displacement = disp_x
[../]
[./accel_y]
type = TestNewmarkTI
variable = accel_y
displacement = disp_y
first = false
[../]
[./vel_y]
type = TestNewmarkTI
variable = vel_y
displacement = disp_x
[../]
[./accel_z]
type = TestNewmarkTI
variable = accel_z
displacement = disp_z
first = false
[../]
[./vel_z]
type = TestNewmarkTI
variable = vel_z
displacement = disp_z
[../]
[]
[Kernels]
[./DynamicTensorMechanics]
displacements = 'disp_x disp_y disp_z'
[../]
[./inertia_x]
type = InertialForce
variable = disp_x
[../]
[./inertia_y]
type = InertialForce
variable = disp_y
[../]
[./inertia_z]
type = InertialForce
variable = disp_z
[../]
[]
[BCs]
[./x_bot]
type = FunctionDirichletBC
variable = disp_x
boundary = 'back'
function = dispx
preset = false
[../]
[./y_bot]
type = FunctionDirichletBC
variable = disp_y
boundary = 'back'
function = dispy
preset = false
[../]
[./z_bot]
type = FunctionDirichletBC
variable = disp_z
boundary = 'back'
function = dispz
preset = false
[../]
[]
[Functions]
[./dispx]
type = PiecewiseLinear
x = '0.0 1.0 2.0 3.0 4.0' # time
y = '0.0 1.0 0.0 -1.0 0.0' # displacement
[../]
[./dispy]
type = ParsedFunction
value = 0.1*t*t*sin(10*t)
[../]
[./dispz]
type = ParsedFunction
value = 0.1*t*t*sin(20*t)
[../]
[]
[Materials]
[./elasticity_tensor_block]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.25
block = 0
[../]
[./strain_block]
type = ComputeIncrementalSmallStrain
block = 0
displacements = 'disp_x disp_y disp_z'
implicit = false
[../]
[./stress_block]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = density
prop_values = 1e4
[../]
[]
[Executioner]
type = Transient
start_time = -0.01
end_time = 0.1
dt = 0.005
timestep_tolerance = 1e-6
[./TimeIntegrator]
type = CentralDifference
solve_type = lumped
[../]
[]
[Postprocessors]
[./accel_10x]
type = NodalVariableValue
nodeid = 10
variable = accel_x
[../]
[]
[Outputs]
exodus = false
csv = true
[]
(modules/peridynamics/test/tests/generalized_plane_strain/planestrain_prescribed_OSPD.i)
[GlobalParams]
displacements = 'disp_x disp_y'
scalar_out_of_plane_strain = scalar_strain_zz
[]
[Mesh]
type = PeridynamicsMesh
horizon_number = 3
[./gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 4
ny = 4
[../]
[./gpd]
type = MeshGeneratorPD
input = gmg
retain_fe_mesh = false
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./temp]
[../]
[./scalar_strain_zz]
order = FIRST
family = SCALAR
[../]
[./strain_zz]
[../]
[]
[Modules/Peridynamics/Mechanics/Master]
[./all]
formulation = ORDINARY_STATE
[../]
[]
[AuxKernels]
[./tempfuncaux]
type = FunctionAux
variable = temp
function = tempfunc
use_displaced_mesh = false
[../]
[./strain_zz]
type = NodalRankTwoPD
variable = strain_zz
rank_two_tensor = total_strain
output_type = component
index_i = 2
index_j = 2
[../]
[]
[AuxScalarKernels]
[./scalar_strain_zz]
type = FunctionScalarAux
variable = scalar_strain_zz
function = scalar_strain_zz_func
[../]
[]
[Functions]
[./tempfunc]
type = ParsedFunction
value = '(1 - x) * t'
[../]
[./scalar_strain_zz_func]
type = PiecewiseLinear
xy_data = '0 0
1 7.901e-5
2 1.103021e-2'
[../]
[]
[BCs]
[./bottom_x]
type = DirichletBC
boundary = 1000
variable = disp_x
value = 0.0
[../]
[./bottom_y]
type = DirichletBC
boundary = 1000
variable = disp_y
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
poissons_ratio = 0.3
youngs_modulus = 1e6
[../]
[./force_density]
type = ComputeSmallStrainConstantHorizonMaterialOSPD
temperature = temp
thermal_expansion_coeff = 0.02
stress_free_temperature = 0.5
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
line_search = none
start_time = 0.0
end_time = 2.0
[]
[Outputs]
exodus = true
file_base = planestrain_prescribed_OSPD
[]
(modules/richards/test/tests/dirac/bh05.i)
# unsaturated
# injection
[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
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '500 500 1E1'
x = '4000 5000 6500'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1000
bulk_mod = 2E9
[../]
[./Seff1VG]
type = RichardsSeff1VG
m = 0.8
al = 1E-5
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0
sum_s_res = 0
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 1E8
[../]
[./borehole_total_outflow_mass]
type = RichardsSumQuantity
[../]
[]
[Variables]
active = 'pressure'
[./pressure]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./p_ic]
type = FunctionIC
variable = pressure
function = initial_pressure
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[Kernels]
active = 'richardsf richardst'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[DiracKernels]
[./bh]
type = RichardsBorehole
bottom_pressure = 0
point_file = bh03.bh
SumQuantityUO = borehole_total_outflow_mass
variable = pressure
unit_weight = '0 0 0'
character = -1
[../]
[]
[Postprocessors]
[./bh_report]
type = RichardsPlotQuantity
uo = borehole_total_outflow_mass
[../]
[./fluid_mass0]
type = RichardsMass
variable = pressure
execute_on = timestep_begin
[../]
[./fluid_mass1]
type = RichardsMass
variable = pressure
execute_on = timestep_end
[../]
[./zmass_error]
type = FunctionValuePostprocessor
function = mass_bal_fcn
execute_on = timestep_end
[../]
[./p0]
type = PointValue
variable = pressure
point = '1 1 1'
execute_on = timestep_end
[../]
[]
[Functions]
[./initial_pressure]
type = ParsedFunction
value = -2E5
[../]
[./mass_bal_fcn]
type = ParsedFunction
value = abs((a-c+d)/2/(a+c))
vars = 'a c d'
vals = 'fluid_mass1 fluid_mass0 bh_report'
[../]
[]
[Materials]
[./all]
type = RichardsMaterial
block = 0
viscosity = 1E-3
mat_porosity = 0.1
mat_permeability = '1E-12 0 0 0 1E-12 0 0 0 1E-12'
density_UO = DensityConstBulk
relperm_UO = RelPermPower
sat_UO = Saturation
seff_UO = Seff1VG
SUPG_UO = SUPGstandard
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = Seff1VG
pressure_vars = pressure
[../]
[]
[Preconditioning]
[./usual]
type = SMP
full = true
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -ksp_max_it'
petsc_options_value = 'bcgs bjacobi 1E-10 1E-10 10000 30'
[../]
[]
[Executioner]
type = Transient
end_time = 6500
solve_type = NEWTON
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = bh05
exodus = false
csv = true
execute_on = timestep_end
[]
(modules/tensor_mechanics/test/tests/thermal_expansion_function/dilatation.i)
# This test checks the thermal expansion calculated via an dilatation function.
# The coefficient is selected so as to result in a 1e-4 strain in the x-axis, and to cross over
# from positive to negative strain.
[Mesh]
[./gen]
type = GeneratedMeshGenerator
dim = 3
[../]
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[AuxVariables]
[./temp]
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
add_variables = true
eigenstrain_names = eigenstrain
generate_output = 'strain_xx strain_yy strain_zz'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./bottom]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./back]
type = DirichletBC
variable = disp_z
boundary = back
value = 0.0
[../]
[]
[AuxKernels]
[./temp]
type = FunctionAux
variable = temp
function = '1 + t'
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[./thermal_expansion_strain]
type = ComputeDilatationThermalExpansionFunctionEigenstrain
dilatation_function = cte_dilatation
stress_free_temperature = 1.5
temperature = temp
eigenstrain_name = eigenstrain
[../]
[]
[Functions]
[./cte_dilatation]
type = PiecewiseLinear
x = '1 2'
y = '-1e-4 1e-4'
[../]
[]
[Postprocessors]
[./disp_x_max]
type = SideAverageValue
variable = disp_x
boundary = right
[../]
[./temp_avg]
type = ElementAverageValue
variable = temp
[../]
[]
[Executioner]
type = Transient
end_time = 1.0
dt = 0.1
[]
[Outputs]
csv = true
[]
(test/tests/geomsearch/3d_moving_penetration/pl_test1q.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
file = pl_test1q.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./normal_z]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./closest_point_z]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[./diff_z]
type = Diffusion
variable = disp_z
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = normal_z
boundary = 11
paired_boundary = 12
quantity = normal_z
[../]
[./penetrate10]
type = PenetrationAux
variable = normal_z
boundary = 12
paired_boundary = 11
quantity = normal_z
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate13]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate14]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate15]
type = PenetrationAux
variable = closest_point_z
boundary = 11
paired_boundary = 12
quantity = closest_point_z
[../]
[./penetrate16]
type = PenetrationAux
variable = closest_point_z
boundary = 12
paired_boundary = 11
quantity = closest_point_z
[../]
[./penetrate17]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate18]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate19]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate20]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b1z]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[./b2z]
type = DirichletBC
variable = disp_z
boundary = 2
value = 0
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 0.7 -0.7 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_abs_tol = 1e-7
l_max_its = 10
start_time = 0.0
dt = 0.05
end_time = 1.0
[./Quadrature]
order = THIRD
[../]
[]
[Outputs]
file_base = pl_test1q_out
exodus = true
[]
(modules/tensor_mechanics/test/tests/ad_plastic/power_law_creep.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
second_order = true
[]
[GlobalParams]
displacements = 'disp_x disp_y'
volumetric_locking_correction = false
[]
[AuxVariables]
[./hydrostatic_stress]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./hydrostatic_stress]
type = ADRankTwoScalarAux
variable = hydrostatic_stress
rank_two_tensor = stress
scalar_type = Hydrostatic
[../]
[]
[Variables]
[./disp_x]
order = SECOND
scaling = 1e-10
[../]
[./disp_y]
order = SECOND
scaling = 1e-10
[../]
[]
[Functions]
[./pull]
type = PiecewiseLinear
x = '0 10'
y = '0 1e-3'
[../]
[]
[Kernels]
[./stress_x]
type = ADStressDivergenceTensors
component = 0
variable = disp_x
[../]
[./stress_y]
type = ADStressDivergenceTensors
component = 1
variable = disp_y
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1e10
poissons_ratio = 0.3
[../]
[./strain]
type = ADComputeIncrementalSmallStrain
[../]
[./elastic_strain]
type = ADComputeMultipleInelasticStress
[../]
[./creep_ten]
type = ADPowerLawCreepStressUpdate
coefficient = 10e-24
n_exponent = 4
activation_energy = 0
base_name = creep_ten
[../]
[./creep_ten2]
type = ADPowerLawCreepStressUpdate
coefficient = 10e-24
n_exponent = 4
activation_energy = 0
base_name = creep_ten2
[../]
[./creep_one]
type = ADPowerLawCreepStressUpdate
coefficient = 1e-24
n_exponent = 4
activation_energy = 0
base_name = creep_one
[../]
[./creep_nine]
type = ADPowerLawCreepStressUpdate
coefficient = 9e-24
n_exponent = 4
activation_energy = 0
base_name = creep_nine
[../]
[./creep_zero]
type = ADPowerLawCreepStressUpdate
coefficient = 0e-24
n_exponent = 4
activation_energy = 0
base_name = creep_zero
[../]
[]
[BCs]
[./no_disp_x]
type = ADDirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./no_disp_y]
type = ADDirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./pull_disp_y]
type = ADFunctionDirichletBC
variable = disp_y
boundary = top
function = pull
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
petsc_options_iname = -pc_hypre_type
petsc_options_value = boomeramg
line_search = 'none'
nl_rel_tol = 1e-5
num_steps = 5
dt = 1e-1
[]
[Postprocessors]
[./max_disp_x]
type = ElementExtremeValue
variable = disp_x
[../]
[./max_disp_y]
type = ElementExtremeValue
variable = disp_y
[../]
[./max_hydro]
type = ElementAverageValue
variable = hydrostatic_stress
[../]
[./dt]
type = TimestepSize
[../]
[./num_lin]
type = NumLinearIterations
outputs = console
[../]
[./num_nonlin]
type = NumNonlinearIterations
outputs = console
[../]
[]
[Outputs]
csv = true
[]
(test/tests/geomsearch/3d_moving_penetration_smoothing/pl_test4qns.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
file = pl_test4q.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./normal_z]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./closest_point_z]
[../]
# [./element_id]
# [../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[./diff_z]
type = Diffusion
variable = disp_z
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
normal_smoothing_distance = 0.2
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
normal_smoothing_distance = 0.2
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = normal_z
boundary = 11
paired_boundary = 12
quantity = normal_z
[../]
[./penetrate10]
type = PenetrationAux
variable = normal_z
boundary = 12
paired_boundary = 11
quantity = normal_z
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate13]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate14]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate15]
type = PenetrationAux
variable = closest_point_z
boundary = 11
paired_boundary = 12
quantity = closest_point_z
[../]
[./penetrate16]
type = PenetrationAux
variable = closest_point_z
boundary = 12
paired_boundary = 11
quantity = closest_point_z
[../]
# [./penetrate17]
# type = PenetrationAux
# variable = element_id
# boundary = 11
# paired_boundary = 12
# quantity = element_id
# [../]
#
# [./penetrate18]
# type = PenetrationAux
# variable = element_id
# boundary = 12
# paired_boundary = 11
# quantity = element_id
# [../]
[./penetrate19]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate20]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b1z]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[./b2z]
type = DirichletBC
variable = disp_z
boundary = 2
value = 0
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-9
l_max_its = 10
start_time = 0.0
dt = 0.025
end_time = 1.0
[./Quadrature]
order = THIRD
[../]
[]
[Outputs]
file_base = pl_test4qns_out
exodus = true
[]
(test/tests/geomsearch/3d_moving_penetration/pl_test2q.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
file = pl_test2q.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./normal_z]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./closest_point_z]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[./diff_z]
type = Diffusion
variable = disp_z
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = normal_z
boundary = 11
paired_boundary = 12
quantity = normal_z
[../]
[./penetrate10]
type = PenetrationAux
variable = normal_z
boundary = 12
paired_boundary = 11
quantity = normal_z
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate13]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate14]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate15]
type = PenetrationAux
variable = closest_point_z
boundary = 11
paired_boundary = 12
quantity = closest_point_z
[../]
[./penetrate16]
type = PenetrationAux
variable = closest_point_z
boundary = 12
paired_boundary = 11
quantity = closest_point_z
[../]
[./penetrate17]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate18]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate19]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate20]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b1z]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[./b2z]
type = DirichletBC
variable = disp_z
boundary = 2
value = 0
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 0.7 -0.7 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_abs_tol = 1e-7
l_max_its = 10
start_time = 0.0
dt = 0.05
end_time = 1.0
[./Quadrature]
order = THIRD
[../]
[]
[Outputs]
file_base = pl_test2q_out
exodus = true
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_htonly/cyl2D_xz.i)
#
# 2D Cylindrical Gap Heat Transfer Test.
#
# This test exercises 2D gap heat transfer for a constant conductivity gap.
#
# The mesh consists of an inner solid cylinder of radius = 1 unit, and outer
# hollow cylinder with an inner radius of 2 in the x-z plane. In other words,
# the gap between them is 1 radial unit in length.
#
# The calculated results are the same as for the cyl2D.i case in the x-y plane.
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
[file]
type = FileMeshGenerator
file = cyl2D.e
[]
[./rotate]
type = TransformGenerator
transform = ROTATE
vector_value = '0 90 0'
input = file
[../]
[]
[Functions]
[./temp]
type = PiecewiseLinear
x = '0 1'
y = '100 200'
[../]
[]
[Variables]
[./temp]
initial_condition = 100
[../]
[]
[AuxVariables]
[./gap_conductance]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./heat_conduction]
type = HeatConduction
variable = temp
[../]
[]
[AuxKernels]
[./gap_cond]
type = MaterialRealAux
property = gap_conductance
variable = gap_conductance
boundary = 2
[../]
[]
[Materials]
[./heat1]
type = HeatConductionMaterial
block = '1 2'
specific_heat = 1.0
thermal_conductivity = 1000000.0
[../]
[]
[ThermalContact]
[./thermal_contact]
type = GapHeatTransfer
variable = temp
primary = 3
secondary = 2
emissivity_primary = 0
emissivity_secondary = 0
gap_conductivity = 1
quadrature = true
gap_geometry_type = CYLINDER
cylinder_axis_point_1 = '0 0 0'
cylinder_axis_point_2 = '0 1 0'
[../]
[]
[BCs]
[./mid]
type = FunctionDirichletBC
boundary = 1
variable = temp
function = temp
[../]
[./temp_far_right]
type = DirichletBC
boundary = 4
variable = temp
value = 100
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
dt = 1
dtmin = 0.01
end_time = 1
nl_rel_tol = 1e-12
nl_abs_tol = 1e-7
[./Quadrature]
order = fifth
side_order = seventh
[../]
[]
[Outputs]
exodus = true
[]
[Postprocessors]
[./temp_left]
type = SideAverageValue
boundary = 2
variable = temp
[../]
[./temp_right]
type = SideAverageValue
boundary = 3
variable = temp
[../]
[./flux_left]
type = SideFluxIntegral
variable = temp
boundary = 2
diffusivity = thermal_conductivity
[../]
[./flux_right]
type = SideFluxIntegral
variable = temp
boundary = 3
diffusivity = thermal_conductivity
[../]
[]
(modules/tensor_mechanics/test/tests/shell/static/large_strain_m_40_AD.i)
# Large strain/rotation test for shell elements
# A cantilever beam that is 40 m long (Y direction) with 1 m x 1 m
# cross-section is modeled using 5 shell elements placed along its
# length. The bottom boundary is fixed in all displacements and
# rotations. A load of 0.140625 N is applied at each node on the top
# boundary, resulting in a total load of 0.28125 N. E = 1800 Pa and
# v = 0.0.
# The reference solution for large deflection of this beam is based on
# K. E. Bisshopp and D.C. Drucker, Quaterly of Applied Mathematics,
# Vol 3, No. # 3, 1945.
# For PL^2/EI = 3, disp_z at tip = 0.6L = 24 m & disp_y at tip = 0.76*L-L = -9.6 m
# The FEM solution at tip of cantilever is:
# disp_z = 24.85069 m; relative error = 3.54 %
# disp_y = -9.125937 m; relative error = 5.19 %
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 5
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 40.0
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[./rot_x]
order = FIRST
family = LAGRANGE
[../]
[./rot_y]
order = FIRST
family = LAGRANGE
[../]
[]
[BCs]
[./fixy1]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./fixz1]
type = DirichletBC
variable = disp_z
boundary = bottom
value = 0.0
[../]
[./fixr1]
type = DirichletBC
variable = rot_x
boundary = bottom
value = 0.0
[../]
[./fixr2]
type = DirichletBC
variable = rot_y
boundary = bottom
value = 0.0
[../]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = bottom
value = 0.0
[../]
[]
[NodalKernels]
[./force_y2]
type = UserForcingFunctionNodalKernel
variable = disp_z
boundary = top
function = force_y
[../]
[]
[Functions]
[./force_y]
type = PiecewiseLinear
x = '0.0 1.0 3.0'
y = '0.0 1.0 1.0'
scale_factor = 0.140625
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
automatic_scaling = true
line_search = 'none'
nl_rel_tol = 1e-12
nl_abs_tol = 1e-14
dt = 0.1
dtmin = 0.1
end_time = 3.0
[]
[Kernels]
[./solid_disp_x]
type = ADStressDivergenceShell
block = '0'
component = 0
variable = disp_x
through_thickness_order = SECOND
large_strain = true
[../]
[./solid_disp_y]
type = ADStressDivergenceShell
block = '0'
component = 1
variable = disp_y
through_thickness_order = SECOND
large_strain = true
[../]
[./solid_disp_z]
type = ADStressDivergenceShell
block = '0'
component = 2
variable = disp_z
through_thickness_order = SECOND
large_strain = true
[../]
[./solid_rot_x]
type = ADStressDivergenceShell
block = '0'
component = 3
variable = rot_x
through_thickness_order = SECOND
large_strain = true
[../]
[./solid_rot_y]
type = ADStressDivergenceShell
block = '0'
component = 4
variable = rot_y
through_thickness_order = SECOND
large_strain = true
[../]
[]
[Materials]
[./elasticity]
type = ADComputeIsotropicElasticityTensorShell
youngs_modulus = 1800
poissons_ratio = 0.0
block = 0
through_thickness_order = SECOND
[../]
[./strain]
type = ADComputeFiniteShellStrain
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y'
thickness = 1.0
through_thickness_order = SECOND
[../]
[./stress]
type = ADComputeShellStress
block = 0
through_thickness_order = SECOND
[../]
[]
[Postprocessors]
[./disp_z2]
type = PointValue
point = '1.0 40.0 0.0'
variable = disp_z
[../]
[./disp_y2]
type = PointValue
point = '1.0 40.0 0.0'
variable = disp_y
[../]
[]
[Outputs]
exodus = true
[]
(modules/combined/test/tests/reference_residual/reference_residual.i)
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 4
ny = 4
nz = 4
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[./temp]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./saved_x]
[../]
[./saved_y]
[../]
[./saved_z]
[../]
[./saved_t]
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
volumetric_locking_correction = true
incremental = true
save_in = 'saved_x saved_y saved_z'
eigenstrain_names = thermal_expansion
strain = FINITE
decomposition_method = EigenSolution
extra_vector_tags = 'ref'
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
save_in = saved_t
extra_vector_tags = 'ref'
[../]
[]
[Functions]
[./pull]
type = PiecewiseLinear
x = '0 1 2'
y = '0 1 1'
scale_factor = 0.1
[../]
[]
[BCs]
[./bottom_x]
type = DirichletBC
variable = disp_x
boundary = bottom
value = 0.0
[../]
[./bottom_y]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./bottom_z]
type = DirichletBC
variable = disp_z
boundary = bottom
value = 0.0
[../]
[./top_x]
type = DirichletBC
variable = disp_x
boundary = top
value = 0.0
[../]
[./top_y]
type = FunctionDirichletBC
variable = disp_y
boundary = top
function = pull
[../]
[./top_z]
type = DirichletBC
variable = disp_z
boundary = top
value = 0.0
[../]
[./bottom_temp]
type = DirichletBC
variable = temp
boundary = bottom
value = 10.0
[../]
[./top_temp]
type = DirichletBC
variable = temp
boundary = top
value = 20.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = 0
youngs_modulus = 1.0
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[./thermal_expansion]
type = ComputeThermalExpansionEigenstrain
block = 0
eigenstrain_name = thermal_expansion
temperature = temp
thermal_expansion_coeff = 1e-5
stress_free_temperature = 0.0
[../]
[./heat1]
type = HeatConductionMaterial
block = 0
specific_heat = 1.0
thermal_conductivity = 1e-3 #Tuned to give temperature reference resid close to that of solidmech
[../]
[./density]
type = Density
block = 0
density = 1.0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
nl_rel_tol = 1e-10
l_tol = 1e-3
l_max_its = 100
dt = 1.0
end_time = 2.0
[]
[Postprocessors]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./ref_resid_z]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_z
[../]
[./ref_resid_t]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_t
[../]
[./nonlinear_its]
type = NumNonlinearIterations
[]
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/plane_stress/ad_weak_plane_stress_small.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
temperature = temp
out_of_plane_strain = strain_zz
[]
[Mesh]
[./square]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 2
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./strain_zz]
[../]
[]
[AuxVariables]
[./temp]
[../]
[./nl_strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Postprocessors]
[./react_z]
type = ADMaterialTensorIntegral
rank_two_tensor = stress
index_i = 2
index_j = 2
[../]
[./min_strain_zz]
type = NodalExtremeValue
variable = strain_zz
value_type = min
[../]
[./max_strain_zz]
type = NodalExtremeValue
variable = strain_zz
value_type = max
[../]
[]
[Modules/TensorMechanics/Master]
[./plane_stress]
planar_formulation = WEAK_PLANE_STRESS
strain = SMALL
generate_output = 'stress_xx stress_xy stress_yy stress_zz strain_xx strain_xy strain_yy'
eigenstrain_names = eigenstrain
use_automatic_differentiation = true
[../]
[]
[AuxKernels]
[./tempfuncaux]
type = FunctionAux
variable = temp
function = tempfunc
use_displaced_mesh = false
[../]
[./strain_zz]
type = ADRankTwoAux
rank_two_tensor = total_strain
variable = nl_strain_zz
index_i = 2
index_j = 2
[../]
[]
[Functions]
[./pull]
type = PiecewiseLinear
x='0 1 100'
y='0 0.00 0.00'
[../]
[./tempfunc]
type = ParsedFunction
value = '(1 - x) * t'
[../]
[]
[BCs]
[./bottomx]
type = DirichletBC
boundary = 0
variable = disp_x
value = 0.0
[../]
[./bottomy]
type = DirichletBC
boundary = 0
variable = disp_y
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
poissons_ratio = 0.3
youngs_modulus = 1e6
[../]
[./thermal_strain]
type = ADComputeThermalExpansionEigenstrain
thermal_expansion_coeff = 0.02
stress_free_temperature = 0.5
eigenstrain_name = eigenstrain
[../]
[./stress]
type = ADComputeLinearElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-14
nl_abs_tol = 1e-12
# time control
start_time = 0.0
dt = 1.0
dtmin = 1.0
end_time = 2.0
[]
[Outputs]
file_base = 'weak_plane_stress_small_out'
exodus = true
[]
(modules/tensor_mechanics/test/tests/dynamics/acceleration_bc/AccelerationBC_test_ti.i)
# Test for Acceleration boundary condition
# This test contains one brick element which is fixed in the y and z direction.
# Base acceleration is applied in the x direction to all nodes on the bottom surface (y=0).
# The PresetAcceleration converts the given acceleration to a displacement
# using Newmark time integration. This displacement is then prescribed on the boundary.
#
# Result: The acceleration at the bottom node should be same as the input acceleration
# which is a triangular function with peak at t = 0.2 in this case. Width of the triangular function
# is 0.2 s.
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = 0.0
xmax = 0.1
ymin = 0.0
ymax = 1.0
zmin = 0.0
zmax = 0.1
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./vel_x]
[../]
[./accel_x]
[../]
[./vel_y]
[../]
[./accel_y]
[../]
[./vel_z]
[../]
[./accel_z]
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./TensorMechanics]
[../]
[./inertia_x]
type = InertialForce
variable = disp_x
[../]
[./inertia_y]
type = InertialForce
variable = disp_y
[../]
[./inertia_z]
type = InertialForce
variable = disp_z
[../]
[]
[AuxKernels]
[./accel_x] # These auxkernels are only to check output
type = TestNewmarkTI
displacement = disp_x
variable = accel_x
first = false
[../]
[./accel_y]
type = TestNewmarkTI
displacement = disp_y
variable = accel_y
first = false
[../]
[./accel_z]
type = TestNewmarkTI
displacement = disp_z
variable = accel_z
first = false
[../]
[./vel_x]
type = TestNewmarkTI
displacement = disp_x
variable = vel_x
[../]
[./vel_y]
type = TestNewmarkTI
displacement = disp_y
variable = vel_y
[../]
[./vel_z]
type = TestNewmarkTI
displacement = disp_z
variable = vel_z
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 0
index_j = 1
[../]
[./strain_yy]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_yy
index_i = 0
index_j = 1
[../]
[]
[Functions]
[./acceleration_bottom]
type = PiecewiseLinear
data_file = acceleration.csv
format = columns
[../]
[]
[BCs]
[./top_y]
type = DirichletBC
variable = disp_y
boundary = top
value=0.0
[../]
[./top_z]
type = DirichletBC
variable = disp_z
boundary = top
value=0.0
[../]
[./bottom_y]
type = DirichletBC
variable = disp_y
boundary = bottom
value=0.0
[../]
[./bottom_z]
type = DirichletBC
variable = disp_z
boundary = bottom
value=0.0
[../]
[./preset_accelertion]
type = PresetAcceleration
boundary = bottom
function = acceleration_bottom
variable = disp_x
beta = 0.25
acceleration = accel_x
velocity = vel_x
[../]
[]
[Materials]
[./Elasticity_tensor]
type = ComputeElasticityTensor
fill_method = symmetric_isotropic
C_ijkl = '210e9 0'
[../]
[./strain]
type = ComputeSmallStrain
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[./density]
type = GenericConstantMaterial
prop_names = 'density'
prop_values = '7750'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart'
petsc_options_value = 'hypre boomeramg 101'
start_time = 0
end_time = 2.0
dt = 0.01
dtmin = 0.01
nl_abs_tol = 1e-8
nl_rel_tol = 1e-8
l_tol = 1e-8
timestep_tolerance = 1e-8
# Time integrator scheme
schem = "newmark-beta"
[]
[Postprocessors]
[./_dt]
type = TimestepSize
[../]
[./disp]
type = NodalVariableValue
variable = disp_x
nodeid = 1
[../]
[./vel]
type = NodalVariableValue
variable = vel_x
nodeid = 1
[../]
[./accel]
type = NodalVariableValue
variable = accel_x
nodeid = 1
[../]
[]
[Outputs]
file_base = "AccelerationBC_test_out"
csv = true
exodus = true
perf_graph = true
[]
(modules/tensor_mechanics/test/tests/ad_anisotropic_creep/anis_mech_hill_tensor_creep.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 128
ny = 128
second_order = true
[]
[GlobalParams]
displacements = 'disp_x disp_y'
volumetric_locking_correction = false
[]
[AuxVariables]
[hydrostatic_stress]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[hydrostatic_stress]
type = ADRankTwoScalarAux
variable = hydrostatic_stress
rank_two_tensor = stress
scalar_type = Hydrostatic
[]
[]
[Variables]
[disp_x]
order = SECOND
scaling = 1e-10
[]
[disp_y]
order = SECOND
scaling = 1e-10
[]
[]
[Functions]
[pull]
type = PiecewiseLinear
x = '0 10e3'
y = '0 1e-4'
[]
[]
[Kernels]
[stress_x]
type = ADStressDivergenceTensors
component = 0
variable = disp_x
[]
[stress_y]
type = ADStressDivergenceTensors
component = 1
variable = disp_y
[]
[]
[Modules/TensorMechanics/Master]
[all]
strain = FINITE
add_variables = true
generate_output = 'elastic_strain_xx elastic_strain_yy elastic_strain_xy'
use_automatic_differentiation = true
[]
[]
[Materials]
[elasticity_tensor]
type = ADComputeElasticityTensor
fill_method = orthotropic
C_ijkl = '2.0e3 2.0e5 2.0e3 0.71428571e3 0.71428571e3 0.71428571e3 0.4 0.2 0.004 0.004 0.2 0.4'
[]
[elastic_strain]
type = ADComputeMultipleInelasticStress
inelastic_models = "trial_creep"
max_iterations = 300
[]
[trial_creep]
type = ADHillCreepStressUpdate
coefficient = 1e-24
n_exponent = 4
m_exponent = 0
activation_energy = 0
# internal_solve_output_on = always
# F G H L M N
hill_constants = "0.5 0.5 0.3866 1.6413 1.6413 1.2731"
base_name = trial_creep
[]
[creep_one]
type = ADPowerLawCreepStressUpdate
coefficient = 1e-24
n_exponent = 4
activation_energy = 0
base_name = creep_one
[]
[creep_nine]
type = ADPowerLawCreepStressUpdate
coefficient = 9e-24
n_exponent = 4
activation_energy = 0
base_name = creep_nine
[]
[]
[BCs]
[no_disp_x]
type = ADDirichletBC
variable = disp_x
boundary = left
value = 0.0
[]
[no_disp_y]
type = ADDirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[]
[pull_disp_y]
type = ADFunctionDirichletBC
variable = disp_y
boundary = top
function = pull
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = Newton
petsc_options_iname = '-ksp_gmres_restart -pc_type -sub_pc_type'
petsc_options_value = '101 asm lu'
line_search = 'none'
nl_rel_tol = 1e-5
nl_abs_tol = 1.0e-13
num_steps = 200
dt = 1.0e2
automatic_scaling = true
[]
[Postprocessors]
[max_disp_x]
type = ElementExtremeValue
variable = disp_x
[]
[max_disp_y]
type = ElementExtremeValue
variable = disp_y
[]
[max_hydro]
type = ElementAverageValue
variable = hydrostatic_stress
[]
[dt]
type = TimestepSize
[]
[num_lin]
type = NumLinearIterations
outputs = console
[]
[num_nonlin]
type = NumNonlinearIterations
outputs = console
[]
[]
[Outputs]
csv = true
exodus = true
[]
(modules/combined/test/tests/generalized_plane_strain_tm_contact/out_of_plane_pressure.i)
# Tests for application of out-of-plane pressure in generalized plane strain.
[Mesh]
type = GeneratedMesh
nx = 2
ny = 2
dim = 2
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
displacements = 'disp_x disp_y'
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./scalar_strain_zz]
order = FIRST
family = SCALAR
[../]
[]
[AuxVariables]
[./saved_x]
order = FIRST
family = LAGRANGE
[../]
[./saved_y]
order = FIRST
family = LAGRANGE
[../]
[./saved_zz]
order = FIRST
family = SCALAR
[../]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Postprocessors]
[./react_z]
type = MaterialTensorIntegral
rank_two_tensor = stress
index_i = 2
index_j = 2
[../]
[]
[Modules]
[./TensorMechanics]
[./GeneralizedPlaneStrain]
[./gps]
displacements = 'disp_x disp_y'
scalar_out_of_plane_strain = scalar_strain_zz
out_of_plane_pressure = traction_function
factor = 1e5
[../]
[../]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
displacements = 'disp_x disp_y'
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
[../]
[]
[AuxScalarKernels]
[./gps_ref_res]
type = GeneralizedPlaneStrainReferenceResidual
variable = saved_zz
generalized_plane_strain = gps_GeneralizedPlaneStrainUserObject
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
[../]
[./strain_xx]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_xx
index_i = 0
index_j = 0
[../]
[./strain_xy]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_xy
index_i = 0
index_j = 1
[../]
[./strain_yy]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_yy
index_i = 1
index_j = 1
[../]
[./strain_zz]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_zz
index_i = 2
index_j = 2
[../]
[]
[Functions]
[./traction_function]
type = PiecewiseLinear
x = '0 2'
y = '0 1'
[../]
[]
[BCs]
[./leftx]
type = DirichletBC
boundary = left
variable = disp_x
value = 0.0
[../]
[./bottomy]
type = DirichletBC
boundary = bottom
variable = disp_y
value = 0.0
[../]
[]
[Materials]
[./elastic_tensor]
type = ComputeIsotropicElasticityTensor
poissons_ratio = 0.3
youngs_modulus = 1e6
[../]
[./strain]
type = ComputePlaneSmallStrain
displacements = 'disp_x disp_y'
scalar_out_of_plane_strain = scalar_strain_zz
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
line_search = none
# controls for linear iterations
l_max_its = 100
l_tol = 1e-4
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-14
nl_abs_tol = 1e-11
# time control
start_time = 0.0
dt = 1.0
dtmin = 1.0
end_time = 2.0
num_steps = 5000
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/coupled_pressure/coupled_pressure_test.i)
#
# Pressure Test
#
# This test is designed to compute pressure loads on three faces of a unit cube.
# The pressure is computed as an auxiliary variable. It should give the same result
# as pressure_test.i
#
# The mesh is composed of one block with a single element. Symmetry bcs are
# applied to the faces opposite the pressures. Poisson's ratio is zero,
# which makes it trivial to check displacements.
#
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
type = FileMesh
file = pressure_test.e
[]
[Functions]
[./rampConstant]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 1.'
scale_factor = 1.0
[../]
[./zeroRamp]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 0. 1.'
scale_factor = 2.0
[../]
[./rampUnramp]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 0.'
scale_factor = 10.0
[../]
[]
[AuxVariables]
[./pressure_1]
[../]
[./pressure_2]
[../]
[./pressure_3]
[../]
[]
[AuxKernels]
[./side1_pressure_ak]
type = FunctionAux
variable = pressure_1
boundary = 1
function = rampConstant
[../]
[./side2_pressure_ak]
type = FunctionAux
variable = pressure_2
boundary = 2
function = zeroRamp
[../]
[./side3_pressure_ak]
type = FunctionAux
variable = pressure_3
boundary = 3
function = rampUnramp
[../]
[]
[Modules]
[./TensorMechanics]
[./Master]
[./all]
strain = SMALL
add_variables = true
[../]
[../]
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 4
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = 5
value = 0.0
[../]
[./no_z]
type = DirichletBC
variable = disp_z
boundary = 6
value = 0.0
[../]
[./CoupledPressure]
[./Side1]
boundary = '1'
pressure = pressure_1
displacements = 'disp_x disp_y disp_z'
[../]
[./Side2]
boundary = '2'
pressure = pressure_2
displacements = 'disp_x disp_y disp_z'
[../]
[../]
[./side3_x]
type = CoupledPressureBC
variable = 'disp_x'
boundary = '3'
pressure = pressure_3
component = 0
[../]
[./side3_y]
type = CoupledPressureBC
variable = 'disp_y'
boundary = '3'
pressure = pressure_3
component = 1
[../]
[./side3_z]
type = CoupledPressureBC
variable = 'disp_z'
boundary = '3'
pressure = pressure_3
component = 2
[../]
[]
[Materials]
[./Elasticity_tensor]
type = ComputeElasticityTensor
fill_method = symmetric_isotropic
C_ijkl = '0 0.5e6'
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
nl_abs_tol = 1e-10
l_max_its = 20
start_time = 0.0
dt = 1.0
num_steps = 2
end_time = 2.0
[]
[Outputs]
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[]
(modules/tensor_mechanics/test/tests/plane_stress/ad_weak_plane_stress_finite.i)
[GlobalParams]
displacements = 'disp_x disp_y'
temperature = temp
out_of_plane_strain = strain_zz
[]
[Mesh]
[./square]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 2
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./strain_zz]
[../]
[]
[AuxVariables]
[./temp]
[../]
[./nl_strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Postprocessors]
[./react_z]
type = ADMaterialTensorIntegral
rank_two_tensor = stress
index_i = 2
index_j = 2
[../]
[./min_strain_zz]
type = NodalExtremeValue
variable = strain_zz
value_type = min
[../]
[./max_strain_zz]
type = NodalExtremeValue
variable = strain_zz
value_type = max
[../]
[]
[Modules/TensorMechanics/Master]
[./plane_stress]
planar_formulation = WEAK_PLANE_STRESS
strain = FINITE
generate_output = 'stress_xx stress_xy stress_yy stress_zz strain_xx strain_xy strain_yy'
eigenstrain_names = eigenstrain
use_automatic_differentiation = true
[../]
[]
[AuxKernels]
[./tempfuncaux]
type = FunctionAux
variable = temp
function = tempfunc
use_displaced_mesh = false
[../]
[./strain_zz]
type = ADRankTwoAux
rank_two_tensor = total_strain
variable = nl_strain_zz
index_i = 2
index_j = 2
[../]
[]
[Functions]
[./pull]
type = PiecewiseLinear
x='0 1 100'
y='0 0.00 0.00'
[../]
[./tempfunc]
type = ParsedFunction
value = '(1 - x) * t'
[../]
[]
[BCs]
[./bottomx]
type = DirichletBC
boundary = 0
variable = disp_x
value = 0.0
[../]
[./bottomy]
type = DirichletBC
boundary = 0
variable = disp_y
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
poissons_ratio = 0.3
youngs_modulus = 1e6
[../]
[./thermal_strain]
type = ADComputeThermalExpansionEigenstrain
thermal_expansion_coeff = 0.02
stress_free_temperature = 0.5
eigenstrain_name = eigenstrain
[../]
[./stress]
type = ADComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-14
nl_abs_tol = 1e-12
# time control
start_time = 0.0
dt = 1.0
dtmin = 1.0
end_time = 2.0
[]
[Outputs]
file_base = 'weak_plane_stress_finite_out'
exodus = true
[]
(modules/combined/test/tests/ad_power_law_creep/power_law_creep_smallstrain.i)
# 1x1x1 unit cube with uniform pressure on top face for the case of small strain.
# This test does not have a solid mechanics analog because there is not an equvialent
# small strain with rotations strain calculator material in solid mechanics
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
[]
[Variables]
[./temp]
order = FIRST
family = LAGRANGE
initial_condition = 1000.0
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
incremental = true
add_variables = true
generate_output = 'stress_yy creep_strain_xx creep_strain_yy creep_strain_zz elastic_strain_yy'
use_automatic_differentiation = true
[../]
[]
[Functions]
[./top_pull]
type = PiecewiseLinear
x = '0 1'
y = '1 1'
[../]
[]
[Kernels]
[./heat]
type = ADHeatConduction
variable = temp
[../]
[./heat_ie]
type = ADHeatConductionTimeDerivative
variable = temp
[../]
[]
[BCs]
[./u_top_pull]
type = ADPressure
variable = disp_y
component = 1
boundary = top
constant = -10.0e6
function = top_pull
[../]
[./u_bottom_fix]
type = ADDirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./u_yz_fix]
type = ADDirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./u_xy_fix]
type = ADDirichletBC
variable = disp_z
boundary = back
value = 0.0
[../]
[./temp_fix]
type = DirichletBC
variable = temp
boundary = 'bottom top'
value = 1000.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 2e11
poissons_ratio = 0.3
constant_on = SUBDOMAIN
[../]
[./radial_return_stress]
type = ADComputeMultipleInelasticStress
inelastic_models = 'power_law_creep'
[../]
[./power_law_creep]
type = ADPowerLawCreepStressUpdate
coefficient = 1.0e-15
n_exponent = 4
activation_energy = 3.0e5
temperature = temp
[../]
[./thermal]
type = ADHeatConductionMaterial
specific_heat = 1.0
thermal_conductivity = 100.
[../]
[./density]
type = ADDensity
density = 1.0
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 20
nl_max_its = 20
nl_rel_tol = 1e-6
nl_abs_tol = 1e-6
l_tol = 1e-5
start_time = 0.0
end_time = 1.0
num_steps = 10
dt = 0.1
[]
[Outputs]
exodus = true
[]
(test/tests/geomsearch/2d_moving_penetration/pl_test2.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
file = pl_test2.e
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate10]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate13]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate14]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate15]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate16]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 0.7 -0.7 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-9
l_max_its = 10
start_time = 0.0
dt = 0.05
end_time = 1.0
[]
[Outputs]
file_base = pl_test2_out
exodus = true
[]
(modules/tensor_mechanics/test/tests/ad_smeared_cracking/cracking.i)
#
# Simple pull test for cracking.
# The stress increases for two steps and then drops to zero.
[Mesh]
file = cracking_test.e
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Functions]
[./displ]
type = PiecewiseLinear
x = '0 1 2 3 4'
y = '0 1 0 -1 0'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx'
use_automatic_differentiation = true
[../]
[]
[BCs]
[./pull]
type = ADFunctionDirichletBC
variable = disp_x
boundary = 4
function = displ
[../]
[./left]
type = ADDirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./bottom]
type = ADDirichletBC
variable = disp_y
boundary = 2
value = 0.0
[../]
[./back]
type = ADDirichletBC
variable = disp_z
boundary = 3
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 2.8e7
poissons_ratio = 0
[../]
[./elastic_stress]
type = ADComputeSmearedCrackingStress
cracking_stress = 1.68e6
softening_models = abrupt_softening
[../]
[./abrupt_softening]
type = ADAbruptSoftening
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
petsc_options_iname = '-ksp_gmres_restart -pc_type -sub_pc_type'
petsc_options_value = '101 asm lu'
line_search = 'none'
l_max_its = 100
nl_max_its = 100
nl_rel_tol = 1e-8
nl_abs_tol = 1e-8
l_tol = 1e-5
start_time = 0.0
end_time = 0.1
dt = 0.025
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/dynamics/wave_1D/wave_rayleigh_hht_AD.i)
# Wave propogation in 1D using HHT time integration in the presence of Rayleigh damping
#
# The test is for an 1D bar element of length 4m fixed on one end
# with a sinusoidal pulse dirichlet boundary condition applied to the other end.
# alpha, beta and gamma are HHT time integration parameters
# eta and zeta are mass dependent and stiffness dependent Rayleigh damping
# coefficients, respectively.
# The equation of motion in terms of matrices is:
#
# M*accel + (eta*M+zeta*K)*((1+alpha)*vel-alpha*vel_old)
# +(1+alpha)*K*disp-alpha*K*disp_old = 0
#
# Here M is the mass matrix, K is the stiffness matrix
#
# The displacement at the first, second, third and fourth node at t = 0.1 are
# -7.787499960311491942e-02, 1.955566679096475483e-02 and -4.634888180231294501e-03, respectively.
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 4
nz = 1
xmin = 0.0
xmax = 0.1
ymin = 0.0
ymax = 4.0
zmin = 0.0
zmax = 0.1
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./vel_x]
[../]
[./accel_x]
[../]
[./vel_y]
[../]
[./accel_y]
[../]
[./vel_z]
[../]
[./accel_z]
[../]
[]
[Kernels]
[./DynamicTensorMechanics]
displacements = 'disp_x disp_y disp_z'
alpha = -0.3
zeta = 0.1
use_automatic_differentiation = true
[../]
[./inertia_x]
type = InertialForce
variable = disp_x
velocity = vel_x
acceleration = accel_x
beta = 0.422
gamma = 0.8
eta=0.1
alpha = -0.3
[../]
[./inertia_y]
type = InertialForce
variable = disp_y
velocity = vel_y
acceleration = accel_y
beta = 0.422
gamma = 0.8
eta=0.1
alpha = -0.3
[../]
[./inertia_z]
type = InertialForce
variable = disp_z
velocity = vel_z
acceleration = accel_z
beta = 0.422
gamma = 0.8
eta = 0.1
alpha = -0.3
[../]
[]
[AuxKernels]
[./accel_x]
type = NewmarkAccelAux
variable = accel_x
displacement = disp_x
velocity = vel_x
beta = 0.422
execute_on = timestep_end
[../]
[./vel_x]
type = NewmarkVelAux
variable = vel_x
acceleration = accel_x
gamma = 0.8
execute_on = timestep_end
[../]
[./accel_y]
type = NewmarkAccelAux
variable = accel_y
displacement = disp_y
velocity = vel_y
beta = 0.422
execute_on = timestep_end
[../]
[./vel_y]
type = NewmarkVelAux
variable = vel_y
acceleration = accel_y
gamma = 0.8
execute_on = timestep_end
[../]
[./accel_z]
type = NewmarkAccelAux
variable = accel_z
displacement = disp_z
velocity = vel_z
beta = 0.422
execute_on = timestep_end
[../]
[./vel_z]
type = NewmarkVelAux
variable = vel_z
acceleration = accel_z
gamma = 0.8
execute_on = timestep_end
[../]
[]
[BCs]
[./top_y]
type = DirichletBC
variable = disp_y
boundary = top
value=0.0
[../]
[./top_x]
type = DirichletBC
variable = disp_x
boundary = top
value=0.0
[../]
[./top_z]
type = DirichletBC
variable = disp_z
boundary = top
value=0.0
[../]
[./right_x]
type = DirichletBC
variable = disp_x
boundary = right
value=0.0
[../]
[./right_z]
type = DirichletBC
variable = disp_z
boundary = right
value=0.0
[../]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = left
value=0.0
[../]
[./left_z]
type = DirichletBC
variable = disp_z
boundary = left
value=0.0
[../]
[./front_x]
type = DirichletBC
variable = disp_x
boundary = front
value=0.0
[../]
[./front_z]
type = DirichletBC
variable = disp_z
boundary = front
value=0.0
[../]
[./back_x]
type = DirichletBC
variable = disp_x
boundary = back
value=0.0
[../]
[./back_z]
type = DirichletBC
variable = disp_z
boundary = back
value=0.0
[../]
[./bottom_x]
type = DirichletBC
variable = disp_x
boundary = bottom
value=0.0
[../]
[./bottom_z]
type = DirichletBC
variable = disp_z
boundary = bottom
value=0.0
[../]
[./bottom_y]
type = FunctionDirichletBC
variable = disp_y
boundary = bottom
function = displacement_bc
[../]
[]
[Materials]
[./Elasticity_tensor]
type = ADComputeElasticityTensor
block = 0
fill_method = symmetric_isotropic
C_ijkl = '1 0'
[../]
[./strain]
type = ADComputeSmallStrain
block = 0
displacements = 'disp_x disp_y disp_z'
[../]
[./stress]
type = ADComputeLinearElasticStress
block = 0
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = 'density'
prop_values = '1'
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
start_time = 0
end_time = 6.0
l_tol = 1e-12
nl_rel_tol = 1e-12
dt = 0.1
[]
[Functions]
[./displacement_bc]
type = PiecewiseLinear
data_file = 'sine_wave.csv'
format = columns
[../]
[]
[Postprocessors]
[./_dt]
type = TimestepSize
[../]
[./disp_1]
type = NodalVariableValue
nodeid = 1
variable = disp_y
[../]
[./disp_2]
type = NodalVariableValue
nodeid = 3
variable = disp_y
[../]
[./disp_3]
type = NodalVariableValue
nodeid = 10
variable = disp_y
[../]
[./disp_4]
type = NodalVariableValue
nodeid = 14
variable = disp_y
[../]
[]
[Outputs]
file_base = 'wave_rayleigh_hht_out'
exodus = true
perf_graph = true
[]
(modules/richards/test/tests/gravity_head_1/gh22.i)
# investigating validity of immobile saturation
# 50 elements, no SUPG
[Mesh]
type = GeneratedMesh
dim = 1
nx = 50
xmin = -1
xmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1 10 100 1000 10000'
x = '0 10 100 1000 10000'
[../]
[]
[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 = 0.3
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGnone]
type = RichardsSUPGnone
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
initial_condition = -1.0
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[Kernels]
active = 'richardsf richardst'
[./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-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 = Transient
solve_type = Newton
dt = 1E0
end_time = 1E5
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = gh22
execute_on = 'timestep_end final'
interval = 10000
exodus = true
[]
(test/tests/geomsearch/2d_moving_penetration/pl_test2q.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
file = pl_test2q.e
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate10]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate13]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate14]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate15]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate16]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 0.7 -0.7 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1.e-9
l_max_its = 10
start_time = 0.0
dt = 0.05
end_time = 1.0
[./Quadrature]
order = THIRD
[../]
[]
[Outputs]
file_base = pl_test2q_out
exodus = true
[]
(modules/contact/test/tests/incremental_slip/incremental_slip.i)
[Mesh]
file = incremental_slip.e
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
incremental = true
add_variables = true
[../]
[]
[Functions]
[./secondary_x]
type = PiecewiseLinear
x = '0 1 2 3 4 5 6 7 8 9'
y = '0 0 0.5 0 0 0 -0.25 0 0.5 0'
[../]
[./secondary_y]
type = PiecewiseLinear
x = '0 1 9'
y = '0 -0.15 -0.15'
[../]
[./secondary_z]
type = PiecewiseLinear
x = '0 1 2 3 4 5 6 7 8 9'
y = '0 0 -0.5 0 0 0 0.25 0 -0.5 0'
[../]
[./primary_x]
type = PiecewiseLinear
x = '0 1 2 3 4 5 6 7 8 9'
y = '0 0 0 0 0.5 0 0.25 0 0.5 0'
[../]
[./primary_y]
type = PiecewiseLinear
x = '0 9'
y = '0 0'
[../]
[./primary_z]
type = PiecewiseLinear
x = '0 1 2 3 4 5 6 7 8 9'
y = '0 0 0 0 0.5 0 -0.25 0 -0.5 0'
[../]
[]
[AuxVariables]
[./inc_slip_x]
order = FIRST
family = LAGRANGE
[../]
[./inc_slip_y]
order = FIRST
family = LAGRANGE
[../]
[./inc_slip_z]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
quantity = incremental_slip_x
boundary = 3
paired_boundary = 2
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
quantity = incremental_slip_y
boundary = 3
paired_boundary = 2
[../]
[./inc_slip_z]
type = PenetrationAux
variable = inc_slip_z
quantity = incremental_slip_z
boundary = 3
paired_boundary = 2
[../]
[]
[Contact]
[./dummy_name]
primary = 2
secondary = 3
penalty = 1e7
[../]
[]
[BCs]
[./secondary_x]
type = FunctionDirichletBC
variable = disp_x
preset = false
boundary = 4
function = secondary_x
[../]
[./secondary_y]
type = FunctionDirichletBC
variable = disp_y
preset = false
boundary = 4
function = secondary_y
[../]
[./secondary_z]
type = FunctionDirichletBC
variable = disp_z
preset = false
boundary = 4
function = secondary_z
[../]
[./primary_x]
type = FunctionDirichletBC
variable = disp_x
boundary = '1 2'
function = primary_x
[../]
[./primary_y]
type = FunctionDirichletBC
variable = disp_y
boundary = '1 2'
function = primary_y
[../]
[./primary_z]
type = FunctionDirichletBC
variable = disp_z
boundary = '1 2'
function = primary_z
[../]
[] # BCs
[Materials]
[./elasticity_tensor_1]
type = ComputeIsotropicElasticityTensor
block = 1
youngs_modulus = 1.0e6
poissons_ratio = 0.0
[../]
[./stress_1]
type = ComputeFiniteStrainElasticStress
block = 1
[../]
[./elasticity_tensor_2]
type = ComputeIsotropicElasticityTensor
block = 2
youngs_modulus = 1.0e6
poissons_ratio = 0.0
[../]
[./stress_2]
type = ComputeFiniteStrainElasticStress
block = 2
[../]
[]
[Executioner]
type = Transient
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-8
l_max_its = 100
nl_max_its = 10
dt = 1.0
num_steps = 9
[] # Executioner
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/material_limit_time_step/elas_plas/nafems_nl1_lim.i)
#
# Tests material model IsotropicPlasticity with material based time stepper
# Boundary conditions from NAFEMS test NL1
#
[GlobalParams]
order = FIRST
family = LAGRANGE
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]#Comment
file = one_elem2.e
[] # Mesh
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[] # Variables
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./vonmises]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./plastic_strain_eff]
order = CONSTANT
family = MONOMIAL
[../]
[./tot_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[] # AuxVariables
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
[../]
[./vonmises]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = vonmises
scalar_type = VonMisesStress
execute_on = timestep_end
[../]
[./elastic_strain_yy]
type = RankTwoAux
rank_two_tensor = elastic_strain
variable = elastic_strain_yy
index_i = 1
index_j = 1
[../]
[./plastic_strain_eff]
type = MaterialRealAux
property = effective_plastic_strain
variable = plastic_strain_eff
[../]
[./tot_strain_yy]
type = RankTwoAux
rank_two_tensor = total_strain
variable = tot_strain_yy
index_i = 1
index_j = 1
[../]
[] # AuxKernels
[Functions]
[./appl_dispx]
type = PiecewiseLinear
x = '0 1.0 2.0 3.0 4.0 5.0 6.0 7.0 8.0'
y = '0.0 0.25e-4 0.50e-4 0.50e-4 0.50e-4 0.25e-4 0.0 0.0 0.0'
[../]
[./appl_dispy]
type = PiecewiseLinear
x = '0 1.0 2.0 3.0 4.0 5.0 6.0 7.0 8.0'
y = '0.0 0.0 0.0 0.25e-4 0.50e-4 0.50e-4 0.50e-4 0.25e-4 0.0 '
[../]
[]
[BCs]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 101
value = 0.0
[../]
[./origin_x]
type = DirichletBC
variable = disp_x
boundary = 103
value = 0.0
[../]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 102
value = 0.0
[../]
[./origin_y]
type = DirichletBC
variable = disp_y
boundary = 103
value = 0.0
[../]
[./top_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 1
function = appl_dispy
[../]
[./right_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 2
function = appl_dispx
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = 1
youngs_modulus = 250e9
poissons_ratio = 0.25
[../]
[./strain]
type = ComputePlaneFiniteStrain
block = 1
[../]
[./stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'isoplas'
block = 1
[../]
[./isoplas]
type = IsotropicPlasticityStressUpdate
yield_stress = 5e6
hardening_constant = 0.0
relative_tolerance = 1e-20
absolute_tolerance = 1e-8
max_inelastic_increment = 0.000001
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
nl_rel_tol = 1e-10
nl_abs_tol = 1e-12
l_tol = 1e-4
l_max_its = 100
nl_max_its = 20
[./TimeStepper]
type = IterationAdaptiveDT
dt = 0.1
time_t = '1.0 2.0 3.0 4.0 5.0 6.0 7.0 8.0'
time_dt = '0.1 0.1 0.1 0.1 0.1 0.1 0.1 0.1'
optimal_iterations = 30
iteration_window = 9
growth_factor = 2.0
cutback_factor = 0.5
timestep_limiting_postprocessor = matl_ts_min
[../]
start_time = 0.0
num_steps = 1000
end_time = 8.0
[] # Executioner
[Postprocessors]
[./matl_ts_min]
type = MaterialTimeStepPostprocessor
[../]
[./stress_xx]
type = ElementAverageValue
variable = stress_xx
[../]
[./stress_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./stress_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./vonmises]
type = ElementAverageValue
variable = vonmises
[../]
[./el_strain_yy]
type = ElementAverageValue
variable = elastic_strain_yy
[../]
[./plas_strain_eff]
type = ElementAverageValue
variable = plastic_strain_eff
[../]
[./tot_strain_yy]
type = ElementAverageValue
variable = tot_strain_yy
[../]
[./disp_x1]
type = NodalVariableValue
nodeid = 0
variable = disp_x
[../]
[./disp_x4]
type = NodalVariableValue
nodeid = 3
variable = disp_x
[../]
[./disp_y1]
type = NodalVariableValue
nodeid = 0
variable = disp_y
[../]
[./disp_y4]
type = NodalVariableValue
nodeid = 3
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[]
[Outputs]
exodus = true
csv = true
[./console]
type = Console
output_linear = true
[../]
[] # Outputs
(modules/combined/test/tests/ad_cavity_pressure/rz.i)
#
# Cavity Pressure Test
#
# This test is designed to compute an internal pressure based on
# p = n * R * T / V
# where
# p is the pressure
# n is the amount of material in the volume (moles)
# R is the universal gas constant
# T is the temperature
# V is the volume
#
# The mesh is composed of one block (2) with an interior cavity of volume 8.
# Block 1 sits in the cavity and has a volume of 1. Thus, the total
# initial volume is 7.
# The test adjusts T in the following way:
# T => T0 + beta * t
# with
# beta = T0
# T0 = 240.54443866068704
# V0 = 7
# n0 = f(p0)
# p0 = 100
# R = 8.314472 J * K^(-1) * mol^(-1)
#
# So, n0 = p0 * V0 / R / T0 = 100 * 7 / 8.314472 / 240.544439
# = 0.35
#
# At t = 1, p = 200.
[Problem]
coord_type = RZ
[]
[GlobalParams]
displacements = 'disp_r disp_z'
[]
[Mesh]
file = rz.e
[]
[Functions]
[./temperature]
type = PiecewiseLinear
x = '0 1'
y = '1 2'
scale_factor = 240.54443866068704
[../]
[]
[Variables]
[./disp_r]
[../]
[./disp_z]
[../]
[./temp]
initial_condition = 240.54443866068704
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
use_automatic_differentiation = true
[../]
[./heat]
type = ADDiffusion
variable = temp
use_displaced_mesh = true
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
variable = disp_r
boundary = '1 2'
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_z
boundary = '1 2'
value = 0.0
[../]
[./temperatureInterior]
type = ADFunctionDirichletBC
preset = false
boundary = 2
function = temperature
variable = temp
[../]
[./CavityPressure]
[./1]
boundary = 2
initial_pressure = 100
R = 8.314472
temperature = aveTempInterior
volume = internalVolume
startup_time = 0.5
output = ppress
use_automatic_differentiation = true
[../]
[../]
[]
[Materials]
[./elastic_tensor1]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
block = 1
[../]
[./strain1]
type = ADComputeAxisymmetricRZFiniteStrain
block = 1
[../]
[./stress1]
type = ADComputeFiniteStrainElasticStress
block = 1
[../]
[./elastic_tensor2]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
block = 2
[../]
[./strain2]
type = ADComputeAxisymmetricRZFiniteStrain
block = 2
[../]
[./stress2]
type = ADComputeFiniteStrainElasticStress
block = 2
[../]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_type'
petsc_options_value = 'asm lu'
nl_abs_tol = 1e-10
l_max_its = 20
dt = 0.5
end_time = 1.0
[]
[Postprocessors]
[./internalVolume]
type = InternalVolume
boundary = 2
execute_on = 'initial linear'
[../]
[./aveTempInterior]
type = SideAverageValue
boundary = 2
variable = temp
execute_on = 'initial linear'
[../]
[]
[Outputs]
exodus = true
[./checkpoint]
type = Checkpoint
num_files = 1
[../]
[]
(modules/tensor_mechanics/test/tests/central_difference/lumped/1D/1d_nodalmass_implicit.i)
# Test for central difference integration for 1D elements
[Mesh]
[./generated_mesh]
type = GeneratedMeshGenerator
xmin = 0
xmax = 10
nx = 5
dim = 1
[../]
[./all_nodes]
type = BoundingBoxNodeSetGenerator
new_boundary = 'all'
input = 'generated_mesh'
top_right = '10 0 0'
bottom_left = '0 0 0'
[../]
[]
[Variables]
[./disp_x]
[../]
[]
[AuxVariables]
[./accel_x]
[../]
[./vel_x]
[../]
[]
[AuxKernels]
[./accel_x]
type = TestNewmarkTI
variable = accel_x
displacement = disp_x
first = false
[../]
[./vel_x]
type = TestNewmarkTI
variable = vel_x
displacement = disp_x
[../]
[]
[Kernels]
[./DynamicTensorMechanics]
displacements = 'disp_x'
[../]
[]
[NodalKernels]
[./force_x]
type = UserForcingFunctionNodalKernel
variable = disp_x
boundary = right
function = force_x
[../]
[./nodal_masses]
type = NodalTranslationalInertia
nodal_mass_file = 'nodal_mass_file.csv'
variable = 'disp_x'
boundary = 'all'
[../]
[]
[Functions]
[./force_x]
type = PiecewiseLinear
x = '0.0 1.0 2.0 3.0 4.0' # time
y = '0.0 1.0 0.0 -1.0 0.0' # force
scale_factor = 1e3
[../]
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor_block]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.25
block = 0
[../]
[./strain_block]
type = ComputeIncrementalSmallStrain
block = 0
displacements = 'disp_x'
[../]
[./stress_block]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[]
[Executioner]
type = Transient
start_time = -0.01
end_time = 0.1
dt = 0.005
timestep_tolerance = 2e-10
[./TimeIntegrator]
type = NewmarkBeta
beta = 0.25
gamma = 0.5
[../]
[]
[Postprocessors]
[./accel_x]
type = PointValue
point = '10.0 0.0 0.0'
variable = accel_x
[../]
[]
[Outputs]
exodus = false
csv = true
[]
(modules/tensor_mechanics/test/tests/combined_creep_plasticity/combined_creep_plasticity_start_time.i)
#
# This test is Example 2 from "A Consistent Formulation for the Integration
# of Combined Plasticity and Creep" by P. Duxbury, et al., Int J Numerical
# Methods in Engineering, Vol. 37, pp. 1277-1295, 1994.
#
# The problem is a one-dimensional bar which is loaded from yield to a value of twice
# the initial yield stress and then unloaded to return to the original stress. The
# bar must harden to the required yield stress during the load ramp, with no
# further yielding during unloading. The initial yield stress (sigma_0) is prescribed
# as 20 with a plastic strain hardening of 100. The mesh is a 1x1x1 cube with symmetry
# boundary conditions on three planes to provide a uniaxial stress field.
#
# In the PowerLawCreep model, the creep strain rate is defined by:
#
# edot = A(sigma)**n * exp(-Q/(RT)) * t**m
#
# The creep law specified in the paper, however, defines the creep strain rate as:
#
# edot = Ao * mo * (sigma)**n * t**(mo-1)
# with the creep parameters given by
# Ao = 1e-7
# mo = 0.5
# n = 5
#
# thus, input parameters for the test were specified as:
# A = Ao * mo = 1e-7 * 0.5 = 0.5e-7
# m = mo-1 = -0.5
# n = 5
# Q = 0
#
# The variation of load P with time is:
# P = 20 + 20t 0 < t < 1
# P = 40 - 40(t-1) 1 < t 1.5
#
# The analytic solution for total strain during the loading period 0 < t < 1 is:
#
# e_tot = (sigma_0 + 20*t)/E + 0.2*t + A * t**0.5 * sigma_0**n * [ 1 + (5/3)*t +
# + 2*t**2 + (10/7)*t**3 + (5/9)**t**4 + (1/11)*t**5 ]
#
# and during the unloading period 1 < t < 1.5:
#
# e_tot = (sigma_1 - 40*(t-1))/E + 0.2 + (4672/693) * A * sigma_0**n +
# A * sigma_0**n * [ t**0.5 * ( 32 - (80/3)*t + 16*t**2 - (40/7)*t**3
# + (10/9)*t**4 - (1/11)*t**5 ) - (11531/693) ]
#
# where sigma_1 is the stress at time t = 1.
#
# Assuming a Young's modulus (E) of 1000 and using the parameters defined above:
#
# e_tot(1) = 2.39734
# e_tot(1.5) = 3.16813
#
#
# The numerically computed solution is:
#
# e_tot(1) = 2.39718 (~0.006% error)
# e_tot(1.5) = 3.15555 (~0.40% error)
#
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
incremental = true
add_variables = true
generate_output = 'stress_yy elastic_strain_yy creep_strain_yy plastic_strain_yy'
[../]
[]
[Functions]
[./top_pull]
type = PiecewiseLinear
x = ' 10 11 11.5'
y = '-20 -40 -20'
[../]
[./dts]
type = PiecewiseLinear
x = '10 10.5 11.0 11.5'
y = '0.015 0.015 0.005 0.005'
[../]
[]
[BCs]
[./u_top_pull]
type = Pressure
variable = disp_y
component = 1
boundary = top
factor = 1
function = top_pull
[../]
[./u_bottom_fix]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./u_yz_fix]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./u_xy_fix]
type = DirichletBC
variable = disp_z
boundary = back
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = 0
youngs_modulus = 1e3
poissons_ratio = 0.3
[../]
[./creep_plas]
type = ComputeMultipleInelasticStress
block = 0
tangent_operator = elastic
inelastic_models = 'creep plas'
max_iterations = 50
absolute_tolerance = 1e-05
combined_inelastic_strain_weights = '0.0 1.0'
[../]
[./creep]
type = PowerLawCreepStressUpdate
block = 0
coefficient = 0.5e-7
n_exponent = 5
m_exponent = -0.5
activation_energy = 0
start_time = 10
[../]
[./plas]
type = IsotropicPlasticityStressUpdate
block = 0
hardening_constant = 100
yield_stress = 20
[../]
[]
[Executioner]
type = Transient
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options = '-snes_ksp'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 20
nl_max_its = 6
nl_rel_tol = 1e-6
nl_abs_tol = 1e-10
l_tol = 1e-5
start_time = 10.0
end_time = 11.5
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
exodus = true
[]
(modules/contact/test/tests/verification/hertz_cyl/half_symm_q4/hertz_cyl_half_1deg_template1.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = hertz_cyl_half_1deg.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Functions]
[./disp_ramp_vert]
type = PiecewiseLinear
x = '0. 1. 3.5'
y = '0. -0.0020 -0.0020'
[../]
[./disp_ramp_horz]
type = PiecewiseLinear
x = '0. 1. 3.5'
y = '0. 0.0 0.0014'
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
[../]
[]
[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_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 2
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 2
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 4
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 4
[../]
[./disp_x226]
type = NodalVariableValue
nodeid = 225
variable = disp_x
[../]
[./disp_y226]
type = NodalVariableValue
nodeid = 225
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./side_x]
type = DirichletBC
variable = disp_y
boundary = '1 2'
value = 0.0
[../]
[./bot_y]
type = DirichletBC
variable = disp_x
boundary = '1 2'
value = 0.0
[../]
[./top_y_disp]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = disp_ramp_vert
[../]
[./top_x_disp]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = disp_ramp_horz
[../]
[]
[Materials]
[./stuff1_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e10
poissons_ratio = 0.0
[../]
[./stuff1_strain]
type = ComputeFiniteStrain
block = '1'
[../]
[./stuff1_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./stuff2_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff2_strain]
type = ComputeFiniteStrain
block = '2'
[../]
[./stuff2_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[./stuff3_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '3'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff3_strain]
type = ComputeFiniteStrain
block = '3'
[../]
[./stuff3_stress]
type = ComputeFiniteStrainElasticStress
block = '3'
[../]
[./stuff4_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '4'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff4_strain]
type = ComputeFiniteStrain
block = '4'
[../]
[./stuff4_stress]
type = ComputeFiniteStrainElasticStress
block = '4'
[../]
[./stuff5_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '5'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff5_strain]
type = ComputeFiniteStrain
block = '5'
[../]
[./stuff5_stress]
type = ComputeFiniteStrainElasticStress
block = '5'
[../]
[./stuff6_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '6'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff6_strain]
type = ComputeFiniteStrain
block = '6'
[../]
[./stuff6_stress]
type = ComputeFiniteStrainElasticStress
block = '6'
[../]
[./stuff7_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '7'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff7_strain]
type = ComputeFiniteStrain
block = '7'
[../]
[./stuff7_stress]
type = ComputeFiniteStrainElasticStress
block = '7'
[../]
[]
[Executioner]
type = Transient
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-6
nl_rel_tol = 1e-5
l_max_its = 100
nl_max_its = 200
start_time = 0.0
end_time = 3.5
l_tol = 1e-3
dt = 0.1
dtmin = 0.1
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '3 4'
sort_by = id
[../]
[./y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '3 4'
sort_by = id
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = id
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'x_disp y_disp cont_press'
start_time = 0.9
execute_vector_postprocessors_on = timestep_end
[../]
[./chkfile2]
type = CSV
show = 'bot_react_x bot_react_y disp_x226 disp_y226 top_react_x top_react_y'
start_time = 0.9
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./interface]
primary = 2
secondary = 3
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+10
[../]
[]
(modules/xfem/test/tests/solid_mechanics_basic/square_branch_quad_2d.i)
[GlobalParams]
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[UserObjects]
[./line_seg_cut_uo0]
type = LineSegmentCutUserObject
cut_data = '-1.0000e-10 6.6340e-01 6.6340e-01 -1.0000e-10'
time_start_cut = 0.0
time_end_cut = 1.0
[../]
[./line_seg_cut_uo1]
type = LineSegmentCutUserObject
cut_data = '3.3120e-01 3.3200e-01 1.0001e+00 3.3200e-01'
time_start_cut = 1.0
time_end_cut = 2.0
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
planar_formulation = PLANE_STRAIN
add_variables = true
[../]
[]
[Functions]
[./right_disp_x]
type = PiecewiseLinear
x = '0 1.0 2.0 3.0'
y = '0 0.005 0.01 0.01'
[../]
[./top_disp_y]
type = PiecewiseLinear
x = '0 1.0 2.0 3.0'
y = '0 0.005 0.01 0.01'
[../]
[]
[BCs]
[./right_x]
type = FunctionDirichletBC
boundary = 1
variable = disp_x
function = right_disp_x
[../]
[./top_y]
type = FunctionDirichletBC
boundary = 2
variable = disp_y
function = top_disp_y
[../]
[./bottom_y]
type = DirichletBC
boundary = 0
variable = disp_y
value = 0.0
[../]
[./left_x]
type = DirichletBC
boundary = 3
variable = disp_x
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-16
nl_abs_tol = 1e-10
# time control
start_time = 0.0
dt = 1.0
end_time = 2.2
num_steps = 5000
[]
[Outputs]
file_base = square_branch_quad_2d_out
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/tensor_mechanics/test/tests/temperature_dependent_hardening/temp_dep_hardening.i)
#
# This is a test of the piece-wise linear strain hardening model using the
# small strain formulation. This test exercises the temperature-dependent
# hardening curve capability.
#
# Test procedure:
# 1. The element is pulled to and then beyond the yield stress for a given
# temperature.
# 2. The displacement is then constant while the temperature increases and
# the yield stress decreases. This results in a lower stress with more
# plastic strain.
# 3. The temperature decreases beyond its original value giving a higher
# yield stress. The displacement increases, causing increases stress to
# the new yield stress.
# 4. The temperature and yield stress are constant with increasing
# displacement giving a constant stress and more plastic strain.
#
# Plotting total_strain_yy on the x axis and stress_yy on the y axis shows
# the stress history in a clear way.
#
# s |
# t | *****
# r | *
# e | ***** *
# s | * * *
# s | * *
# |*
# +------------------
# total strain
#
# The exact same problem was run in Abaqus with exactly the same result.
[Mesh]
type = GeneratedMesh
dim = 3
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]
displacements = 'disp_x disp_y disp_z'
[]
[AuxVariables]
[./temp]
order = FIRST
family = LAGRANGE
initial_condition = 500.0
[../]
[]
[AuxKernels]
[./temp_aux]
type = FunctionAux
variable = temp
function = temp_hist
[../]
[]
[Functions]
[./top_pull]
type = PiecewiseLinear
x = '0 1 2 4 5 6'
y = '0 0.025 0.05 0.05 0.06 0.085'
[../]
[./hf1]
type = PiecewiseLinear
x = '0.0 0.01 0.02 0.03 0.1'
y = '5000 5030 5060 5090 5300'
[../]
[./hf2]
type = PiecewiseLinear
x = '0.0 0.01 0.02 0.03 0.1'
y = '4000 4020 4040 4060 4200'
[../]
[./temp_hist]
type = PiecewiseLinear
x = '0 1 2 3 4'
y = '500 500 500 600 400'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
incremental = true
add_variables = true
generate_output = 'stress_yy strain_yy plastic_strain_xx plastic_strain_yy plastic_strain_zz'
[../]
[]
[BCs]
[./y_pull_function]
type = FunctionDirichletBC
variable = disp_y
boundary = 3
function = top_pull
[../]
[./x_bot]
type = DirichletBC
variable = disp_x
boundary = 4
value = 0.0
[../]
[./y_bot]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./z_bot]
type = DirichletBC
variable = disp_z
boundary = 0
value = 0.0
[../]
[]
[Postprocessors]
[./stress_yy_el]
type = ElementalVariableValue
variable = stress_yy
elementid = 0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 2e5
poissons_ratio = 0.3
[../]
[./temp_dep_hardening]
type = TemperatureDependentHardeningStressUpdate
hardening_functions = 'hf1 hf2'
temperatures = '300.0 800.0'
relative_tolerance = 1e-25
absolute_tolerance = 1e-5
temperature = temp
[../]
[./radial_return_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'temp_dep_hardening'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 4'
line_search = 'none'
l_max_its = 100
nl_max_its = 100
nl_rel_tol = 1e-12
nl_abs_tol = 1e-10
l_tol = 1e-9
start_time = 0.0
end_time = 6
dt = 0.1
[]
[Outputs]
[./out]
type = Exodus
[../]
[]
(modules/combined/test/tests/adaptive_timestepping/adapt_tstep_function_change_restart1.i)
# This is a test designed to evaluate the cabability of the
# IterationAdaptiveDT TimeStepper to adjust time step size according to
# a function. For example, if the power input function for a BISON
# simulation rapidly increases or decreases, the IterationAdaptiveDT
# TimeStepper should take time steps small enough to capture the
# oscillation.
[GlobalParams]
order = FIRST
family = LAGRANGE
block = 1
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
file = 1hex8_10mm_cube.e
[]
[Functions]
[./Fiss_Function]
type = PiecewiseLinear
x = '0 1e6 2e6 2.001e6 2.002e6'
y = '0 3e8 3e8 12e8 0'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[./temp]
initial_condition = 300.0
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
incremental = true
volumetric_locking_correction = true
eigenstrain_names = thermal_expansion
decomposition_method = EigenSolution
add_variables = true
generate_output = 'vonmises_stress'
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[./heat_ie]
type = HeatConductionTimeDerivative
variable = temp
[../]
[./heat_source]
type = HeatSource
variable = temp
value = 1.0
function = Fiss_Function
[../]
[]
[BCs]
[./bottom_temp]
type = DirichletBC
variable = temp
boundary = 1
value = 300
[../]
[./top_bottom_disp_x]
type = DirichletBC
variable = disp_x
boundary = '1'
value = 0
[../]
[./top_bottom_disp_y]
type = DirichletBC
variable = disp_y
boundary = '1'
value = 0
[../]
[./top_bottom_disp_z]
type = DirichletBC
variable = disp_z
boundary = '1'
value = 0
[../]
[]
[Materials]
[./thermal]
type = HeatConductionMaterial
temp = temp
specific_heat = 1.0
thermal_conductivity = 1.0
[../]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 300e6
poissons_ratio = .3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[./thermal_expansion]
type = ComputeThermalExpansionEigenstrain
thermal_expansion_coeff = 5e-6
stress_free_temperature = 300.0
temperature = temp
eigenstrain_name = thermal_expansion
[../]
[./density]
type = Density
density = 10963.0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
verbose = true
nl_abs_tol = 1e-10
start_time = 0.0
num_steps = 65
end_time = 2.002e6
[./TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_function = Fiss_Function
max_function_change = 3e7
dt = 1e6
[../]
[]
[Postprocessors]
[./Temperature_of_Block]
type = ElementAverageValue
variable = temp
execute_on = 'initial timestep_end'
[../]
[./vonMises]
type = ElementAverageValue
variable = vonmises_stress
execute_on = 'initial timestep_end'
[../]
[]
[Outputs]
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 10
[../]
[./checkpoint]
type = Checkpoint
num_files = 1
[../]
[]
(modules/xfem/test/tests/second_order_elements/diffusion_3d_hex20.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 3
ny = 4
nz = 2
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
zmin = 0.0
zmax = 0.2
elem_type = HEX20
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./square_planar_cut_uo]
type = RectangleCutUserObject
cut_data = ' 0.35 1.01 -0.001
0.35 0.49 -0.001
0.35 0.49 0.201
0.35 1.01 0.201'
[../]
[]
[Variables]
[./u]
[../]
[]
[Functions]
[./u_left]
type = PiecewiseLinear
x = '0 2'
y = '0 0.1'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = FunctionDirichletBC
variable = u
boundary = left
function = u_left
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 0
[../]
[]
[Executioner]
type = Transient
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
start_time = 0.0
dt = 1.0
end_time = 1.0
[]
[Outputs]
interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/combined/test/tests/thermo_mech/ad-youngs_modulus_function_temp.i)
# ---------------------------------------------------------------------------
# This test is designed to verify the variable elasticity tensor functionality in the
# ADComputeFiniteStrainElasticStress class with the elasticity_tensor_has_changed flag
# by varying the young's modulus with temperature. A constant strain is applied
# to the mesh in this case, and the stress varies with the changing elastic constants.
#
# Geometry: A single element cube in symmetry boundary conditions and pulled
# at a constant displacement to create a constant strain in the x-direction.
#
# Temperature: The temperature varies from 400K to 700K in this simulation by
# 100K each time step. The temperature is held constant in the last
# timestep to ensure that the elasticity tensor components are constant
# under constant temperature.
#
# Results: Because Poisson's ratio is set to zero, only the stress along the x
# axis is non-zero. The stress changes with temperature.
#
# Temperature(K) strain_{xx}(m/m) Young's Modulus(Pa) stress_{xx}(Pa)
# 400 0.001 10.0e6 1.0e4
# 500 0.001 10.0e6 1.0e4
# 600 0.001 9.94e6 9.94e3
# 700 0.001 9.93e6 9.93e3
#
# The tensor mechanics results align exactly with the analytical results above
# when this test is run with ComputeIncrementalSmallStrain. When the test is
# run with ComputeFiniteStrain, a 0.05% discrepancy between the analytical
# strains and the simulation strain results is observed, and this discrepancy
# is carried over into the calculation of the elastic stress.
#-------------------------------------------------------------------------
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[./temp]
initial_condition = 400
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./temperature_function]
type = PiecewiseLinear
x = '1 4'
y = '400 700'
[../]
[]
[Kernels]
[./heat]
type = ADDiffusion
variable = temp
[../]
[./TensorMechanics]
use_displaced_mesh = true
use_automatic_differentiation = true
[../]
[]
[AuxKernels]
[./stress_xx]
type = ADRankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
[../]
[./elastic_strain_xx]
type = ADRankTwoAux
rank_two_tensor = elastic_strain
variable = elastic_strain_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[]
[BCs]
[./u_left_fix]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./u_bottom_fix]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./u_back_fix]
type = DirichletBC
variable = disp_z
boundary = back
value = 0.0
[../]
[./u_pull_right]
type = DirichletBC
variable = disp_x
boundary = right
value = 0.001
[../]
[./temp_bc_1]
type = ADFunctionDirichletBC
variable = temp
preset = false
boundary = '1 2 3 4'
function = temperature_function
[../]
[]
[Materials]
[./youngs_modulus]
type = ADPiecewiseLinearInterpolationMaterial
xy_data = '0 10e+6
599.9999 10e+6
600 9.94e+6
99900 10e3'
property = youngs_modulus
variable = temp
[../]
[./elasticity_tensor]
type = ADComputeVariableIsotropicElasticityTensor
youngs_modulus = youngs_modulus
poissons_ratio = 0.0
[../]
[./strain]
type = ADComputeIncrementalSmallStrain
[../]
[./stress]
type = ADComputeFiniteStrainElasticStress
[../]
[]
[Preconditioning]
[./full]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
end_time = 5
[]
[Postprocessors]
[./elastic_strain_xx]
type = ElementAverageValue
variable = elastic_strain_xx
[../]
[./elastic_stress_xx]
type = ElementAverageValue
variable = stress_xx
[../]
[./temp]
type = AverageNodalVariableValue
variable = temp
[../]
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/ad_smeared_cracking/cracking_xyz.i)
#
[Mesh]
file = cracking_test.e
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Functions]
[./displx]
type = PiecewiseLinear
x = '0 1'
y = '0 0.00175'
[../]
[./velocity_y]
type = ParsedFunction
value = 'if(t < 2, 0.00175, 0)'
[../]
[./velocity_z]
type = ParsedFunction
value = 0.00175
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx'
use_automatic_differentiation = true
[../]
[]
[BCs]
[./fix_x]
type = ADDirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./move_x]
type = ADFunctionDirichletBC
variable = disp_x
boundary = 4
function = displx
[../]
[./fix_y]
type = ADDirichletBC
variable = disp_y
boundary = 2
value = 0.0
[../]
[./move_y]
type = PresetVelocity
variable = disp_y
boundary = 5
function = velocity_y
# time_periods = 'p2 p3'
[../]
[./fix_z]
type = ADDirichletBC
variable = disp_z
boundary = 3
value = 0.0
[../]
[./move_z]
type = PresetVelocity
variable = disp_z
boundary = 6
function = velocity_z
# time_periods = 'p3'
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 186.5e9
poissons_ratio = .316
[../]
[./elastic_stress]
type = ADComputeSmearedCrackingStress
cracking_stress = 119.3e6
softening_models = exponential_softening
[../]
[./exponential_softening]
type = ADExponentialSoftening
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
petsc_options_iname = '-ksp_gmres_restart -pc_type'
petsc_options_value = '101 lu'
line_search = 'none'
l_max_its = 100
l_tol = 1e-5
nl_max_its = 100
nl_abs_tol = 1e-4
#nl_rel_tol = 1e-4
nl_rel_tol = 1e-6
start_time = 0.0
end_time = 3.0
dt = 0.01
[]
[Controls]
[./p1]
type = TimePeriod
start_time = 0.0
end_time = 1.0
disable_objects = 'BCs/move_y BCs/move_z'
reverse_on_false = false
execute_on = 'initial timestep_begin'
[../]
[./p2]
type = TimePeriod
start_time = 1.0
end_time = 2.0
disable_objects = 'BCs/move_z'
enable_objects = 'BCs/move_y'
reverse_on_false = false
execute_on = 'initial timestep_begin'
[../]
[./p3]
type = TimePeriod
start_time = 2.0
end_time = 3.0
enable_objects = 'BCs/move_y BCs/move_z'
reverse_on_false = false
execute_on = 'initial timestep_begin'
set_sync_times = true
[../]
[]
[Outputs]
exodus = true
[]
(modules/contact/test/tests/glued/glued_contact_mechanical_constraint_test.i)
# This is a mechanical constraint (contact formulation) version of glued_contact_mechanical_constraint.i
[Mesh]
file = glued_contact_test.e
[]
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y disp_z'
[]
[Functions]
[./up]
type = PiecewiseLinear
x = '0 1'
y = '0 0.5001'
[../]
[./lateral]
type = PiecewiseLinear
x = '0 1 2 3'
y = '0 0 1 0'
scale_factor = 0.5
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
[../]
[]
[Contact]
[./dummy_name]
primary = 2
secondary = 3
penalty = 1e6
model = glued
formulation = kinematic
[../]
[]
[BCs]
[./bottom_lateral]
type = FunctionDirichletBC
variable = disp_x
boundary = 1
function = lateral
[../]
[./bottom_up]
type = FunctionDirichletBC
variable = disp_y
boundary = 1
function = up
[../]
[./bottom_out]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0.0
[../]
[./top]
type = DirichletBC
variable = disp_y
boundary = 4
value = 0.0
[../]
[]
[Materials]
[./stiffStuff1]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stiffStuff1_strain]
type= ComputeFiniteStrain
block = '1'
[../]
[./stiffStuff1_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./stiffStuff2]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stiffStuff2_strain]
type= ComputeFiniteStrain
block = '2'
[../]
[./stiffStuff2_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
#petsc_options_iname = '-pc_type -pc_hypre_type -snes_type -snes_ls -snes_linesearch_type -ksp_gmres_restart'
#petsc_options_value = 'hypre boomeramg ls basic basic 101'
petsc_options_iname = '-pc_type -ksp_gmres_restart'
petsc_options_value = 'ilu 101'
line_search = 'none'
nl_abs_tol = 1e-8
nl_rel_tol = 1e-8
l_tol = 1e-4
l_max_its = 100
nl_max_its = 10
dt = 0.1
num_steps = 30
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
[]
[Postprocessors]
active = ''
[./resid]
type = Residual
[../]
[./iters]
type = NumNonlinearIterations
[../]
[]
[Outputs]
file_base = mechanical_constraint_out
exodus = true
[]
(test/tests/geomsearch/3d_moving_penetration/pl_test4q.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
file = pl_test4q.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./normal_z]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./closest_point_z]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[./diff_z]
type = Diffusion
variable = disp_z
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = normal_z
boundary = 11
paired_boundary = 12
quantity = normal_z
[../]
[./penetrate10]
type = PenetrationAux
variable = normal_z
boundary = 12
paired_boundary = 11
quantity = normal_z
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate13]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate14]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate15]
type = PenetrationAux
variable = closest_point_z
boundary = 11
paired_boundary = 12
quantity = closest_point_z
[../]
[./penetrate16]
type = PenetrationAux
variable = closest_point_z
boundary = 12
paired_boundary = 11
quantity = closest_point_z
[../]
[./penetrate17]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate18]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate19]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate20]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b1z]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[./b2z]
type = DirichletBC
variable = disp_z
boundary = 2
value = 0
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-9
l_max_its = 10
start_time = 0.0
dt = 0.025
end_time = 1.0
[./Quadrature]
order = THIRD
[../]
[]
[Outputs]
file_base = pl_test4q_out
exodus = true
[]
(modules/richards/test/tests/gravity_head_2/ghQ2P_pgas.i)
# quick two phase with Pgas and Swater being variables
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
xmin = 0
xmax = 1
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1E-2 1E-1 1E0 1E1 1E3 1E4 1E5 1E6 1E7'
x = '0 1E-1 1E0 1E1 1E2 1E3 1E4 1E5 1E6'
[../]
[]
[UserObjects]
[./DensityWater]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0E2
[../]
[./DensityGas]
type = RichardsDensityConstBulk
dens0 = 0.5
bulk_mod = 0.5E2
[../]
[./RelPermWater]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./RelPermGas]
type = Q2PRelPermPowerGas
simm = 0.0
n = 3
[../]
[]
[Variables]
[./pgas]
[../]
[./swater]
[../]
[]
[ICs]
[./pp_ic]
type = ConstantIC
value = 1
variable = pgas
[../]
[./sat_ic]
type = ConstantIC
value = 0.5
variable = swater
[../]
[]
[Q2P]
porepressure = pgas
saturation = swater
water_density = DensityWater
water_relperm = RelPermWater
water_viscosity = 1
gas_density = DensityGas
gas_relperm = RelPermGas
gas_viscosity = 1
diffusivity = 0
[]
[Postprocessors]
[./pp_left]
type = PointValue
point = '0 0 0'
variable = pgas
[../]
[./pp_right]
type = PointValue
point = '1 0 0'
variable = pgas
[../]
[./sat_left]
type = PointValue
point = '0 0 0'
variable = swater
[../]
[./sat_right]
type = PointValue
point = '1 0 0'
variable = swater
[../]
[]
[Materials]
[./rock]
type = Q2PMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
gravity = '-1 0 0'
[../]
[]
[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-10 1E-10 10000'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
end_time = 1E6
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = ghQ2P_pgas
csv = true
exodus = true
[]
(modules/tensor_mechanics/test/tests/j_integral/j_integral_3d_as_2d.i)
#This tests the J-Integral evaluation capability.
#This is a 3d extrusion of a 2d plane strain model with one element
#through the thickness, and calculates the J-Integrals using options
#to treat it as 2d.
#The analytic solution for J1 is 2.434. This model
#converges to that solution with a refined mesh.
#Reference: National Agency for Finite Element Methods and Standards (U.K.):
#Test 1.1 from NAFEMS publication "Test Cases in Linear Elastic Fracture
#Mechanics" R0020.
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[Mesh]
file = crack_3d_as_2d.e
partitioner = centroid
centroid_partitioner_direction = z
[]
[AuxVariables]
[./SED]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./rampConstant]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = -1e2
[../]
[]
[DomainIntegral]
integrals = JIntegral
boundary = 800
crack_direction_method = CrackDirectionVector
crack_direction_vector = '1 0 0'
2d = true
axis_2d = 2
radius_inner = '4.0 4.5 5.0 5.5 6.0'
radius_outer = '4.5 5.0 5.5 6.0 6.5'
output_q = false
incremental = true
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
[../]
[]
[AuxKernels]
[./SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[../]
[]
[BCs]
[./crack_y]
type = DirichletBC
variable = disp_y
boundary = 100
value = 0.0
[../]
[./no_z]
type = DirichletBC
variable = disp_z
boundary = 500
value = 0.0
[../]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 700
value = 0.0
[../]
[./Pressure]
[./Side1]
boundary = 400
function = rampConstant
[../]
[../]
[] # BCs
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
# Two sets of linesearch options are for petsc 3.1 and 3.3 respectively
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_abs_tol = 1e-5
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Outputs]
file_base = j_integral_3d_as_2d_out
exodus = true
csv = true
[]
(modules/tensor_mechanics/test/tests/smeared_cracking/cracking_exponential.i)
#
# Test to exercise the exponential stress release
#
# Stress vs. strain should show a linear relationship until cracking,
# an exponential stress release, a linear relationship back to zero
# strain, a linear relationship with the original stiffness in
# compression and then back to zero strain, a linear relationship
# back to the exponential curve, and finally further exponential
# stress release.
#
[Mesh]
file = cracking_test.e
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Functions]
[./displx]
type = PiecewiseLinear
x = '0 1 2 3 4 5 6'
y = '0 0.00175 0 -0.0001 0 0.00175 0.0035'
[../]
[./disply]
type = PiecewiseLinear
x = '0 5 6'
y = '0 0 .00175'
[../]
[./displz]
type = PiecewiseLinear
x = '0 2 3'
y = '0 0 .0035'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx'
[../]
[]
[BCs]
[./pullx]
type = FunctionDirichletBC
#type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = displx
[../]
[./left]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./fix_y]
type = DirichletBC
variable = disp_y
boundary = '11 12'
value = 0.0
[../]
[./move_y]
type = FunctionDirichletBC
variable = disp_y
boundary = '15 16'
function = disply
[../]
[./back]
type = DirichletBC
variable = disp_z
boundary = '3'
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 186.5e9
poissons_ratio = .316
[../]
[./elastic_stress]
type = ComputeSmearedCrackingStress
cracking_stress = 119.3e6
softening_models = exponential_softening
[../]
[./exponential_softening]
type = ExponentialSoftening
[../]
[]
[Executioner]
type = Transient
petsc_options_iname = '-ksp_gmres_restart -pc_type'
petsc_options_value = '101 lu'
line_search = 'none'
l_max_its = 100
l_tol = 1e-6
nl_max_its = 10
nl_rel_tol = 1e-12
nl_abs_tol = 1.e-4
start_time = 0.0
dt = 0.02
dtmin = 0.02
num_steps = 300
[]
[Outputs]
exodus = true
[]
(test/tests/time_steppers/iteration_adaptive/hit_function_knot.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 50
ny = 2
xmax = 5
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
[./knot]
type = PiecewiseLinear
x = '0 1 2'
y = '0 0 0'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./dt]
type = TimeDerivative
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 10
[../]
[./right]
type = NeumannBC
variable = u
boundary = right
value = -1
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
start_time = 0.0
end_time = 2.0
timestep_tolerance = 0.3
verbose = true
[./TimeStepper]
type = IterationAdaptiveDT
dt = 0.9
optimal_iterations = 10
[../]
[]
[Postprocessors]
[./_dt]
type = TimestepSize
[../]
[]
[Outputs]
exodus = true
[]
(modules/combined/test/tests/axisymmetric_2d3d_solution_function/2d.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Problem]
coord_type = RZ
[]
[Mesh]
file = 2d.e
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./temp]
initial_condition = 400
[../]
[]
[AuxVariables]
[./hoop_stress]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./temp_inner_func]
type = PiecewiseLinear
xy_data = '0 400
1 350'
[../]
[./temp_outer_func]
type = PiecewiseLinear
xy_data = '0 400
1 400'
[../]
[./press_func]
type = PiecewiseLinear
xy_data = '0 15
1 15'
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
volumetric_locking_correction = true
add_variables = true
incremental = true
strain = FINITE
eigenstrain_names = thermal_expansion
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress hydrostatic_stress'
[../]
[]
[AuxKernels]
[./hoop_stress]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = hoop_stress
scalar_type = HoopStress
execute_on = timestep_end
[../]
[]
[BCs]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = '1'
value = 0.0
[../]
[./Pressure]
[./internal_pressure]
boundary = '4'
factor = 1.e6
function = press_func
[../]
[../]
[./t_in]
type = FunctionDirichletBC
variable = temp
boundary = '4'
function = temp_inner_func
[../]
[./t_out]
type = FunctionDirichletBC
variable = temp
boundary = '2'
function = temp_outer_func
[../]
[]
[Constraints]
[./disp_y]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = '65'
secondary = '3'
penalty = 1e18
[../]
[]
[Materials]
[./thermal1]
type = HeatConductionMaterial
block = '1'
thermal_conductivity = 25.0
specific_heat = 490.0
temp = temp
[../]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 193.05e9
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[./thermal_expansion]
type = ComputeThermalExpansionEigenstrain
thermal_expansion_coeff = 13e-6
stress_free_temperature = 295.00
temperature = temp
eigenstrain_name = thermal_expansion
[../]
[./density]
type = Density
block = '1'
density = 8000.0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-ksp_snes_ew'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = ' 201 hypre boomeramg 4'
line_search = 'none'
l_max_its = 25
nl_max_its = 20
nl_rel_tol = 1e-9
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 1
dtmin = 1
[]
[Outputs]
file_base = 2d_out
exodus = true
[./console]
type = Console
max_rows = 25
[../]
[]
(test/tests/geomsearch/3d_moving_penetration_smoothing/pl_test3ns.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
file = pl_test3.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./normal_z]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./closest_point_z]
[../]
# [./element_id]
# [../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[./diff_z]
type = Diffusion
variable = disp_z
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
normal_smoothing_distance = 0.2
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
normal_smoothing_distance = 0.2
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = normal_z
boundary = 11
paired_boundary = 12
quantity = normal_z
[../]
[./penetrate10]
type = PenetrationAux
variable = normal_z
boundary = 12
paired_boundary = 11
quantity = normal_z
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate13]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate14]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate15]
type = PenetrationAux
variable = closest_point_z
boundary = 11
paired_boundary = 12
quantity = closest_point_z
[../]
[./penetrate16]
type = PenetrationAux
variable = closest_point_z
boundary = 12
paired_boundary = 11
quantity = closest_point_z
[../]
# [./penetrate17]
# type = PenetrationAux
# variable = element_id
# boundary = 11
# paired_boundary = 12
# quantity = element_id
# [../]
#
# [./penetrate18]
# type = PenetrationAux
# variable = element_id
# boundary = 12
# paired_boundary = 11
# quantity = element_id
# [../]
[./penetrate19]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate20]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
preset = false
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
preset = false
boundary = 1
value = 0
[../]
[./b1z]
type = DirichletBC
variable = disp_z
preset = false
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
preset = false
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
preset = false
boundary = 2
function = disp_y
[../]
[./b2z]
type = DirichletBC
variable = disp_z
preset = false
boundary = 2
value = 0
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-9
l_max_its = 10
start_time = 0.0
dt = 0.02
end_time = 1.0
[]
[Outputs]
file_base = pl_test3ns_out
exodus = true
[]
(modules/tensor_mechanics/test/tests/strain_energy_density/rate_model.i)
# Single element test to check the strain energy density calculation
[GlobalParams]
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
xmin = 0
xmax = 1
ymin = 0
ymax = 2
[]
[AuxVariables]
[./SERD]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./rampConstantUp]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = -100
[../]
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress strain_xx strain_yy strain_zz'
planar_formulation = PLANE_STRAIN
[../]
[]
[AuxKernels]
[./SERD]
type = MaterialRealAux
variable = SERD
property = strain_energy_rate_density
execute_on = timestep_end
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 'left'
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = 'bottom'
value = 0.0
[../]
[./Pressure]
[./top]
boundary = 'top'
function = rampConstantUp
[../]
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 206800
poissons_ratio = 0.0
[../]
[./radial_return_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'powerlawcrp'
[../]
[./powerlawcrp]
type = PowerLawCreepStressUpdate
coefficient = 3.125e-21 # 7.04e-17 #
n_exponent = 4.0
m_exponent = 0.0
activation_energy = 0.0
# max_inelastic_increment = 0.01
[../]
[./strain_energy_rate_density]
type = StrainEnergyRateDensity
inelastic_models = 'powerlawcrp'
[../]
[]
[Executioner]
type = Transient
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 4'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_abs_tol = 3e-7
nl_rel_tol = 1e-12
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Postprocessors]
[./epxx]
type = ElementalVariableValue
variable = strain_xx
elementid = 0
[../]
[./epyy]
type = ElementalVariableValue
variable = strain_yy
elementid = 0
[../]
[./epzz]
type = ElementalVariableValue
variable = strain_zz
elementid = 0
[../]
[./sigxx]
type = ElementAverageValue
variable = stress_xx
[../]
[./sigyy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigzz]
type = ElementAverageValue
variable = stress_zz
[../]
[./SERD]
type = ElementAverageValue
variable = SERD
[../]
[]
[Outputs]
exodus = true
csv = true
[]
(modules/tensor_mechanics/test/tests/ad_smeared_cracking/cracking_exponential.i)
#
# Test to exercise the exponential stress release
#
# Stress vs. strain should show a linear relationship until cracking,
# an exponential stress release, a linear relationship back to zero
# strain, a linear relationship with the original stiffness in
# compression and then back to zero strain, a linear relationship
# back to the exponential curve, and finally further exponential
# stress release.
#
[Mesh]
file = cracking_test.e
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Functions]
[./displx]
type = PiecewiseLinear
x = '0 1 2 3 4 5 6'
y = '0 0.00175 0 -0.0001 0 0.00175 0.0035'
[../]
[./disply]
type = PiecewiseLinear
x = '0 5 6'
y = '0 0 .00175'
[../]
[./displz]
type = PiecewiseLinear
x = '0 2 3'
y = '0 0 .0035'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx'
use_automatic_differentiation = true
[../]
[]
[BCs]
[./pullx]
type = ADFunctionDirichletBC
variable = disp_x
boundary = 4
function = displx
[../]
[./left]
type = ADDirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./fix_y]
type = ADDirichletBC
variable = disp_y
boundary = '11 12'
value = 0.0
[../]
[./move_y]
type = ADFunctionDirichletBC
variable = disp_y
boundary = '15 16'
function = disply
[../]
[./back]
type = ADDirichletBC
variable = disp_z
boundary = '3'
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 186.5e9
poissons_ratio = .316
[../]
[./elastic_stress]
type = ADComputeSmearedCrackingStress
cracking_stress = 119.3e6
softening_models = exponential_softening
[../]
[./exponential_softening]
type = ADExponentialSoftening
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
petsc_options_iname = '-ksp_gmres_restart -pc_type'
petsc_options_value = '101 lu'
line_search = 'none'
l_max_its = 100
l_tol = 1e-6
nl_max_its = 10
nl_rel_tol = 1e-12
nl_abs_tol = 1.e-4
start_time = 0.0
dt = 0.02
dtmin = 0.02
num_steps = 300
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/central_difference/consistent/2D/2d_consistent_explicit.i)
# Test for the central difference time integrator for a 2D mesh
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 2
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 2.0
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./vel_x]
[../]
[./accel_x]
[../]
[./vel_y]
[../]
[./accel_y]
[../]
[]
[Kernels]
[./DynamicTensorMechanics]
displacements = 'disp_x disp_y'
[../]
[./inertia_x]
type = InertialForce
variable = disp_x
[../]
[./inertia_y]
type = InertialForce
variable = disp_y
[../]
[]
[AuxKernels]
[./accel_x]
type = TestNewmarkTI
variable = accel_x
displacement = disp_x
first = false
[../]
[./vel_x]
type = TestNewmarkTI
variable = vel_x
displacement = disp_x
[../]
[./accel_y]
type = TestNewmarkTI
variable = accel_y
displacement = disp_y
first = false
[../]
[./vel_y]
type = TestNewmarkTI
variable = vel_y
displacement = disp_y
[../]
[]
[BCs]
[./y_bot]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./x_bot]
type = FunctionDirichletBC
boundary = bottom
variable = disp_x
function = disp
preset = false
[../]
[]
[Functions]
[./disp]
type = PiecewiseLinear
x = '0.0 1.0 2.0 3.0 4.0' # time
y = '0.0 1.0 0.0 -1.0 0.0' # displacement
[../]
[]
[Materials]
[./elasticity_tensor_block]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.25
block = 0
[../]
[./strain_block]
type = ComputeIncrementalSmallStrain
block = 0
displacements = 'disp_x disp_y'
implicit = false
[../]
[./stress_block]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = density
prop_values = 1e4
[../]
[]
[Executioner]
type = Transient
start_time = 0
end_time = 0.1
dt = 0.005
timestep_tolerance = 1e-6
[./TimeIntegrator]
type = CentralDifference
[../]
[]
[Postprocessors]
[./_dt]
type = TimestepSize
[../]
[./accel_2x]
type = PointValue
point = '1.0 2.0 0.0'
variable = accel_x
[../]
[./accel_2y]
type = PointValue
point = '1.0 2.0 0.0'
variable = accel_y
[../]
[]
[Outputs]
exodus = false
csv = true
[]
(modules/richards/test/tests/gravity_head_2/gh_lumped_18.i)
# with immobile saturation
# unsaturated = true
# gravity = true
# supg = true
# transient = true
# lumped = true
[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'
viscosity = '1E-3 0.5E-3'
gravity = '-1 0 0'
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1E-2 1E-1 1E0 0.5E1 0.5E2 0.4E4 1E5 1E6 1E7'
x = '0 1E-1 1E0 1E1 1E2 1E3 1E4 1E5 1E6'
[../]
[]
[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 = 0.4
n = 2
[../]
[./RelPermGas]
type = RichardsRelPermPower
simm = 0.3
n = 2
[../]
[./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-5
[../]
[./SUPGgas]
type = RichardsSUPGstandard
p_SUPG = 1E-5
[../]
[]
[Variables]
[./pwater]
order = FIRST
family = LAGRANGE
[../]
[./pgas]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./water_ic]
type = ConstantIC
value = 1
variable = pwater
[../]
[./gas_ic]
type = ConstantIC
value = 2
variable = pgas
[../]
[]
[Kernels]
active = 'richardsfwater richardstwater richardsfgas richardstgas'
[./richardstwater]
type = RichardsLumpedMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFlux
variable = pwater
[../]
[./richardstgas]
type = RichardsLumpedMassChange
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
[../]
[./mass_error_gas]
type = FunctionValuePostprocessor
function = fcn_mass_error_g
[../]
[./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((-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'
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-10 1E-10 10'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
end_time = 1E6
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = gh_lumped_18
execute_on = 'timestep_end final'
interval = 100000
exodus = true
[]
(modules/combined/test/tests/combined_plasticity_temperature/plasticity_temperature_dep_yield.i)
#
# This is a test of the piece-wise linear strain hardening model using the
# small strain formulation. This test exercises the temperature-dependent
# yield stress.
#
# Test procedure:
# 1. The element is pulled to and then beyond the yield stress for a given
# temperature.
# 2. The displacement is then constant while the temperature increases and
# the yield stress decreases. This results in a lower stress with more
# plastic strain.
# 3. The temperature decreases beyond its original value giving a higher
# yield stress. The displacement increases, causing increases stress to
# the new yield stress.
# 4. The temperature and yield stress are constant with increasing
# displacement giving a constant stress and more plastic strain.
#
# Plotting total_strain_yy on the x axis and stress_yy on the y axis shows
# the stress history in a clear way.
#
# s |
# t | *****
# r | *
# e | ***** *
# s | * * *
# s | * *
# |*
# +------------------
# total strain
#
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
incremental = true
add_variables = true
generate_output = 'stress_yy plastic_strain_xx plastic_strain_yy plastic_strain_zz'
[../]
[]
[Variables]
[./temp]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
[./top_pull]
type = PiecewiseLinear
x = '0 1 2 4 5 6'
y = '0 0.025 0.05 0.05 0.06 0.085'
[../]
[./yield]
type = PiecewiseLinear
x = '400 500 600'
y = '6e3 5e3 4e3'
[../]
[./temp]
type = PiecewiseLinear
x = '0 1 2 3 4'
y = '500 500 500 600 400'
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[]
[BCs]
[./y_pull_function]
type = FunctionDirichletBC
variable = disp_y
boundary = top
function = top_pull
[../]
[./x_bot]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./y_bot]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./z_bot]
type = DirichletBC
variable = disp_z
boundary = back
value = 0.0
[../]
[./temp]
type = FunctionDirichletBC
variable = temp
function = temp
boundary = left
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = 0
youngs_modulus = 2.0e5
poissons_ratio = 0.3
[../]
[./creep_plas]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
block = 0
inelastic_models = 'plasticity'
max_iterations = 50
absolute_tolerance = 1e-05
[../]
[./plasticity]
type = IsotropicPlasticityStressUpdate
block = 0
hardening_constant = 0
yield_stress_function = yield
temperature = temp
[../]
[./heat_conduction]
type = HeatConductionMaterial
block = 0
specific_heat = 1
thermal_conductivity = 1
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 4'
line_search = 'none'
l_max_its = 100
nl_max_its = 100
nl_rel_tol = 1e-12
nl_abs_tol = 1e-10
l_tol = 1e-9
start_time = 0.0
end_time = 6
dt = 0.1
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/j_integral/j_integral_3d.i)
#This tests the J-Integral evaluation capability.
#This is a 3d extrusion of a 2d plane strain model with 2 elements
#through the thickness, and calculates the J-Integrals using options
#to treat it as 3d.
#The analytic solution for J1 is 2.434. This model
#converges to that solution with a refined mesh.
#Reference: National Agency for Finite Element Methods and Standards (U.K.):
#Test 1.1 from NAFEMS publication "Test Cases in Linear Elastic Fracture
#Mechanics" R0020.
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[Mesh]
file = crack3d.e
[]
[AuxVariables]
[./SED]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./rampConstant]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = -1e2
[../]
[]
[DomainIntegral]
integrals = JIntegral
boundary = 800
crack_direction_method = CrackDirectionVector
crack_direction_vector = '1 0 0'
radius_inner = '4.0 5.5'
radius_outer = '5.5 7.0'
output_variable = 'disp_x'
output_q = false
incremental = true
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
[../]
[]
[AuxKernels]
[./SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[../]
[]
[BCs]
[./crack_y]
type = DirichletBC
variable = disp_y
boundary = 100
value = 0.0
[../]
[./no_z]
type = DirichletBC
variable = disp_z
boundary = 500
value = 0.0
[../]
[./no_z2]
type = DirichletBC
variable = disp_z
boundary = 510
value = 0.0
[../]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 700
value = 0.0
[../]
[./Pressure]
[./Side1]
boundary = 400
function = rampConstant
[../]
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_abs_tol = 1e-5
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Postprocessors]
[./disp_x_centercrack]
type = CrackFrontData
crack_front_definition = crackFrontDefinition
variable = disp_x
crack_front_point_index = 1
[../]
[]
[Outputs]
file_base = j_integral_3d_out
exodus = true
csv = true
[]
(modules/fsi/test/tests/fsi_acoustics/1D_struc_acoustic/1D_struc_acoustic.i)
# Test for `StructureAcousticInterface` interface kernel. The domain is 1D with 20m
# length. The fluid domain is on the right and the structural domain is on the left.
# Fluid end is subjected to a 250Hz sine wave with a single peak of amplitude unity.
# Structural domain is 4 times as dense as the fluid domain with all other material
# properties being the same. Fluid pressure is recorded at the midpoint in the fluid
# domain (i.e., at 15m). Structural stress is recorded at the midpoint in the structural
# domain (i.e., at 5m). The recorded pressure and stress amplitudes should match
# with theoretical values.
#
# Input parameters:
# Dimensions = 1
# Length = 20 meters
# Fluid speed of sound = 1500 m/s
# Fluid density = 1e-6 Giga kg/m^3
# Structural bulk modulus = 2.25 GPa
# Structural shear modulus = 0 GPa
# Structural density = 4e-6 Giga kg/m^3
# Fluid domain = true
# Fluid BC = single peak sine wave applied as a pressure on the fluid end
# Structural domain = true
# Structural BC = Neumann BC with value zero applied on the structural end.
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 50
xmax = 20
[]
[./subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '10.0 0 0'
block_id = 1
top_right = '20.0 0.0 0'
[../]
[./interface1]
type = SideSetsBetweenSubdomainsGenerator
input = subdomain1
primary_block = '1'
paired_block = 0
new_boundary = 'interface1'
[../]
[]
[GlobalParams]
[]
[Variables]
[./p]
block = 1
[../]
[./disp_x]
block = 0
[../]
[]
[AuxVariables]
[./vel_x]
order = FIRST
family = LAGRANGE
block = 0
[../]
[./accel_x]
order = FIRST
family = LAGRANGE
block = 0
[../]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
block = 0
[../]
[]
[Kernels]
[./diffusion]
type = Diffusion
variable = 'p'
block = 1
[../]
[./inertia]
type = AcousticInertia
variable = p
block = 1
[../]
[./DynamicTensorMechanics]
displacements = 'disp_x'
block = 0
[../]
[./inertia_x1]
type = InertialForce
variable = disp_x
block = 0
[../]
[]
[AuxKernels]
[./accel_x]
type = TestNewmarkTI
displacement = disp_x
variable = accel_x
first = false
block = 0
[../]
[./vel_x]
type = TestNewmarkTI
displacement = disp_x
variable = vel_x
block = 0
[../]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
block = 0
[../]
[]
[InterfaceKernels]
[./interface1]
type = StructureAcousticInterface
variable = p
neighbor_var = disp_x
boundary = 'interface1'
D = 1e-6
component = 0
[../]
[]
[BCs]
[./bottom_accel]
type = FunctionDirichletBC
variable = p
boundary = 'right'
function = accel_bottom
[../]
[./disp_x1]
type = NeumannBC
boundary = 'left'
variable = disp_x
value = 0.0
[../]
[]
[Functions]
[./accel_bottom]
type = PiecewiseLinear
data_file = Input_1Peak_highF.csv
scale_factor = 1e-2
format = 'columns'
[../]
[]
[Materials]
[./co_sq]
type = GenericConstantMaterial
prop_names = inv_co_sq
prop_values = 4.44e-7
block = '1'
[../]
[./density0]
type = GenericConstantMaterial
block = 0
prop_names = density
prop_values = 4e-6
[../]
[./elasticity_base]
type = ComputeIsotropicElasticityTensor
bulk_modulus = 2.25
shear_modulus = 0.0
block = 0
[../]
[./strain]
type = ComputeFiniteStrain
block = 0
displacements = 'disp_x'
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
start_time = 0.0
end_time = 0.01
dt = 0.0001
dtmin = 0.00001
nl_abs_tol = 1e-12
nl_rel_tol = 1e-12
l_tol = 1e-12
l_max_its = 25
timestep_tolerance = 1e-8
automatic_scaling = true
[TimeIntegrator]
type = NewmarkBeta
[]
[]
[Postprocessors]
[./p1]
type = PointValue
point = '10.0 0.0 0.0'
variable = p
[../]
[./stress1]
type = PointValue
point = '10.0 0.0 0.0'
variable = stress_xx
[../]
[]
[Outputs]
csv = true
exodus = true
perf_graph = true
print_linear_residuals = true
[]
(modules/richards/test/tests/gravity_head_1/gh20.i)
# investigating validity of immobile saturation
# 5 elements, no SUPG
[Mesh]
type = GeneratedMesh
dim = 1
nx = 5
xmin = -1
xmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1 10 100 1000 10000'
x = '0 10 100 1000 10000'
[../]
[]
[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 = 0.3
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGnone]
type = RichardsSUPGnone
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
initial_condition = -1.0
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[Kernels]
active = 'richardsf richardst'
[./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-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 = Transient
solve_type = Newton
dt = 1E0
end_time = 1E5
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = gh20
execute_on = 'timestep_end final'
interval = 10000
exodus = true
[]
(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
[]
(modules/tensor_mechanics/test/tests/j_integral_vtest/j_int_surfbreak_ellip_crack_sym_mm_cfp.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[Mesh]
file = ellip_crack_4sym_norad_mm.e
partitioner = centroid
centroid_partitioner_direction = z
[]
[AuxVariables]
[./SED]
order = CONSTANT
family = MONOMIAL
[../]
[./resid_z]
[../]
[]
[Functions]
[./rampConstantUp]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 0.1'
scale_factor = -689.5 #MPa
[../]
[]
[DomainIntegral]
integrals = JIntegral
crack_direction_method = CurvedCrackFront
crack_end_direction_method = CrackDirectionVector
crack_direction_vector_end_1 = '0.0 1.0 0.0'
crack_direction_vector_end_2 = '1.0 0.0 0.0'
crack_front_points = '0 254 0
127.308 248.843 0
249.446 233.581 0
361.455 208.835 0
508.003 152.398 0
602.415 80.3208 0
635 0 0'
radius_inner = '12.5 25.0 37.5'
radius_outer = '25.0 37.5 50.0'
intersecting_boundary = '1 2'
symmetry_plane = 2
incremental = true
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
[../]
[]
[AuxKernels]
[./SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[../]
[]
[BCs]
[./crack_y]
type = DirichletBC
variable = disp_z
boundary = 6
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = 12
value = 0.0
[../]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./Pressure]
[./Side1]
boundary = 5
function = rampConstantUp
[../]
[../]
[] # BCs
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 206800
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
# Two sets of linesearch options are for petsc 3.1 and 3.3 respectively
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
# petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 4'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_abs_tol = 1e-5
nl_rel_tol = 1e-11
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Postprocessors]
[./_dt]
type = TimestepSize
[../]
[./nl_its]
type = NumNonlinearIterations
[../]
[./lin_its]
type = NumLinearIterations
[../]
[./react_z]
type = NodalSum
variable = resid_z
boundary = 5
[../]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = j_int_surfbreak_ellip_crack_sym_mm_cfp_out
exodus = true
csv = true
[]
(modules/richards/test/tests/buckley_leverett/bl20_lumped.i)
# two-phase version
[Mesh]
type = GeneratedMesh
dim = 1
nx = 30
xmin = 0
xmax = 15
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = 'DensityWater DensityGas'
relperm_UO = 'RelPermWater RelPermGas'
SUPG_UO = 'SUPGwater SUPGgas'
sat_UO = 'SatWater SatGas'
seff_UO = 'SeffWater SeffGas'
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '0.1 0.5 0.5 1 2 4'
x = '0 0.1 1 5 40 42'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = 'pwater pgas'
[../]
[./DensityWater]
type = RichardsDensityConstBulk
dens0 = 1000
bulk_mod = 2E6
[../]
[./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 = 2
[../]
[./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 = 1E-5
[../]
[./SUPGgas]
type = RichardsSUPGstandard
p_SUPG = 1E-5
[../]
[]
[Variables]
[./pwater]
order = FIRST
family = LAGRANGE
[../]
[./pgas]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./w_aux_seff]
[../]
[]
[Kernels]
[./richardstwater]
type = RichardsLumpedMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFlux
variable = pwater
[../]
[./richardstgas]
type = RichardsLumpedMassChange
variable = pgas
[../]
[./richardsfgas]
type = RichardsFlux
variable = pgas
[../]
[]
[AuxKernels]
[./w_aux_seff_auxk]
type = RichardsSeffAux
seff_UO = SeffWater
pressure_vars = 'pwater pgas'
variable = w_aux_seff
[../]
[]
[ICs]
[./water_ic]
type = FunctionIC
variable = pwater
function = initial_water
[../]
[./gas_ic]
type = FunctionIC
variable = pgas
function = initial_gas
[../]
[]
[BCs]
[./left_w]
type = DirichletBC
variable = pwater
boundary = left
value = 1E6
[../]
[./left_g]
type = DirichletBC
variable = pgas
boundary = left
value = 1000
[../]
[./right_w]
type = DirichletBC
variable = pwater
boundary = right
value = -300000
[../]
[./right_g]
type = DirichletBC
variable = pgas
boundary = right
value = 0
[../]
[]
[Functions]
[./initial_water]
type = ParsedFunction
value = 1000000*(1-min(x/5,1))-if(x<5,0,300000)
[../]
[./initial_gas]
type = ParsedFunction
value = 1000
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.15
mat_permeability = '1E-10 0 0 0 1E-10 0 0 0 1E-10'
viscosity = '1E-3 1E-6'
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
active = 'standard'
[./bounded]
# must use --use-petsc-dm command line argument
type = SMP
full = true
petsc_options_iname = '-snes_type -pc_factor_shift_type'
petsc_options_value = 'vinewtonssls nonzero'
[../]
[./standard]
type = SMP
full = true
petsc_options_iname = '-pc_factor_shift_type'
petsc_options_value = 'nonzero'
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
end_time = 50
nl_rel_tol = 1.e-9
nl_max_its = 10
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = bl20_lumped
execute_on = 'initial timestep_end final'
interval = 100000
exodus = true
hide = pgas
[./console_out]
type = Console
interval = 1
[../]
[]
(modules/xfem/test/tests/pressure_bc/2d_pressure_displaced_mesh.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
volumetric_locking_correction = false
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 5
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.0 0.5 1.0 0.5'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
planar_formulation = PLANE_STRAIN
generate_output = 'stress_xx stress_yy'
[../]
[]
[Functions]
[./pressure]
type = PiecewiseLinear
x = '0 1.0'
y = '500 500'
[../]
[./bc_func_tx]
type = ParsedFunction
value = '0.5-(0.5-x)*cos(pi*t/2.0)-x'
[../]
[./bc_func_ty]
type = ParsedFunction
value = '(0.5-x)*sin(pi*t/2.0)+0.5'
[../]
[]
[BCs]
[./bottom_y]
type = DirichletBC
boundary = 0
preset = false
variable = disp_y
value = 0.0
[../]
[./bottom_x]
type = DirichletBC
boundary = 0
preset = false
variable = disp_x
value = 0.0
[../]
[./top_right_y]
type = FunctionDirichletBC
boundary = 2
preset = false
variable = disp_y
function = bc_func_ty
[../]
[./top_right_x]
type = FunctionDirichletBC
boundary = 2
preset = false
variable = disp_x
function = bc_func_tx
[../]
[]
[DiracKernels]
[./pressure_x]
type = XFEMPressure
variable = disp_x
component = 0
function = pressure
use_displaced_mesh = true
[../]
[./pressure_y]
type = XFEMPressure
variable = disp_y
component = 1
function = pressure
use_displaced_mesh = true
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-14
# time control
start_time = 0.0
dt = 0.1
end_time = 1.0
[]
[Outputs]
file_base = 2d_pressure_displaced_mesh_out
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/tensor_mechanics/test/tests/central_difference/lumped/1D/1d_lumped_explicit.i)
# Test for central difference integration for a 1D element
[Mesh]
[./generated_mesh]
type = GeneratedMeshGenerator
xmin = 0
xmax = 10
nx = 5
dim = 1
[../]
[]
[Variables]
[./disp_x]
[../]
[]
[AuxVariables]
[./accel_x]
[../]
[./vel_x]
[../]
[]
[AuxKernels]
[./accel_x]
type = TestNewmarkTI
variable = accel_x
displacement = disp_x
first = false
[../]
[./vel_x]
type = TestNewmarkTI
variable = vel_x
displacement = disp_x
[../]
[]
[Kernels]
[./DynamicTensorMechanics]
displacements = 'disp_x'
[../]
[./inertia_x]
type = InertialForce
variable = disp_x
[../]
[]
[NodalKernels]
[./force_x]
type = UserForcingFunctionNodalKernel
variable = disp_x
boundary = right
function = force_x
[../]
[]
[Functions]
[./force_x]
type = PiecewiseLinear
x = '0.0 1.0 2.0 3.0 4.0' # time
y = '0.0 1.0 0.0 -1.0 0.0' # force
scale_factor = 1e3
[../]
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor_block]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.25
block = 0
[../]
[./strain_block]
type = ComputeIncrementalSmallStrain
block = 0
displacements = 'disp_x'
implicit = false
[../]
[./stress_block]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = density
prop_values = 2500
[../]
[]
[Executioner]
type = Transient
start_time = -0.01
end_time = 0.1
timestep_tolerance = 2e-10
dt = 0.005
[./TimeIntegrator]
type = CentralDifference
solve_type = lumped
[../]
[]
[Postprocessors]
[./accel_x]
type = PointValue
point = '10.0 0.0 0.0'
variable = accel_x
[../]
[]
[Outputs]
exodus = false
csv = true
[]
(modules/tensor_mechanics/test/tests/j_integral/j_integral_3d_points.i)
#This tests the J-Integral evaluation capability.
#This is a 3d extrusion of a 2d plane strain model with 2 elements
#through the thickness, and calculates the J-Integrals using options
#to treat it as 3d.
#The analytic solution for J1 is 2.434. This model
#converges to that solution with a refined mesh.
#Reference: National Agency for Finite Element Methods and Standards (U.K.):
#Test 1.1 from NAFEMS publication "Test Cases in Linear Elastic Fracture
#Mechanics" R0020.
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[Mesh]
file = crack3d.e
[]
[AuxVariables]
[./SED]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./rampConstant]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = -1e2
[../]
[]
[DomainIntegral]
integrals = JIntegral
crack_front_points = '0 -10 .5
0 -10 0
0 -10 -.5'
crack_direction_method = CrackDirectionVector
crack_direction_vector = '1 0 0'
radius_inner = '4.0 5.5'
radius_outer = '5.5 7.0'
output_q = false
incremental = true
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
[../]
[]
[AuxKernels]
[./SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[../]
[]
[BCs]
[./crack_y]
type = DirichletBC
variable = disp_y
boundary = 100
value = 0.0
[../]
[./no_z]
type = DirichletBC
variable = disp_z
boundary = 500
value = 0.0
[../]
[./no_z2]
type = DirichletBC
variable = disp_z
boundary = 510
value = 0.0
[../]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 700
value = 0.0
[../]
[./Pressure]
[./Side1]
boundary = 400
function = rampConstant
[../]
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_abs_tol = 1e-5
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Outputs]
file_base = j_integral_3d_points_out
exodus = true
csv = true
[]
(modules/geochemistry/test/tests/time_dependent_reactions/seawater_evaporation_flow_through.i)
#Progressively remove H2O until virtually none remains, all the while removing any minerals that precipitate
[UserObjects]
[definition]
type = GeochemicalModelDefinition
database_file = "../../../database/moose_geochemdb.json"
basis_species = "H2O H+ Cl- Ca++ Mg++ Na+ K+ SO4-- HCO3-"
equilibrium_minerals = "Dolomite Epsomite Gypsum Halite Magnesite Mirabilite Sylvite"
equilibrium_gases = "CO2(g)"
piecewise_linear_interpolation = true # for precise agreement with GWB
[]
[]
[TimeDependentReactionSolver]
model_definition = definition
geochemistry_reactor_name = reactor
swap_out_of_basis = "H+"
swap_into_basis = " CO2(g)"
charge_balance_species = "Cl-" # this means the bulk moles of Cl- will not be exactly as set below
constraint_species = "H2O CO2(g) Cl- Na+ SO4-- Mg++ Ca++ K+ HCO3-"
constraint_value = " 1.0 -3.5 0.5656 0.4850 0.02924 0.05501 0.01063 0.010576055 0.002412"
constraint_meaning = "kg_solvent_water log10fugacity 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"
source_species_names = "H2O"
source_species_rates = "-1.0" # 1kg H2O = 55.51 moles, each time step removes 1 mole
mode = mode
ramp_max_ionic_strength_initial = 0 # not needed in this simple example
stoichiometric_ionic_str_using_Cl_only = true # for precise agreement with GWB
execute_console_output_on = '' # only CSV output for this example
[]
[Functions]
[timestepper]
type = PiecewiseLinear
x = '0 50 55'
y = '5 5 1'
[]
[]
[Executioner]
type = Transient
[TimeStepper]
type = FunctionDT
function = timestepper
[]
end_time = 55
[]
[AuxVariables]
[mode]
[]
[dolomite_mol]
[]
[halite_mol]
[]
[gypsum_mol]
[]
[mirabilite_mol]
[]
[]
[AuxKernels]
[mode_auxk]
type = FunctionAux
variable = mode
function = 'if(t<=1.0, 1.0, 2.0)' # initial "dump" then "flow_through"
execute_on = 'timestep_begin'
[]
[dolomite_mol_auxk]
type = GeochemistryQuantityAux
reactor = reactor
variable = dolomite_mol
species = Dolomite
quantity = moles_dumped
[]
[gypsum_mol_auxk]
type = GeochemistryQuantityAux
reactor = reactor
variable = gypsum_mol
species = Gypsum
quantity = moles_dumped
[]
[halite_mol]
type = GeochemistryQuantityAux
reactor = reactor
variable = halite_mol
species = Halite
quantity = moles_dumped
[]
[mirabilite_mol]
type = GeochemistryQuantityAux
reactor = reactor
variable = mirabilite_mol
species = Mirabilite
quantity = moles_dumped
[]
[]
[GlobalParams]
point = '0 0 0'
[]
[Postprocessors]
[solvent_kg]
type = PointValue
variable = 'kg_solvent_H2O'
[]
[dolomite_mol]
type = PointValue
variable = dolomite_mol
[]
[gypsum_mol]
type = PointValue
variable = 'gypsum_mol'
[]
[halite_mol]
type = PointValue
variable = 'halite_mol'
[]
[mirabilite_mol]
type = PointValue
variable = 'mirabilite_mol'
[]
[]
[Outputs]
csv = true
[]
(modules/tensor_mechanics/test/tests/action/action_multi_eigenstrain.i)
# This tests the thermal expansion coefficient function using both
# options to specify that function: mean and instantaneous. There
# two blocks, each containing a single element, and these use the
# two variants of the function.
# In this test, the instantaneous CTE function has a constant value,
# while the mean CTE function is an analytic function designed to
# give the same response. If \bar{alpha}(T) is the mean CTE function,
# and \alpha(T) is the instantaneous CTE function,
# \bar{\alpha}(T) = 1/(T-Tref) \intA^{T}_{Tsf} \alpha(T) dT
# where Tref is the reference temperature used to define the mean CTE
# function, and Tsf is the stress-free temperature.
# This version of the test uses finite deformation theory.
# The two models produce very similar results. There are slight
# differences due to the large deformation treatment.
[Mesh]
file = 'blocks.e'
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[AuxVariables]
[./temp]
order = FIRST
family = LAGRANGE
[../]
[]
[Problem]
solve = false
[]
[Modules/TensorMechanics/Master]
[./block1]
block = 1
strain = FINITE
add_variables = true
automatic_eigenstrain_names = true
generate_output = 'strain_xx strain_yy strain_zz'
[../]
[./block2]
block = 2
strain = FINITE
add_variables = true
automatic_eigenstrain_names = true
generate_output = 'strain_xx strain_yy strain_zz'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = disp_x
boundary = 3
value = 0.0
[../]
[./bottom]
type = DirichletBC
variable = disp_y
boundary = 2
value = 0.0
[../]
[./back]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0.0
[../]
[]
[AuxKernels]
[./temp]
type = FunctionAux
variable = temp
block = '1 2'
function = temp_func
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./small_stress]
type = ComputeFiniteStrainElasticStress
[../]
[./thermal_expansion_strain1]
type = ComputeMeanThermalExpansionFunctionEigenstrain
block = 1
thermal_expansion_function = cte_func_mean
thermal_expansion_function_reference_temperature = 0.5
stress_free_temperature = 0.0
temperature = temp
eigenstrain_name = eigenstrain1
[../]
[./thermal_expansion_strain2]
type = ComputeInstantaneousThermalExpansionFunctionEigenstrain
block = 2
thermal_expansion_function = cte_func_inst
stress_free_temperature = 0.0
temperature = temp
eigenstrain_name = eigenstrain2
[../]
[]
[Functions]
[./cte_func_mean]
type = ParsedFunction
vars = 'tsf tref scale' #stress free temp, reference temp, scale factor
vals = '0.0 0.5 1e-4'
value = 'scale * (t - tsf) / (t - tref)'
[../]
[./cte_func_inst]
type = PiecewiseLinear
xy_data = '0 1.0
2 1.0'
scale_factor = 1e-4
[../]
[./temp_func]
type = PiecewiseLinear
xy_data = '0 1
1 2'
[../]
[]
[Postprocessors]
[./disp_1]
type = NodalMaxValue
variable = disp_x
boundary = 101
[../]
[./disp_2]
type = NodalMaxValue
variable = disp_x
boundary = 102
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
l_max_its = 100
l_tol = 1e-4
nl_abs_tol = 1e-8
nl_rel_tol = 1e-12
start_time = 0.0
end_time = 1.0
dt = 0.1
[]
[Outputs]
csv = true
[]
(modules/tensor_mechanics/test/tests/1D_axisymmetric/axisymm_gps_small.i)
# this test checks the asixymmetric 1D generalized plane strain formulation using incremental small strains
[GlobalParams]
displacements = disp_x
scalar_out_of_plane_strain = scalar_strain_yy
[]
[Problem]
coord_type = RZ
[]
[Mesh]
file = line.e
[]
[Variables]
[./disp_x]
[../]
[./scalar_strain_yy]
order = FIRST
family = SCALAR
[../]
[]
[AuxVariables]
[./strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./temp]
initial_condition = 580.0
[../]
[]
[Functions]
[./temp]
type = PiecewiseLinear
x = '0 1 2'
y = '580 580 680'
[../]
[./disp_x]
type = PiecewiseLinear
x = '0 1'
y = '0 2e-6'
[../]
[]
[Kernels]
[./TensorMechanics]
[../]
[]
[Modules]
[./TensorMechanics]
[./GeneralizedPlaneStrain]
[./gps]
[../]
[../]
[../]
[]
[AuxKernels]
[./strain_xx]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_xx
index_i = 0
index_j = 0
[../]
[./strain_yy]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_yy
index_i = 1
index_j = 1
[../]
[./strain_zz]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_zz
index_i = 2
index_j = 2
[../]
[./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_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./temp]
type = FunctionAux
variable = temp
function = temp
execute_on = 'timestep_begin'
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
boundary = 1
value = 0
variable = disp_x
[../]
[./disp_x]
type = FunctionDirichletBC
boundary = 2
function = disp_x
variable = disp_x
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 3600
poissons_ratio = 0.2
[../]
[./strain]
type = ComputeAxisymmetric1DSmallStrain
eigenstrain_names = eigenstrain
scalar_out_of_plane_strain = scalar_strain_yy
[../]
[./thermal_strain]
type = ComputeThermalExpansionEigenstrain
thermal_expansion_coeff = 1e-8
temperature = temp
stress_free_temperature = 580
eigenstrain_name = eigenstrain
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
line_search = 'none'
l_max_its = 50
l_tol = 1e-6
nl_max_its = 15
nl_rel_tol = 1e-8
nl_abs_tol = 1e-10
start_time = 0
end_time = 2
num_steps = 2
[]
[Outputs]
exodus = true
console = true
[]
(modules/tensor_mechanics/test/tests/beam/fric_constraint/2_block_common_cross_stick.i)
# Test for LineElementAction on multiple blocks by placing parameters
# common to all blocks outside of the individual action blocks
# 2 beams of length 1m are fixed at one end and a force of 1e-4 N
# is applied at the other end of the beams. Beam 1 is in block 1
# and beam 2 is in block 2. All the material properties for the two
# beams are identical. The moment of inertia of beam 2 is twice that
# of beam 1.
# Since the end displacement of a cantilever beam is inversely proportional
# to the moment of inertia, the y displacement at the end of beam 1 should be twice
# that of beam 2.
[Mesh]
type = FileMesh
file = test_fric_cross.e
#displacements = 'disp_x disp_y disp_z'
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = '1 2 3'
value = 0.0
[../]
[./fixy1]
type = DirichletBC
variable = disp_y
boundary = '1 2 3'
value = 0.0
[../]
[./fixz1]
type = DirichletBC
variable = disp_z
boundary = '1 3'
value = 0.0
[../]
[./fixr1]
type = DirichletBC
variable = rot_x
boundary = '1 2 3'
value = 0.0
[../]
[./fixr2]
type = DirichletBC
variable = rot_y
boundary = '1 2 3'
value = 0.0
[../]
[./fixr3]
type = DirichletBC
variable = rot_z
boundary = '1 2 3'
value = 0.0
[../]
[./move_z4]
type = FunctionDirichletBC
variable = disp_z
boundary = 2
function = pull
[../]
[]
[Functions]
[./pull]
type = PiecewiseLinear
x = '0.0 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'
y = '0.0 0.0 -0.2 -0.4 -0.6 -0.8 -0.6 -0.4 -0.2 0.0 0.2 0.4 0.6 0.8'
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
line_search = 'none'
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 5e-5
l_max_its = 10
dt = 1
dtmin = 1
end_time = 13
[]
[Modules/TensorMechanics/LineElementMaster]
# parameters common to all blocks
add_variables = true
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
# Geometry parameters
area = 0.5
y_orientation = '0.0 1.0 0.0'
[./block_1]
Iy = 1e-5
Iz = 1e-5
block = 1
[../]
[./block_2]
Iy = 8e-4
Iz = 8e-4
block = '2 3'
[../]
[]
[Materials]
[./stress]
type = ComputeBeamResultants
block = '1 2 3'
[../]
[./elasticity_1]
type = ComputeElasticityBeam
youngs_modulus = 2.0
poissons_ratio = 0.3
shear_coefficient = 1.0
block = '1 2 3'
[../]
[]
[Constraints]
[./tie_z]
type = NodalStickConstraint
penalty = 1e8
boundary = 6
secondary = 4
variable = disp_z
formulation = kinematic
[../]
[./tie_z2]
type = NodalStickConstraint
penalty = 1e8
boundary = 6
secondary = 5
variable = disp_z
formulation = kinematic
[../]
[]
[Postprocessors]
[./disp_x_1]
type = NodalVariableValue
nodeid = 1
variable = disp_x
[../]
[./disp_x_2]
type = NodalVariableValue
nodeid = 2
variable = disp_x
[../]
[./disp_z_1]
type = NodalVariableValue
nodeid = 1
variable = disp_z
[../]
[./disp_z_2]
type = NodalVariableValue
nodeid = 2
variable = disp_z
[../]
[]
[Outputs]
#file_base = '2_block_out'
exodus = true
[]
(test/tests/multiapps/multilevel/time_dt_from_master_master.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmax = 100
[]
[Functions]
[./dts]
type = PiecewiseLinear
x = '0 1'
y = '0.25 1'
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./td]
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 = Transient
num_steps = 4
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
dt = 0.25
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
exodus = true
[./out]
type = Console
output_file = true
[../]
[]
[MultiApps]
[./sub]
type = TransientMultiApp
app_type = MooseTestApp
positions = '0 0 0 0.5 0.5 0'
input_files = time_dt_from_master_sub.i
[../]
[]
(modules/tensor_mechanics/test/tests/beam/static/euler_finite_rot_z.i)
# Large strain/large rotation cantilever beam test
# A 300 N point load is applied at the end of a 4 m long cantilever beam.
# Young's modulus (E) = 1e4
# Shear modulus (G) = 1e8
# Poisson's ratio (nu) = -0.99995
# shear coefficient (k) = 1.0
# Area (A) = 1.0
# Iy = Iz = 0.16
# The dimensionless parameter alpha = kAGL^2/EI = 1e6
# Since the value of alpha ia quite high, the beam behaves like
# a thin beam where shear effects are not significant.
# Beam deflection:
# small strain+rot = 3.998 m (exact 4.0)
# large strain + small rotation = -0.05 m in x and 3.74 m in z
# large rotations + small strain = -0.92 m in x and 2.38 m in z
# large rotations + large strain = -0.954 m in x and 2.37 m in z (exact -1.0 m in x and 2.4 m in z)
# References:
# K. E. Bisshopp and D.C. Drucker, Quaterly of Applied Mathematics, Vol 3, No. 3, 1945.
[Mesh]
type = FileMesh
file = beam_finite_rot_test_2.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[./rot_x]
order = FIRST
family = LAGRANGE
[../]
[./rot_y]
order = FIRST
family = LAGRANGE
[../]
[./rot_z]
order = FIRST
family = LAGRANGE
[../]
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./fixy1]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./fixz1]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0.0
[../]
[./fixr1]
type = DirichletBC
variable = rot_x
boundary = 1
value = 0.0
[../]
[./fixr2]
type = DirichletBC
variable = rot_y
boundary = 1
value = 0.0
[../]
[./fixr3]
type = DirichletBC
variable = rot_z
boundary = 1
value = 0.0
[../]
[]
[NodalKernels]
[./force_z2]
type = UserForcingFunctionNodalKernel
variable = disp_z
boundary = 2
function = force
[../]
[]
[Functions]
[./force]
type = PiecewiseLinear
x = '0.0 2.0 8.0'
y = '0.0 300.0 300.0'
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
line_search = 'none'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 4'
nl_max_its = 50
nl_rel_tol = 1e-9
nl_abs_tol = 1e-7
l_max_its = 50
dt = 0.05
end_time = 2.1
[]
[Kernels]
[./solid_disp_x]
type = StressDivergenceBeam
block = '1'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 0
variable = disp_x
[../]
[./solid_disp_y]
type = StressDivergenceBeam
block = '1'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 1
variable = disp_y
[../]
[./solid_disp_z]
type = StressDivergenceBeam
block = '1'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 2
variable = disp_z
[../]
[./solid_rot_x]
type = StressDivergenceBeam
block = '1'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 3
variable = rot_x
[../]
[./solid_rot_y]
type = StressDivergenceBeam
block = '1'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 4
variable = rot_y
[../]
[./solid_rot_z]
type = StressDivergenceBeam
block = '1'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 5
variable = rot_z
[../]
[]
[Materials]
[./elasticity]
type = ComputeElasticityBeam
youngs_modulus = 1e4
poissons_ratio = -0.99995
shear_coefficient = 1.0
block = 1
[../]
[./strain]
type = ComputeFiniteBeamStrain
block = '1'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
area = 1.0
Ay = 0.0
Az = 0.0
Iy = 0.16
Iz = 0.16
y_orientation = '0.0 1.0 0.0'
large_strain = true
[../]
[./stress]
type = ComputeBeamResultants
block = 1
[../]
[]
[Postprocessors]
[./disp_x]
type = PointValue
point = '4.0 0.0 0.0'
variable = disp_x
[../]
[./disp_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = disp_z
[../]
[./rot_z]
type = PointValue
point = '4.0 0.0 0.0'
variable = rot_y
[../]
[]
[Outputs]
exodus = true
perf_graph = true
[]
(modules/combined/test/tests/ad_cavity_pressure/initial_temperature.i)
#
# Cavity Pressure Test
#
# This test is designed to compute an internal pressure based on
# p = n * R * T / V
# where
# p is the pressure
# n is the amount of material in the volume (moles)
# R is the universal gas constant
# T is the temperature
# V is the volume
#
# The mesh is composed of one block (1) with an interior cavity of volume 8.
# Block 2 sits in the cavity and has a volume of 1. Thus, the total
# initial volume is 7.
# The test adjusts n, T, and V in the following way:
# n => n0 + alpha * t
# T => T0 + beta * t
# V => V0 + gamma * t
# with
# alpha = n0
# beta = T0 / 2
# gamma = -(0.003322259...) * V0
# T0 = 240.54443866068704
# V0 = 7
# n0 = f(p0)
# p0 = 100
# R = 8.314472 J * K^(-1) * mol^(-1)
#
# So, n0 = p0 * V0 / R / T0 = 100 * 7 / 8.314472 / 240.544439
# = 0.35
#
# The parameters combined at t = 1 gives p = 301.
#
# This test sets the initial temperature to 500, but the CavityPressure
# is told that that initial temperature is T0. Thus, the final solution
# is unchanged.
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
file = 3d.e
[]
[GlobalParams]
volumetric_locking_correction = true
[]
[Functions]
[./displ_positive]
type = PiecewiseLinear
x = '0 1'
y = '0 0.0029069767441859684'
[../]
[./displ_negative]
type = PiecewiseLinear
x = '0 1'
y = '0 -0.0029069767441859684'
[../]
[./temp1]
type = PiecewiseLinear
x = '0 1'
y = '1 1.5'
scale_factor = 240.54443866068704
[../]
[./material_input_function]
type = PiecewiseLinear
x = '0 1'
y = '0 0.35'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[./temp]
initial_condition = 500
[../]
[./material_input]
[../]
[]
[AuxVariables]
[./pressure_residual_x]
[../]
[./pressure_residual_y]
[../]
[./pressure_residual_z]
[../]
[./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_zx]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
use_automatic_differentiation = true
[../]
[./heat]
type = ADDiffusion
variable = temp
use_displaced_mesh = true
[../]
[./material_input_dummy]
type = ADDiffusion
variable = material_input
use_displaced_mesh = true
[../]
[]
[AuxKernels]
[./stress_xx]
type = ADRankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 0
variable = stress_xx
[../]
[./stress_yy]
type = ADRankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 1
variable = stress_yy
[../]
[./stress_zz]
type = ADRankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 2
variable = stress_zz
[../]
[./stress_xy]
type = ADRankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 1
variable = stress_xy
[../]
[./stress_yz]
type = ADRankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 2
variable = stress_yz
[../]
[./stress_zx]
type = ADRankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 0
variable = stress_zx
[../]
[]
[BCs]
[./no_x_exterior]
type = DirichletBC
variable = disp_x
boundary = '7 8'
value = 0.0
[../]
[./no_y_exterior]
type = DirichletBC
variable = disp_y
boundary = '9 10'
value = 0.0
[../]
[./no_z_exterior]
type = DirichletBC
variable = disp_z
boundary = '11 12'
value = 0.0
[../]
[./prescribed_left]
type = ADFunctionDirichletBC
variable = disp_x
boundary = 13
function = displ_positive
[../]
[./prescribed_right]
type = ADFunctionDirichletBC
variable = disp_x
boundary = 14
function = displ_negative
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = '15 16'
value = 0.0
[../]
[./no_z]
type = DirichletBC
variable = disp_z
boundary = '17 18'
value = 0.0
[../]
[./no_x_interior]
type = DirichletBC
variable = disp_x
boundary = '1 2'
value = 0.0
[../]
[./no_y_interior]
type = DirichletBC
variable = disp_y
boundary = '3 4'
value = 0.0
[../]
[./no_z_interior]
type = DirichletBC
variable = disp_z
boundary = '5 6'
value = 0.0
[../]
[./temperatureInterior]
type = ADFunctionDirichletBC
boundary = 100
function = temp1
variable = temp
[../]
[./MaterialInput]
type = ADFunctionDirichletBC
boundary = '100 13 14 15 16'
function = material_input_function
variable = material_input
[../]
[./CavityPressure]
[./1]
boundary = 100
initial_pressure = 100
material_input = materialInput
R = 8.314472
temperature = aveTempInterior
initial_temperature = 240.54443866068704
volume = internalVolume
startup_time = 0.5
output = ppress
save_in = 'pressure_residual_x pressure_residual_y pressure_residual_z'
use_automatic_differentiation = true
[../]
[../]
[]
[Materials]
[./elast_tensor1]
type = ADComputeElasticityTensor
C_ijkl = '0 5'
fill_method = symmetric_isotropic
block = 1
[../]
[./strain1]
type = ADComputeFiniteStrain
block = 1
[../]
[./stress1]
type = ADComputeFiniteStrainElasticStress
block = 1
[../]
[./elast_tensor2]
type = ADComputeElasticityTensor
C_ijkl = '0 5'
fill_method = symmetric_isotropic
block = 2
[../]
[./strain2]
type = ADComputeFiniteStrain
block = 2
[../]
[./stress2]
type = ADComputeFiniteStrainElasticStress
block = 2
[../]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_type'
petsc_options_value = 'asm lu'
nl_rel_tol = 1e-12
l_tol = 1e-12
l_max_its = 20
dt = 0.5
end_time = 1.0
[]
[Postprocessors]
[./internalVolume]
type = InternalVolume
boundary = 100
execute_on = 'initial linear'
[../]
[./aveTempInterior]
type = SideAverageValue
boundary = 100
variable = temp
execute_on = 'initial linear'
[../]
[./materialInput]
type = SideAverageValue
boundary = '7 8 9 10 11 12'
variable = material_input
execute_on = linear
[../]
[]
[Outputs]
exodus = true
[]
(test/tests/geomsearch/2d_moving_penetration/pl_test4qnns.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
file = pl_test4q.e
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
normal_smoothing_method = nodal_normal_based
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate10]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate13]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate14]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate15]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate16]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1.e-9
l_max_its = 10
start_time = 0.0
dt = 0.02
end_time = 1.0
[./Quadrature]
order = THIRD
[../]
[]
[Outputs]
file_base = pl_test4qnns_out
exodus = true
[]
[NodalNormals]
boundary = 11
corner_boundary = 20
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_htonly/planar_xz.i)
# 1-D Gap Heat Transfer Test without mechanics
#
# This test exercises 1-D gap heat transfer for a constant conductivity gap.
#
# The mesh consists of two element blocks in the x-z plane. Each element block
# is a square. They sit next to one another with a unit between them.
#
# The conductivity of both blocks is set very large to achieve a uniform temperature
# across each block. The temperature of the far bottom boundary
# is ramped from 100 to 200 over one time unit. The temperature of the far top
# boundary is held fixed at 100.
#
# A simple analytical solution is possible for the heat flux between the blocks:
#
# Flux = (T_left - T_right) * (gapK/gap_width)
#
# The gap conductivity is specified as 1, thus
#
# gapK(Tavg) = 1.0*Tavg
#
# The heat flux across the gap at time = 1 is then:
#
# Flux = 100 * (1.0/1.0) = 100
#
# For comparison, see results from the flux post processors. These results
# are the same as for the unit 1-D gap heat transfer between two unit cubes.
[Mesh]
[file]
type = FileMeshGenerator
file = simple_2D.e
[]
[./rotate]
type = TransformGenerator
transform = ROTATE
vector_value = '0 90 0'
input = file
[../]
[]
[Functions]
[./temp]
type = PiecewiseLinear
x = '0 1 2'
y = '100 200 200'
[../]
[]
[ThermalContact]
[./thermal_contact]
type = GapHeatTransfer
variable = temp
primary = 3
secondary = 2
emissivity_primary = 0
emissivity_secondary = 0
[../]
[]
[Variables]
[./temp]
order = FIRST
family = LAGRANGE
initial_condition = 100
[../]
[]
[AuxVariables]
[./gap_cond]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[]
[BCs]
[./temp_far_bottom]
type = FunctionDirichletBC
boundary = 1
variable = temp
function = temp
[../]
[./temp_far_top]
type = DirichletBC
boundary = 4
variable = temp
value = 100
[../]
[]
[AuxKernels]
[./conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_cond
boundary = 2
[../]
[]
[Materials]
[./heat1]
type = HeatConductionMaterial
block = '1 2'
specific_heat = 1.0
thermal_conductivity = 100000000.0
[../]
[./density]
type = GenericConstantMaterial
block = '1 2'
prop_names = 'density'
prop_values = '1.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 4'
line_search = 'none'
nl_rel_tol = 1e-12
l_tol = 1e-3
l_max_its = 100
dt = 1e-1
end_time = 1.0
[]
[Postprocessors]
[./temp_bottom]
type = SideAverageValue
boundary = 2
variable = temp
execute_on = 'initial timestep_end'
[../]
[./temp_top]
type = SideAverageValue
boundary = 3
variable = temp
execute_on = 'initial timestep_end'
[../]
[./flux_bottom]
type = SideFluxIntegral
variable = temp
boundary = 2
diffusivity = thermal_conductivity
execute_on = 'initial timestep_end'
[../]
[./flux_top]
type = SideFluxIntegral
variable = temp
boundary = 3
diffusivity = thermal_conductivity
execute_on = 'initial timestep_end'
[../]
[]
[Outputs]
exodus = true
[]
(modules/contact/test/tests/hertz_spherical/hertz_contact_hex27.i)
# Hertz Contact: Sphere on sphere
# Spheres have the same radius, Young's modulus, and Poisson's ratio.
# Define E:
# 1/E = (1-nu1^2)/E1 + (1-nu2^2)/E2
#
# Effective radius R:
# 1/R = 1/R1 + 1/R2
#
# F is the applied compressive load.
#
# Area of contact a::
# a^3 = 3FR/4E
#
# Depth of indentation d:
# d = a^2/R
#
#
# Let R1 = R2 = 2. Then R = 1.
#
# Let nu1 = nu2 = 0.25, E1 = E2 = 1.40625e7. Then E = 7.5e6.
#
# Let F = 10000. Then a = 0.1, d = 0.01.
#
[GlobalParams]
volumetric_locking_correction = false
displacements = 'disp_x disp_y disp_z'
order = SECOND
[]
[Mesh]#Comment
file = hertz_contact_hex27.e
allow_renumbering = false
[] # Mesh
[Functions]
[./pressure]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 1.'
scale_factor = 795.77471545947674 # 10000/pi/2^2
[../]
[./disp_y]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. -0.01 -0.01'
[../]
[] # Functions
[Variables]
[./disp_x]
order = SECOND
family = LAGRANGE
[../]
[./disp_y]
order = SECOND
family = LAGRANGE
[../]
[./disp_z]
order = SECOND
family = LAGRANGE
[../]
[] # Variables
[AuxVariables]
[./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_zx]
order = CONSTANT
family = MONOMIAL
[../]
[./vonmises]
order = CONSTANT
family = MONOMIAL
[../]
[./hydrostatic]
order = CONSTANT
family = MONOMIAL
[../]
[] # AuxVariables
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = SMALL
# extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 0
variable = stress_xx
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 1
variable = stress_yy
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 2
variable = stress_zz
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 1
variable = stress_xy
[../]
[./stress_yz]
type = RankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 2
variable = stress_yz
[../]
[./stress_zx]
type = RankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 0
variable = stress_zx
[../]
[] # AuxKernels
[BCs]
[./base_x]
type = DirichletBC
variable = disp_x
boundary = 1000
value = 0.0
[../]
[./base_y]
type = DirichletBC
variable = disp_y
boundary = 1000
value = 0.0
[../]
[./base_z]
type = DirichletBC
variable = disp_z
boundary = 1000
value = 0.0
[../]
[./symm_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./symm_z]
type = DirichletBC
variable = disp_z
boundary = 3
value = 0.0
[../]
[./disp_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[] # BCs
[Contact]
[./dummy_name]
primary = 1000
secondary = 100
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+10
[../]
[]
[Materials]
[./tensor]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1.40625e7
poissons_ratio = 0.25
[../]
[./stress]
type = ComputeLinearElasticStress
block = '1'
[../]
[./tensor_1000]
type = ComputeIsotropicElasticityTensor
block = '1000'
youngs_modulus = 1e6
poissons_ratio = 0.0
[../]
[./stress_1000]
type = ComputeLinearElasticStress
block = '1000'
[../]
[] # Materials
[Preconditioning]
[./SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-7
l_max_its = 10
start_time = 0.0
dt = 0.5
end_time = 0.5 # was 2.0
[./Quadrature]
order = FIFTH
[../]
[] # Executioner
[Postprocessors]
[./maxdisp]
type = NodalVariableValue
nodeid = 386 # 387-1 where 387 is the exodus node number of the top-center node
variable = disp_y
[../]
[]
[Outputs]
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[] # Outputs
(test/tests/geomsearch/3d_moving_penetration_smoothing/pl_test4qnstt.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
file = pl_test4qtt.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./normal_z]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./closest_point_z]
[../]
# [./element_id]
# [../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[./diff_z]
type = Diffusion
variable = disp_z
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
tangential_tolerance = 0.09
normal_smoothing_distance = 0.2
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
tangential_tolerance = 0.09
normal_smoothing_distance = 0.2
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = normal_z
boundary = 11
paired_boundary = 12
quantity = normal_z
[../]
[./penetrate10]
type = PenetrationAux
variable = normal_z
boundary = 12
paired_boundary = 11
quantity = normal_z
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate13]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate14]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate15]
type = PenetrationAux
variable = closest_point_z
boundary = 11
paired_boundary = 12
quantity = closest_point_z
[../]
[./penetrate16]
type = PenetrationAux
variable = closest_point_z
boundary = 12
paired_boundary = 11
quantity = closest_point_z
[../]
# [./penetrate17]
# type = PenetrationAux
# variable = element_id
# boundary = 11
# paired_boundary = 12
# quantity = element_id
# [../]
#
# [./penetrate18]
# type = PenetrationAux
# variable = element_id
# boundary = 12
# paired_boundary = 11
# quantity = element_id
# [../]
[./penetrate19]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate20]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
preset = false
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
preset = false
boundary = 1
value = 0
[../]
[./b1z]
type = DirichletBC
variable = disp_z
preset = false
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
preset = false
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
preset = false
boundary = 2
function = disp_y
[../]
[./b2z]
type = DirichletBC
variable = disp_z
preset = false
boundary = 2
value = 0
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_abs_tol = 1e-7
l_max_its = 10
start_time = 0.0
dt = 0.02
end_time = 1.0
[./Quadrature]
order = THIRD
[../]
[]
[Outputs]
file_base = pl_test4qnstt_out
exodus = true
[]
(modules/tensor_mechanics/test/tests/material_limit_time_step/damage/scalar_material_damage_timestep_limit.i)
# This is a basic test of the system for continuum damage mechanics
# materials. It uses ScalarMaterialDamage for the damage model,
# which simply gets its damage index from another material. In this
# case, we prescribe the evolution of the damage index using a
# function. A single element has a fixed prescribed displacement
# on one side that puts the element in tension, and then the
# damage index evolves from 0 to 1 over time, and this verifies
# that the stress correspondingly drops to 0.
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
elem_type = HEX8
[]
[AuxVariables]
[damage_index]
order = CONSTANT
family = MONOMIAL
[]
[]
[Modules/TensorMechanics/Master]
[all]
strain = SMALL
incremental = true
add_variables = true
generate_output = 'stress_xx strain_xx'
[]
[]
[AuxKernels]
[damage_index]
type = MaterialRealAux
variable = damage_index
property = damage_index_prop
execute_on = timestep_end
[]
[]
[BCs]
[symmy]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0
[]
[symmx]
type = DirichletBC
variable = disp_x
boundary = left
value = 0
[]
[symmz]
type = DirichletBC
variable = disp_z
boundary = back
value = 0
[]
[axial_load]
type = DirichletBC
variable = disp_x
boundary = right
value = 0.01
[]
[]
[Functions]
[damage_evolution]
type = PiecewiseLinear
xy_data = '0.0 0.0
0.1 0.0
2.1 2.0'
[]
[]
[Materials]
[damage_index]
type = GenericFunctionMaterial
prop_names = damage_index_prop
prop_values = damage_evolution
[]
[damage]
type = ScalarMaterialDamage
damage_index = damage_index_prop
[]
[stress]
type = ComputeDamageStress
damage_model = damage
[]
[elasticity]
type = ComputeIsotropicElasticityTensor
poissons_ratio = 0.2
youngs_modulus = 10e9
[]
[]
[Postprocessors]
[stress_xx]
type = ElementAverageValue
variable = stress_xx
[]
[strain_xx]
type = ElementAverageValue
variable = strain_xx
[]
[damage_index]
type = ElementAverageValue
variable = damage_index
[]
[time_step_limit]
type = MaterialTimeStepPostprocessor
[]
[]
[Executioner]
type = Transient
l_max_its = 50
l_tol = 1e-8
nl_max_its = 20
nl_rel_tol = 1e-12
nl_abs_tol = 1e-8
dt = 0.1
dtmin = 0.001
end_time = 1.1
[TimeStepper]
type = IterationAdaptiveDT
dt = 0.1
growth_factor = 2.0
cutback_factor = 0.5
timestep_limiting_postprocessor = time_step_limit
[]
[]
[Outputs]
csv=true
[]
(modules/contact/test/tests/catch_release/catch_release.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
file = catch_release.e
[]
[Functions]
[./up]
type = PiecewiseLinear
x = '0 1 2.00 3 4'
y = '0 1 1.01 1 0'
scale_factor = 0.5
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = FINITE
generate_output = 'stress_yy'
[]
[]
[Contact]
[./dummy_name]
primary = 2
secondary = 3
penalty = 1e6
model = frictionless
[../]
[]
[BCs]
[./lateral]
type = DirichletBC
variable = disp_x
boundary = '1 4'
value = 0.0
[../]
[./bottom_up]
type = FunctionDirichletBC
variable = disp_y
preset = false
boundary = 1
function = up
[../]
[./out]
type = DirichletBC
variable = disp_z
boundary = '1 4'
value = 0.0
[../]
[./top]
type = DirichletBC
variable = disp_y
boundary = 4
value = 0.0
[../]
[]
[Materials]
[./stiffStuff]
type = ComputeIsotropicElasticityTensor
block = '1 2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stiffStuffStress]
type = ComputeFiniteStrainElasticStress
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
#petsc_options_iname = '-pc_type -snes_type -snes_ls -snes_linesearch_type -ksp_gmres_restart'
#petsc_options_value = 'ilu ls basic basic 101'
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart'
petsc_options_value = 'hypre boomeramg 101'
line_search = 'none'
nl_abs_tol = 1e-8
nl_rel_tol = 1e-4
l_tol = 1e-4
l_max_its = 100
nl_max_its = 20
dt = 1.0
end_time = 4.0
[]
[Outputs]
exodus = true
[]
(modules/contact/test/tests/verification/hertz_cyl/quart_symm_q8/hertz_cyl_qsym_1deg_template1.i)
[GlobalParams]
order = SECOND
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Mesh]
file = hertz_cyl_qsym_1deg_q8.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Functions]
[./disp_ramp_vert]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. -0.0020 -0.0020'
[../]
[./disp_ramp_zero]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 0.0 0.0'
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
[../]
[]
[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_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 4
paired_boundary = 3
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 4
paired_boundary = 3
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 4
paired_boundary = 3
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./disp_x281]
type = NodalVariableValue
nodeid = 280
variable = disp_x
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./side_x]
type = DirichletBC
variable = disp_y
boundary = '1 3'
value = 0.0
[../]
[./bot_y]
type = DirichletBC
variable = disp_x
boundary = '1 2 3'
value = 0.0
[../]
[./top_y_disp]
type = FunctionDirichletBC
variable = disp_y
boundary = 5
function = disp_ramp_vert
[../]
[]
[Materials]
[./stuff1_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e10
poissons_ratio = 0.0
[../]
[./stuff1_strain]
type = ComputeFiniteStrain
block = '1'
[../]
[./stuff1_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./stuff2_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff2_strain]
type = ComputeFiniteStrain
block = '2'
[../]
[./stuff2_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[./stuff3_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '3'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff3_strain]
type = ComputeFiniteStrain
block = '3'
[../]
[./stuff3_stress]
type = ComputeFiniteStrainElasticStress
block = '3'
[../]
[./stuff4_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '4'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff4_strain]
type = ComputeFiniteStrain
block = '4'
[../]
[./stuff4_stress]
type = ComputeFiniteStrainElasticStress
block = '4'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-7
nl_rel_tol = 1e-6
l_max_its = 50
nl_max_its = 100
start_time = 0.0
dt = 0.1
dtmin = 0.1
num_steps = 10
end_time = 1.0
l_tol = 1e-4
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '3 4 5'
sort_by = id
[../]
[./y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '3 4 5'
sort_by = id
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '4'
sort_by = id
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x281 top_react_x top_react_y x_disp y_disp cont_press'
start_time = 0.9
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./interface]
primary = 3
secondary = 4
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+11
[../]
[]
(modules/geochemistry/test/tests/solubilities_and_activities/gypsum_solubility.i)
[TimeDependentReactionSolver]
model_definition = definition
swap_out_of_basis = "Ca++"
swap_into_basis = "Gypsum"
charge_balance_species = "SO4--"
constraint_species = "H2O Cl- Na+ SO4-- Gypsum"
constraint_value = " 1.0 1E-10 1E-10 1E-6 0.5814"
constraint_meaning = "kg_solvent_water free_concentration free_concentration bulk_composition free_mineral"
constraint_unit = " kg molal molal moles moles"
source_species_names = 'NaCl'
source_species_rates = '1.0'
add_aux_pH = false # there is no H+ in the problem
ramp_max_ionic_strength_initial = 0 # not needed in this simple problem
stoichiometric_ionic_str_using_Cl_only = true # for comparison with GWB
abs_tol = 1E-12
execute_console_output_on = '' # only CSV output in this example
[]
[UserObjects]
[definition]
type = GeochemicalModelDefinition
database_file = "../../../database/moose_geochemdb.json"
basis_species = "H2O Cl- Na+ SO4-- Ca++"
equilibrium_minerals = "Gypsum"
piecewise_linear_interpolation = true # for comparison with GWB
[]
[]
[Functions]
[timestepper]
type = PiecewiseLinear
x = '0 0.1'
y = '0.01 0.1'
[]
[]
[Executioner]
type = Transient
[TimeStepper]
type = FunctionDT
function = timestepper
[]
end_time = 3
[]
[Outputs]
csv = true
[]
[AuxVariables]
[dissolved_gypsum_moles]
[]
[]
[AuxKernels]
[dissolved_gypsum_moles]
type = ParsedAux
args = 'bulk_moles_Gypsum free_mg_Gypsum'
function = 'bulk_moles_Gypsum - free_mg_Gypsum / 1000 / 172.168 '
variable = dissolved_gypsum_moles
execute_on = 'timestep_end'
[]
[]
[Postprocessors]
[cl_molal]
type = PointValue
point = '0 0 0'
variable = 'molal_Cl-'
[]
[dissolved_gypsum_mol]
type = PointValue
point = '0 0 0'
variable = dissolved_gypsum_moles
[]
[]
(test/tests/geomsearch/3d_moving_penetration/pl_test3qtt.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
file = pl_test3qtt.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./normal_z]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./closest_point_z]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[./diff_z]
type = Diffusion
variable = disp_z
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
tangential_tolerance = 0.1
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
tangential_tolerance = 0.1
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = normal_z
boundary = 11
paired_boundary = 12
quantity = normal_z
[../]
[./penetrate10]
type = PenetrationAux
variable = normal_z
boundary = 12
paired_boundary = 11
quantity = normal_z
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate13]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate14]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate15]
type = PenetrationAux
variable = closest_point_z
boundary = 11
paired_boundary = 12
quantity = closest_point_z
[../]
[./penetrate16]
type = PenetrationAux
variable = closest_point_z
boundary = 12
paired_boundary = 11
quantity = closest_point_z
[../]
[./penetrate17]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate18]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate19]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate20]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b1z]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[./b2z]
type = DirichletBC
variable = disp_z
boundary = 2
value = 0
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_abs_tol = 1e-7
l_max_its = 10
start_time = 0.0
dt = 0.0125
end_time = 1.0
[./Quadrature]
order = THIRD
[../]
[]
[Outputs]
file_base = pl_test3qtt_out
exodus = true
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_htonly/planar_yz.i)
# 1-D Gap Heat Transfer Test without mechanics
#
# This test exercises 1-D gap heat transfer for a constant conductivity gap.
#
# The mesh consists of two element blocks in the y-z plane. Each element block
# is a square. They sit next to one another with a unit between them.
#
# The conductivity of both blocks is set very large to achieve a uniform temperature
# across each block. The temperature of the far bottom boundary
# is ramped from 100 to 200 over one time unit. The temperature of the far top
# boundary is held fixed at 100.
#
# A simple analytical solution is possible for the heat flux between the blocks:
#
# Flux = (T_left - T_right) * (gapK/gap_width)
#
# The gap conductivity is specified as 1, thus
#
# gapK(Tavg) = 1.0*Tavg
#
# The heat flux across the gap at time = 1 is then:
#
# Flux = 100 * (1.0/1.0) = 100
#
# For comparison, see results from the flux post processors. These results
# are the same as for the unit 1-D gap heat transfer between two unit cubes.
[Mesh]
[file]
type = FileMeshGenerator
file = simple_2D.e
[]
[./rotate]
type = TransformGenerator
transform = ROTATE
vector_value = '0 90 90'
input = file
[../]
[]
[Functions]
[./temp]
type = PiecewiseLinear
x = '0 1 2'
y = '100 200 200'
[../]
[]
[ThermalContact]
[./thermal_contact]
type = GapHeatTransfer
variable = temp
primary = 3
secondary = 2
emissivity_primary = 0
emissivity_secondary = 0
[../]
[]
[Variables]
[./temp]
order = FIRST
family = LAGRANGE
initial_condition = 100
[../]
[]
[AuxVariables]
[./gap_cond]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[]
[BCs]
[./temp_far_bottom]
type = FunctionDirichletBC
boundary = 1
variable = temp
function = temp
[../]
[./temp_far_top]
type = DirichletBC
boundary = 4
variable = temp
value = 100
[../]
[]
[AuxKernels]
[./conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_cond
boundary = 2
[../]
[]
[Materials]
[./heat1]
type = HeatConductionMaterial
block = '1 2'
specific_heat = 1.0
thermal_conductivity = 100000000.0
[../]
[./density]
type = GenericConstantMaterial
block = '1 2'
prop_names = 'density'
prop_values = '1.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 4'
line_search = 'none'
nl_rel_tol = 1e-12
l_tol = 1e-3
l_max_its = 100
dt = 1e-1
end_time = 1.0
[]
[Postprocessors]
[./temp_bottom]
type = SideAverageValue
boundary = 2
variable = temp
execute_on = 'initial timestep_end'
[../]
[./temp_top]
type = SideAverageValue
boundary = 3
variable = temp
execute_on = 'initial timestep_end'
[../]
[./flux_bottom]
type = SideFluxIntegral
variable = temp
boundary = 2
diffusivity = thermal_conductivity
execute_on = 'initial timestep_end'
[../]
[./flux_top]
type = SideFluxIntegral
variable = temp
boundary = 3
diffusivity = thermal_conductivity
execute_on = 'initial timestep_end'
[../]
[]
[Outputs]
exodus = true
[]
(modules/geochemistry/test/tests/time_dependent_reactions/seawater_evaporation_no_flow_through.i)
#Progressively remove H2O until virtually none remains
[UserObjects]
[definition]
type = GeochemicalModelDefinition
database_file = "../../../database/moose_geochemdb.json"
basis_species = "H2O H+ Cl- Ca++ Mg++ Na+ K+ SO4-- HCO3-"
equilibrium_minerals = "Dolomite Epsomite Gypsum Halite Magnesite Mirabilite Sylvite"
equilibrium_gases = "CO2(g)"
piecewise_linear_interpolation = true # for precise agreement with GWB
[]
[]
[TimeDependentReactionSolver]
model_definition = definition
geochemistry_reactor_name = reactor
swap_out_of_basis = "H+"
swap_into_basis = " CO2(g)"
charge_balance_species = "Cl-" # this means the bulk moles of Cl- will not be exactly as set below
constraint_species = "H2O CO2(g) Cl- Na+ SO4-- Mg++ Ca++ K+ HCO3-"
constraint_value = " 1.0 -3.5 0.5656 0.4850 0.02924 0.05501 0.01063 0.010576055 0.002412"
constraint_meaning = "kg_solvent_water log10fugacity 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"
close_system_at_time = 0
source_species_names = "H2O"
source_species_rates = "-1.0" # 1kg H2O = 55.51 moles, each time step removes 1 mole
mode = mode
ramp_max_ionic_strength_initial = 0 # not needed in this simple example
stoichiometric_ionic_str_using_Cl_only = true # for precise agreement with GWB
execute_console_output_on = '' # only CSV output for this example
[]
[Functions]
[timestepper]
type = PiecewiseLinear
x = '0 50 55'
y = '5 5 1'
[]
[]
[Executioner]
type = Transient
[TimeStepper]
type = FunctionDT
function = timestepper
[]
end_time = 55
[]
[AuxVariables]
[mode]
[]
[]
[AuxKernels]
[mode]
type = FunctionAux
variable = mode
function = 'if(t<=1.0, 1.0, 0.0)' # initial "dump" then "normal"
execute_on = 'timestep_begin'
[]
[]
[GlobalParams]
point = '0 0 0'
[]
[Postprocessors]
[solvent_kg]
type = PointValue
variable = 'kg_solvent_H2O'
[]
[dolomite]
type = PointValue
variable = 'free_cm3_Dolomite'
[]
[gypsum]
type = PointValue
variable = 'free_cm3_Gypsum'
[]
[halite]
type = PointValue
variable = 'free_cm3_Halite'
[]
[mirabilite]
type = PointValue
variable = 'free_cm3_Mirabilite'
[]
[]
[Outputs]
csv = 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
[]
(modules/tensor_mechanics/test/tests/combined_creep_plasticity/combined_creep_plasticity.i)
#
# This test is Example 2 from "A Consistent Formulation for the Integration
# of Combined Plasticity and Creep" by P. Duxbury, et al., Int J Numerical
# Methods in Engineering, Vol. 37, pp. 1277-1295, 1994.
#
# The problem is a one-dimensional bar which is loaded from yield to a value of twice
# the initial yield stress and then unloaded to return to the original stress. The
# bar must harden to the required yield stress during the load ramp, with no
# further yielding during unloading. The initial yield stress (sigma_0) is prescribed
# as 20 with a plastic strain hardening of 100. The mesh is a 1x1x1 cube with symmetry
# boundary conditions on three planes to provide a uniaxial stress field.
#
# In the PowerLawCreep model, the creep strain rate is defined by:
#
# edot = A(sigma)**n * exp(-Q/(RT)) * t**m
#
# The creep law specified in the paper, however, defines the creep strain rate as:
#
# edot = Ao * mo * (sigma)**n * t**(mo-1)
# with the creep parameters given by
# Ao = 1e-7
# mo = 0.5
# n = 5
#
# thus, input parameters for the test were specified as:
# A = Ao * mo = 1e-7 * 0.5 = 0.5e-7
# m = mo-1 = -0.5
# n = 5
# Q = 0
#
# The variation of load P with time is:
# P = 20 + 20t 0 < t < 1
# P = 40 - 40(t-1) 1 < t 1.5
#
# The analytic solution for total strain during the loading period 0 < t < 1 is:
#
# e_tot = (sigma_0 + 20*t)/E + 0.2*t + A * t**0.5 * sigma_0**n * [ 1 + (5/3)*t +
# + 2*t**2 + (10/7)*t**3 + (5/9)**t**4 + (1/11)*t**5 ]
#
# and during the unloading period 1 < t < 1.5:
#
# e_tot = (sigma_1 - 40*(t-1))/E + 0.2 + (4672/693) * A * sigma_0**n +
# A * sigma_0**n * [ t**0.5 * ( 32 - (80/3)*t + 16*t**2 - (40/7)*t**3
# + (10/9)*t**4 - (1/11)*t**5 ) - (11531/693) ]
#
# where sigma_1 is the stress at time t = 1.
#
# Assuming a Young's modulus (E) of 1000 and using the parameters defined above:
#
# e_tot(1) = 2.39734
# e_tot(1.5) = 3.16813
#
#
# The numerically computed solution is:
#
# e_tot(1) = 2.39718 (~0.006% error)
# e_tot(1.5) = 3.15555 (~0.40% error)
#
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
incremental = true
add_variables = true
generate_output = 'stress_yy elastic_strain_yy creep_strain_yy plastic_strain_yy'
[../]
[]
[Functions]
[./top_pull]
type = PiecewiseLinear
x = ' 0 1 1.5'
y = '-20 -40 -20'
[../]
[./dts]
type = PiecewiseLinear
x = '0 0.5 1.0 1.5'
y = '0.015 0.015 0.005 0.005'
[../]
[]
[BCs]
[./u_top_pull]
type = Pressure
variable = disp_y
component = 1
boundary = top
factor = 1
function = top_pull
[../]
[./u_bottom_fix]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./u_yz_fix]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./u_xy_fix]
type = DirichletBC
variable = disp_z
boundary = back
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = 0
youngs_modulus = 1e3
poissons_ratio = 0.3
[../]
[./creep_plas]
type = ComputeMultipleInelasticStress
block = 0
tangent_operator = elastic
inelastic_models = 'creep plas'
max_iterations = 50
absolute_tolerance = 1e-05
combined_inelastic_strain_weights = '0.0 1.0'
[../]
[./creep]
type = PowerLawCreepStressUpdate
block = 0
coefficient = 0.5e-7
n_exponent = 5
m_exponent = -0.5
activation_energy = 0
[../]
[./plas]
type = IsotropicPlasticityStressUpdate
block = 0
hardening_constant = 100
yield_stress = 20
[../]
[]
[Executioner]
type = Transient
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options = '-snes_ksp'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 20
nl_max_its = 6
nl_rel_tol = 1e-6
nl_abs_tol = 1e-10
l_tol = 1e-5
start_time = 0.0
end_time = 1.5
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/pressure/pressure_test.i)
#
# Pressure Test
#
# This test is designed to compute pressure loads on three faces of a unit cube.
#
# The mesh is composed of one block with a single element. Symmetry bcs are
# applied to the faces opposite the pressures. Poisson's ratio is zero,
# which makes it trivial to check displacements.
#
[Mesh]
type = FileMesh
file = pressure_test.e
displacements = 'disp_x disp_y disp_z'
[]
[Functions]
[./rampConstant]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 1.'
scale_factor = 1.0
[../]
[./zeroRamp]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 0. 1.'
scale_factor = 1.0
[../]
[./rampUnramp]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 0.'
scale_factor = 10.0
[../]
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./TensorMechanics]
displacements = 'disp_x disp_y disp_z'
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 4
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = 5
value = 0.0
[../]
[./no_z]
type = DirichletBC
variable = disp_z
boundary = 6
value = 0.0
[../]
[./Pressure]
[./Side1]
boundary = 1
function = rampConstant
displacements = 'disp_x disp_y disp_z'
[../]
[./Side2]
boundary = 2
function = zeroRamp
displacements = 'disp_x disp_y disp_z'
factor = 2.0
[../]
[./Side3]
boundary = 3
function = rampUnramp
displacements = 'disp_x disp_y disp_z'
[../]
[../]
[]
[Materials]
[./Elasticity_tensor]
type = ComputeElasticityTensor
block = 1
fill_method = symmetric_isotropic
C_ijkl = '0 0.5e6'
[../]
[./strain]
type = ComputeSmallStrain
displacements = 'disp_x disp_y disp_z'
block = 1
[../]
[./stress]
type = ComputeLinearElasticStress
block = 1
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
nl_abs_tol = 1e-10
l_max_its = 20
start_time = 0.0
dt = 1.0
num_steps = 2
end_time = 2.0
[]
[Outputs]
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[]
(modules/porous_flow/test/tests/buckley_leverett/bl01.i)
# Buckley-Leverett 1-phase.
# The front starts at (around) x=5, and at t=50 it should
# have moved to x=9.6. The version below has a nonzero
# suction function, and at t=50, the front sits between
# (about) x=9.6 and x=9.9. Changing the van-Genuchten
# al parameter to 1E-4 softens the front so it sits between
# (about) x=9.7 and x=10.4, and the simulation runs much faster.
# With al=1E-2 and nx=600, the front sits between x=9.6 and x=9.8,
# but takes about 100 times longer to run.
[Mesh]
type = GeneratedMesh
dim = 1
nx = 150
xmin = 0
xmax = 15
[]
[GlobalParams]
PorousFlowDictator = dictator
compute_enthalpy = false
compute_internal_energy = false
[]
[Variables]
[pp]
[InitialCondition]
type = FunctionIC
function = 'max((1000000-x/5*1000000)-20000,-20000)'
[]
[]
[]
[Kernels]
[mass0]
type = PorousFlowMassTimeDerivative
fluid_component = 0
variable = pp
[]
[flux0]
type = PorousFlowAdvectiveFlux
fluid_component = 0
variable = pp
gravity = '0 0 0'
[]
[]
[BCs]
[left]
type = DirichletBC
variable = pp
boundary = left
value = 980000
[]
[]
[AuxVariables]
[sat]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[sat]
type = MaterialStdVectorAux
variable = sat
execute_on = timestep_end
index = 0
property = PorousFlow_saturation_qp
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureVG
m = 0.8
alpha = 1e-3
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 2e6
viscosity = 1e-3
density0 = 1000
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 = '1E-10 0 0 0 1E-10 0 0 0 1E-10'
[]
[relperm]
type = PorousFlowRelativePermeabilityCorey
n = 2
phase = 0
[]
[porosity]
type = PorousFlowPorosityConst
porosity = 0.15
[]
[]
[Preconditioning]
active = andy
[andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'gmres bjacobi 1E-10 1E-10 20'
[]
[]
[Functions]
[timestepper]
type = PiecewiseLinear
x = '0 0.01 0.1 1 1.5 2 20 30 40 50'
y = '0.01 0.1 0.2 0.3 0.1 0.3 0.3 0.4 0.4 0.5'
[]
[]
[Executioner]
type = Transient
solve_type = Newton
end_time = 50
[TimeStepper]
type = FunctionDT
function = timestepper
[]
[]
[VectorPostprocessors]
[pp]
type = LineValueSampler
start_point = '0 0 0'
end_point = '15 0 0'
num_points = 150
sort_by = x
variable = pp
[]
[sat]
type = LineValueSampler
start_point = '0 0 0'
end_point = '15 0 0'
num_points = 150
sort_by = x
variable = sat
[]
[]
[Outputs]
file_base = bl01
[csv]
type = CSV
sync_only = true
sync_times = '0.01 50'
[]
[exodus]
type = Exodus
execute_on = 'initial final'
[]
[]
(test/tests/auxkernels/time_integration/time_integration.i)
# This test covers the usage of the VariableTimeIntegrationAux
# kernel. Here we test three different schemes for integrating a field
# variable in time. Midpoint, Trapezoidal, and Simpson's rule are
# used. For this test, we use a manufactured solution and we compare
# the Trapezoidal and Simpson's rule, which must be exact for this
# exact solution, which is a linear function of time.
#
# The set up problem is
#
# du/dt - Laplacian(u) = Q
#
# with exact solution: u = t*(x*x+y*y).
[Mesh]
type = GeneratedMesh
dim = 2
elem_type = QUAD9
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 10
ny = 10
[]
[Functions]
[./dts]
type = PiecewiseLinear
x = '0.01 0.1'
y = '0.005 0.05'
[../]
[]
[Variables]
[./u]
initial_condition = 0.0
family = LAGRANGE
order = SECOND
[../]
[]
[Kernels]
active = 'diff timederivative sourceterm'
[./diff]
type = Diffusion
variable = u
[../]
[./timederivative]
type = TimeDerivative
variable = u
[../]
[./sourceterm]
type = BodyForce
variable = u
function = Source
[../]
[]
[AuxVariables]
active = 'v_midpoint v_trapazoid v_simpson'
[./v_midpoint]
[../]
[./v_trapazoid]
[../]
[./v_simpson]
[../]
[]
[AuxKernels]
[./MidpointTimeIntegrator]
type = VariableTimeIntegrationAux
variable_to_integrate = u
variable = v_midpoint
order = 1
[../]
[./TrapazoidalTimeIntegrator]
type = VariableTimeIntegrationAux
variable_to_integrate = u
variable = v_trapazoid
order = 2
[../]
[./SimpsonsTimeIntegrator]
type = VariableTimeIntegrationAux
variable_to_integrate = u
variable = v_simpson
order = 3
[../]
[]
[BCs]
active = 'RightBC LeftBC TopBC BottomBC'
[./RightBC]
type = FunctionDirichletBC
variable = u
function = RightBC
boundary = 'right'
[../]
[./LeftBC]
type = FunctionDirichletBC
variable = u
function = LeftBC
boundary = 'left'
[../]
[./TopBC]
type = FunctionDirichletBC
variable = u
function = TopBC
boundary = 'top'
[../]
[./BottomBC]
type = FunctionDirichletBC
variable = u
function = BottomBC
boundary = 'bottom'
[../]
[]
[Functions]
active = 'Soln Source TopBC BottomBC RightBC LeftBC'
[./Soln]
type = ParsedFunction
value = 't*(x*x+y*y)'
[../]
[./Source]
type = ParsedFunction
value = '(x*x + y*y) - 4*t'
[../]
[./TopBC]
type = ParsedFunction
value = 't*(x*x+1)'
[../]
[./BottomBC]
type = ParsedFunction
value = 't*x*x'
[../]
[./RightBC]
type = ParsedFunction
value = 't*(y*y+1)'
[../]
[./LeftBC]
type = ParsedFunction
value = 't*y*y'
[../]
[]
[Postprocessors]
[./l2_error]
type = NodalL2Error
variable = u
function = Soln
[../]
[]
[Executioner]
type = Transient
end_time = 0.1
# dt = 0.1
# num_steps = 10
[./TimeStepper]
type = FunctionDT
function = dts
[../]
nl_abs_tol = 1.e-15
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(modules/tensor_mechanics/test/tests/central_difference/consistent/2D/2d_consistent_implicit.i)
# Test for the central difference time integrator for a 2D mesh
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 2
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 2.0
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./vel_x]
[../]
[./accel_x]
[../]
[./vel_y]
[../]
[./accel_y]
[../]
[]
[Kernels]
[./DynamicTensorMechanics]
displacements = 'disp_x disp_y'
[../]
[./inertia_x]
type = InertialForce
variable = disp_x
[../]
[./inertia_y]
type = InertialForce
variable = disp_y
[../]
[]
[AuxKernels]
[./accel_x]
type = TestNewmarkTI
variable = accel_x
displacement = disp_x
first = false
[../]
[./vel_x]
type = TestNewmarkTI
variable = vel_x
displacement = disp_x
[../]
[./accel_y]
type = TestNewmarkTI
variable = accel_y
displacement = disp_y
first = false
[../]
[./vel_y]
type = TestNewmarkTI
variable = vel_y
displacement = disp_y
[../]
[]
[BCs]
[./y_bot]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./x_bot]
type = PresetDisplacement
boundary = bottom
variable = disp_x
beta = 0.25
velocity = vel_x
acceleration = accel_x
function = disp
[../]
[]
[Functions]
[./disp]
type = PiecewiseLinear
x = '0.0 1.0 2.0 3.0 4.0' # time
y = '0.0 1.0 0.0 -1.0 0.0' # displacement
[../]
[]
[Materials]
[./elasticity_tensor_block]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.25
block = 0
[../]
[./strain_block]
type = ComputeIncrementalSmallStrain
block = 0
displacements = 'disp_x disp_y'
[../]
[./stress_block]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = density
prop_values = 1e4
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
nl_abs_tol = 1e-11
nl_rel_tol = 1e-11
start_time = -0.01
end_time = 0.1
dt = 0.005
timestep_tolerance = 1e-6
[./TimeIntegrator]
type = NewmarkBeta
beta = 0.25
gamma = 0.5
[../]
[]
[Postprocessors]
[./_dt]
type = TimestepSize
[../]
[./accel_2x]
type = PointValue
point = '1.0 2.0 0.0'
variable = accel_x
[../]
[./accel_2y]
type = PointValue
point = '1.0 2.0 0.0'
variable = accel_y
[../]
[]
[Outputs]
exodus = false
csv = true
[]
(modules/tensor_mechanics/test/tests/smeared_cracking/cracking_power.i)
#
# Simple test of power law softening law for smeared cracking.
# Upon reaching the failure stress in the x direction, the
# softening model abruptly reduces the stress to a fraction
# of its original value, and re-loading occurs at a reduced
# stiffness. This is repeated multiple times.
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Functions]
[./displ]
type = PiecewiseLinear
x = '0 1 2 3 4'
y = '0 1 0 -1 0'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx'
[../]
[]
[BCs]
[./pull]
type = FunctionDirichletBC
variable = disp_x
boundary = right
function = displ
[../]
[./left]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./bottom]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./back]
type = DirichletBC
variable = disp_z
boundary = back
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 2.8e7
poissons_ratio = 0
[../]
[./elastic_stress]
type = ComputeSmearedCrackingStress
cracking_stress = 1.68e6
softening_models = power_law_softening
[../]
[./power_law_softening]
type = PowerLawSoftening
stiffness_reduction = 0.3333
[../]
[]
[Executioner]
type = Transient
petsc_options_iname = '-ksp_gmres_restart -pc_type -sub_pc_type'
petsc_options_value = '101 asm lu'
line_search = 'none'
l_max_its = 100
nl_max_its = 100
nl_rel_tol = 1e-8
nl_abs_tol = 1e-8
l_tol = 1e-5
start_time = 0.0
end_time = 1.0
dt = 0.01
[]
[Outputs]
exodus = true
[]
(modules/combined/test/tests/fdp_geometric_coupling/fdp_geometric_coupling.i)
[Mesh]
file = twoBlocksContactDiceSecondary2OffsetGap.e
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[./temp]
initial_condition = 100.0
[../]
[]
[Functions]
[./pressure]
type = PiecewiseLinear
x = '0 1 2'
y = '0 1 1'
scale_factor = 10.0
[../]
[./tempFunc]
type = PiecewiseLinear
x = '0. 3.'
y = '100.0 440.0'
[../]
[]
[Modules/TensorMechanics/Master]
[./block1]
block = 1
volumetric_locking_correction = true
incremental = true
strain = FINITE
eigenstrain_names = 'thermal_expansion1'
decomposition_method = EigenSolution
[../]
[./block2]
block = 2
volumetric_locking_correction = true
incremental = true
strain = FINITE
eigenstrain_names = 'thermal_expansion2'
decomposition_method = EigenSolution
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[]
[BCs]
[./left_right_x]
type = DirichletBC
variable = disp_x
boundary = '1 4'
value = 0.0
[../]
[./left_right_y]
type = DirichletBC
variable = disp_y
boundary = '1 4'
value = 0.0
[../]
[./left_right_z]
type = DirichletBC
variable = disp_z
boundary = '1 4'
value = 0.0
[../]
[./temp]
type = FunctionDirichletBC
variable = temp
boundary = '2 3'
function = tempFunc
[../]
[]
[Contact]
[./dummy_name]
primary = 2
secondary = 3
penalty = 1e8
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = '1 2'
youngs_modulus = 1e6
poissons_ratio = 0.0
[../]
[./stress1]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[../]
[./thermal_expansion1]
type = ComputeThermalExpansionEigenstrain
block = 1
thermal_expansion_coeff = 1e-4
stress_free_temperature = 100.0
temperature = temp
eigenstrain_name = thermal_expansion1
[../]
[./thermal_expansion2]
type = ComputeThermalExpansionEigenstrain
block = 2
thermal_expansion_coeff = 1e-5
stress_free_temperature = 100.0
temperature = temp
eigenstrain_name = thermal_expansion2
[../]
[./heat]
type = HeatConductionMaterial
block = '1 2'
specific_heat = 1.0
thermal_conductivity = 1.0
[../]
[./density]
type = Density
block = '1 2'
density = 1.0
[../]
[]
[Preconditioning]
[./FDP]
type = FDP
full = true
implicit_geometric_coupling = true
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -mat_fd_coloring_err -mat_fd_type'
petsc_options_value = 'lu 1e-8 ds'
nl_rel_tol = 1e-10
l_max_its = 5
nl_max_its = 3
dt = 5.0e-1
num_steps = 2
[]
[Outputs]
file_base = fdp_geometric_coupling_out
exodus = true
[]
(modules/tensor_mechanics/test/tests/domain_integral_thermal/j_integral_2d_inst_ctefunc.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[Mesh]
file = crack2d.e
[]
[AuxVariables]
[./SED]
order = CONSTANT
family = MONOMIAL
[../]
[./temp]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
[./tempfunc]
type = ParsedFunction
value = 10.0*(2*x/504)
[../]
[./cte_func_inst]
type = PiecewiseLinear
xy_data = '-10 -10
10 10'
scale_factor = 1e-6
[../]
[]
[DomainIntegral]
integrals = JIntegral
boundary = 800
crack_direction_method = CrackDirectionVector
crack_direction_vector = '1 0 0'
2d = true
axis_2d = 2
radius_inner = '60.0 80.0 100.0 120.0'
radius_outer = '80.0 100.0 120.0 140.0'
temperature = temp
incremental = true
eigenstrain_names = thermal_expansion
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
planar_formulation = PLANE_STRAIN
eigenstrain_names = thermal_expansion
[../]
[]
[AuxKernels]
[./SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[../]
[./tempfuncaux]
type = FunctionAux
variable = temp
function = tempfunc
block = 1
[../]
[]
[BCs]
[./crack_y]
type = DirichletBC
variable = disp_y
boundary = 100
value = 0.0
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = 400
value = 0.0
[../]
[./no_x1]
type = DirichletBC
variable = disp_x
boundary = 900
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeFiniteStrainElasticStress
[../]
[./thermal_expansion_strain]
type = ComputeInstantaneousThermalExpansionFunctionEigenstrain
block = 1
thermal_expansion_function = cte_func_inst
stress_free_temperature = 0.0
temperature = temp
eigenstrain_name = thermal_expansion
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_ksp_type -sub_pc_type -pc_asm_overlap'
petsc_options_value = 'asm 31 preonly lu 1'
line_search = 'none'
l_max_its = 50
nl_max_its = 40
nl_rel_step_tol= 1e-10
nl_rel_tol = 1e-10
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Outputs]
csv = true
execute_on = 'timestep_end'
[]
[Preconditioning]
[./smp]
type = SMP
pc_side = left
ksp_norm = preconditioned
full = true
[../]
[]
(modules/combined/test/tests/ad_power_law_creep/power_law_creep_restart1.i)
# 1x1x1 unit cube with uniform pressure on top face
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
[]
[Variables]
[./temp]
order = FIRST
family = LAGRANGE
initial_condition = 1000.0
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
incremental = true
add_variables = true
generate_output = 'stress_yy creep_strain_xx creep_strain_yy creep_strain_zz elastic_strain_yy'
use_automatic_differentiation = true
[../]
[]
[Functions]
[./top_pull]
type = PiecewiseLinear
x = '0 1'
y = '1 1'
[../]
[]
[Kernels]
[./heat]
type = ADHeatConduction
variable = temp
[../]
[./heat_ie]
type = ADHeatConductionTimeDerivative
variable = temp
[../]
[]
[BCs]
[./u_top_pull]
type = ADPressure
variable = disp_y
component = 1
boundary = top
constant = -10.0e6
function = top_pull
[../]
[./u_bottom_fix]
type = ADDirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./u_yz_fix]
type = ADDirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./u_xy_fix]
type = ADDirichletBC
variable = disp_z
boundary = back
value = 0.0
[../]
[./temp_fix]
type = DirichletBC
variable = temp
boundary = 'bottom top'
value = 1000.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 2e11
poissons_ratio = 0.3
constant_on = SUBDOMAIN
[../]
[./radial_return_stress]
type = ADComputeMultipleInelasticStress
inelastic_models = 'power_law_creep'
[../]
[./power_law_creep]
type = ADPowerLawCreepStressUpdate
coefficient = 1.0e-15
n_exponent = 4
activation_energy = 3.0e5
temperature = temp
[../]
[./thermal]
type = ADHeatConductionMaterial
specific_heat = 1.0
thermal_conductivity = 100.
[../]
[./density]
type = ADDensity
density = 1.0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 20
nl_max_its = 20
nl_rel_tol = 1e-6
nl_abs_tol = 1e-6
l_tol = 1e-5
start_time = 0.0
end_time = 1.0
num_steps = 6
dt = 0.1
[]
[Outputs]
exodus = true
csv = true
[./out]
type = Checkpoint
num_files = 1
[../]
[]
(modules/tensor_mechanics/test/tests/ad_thermal_expansion_function/small_const.i)
# This tests the thermal expansion coefficient function using both
# options to specify that function: mean and instantaneous. There
# two blocks, each containing a single element, and these use the
# two variants of the function.
# In this test, the instantaneous CTE function has a constant value,
# while the mean CTE function is an analytic function designed to
# give the same response. If \bar{alpha}(T) is the mean CTE function,
# and \alpha(T) is the instantaneous CTE function,
# \bar{\alpha}(T) = 1/(T-Tref) \intA^{T}_{Tsf} \alpha(T) dT
# where Tref is the reference temperature used to define the mean CTE
# function, and Tsf is the stress-free temperature.
# This version of the test uses small deformation theory. The results
# from the two models are identical.
[Mesh]
file = 'blocks.e'
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[AuxVariables]
[./temp]
order = FIRST
family = LAGRANGE
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
add_variables = true
eigenstrain_names = eigenstrain
generate_output = 'strain_xx strain_yy strain_zz'
use_automatic_differentiation = true
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = disp_x
boundary = 3
value = 0.0
[../]
[./bottom]
type = DirichletBC
variable = disp_y
boundary = 2
value = 0.0
[../]
[./back]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0.0
[../]
[]
[AuxKernels]
[./temp]
type = FunctionAux
variable = temp
block = '1 2'
function = temp_func
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./small_stress]
type = ADComputeLinearElasticStress
[../]
[./thermal_expansion_strain1]
type = ADComputeMeanThermalExpansionFunctionEigenstrain
block = 1
thermal_expansion_function = cte_func_mean
thermal_expansion_function_reference_temperature = 0.5
stress_free_temperature = 0.0
temperature = temp
eigenstrain_name = eigenstrain
[../]
[./thermal_expansion_strain2]
type = ADComputeInstantaneousThermalExpansionFunctionEigenstrain
block = 2
thermal_expansion_function = cte_func_inst
stress_free_temperature = 0.0
temperature = temp
eigenstrain_name = eigenstrain
[../]
[]
[Functions]
[./cte_func_mean]
type = ParsedFunction
vars = 'tsf tref scale' #stress free temp, reference temp, scale factor
vals = '0.0 0.5 1e-4'
value = 'scale * (t - tsf) / (t - tref)'
[../]
[./cte_func_inst]
type = PiecewiseLinear
xy_data = '0 1.0
2 1.0'
scale_factor = 1e-4
[../]
[./temp_func]
type = PiecewiseLinear
xy_data = '0 1
1 2'
[../]
[]
[Postprocessors]
[./disp_1]
type = NodalMaxValue
variable = disp_x
boundary = 101
[../]
[./disp_2]
type = NodalMaxValue
variable = disp_x
boundary = 102
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
l_max_its = 100
l_tol = 1e-4
nl_abs_tol = 1e-8
nl_rel_tol = 1e-12
start_time = 0.0
end_time = 1.0
dt = 0.1
[]
[Outputs]
csv = true
[]
(modules/tensor_mechanics/test/tests/dynamics/rayleigh_damping/rayleigh_hht_ti.i)
# Test for rayleigh damping implemented using HHT time integration
#
# The test is for an 1D bar element of unit length fixed on one end
# with a ramped pressure boundary condition applied to the other end.
# zeta and eta correspond to the stiffness and mass proportional rayleigh damping
# alpha, beta and gamma are HHT time integration parameters
# The equation of motion in terms of matrices is:
#
# M*accel + (eta*M+zeta*K)*[(1+alpha)vel-alpha vel_old]
# + alpha*(K*disp - K*disp_old) + K*disp = P(t+alpha dt)*Area
#
# Here M is the mass matrix, K is the stiffness matrix, P is the applied pressure
#
# This equation is equivalent to:
#
# density*accel + eta*density*[(1+alpha)vel-alpha vel_old]
# + zeta*[(1+alpha)*d/dt(Div stress)- alpha*d/dt(Div stress_old)]
# + alpha *(Div stress - Div stress_old) +Div Stress= P(t+alpha dt)
#
# The first two terms on the left are evaluated using the Inertial force kernel
# The next three terms on the left involving zeta and alpha are evaluated using
# the DynamicStressDivergenceTensors Kernel
# The residual due to Pressure is evaluated using Pressure boundary condition
#
# The system will come to steady state slowly after the pressure becomes constant.
# Alpha equal to zero will result in Newmark integration.
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = 0.0
xmax = 0.1
ymin = 0.0
ymax = 1.0
zmin = 0.0
zmax = 0.1
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./vel_x]
[../]
[./accel_x]
[../]
[./vel_y]
[../]
[./accel_y]
[../]
[./vel_z]
[../]
[./accel_z]
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./DynamicTensorMechanics]
displacements = 'disp_x disp_y disp_z'
zeta = 0.1
alpha = 0.11
[../]
[./inertia_x]
type = InertialForce
variable = disp_x
eta=0.1
alpha = 0.11
[../]
[./inertia_y]
type = InertialForce
variable = disp_y
eta=0.1
alpha = 0.11
[../]
[./inertia_z]
type = InertialForce
variable = disp_z
eta = 0.1
alpha = 0.11
[../]
[]
[AuxKernels]
[./accel_x] # These auxkernels are only to check output
type = TestNewmarkTI
displacement = disp_x
variable = accel_x
first = false
[../]
[./accel_y]
type = TestNewmarkTI
displacement = disp_y
variable = accel_y
first = false
[../]
[./accel_z]
type = TestNewmarkTI
displacement = disp_z
variable = accel_z
first = false
[../]
[./vel_x]
type = TestNewmarkTI
displacement = disp_x
variable = vel_x
[../]
[./vel_y]
type = TestNewmarkTI
displacement = disp_y
variable = vel_y
[../]
[./vel_z]
type = TestNewmarkTI
displacement = disp_z
variable = vel_z
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 0
index_j = 1
[../]
[./strain_yy]
type = RankTwoAux
rank_two_tensor = total_strain
variable = strain_yy
index_i = 0
index_j = 1
[../]
[]
[BCs]
[./top_y]
type = DirichletBC
variable = disp_y
boundary = top
value=0.0
[../]
[./top_x]
type = DirichletBC
variable = disp_x
boundary = top
value=0.0
[../]
[./top_z]
type = DirichletBC
variable = disp_z
boundary = top
value=0.0
[../]
[./bottom_x]
type = DirichletBC
variable = disp_x
boundary = bottom
value=0.0
[../]
[./bottom_z]
type = DirichletBC
variable = disp_z
boundary = bottom
value=0.0
[../]
[./Pressure]
[./Side1]
boundary = bottom
function = pressure
displacements = 'disp_x disp_y disp_z'
factor = 1
alpha = 0.11
[../]
[../]
[]
[Materials]
[./Elasticity_tensor]
type = ComputeElasticityTensor
block = 0
fill_method = symmetric_isotropic
C_ijkl = '210e9 0'
[../]
[./strain]
type = ComputeSmallStrain
block = 0
displacements = 'disp_x disp_y disp_z'
[../]
[./stress]
type = ComputeLinearElasticStress
block = 0
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = 'density'
prop_values = '7750'
[../]
[]
[Executioner]
type = Transient
start_time = 0
end_time = 2
dt = 0.1
# Time integrator scheme
scheme = "newmark-beta"
[]
[Functions]
[./pressure]
type = PiecewiseLinear
x = '0.0 0.1 0.2 1.0 2.0 5.0'
y = '0.0 0.1 0.2 1.0 1.0 1.0'
scale_factor = 1e9
[../]
[]
[Postprocessors]
[./_dt]
type = TimestepSize
[../]
[./disp]
type = NodalMaxValue
variable = disp_y
boundary = bottom
[../]
[./vel]
type = NodalMaxValue
variable = vel_y
boundary = bottom
[../]
[./accel]
type = NodalMaxValue
variable = accel_y
boundary = bottom
[../]
[./stress_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./strain_yy]
type = ElementAverageValue
variable = strain_yy
[../]
[]
[Outputs]
file_base = 'rayleigh_hht_out'
exodus = true
perf_graph = true
[]
(modules/contact/test/tests/verification/hertz_cyl/half_symm_q8/hertz_cyl_half_1deg_template1.i)
[GlobalParams]
order = SECOND
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Mesh]
file = hertz_cyl_half_1deg.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Functions]
[./disp_ramp_vert]
type = PiecewiseLinear
x = '0. 1. 3.5'
y = '0. -0.0020 -0.0020'
[../]
[./disp_ramp_horz]
type = PiecewiseLinear
x = '0. 1. 3.5'
y = '0. 0.0 0.0014'
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
[../]
[]
[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_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 2
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 2
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 4
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 4
[../]
[./disp_x639]
type = NodalVariableValue
nodeid = 638
variable = disp_x
[../]
[./disp_y639]
type = NodalVariableValue
nodeid = 638
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./side_x]
type = DirichletBC
variable = disp_y
boundary = '1 2'
value = 0.0
[../]
[./bot_y]
type = DirichletBC
variable = disp_x
boundary = '1 2'
value = 0.0
[../]
[./top_y_disp]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = disp_ramp_vert
[../]
[./top_x_disp]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = disp_ramp_horz
[../]
[]
[Materials]
[./stuff1_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e10
poissons_ratio = 0.0
[../]
[./stuff1_strain]
type = ComputeFiniteStrain
block = '1'
[../]
[./stuff1_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./stuff2_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff2_strain]
type = ComputeFiniteStrain
block = '2'
[../]
[./stuff2_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[./stuff3_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '3'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff3_strain]
type = ComputeFiniteStrain
block = '3'
[../]
[./stuff3_stress]
type = ComputeFiniteStrainElasticStress
block = '3'
[../]
[./stuff4_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '4'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff4_strain]
type = ComputeFiniteStrain
block = '4'
[../]
[./stuff4_stress]
type = ComputeFiniteStrainElasticStress
block = '4'
[../]
[./stuff5_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '5'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff5_strain]
type = ComputeFiniteStrain
block = '5'
[../]
[./stuff5_stress]
type = ComputeFiniteStrainElasticStress
block = '5'
[../]
[./stuff6_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '6'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff6_strain]
type = ComputeFiniteStrain
block = '6'
[../]
[./stuff6_stress]
type = ComputeFiniteStrainElasticStress
block = '6'
[../]
[./stuff7_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '7'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff7_strain]
type = ComputeFiniteStrain
block = '7'
[../]
[./stuff7_stress]
type = ComputeFiniteStrainElasticStress
block = '7'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-6
nl_rel_tol = 1e-5
l_max_its = 100
nl_max_its = 200
start_time = 0.0
end_time = 3.5
l_tol = 1e-3
dt = 0.1
dtmin = 0.1
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '3 4'
sort_by = id
[../]
[./y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '3 4'
sort_by = id
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = id
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'x_disp y_disp cont_press'
start_time = 0.9
execute_vector_postprocessors_on = timestep_end
[../]
[./chkfile2]
type = CSV
show = 'bot_react_x bot_react_y disp_x639 disp_y639 top_react_x top_react_y'
start_time = 0.9
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./interface]
primary = 2
secondary = 3
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+10
[../]
[]
(modules/tensor_mechanics/test/tests/substepping/power_law_creep.i)
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
nx = 2
ny = 2
nz = 2
[../]
[]
[AuxVariables]
[./temp]
initial_condition = 1000.0
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_zz elastic_strain_zz creep_strain_zz'
use_automatic_differentiation = false
[../]
[]
[Functions]
[./front_pull]
type = PiecewiseLinear
x = '0 1'
y = '0 1'
scale_factor = 0.5
[../]
[]
[BCs]
[./u_front_pull]
type = ADFunctionDirichletBC
variable = disp_z
boundary = front
function = front_pull
[../]
[./uz_back_fix]
type = ADDirichletBC
variable = disp_z
boundary = back
value = 0.0
[../]
[./u_yz_fix]
type = ADDirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./u_xz_fix]
type = ADDirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 2e11
poissons_ratio = 0.3
[../]
[./radial_return_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'power_law_creep'
[../]
[./power_law_creep]
type = PowerLawCreepStressUpdate
coefficient = 1.0e-15
n_exponent = 4
activation_energy = 0.0
temperature = temp
# options for using substepping
use_substep = true
substep_strain_tolerance = 0.1
max_inelastic_increment = 0.01
[../]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type '
petsc_options_value = 'lu '
line_search = 'none'
nl_max_its = 10
nl_rel_tol = 1e-6
nl_abs_tol = 1e-10
end_time = 0.1
dt = 0.1
[]
[Outputs]
exodus = true
[]
(modules/porous_flow/test/tests/poro_elasticity/mandel_basicthm.i)
# using a BasicTHM Action
#
# Mandel's problem of consolodation of a drained medium
# Using the FullySaturatedDarcyBase and FullySaturatedFullySaturatedMassTimeDerivative kernels
# with multiply_by_density = false, so that this problem becomes linear
# Note the use of consistent_with_displaced_mesh = false in the calculation of volumetric strain
#
# A sample is in plane strain.
# -a <= x <= a
# -b <= y <= b
# It is squashed with constant force by impermeable, frictionless plattens on its top and bottom surfaces (at y=+/-b)
# Fluid is allowed to leak out from its sides (at x=+/-a)
# The porepressure within the sample is monitored.
#
# As is common in the literature, this is simulated by
# considering the quarter-sample, 0<=x<=a and 0<=y<=b, with
# impermeable, roller BCs at x=0 and y=0 and y=b.
# Porepressure is fixed at zero on x=a.
# Porepressure and displacement are initialised to zero.
# Then the top (y=b) is moved downwards with prescribed velocity,
# so that the total force that is inducing this downwards velocity
# is fixed. The velocity is worked out by solving Mandel's problem
# analytically, and the total force is monitored in the simulation
# to check that it indeed remains constant.
#
# Here are the problem's parameters, and their values:
# Soil width. a = 1
# Soil height. b = 0.1
# Soil's Lame lambda. la = 0.5
# Soil's Lame mu, which is also the Soil's shear modulus. mu = G = 0.75
# Soil bulk modulus. K = la + 2*mu/3 = 1
# Drained Poisson ratio. nu = (3K - 2G)/(6K + 2G) = 0.2
# Soil bulk compliance. 1/K = 1
# Fluid bulk modulus. Kf = 8
# Fluid bulk compliance. 1/Kf = 0.125
# Soil initial porosity. phi0 = 0.1
# Biot coefficient. alpha = 0.6
# Biot modulus. M = 1/(phi0/Kf + (alpha - phi0)(1 - alpha)/K) = 4.705882
# Undrained bulk modulus. Ku = K + alpha^2*M = 2.694118
# Undrained Poisson ratio. nuu = (3Ku - 2G)/(6Ku + 2G) = 0.372627
# Skempton coefficient. B = alpha*M/Ku = 1.048035
# Fluid mobility (soil permeability/fluid viscosity). k = 1.5
# Consolidation coefficient. c = 2*k*B^2*G*(1-nu)*(1+nuu)^2/9/(1-nuu)/(nuu-nu) = 3.821656
# Normal stress on top. F = 1
#
# The solution for porepressure and displacements is given in
# AHD Cheng and E Detournay "A direct boundary element method for plane strain poroelasticity" International Journal of Numerical and Analytical Methods in Geomechanics 12 (1988) 551-572.
# The solution involves complicated infinite series, so I shall not write it here
[Mesh]
type = GeneratedMesh
dim = 3
nx = 10
ny = 1
nz = 1
xmin = 0
xmax = 1
ymin = 0
ymax = 0.1
zmin = 0
zmax = 1
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
PorousFlowDictator = dictator
block = 0
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[disp_z]
[]
[porepressure]
[]
[]
[BCs]
[roller_xmin]
type = DirichletBC
variable = disp_x
value = 0
boundary = 'left'
[]
[roller_ymin]
type = DirichletBC
variable = disp_y
value = 0
boundary = 'bottom'
[]
[plane_strain]
type = DirichletBC
variable = disp_z
value = 0
boundary = 'back front'
[]
[xmax_drained]
type = DirichletBC
variable = porepressure
value = 0
boundary = right
[]
[top_velocity]
type = FunctionDirichletBC
variable = disp_y
function = top_velocity
boundary = top
[]
[]
[Functions]
[top_velocity]
type = PiecewiseLinear
x = '0 0.002 0.006 0.014 0.03 0.046 0.062 0.078 0.094 0.11 0.126 0.142 0.158 0.174 0.19 0.206 0.222 0.238 0.254 0.27 0.286 0.302 0.318 0.334 0.35 0.366 0.382 0.398 0.414 0.43 0.446 0.462 0.478 0.494 0.51 0.526 0.542 0.558 0.574 0.59 0.606 0.622 0.638 0.654 0.67 0.686 0.702'
y = '-0.041824842 -0.042730269 -0.043412712 -0.04428867 -0.045509181 -0.04645965 -0.047268246 -0.047974749 -0.048597109 -0.0491467 -0.049632388 -0.050061697 -0.050441198 -0.050776675 -0.051073238 -0.0513354 -0.051567152 -0.051772022 -0.051953128 -0.052113227 -0.052254754 -0.052379865 -0.052490464 -0.052588233 -0.052674662 -0.052751065 -0.052818606 -0.052878312 -0.052931093 -0.052977751 -0.053018997 -0.053055459 -0.053087691 -0.053116185 -0.053141373 -0.05316364 -0.053183324 -0.053200724 -0.053216106 -0.053229704 -0.053241725 -0.053252351 -0.053261745 -0.053270049 -0.053277389 -0.053283879 -0.053289615'
[]
[]
[AuxVariables]
[tot_force]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[tot_force]
type = ParsedAux
args = 'stress_yy porepressure'
execute_on = timestep_end
variable = tot_force
function = '-stress_yy+0.6*porepressure'
[]
[]
[Modules]
[FluidProperties]
[the_simple_fluid]
type = SimpleFluidProperties
thermal_expansion = 0.0
bulk_modulus = 8.0
viscosity = 1.0
density0 = 1.0
[]
[]
[]
[PorousFlowBasicTHM]
coupling_type = HydroMechanical
displacements = 'disp_x disp_y disp_z'
multiply_by_density = false
porepressure = porepressure
biot_coefficient = 0.6
gravity = '0 0 0'
fp = the_simple_fluid
[]
[Materials]
[elasticity_tensor]
type = ComputeElasticityTensor
C_ijkl = '0.5 0.75'
# bulk modulus is lambda + 2*mu/3 = 0.5 + 2*0.75/3 = 1
fill_method = symmetric_isotropic
[]
[strain]
type = ComputeSmallStrain
[]
[stress]
type = ComputeLinearElasticStress
[]
[porosity]
type = PorousFlowPorosityConst # only the initial value of this is ever used
porosity = 0.1
[]
[biot_modulus]
type = PorousFlowConstantBiotModulus
biot_coefficient = 0.6
solid_bulk_compliance = 1
fluid_bulk_modulus = 8
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1.5 0 0 0 1.5 0 0 0 1.5'
[]
[]
[Postprocessors]
[p0]
type = PointValue
outputs = csv
point = '0.0 0 0'
variable = porepressure
[]
[p1]
type = PointValue
outputs = csv
point = '0.1 0 0'
variable = porepressure
[]
[p2]
type = PointValue
outputs = csv
point = '0.2 0 0'
variable = porepressure
[]
[p3]
type = PointValue
outputs = csv
point = '0.3 0 0'
variable = porepressure
[]
[p4]
type = PointValue
outputs = csv
point = '0.4 0 0'
variable = porepressure
[]
[p5]
type = PointValue
outputs = csv
point = '0.5 0 0'
variable = porepressure
[]
[p6]
type = PointValue
outputs = csv
point = '0.6 0 0'
variable = porepressure
[]
[p7]
type = PointValue
outputs = csv
point = '0.7 0 0'
variable = porepressure
[]
[p8]
type = PointValue
outputs = csv
point = '0.8 0 0'
variable = porepressure
[]
[p9]
type = PointValue
outputs = csv
point = '0.9 0 0'
variable = porepressure
[]
[p99]
type = PointValue
outputs = csv
point = '1 0 0'
variable = porepressure
[]
[xdisp]
type = PointValue
outputs = csv
point = '1 0.1 0'
variable = disp_x
[]
[ydisp]
type = PointValue
outputs = csv
point = '1 0.1 0'
variable = disp_y
[]
[total_downwards_force]
type = ElementAverageValue
outputs = csv
variable = tot_force
[]
[dt]
type = FunctionValuePostprocessor
outputs = console
function = if(0.15*t<0.01,0.15*t,0.01)
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'gmres asm lu 1E-14 1E-10 10000'
[]
[]
[Executioner]
type = Transient
solve_type = Newton
start_time = 0
end_time = 0.7
[TimeStepper]
type = PostprocessorDT
postprocessor = dt
dt = 0.001
[]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = mandel_basicthm
[csv]
interval = 3
type = CSV
[]
[]
(modules/tensor_mechanics/test/tests/beam/dynamic/dyn_euler_small_added_mass_dyn_variable_action.i)
# Test for small strain euler beam vibration in y direction
# The velocity and acceleration AuxVariables and the corresponding AuxKernels
# are set up using the LineElementAction using add_dynamic_variables. The action
# also creates the displacement variables, stress divergence kernels and
# beam strain. NodalTranslationalInertia is not created by the action.
# An impulse load is applied at the end of a cantilever beam of length 4m.
# The beam is massless with a lumped mass at the end of the beam
# The properties of the cantilever beam are as follows:
# Young's modulus (E) = 1e4
# Shear modulus (G) = 4e7
# Shear coefficient (k) = 1.0
# Cross-section area (A) = 0.01
# Iy = 1e-4 = Iz
# Length (L)= 4 m
# mass (m) = 0.01899772
# For this beam, the dimensionless parameter alpha = kAGL^2/EI = 6.4e6
# Therefore, the beam behaves like a Euler-Bernoulli beam.
# The theoretical first frequency of this beam is:
# f1 = 1/(2 pi) * sqrt(3EI/(mL^3)) = 0.25
# This implies that the corresponding time period of this beam is 4s.
# The FEM solution for this beam with 10 element gives time periods of 4s with time step of 0.01s.
# A higher time step of 0.1 s is used in the test to reduce computational time.
# The time history from this analysis matches with that obtained from Abaqus.
# Values from the first few time steps are as follows:
# time disp_y vel_y accel_y
# 0.0 0.0 0.0 0.0
# 0.1 0.0013076435060869 0.026152870121738 0.52305740243477
# 0.2 0.0051984378734383 0.051663017225289 -0.01285446036375
# 0.3 0.010269120909367 0.049750643493289 -0.02539301427625
# 0.4 0.015087433925158 0.046615616822532 -0.037307519138892
# 0.5 0.019534963888307 0.042334982440433 -0.048305168503101
[Mesh]
type = GeneratedMesh
xmin = 0.0
xmax = 4.0
nx = 10
dim = 1
displacements = 'disp_x disp_y disp_z'
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./fixy1]
type = DirichletBC
variable = disp_y
boundary = left
value = 0.0
[../]
[./fixz1]
type = DirichletBC
variable = disp_z
boundary = left
value = 0.0
[../]
[./fixr1]
type = DirichletBC
variable = rot_x
boundary = left
value = 0.0
[../]
[./fixr2]
type = DirichletBC
variable = rot_y
boundary = left
value = 0.0
[../]
[./fixr3]
type = DirichletBC
variable = rot_z
boundary = left
value = 0.0
[../]
[]
[NodalKernels]
[./force_y2]
type = UserForcingFunctionNodalKernel
variable = disp_y
boundary = right
function = force
[../]
[./x_inertial]
type = NodalTranslationalInertia
variable = disp_x
velocity = vel_x
acceleration = accel_x
boundary = right
beta = 0.25
gamma = 0.5
mass = 0.01899772
[../]
[./y_inertial]
type = NodalTranslationalInertia
variable = disp_y
velocity = vel_y
acceleration = accel_y
boundary = right
beta = 0.25
gamma = 0.5
mass = 0.01899772
[../]
[./z_inertial]
type = NodalTranslationalInertia
variable = disp_z
velocity = vel_z
acceleration = accel_z
boundary = right
beta = 0.25
gamma = 0.5
mass = 0.01899772
[../]
[]
[Functions]
[./force]
type = PiecewiseLinear
x = '0.0 0.1 0.2 10.0'
y = '0.0 1e-2 0.0 0.0'
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options_iname = '-ksp_type -pc_type'
petsc_options_value = 'preonly lu'
dt = 0.1
end_time = 5.0
timestep_tolerance = 1e-6
[]
[Modules/TensorMechanics/LineElementMaster]
[./all]
add_variables = true
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
# Geometry parameters
area = 0.01
Iy = 1e-4
Iz = 1e-4
y_orientation = '0.0 1.0 0.0'
# Add AuxVariables and AuxKernels for dynamic simulation
add_dynamic_variables = true
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y rot_vel_z'
rotational_accelerations = 'rot_accel_x rot_accel_y rot_accel_z'
beta = 0.25 # Newmark time integration parameter
gamma = 0.5 # Newmark time integration parameter
[../]
[]
[Materials]
[./elasticity]
type = ComputeElasticityBeam
youngs_modulus = 1.0e4
poissons_ratio = -0.999875
shear_coefficient = 1.0
block = 0
[../]
[./stress]
type = ComputeBeamResultants
block = 0
[../]
[]
[Postprocessors]
[./disp_x]
type = PointValue
point = '4.0 0.0 0.0'
variable = disp_x
[../]
[./disp_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = disp_y
[../]
[./vel_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = vel_y
[../]
[./accel_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = accel_y
[../]
[]
[Outputs]
file_base = 'dyn_euler_small_added_mass_out'
hide = 'rot_vel_x rot_vel_y rot_vel_z rot_accel_x rot_accel_y rot_accel_z'
exodus = true
csv = true
[]
(modules/tensor_mechanics/test/tests/central_difference/lumped/3D/3d_nodalmass_explicit.i)
# Test for the CentralDifference time integrator
[Mesh]
[./generated_mesh]
type = GeneratedMeshGenerator
dim = 3
nx = 1
ny = 1
nz = 2
xmin = 0.0
xmax = 1
ymin = 0.0
ymax = 1
zmin = 0.0
zmax = 2
[../]
[./all_nodes]
type = BoundingBoxNodeSetGenerator
new_boundary = 'all'
input = 'generated_mesh'
top_right = '1 1 2'
bottom_left = '0 0 0'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./vel_x]
[../]
[./accel_x]
[../]
[./vel_y]
[../]
[./accel_y]
[../]
[./vel_z]
[../]
[./accel_z]
[../]
[]
[Kernels]
[./DynamicTensorMechanics]
displacements = 'disp_x disp_y disp_z'
[../]
[]
[AuxKernels]
[./accel_x]
type = TestNewmarkTI
variable = accel_x
displacement = disp_x
first = false
[../]
[./vel_x]
type = TestNewmarkTI
variable = vel_x
displacement = disp_x
[../]
[./accel_y]
type = TestNewmarkTI
variable = accel_y
displacement = disp_y
first = false
[../]
[./vel_y]
type = TestNewmarkTI
variable = vel_y
displacement = disp_y
[../]
[./accel_z]
type = TestNewmarkTI
variable = accel_z
displacement = disp_z
first = false
[../]
[./vel_z]
type = TestNewmarkTI
variable = vel_z
displacement = disp_z
[../]
[]
[BCs]
[./x_bot]
type = FunctionDirichletBC
boundary = 'back'
variable = disp_x
function = dispx
preset = false
[../]
[./y_bot]
type = FunctionDirichletBC
variable = disp_y
boundary = back
function = dispy
preset = false
[../]
[./z_bot]
type = FunctionDirichletBC
variable = disp_z
boundary = back
function = dispz
preset = false
[../]
[]
[Functions]
[./dispx]
type = PiecewiseLinear
x = '0.0 1.0 2.0 3.0 4.0' # time
y = '0.0 1.0 0.0 -1.0 0.0' # displacement
[../]
[./dispy]
type = ParsedFunction
value = 0.1*t*t*sin(10*t)
[../]
[./dispz]
type = ParsedFunction
value = 0.1*t*t*sin(20*t)
[../]
[]
[NodalKernels]
[./nodal_mass_x]
type = NodalTranslationalInertia
boundary = 'all'
nodal_mass_file = 'nodal_mass_file.csv'
variable = 'disp_x'
[../]
[./nodal_mass_y]
type = NodalTranslationalInertia
boundary = 'all'
nodal_mass_file = 'nodal_mass_file.csv'
variable = 'disp_y'
[../]
[./nodal_mass_z]
type = NodalTranslationalInertia
boundary = 'all'
nodal_mass_file = 'nodal_mass_file.csv'
variable = 'disp_z'
[../]
[]
[Materials]
[./elasticity_tensor_block]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.25
block = 0
[../]
[./strain_block]
type = ComputeIncrementalSmallStrain
block = 0
displacements = 'disp_x disp_y disp_z'
implicit = false
[../]
[./stress_block]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[]
[Executioner]
type = Transient
start_time = -0.01
end_time = 0.1
dt = 0.005
timestep_tolerance = 1e-6
[./TimeIntegrator]
type = CentralDifference
[../]
[]
[Postprocessors]
[./accel_10x]
type = NodalVariableValue
nodeid = 10
variable = accel_x
[../]
[]
[Outputs]
exodus = false
csv = true
[]
(modules/porous_flow/test/tests/infiltration_and_drainage/rd01.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 120
ny = 1
xmin = 0
xmax = 6
ymin = 0
ymax = 0.05
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Functions]
[dts]
type = PiecewiseLinear
y = '1E-2 1 10 500 5000 5000'
x = '0 10 100 1000 10000 100000'
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = pressure
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureVG
m = 0.336
alpha = 1.43e-4
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 2e7
viscosity = 1.01e-3
density0 = 1000
thermal_expansion = 0
[]
[]
[]
[Materials]
[massfrac]
type = PorousFlowMassFraction
[]
[temperature]
type = PorousFlowTemperature
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pressure
capillary_pressure = pc
[]
[relperm]
type = PorousFlowRelativePermeabilityVG
m = 0.336
seff_turnover = 0.99
phase = 0
[]
[porosity]
type = PorousFlowPorosityConst
porosity = 0.33
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '0.295E-12 0 0 0 0.295E-12 0 0 0 0.295E-12'
[]
[]
[Variables]
[pressure]
initial_condition = -72620.4
[]
[]
[Kernels]
[mass0]
type = PorousFlowMassTimeDerivative
fluid_component = 0
variable = pressure
[]
[flux0]
type = PorousFlowAdvectiveFlux
fluid_component = 0
variable = pressure
gravity = '-10 0 0'
[]
[]
[AuxVariables]
[SWater]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[SWater]
type = MaterialStdVectorAux
property = PorousFlow_saturation_qp
index = 0
variable = SWater
[]
[]
[BCs]
[base]
type = PorousFlowSink
boundary = right
flux_function = -2.315E-3
variable = pressure
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
petsc_options = '-snes_converged_reason -ksp_diagonal_scale -ksp_diagonal_scale_fix -ksp_gmres_modifiedgramschmidt -snes_linesearch_monitor'
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -sub_pc_factor_shift_type -pc_asm_overlap -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'gmres asm lu NONZERO 2 1E-10 1E-10 10'
[]
[]
[VectorPostprocessors]
[swater]
type = LineValueSampler
variable = SWater
start_point = '0 0 0'
end_point = '6 0 0'
sort_by = x
num_points = 121
execute_on = timestep_end
[]
[]
[Executioner]
type = Transient
solve_type = Newton
petsc_options = '-snes_converged_reason'
end_time = 359424
[TimeStepper]
type = FunctionDT
function = dts
[]
[]
[Outputs]
file_base = rd01
[exodus]
type = Exodus
execute_on = 'initial final'
[]
[along_line]
type = CSV
execute_on = final
[]
[]
(modules/xfem/test/tests/second_order_elements/diffusion_2d_quad9_test.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD9
[]
[XFEM]
cut_data = '0.35 1.0 0.35 0.4 0 0'
qrule = volfrac
output_cut_plane = true
[]
[Variables]
[./u]
[../]
[]
[Functions]
[./u_left]
type = PiecewiseLinear
x = '0 2'
y = '0 0.1'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = FunctionDirichletBC
variable = u
boundary = 3
function = u_left
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Transient
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
start_time = 0.0
dt = 1.0
end_time = 2.0
[]
[Outputs]
interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(test/tests/geomsearch/3d_moving_penetration/pl_test2tt.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
file = pl_test2tt.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./normal_z]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./closest_point_z]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[./diff_z]
type = Diffusion
variable = disp_z
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
tangential_tolerance = 0.1
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
tangential_tolerance = 0.1
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = normal_z
boundary = 11
paired_boundary = 12
quantity = normal_z
[../]
[./penetrate10]
type = PenetrationAux
variable = normal_z
boundary = 12
paired_boundary = 11
quantity = normal_z
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate13]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate14]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate15]
type = PenetrationAux
variable = closest_point_z
boundary = 11
paired_boundary = 12
quantity = closest_point_z
[../]
[./penetrate16]
type = PenetrationAux
variable = closest_point_z
boundary = 12
paired_boundary = 11
quantity = closest_point_z
[../]
[./penetrate17]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate18]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate19]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate20]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b1z]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[./b2z]
type = DirichletBC
variable = disp_z
boundary = 2
value = 0
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 0.7 -0.7 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-9
l_max_its = 10
start_time = 0.0
dt = 0.05
end_time = 1.0
[]
[Outputs]
file_base = pl_test2tt_out
exodus = true
[]
(modules/tensor_mechanics/test/tests/thermal_expansion_function/finite_const.i)
# This tests the thermal expansion coefficient function using both
# options to specify that function: mean and instantaneous. There
# two blocks, each containing a single element, and these use the
# two variants of the function.
# In this test, the instantaneous CTE function has a constant value,
# while the mean CTE function is an analytic function designed to
# give the same response. If \bar{alpha}(T) is the mean CTE function,
# and \alpha(T) is the instantaneous CTE function,
# \bar{\alpha}(T) = 1/(T-Tref) \intA^{T}_{Tsf} \alpha(T) dT
# where Tref is the reference temperature used to define the mean CTE
# function, and Tsf is the stress-free temperature.
# This version of the test uses finite deformation theory.
# The two models produce very similar results. There are slight
# differences due to the large deformation treatment.
[Mesh]
file = 'blocks.e'
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[AuxVariables]
[./temp]
order = FIRST
family = LAGRANGE
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
eigenstrain_names = eigenstrain
generate_output = 'strain_xx strain_yy strain_zz'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = disp_x
boundary = 3
value = 0.0
[../]
[./bottom]
type = DirichletBC
variable = disp_y
boundary = 2
value = 0.0
[../]
[./back]
type = DirichletBC
variable = disp_z
boundary = 1
value = 0.0
[../]
[]
[AuxKernels]
[./temp]
type = FunctionAux
variable = temp
block = '1 2'
function = temp_func
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./small_stress]
type = ComputeFiniteStrainElasticStress
[../]
[./thermal_expansion_strain1]
type = ComputeMeanThermalExpansionFunctionEigenstrain
block = 1
thermal_expansion_function = cte_func_mean
thermal_expansion_function_reference_temperature = 0.5
stress_free_temperature = 0.0
temperature = temp
eigenstrain_name = eigenstrain
[../]
[./thermal_expansion_strain2]
type = ComputeInstantaneousThermalExpansionFunctionEigenstrain
block = 2
thermal_expansion_function = cte_func_inst
stress_free_temperature = 0.0
temperature = temp
eigenstrain_name = eigenstrain
[../]
[]
[Functions]
[./cte_func_mean]
type = ParsedFunction
vars = 'tsf tref scale' #stress free temp, reference temp, scale factor
vals = '0.0 0.5 1e-4'
value = 'scale * (t - tsf) / (t - tref)'
[../]
[./cte_func_inst]
type = PiecewiseLinear
xy_data = '0 1.0
2 1.0'
scale_factor = 1e-4
[../]
[./temp_func]
type = PiecewiseLinear
xy_data = '0 1
1 2'
[../]
[]
[Postprocessors]
[./disp_1]
type = NodalMaxValue
variable = disp_x
boundary = 101
[../]
[./disp_2]
type = NodalMaxValue
variable = disp_x
boundary = 102
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
l_max_its = 100
l_tol = 1e-4
nl_abs_tol = 1e-8
nl_rel_tol = 1e-12
start_time = 0.0
end_time = 1.0
dt = 0.1
[]
[Outputs]
csv = true
[]
(modules/tensor_mechanics/test/tests/beam/dynamic/dyn_euler_small_added_mass_inertia_damping_action.i)
# Test for small strain euler beam vibration in y direction
# An impulse load is applied at the end of a cantilever beam of length 4m.
# The beam is massless with a lumped mass at the end of the beam. The lumped
# mass also has a moment of inertia associated with it.
# The properties of the cantilever beam are as follows:
# Young's modulus (E) = 1e4
# Shear modulus (G) = 4e7
# Shear coefficient (k) = 1.0
# Cross-section area (A) = 0.01
# Iy = 1e-4 = Iz
# Length (L)= 4 m
# mass (m) = 0.01899772
# Moment of inertia of lumped mass:
# Ixx = 0.2
# Iyy = 0.1
# Izz = 0.1
# mass proportional damping coefficient (eta) = 0.1
# For this beam, the dimensionless parameter alpha = kAGL^2/EI = 6.4e6
# Therefore, the beam behaves like a Euler-Bernoulli beam.
# The displacement time history from this analysis matches with that obtained from Abaqus.
# Values from the first few time steps are as follows:
# time disp_y vel_y accel_y
# 0.0 0.0 0.0 0.0
# 0.1 0.001278249649738 0.025564992994761 0.51129985989521
# 0.2 0.0049813090917644 0.048496195845768 -0.052675802875074
# 0.3 0.0094704658873002 0.041286940064947 -0.091509312741339
# 0.4 0.013082280729802 0.03094935678508 -0.115242352856
# 0.5 0.015588313103503 0.019171290688959 -0.12031896906642
[Mesh]
type = GeneratedMesh
dim = 1
nx = 10
xmin = 0.0
xmax = 4.0
displacements = 'disp_x disp_y disp_z'
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./fixy1]
type = DirichletBC
variable = disp_y
boundary = left
value = 0.0
[../]
[./fixz1]
type = DirichletBC
variable = disp_z
boundary = left
value = 0.0
[../]
[./fixr1]
type = DirichletBC
variable = rot_x
boundary = left
value = 0.0
[../]
[./fixr2]
type = DirichletBC
variable = rot_y
boundary = left
value = 0.0
[../]
[./fixr3]
type = DirichletBC
variable = rot_z
boundary = left
value = 0.0
[../]
[]
[NodalKernels]
[./force_y2]
type = UserForcingFunctionNodalKernel
variable = disp_y
boundary = right
function = force
[../]
[]
[Functions]
[./force]
type = PiecewiseLinear
x = '0.0 0.1 0.2 10.0'
y = '0.0 1e-2 0.0 0.0'
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options_iname = '-ksp_type -pc_type'
petsc_options_value = 'preonly lu'
dt = 0.1
end_time = 5.0
timestep_tolerance = 1e-6
[]
[Modules/TensorMechanics/LineElementMaster]
[./all]
add_variables = true
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
# Geometry parameters
area = 0.01
Iy = 1e-4
Iz = 1e-4
y_orientation = '0.0 1.0 0.0'
# dynamic simulation using consistent mass/inertia matrix
dynamic_nodal_translational_inertia = true
nodal_mass = 0.01899772
dynamic_nodal_rotational_inertia = true
nodal_Ixx = 2e-1
nodal_Iyy = 1e-1
nodal_Izz = 1e-1
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y rot_vel_z'
rotational_accelerations = 'rot_accel_x rot_accel_y rot_accel_z'
beta = 0.25 # Newmark time integration parameter
gamma = 0.5 # Newmark time integration parameter
boundary = right # Node set where nodal mass and nodal inertia are applied
# optional parameters for Rayleigh damping
eta = 0.1 # Mass proportional Rayleigh damping
[../]
[]
[Materials]
[./elasticity]
type = ComputeElasticityBeam
youngs_modulus = 1.0e4
poissons_ratio = -0.999875
shear_coefficient = 1.0
block = 0
[../]
[./stress]
type = ComputeBeamResultants
block = 0
[../]
[]
[Postprocessors]
[./disp_x]
type = PointValue
point = '4.0 0.0 0.0'
variable = disp_x
[../]
[./disp_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = disp_y
[../]
[./vel_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = vel_y
[../]
[./accel_y]
type = PointValue
point = '4.0 0.0 0.0'
variable = accel_y
[../]
[]
[Outputs]
file_base = 'dyn_euler_small_added_mass_inertia_damping_out'
exodus = true
csv = true
perf_graph = true
[]
(modules/tensor_mechanics/test/tests/ad_anisotropic_creep/anis_mech_hill_tensor_creep_small_tiny_step_ts_limit_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
second_order = true
[]
[GlobalParams]
displacements = 'disp_x disp_y'
volumetric_locking_correction = false
[]
[Modules/TensorMechanics/Master]
[all]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'elastic_strain_xx elastic_strain_yy elastic_strain_xy stress_xx stress_xy '
'stress_yy'
use_automatic_differentiation = true
[]
[]
[AuxVariables]
[hydrostatic_stress]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_xx]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_xy]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_yy]
order = CONSTANT
family = MONOMIAL
[]
[]
[Variables]
[disp_x]
order = SECOND
[]
[disp_y]
order = SECOND
[]
[]
[AuxKernels]
[hydrostatic_stress]
type = ADRankTwoScalarAux
variable = hydrostatic_stress
rank_two_tensor = stress
scalar_type = Hydrostatic
[]
[creep_strain_xx]
type = ADRankTwoAux
rank_two_tensor = trial_creep_creep_strain
variable = creep_strain_xx
index_i = 0
index_j = 0
[]
[creep_strain_xy]
type = ADRankTwoAux
rank_two_tensor = trial_creep_creep_strain
variable = creep_strain_xy
index_i = 0
index_j = 1
[]
[creep_strain_yy]
type = ADRankTwoAux
rank_two_tensor = trial_creep_creep_strain
variable = creep_strain_yy
index_i = 1
index_j = 1
[]
[]
[Functions]
[pull]
type = PiecewiseLinear
x = '0 1e3 1e8'
y = '0 1e2 1e2'
[]
[]
[Materials]
[elasticity_tensor]
type = ADComputeElasticityTensor
fill_method = orthotropic
C_ijkl = '2.0e3 2.0e5 2.0e3 0.71428571e3 0.71428571e3 0.71428571e3 0.4 0.2 0.004 0.004 0.2 0.4'
[]
[elastic_strain]
type = ADComputeMultipleInelasticStress
inelastic_models = "trial_creep trial_creep_two"
max_iterations = 5
absolute_tolerance = 1e-05
[]
[trial_creep]
type = ADHillCreepStressUpdate
coefficient = 3e-18
n_exponent = 5
m_exponent = 0
activation_energy = 0
# F G H L M N
hill_constants = "0.5 0.5 0.3866 1.6413 1.6413 1.2731"
max_inelastic_increment = 1.0e-5
base_name = trial_creep
# Force it to not use integration error
max_integration_error = 1.0
[]
[trial_creep_two]
type = ADHillCreepStressUpdate
coefficient = 3e-18
n_exponent = 5
m_exponent = 0
activation_energy = 0
# F G H L M N
hill_constants = "0.5 0.5 0.3866 1.6413 1.6413 1.2731"
max_inelastic_increment = 1.0e-5
base_name = trial_creep_two
# Force it to not use integration error
max_integration_error = 1.0
[]
[]
[BCs]
[no_disp_x]
type = ADDirichletBC
variable = disp_x
boundary = bottom
value = 0.0
[]
[no_disp_y]
type = ADDirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[]
[Pressure]
[Side1]
boundary = top
function = pull
[]
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options_iname = '-ksp_gmres_restart -pc_type -sub_pc_type'
petsc_options_value = '101 asm lu'
line_search = 'none'
nl_rel_tol = 1e-10
nl_abs_tol = 1.0e-14
l_max_its = 90
num_steps = 7
start_time = 0
automatic_scaling = true
[TimeStepper]
type = IterationAdaptiveDT
optimal_iterations = 30
iteration_window = 9
growth_factor = 2.0
cutback_factor = 0.5
timestep_limiting_postprocessor = matl_ts_min
dt = 5.0e1
[]
[]
[Postprocessors]
[matl_ts_min]
type = MaterialTimeStepPostprocessor
[]
[max_disp_x]
type = ElementExtremeValue
variable = disp_x
[]
[max_disp_y]
type = ElementExtremeValue
variable = disp_y
[]
[max_hydro]
type = ElementAverageValue
variable = hydrostatic_stress
[]
[dt]
type = TimestepSize
[]
[num_lin]
type = NumLinearIterations
outputs = console
[]
[num_nonlin]
type = NumNonlinearIterations
outputs = console
[]
[]
[Outputs]
csv = true
exodus = true
perf_graph = 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
[]
(modules/fsi/test/tests/fsi_acoustics/3D_struc_acoustic/3D_struc_acoustic.i)
# Test for `StructureAcousticInterface` interface kernel. The domain is 3D with lengths
# 10 X 0.1 X 0.1 meters. The fluid domain is on the right and the structural domain
# is on the left. Fluid end is subjected to a 250Hz sine wave with a single peak.
# Structural domain has the same material properties as the fluid. Interface between
# structure and fluid is located at 5.0m in the x-direction. Fluid pressure is recorded
# at (5, 0.05, 0.05). Structural stress is also recorded at the same location. Fluid
# pressure and structural stress should be almost equal and opposite to each other.
#
# Input parameters:
# Dimensions = 3
# Lengths = 10 X 0.1 X 0.1 meters
# Fluid speed of sound = 1500 m/s
# Fluid density = 1e-6 Giga kg/m^3
# Structural bulk modulus = 2.25 GPa
# Structural shear modulus = 0 GPa
# Structural density = 1e-6 Giga kg/m^3
# Fluid domain = true
# Fluid BC = single peak sine wave applied as a pressure on the fluid end
# Structural domain = true
# Structural BC = Neumann BC with value zero applied on the structural end.
# Fluid-structure interface location = 5.0m along the x-direction
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
nx = 100
ny = 1
nz = 1
xmax = 10
ymax = 0.1
zmax = 0.1
[]
[./subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '5.0 0.0 0.0'
block_id = 1
top_right = '10.0 0.1 0.1'
[../]
[./interface1]
type = SideSetsBetweenSubdomainsGenerator
input = subdomain1
primary_block = 1
paired_block = 0
new_boundary = 'interface1'
[../]
[]
[GlobalParams]
[]
[Variables]
[./p]
block = 1
[../]
[./disp_x]
block = 0
[../]
[./disp_y]
block = 0
[../]
[./disp_z]
block = 0
[../]
[]
[AuxVariables]
[./vel_x]
order = FIRST
family = LAGRANGE
block = 0
[../]
[./accel_x]
order = FIRST
family = LAGRANGE
block = 0
[../]
[./vel_y]
order = FIRST
family = LAGRANGE
block = 0
[../]
[./accel_y]
order = FIRST
family = LAGRANGE
block = 0
[../]
[./vel_z]
order = FIRST
family = LAGRANGE
block = 0
[../]
[./accel_z]
order = FIRST
family = LAGRANGE
block = 0
[../]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
block = 0
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
block = 0
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
block = 0
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
block = 0
[../]
[./stress_xz]
order = CONSTANT
family = MONOMIAL
block = 0
[../]
[./stress_yz]
order = CONSTANT
family = MONOMIAL
block = 0
[../]
[]
[Kernels]
[./diffusion]
type = Diffusion
variable = 'p'
block = 1
[../]
[./inertia]
type = AcousticInertia
variable = p
block = 1
[../]
[./DynamicTensorMechanics]
displacements = 'disp_x disp_y disp_z'
block = 0
[../]
[./inertia_x]
type = InertialForce
variable = disp_x
block = 0
[../]
[./inertia_y]
type = InertialForce
variable = disp_y
block = 0
[../]
[./inertia_z]
type = InertialForce
variable = disp_z
block = 0
[../]
[]
[AuxKernels]
[./accel_x]
type = TestNewmarkTI
displacement = disp_x
variable = accel_x
first = false
block = 0
[../]
[./vel_x]
type = TestNewmarkTI
displacement = disp_x
variable = vel_x
block = 0
[../]
[./accel_y]
type = TestNewmarkTI
displacement = disp_y
variable = accel_y
first = false
block = 0
[../]
[./vel_y]
type = TestNewmarkTI
displacement = disp_y
variable = vel_y
block = 0
[../]
[./accel_z]
type = TestNewmarkTI
displacement = disp_z
variable = accel_z
first = false
block = 0
[../]
[./vel_z]
type = TestNewmarkTI
displacement = disp_z
variable = vel_z
block = 0
[../]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
block = 0
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
block = 0
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
block = 0
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
block = 0
[../]
[./stress_xz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xz
index_i = 0
index_j = 2
block = 0
[../]
[./stress_yz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yz
index_i = 1
index_j = 2
block = 0
[../]
[]
[InterfaceKernels]
[./interface1]
type = StructureAcousticInterface
variable = p
neighbor_var = disp_x
boundary = 'interface1'
D = 1e-6
component = 0
[../]
[./interface2]
type = StructureAcousticInterface
variable = p
neighbor_var = disp_y
boundary = 'interface1'
D = 1e-6
component = 1
[../]
[./interface3]
type = StructureAcousticInterface
variable = p
neighbor_var = disp_z
boundary = 'interface1'
D = 1e-6
component = 2
[../]
[]
[BCs]
[./bottom_accel]
type = FunctionDirichletBC
variable = p
boundary = 'right'
function = accel_bottom
[../]
[./disp_x1]
type = NeumannBC
boundary = 'left'
variable = disp_x
value = 0.0
[../]
[./disp_y1]
type = NeumannBC
boundary = 'left'
variable = disp_y
value = 0.0
[../]
[./disp_z1]
type = NeumannBC
boundary = 'left'
variable = disp_z
value = 0.0
[../]
[]
[Functions]
[./accel_bottom]
type = PiecewiseLinear
data_file = ../1D_struc_acoustic/Input_1Peak_highF.csv
scale_factor = 1e-2
format = 'columns'
[../]
[]
[Materials]
[./co_sq]
type = GenericConstantMaterial
prop_names = inv_co_sq
prop_values = 4.44e-7
block = '1'
[../]
[./density0]
type = GenericConstantMaterial
block = 0
prop_names = density
prop_values = 1e-6
[../]
[./elasticity_base]
type = ComputeIsotropicElasticityTensor
bulk_modulus = 2.25
shear_modulus = 0.0
block = 0
[../]
[./strain]
type = ComputeFiniteStrain
block = 0
displacements = 'disp_x disp_y disp_z'
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
start_time = 0.0
end_time = 0.005
dt = 0.0001
dtmin = 0.00001
nl_abs_tol = 1e-8
nl_rel_tol = 1e-8
l_tol = 1e-8
l_max_its = 25
timestep_tolerance = 1e-8
automatic_scaling = true
[TimeIntegrator]
type = NewmarkBeta
[]
[]
[Postprocessors]
[./p1]
type = PointValue
point = '5.0 0.05 0.05'
variable = p
[../]
[./stress_xx]
type = PointValue
point = '5.0 0.05 0.05'
variable = stress_xx
[../]
[]
[Outputs]
csv = true
exodus = true
perf_graph = true
print_linear_residuals = true
[]
(test/tests/time_steppers/function_dt/function_dt_min.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 = t*t*(x*x+y*y)
[../]
[./forcing_fn]
type = ParsedFunction
value = 2*t*(x*x+y*y)-4*t*t
[../]
[./dts]
type = PiecewiseLinear
x = '0 0.85 2'
y = '0.2 0.2 0.2'
[../]
[]
[Variables]
[./u]
family = LAGRANGE
order = SECOND
[../]
[]
[ICs]
[./u_var]
type = FunctionIC
variable = u
function = exact_fn
[../]
[]
[Kernels]
[./td]
type = TimeDerivative
variable = u
[../]
[./diff]
type = Diffusion
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
boundary = 'left right top bottom'
function = exact_fn
[../]
[]
[Executioner]
type = Transient
start_time = 0
num_steps = 10
[./TimeStepper]
type = FunctionDT
function = dts
min_dt = 0.1
[../]
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/j_integral/j_integral_3d_as_2d_topo_q_func.i)
#This tests the J-Integral evaluation capability.
#This is a 3d extrusion of a 2d plane strain model with one element
#through the thickness, and calculates the J-Integrals using options
#to treat it as 2d.
#The analytic solution for J1 is 2.434. This model
#converges to that solution with a refined mesh.
#Reference: National Agency for Finite Element Methods and Standards (U.K.):
#Test 1.1 from NAFEMS publication "Test Cases in Linear Elastic Fracture
#Mechanics" R0020.
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[Mesh]
file = crack_3d_as_2d.e
partitioner = centroid
centroid_partitioner_direction = z
[]
[AuxVariables]
[./SED]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./rampConstant]
type = PiecewiseLinear
x = '0. 1.'
y = '0. 1.'
scale_factor = -1e2
[../]
[]
[DomainIntegral]
integrals = JIntegral
boundary = 800
crack_direction_method = CrackDirectionVector
crack_direction_vector = '1 0 0'
2d = true
axis_2d = 2
q_function_type = Topology
ring_first = 1
ring_last = 3
output_q = false
incremental = true
[]
[Modules/TensorMechanics/Master]
[./master]
strain = FINITE
add_variables = true
incremental = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
[../]
[]
[AuxKernels]
[./SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[../]
[]
[BCs]
[./crack_y]
type = DirichletBC
variable = disp_y
boundary = 100
value = 0.0
[../]
[./no_z]
type = DirichletBC
variable = disp_z
boundary = 500
value = 0.0
[../]
[./no_x]
type = DirichletBC
variable = disp_x
boundary = 700
value = 0.0
[../]
[./Pressure]
[./Side1]
boundary = 400
function = rampConstant
[../]
[../]
[] # BCs
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
[../]
[./elastic_stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
# Two sets of linesearch options are for petsc 3.1 and 3.3 respectively
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 50
nl_max_its = 20
nl_abs_tol = 1e-5
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 1
num_steps = 1
[]
[Outputs]
file_base = j_integral_3d_as_2d_topo_q_func_out
exodus = true
csv = true
[]
(modules/richards/test/tests/gravity_head_2/gh07.i)
# unsaturated = true
# gravity = false
# supg = true
# transient = true
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
xmin = 0
xmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1E-2 1E-1 1E0 1E1 1E3 1E4 1E5 1E6 1E7'
x = '0 1E-1 1E0 1E1 1E2 1E3 1E4 1E5 1E6'
[../]
[]
[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 = 0.2
max = 0.8
variable = pwater
[../]
[./gas_ic]
type = RandomIC
min = 1.2
max = 1.8
variable = pgas
[../]
[]
[Kernels]
active = 'richardsfwater richardstwater richardsfgas richardstgas'
[./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
[../]
[./mass_error_gas]
type = FunctionValuePostprocessor
function = fcn_mass_error_g
[../]
[./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 -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-13 1E-10 10000'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
end_time = 1E6
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = gh07
csv = true
[]
(modules/tensor_mechanics/test/tests/finite_strain_tensor_mechanics_tests/finite_strain_patch.i)
# Patch Test
# This test is designed to compute constant xx, yy, zz, xy, yz, and zx
# stress on a set of irregular hexes. The mesh is composed of one
# block with seven elements. The elements form a unit cube with one
# internal element. There is a nodeset for each exterior node.
# The cube is displaced by 1e-6 units in x, 2e-6 in y, and 3e-6 in z.
# The faces are sheared as well (1e-6, 2e-6, and 3e-6 for xy, yz, and
# zx). This gives a uniform strain/stress state for all six unique
# tensor components.
# With Young's modulus at 1e6 and Poisson's ratio at 0, the shear
# modulus is 5e5 (G=E/2/(1+nu)). Therefore,
#
# stress xx = 1e6 * 1e-6 = 1
# stress yy = 1e6 * 2e-6 = 2
# stress zz = 1e6 * 3e-6 = 3
# stress xy = 2 * 5e5 * 1e-6 / 2 = 0.5
# (2 * G * gamma_xy / 2 = 2 * G * epsilon_xy)
# stress yz = 2 * 5e5 * 2e-6 / 2 = 1
# stress zx = 2 * 5e5 * 3e-6 / 2 = 1.5
[Mesh]
# Comment
# Mesh
file = patch_mesh.e
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Functions]
# Functions
[./rampConstant1]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 1.'
scale_factor = 1e-6
[../]
[./rampConstant2]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 1.'
scale_factor = 2e-6
[../]
[./rampConstant3]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 1.'
scale_factor = 3e-6
[../]
[./rampConstant4]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 1.'
scale_factor = 4e-6
[../]
[./rampConstant6]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 1.'
scale_factor = 6e-6
[../]
[]
[Variables]
# Variables
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
# AuxVariables
[./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_zx]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
[../]
[]
[AuxKernels]
# AuxKernels
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
[../]
[./stress_yz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yz
index_i = 1
index_j = 2
[../]
[./stress_zx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zx
index_i = 2
index_j = 0
[../]
[]
[BCs]
# BCs
[./node1_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./node1_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 1
function = rampConstant2
[../]
[./node1_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 1
function = rampConstant3
[../]
[./node2_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 2
function = rampConstant1
[../]
[./node2_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = rampConstant2
[../]
[./node2_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 2
function = rampConstant6
[../]
[./node3_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 3
function = rampConstant1
[../]
[./node3_y]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.0
[../]
[./node3_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 3
function = rampConstant3
[../]
[./node4_x]
type = DirichletBC
variable = disp_x
boundary = 4
value = 0.0
[../]
[./node4_y]
type = DirichletBC
variable = disp_y
boundary = 4
value = 0.0
[../]
[./node4_z]
type = DirichletBC
variable = disp_z
boundary = 4
value = 0.0
[../]
[./node5_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 5
function = rampConstant1
[../]
[./node5_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 5
function = rampConstant4
[../]
[./node5_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 5
function = rampConstant3
[../]
[./node6_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 6
function = rampConstant2
[../]
[./node6_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 6
function = rampConstant4
[../]
[./node6_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 6
function = rampConstant6
[../]
[./node7_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 7
function = rampConstant2
[../]
[./node7_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 7
function = rampConstant2
[../]
[./node7_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 7
function = rampConstant3
[../]
[./node8_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 8
function = rampConstant1
[../]
[./node8_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 8
function = rampConstant2
[../]
[./node8_z]
type = DirichletBC
variable = disp_z
boundary = 8
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeElasticityTensor
block = '1 2 3 4 5 6 7'
C_ijkl = '1.0e6 0.0 0.0 1.0e6 0.0 1.0e6 0.5e6 0.5e6 0.5e6'
fill_method = symmetric9
[../]
[./strain]
type = ComputeFiniteStrain
block = '1 2 3 4 5 6 7'
displacements = 'disp_x disp_y disp_z'
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = '1 2 3 4 5 6 7'
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
# Executioner
type = Transient
solve_type = 'NEWTON'
nl_abs_tol = 1e-10
l_max_its = 20
start_time = 0.0
dt = 1.0
num_steps = 2
petsc_options_iname = -pc_type
petsc_options_value = lu
end_time = 2.0
[]
[Outputs]
exodus = true
[] # Output
(modules/tensor_mechanics/test/tests/scalar_material_damage/scalar_material_damage_creep.i)
# This is a basic test of the system for continuum damage mechanics
# materials. It uses ScalarMaterialDamage for the damage model,
# which simply gets its damage index from another material. In this
# case, we prescribe the evolution of the damage index using a
# function. A single element has a fixed prescribed displacement
# on one side that puts the element in tension, and then the
# damage index evolves from 0 to 1 over time, and this verifies
# that the stress correspondingly drops to 0.
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
elem_type = HEX8
[]
[AuxVariables]
[damage_index]
order = CONSTANT
family = MONOMIAL
[]
[]
[Modules/TensorMechanics/Master]
[all]
strain = SMALL
incremental = true
add_variables = true
generate_output = 'stress_xx strain_xx creep_strain_xx'
[]
[]
[AuxKernels]
[damage_index]
type = MaterialRealAux
variable = damage_index
property = damage_index_prop
execute_on = timestep_end
[]
[]
[BCs]
[symmy]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0
[]
[symmx]
type = DirichletBC
variable = disp_x
boundary = left
value = 0
[]
[symmz]
type = DirichletBC
variable = disp_z
boundary = back
value = 0
[]
[axial_load]
type = DirichletBC
variable = disp_x
boundary = right
value = 0.01
[]
[]
[Functions]
[damage_evolution]
type = PiecewiseLinear
xy_data = '0.0 0.0
0.1 0.0
2.1 2.0'
[]
[]
[Materials]
[damage_index]
type = GenericFunctionMaterial
prop_names = damage_index_prop
prop_values = damage_evolution
[]
[damage]
type = ScalarMaterialDamage
damage_index = damage_index_prop
[]
[stress]
type = ComputeMultipleInelasticStress
damage_model = damage
inelastic_models = 'creep'
[]
[kelvin_voigt]
type = GeneralizedKelvinVoigtModel
creep_modulus = '10e9 10e9'
creep_viscosity = '1 10'
poisson_ratio = 0.2
young_modulus = 10e9
[]
[creep]
type = LinearViscoelasticStressUpdate
[]
[]
[UserObjects]
[./update]
type = LinearViscoelasticityManager
viscoelastic_model = kelvin_voigt
[../]
[]
[Postprocessors]
[stress_xx]
type = ElementAverageValue
variable = stress_xx
[]
[strain_xx]
type = ElementAverageValue
variable = strain_xx
[]
[./creep_strain_xx]
type = ElementAverageValue
variable = creep_strain_xx
[../]
[damage_index]
type = ElementAverageValue
variable = damage_index
[]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
l_max_its = 50
l_tol = 1e-8
nl_max_its = 20
nl_rel_tol = 1e-10
nl_abs_tol = 1e-8
dt = 0.1
dtmin = 0.001
end_time = 1.1
[]
[Outputs]
csv=true
exodus = true
[]
(modules/contact/test/tests/verification/hertz_cyl/half_symm_q4/hertz_cyl_half_1deg_template3.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = hertz_cyl_half_1deg.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Functions]
[./disp_ramp_vert]
type = PiecewiseLinear
x = '0. 1. 11.'
y = '0. -0.0020 -0.0020'
[../]
[./disp_ramp_horz]
type = PiecewiseLinear
x = '0. 1. 11.'
y = '0. 0.0 0.0014'
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
extra_vector_tags = 'ref'
save_in = 'saved_x saved_y'
[../]
[]
[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_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 2
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 2
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 4
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 4
[../]
[./disp_x226]
type = NodalVariableValue
nodeid = 225
variable = disp_x
[../]
[./disp_y226]
type = NodalVariableValue
nodeid = 225
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./side_x]
type = DirichletBC
variable = disp_y
boundary = '1 2'
value = 0.0
[../]
[./bot_y]
type = DirichletBC
variable = disp_x
boundary = '1 2'
value = 0.0
[../]
[./top_y_disp]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = disp_ramp_vert
[../]
[./top_x_disp]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = disp_ramp_horz
[../]
[]
[Materials]
[./stuff1_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e10
poissons_ratio = 0.0
[../]
[./stuff1_strain]
type = ComputeFiniteStrain
block = '1'
[../]
[./stuff1_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./stuff2_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff2_strain]
type = ComputeFiniteStrain
block = '2'
[../]
[./stuff2_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[./stuff3_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '3'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff3_strain]
type = ComputeFiniteStrain
block = '3'
[../]
[./stuff3_stress]
type = ComputeFiniteStrainElasticStress
block = '3'
[../]
[./stuff4_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '4'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff4_strain]
type = ComputeFiniteStrain
block = '4'
[../]
[./stuff4_stress]
type = ComputeFiniteStrainElasticStress
block = '4'
[../]
[./stuff5_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '5'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff5_strain]
type = ComputeFiniteStrain
block = '5'
[../]
[./stuff5_stress]
type = ComputeFiniteStrainElasticStress
block = '5'
[../]
[./stuff6_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '6'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff6_strain]
type = ComputeFiniteStrain
block = '6'
[../]
[./stuff6_stress]
type = ComputeFiniteStrainElasticStress
block = '6'
[../]
[./stuff7_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '7'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff7_strain]
type = ComputeFiniteStrain
block = '7'
[../]
[./stuff7_stress]
type = ComputeFiniteStrainElasticStress
block = '7'
[../]
[]
[Executioner]
type = Transient
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-7
nl_rel_tol = 1e-6
l_max_its = 100
nl_max_its = 200
start_time = 0.0
end_time = 2.0
l_tol = 5e-4
dt = 0.1
dtmin = 0.1
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '3 4'
sort_by = id
[../]
[./y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '3 4'
sort_by = id
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = id
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'x_disp y_disp cont_press'
start_time = 0.9
execute_vector_postprocessors_on = timestep_end
[../]
[./chkfile2]
type = CSV
show = 'bot_react_x bot_react_y disp_x226 disp_y226 top_react_x top_react_y'
start_time = 0.9
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./interface]
primary = 2
secondary = 3
model = coulomb
friction_coefficient = 0.0
formulation = penalty
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
[../]
[]
[Dampers]
[./contact_slip]
type = ContactSlipDamper
primary = '2'
secondary = '3'
[../]
[]
(modules/contact/test/tests/hertz_spherical/hertz_contact_rz_quad8.i)
# Hertz Contact: Sphere on sphere
# Spheres have the same radius, Young's modulus, and Poisson's ratio.
# Define E:
# 1/E = (1-nu1^2)/E1 + (1-nu2^2)/E2
#
# Effective radius R:
# 1/R = 1/R1 + 1/R2
#
# F is the applied compressive load.
#
# Area of contact a::
# a^3 = 3FR/4E
#
# Depth of indentation d:
# d = a^2/R
#
#
# Let R1 = R2 = 2. Then R = 1.
#
# Let nu1 = nu2 = 0.25, E1 = E2 = 1.40625e7. Then E = 7.5e6.
#
# Let F = 10000. Then a = 0.1, d = 0.01.
#
[GlobalParams]
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
order = SECOND
[]
[Problem]
coord_type = RZ
[]
[Mesh]#Comment
file = hertz_contact_rz_quad8.e
displacements = 'disp_x disp_y'
allow_renumbering = false
[] # Mesh
[Functions]
[./pressure]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 1.'
scale_factor = 795.77471545947674 # 10000/pi/2^2
[../]
[./disp_y]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. -0.01 -0.01'
[../]
[] # Functions
[Variables]
[./disp_x]
order = SECOND
family = LAGRANGE
[../]
[./disp_y]
order = SECOND
family = LAGRANGE
[../]
[] # Variables
[AuxVariables]
[./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_zx]
order = CONSTANT
family = MONOMIAL
[../]
[./vonmises]
order = CONSTANT
family = MONOMIAL
[../]
[./hydrostatic]
order = CONSTANT
family = MONOMIAL
[../]
[] # AuxVariables
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = SMALL
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 0
variable = stress_xx
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 1
variable = stress_yy
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 2
variable = stress_zz
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 1
variable = stress_xy
[../]
[./stress_yz]
type = RankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 2
variable = stress_yz
[../]
[./stress_zx]
type = RankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 0
variable = stress_zx
[../]
[] # AuxKernels
[BCs]
[./base_y]
type = DirichletBC
variable = disp_y
boundary = 1000
value = 0.0
[../]
[./symm_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./disp_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[] # BCs
[Contact]
[./dummy_name]
primary = 1000
secondary = 100
# normal_smoothing_distance = 0.01
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+10
[../]
[]
[Materials]
[./tensor]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1.40625e7
poissons_ratio = 0.25
[../]
[./stress]
type = ComputeLinearElasticStress
block = '1'
[../]
[./tensor_1000]
type = ComputeIsotropicElasticityTensor
block = '1000'
youngs_modulus = 1e6
poissons_ratio = 0.0
[../]
[./stress_1000]
type = ComputeLinearElasticStress
block = '1000'
[../]
[] # Materials
[Preconditioning]
[./SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-7
l_abs_tol = 1e-9
l_max_its = 200
start_time = 0.0
dt = 0.5
end_time = 2.0
[./Quadrature]
order = FIFTH
[../]
[] # Executioner
[Postprocessors]
[./maxdisp]
type = NodalVariableValue
nodeid = 103 # 104-1 where 104 is the exodus node number of the top-left node
variable = disp_y
[../]
[]
[Outputs]
[./out]
type = Exodus
[../]
[] # Output
(test/tests/geomsearch/2d_moving_penetration/pl_test4.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
file = pl_test4.e
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate10]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate13]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate14]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate15]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate16]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-10
l_max_its = 10
start_time = 0.0
dt = 0.0125
end_time = 1.0
[]
[Outputs]
file_base = pl_test4_out
exodus = true
[]
(modules/xfem/test/tests/pressure_bc/inclined_edge_2d_pressure.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
volumetric_locking_correction = False
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 9
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.0 0.33 0.5 0.67'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
generate_output = 'stress_xx stress_yy'
[../]
[]
[Functions]
[./pressure]
type = PiecewiseLinear
x = '0 1.0 2.0'
y = '0 500 1000'
[../]
[]
[BCs]
[./bottom_y]
type = DirichletBC
boundary = 0
variable = disp_y
value = 0.0
[../]
[./top_y]
type = DirichletBC
boundary = 2
variable = disp_y
value = 0.0
[../]
[./bottom_x]
type = DirichletBC
boundary = 0
variable = disp_x
value = 0.0
[../]
[]
[DiracKernels]
[./pressure_x]
type = XFEMPressure
variable = disp_x
component = 0
function = pressure
[../]
[./pressure_y]
type = XFEMPressure
variable = disp_y
component = 1
function = pressure
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-12
# time control
start_time = 0.0
dt = 1
end_time = 2
[]
[Outputs]
file_base = inclined_edge_2d_pressure_out
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/heat_conduction/test/tests/gap_heat_transfer_htonly/gap_heat_transfer_htonly_syntax.i)
#
# 1-D Gap Heat Transfer Test without mechanics
#
# This test exercises 1-D gap heat transfer for a constant conductivity gap.
#
# The mesh consists of two element blocks containing one element each. Each
# element is a unit cube. They sit next to one another with a unit between them.
#
# The conductivity of both blocks is set very large to achieve a uniform temperature
# across each block. The temperature of the far left boundary
# is ramped from 100 to 200 over one time unit. The temperature of the far right
# boundary is held fixed at 100.
#
# A simple analytical solution is possible for the heat flux between the blocks:
#
# Flux = (T_left - T_right) * (gapK/gap_width)
#
# The gap conductivity is specified as 1, thus
#
# gapK(Tavg) = 1.0*Tavg
#
#
# The heat flux across the gap at time = 1 is then:
#
# Flux(2) = 100 * (1.0/1.0) = 100
#
# For comparison, see results from the flux post processors
#
# This test has been augmented with a second scalar field that solves nearly
# the same problem. The conductivity has been changed to 10. Thus, the
# flux for the second field is 1000.
#
[Mesh]
file = gap_heat_transfer_htonly_test.e
[]
[Functions]
[./temp]
type = PiecewiseLinear
x = '0 1 2'
y = '100 200 200'
[../]
[]
[Modules/HeatConduction/ThermalContact/BC]
[./thermal_contact]
type = GapHeatTransfer
variable = temp
primary = 3
secondary = 2
emissivity_primary = 0
emissivity_secondary = 0
[../]
[./awesomium_contact]
type = GapHeatTransfer
variable = awesomium
primary = 3
secondary = 2
emissivity_primary = 0
emissivity_secondary = 0
gap_conductivity = 10
appended_property_name = _awesomium
[../]
[]
[Variables]
[./temp]
order = FIRST
family = LAGRANGE
initial_condition = 100
[../]
[./awesomium]
order = FIRST
family = LAGRANGE
initial_condition = 100
[../]
[]
[AuxVariables]
[./gap_cond]
order = CONSTANT
family = MONOMIAL
[../]
[./gap_cond_awesomium]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[./awe]
type = HeatConduction
variable = awesomium
[../]
[]
[BCs]
[./temp_far_left]
type = FunctionDirichletBC
boundary = 1
variable = temp
function = temp
[../]
[./temp_far_right]
type = DirichletBC
boundary = 4
variable = temp
value = 100
[../]
[./awesomium_far_left]
type = FunctionDirichletBC
boundary = 1
variable = awesomium
function = temp
[../]
[./awesomium_far_right]
type = DirichletBC
boundary = 4
variable = awesomium
value = 100
[../]
[]
[AuxKernels]
[./conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_cond
boundary = 2
[../]
[./conductance_awe]
type = MaterialRealAux
property = gap_conductance_awesomium
variable = gap_cond_awesomium
boundary = 2
[../]
[]
[Materials]
[./heat1]
type = HeatConductionMaterial
block = '1 2'
specific_heat = 1.0
thermal_conductivity = 100000000.0
[../]
[./density]
type = GenericConstantMaterial
block = '1 2'
prop_names = 'density'
prop_values = '1.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 4'
line_search = 'none'
nl_rel_tol = 1e-12
l_tol = 1e-3
l_max_its = 100
dt = 1e-1
end_time = 1.0
[]
[Postprocessors]
[./temp_left]
type = SideAverageValue
boundary = 2
variable = temp
execute_on = 'initial timestep_end'
[../]
[./temp_right]
type = SideAverageValue
boundary = 3
variable = temp
execute_on = 'initial timestep_end'
[../]
[./flux_left]
type = SideFluxIntegral
variable = temp
boundary = 2
diffusivity = thermal_conductivity
execute_on = 'initial timestep_end'
[../]
[./flux_right]
type = SideFluxIntegral
variable = temp
boundary = 3
diffusivity = thermal_conductivity
execute_on = 'initial timestep_end'
[../]
[./awe_left]
type = SideAverageValue
boundary = 2
variable = awesomium
execute_on = 'initial timestep_end'
[../]
[./awe_right]
type = SideAverageValue
boundary = 3
variable = awesomium
execute_on = 'initial timestep_end'
[../]
[./awe_flux_left]
type = SideFluxIntegral
variable = awesomium
boundary = 2
diffusivity = thermal_conductivity
execute_on = 'initial timestep_end'
[../]
[./awe_flux_right]
type = SideFluxIntegral
variable = awesomium
boundary = 3
diffusivity = thermal_conductivity
execute_on = 'initial timestep_end'
[../]
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/recompute_radial_return/isotropic_plasticity_incremental_strain.i)
# This simulation uses the piece-wise linear strain hardening model
# with the incremental small strain formulation; incremental small strain
# is required to produce the strain_increment for the DiscreteRadialReturnStressIncrement
# class, which handles the calculation of the stress increment to return
# to the yield surface in a J2 (isotropic) plasticity problem.
#
# This test assumes a Poissons ratio of zero and applies a displacement loading
# condition on the top in the y direction while fixing the displacement in the x
# and z directions; thus, only the normal stress and the normal strains in the
# y direction are compared in this problem.
#
# A similar problem was run in Abaqus on a similar 1 element mesh and was used
# to verify the SolidMechanics solution; this TensorMechanics code matches the
# SolidMechanics solution.
#
# Mechanical strain is the sum of the elastic and plastic strains but is different
# from total strain in cases with eigen strains, e.g. thermal strain.
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Functions]
[./top_pull]
type = ParsedFunction
value = t*(0.01)
[../]
[./hf]
type = PiecewiseLinear
x = '0 0.00004 0.0001 0.1'
y = '50 54 56 60'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
incremental = true
add_variables = true
generate_output = 'stress_yy plastic_strain_xx plastic_strain_yy plastic_strain_zz'
[../]
[]
[BCs]
[./y_pull_function]
type = FunctionDirichletBC
variable = disp_y
boundary = top
function = top_pull
[../]
[./x_sides]
type = DirichletBC
variable = disp_x
boundary = 'left right'
value = 0.0
[../]
[./y_bot]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./z_sides]
type = DirichletBC
variable = disp_z
boundary = 'back front'
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 2.5e5
poissons_ratio = 0.0
[../]
[./isotropic_plasticity]
type = IsotropicPlasticityStressUpdate
yield_stress = 25.
hardening_constant = 1000.0
[../]
[./radial_return_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'isotropic_plasticity'
[../]
[]
[Executioner]
type = Transient
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 20
nl_max_its = 20
nl_rel_tol = 1e-10
nl_abs_tol = 1e-12
l_tol = 1e-9
start_time = 0.0
end_time = 0.01875
dt = 0.00125
dtmin = 0.0001
[]
[Outputs]
exodus = true
print_linear_residuals = true
perf_graph = true
[]
(modules/richards/test/tests/recharge_discharge/rd02.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 120
ny = 1
xmin = 0
xmax = 6
ymin = 0
ymax = 0.05
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1E-2 1 10 500 5000 50000'
x = '0 10 100 1000 10000 500000'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1E3
bulk_mod = 2E7
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.336
al = 1.43E-4
[../]
[./RelPermPower]
type = RichardsRelPermVG1
scut = 0.99
simm = 0.0
m = 0.336
[../]
[./Saturation]
type = RichardsSat
s_res = 0.0
sum_s_res = 0.0
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 1.0E+0
[../]
[]
[Variables]
active = 'pressure'
[./pressure]
order = FIRST
family = LAGRANGE
initial_condition = 0.0
[../]
[]
[Kernels]
active = 'richardsf richardst'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = SeffVG
pressure_vars = pressure
[../]
[]
[BCs]
active = 'fix_bot'
[./fix_bot]
type = DirichletBC
variable = pressure
boundary = 'left'
value = 0.0
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.33
mat_permeability = '0.295E-12 0 0 0 0.295E-12 0 0 0 0.295E-12'
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGstandard
sat_UO = Saturation
seff_UO = SeffVG
viscosity = 1.01E-3
gravity = '-10 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
active = 'andy'
[./andy]
type = SMP
full = true
petsc_options = ''
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-13 1E-15 10000'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
petsc_options = '-snes_converged_reason'
end_time = 345600
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = rd02
interval = 100000
execute_on = 'initial final'
exodus = true
[]
(test/tests/geomsearch/2d_moving_penetration/pl_test4ns.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
file = pl_test4.e
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
normal_smoothing_distance = 0.2
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
normal_smoothing_distance = 0.2
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate10]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate13]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate14]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate15]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate16]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-10
l_max_its = 10
start_time = 0.0
dt = 0.0125
end_time = 1.0
[]
[Outputs]
file_base = pl_test4ns_out
exodus = true
[]
(modules/combined/test/tests/adaptive_timestepping/adapt_tstep_function_change.i)
# This is a test designed to evaluate the cabability of the
# IterationAdaptiveDT TimeStepper to adjust time step size according to
# a function. For example, if the power input function for a BISON
# simulation rapidly increases or decreases, the IterationAdaptiveDT
# TimeStepper should take time steps small enough to capture the
# oscillation.
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
order = FIRST
family = LAGRANGE
block = 1
[]
[Mesh]
file = 1hex8_10mm_cube.e
[]
[Functions]
[./Fiss_Function]
type = PiecewiseLinear
x = '0 1e6 2e6 2.001e6 2.002e6'
y = '0 3e8 3e8 12e8 0'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[./temp]
initial_condition = 300.0
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
volumetric_locking_correction = true
incremental = true
eigenstrain_names = thermal_expansion
decomposition_method = EigenSolution
add_variables = true
generate_output = 'vonmises_stress'
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[./heat_ie]
type = HeatConductionTimeDerivative
variable = temp
[../]
[./heat_source]
type = HeatSource
variable = temp
value = 1.0
function = Fiss_Function
[../]
[]
[BCs]
[./bottom_temp]
type = DirichletBC
variable = temp
boundary = 1
value = 300
[../]
[./top_bottom_disp_x]
type = DirichletBC
variable = disp_x
boundary = '1'
value = 0
[../]
[./top_bottom_disp_y]
type = DirichletBC
variable = disp_y
boundary = '1'
value = 0
[../]
[./top_bottom_disp_z]
type = DirichletBC
variable = disp_z
boundary = '1'
value = 0
[../]
[]
[Materials]
[./thermal]
type = HeatConductionMaterial
temp = temp
specific_heat = 1.0
thermal_conductivity = 1.0
[../]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 300e6
poissons_ratio = .3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[./thermal_expansion]
type = ComputeThermalExpansionEigenstrain
thermal_expansion_coeff = 5e-6
stress_free_temperature = 300.0
temperature = temp
eigenstrain_name = thermal_expansion
[../]
[./density]
type = Density
density = 10963.0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
verbose = true
nl_abs_tol = 1e-10
start_time = 0.0
num_steps = 50000
end_time = 2.002e6
[./TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_function = Fiss_Function
max_function_change = 3e7
dt = 1e6
[../]
[]
[Postprocessors]
[./Temperature_of_Block]
type = ElementAverageValue
variable = temp
execute_on = 'initial timestep_end'
[../]
[./vonMises]
type = ElementAverageValue
variable = vonmises_stress
execute_on = 'initial timestep_end'
[../]
[]
[Outputs]
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 10
[../]
[]
(modules/tensor_mechanics/test/tests/central_difference/consistent/3D/3d_consistent_implicit.i)
# One element test for the Newmark-Beta time integrator.
[Mesh]
type = GeneratedMesh # Can generate simple lines, rectangles and rectangular prisms
dim = 3 # Dimension of the mesh
nx = 1 # Number of elements in the x direction
ny = 1 # Number of elements in the y direction
nz = 2 # Number of elements in the z direction
xmin = 0.0
xmax = 1
ymin = 0.0
ymax = 1
zmin = 0.0
zmax = 2
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./vel_x]
[../]
[./accel_x]
[../]
[./vel_y]
[../]
[./accel_y]
[../]
[./vel_z]
[../]
[./accel_z]
[../]
[]
[Kernels]
[./DynamicTensorMechanics]
displacements = 'disp_x disp_y disp_z'
[../]
[./inertia_x]
type = InertialForce
variable = disp_x
[../]
[./inertia_y]
type = InertialForce
variable = disp_y
[../]
[./inertia_z]
type = InertialForce
variable = disp_z
[../]
[]
[AuxKernels]
[./accel_x]
type = TestNewmarkTI
variable = accel_x
displacement = disp_x
first = false
[../]
[./vel_x]
type = TestNewmarkTI
variable = vel_x
displacement = disp_x
[../]
[./accel_y]
type = TestNewmarkTI
variable = accel_y
displacement = disp_y
first = false
[../]
[./vel_y]
type = TestNewmarkTI
variable = vel_y
displacement = disp_y
[../]
[./accel_z]
type = TestNewmarkTI
variable = accel_z
displacement = disp_z
first = false
[../]
[./vel_z]
type = TestNewmarkTI
variable = vel_z
displacement = disp_z
[../]
[]
[BCs]
[./x_bot]
type = PresetDisplacement
boundary = 'back'
variable = disp_x
beta = 0.25
velocity = vel_x
acceleration = accel_x
function = dispx
[../]
[./y_bot]
type = PresetDisplacement
boundary = 'back'
variable = disp_y
beta = 0.25
velocity = vel_y
acceleration = accel_y
function = dispy
[../]
[./z_bot]
type = PresetDisplacement
boundary = 'back'
variable = disp_z
beta = 0.25
velocity = vel_z
acceleration = accel_z
function = dispz
[../]
[./Periodic]
[./x_dir]
variable = 'disp_x disp_y disp_z'
primary = 'left'
secondary = 'right'
translation = '1.0 0.0 0.0'
[../]
[./y_dir]
variable = 'disp_x disp_y disp_z'
primary = 'bottom'
secondary = 'top'
translation = '0.0 1.0 0.0'
[../]
[../]
[]
[Functions]
[./dispx]
type = PiecewiseLinear
x = '0.0 1.0 2.0 3.0 4.0' # time
y = '0.0 1.0 0.0 -1.0 0.0' # displacement
[../]
[./dispy]
type = ParsedFunction
value = 0.1*t*t*sin(10*t)
[../]
[./dispz]
type = ParsedFunction
value = 0.1*t*t*sin(20*t)
[../]
[]
[Materials]
[./elasticity_tensor_block]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.25
block = 0
[../]
[./strain_block]
type = ComputeIncrementalSmallStrain
block = 0
displacements = 'disp_x disp_y disp_z'
[../]
[./stress_block]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = density
prop_values = 1e4
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
nl_abs_tol = 1e-08
nl_rel_tol = 1e-08
timestep_tolerance = 1e-6
start_time = -0.01
end_time = 0.1
dt = 0.005
[./TimeIntegrator]
type = NewmarkBeta
beta = 0.25
gamma = 0.5
[../]
[]
[Postprocessors]
[./accel_6x]
type = NodalVariableValue
nodeid = 6
variable = accel_x
[../]
[]
[Outputs]
exodus = false
csv = true
[]
(modules/combined/test/tests/cavity_pressure/3d.i)
#
# Cavity Pressure Test
#
# This test is designed to compute an internal pressure based on
# p = n * R * T / V
# where
# p is the pressure
# n is the amount of material in the volume (moles)
# R is the universal gas constant
# T is the temperature
# V is the volume
#
# The mesh is composed of one block (1) with an interior cavity of volume 8.
# Block 2 sits in the cavity and has a volume of 1. Thus, the total
# initial volume is 7.
# The test adjusts n, T, and V in the following way:
# n => n0 + alpha * t
# T => T0 + beta * t
# V => V0 + gamma * t
# with
# alpha = n0
# beta = T0 / 2
# gamma = - (0.003322259...) * V0
# T0 = 240.54443866068704
# V0 = 7
# n0 = f(p0)
# p0 = 100
# R = 8.314472 J * K^(-1) * mol^(-1)
#
# So, n0 = p0 * V0 / R / T0 = 100 * 7 / 8.314472 / 240.544439
# = 0.35
#
# The parameters combined at t = 1 gives p = 301.
#
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[Mesh]
file = 3d.e
[]
[Functions]
[./displ_positive]
type = PiecewiseLinear
x = '0 1'
y = '0 0.0029069767441859684'
[../]
[./displ_negative]
type = PiecewiseLinear
x = '0 1'
y = '0 -0.0029069767441859684'
[../]
[./temp1]
type = PiecewiseLinear
x = '0 1'
y = '1 1.5'
scale_factor = 240.54443866068704
[../]
[./material_input_function]
type = PiecewiseLinear
x = '0 1'
y = '0 0.35'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[./temp]
initial_condition = 240.54443866068704
[../]
[./material_input]
[../]
[]
[AuxVariables]
[./pressure_residual_x]
[../]
[./pressure_residual_y]
[../]
[./pressure_residual_z]
[../]
[./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_zx]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
[../]
[./heat]
type = Diffusion
variable = temp
use_displaced_mesh = true
[../]
[./material_input_dummy]
type = Diffusion
variable = material_input
use_displaced_mesh = true
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 0
variable = stress_xx
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 1
variable = stress_yy
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 2
variable = stress_zz
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 1
variable = stress_xy
[../]
[./stress_yz]
type = RankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 2
variable = stress_yz
[../]
[./stress_zx]
type = RankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 0
variable = stress_zx
[../]
[]
[BCs]
[./no_x_exterior]
type = DirichletBC
variable = disp_x
boundary = '7 8'
value = 0.0
[../]
[./no_y_exterior]
type = DirichletBC
variable = disp_y
boundary = '9 10'
value = 0.0
[../]
[./no_z_exterior]
type = DirichletBC
variable = disp_z
boundary = '11 12'
value = 0.0
[../]
[./prescribed_left]
type = FunctionDirichletBC
variable = disp_x
boundary = 13
function = displ_positive
[../]
[./prescribed_right]
type = FunctionDirichletBC
variable = disp_x
boundary = 14
function = displ_negative
[../]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = '15 16'
value = 0.0
[../]
[./no_z]
type = DirichletBC
variable = disp_z
boundary = '17 18'
value = 0.0
[../]
[./no_x_interior]
type = DirichletBC
variable = disp_x
boundary = '1 2'
value = 0.0
[../]
[./no_y_interior]
type = DirichletBC
variable = disp_y
boundary = '3 4'
value = 0.0
[../]
[./no_z_interior]
type = DirichletBC
variable = disp_z
boundary = '5 6'
value = 0.0
[../]
[./temperatureInterior]
type = FunctionDirichletBC
boundary = 100
function = temp1
variable = temp
[../]
[./MaterialInput]
type = FunctionDirichletBC
boundary = '100 13 14 15 16'
function = material_input_function
variable = material_input
[../]
[./CavityPressure]
[./1]
boundary = 100
initial_pressure = 100
material_input = materialInput
R = 8.314472
temperature = aveTempInterior
volume = internalVolume
startup_time = 0.5
output = ppress
save_in = 'pressure_residual_x pressure_residual_y pressure_residual_z'
[../]
[../]
[]
[Materials]
[./elast_tensor1]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e1
poissons_ratio = 0
block = 1
[../]
[./strain1]
type = ComputeFiniteStrain
block = 1
[../]
[./stress1]
type = ComputeFiniteStrainElasticStress
block = 1
[../]
[./elast_tensor2]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0
block = 2
[../]
[./strain2]
type = ComputeFiniteStrain
block = 2
[../]
[./stress2]
type = ComputeFiniteStrainElasticStress
block = 2
[../]
[]
[Executioner]
type = Transient
petsc_options_iname = '-pc_type -sub_pc_type'
petsc_options_value = 'asm lu'
nl_rel_tol = 1e-12
l_tol = 1e-12
l_max_its = 20
dt = 0.5
end_time = 1.0
[]
[Postprocessors]
[./internalVolume]
type = InternalVolume
boundary = 100
execute_on = 'initial linear'
[../]
[./aveTempInterior]
type = SideAverageValue
boundary = 100
variable = temp
execute_on = 'initial linear'
[../]
[./materialInput]
type = SideAverageValue
boundary = '7 8 9 10 11 12'
variable = material_input
execute_on = linear
[../]
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/elastic_patch/elastic_patch.i)
# Patch Test
# This test is designed to compute constant xx, yy, zz, xy, yz, and zx
# stress on a set of irregular hexes. The mesh is composed of one
# block with seven elements. The elements form a unit cube with one
# internal element. There is a nodeset for each exterior node.
# The cube is displaced by 1e-6 units in x, 2e-6 in y, and 3e-6 in z.
# The faces are sheared as well (1e-6, 2e-6, and 3e-6 for xy, yz, and
# zx). This gives a uniform strain/stress state for all six unique
# tensor components.
# With Young's modulus at 1e6 and Poisson's ratio at 0, the shear
# modulus is 5e5 (G=E/2/(1+nu)). Therefore,
#
# stress xx = 1e6 * 1e-6 = 1
# stress yy = 1e6 * 2e-6 = 2
# stress zz = 1e6 * 3e-6 = 3
# stress xy = 2 * 5e5 * 1e-6 / 2 = 0.5
# (2 * G * gamma_xy / 2 = 2 * G * epsilon_xy)
# stress yz = 2 * 5e5 * 2e-6 / 2 = 1
# stress zx = 2 * 5e5 * 3e-6 / 2 = 1.5
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
block = '1 2 3 4 5 6 7'
[]
[Mesh]#Comment
file = elastic_patch.e
[] # Mesh
[Functions]
[./rampConstant1]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 1.'
scale_factor = 1e-6
[../]
[./rampConstant2]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 1.'
scale_factor = 2e-6
[../]
[./rampConstant3]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 1.'
scale_factor = 3e-6
[../]
[./rampConstant4]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 1.'
scale_factor = 4e-6
[../]
[./rampConstant6]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 1. 1.'
scale_factor = 6e-6
[../]
[] # Functions
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[] # Variables
[AuxVariables]
[./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_zx]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_energy]
order = CONSTANT
family = MONOMIAL
[../]
[./vonmises]
order = CONSTANT
family = MONOMIAL
[../]
[./hydrostatic]
order = CONSTANT
family = MONOMIAL
[../]
[./firstinv]
order = CONSTANT
family = MONOMIAL
[../]
[./secondinv]
order = CONSTANT
family = MONOMIAL
[../]
[./thirdinv]
order = CONSTANT
family = MONOMIAL
[../]
[./maxprincipal]
order = CONSTANT
family = MONOMIAL
[../]
[./midprincipal]
order = CONSTANT
family = MONOMIAL
[../]
[./minprincipal]
order = CONSTANT
family = MONOMIAL
[../]
[./direction]
order = CONSTANT
family = MONOMIAL
[../]
[./max_shear]
order = CONSTANT
family = MONOMIAL
[../]
[./sint]
order = CONSTANT
family = MONOMIAL
[../]
[] # AuxVariables
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
[../]
[./stress_yz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yz
index_i = 1
index_j = 2
[../]
[./stress_zx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zx
index_i = 2
index_j = 0
[../]
[./elastic_energy]
type = ElasticEnergyAux
variable = elastic_energy
[../]
[./vonmises]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = vonmises
scalar_type = vonmisesStress
[../]
[./hydrostatic]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = hydrostatic
scalar_type = hydrostatic
[../]
[./fi]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = firstinv
scalar_type = firstinvariant
[../]
[./si]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = secondinv
scalar_type = secondinvariant
[../]
[./ti]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = thirdinv
scalar_type = thirdinvariant
[../]
[./maxprincipal]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = maxprincipal
scalar_type = MaxPRiNCIpAl
[../]
[./midprincipal]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = midprincipal
scalar_type = MidPRiNCIpAl
[../]
[./minprincipal]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = minprincipal
scalar_type = MiNPRiNCIpAl
[../]
[./direction]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = direction
scalar_type = direction
direction = '1 1 1'
[../]
[./max_shear]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = max_shear
scalar_type = MaxShear
[../]
[./sint]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = sint
scalar_type = StressIntensity
[../]
[] # AuxKernels
[BCs]
[./node1_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./node1_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 1
function = rampConstant2
[../]
[./node1_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 1
function = rampConstant3
[../]
[./node2_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 2
function = rampConstant1
[../]
[./node2_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = rampConstant2
[../]
[./node2_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 2
function = rampConstant6
[../]
[./node3_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 3
function = rampConstant1
[../]
[./node3_y]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.0
[../]
[./node3_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 3
function = rampConstant3
[../]
[./node4_x]
type = DirichletBC
variable = disp_x
boundary = 4
value = 0.0
[../]
[./node4_y]
type = DirichletBC
variable = disp_y
boundary = 4
value = 0.0
[../]
[./node4_z]
type = DirichletBC
variable = disp_z
boundary = 4
value = 0.0
[../]
[./node5_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 5
function = rampConstant1
[../]
[./node5_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 5
function = rampConstant4
[../]
[./node5_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 5
function = rampConstant3
[../]
[./node6_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 6
function = rampConstant2
[../]
[./node6_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 6
function = rampConstant4
[../]
[./node6_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 6
function = rampConstant6
[../]
[./node7_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 7
function = rampConstant2
[../]
[./node7_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 7
function = rampConstant2
[../]
[./node7_z]
type = FunctionDirichletBC
variable = disp_z
boundary = 7
function = rampConstant3
[../]
[./node8_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 8
function = rampConstant1
[../]
[./node8_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 8
function = rampConstant2
[../]
[./node8_z]
type = DirichletBC
variable = disp_z
boundary = 8
value = 0.0
[../]
[] # BCs
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.0
[../]
[./strain]
type = ComputeFiniteStrain
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[] # Materials
[Executioner]
type = Transient
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
nl_abs_tol = 1e-10
l_max_its = 20
start_time = 0.0
dt = 1.0
num_steps = 2
end_time = 2.0
[] # Executioner
[Outputs]
exodus = true
[] # Outputs
(modules/richards/test/tests/gravity_head_2/gh17.i)
# unsaturated = false
# gravity = true
# supg = true
# transient = true
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
xmin = 0
xmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1E-2 1E-1 1E0 1E1 1E3 1E4 1E5 1E6 1E7'
x = '0 1E-1 1E0 1E1 1E2 1E3 1E4 1E5 1E6'
[../]
[]
[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 = 0.1
[../]
[./SUPGgas]
type = RichardsSUPGstandard
p_SUPG = 0.01
[../]
[]
[Variables]
[./pwater]
order = FIRST
family = LAGRANGE
[../]
[./pgas]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./water_ic]
type = ConstantIC
value = 1
variable = pwater
[../]
[./gas_ic]
type = ConstantIC
value = 1
variable = pgas
[../]
[]
[Kernels]
active = 'richardsfwater richardstwater richardsfgas richardstgas'
[./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
[../]
[./mass_error_gas]
type = FunctionValuePostprocessor
function = fcn_mass_error_g
[../]
[./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
[../]
[]
[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((-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'
[../]
[]
[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 -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-15 10000'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
end_time = 1E6
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
execute_on = 'timestep_end'
file_base = gh17
csv = true
[]
(test/tests/geomsearch/3d_moving_penetration_smoothing/pl_test3nns.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
file = pl_test3.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./normal_z]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./closest_point_z]
[../]
# [./element_id]
# [../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[./diff_z]
type = Diffusion
variable = disp_z
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
normal_smoothing_method = nodal_normal_based
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = normal_z
boundary = 11
paired_boundary = 12
quantity = normal_z
[../]
[./penetrate10]
type = PenetrationAux
variable = normal_z
boundary = 12
paired_boundary = 11
quantity = normal_z
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate13]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate14]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate15]
type = PenetrationAux
variable = closest_point_z
boundary = 11
paired_boundary = 12
quantity = closest_point_z
[../]
[./penetrate16]
type = PenetrationAux
variable = closest_point_z
boundary = 12
paired_boundary = 11
quantity = closest_point_z
[../]
# [./penetrate17]
# type = PenetrationAux
# variable = element_id
# boundary = 11
# paired_boundary = 12
# quantity = element_id
# [../]
#
# [./penetrate18]
# type = PenetrationAux
# variable = element_id
# boundary = 12
# paired_boundary = 11
# quantity = element_id
# [../]
[./penetrate19]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate20]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
preset = false
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
preset = false
boundary = 1
value = 0
[../]
[./b1z]
type = DirichletBC
variable = disp_z
preset = false
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
preset = false
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
preset = false
boundary = 2
function = disp_y
[../]
[./b2z]
type = DirichletBC
variable = disp_z
preset = false
boundary = 2
value = 0
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-9
l_max_its = 10
start_time = 0.0
dt = 0.02
end_time = 1.0
[]
[Outputs]
file_base = pl_test3nns_out
exodus = true
[]
[NodalNormals]
boundary = 11
corner_boundary = 20
[]
(modules/tensor_mechanics/test/tests/shell/dynamics/shell_dynamics_bending_moment_free.i)
# Test to verify the fundamental natural frequency of a one element ADComputeShellStress
# BCs: Clamped on one end, free on others.
# Initial perturbation applied to edge of the beam. After that, the shell vibrates freely.
#
# Results have been compared for various thicknesses with the following approximate Results
# (Moose results were obtained with 8 elements along the length)
# Thickness = 0.1. Reference freq: 10.785 Hz, Moose freq: 10.612 Hz
# Thickness = 0.05. Reference freq: 5.393 Hz, Moose freq: 5.335 Hz
# Thickness = 0.025. Reference freq: 2.696 Hz, Moose freq: 2.660 Hz
#
# Reference values have been obtained from Robert Blevins, "Formulas for Dynamics, Acoustics and Vibration",
# Table 5.3 case 11. Formula looks like: f = lambda^2/(2*pi*a^2) * sqrt(E*h^2/(12*(1-nu*nu))), where lambda
# changes as a function of shell dimensions.
# This test uses one single element for speed reasons.
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1 # 1
ny = 1# 4
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.5
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[./rot_x]
[../]
[./rot_y]
[../]
[]
[AuxVariables]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yz]
order = CONSTANT
family = MONOMIAL
[../]
# aux variables for dynamics
[./vel_x]
[../]
[./vel_y]
[../]
[./vel_z]
[../]
[./accel_x]
[../]
[./accel_y]
[../]
[./accel_z]
[../]
[./rot_vel_x]
[../]
[./rot_vel_y]
[../]
[./rot_accel_x]
[../]
[./rot_accel_y]
[../]
[]
[AuxKernels]
[./stress_yy]
type = RankTwoAux
variable = stress_yy
rank_two_tensor = global_stress_t_points_0
index_i = 1
index_j = 1
[../]
[./stress_yz]
type = RankTwoAux
variable = stress_yz
rank_two_tensor = global_stress_t_points_0
index_i = 1
index_j = 2
[../]
# Kernels for dynamics
[./accel_x]
type = NewmarkAccelAux
variable = accel_x
displacement = disp_x
velocity = vel_x
beta = 0.25
execute_on = timestep_end
[../]
[./vel_x]
type = NewmarkVelAux
variable = vel_x
acceleration = accel_x
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_y]
type = NewmarkAccelAux
variable = accel_y
displacement = disp_y
velocity = vel_y
beta = 0.25
execute_on = timestep_end
[../]
[./vel_y]
type = NewmarkVelAux
variable = vel_y
acceleration = accel_y
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_z]
type = NewmarkAccelAux
variable = accel_z
displacement = disp_z
velocity = vel_z
beta = 0.25
execute_on = timestep_end
[../]
[./vel_z]
type = NewmarkVelAux
variable = vel_z
acceleration = accel_z
gamma = 0.5
execute_on = timestep_end
[../]
[./rot_accel_x]
type = NewmarkAccelAux
variable = rot_accel_x
displacement = rot_x
velocity = rot_vel_x
beta = 0.25
execute_on = timestep_end
[../]
[./rot_vel_x]
type = NewmarkVelAux
variable = rot_vel_x
acceleration = rot_accel_x
gamma = 0.5
execute_on = timestep_end
[../]
[./rot_accel_y]
type = NewmarkAccelAux
variable = rot_accel_y
displacement = rot_y
velocity = rot_vel_y
beta = 0.25
execute_on = timestep_end
[../]
[./rot_vel_y]
type = NewmarkVelAux
variable = rot_vel_y
acceleration = rot_accel_y
gamma = 0.5
execute_on = timestep_end
[../]
[]
[BCs]
[./fixy1]
type = DirichletBC
variable = disp_y
boundary = 'bottom'
value = 0.0
[../]
[./fixz1]
type = DirichletBC
variable = disp_z
boundary = 'bottom'
value = 0.0
[../]
[./fixr1]
type = DirichletBC
variable = rot_x
boundary = 'bottom'
value = 0.0
[../]
[./fixr2]
type = DirichletBC
variable = rot_y
boundary = 'bottom'
value = 0.0
[../]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = 'bottom'
value = 0.0
[../]
[]
[Functions]
[./force_function]
type = PiecewiseLinear
x = '0.0 0.01 0.15 10.0'
y = '0.0 0.01 0.0 0.0'
[../]
[]
[NodalKernels]
[./force_z2]
type = UserForcingFunctionNodalKernel
variable = disp_z
boundary = 'top'
function = force_function
[../]
[]
[Kernels]
[./solid_disp_x]
type = ADStressDivergenceShell
block = '0'
component = 0
variable = disp_x
through_thickness_order = SECOND
[../]
[./solid_disp_y]
type = ADStressDivergenceShell
block = '0'
component = 1
variable = disp_y
through_thickness_order = SECOND
[../]
[./solid_disp_z]
type = ADStressDivergenceShell
block = '0'
component = 2
variable = disp_z
through_thickness_order = SECOND
[../]
[./solid_rot_x]
type = ADStressDivergenceShell
block = '0'
component = 3
variable = rot_x
through_thickness_order = SECOND
[../]
[./solid_rot_y]
type = ADStressDivergenceShell
block = '0'
component = 4
variable = rot_y
through_thickness_order = SECOND
[../]
[./inertial_force_x]
type = ADInertialForceShell
# use_displaced_mesh = true
eta = 0.0
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y'
rotational_accelerations = 'rot_accel_x rot_accel_y'
component = 0
variable = disp_x
thickness = 0.1
[../]
[./inertial_force_y]
type = ADInertialForceShell
eta = 0.0
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y'
rotational_accelerations = 'rot_accel_x rot_accel_y'
component = 1
variable = disp_y
thickness = 0.1
[../]
[./inertial_force_z]
type = ADInertialForceShell
eta = 0.0
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y'
rotational_accelerations = 'rot_accel_x rot_accel_y'
component = 2
variable = disp_z
thickness = 0.1
[../]
[./inertial_force_rot_x]
type = ADInertialForceShell
eta = 0.0
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y'
rotational_accelerations = 'rot_accel_x rot_accel_y'
component = 3
variable = rot_x
thickness = 0.1
[../]
[./inertial_force_rot_y]
type = ADInertialForceShell
eta = 0.0
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y'
rotational_accelerations = 'rot_accel_x rot_accel_y'
component = 4
variable = rot_y
thickness = 0.1
[../]
[]
[Materials]
[./elasticity]
type = ADComputeIsotropicElasticityTensorShell
youngs_modulus = 2100000
poissons_ratio = 0.3
block = 0
through_thickness_order = SECOND
[../]
[./strain]
type = ADComputeIncrementalShellStrain
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y'
thickness = 0.1
through_thickness_order = SECOND
[../]
[./stress]
type = ADComputeShellStress
block = 0
through_thickness_order = SECOND
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = 'density'
prop_values = '1.0'
[../]
[]
[Postprocessors]
[./disp_z_tip]
type = PointValue
point = '1.0 1.0 0.0'
variable = disp_z
[../]
[./rot_x_tip]
type = PointValue
point = '0.0 1.0 0.0'
variable = rot_x
[../]
[./stress_yy_el_0]
type = ElementalVariableValue
elementid = 0
variable = stress_yy
[../]
[./stress_yy_el_1]
type = ElementalVariableValue
elementid = 1
variable = stress_yy
[../]
[./stress_yy_el_2]
type = ElementalVariableValue
elementid = 2
variable = stress_yy
[../]
[./stress_yy_el_3]
type = ElementalVariableValue
elementid = 3
variable = stress_yy
[../]
[./stress_yz_el_0]
type = ElementalVariableValue
elementid = 0
variable = stress_yz
[../]
[./stress_yz_el_1]
type = ElementalVariableValue
elementid = 1
variable = stress_yz
[../]
[./stress_yz_el_2]
type = ElementalVariableValue
elementid = 2
variable = stress_yz
[../]
[./stress_yz_el_3]
type = ElementalVariableValue
elementid = 3
variable = stress_yz
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
l_tol = 1e-11
nl_max_its = 15
nl_rel_tol = 1e-11
nl_abs_tol = 1e-10
l_max_its = 20
dt = 0.005
dtmin = 0.005
timestep_tolerance = 2e-13
end_time = 0.5
[./TimeIntegrator]
type = NewmarkBeta
beta = 0.25
gamma = 0.5
[../]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[]
(modules/tensor_mechanics/test/tests/1D_axisymmetric/axisymmetric_gps_incremental.i)
#
# This test checks the generalized plane strain using incremental small strain formulation.
# The model consists of two sets of line elements. One undergoes a temperature rise of 100 with
# the other seeing a temperature rise of 300. Young's modulus is 3600, and
# Poisson's ratio is 0.2. The thermal expansion coefficient is 1e-8. All
# nodes are constrained against movement.
#
# For plane strain case, i.e., without constraining the strain_yy to be uniform,
# the stress solution would be [-6e-3, -6e-3, -6e-3] and [-18e-3, -18e-3, -18e-3] (xx, yy, zz).
# The generalized plane strain kernels work to balance the force in y direction.
#
# With out of plane strain of 3e-6, the stress solution becomes
# [-3e-3, 6e-3, -3e-3] and [-15e-3, -6e-3, -15e-3] (xx, yy, zz). This gives
# a domain integral of out-of-plane stress to be zero.
#
[GlobalParams]
displacements = disp_x
scalar_out_of_plane_strain = scalar_strain_yy
[]
[Problem]
coord_type = RZ
[]
[Mesh]
file = lines.e
[]
[Variables]
[./disp_x]
[../]
[./temp]
initial_condition = 580.0
[../]
[./scalar_strain_yy]
order = FIRST
family = SCALAR
[../]
[]
[Functions]
[./temp100]
type = PiecewiseLinear
x = '0 1'
y = '580 680'
[../]
[./temp300]
type = PiecewiseLinear
x = '0 1'
y = '580 880'
[../]
[]
[Kernels]
[./heat]
type = Diffusion
variable = temp
[../]
[]
[Modules]
[./TensorMechanics]
[./Master]
[./gps]
planar_formulation = GENERALIZED_PLANE_STRAIN
scalar_out_of_plane_strain = scalar_strain_yy
strain = SMALL
incremental = true
generate_output = 'strain_xx strain_yy strain_zz stress_xx stress_yy stress_zz'
eigenstrain_names = eigenstrain
[../]
[../]
[../]
[]
[BCs]
[./no_x]
type = DirichletBC
boundary = 1000
value = 0
variable = disp_x
[../]
[./temp100]
type = FunctionDirichletBC
variable = temp
function = temp100
boundary = 2
[../]
[./temp300]
type = FunctionDirichletBC
variable = temp
function = temp300
boundary = 3
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 3600
poissons_ratio = 0.2
[../]
[./thermal_strain]
type = ComputeThermalExpansionEigenstrain
thermal_expansion_coeff = 1e-8
temperature = temp
stress_free_temperature = 580
eigenstrain_name = eigenstrain
[../]
[./stress]
type = ComputeStrainIncrementBasedStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
line_search = 'none'
l_max_its = 50
l_tol = 1e-6
nl_max_its = 15
nl_abs_tol = 1e-10
start_time = 0
end_time = 1
num_steps = 1
[]
[Outputs]
exodus = true
console = true
[]
(test/tests/multiapps/picard/function_dt_master.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
ymin = 0
xmax = 1
ymax = 1
nx = 10
ny = 10
[]
[Functions]
[./v_fn]
type = ParsedFunction
value = t*x
[../]
[./ffn]
type = ParsedFunction
value = x
[../]
[./dts]
type = PiecewiseLinear
x = '0.1 10'
y = '0.1 10'
[../]
[]
[AuxVariables]
[./v]
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./td]
type = TimeDerivative
variable = u
[../]
[./ufn]
type = BodyForce
variable = u
function = ffn
[../]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
boundary = 'left right top bottom'
function = v_fn
[../]
[]
[Executioner]
type = Transient
dt = 0.1
solve_type = 'PJFNK'
nl_abs_tol = 1e-10
picard_max_its = 2
start_time = 0
num_steps = 3
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
exodus = true
[]
[MultiApps]
[./sub_app]
app_type = MooseTestApp
type = TransientMultiApp
input_files = 'function_dt_sub.i'
execute_on = timestep_end
positions = '0 -1 0'
[../]
[]
[Transfers]
[./from_sub]
type = MultiAppNearestNodeTransfer
direction = from_multiapp
multi_app = sub_app
source_variable = u
variable = v
[../]
[]
(modules/contact/test/tests/tension_release/4ElemTensionRelease_mechanical_constraint.i)
# This is a mechanical constraint (contact formulation) version of 4ElemTensionRelease.i
[Mesh]
file = 4ElemTensionRelease.e
[]
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Functions]
[./up]
type = PiecewiseLinear
x = '0 1 2 3'
y = '0 0.0001 0 -.0001'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = SMALL
generate_output = 'stress_yy'
[]
[]
[Contact]
[./dummy_name]
primary = 2
secondary = 3
penalty = 1e6
model = frictionless
tangential_tolerance = 0.01
[../]
[]
[BCs]
[./lateral]
type = DirichletBC
variable = disp_x
boundary = '1 4'
value = 0
[../]
[./bottom_up]
type = FunctionDirichletBC
variable = disp_y
boundary = 1
function = up
[../]
[./top]
type = DirichletBC
variable = disp_y
boundary = 4
value = 0.0
[../]
[]
[Materials]
[./stiffStuff1]
type = ComputeIsotropicElasticityTensor
block = '1 2'
youngs_modulus = 1.0e6
poissons_ratio = 0.3
[../]
[./stiffStuff1_stress]
type = ComputeLinearElasticStress
block = '1 2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart'
petsc_options_value = 'hypre boomeramg 101'
line_search = 'none'
nl_rel_tol = 1e-8
nl_abs_tol = 1e-10
l_tol = 1e-4
l_max_its = 100
nl_max_its = 10
dt = 0.2
dtmin = 0.2
end_time = 3
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
[]
[Outputs]
exodus = true
[]
(modules/tensor_mechanics/test/tests/ad_viscoplasticity_stress_update/lps_dual.i)
# This test provides an example of combining two LPS viscoplasticity models with different stress
# exponents.
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 1
ny = 1
xmax = 0.002
ymax = 0.002
[]
[Variables]
[./temp]
initial_condition = 1000
[../]
[]
[Kernels]
[./dt]
type = ADTimeDerivative
variable = temp
[../]
[./diff]
type = ADDiffusion
variable = temp
[../]
[]
[Modules/TensorMechanics/Master/All]
strain = FINITE
add_variables = true
generate_output = 'strain_xx strain_yy strain_xy hydrostatic_stress vonmises_stress'
use_automatic_differentiation = true
[]
[Functions]
[./pull]
type = PiecewiseLinear
x = '0 0.1'
y = '0 1e-5'
[../]
[./tot_effective_viscoplasticity]
type = ParsedFunction
vals = 'lps_1_eff_creep_strain lps_3_eff_creep_strain'
vars = 'lps_1_eff_creep_strain lps_3_eff_creep_strain'
value = 'lps_1_eff_creep_strain+lps_3_eff_creep_strain'
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1e10
poissons_ratio = 0.3
[../]
[./stress]
type = ADComputeMultipleInelasticStress
inelastic_models = 'one two'
outputs = all
[../]
[./porosity]
type = ADPorosityFromStrain
initial_porosity = 0.1
inelastic_strain = 'combined_inelastic_strain'
outputs = 'all'
[../]
[./one]
type = ADViscoplasticityStressUpdate
coefficient = 'coef_3'
power = 3
base_name = 'lps_1'
outputs = all
relative_tolerance = 1e-11
[../]
[./two]
type = ADViscoplasticityStressUpdate
coefficient = 1e-10
power = 1
base_name = 'lps_3'
outputs = all
relative_tolerance = 1e-11
[../]
[./coef]
type = ADParsedMaterial
f_name = coef_3
# Example of creep power law
args = temp
function = '0.5e-18 * exp(-4e4 / 1.987 / temp)'
[../]
[]
[BCs]
[./no_disp_x]
type = ADDirichletBC
variable = disp_x
boundary = left
value = 0.0
[../]
[./no_disp_y]
type = ADDirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[./pull_disp_y]
type = ADFunctionDirichletBC
variable = disp_y
boundary = top
function = pull
[../]
[./temp_ramp]
type = ADFunctionDirichletBC
boundary = right
function = '1000 + 400 * t / 0.12'
variable = temp
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
dt = 0.01
end_time = 0.12
[]
[Postprocessors]
[./disp_x]
type = SideAverageValue
variable = disp_x
boundary = right
[../]
[./disp_y]
type = SideAverageValue
variable = disp_y
boundary = top
[../]
[./avg_hydro]
type = ElementAverageValue
variable = hydrostatic_stress
[../]
[./avg_vonmises]
type = ElementAverageValue
variable = vonmises_stress
[../]
[./dt]
type = TimestepSize
[../]
[./num_lin]
type = NumLinearIterations
outputs = console
[../]
[./num_nonlin]
type = NumNonlinearIterations
outputs = console
[../]
[./lps_1_eff_creep_strain]
type = ElementAverageValue
variable = lps_1_effective_viscoplasticity
[../]
[./lps_3_eff_creep_strain]
type = ElementAverageValue
variable = lps_3_effective_viscoplasticity
[../]
[./lps_1_gauge_stress]
type = ElementAverageValue
variable = lps_1_gauge_stress
[../]
[./lps_3_gauge_stress]
type = ElementAverageValue
variable = lps_3_gauge_stress
[../]
[./eff_creep_strain_tot]
type = FunctionValuePostprocessor
function = tot_effective_viscoplasticity
[../]
[./porosity]
type = ElementAverageValue
variable = porosity
[../]
[]
[Outputs]
csv = true
[]
(modules/tensor_mechanics/test/tests/shell/dynamics/shell_dynamics_bending_moment_free_orientation_inclined.i)
# Test to verify the fundamental natural frequency of a one element ADComputeShellStress
# BCs: Clamped on one end, free on others.
# Initial perturbation applied to edge of the beam. After that, the shell vibrates freely.
#
# Results have been compared for various thicknesses with the following approximate Results
# (Moose results were obtained with 8 elements along the length)
# Thickness = 0.1. Reference freq: 10.785 Hz, Moose freq: 10.612 Hz
# Thickness = 0.05. Reference freq: 5.393 Hz, Moose freq: 5.335 Hz
# Thickness = 0.025. Reference freq: 2.696 Hz, Moose freq: 2.660 Hz
#
# Reference values have been obtained from Robert Blevins, "Formulas for Dynamics, Acoustics and Vibration",
# Table 5.3 case 11. Formula looks like: f = lambda^2/(2*pi*a^2) * sqrt(E*h^2/(12*(1-nu*nu))), where lambda
# changes as a function of shell dimensions.
# This test uses one single element for speed reasons.
# Here, the shell, instead of being on the XY plane, is oriented at a 45 deg. angle
# with respect to the Y axis.
[Mesh]
type = FileMesh
file = shell_inclined.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[./rot_x]
[../]
[./rot_y]
[../]
[]
[AuxVariables]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yz]
order = CONSTANT
family = MONOMIAL
[../]
# aux variables for dynamics
[./vel_x]
[../]
[./vel_y]
[../]
[./vel_z]
[../]
[./accel_x]
[../]
[./accel_y]
[../]
[./accel_z]
[../]
[./rot_vel_x]
[../]
[./rot_vel_y]
[../]
[./rot_accel_x]
[../]
[./rot_accel_y]
[../]
[]
[AuxKernels]
[./stress_yy]
type = RankTwoAux
variable = stress_yy
rank_two_tensor = global_stress_t_points_0
index_i = 1
index_j = 1
[../]
[./stress_yz]
type = RankTwoAux
variable = stress_yz
rank_two_tensor = global_stress_t_points_0
index_i = 1
index_j = 2
[../]
# Kernels for dynamics
[./accel_x]
type = NewmarkAccelAux
variable = accel_x
displacement = disp_x
velocity = vel_x
beta = 0.25
execute_on = timestep_end
[../]
[./vel_x]
type = NewmarkVelAux
variable = vel_x
acceleration = accel_x
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_y]
type = NewmarkAccelAux
variable = accel_y
displacement = disp_y
velocity = vel_y
beta = 0.25
execute_on = timestep_end
[../]
[./vel_y]
type = NewmarkVelAux
variable = vel_y
acceleration = accel_y
gamma = 0.5
execute_on = timestep_end
[../]
[./accel_z]
type = NewmarkAccelAux
variable = accel_z
displacement = disp_z
velocity = vel_z
beta = 0.25
execute_on = timestep_end
[../]
[./vel_z]
type = NewmarkVelAux
variable = vel_z
acceleration = accel_z
gamma = 0.5
execute_on = timestep_end
[../]
[./rot_accel_x]
type = NewmarkAccelAux
variable = rot_accel_x
displacement = rot_x
velocity = rot_vel_x
beta = 0.25
execute_on = timestep_end
[../]
[./rot_vel_x]
type = NewmarkVelAux
variable = rot_vel_x
acceleration = rot_accel_x
gamma = 0.5
execute_on = timestep_end
[../]
[./rot_accel_y]
type = NewmarkAccelAux
variable = rot_accel_y
displacement = rot_y
velocity = rot_vel_y
beta = 0.25
execute_on = timestep_end
[../]
[./rot_vel_y]
type = NewmarkVelAux
variable = rot_vel_y
acceleration = rot_accel_y
gamma = 0.5
execute_on = timestep_end
[../]
[]
[BCs]
[./fixy1]
type = DirichletBC
variable = disp_y
boundary = '0'
value = 0.0
[../]
[./fixz1]
type = DirichletBC
variable = disp_z
boundary = '0'
value = 0.0
[../]
[./fixr1]
type = DirichletBC
variable = rot_x
boundary = '0'
value = 0.0
[../]
[./fixr2]
type = DirichletBC
variable = rot_y
boundary = '0'
value = 0.0
[../]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = '0'
value = 0.0
[../]
[]
[Functions]
[./force_function]
type = PiecewiseLinear
x = '0.0 0.01 0.15 10.0'
y = '0.0 0.01 0.0 0.0'
[../]
[]
[NodalKernels]
[./force_y2]
type = UserForcingFunctionNodalKernel
variable = disp_z
boundary = '2'
function = force_function
[../]
[]
[Kernels]
[./solid_disp_x]
type = ADStressDivergenceShell
block = '0'
component = 0
variable = disp_x
through_thickness_order = SECOND
[../]
[./solid_disp_y]
type = ADStressDivergenceShell
block = '0'
component = 1
variable = disp_y
through_thickness_order = SECOND
[../]
[./solid_disp_z]
type = ADStressDivergenceShell
block = '0'
component = 2
variable = disp_z
through_thickness_order = SECOND
[../]
[./solid_rot_x]
type = ADStressDivergenceShell
block = '0'
component = 3
variable = rot_x
through_thickness_order = SECOND
[../]
[./solid_rot_y]
type = ADStressDivergenceShell
block = '0'
component = 4
variable = rot_y
through_thickness_order = SECOND
[../]
[./inertial_force_x]
type = ADInertialForceShell
use_displaced_mesh = true
eta = 0.0
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y'
rotational_accelerations = 'rot_accel_x rot_accel_y'
component = 0
variable = disp_x
thickness = 0.1
[../]
[./inertial_force_y]
type = ADInertialForceShell
use_displaced_mesh = true
eta = 0.0
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y'
rotational_accelerations = 'rot_accel_x rot_accel_y'
component = 1
variable = disp_y
thickness = 0.1
[../]
[./inertial_force_z]
type = ADInertialForceShell
use_displaced_mesh = true
eta = 0.0
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y'
rotational_accelerations = 'rot_accel_x rot_accel_y'
component = 2
variable = disp_z
thickness = 0.1
[../]
[./inertial_force_rot_x]
type = ADInertialForceShell
use_displaced_mesh = true
eta = 0.0
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y'
rotational_accelerations = 'rot_accel_x rot_accel_y'
component = 3
variable = rot_x
thickness = 0.1
[../]
[./inertial_force_rot_y]
type = ADInertialForceShell
use_displaced_mesh = true
eta = 0.0
block = 0
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y'
velocities = 'vel_x vel_y vel_z'
accelerations = 'accel_x accel_y accel_z'
rotational_velocities = 'rot_vel_x rot_vel_y'
rotational_accelerations = 'rot_accel_x rot_accel_y'
component = 4
variable = rot_y
thickness = 0.1
[../]
[]
[Materials]
[./elasticity]
type = ADComputeIsotropicElasticityTensorShell
youngs_modulus = 2100000
poissons_ratio = 0.3
block = 0
through_thickness_order = SECOND
[../]
[./strain]
type = ADComputeIncrementalShellStrain
block = '0'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y'
thickness = 0.1
through_thickness_order = SECOND
[../]
[./stress]
type = ADComputeShellStress
block = 0
through_thickness_order = SECOND
[../]
[./density]
type = GenericConstantMaterial
block = 0
prop_names = 'density'
prop_values = '1.0'
[../]
[]
[Postprocessors]
[./disp_z_tip]
type = PointValue
point = '0.0 1.06 1.06'
variable = disp_z
[../]
[./rot_x_tip]
type = PointValue
point = '0.0 1.06 1.06'
variable = rot_x
[../]
[./stress_yy_el_0]
type = ElementalVariableValue
elementid = 0
variable = stress_yy
[../]
[./stress_yy_el_1]
type = ElementalVariableValue
elementid = 1
variable = stress_yy
[../]
[./stress_yy_el_2]
type = ElementalVariableValue
elementid = 2
variable = stress_yy
[../]
[./stress_yy_el_3]
type = ElementalVariableValue
elementid = 3
variable = stress_yy
[../]
[./stress_yz_el_0]
type = ElementalVariableValue
elementid = 0
variable = stress_yz
[../]
[./stress_yz_el_1]
type = ElementalVariableValue
elementid = 1
variable = stress_yz
[../]
[./stress_yz_el_2]
type = ElementalVariableValue
elementid = 2
variable = stress_yz
[../]
[./stress_yz_el_3]
type = ElementalVariableValue
elementid = 3
variable = stress_yz
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
l_tol = 1e-11
nl_max_its = 15
nl_rel_tol = 1e-11
nl_abs_tol = 1e-10
l_max_its = 20
dt = 0.005
dtmin = 0.005
timestep_tolerance = 2e-13
end_time = 0.5
[./TimeIntegrator]
type = NewmarkBeta
beta = 0.25
gamma = 0.5
[../]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[]
(modules/porous_flow/test/tests/infiltration_and_drainage/bw02.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 200
ny = 1
xmin = -10
xmax = 10
ymin = 0
ymax = 0.05
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Functions]
[dts]
type = PiecewiseLinear
y = '1E-1 5E-1 5E-1'
x = '0 1 10'
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = pressure
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureBW
Sn = 0.0
Ss = 1.0
C = 1.5
las = 2
[]
[]
[Modules]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 2e9
viscosity = 4
density0 = 10
thermal_expansion = 0
[]
[]
[]
[Materials]
[massfrac]
type = PorousFlowMassFraction
[]
[temperature]
type = PorousFlowTemperature
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pressure
capillary_pressure = pc
[]
[relperm]
type = PorousFlowRelativePermeabilityBW
Sn = 0.0
Ss = 1.0
Kn = 0
Ks = 1
C = 1.5
phase = 0
[]
[porosity]
type = PorousFlowPorosityConst
porosity = 0.25
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1 0 0 0 1 0 0 0 1'
[]
[]
[Variables]
[pressure]
initial_condition = -9E2
[]
[]
[Kernels]
[mass0]
type = PorousFlowMassTimeDerivative
fluid_component = 0
variable = pressure
[]
[flux0]
type = PorousFlowAdvectiveFlux
fluid_component = 0
variable = pressure
gravity = '-0.1 0 0'
[]
[]
[AuxVariables]
[SWater]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[SWater]
type = MaterialStdVectorAux
property = PorousFlow_saturation_qp
index = 0
variable = SWater
[]
[]
[BCs]
[recharge]
type = PorousFlowSink
variable = pressure
boundary = right
flux_function = -1.25 # corresponds to Rstar being 0.5 because i have to multiply by density*porosity
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
petsc_options = '-snes_converged_reason -ksp_diagonal_scale -ksp_diagonal_scale_fix -ksp_gmres_modifiedgramschmidt -snes_linesearch_monitor'
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -sub_pc_factor_shift_type -pc_asm_overlap -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'gmres asm lu NONZERO 2 1E-10 1E-10 10000'
[]
[]
[Executioner]
type = Transient
solve_type = Newton
petsc_options = '-snes_converged_reason'
end_time = 2
[TimeStepper]
type = FunctionDT
function = dts
[]
[]
[VectorPostprocessors]
[swater]
type = LineValueSampler
variable = SWater
start_point = '-10 0 0'
end_point = '10 0 0'
sort_by = x
num_points = 80
execute_on = timestep_end
[]
[]
[Outputs]
file_base = bw02
sync_times = '0.5 2 8'
[exodus]
type = Exodus
sync_only = true
[]
[along_line]
type = CSV
sync_only = true
[]
[]
(modules/combined/test/tests/heat_conduction_xfem/heat.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 6
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[XFEM]
geometric_cut_userobjects = 'line_seg_cut_uo'
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.5 1.0 0.5 0.5'
time_start_cut = 0.0
time_end_cut = 0.0
[../]
[]
[Variables]
[./temp]
initial_condition = 300.0 # set initial temp to ambient
[../]
[]
[Functions]
[./temp_left]
type = PiecewiseLinear
x = '0 2'
y = '0 0.1'
[../]
[]
[Kernels]
[./heat] # gradient term in heat conduction equation
type = HeatConduction
variable = temp
[../]
[]
[BCs]
# Define boundary conditions
[./left_temp]
type = FunctionDirichletBC
variable = temp
boundary = 3
function = temp_left
[../]
[./right_temp]
type = DirichletBC
variable = temp
boundary = 1
value = 0
[../]
[]
[Materials]
[./fuel_thermal]
type = HeatConductionMaterial
block = 0
temp = temp
thermal_conductivity = 5.0
specific_heat = 1.0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
l_max_its = 100
l_tol = 8e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 1.0
end_time = 2.0
num_steps = 2
[]
[Outputs]
# Define output file(s)
file_base = heat_out
interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/tensor_mechanics/test/tests/beam/constraints/glued_constraint.i)
# Test for glued beam constraint.
#
# Using a simple L-shaped geometry with a glued constraint at the
# corner between the two beams. The longer beam properties and loading is
# taken from an earlier beam regression test for static loading. The maximum
# applied load of 50000 lb should result in a displacement of 3.537e-3. Since
# the constraint is glued, the y-dir displacement of the long beam is
# 3.537e-3 and the short beam y-dir displacement is the same. The stiffness of
# the short beam is much less than the longer beam and thus should not
# significantly influence the displacement solution.
[Mesh]
file = beam_cons_patch.e
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[./rot_x]
order = FIRST
family = LAGRANGE
[../]
[./rot_y]
order = FIRST
family = LAGRANGE
[../]
[./rot_z]
order = FIRST
family = LAGRANGE
[../]
[]
[BCs]
[./fixx1]
type = DirichletBC
variable = disp_x
boundary = '1001 1003'
value = 0.0
[../]
[./fixy1]
type = DirichletBC
variable = disp_y
boundary = '1001 1003'
value = 0.0
[../]
[./fixz1]
type = DirichletBC
variable = disp_z
boundary = '1001 1003'
value = 0.0
[../]
[./fixr1]
type = DirichletBC
variable = rot_x
boundary = '1001 1003'
value = 0.0
[../]
[./fixr2]
type = DirichletBC
variable = rot_y
boundary = '1001 1003'
value = 0.0
[../]
[./fixr3]
type = DirichletBC
variable = rot_z
boundary = '1001 1003'
value = 0.0
[../]
[]
[Constraints]
[./tie_y_fuel]
type = NodalStickConstraint
penalty = 1.2e14
boundary = 1005
secondary = 1004
variable = disp_y
[../]
[./tie_x_fuel]
type = NodalStickConstraint
penalty = 1.2e14
boundary = 1005
secondary = 1004
variable = disp_x
[../]
[./tie_z_fuel]
type = NodalStickConstraint
penalty = 1.2e14
boundary = 1005
secondary = 1004
variable = disp_z
[../]
[./tie_rot_y_fuel]
type = NodalStickConstraint
penalty = 1.2e14
boundary = 1005
secondary = 1004
variable = rot_y
[../]
[./tie_rot_x_fuel]
type = NodalStickConstraint
penalty = 1.2e14
boundary = 1005
secondary = 1004
variable = rot_x
[../]
[./tie_rot_z_fuel]
type = NodalStickConstraint
penalty = 1.2e14
boundary = 1005
secondary = 1004
variable = rot_z
[../]
[]
[Functions]
[./force_loading]
type = PiecewiseLinear
x = '0.0 5.0'
y = '0.0 50000.0'
[../]
[./disp_y_ramp]
type = PiecewiseLinear
x = '0.0 5.0'
y = '0.0 1e-2'
[../]
[]
[NodalKernels]
[./force_x2]
type = UserForcingFunctionNodalKernel
variable = disp_y
boundary = '1004'
function = force_loading
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
line_search = 'none'
nl_max_its = 15
nl_rel_tol = 1e-6
nl_abs_tol = 1e-8
dt = 1
dtmin = 1
end_time = 5
[]
[Kernels]
[./solid_disp_x]
type = StressDivergenceBeam
block = '1 2'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 0
variable = disp_x
[../]
[./solid_disp_y]
type = StressDivergenceBeam
block = '1 2'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 1
variable = disp_y
[../]
[./solid_disp_z]
type = StressDivergenceBeam
block = '1 2'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 2
variable = disp_z
[../]
[./solid_rot_x]
type = StressDivergenceBeam
block = '1 2'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 3
variable = rot_x
[../]
[./solid_rot_y]
type = StressDivergenceBeam
block = '1 2'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 4
variable = rot_y
[../]
[./solid_rot_z]
type = StressDivergenceBeam
block = '1 2'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
component = 5
variable = rot_z
[../]
[]
[Materials]
[./elasticity_pipe]
type = ComputeElasticityBeam
shear_coefficient = 1.0
youngs_modulus = 30e6
poissons_ratio = 0.3
block = 1
outputs = exodus
output_properties = 'material_stiffness material_flexure'
[../]
[./strain_pipe]
type = ComputeIncrementalBeamStrain
block = '1'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
area = 28.274
Ay = 0.0
Az = 0.0
Iy = 1.0
Iz = 1.0
y_orientation = '0.0 0.0 1.0'
[../]
[./stress_pipe]
type = ComputeBeamResultants
block = 1
outputs = exodus
output_properties = 'forces moments'
[../]
[./elasticity_cons]
type = ComputeElasticityBeam
shear_coefficient = 1.0
youngs_modulus = 10e2
poissons_ratio = 0.3
block = 2
outputs = exodus
output_properties = 'material_stiffness material_flexure'
[../]
[./strain_cons]
type = ComputeIncrementalBeamStrain
block = '2'
displacements = 'disp_x disp_y disp_z'
rotations = 'rot_x rot_y rot_z'
area = 1.0
Ay = 0.0
Az = 0.0
Iy = 1.0
Iz = 1.0
y_orientation = '0.0 0.0 1.0'
[../]
[./stress_cons]
type = ComputeBeamResultants
block = 2
outputs = exodus
output_properties = 'forces moments'
[../]
[]
[Postprocessors]
[./disp_y_n4]
type = NodalVariableValue
variable = disp_y
nodeid = 3
[../]
[./disp_y_n2]
type = NodalVariableValue
variable = disp_y
nodeid = 1
[../]
[./forces_y]
type = PointValue
point = '10.0 59.9 0.0'
variable = forces_y
[../]
[]
[Outputs]
csv = true
exodus = true
[]
(test/tests/time_steppers/iteration_adaptive/adapt_tstep_pps_lim.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 50
ny = 2
xmax = 5
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
[./timestep_fn]
type = PiecewiseLinear
x = '0. 40.'
y = '10. 1. '
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./dt]
type = TimeDerivative
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 10
[../]
[./right]
type = NeumannBC
variable = u
boundary = right
value = -1
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
start_time = 0.0
end_time = 40.0
n_startup_steps = 2
dtmax = 6.0
[./TimeStepper]
type = IterationAdaptiveDT
optimal_iterations = 10
timestep_limiting_postprocessor = timestep_pp
dt = 1.0
[../]
[]
[Postprocessors]
[./_dt]
type = TimestepSize
[../]
# Just use a simple postprocessor to test capability to limit the time step length to the postprocessor value
[./timestep_pp]
type = FunctionValuePostprocessor
function = timestep_fn
[../]
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
checkpoint = true
[]
(modules/tensor_mechanics/test/tests/smeared_cracking/cracking_rz_exponential.i)
#
# Test to exercise the exponential stress release
#
# Stress vs. strain should show a linear relationship until cracking,
# an exponential stress release, a linear relationship back to zero
# strain, a linear relationship with the original stiffness in
# compression and then back to zero strain, a linear relationship
# back to the exponential curve, and finally further exponential
# stress release.
[Mesh]
file = cracking_rz_test.e
[]
[Problem]
coord_type = RZ
[]
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Functions]
[./disply]
type = PiecewiseLinear
x = '0 1 2 3 4 5 6'
y = '0 0.00175 0 -0.0001 0 0.00175 0.0035'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx'
[../]
[]
[BCs]
[./pully]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = disply
[../]
[./bottom]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.0
[../]
[./sides]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 186.5e9
poissons_ratio = 0.316
[../]
[./elastic_stress]
type = ComputeSmearedCrackingStress
cracking_stress = 119.3e6
softening_models = exponential_softening
[../]
[./exponential_softening]
type = ExponentialSoftening
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type'
petsc_options_value = '101 lu'
line_search = 'none'
l_max_its = 100
l_tol = 1e-5
nl_max_its = 10
nl_rel_tol = 1e-8
nl_abs_tol = 1e-4
start_time = 0.0
end_time = 6.0
dt = 0.005
dtmin = 0.005
[]
[Outputs]
exodus = true
[]
(test/tests/geomsearch/2d_moving_penetration/pl_test3tt.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
file = pl_test3.e
displacements = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./distance]
[../]
[./tangential_distance]
[../]
[./normal_x]
[../]
[./normal_y]
[../]
[./closest_point_x]
[../]
[./closest_point_y]
[../]
[./element_id]
[../]
[./side]
[../]
[]
[Kernels]
[./diff_x]
type = Diffusion
variable = disp_x
[../]
[./diff_y]
type = Diffusion
variable = disp_y
[../]
[]
[AuxKernels]
[./penetrate]
type = PenetrationAux
variable = distance
boundary = 11 #secondary
paired_boundary = 12 #primary
tangential_tolerance = 0.1
[../]
[./penetrate2]
type = PenetrationAux
variable = distance
boundary = 12 #secondary
paired_boundary = 11 #primary
tangential_tolerance = 0.1
[../]
[./penetrate3]
type = PenetrationAux
variable = tangential_distance
boundary = 11
paired_boundary = 12
quantity = tangential_distance
[../]
[./penetrate4]
type = PenetrationAux
variable = tangential_distance
boundary = 12
paired_boundary = 11
quantity = tangential_distance
[../]
[./penetrate5]
type = PenetrationAux
variable = normal_x
boundary = 11
paired_boundary = 12
quantity = normal_x
[../]
[./penetrate6]
type = PenetrationAux
variable = normal_x
boundary = 12
paired_boundary = 11
quantity = normal_x
[../]
[./penetrate7]
type = PenetrationAux
variable = normal_y
boundary = 11
paired_boundary = 12
quantity = normal_y
[../]
[./penetrate8]
type = PenetrationAux
variable = normal_y
boundary = 12
paired_boundary = 11
quantity = normal_y
[../]
[./penetrate9]
type = PenetrationAux
variable = closest_point_x
boundary = 11
paired_boundary = 12
quantity = closest_point_x
[../]
[./penetrate10]
type = PenetrationAux
variable = closest_point_x
boundary = 12
paired_boundary = 11
quantity = closest_point_x
[../]
[./penetrate11]
type = PenetrationAux
variable = closest_point_y
boundary = 11
paired_boundary = 12
quantity = closest_point_y
[../]
[./penetrate12]
type = PenetrationAux
variable = closest_point_y
boundary = 12
paired_boundary = 11
quantity = closest_point_y
[../]
[./penetrate13]
type = PenetrationAux
variable = element_id
boundary = 11
paired_boundary = 12
quantity = element_id
[../]
[./penetrate14]
type = PenetrationAux
variable = element_id
boundary = 12
paired_boundary = 11
quantity = element_id
[../]
[./penetrate15]
type = PenetrationAux
variable = side
boundary = 11
paired_boundary = 12
quantity = side
[../]
[./penetrate16]
type = PenetrationAux
variable = side
boundary = 12
paired_boundary = 11
quantity = side
[../]
[]
[BCs]
[./b1x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0
[../]
[./b1y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0
[../]
[./b2x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0
[../]
[./b2y]
type = FunctionDirichletBC
variable = disp_y
boundary = 2
function = disp_y
[../]
[]
[Functions]
[./disp_y]
type = PiecewiseLinear
x = '0.0 0.25 0.75 1.0'
y = '0.0 2.0 -2.0 0.0'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
nl_rel_tol = 1e-10
l_max_its = 10
start_time = 0.0
dt = 0.0125
end_time = 1.0
[]
[Outputs]
file_base = pl_test3tt_out
exodus = true
[]
(test/tests/time_steppers/iteration_adaptive/multi_piecewise_linear.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 50
ny = 2
xmax = 5
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
[./temp_spike1]
type = PiecewiseLinear
x = '1 3 5'
y = '1 4 4'
[../]
[./temp_spike2]
type = PiecewiseLinear
x = '0 2 4'
y = '1 1 2'
[../]
[temp_spike]
type = ParsedFunction
value = 'temp_spike1 + temp_spike2'
vars = 'temp_spike1 temp_spike2'
vals = 'temp_spike1 temp_spike2'
[]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./dt]
type = TimeDerivative
variable = u
[../]
[]
[BCs]
[./left]
type = FunctionDirichletBC
variable = u
boundary = left
function = temp_spike
[../]
[./right]
type = NeumannBC
variable = u
boundary = right
value = -1
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
start_time = 0
end_time = 5
verbose = true
[./TimeStepper]
type = IterationAdaptiveDT
dt = 10
optimal_iterations = 10
timestep_limiting_function = 'temp_spike1 temp_spike2'
[../]
[]
[Postprocessors]
[./dt]
type = TimestepSize
[../]
[]
[Outputs]
csv = true
[]