- boundaryThe list of boundary IDs from the mesh where this object applies
C++ Type:std::vector<BoundaryName>
Controllable:No
Description:The list of boundary IDs from the mesh where this object applies
- functorThe functor for this boundary condition. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number.
C++ Type:MooseFunctorName
Unit:(no unit assumed)
Controllable:No
Description:The functor for this boundary condition. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number.
- variableThe name of the variable that this boundary condition applies to
C++ Type:LinearVariableName
Unit:(no unit assumed)
Controllable:No
Description:The name of the variable that this boundary condition applies to
LinearFVAdvectionDiffusionFunctorDirichletBC
Description
LinearFVAdvectionDiffusionFunctorDirichletBC will specify the value of a field at the boundary. The value will be determined by a Functor (through the "functor" parameter).
commentnote
This boundary condition should only be used for problems which involve advection and/or diffusion problems.
Example Syntax
In this example the functor is defined using a ParsedFunction.
[LinearFVBCs<<<{"href": "../../syntax/LinearFVBCs/index.html"}>>>]
[dir]
type = LinearFVAdvectionDiffusionFunctorDirichletBC<<<{"description": "Adds a dirichlet BC which can be used for the assembly of linear finite volume system and whose face values are determined using a functor. This kernel is only designed to work with advection-diffusion problems.", "href": "LinearFVAdvectionDiffusionFunctorDirichletBC.html"}>>>
variable<<<{"description": "The name of the variable that this boundary condition applies to"}>>> = u
boundary<<<{"description": "The list of boundary IDs from the mesh where this object applies"}>>> = "left right top bottom"
functor<<<{"description": "The functor for this boundary condition. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number."}>>> = analytic_solution
[]
[]Input Parameters
- matrix_onlyFalseWhether this object is only doing assembly to matrices (no vectors)
Default:False
C++ Type:bool
Controllable:No
Description:Whether this object is only doing assembly to matrices (no vectors)
Optional Parameters
- absolute_value_vector_tagsThe tags for the vectors this residual object should fill with the absolute value of the residual contribution
C++ Type:std::vector<TagName>
Controllable:No
Description:The tags for the vectors this residual object should fill with the absolute value of the residual contribution
- extra_matrix_tagsThe extra tags for the matrices this Kernel should fill
C++ Type:std::vector<TagName>
Controllable:No
Description:The extra tags for the matrices this Kernel should fill
- extra_vector_tagsThe extra tags for the vectors this Kernel should fill
C++ Type:std::vector<TagName>
Controllable:No
Description:The extra tags for the vectors this Kernel should fill
- matrix_tagssystemThe tag for the matrices this Kernel should fill
Default:system
C++ Type:MultiMooseEnum
Options:nontime, system
Controllable:No
Description:The tag for the matrices this Kernel should fill
- vector_tagsrhsThe tag for the vectors this Kernel should fill
Default:rhs
C++ Type:MultiMooseEnum
Options:rhs, time
Controllable:No
Description:The tag for the vectors this Kernel should fill
Contribution To Tagged Field Data Parameters
- control_tagsAdds user-defined labels for accessing object parameters via control logic.
C++ Type:std::vector<std::string>
Controllable:No
Description:Adds user-defined labels for accessing object parameters via control logic.
- enableTrueSet the enabled status of the MooseObject.
Default:True
C++ Type:bool
Controllable:Yes
Description:Set the enabled status of the MooseObject.
- implicitTrueDetermines whether this object is calculated using an implicit or explicit form
Default:True
C++ Type:bool
Controllable:No
Description:Determines whether this object is calculated using an implicit or explicit form
Advanced Parameters
Input Files
- (modules/navier_stokes/test/tests/postprocessors/flow_rates/conservation_LinearFV.i)
- (test/tests/variables/linearfv/diffusion-1d-aux.i)
- (test/tests/linearfvkernels/diffusion-reaction-advection/advection-diffusion-reaction-1d.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/SIMPLEC/3d/3d-velocity-pressure.i)
- (test/tests/linearfvkernels/diffusion/diffusion-1d_neumann.i)
- (test/tests/linearfvkernels/block-restriction/block-restricted-diffusion.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/linear-segregated/2d/2d-boussinesq-transient.i)
- (modules/navier_stokes/test/tests/finite_volume/wcns/enthalpy_equation/1d_test_h.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/linear-segregated/2d/2d-velocity-pressure.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/linear-segregated/3d/3d-velocity-pressure.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/cht/flow-around-square-linear.i)
- (test/tests/multiapps/linearfv_nonlinearfv/linearfv.i)
- (modules/navier_stokes/test/tests/finite_volume/wcns/enthalpy_equation/enthalpy_equation.i)
- (test/tests/time_integrators/implicit-euler/ie-linearfv.i)
- (test/tests/variables/linearfv/diffusion-1d-pp.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/lid-driven/linear-segregated/lid-driven-segregated.i)
- (test/tests/postprocessors/side_diffusive_flux_integral/side_diffusive_flux_integral_linear_fv.i)
- (test/tests/linearfvkernels/diffusion/diffusion-1d.i)
- (test/tests/linearfvkernels/diffusion-reaction-advection/advection-diffusion-reaction-2d.i)
- (test/tests/transfers/multiapp_copy_transfer/linear_sys_to_aux/linear_sub.i)
- (test/tests/linearfvkernels/block-restriction/block-restricted-diffusion-react.i)
- (test/tests/linearfvkernels/diffusion/diffusion-2d_neumann.i)
- (test/tests/time_steppers/iteration_adaptive/adapt_linear_systems.i)
- (test/tests/linearfvkernels/diffusion/diffusion-2d.i)
- (modules/navier_stokes/test/tests/finite_volume/wcns/enthalpy_equation/1d_test_h_fp.i)
- (test/tests/linearfvkernels/advection/advection-2d.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/SIMPLEC/2d/2d-velocity-pressure.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/linear-segregated/steady-transient-compare/common-blocks.i)
- (test/tests/linearfvkernels/advection/advection-2d-rz.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/natural_convection/linear_segregated/2d/diff_heated_cavity_linear_segregated.i)
- (test/tests/linearfvkernels/block-restriction/block-restricted-adr.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/cht/flow-around-square-linear-fluidonly.i)
- (modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/segregated/channel-drift-flux.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/linear-segregated/2d/2d-boussinesq.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/linear-segregated/2d-heated/fluid.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/segregated-comparison/segregated-linear.i)
- (test/tests/linearfvkernels/anisotropic-diffusion/anisotropic-diffusion-2d.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/linear-segregated/2d-scalar/channel.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/mms/linear-segregated/2d-vortex/2d-vortex.i)
- (modules/navier_stokes/examples/flow-over-circle/flow_over_circle_linearfv.i)
- (test/tests/linearfvkernels/diffusion/diffusion-2d-rz.i)
- (test/tests/linearfvkernels/advection/advection-1d.i)
- (test/tests/outputs/debug/show_execution_linear_fv_flux.i)
- (test/tests/multisystem/picard/linearfv_nonlinearfv/same_input.i)
- (test/tests/tag/tag-linearfv.i)
- (modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/segregated/rayleigh-bernard-two-phase-physics.i)
- (modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/segregated/lid-driven-two-phase-physics.i)
functor
C++ Type:MooseFunctorName
Unit:(no unit assumed)
Controllable:No
Description:The functor for this boundary condition. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number.
(test/tests/linearfvkernels/diffusion/diffusion-2d.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 1
ymax = 0.5
[]
[]
[Problem]
linear_sys_names = 'u_sys'
[]
[Variables]
[u]
type = MooseLinearVariableFVReal
solver_sys = 'u_sys'
initial_condition = 1.0
[]
[]
[LinearFVKernels]
[diffusion]
type = LinearFVDiffusion
variable = u
diffusion_coeff = coeff_func
use_nonorthogonal_correction = false
[]
[source]
type = LinearFVSource
variable = u
source_density = source_func
[]
[]
[LinearFVBCs]
[dir]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = u
boundary = "left right top bottom"
functor = analytic_solution
[]
[]
[Functions]
[coeff_func]
type = ParsedFunction
expression = '1+0.5*x*y'
[]
[source_func]
type = ParsedFunction
expression = '2*(1.5-y*y)+2*x*y*(1.5-y*y)+2*(1.5-x*x)+2*x*y*(1.5-x*x)'
[]
[analytic_solution]
type = ParsedFunction
expression = '(1.5-x*x)*(1.5-y*y)'
[]
[]
[Postprocessors]
[h]
type = AverageElementSize
execute_on = FINAL
[]
[error]
type = ElementL2FunctorError
approximate = u
exact = analytic_solution
execute_on = FINAL
[]
[]
[Convergence]
[linear]
type = IterationCountConvergence
max_iterations = 1
converge_at_max_iterations = true
[]
[]
[Executioner]
type = Steady
system_names = u_sys
l_tol = 1e-10
multi_system_fixed_point=true
multi_system_fixed_point_convergence=linear
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
[csv]
type = CSV
execute_on = FINAL
[]
[]
(modules/navier_stokes/test/tests/postprocessors/flow_rates/conservation_LinearFV.i)
mu = 2.6
rho = 1.1
advected_interp_method='average'
[UserObjects]
[rc]
type = RhieChowMassFlux
u = vel_x
v = vel_y
pressure = pressure
rho = ${rho}
p_diffusion_kernel = p_diffusion
[]
[]
[Mesh]
[mesh]
type = CartesianMeshGenerator
dim = 2
dx = '0.3'
dy = '0.3'
ix = '3'
iy = '3'
[]
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system'
previous_nl_solution_required = true
[]
[Variables]
[vel_x]
type = MooseLinearVariableFVReal
initial_condition = 0.5
solver_sys = u_system
[]
[vel_y]
type = MooseLinearVariableFVReal
solver_sys = v_system
initial_condition = 0.0
[]
[pressure]
type = MooseLinearVariableFVReal
solver_sys = pressure_system
initial_condition = 0.2
[]
[]
[LinearFVKernels]
[u_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_x
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'x'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[v_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_y
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'y'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[u_pressure]
type = LinearFVMomentumPressure
variable = vel_x
pressure = pressure
momentum_component = 'x'
[]
[v_pressure]
type = LinearFVMomentumPressure
variable = vel_y
pressure = pressure
momentum_component = 'y'
[]
[p_diffusion]
type = LinearFVAnisotropicDiffusion
variable = pressure
diffusion_tensor = Ainv
use_nonorthogonal_correction = false
[]
[HbyA_divergence]
type = LinearFVDivergence
variable = pressure
face_flux = HbyA
force_boundary_execution = true
[]
[]
[LinearFVBCs]
[inlet-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_x
functor = '1.1'
[]
[inlet-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_y
functor = '0.0'
[]
[walls-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom'
variable = vel_x
functor = 0.0
[]
[walls-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom'
variable = vel_y
functor = 0.0
[]
[outlet_p]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'right'
variable = pressure
functor = 1.4
[]
[outlet_u]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_x
use_two_term_expansion = false
boundary = right
[]
[outlet_v]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_y
use_two_term_expansion = false
boundary = right
[]
[]
[Executioner]
type = SIMPLE
momentum_l_abs_tol = 1e-10
pressure_l_abs_tol = 1e-10
momentum_l_tol = 0
pressure_l_tol = 0
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
momentum_equation_relaxation = 0.8
pressure_variable_relaxation = 0.3
num_iterations = 100
pressure_absolute_tolerance = 1e-10
momentum_absolute_tolerance = 1e-10
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
print_fields = false
[]
[Postprocessors]
[inlet_mass]
type = VolumetricFlowRate
boundary = left
rhie_chow_user_object = rc
advected_quantity = ${rho}
vel_x = vel_x
vel_y = vel_y
subtract_mesh_velocity = false
[]
[outlet_mass]
type = VolumetricFlowRate
boundary = right
rhie_chow_user_object = rc
advected_quantity = ${rho}
vel_x = vel_x
vel_y = vel_y
subtract_mesh_velocity = false
[]
[]
[Outputs]
csv = true
[]
(test/tests/variables/linearfv/diffusion-1d-aux.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
nx = 10
[]
[]
[Problem]
linear_sys_names = 'u_sys'
[]
[Variables]
[u]
type = MooseLinearVariableFVReal
solver_sys = 'u_sys'
initial_condition = 1.0
[]
[]
[AuxVariables]
[v_volume]
type = MooseLinearVariableFVReal
initial_condition = 50
[]
[v_functor]
type = MooseLinearVariableFVReal
initial_condition = 25
[]
[v_parsed]
type = MooseLinearVariableFVReal
initial_condition = 12.5
[]
[]
[AuxKernels]
[volume]
type = VolumeAux
variable = v_volume
[]
[functor]
type = FunctorAux
variable = v_functor
functor = u
[]
[parsed]
type = ParsedAux
variable = v_parsed
coupled_variables = 'v_volume v_functor'
expression = '0.5*v_volume+0.5*v_functor'
[]
[]
[LinearFVKernels]
[diffusion]
type = LinearFVDiffusion
variable = u
diffusion_coeff = coeff_func
[]
[source]
type = LinearFVSource
variable = u
source_density = source_func
[]
[]
[LinearFVBCs]
[dir]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = u
boundary = "left right"
functor = analytic_solution
[]
[]
[Functions]
[coeff_func]
type = ParsedFunction
expression = '0.5*x'
[]
[source_func]
type = ParsedFunction
expression = '2*x'
[]
[analytic_solution]
type = ParsedFunction
expression = '1-x*x'
[]
[]
[Executioner]
type = Steady
system_names = u_sys
l_tol = 1e-10
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
execute_on = TIMESTEP_END
[]
(test/tests/linearfvkernels/diffusion-reaction-advection/advection-diffusion-reaction-1d.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
nx = 2
[]
[]
[Problem]
linear_sys_names = 'u_sys'
[]
[Variables]
[u]
type = MooseLinearVariableFVReal
solver_sys = 'u_sys'
initial_condition = 1.0
[]
[]
[LinearFVKernels]
[diffusion]
type = LinearFVDiffusion
variable = u
diffusion_coeff = diff_coeff_func
use_nonorthogonal_correction = false
[]
[advection]
type = LinearFVAdvection
variable = u
velocity = "0.5 0 0"
advected_interp_method = average
[]
[reaction]
type = LinearFVReaction
variable = u
coeff = coeff_func
[]
[source]
type = LinearFVSource
variable = u
source_density = source_func
[]
[]
[LinearFVBCs]
inactive = "outflow neumann"
[dir]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = u
boundary = "left right"
functor = analytic_solution
[]
[outflow]
type = LinearFVAdvectionDiffusionOutflowBC
variable = u
boundary = "right"
use_two_term_expansion = true
[]
[neumann]
type = LinearFVAdvectionDiffusionFunctorNeumannBC
variable = u
boundary = "left"
functor = analytic_solution_neumann_left
diffusion_coeff = diff_coeff_func
[]
[]
[Functions]
[diff_coeff_func]
type = ParsedFunction
expression = '1+0.5*x'
[]
[coeff_func]
type = ParsedFunction
expression = '1+1/(1+x)'
[]
[source_func]
type = ParsedFunction
expression = '(1+1/(x+1))*(sin(pi/2*x)+1.5)+0.25*pi*pi*(0.5*x+1)*sin(pi/2*x)'
[]
[analytic_solution]
type = ParsedFunction
expression = 'sin(pi/2*x)+1.5'
[]
[analytic_solution_neumann_left]
type = ParsedFunction
expression = '-(1+0.5*x)*cos(pi/2*x)*pi/2'
[]
[]
[Postprocessors]
[h]
type = AverageElementSize
execute_on = FINAL
[]
[error]
type = ElementL2FunctorError
approximate = u
exact = analytic_solution
execute_on = FINAL
[]
[]
[Convergence]
[linear]
type = IterationCountConvergence
max_iterations = 1
converge_at_max_iterations = true
[]
[]
[Executioner]
type = Steady
system_names = u_sys
multi_system_fixed_point=true
multi_system_fixed_point_convergence=linear
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_rtol'
petsc_options_value = 'hypre boomeramg 1e-10'
[]
[Outputs]
[csv]
type = CSV
execute_on = FINAL
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/SIMPLEC/3d/3d-velocity-pressure.i)
mu = 2.6
rho = 1.0
advected_interp_method = 'average'
[Mesh]
[mesh]
type = CartesianMeshGenerator
dim = 3
dx = '1.0'
dy = '0.3'
dz = '0.3'
ix = '10'
iy = '3'
iz = '3'
[]
[]
[Problem]
linear_sys_names = 'u_system v_system w_system pressure_system'
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = RhieChowMassFlux
u = vel_x
v = vel_y
w = vel_z
pressure = pressure
rho = ${rho}
p_diffusion_kernel = p_diffusion
pressure_projection_method = consistent
[]
[]
[Variables]
[vel_x]
type = MooseLinearVariableFVReal
initial_condition = 0.5
solver_sys = u_system
[]
[vel_y]
type = MooseLinearVariableFVReal
solver_sys = v_system
initial_condition = 0.0
[]
[vel_z]
type = MooseLinearVariableFVReal
solver_sys = w_system
initial_condition = 0.0
[]
[pressure]
type = MooseLinearVariableFVReal
solver_sys = pressure_system
initial_condition = 0.2
[]
[]
[LinearFVKernels]
[u_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_x
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
w = vel_z
momentum_component = 'x'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[v_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_y
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
w = vel_z
momentum_component = 'y'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[w_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_z
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
w = vel_z
momentum_component = 'z'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[u_pressure]
type = LinearFVMomentumPressure
variable = vel_x
pressure = pressure
momentum_component = 'x'
[]
[v_pressure]
type = LinearFVMomentumPressure
variable = vel_y
pressure = pressure
momentum_component = 'y'
[]
[w_pressure]
type = LinearFVMomentumPressure
variable = vel_z
pressure = pressure
momentum_component = 'z'
[]
[p_diffusion]
type = LinearFVAnisotropicDiffusion
variable = pressure
diffusion_tensor = Ainv
use_nonorthogonal_correction = false
[]
[HbyA_divergence]
type = LinearFVDivergence
variable = pressure
face_flux = HbyA
force_boundary_execution = true
[]
[]
[LinearFVBCs]
[inlet-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_x
functor = '1.1'
[]
[inlet-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_y
functor = '0.0'
[]
[inlet-w]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_z
functor = '0.0'
[]
[walls-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom back front'
variable = vel_x
functor = 0.0
[]
[walls-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom back front'
variable = vel_y
functor = 0.0
[]
[walls-w]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom back front'
variable = vel_z
functor = 0.0
[]
[outlet_p]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'right'
variable = pressure
functor = 1.4
[]
[outlet_u]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_x
use_two_term_expansion = false
boundary = right
[]
[outlet_v]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_y
use_two_term_expansion = false
boundary = right
[]
[outlet_w]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_z
use_two_term_expansion = false
boundary = right
[]
[]
[Executioner]
type = SIMPLE
momentum_l_abs_tol = 1e-10
pressure_l_abs_tol = 1e-10
momentum_l_tol = 0
pressure_l_tol = 0
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system w_system'
pressure_system = 'pressure_system'
momentum_equation_relaxation = 0.8
pressure_variable_relaxation = 1.0
num_iterations = 100
pressure_absolute_tolerance = 1e-10
momentum_absolute_tolerance = 1e-10
momentum_petsc_options_iname = '-pc_type -pc_hypre_type -pc_hypre_boomeramg_agg_nl -pc_hypre_boomeramg_agg_num_paths -pc_hypre_boomeramg_truncfactor -pc_hypre_boomeramg_strong_threshold -pc_hypre_boomeramg_coarsen_type -pc_hypre_boomeramg_interp_type'
momentum_petsc_options_value = 'hypre boomeramg 4 1 0.1 0.6 HMIS ext+i'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type -pc_hypre_boomeramg_agg_nl -pc_hypre_boomeramg_agg_num_paths -pc_hypre_boomeramg_truncfactor -pc_hypre_boomeramg_strong_threshold -pc_hypre_boomeramg_coarsen_type -pc_hypre_boomeramg_interp_type'
pressure_petsc_options_value = 'hypre boomeramg 2 1 0.1 0.6 HMIS ext+i'
print_fields = false
[]
[Outputs]
exodus = true
[]
(test/tests/linearfvkernels/diffusion/diffusion-1d_neumann.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
nx = 2
[]
[]
[Problem]
linear_sys_names = 'u_sys'
[]
[Variables]
[u]
type = MooseLinearVariableFVReal
solver_sys = 'u_sys'
initial_condition = 1.0
[]
[]
[LinearFVKernels]
[diffusion]
type = LinearFVDiffusion
variable = u
diffusion_coeff = coeff_func
[]
[source]
type = LinearFVSource
variable = u
source_density = source_func
[]
[]
[LinearFVBCs]
[dir]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = u
boundary = "right"
functor = analytic_solution
[]
[neu]
type = LinearFVAdvectionDiffusionFunctorNeumannBC
variable = u
boundary = "left"
functor = analytic_solution_neumann
[]
[]
[Functions]
[coeff_func]
type = ParsedFunction
expression = '0.5*x'
[]
[source_func]
type = ParsedFunction
expression = '2*x'
[]
[analytic_solution]
type = ParsedFunction
expression = '1-x*x'
[]
[analytic_solution_neumann]
type = ParsedFunction
expression = '-(0.5*x)*(-2*x)'
[]
[]
[Postprocessors]
[h]
type = AverageElementSize
execute_on = FINAL
[]
[error]
type = ElementL2FunctorError
approximate = u
exact = analytic_solution
execute_on = FINAL
[]
[]
[Executioner]
type = Steady
system_names = u_sys
l_tol = 1e-10
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
[csv]
type = CSV
execute_on = FINAL
[]
[]
(test/tests/linearfvkernels/block-restriction/block-restricted-diffusion.i)
[Mesh]
[cmg]
type = CartesianMeshGenerator
dim = 2
dx = '0.1 1 0.1'
dy = '0.1 0.5 0.1'
ix = '1 2 1'
iy = '1 1 1'
subdomain_id = '1 1 1 1 2 3 1 1 1'
[]
[transform]
type = TransformGenerator
input = cmg
transform = TRANSLATE
vector_value = '-0.1 -0.1 0.0'
[]
[create_sides]
type = SideSetsBetweenSubdomainsGenerator
input = transform
new_boundary = sides
primary_block = 2
paired_block = 1
[]
[create_outlet]
type = SideSetsBetweenSubdomainsGenerator
input = create_sides
new_boundary = outlet
primary_block = 2
paired_block = 3
[]
[]
[Problem]
linear_sys_names = 'u_sys'
[]
[Variables]
[u]
type = MooseLinearVariableFVReal
solver_sys = 'u_sys'
initial_condition = 1.0
block = 2
[]
[]
[LinearFVKernels]
[diffusion]
type = LinearFVDiffusion
variable = u
diffusion_coeff = diff_coeff_func
use_nonorthogonal_correction = false
[]
[source]
type = LinearFVSource
variable = u
source_density = source_func
[]
[]
[LinearFVBCs]
[dir]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = u
boundary = "sides outlet"
functor = analytic_solution
[]
[]
[Functions]
[diff_coeff_func]
type = ParsedFunction
expression = '1.0+0.5*x*y'
[]
[source_func]
type = ParsedFunction
expression = '-1.0*x*pi*sin(x*pi)*cos(2*y*pi) - 0.5*y*pi*sin(2*y*pi)*cos(x*pi) + 5*pi^2*(0.5*x*y + 1.0)*sin(x*pi)*sin(2*y*pi)'
[]
[analytic_solution]
type = ParsedFunction
expression = 'sin(x*pi)*sin(2*y*pi) + 1.5'
[]
[]
[Postprocessors]
[h]
type = AverageElementSize
execute_on = FINAL
block = 2
[]
[error]
type = ElementL2FunctorError
approximate = u
exact = analytic_solution
execute_on = FINAL
block = 2
[]
[]
[Convergence]
[linear]
type = IterationCountConvergence
max_iterations = 1
converge_at_max_iterations = true
[]
[]
[Executioner]
type = Steady
system_names = u_sys
l_tol = 1e-10
multi_system_fixed_point=true
multi_system_fixed_point_convergence=linear
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
[csv]
type = CSV
execute_on = FINAL
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/linear-segregated/2d/2d-boussinesq-transient.i)
mu = 2.6
rho = 1.0
advected_interp_method = 'average'
cp = 300
k = 10
alpha_b = 1e-4
[Mesh]
[mesh]
type = CartesianMeshGenerator
dim = 2
dx = '1.'
dy = '0.2'
ix = '10'
iy = '5'
[]
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system energy_system'
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = RhieChowMassFlux
u = vel_x
v = vel_y
pressure = pressure
rho = ${rho}
p_diffusion_kernel = p_diffusion
[]
[]
[Variables]
[vel_x]
type = MooseLinearVariableFVReal
initial_condition = 0.5
solver_sys = u_system
[]
[vel_y]
type = MooseLinearVariableFVReal
solver_sys = v_system
initial_condition = 0.0
[]
[pressure]
type = MooseLinearVariableFVReal
solver_sys = pressure_system
initial_condition = 0.2
[]
[T]
type = MooseLinearVariableFVReal
solver_sys = energy_system
initial_condition = 300
[]
[]
[LinearFVKernels]
[u_time]
type = LinearFVTimeDerivative
variable = vel_x
factor = ${rho}
[]
[v_time]
type = LinearFVTimeDerivative
variable = vel_y
factor = ${rho}
[]
[u_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_x
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'x'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[v_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_y
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'y'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[u_pressure]
type = LinearFVMomentumPressure
variable = vel_x
pressure = pressure
momentum_component = 'x'
[]
[v_pressure]
type = LinearFVMomentumPressure
variable = vel_y
pressure = pressure
momentum_component = 'y'
[]
[u_boussinesq]
type = LinearFVMomentumBoussinesq
variable = vel_x
rho = ${rho}
gravity = '0 -9.81 0'
alpha_name = ${alpha_b}
ref_temperature = 300.0
T_fluid = T
momentum_component = 'x'
[]
[v_boussinesq]
type = LinearFVMomentumBoussinesq
variable = vel_y
rho = ${rho}
gravity = '0 -9.81 0'
alpha_name = ${alpha_b}
ref_temperature = 300.0
T_fluid = T
momentum_component = 'y'
[]
[p_diffusion]
type = LinearFVAnisotropicDiffusion
variable = pressure
diffusion_tensor = Ainv
use_nonorthogonal_correction = false
[]
[HbyA_divergence]
type = LinearFVDivergence
variable = pressure
face_flux = HbyA
force_boundary_execution = true
[]
[h_time]
type = LinearFVTimeDerivative
variable = T
factor = ${fparse rho*cp}
[]
[h_advection]
type = LinearFVEnergyAdvection
variable = T
advected_quantity = temperature
cp = ${cp}
advected_interp_method = ${advected_interp_method}
rhie_chow_user_object = 'rc'
[]
[conduction]
type = LinearFVDiffusion
variable = T
diffusion_coeff = ${k}
use_nonorthogonal_correction = false
[]
[]
[FunctorMaterials]
[constant_functors]
type = GenericFunctorMaterial
prop_names = 'cp alpha_b'
prop_values = '${cp} ${alpha_b}'
[]
[]
[LinearFVBCs]
[inlet-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_x
functor = '1.1'
[]
[inlet-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_y
functor = '0.0'
[]
[walls-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom'
variable = vel_x
functor = 0.0
[]
[walls-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom'
variable = vel_y
functor = 0.0
[]
[outlet_p]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'right'
variable = pressure
functor = 1.4
[]
[outlet_u]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_x
use_two_term_expansion = false
boundary = right
[]
[outlet_v]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_y
use_two_term_expansion = false
boundary = right
[]
[inlet_top_T]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = T
functor = 300.0
boundary = 'left top'
[]
[bottom_T]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = T
functor = wall-temperature
boundary = bottom
[]
[outlet_T]
type = LinearFVAdvectionDiffusionOutflowBC
variable = T
use_two_term_expansion = false
boundary = right
[]
[]
[Functions]
[wall-temperature]
type = ParsedFunction
expression = '350 + 50 * sin(6.28*t)'
[]
[]
[Executioner]
type = PIMPLE
momentum_l_abs_tol = 1e-12
pressure_l_abs_tol = 1e-12
energy_l_abs_tol = 1e-12
momentum_l_tol = 1e-12
pressure_l_tol = 1e-12
energy_l_tol = 1e-12
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
energy_system = 'energy_system'
momentum_equation_relaxation = 0.8
pressure_variable_relaxation = 0.3
energy_equation_relaxation = 0.9
num_iterations = 100
pressure_absolute_tolerance = 1e-11
momentum_absolute_tolerance = 1e-11
energy_absolute_tolerance = 1e-11
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
energy_petsc_options_iname = '-pc_type -pc_hypre_type'
energy_petsc_options_value = 'hypre boomeramg'
print_fields = false
continue_on_max_its = true
dt = 0.01
num_steps = 6
num_piso_iterations = 0
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/wcns/enthalpy_equation/1d_test_h.i)
L = 30
nx = 600
bulk_u = 0.01
q_source = 50000.
A_cp = 976.78
B_cp = 1.0634
T_in = 860.
p_ref = 101325.0
rho = 2000.
advected_interp_method = 'upwind'
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
xmin = 0
xmax = ${L}
nx = ${nx}
[]
allow_renumbering = false
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
advected_interp_method = ${advected_interp_method}
u = vel_x
[]
[Problem]
linear_sys_names = 'u_system pressure_system energy_system'
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = RhieChowMassFlux
u = vel_x
pressure = pressure
rho = 'rho'
p_diffusion_kernel = p_diffusion
[]
[]
[Variables]
[vel_x]
type = MooseLinearVariableFVReal
solver_sys = u_system
initial_condition = ${bulk_u}
[]
[pressure]
type = MooseLinearVariableFVReal
solver_sys = pressure_system
initial_condition = ${p_ref}
[]
[h]
type = MooseLinearVariableFVReal
solver_sys = energy_system
initial_condition = ${fparse 860.*1900.}
[]
[]
[AuxVariables]
[rho_var]
type = MooseLinearVariableFVReal
[]
[cp_var]
type = MooseLinearVariableFVReal
[]
[mu_var]
type = MooseLinearVariableFVReal
[]
[k_var]
type = MooseLinearVariableFVReal
[]
[alpha_var]
type = MooseLinearVariableFVReal
[]
[T]
type = MooseLinearVariableFVReal
initial_condition = 860.
[]
[h_aux]
type = MooseLinearVariableFVReal
[]
[]
[LinearFVKernels]
[u_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_x
mu = 'mu'
momentum_component = 'x'
use_nonorthogonal_correction = false
[]
[u_pressure]
type = LinearFVMomentumPressure
variable = vel_x
pressure = pressure
momentum_component = 'x'
[]
[p_diffusion]
type = LinearFVAnisotropicDiffusion
variable = pressure
diffusion_tensor = Ainv
use_nonorthogonal_correction = false
[]
[HbyA_divergence]
type = LinearFVDivergence
variable = pressure
face_flux = HbyA
force_boundary_execution = true
[]
[temp_advection]
type = LinearFVEnergyAdvection
variable = h
[]
[source]
type = LinearFVSource
variable = h
source_density = source_func
[]
[]
[LinearFVBCs]
[inlet_u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_x
functor = ${bulk_u} #${bulk_u} #'fully_developed_velocity'
[]
[inlet_h]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = h
boundary = 'left'
functor = 'h_from_p_T'
[]
[inlet_T]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = T
boundary = 'left'
functor = ${T_in}
[]
[outlet_p]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'right'
variable = pressure
functor = ${p_ref}
[]
[outlet_h]
type = LinearFVAdvectionDiffusionOutflowBC
variable = h
use_two_term_expansion = false
boundary = 'right'
[]
[outlet_u]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_x
use_two_term_expansion = false
boundary = 'right'
[]
[]
[Functions]
[source_func]
type = ParsedFunction
expression = ${q_source}
[]
[T_analytical]
type = ParsedFunction
expression = ${fparse (-A_cp+sqrt(A_cp^2-2*B_cp*(-q_source/rho/bulk_u*L-A_cp*T_in-B_cp/2*T_in*T_in)))/B_cp}
[]
[]
[FunctorMaterials]
[enthalpy_material]
type = LinearFVEnthalpyFunctorMaterial
pressure = ${p_ref}
T_fluid = T
h = h
h_from_p_T_functor = h_from_p_T_functor
T_from_p_h_functor = T_from_p_h_functor
[]
[h_from_p_T_functor]
type = ParsedFunctorMaterial
property_name = 'h_from_p_T_functor'
functor_names = 'T'
expression = '${A_cp}*T+${B_cp}/2*(T^2)'
[]
[T_from_p_h_functor]
type = ParsedFunctorMaterial
property_name = 'T_from_p_h_functor'
functor_names = 'h'
expression = '(-${A_cp}+sqrt(${A_cp}^2+2*h*${B_cp}))/${B_cp}'
[]
[rho]
type = ADParsedFunctorMaterial
property_name = 'rho'
functor_names = 'T'
expression = ${rho}
[]
[cp]
type = ADParsedFunctorMaterial
property_name = 'cp'
functor_names = 'T'
expression = '${A_cp}+${B_cp}*T'
[]
[mu]
type = ADParsedFunctorMaterial
property_name = 'mu'
functor_names = 'T'
expression = '4.5e-3'
[]
[k]
type = ADParsedFunctorMaterial
property_name = 'k'
functor_names = 'T'
expression = 0.7
[]
[]
[AuxKernels]
[rho_out]
type = FunctorAux
functor = 'rho'
variable = 'rho_var'
execute_on = 'NONLINEAR'
[]
[cp_out]
type = FunctorAux
functor = 'cp'
variable = 'cp_var'
execute_on = 'NONLINEAR'
[]
[mu_out]
type = FunctorAux
functor = 'mu'
variable = 'mu_var'
execute_on = 'NONLINEAR'
[]
[k_out]
type = FunctorAux
functor = 'k'
variable = 'k_var'
execute_on = 'NONLINEAR'
[]
[T_from_h_functor_aux]
type = FunctorAux
functor = 'T_from_p_h'
variable = 'T'
execute_on = 'NONLINEAR'
[]
[h_from_T_functor_aux]
type = FunctorAux
functor = 'h_from_p_T'
variable = 'h_aux'
execute_on = 'NONLINEAR'
[]
[]
[Postprocessors]
[T_out_sim]
type = ElementalVariableValue
variable = T
elementid = ${fparse nx-1}
[]
[T_out_analytic]
type = FunctionValuePostprocessor
function = T_analytical
[]
[]
[Executioner]
type = SIMPLE
momentum_l_abs_tol = 1e-12
pressure_l_abs_tol = 1e-12
energy_l_abs_tol = 1e-12
momentum_l_tol = 0
pressure_l_tol = 0
energy_l_tol = 0
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system'
pressure_system = 'pressure_system'
energy_system = 'energy_system'
momentum_equation_relaxation = 0.7
pressure_variable_relaxation = 0.3
energy_equation_relaxation = 0.95
num_iterations = 100
pressure_absolute_tolerance = 1e-8
momentum_absolute_tolerance = 1e-8
energy_absolute_tolerance = 1e-6
print_fields = false
momentum_l_max_its = 200
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
energy_petsc_options_iname = '-pc_type -pc_hypre_type'
energy_petsc_options_value = 'hypre boomeramg'
continue_on_max_its = true
[]
[Outputs]
[out]
type = CSV
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/linear-segregated/2d/2d-velocity-pressure.i)
mu = 2.6
rho = 1.0
advected_interp_method = 'average'
[Mesh]
[mesh]
type = CartesianMeshGenerator
dim = 2
dx = '0.3'
dy = '0.3'
ix = '3'
iy = '3'
[]
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system'
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = RhieChowMassFlux
u = vel_x
v = vel_y
pressure = pressure
rho = ${rho}
p_diffusion_kernel = p_diffusion
[]
[]
[Variables]
[vel_x]
type = MooseLinearVariableFVReal
initial_condition = 0.5
solver_sys = u_system
[]
[vel_y]
type = MooseLinearVariableFVReal
solver_sys = v_system
initial_condition = 0.0
[]
[pressure]
type = MooseLinearVariableFVReal
solver_sys = pressure_system
initial_condition = 0.2
[]
[]
[LinearFVKernels]
[u_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_x
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'x'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[v_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_y
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'y'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[u_pressure]
type = LinearFVMomentumPressure
variable = vel_x
pressure = pressure
momentum_component = 'x'
[]
[v_pressure]
type = LinearFVMomentumPressure
variable = vel_y
pressure = pressure
momentum_component = 'y'
[]
[p_diffusion]
type = LinearFVAnisotropicDiffusion
variable = pressure
diffusion_tensor = Ainv
use_nonorthogonal_correction = false
[]
[HbyA_divergence]
type = LinearFVDivergence
variable = pressure
face_flux = HbyA
force_boundary_execution = true
[]
[]
[LinearFVBCs]
[inlet-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_x
functor = '1.1'
[]
[inlet-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_y
functor = '0.0'
[]
[walls-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom'
variable = vel_x
functor = 0.0
[]
[walls-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom'
variable = vel_y
functor = 0.0
[]
[outlet_p]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'right'
variable = pressure
functor = 1.4
[]
[outlet_u]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_x
use_two_term_expansion = false
boundary = right
[]
[outlet_v]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_y
use_two_term_expansion = false
boundary = right
[]
[]
[Executioner]
type = SIMPLE
momentum_l_abs_tol = 1e-10
pressure_l_abs_tol = 1e-10
momentum_l_tol = 0
pressure_l_tol = 0
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
momentum_equation_relaxation = 0.8
pressure_variable_relaxation = 0.3
num_iterations = 100
pressure_absolute_tolerance = 1e-10
momentum_absolute_tolerance = 1e-10
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
print_fields = false
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/linear-segregated/3d/3d-velocity-pressure.i)
mu = 2.6
rho = 1.0
advected_interp_method = 'average'
[Mesh]
[mesh]
type = CartesianMeshGenerator
dim = 3
dx = '0.3'
dy = '0.3'
dz = '0.3'
ix = '3'
iy = '3'
iz = '3'
[]
[]
[Problem]
linear_sys_names = 'u_system v_system w_system pressure_system'
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = RhieChowMassFlux
u = vel_x
v = vel_y
w = vel_z
pressure = pressure
rho = ${rho}
p_diffusion_kernel = p_diffusion
[]
[]
[Variables]
[vel_x]
type = MooseLinearVariableFVReal
initial_condition = 0.5
solver_sys = u_system
[]
[vel_y]
type = MooseLinearVariableFVReal
solver_sys = v_system
initial_condition = 0.0
[]
[vel_z]
type = MooseLinearVariableFVReal
solver_sys = w_system
initial_condition = 0.0
[]
[pressure]
type = MooseLinearVariableFVReal
solver_sys = pressure_system
initial_condition = 0.2
[]
[]
[LinearFVKernels]
[u_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_x
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
w = vel_z
momentum_component = 'x'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[v_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_y
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
w = vel_z
momentum_component = 'y'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[w_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_z
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
w = vel_z
momentum_component = 'z'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[u_pressure]
type = LinearFVMomentumPressure
variable = vel_x
pressure = pressure
momentum_component = 'x'
[]
[v_pressure]
type = LinearFVMomentumPressure
variable = vel_y
pressure = pressure
momentum_component = 'y'
[]
[w_pressure]
type = LinearFVMomentumPressure
variable = vel_z
pressure = pressure
momentum_component = 'z'
[]
[p_diffusion]
type = LinearFVAnisotropicDiffusion
variable = pressure
diffusion_tensor = Ainv
use_nonorthogonal_correction = false
[]
[HbyA_divergence]
type = LinearFVDivergence
variable = pressure
face_flux = HbyA
force_boundary_execution = true
[]
[]
[LinearFVBCs]
[inlet-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_x
functor = '1.1'
[]
[inlet-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_y
functor = '0.0'
[]
[inlet-w]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_z
functor = '0.0'
[]
[walls-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom back front'
variable = vel_x
functor = 0.0
[]
[walls-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom back front'
variable = vel_y
functor = 0.0
[]
[walls-w]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom back front'
variable = vel_z
functor = 0.0
[]
[outlet_p]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'right'
variable = pressure
functor = 1.4
[]
[outlet_u]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_x
use_two_term_expansion = false
boundary = right
[]
[outlet_v]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_y
use_two_term_expansion = false
boundary = right
[]
[outlet_w]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_z
use_two_term_expansion = false
boundary = right
[]
[]
[Executioner]
type = SIMPLE
momentum_l_abs_tol = 1e-10
pressure_l_abs_tol = 1e-10
momentum_l_tol = 0
pressure_l_tol = 0
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system w_system'
pressure_system = 'pressure_system'
momentum_equation_relaxation = 0.8
pressure_variable_relaxation = 0.3
num_iterations = 100
pressure_absolute_tolerance = 1e-10
momentum_absolute_tolerance = 1e-10
momentum_petsc_options_iname = '-pc_type -pc_hypre_type -pc_hypre_boomeramg_agg_nl -pc_hypre_boomeramg_agg_num_paths -pc_hypre_boomeramg_truncfactor -pc_hypre_boomeramg_strong_threshold -pc_hypre_boomeramg_coarsen_type -pc_hypre_boomeramg_interp_type'
momentum_petsc_options_value = 'hypre boomeramg 4 1 0.1 0.6 HMIS ext+i'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type -pc_hypre_boomeramg_agg_nl -pc_hypre_boomeramg_agg_num_paths -pc_hypre_boomeramg_truncfactor -pc_hypre_boomeramg_strong_threshold -pc_hypre_boomeramg_coarsen_type -pc_hypre_boomeramg_interp_type'
pressure_petsc_options_value = 'hypre boomeramg 2 1 0.1 0.6 HMIS ext+i'
print_fields = false
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/cht/flow-around-square-linear.i)
mu = 0.01
rho = 1.1
k = 0.0005
cp = 10
k_s = 3.0
h_conv = 5
power_density = 10000
advected_interp_method = 'upwind'
[Mesh]
[generated_mesh]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
xmin = 0
ymin = 0
ymax = 0.1
xmax = 0.1
[]
[subdomain1]
type = SubdomainBoundingBoxGenerator
input = generated_mesh
block_name = subdomain1
bottom_left = '0.04 0.04 0'
block_id = 1
top_right = '0.06 0.06 0'
[]
[interface]
type = SideSetsBetweenSubdomainsGenerator
input = subdomain1
primary_block = 0
paired_block = 1
new_boundary = interface
[]
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system energy_system solid_energy_system'
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = RhieChowMassFlux
u = vel_x
v = vel_y
pressure = pressure
rho = ${rho}
p_diffusion_kernel = p_diffusion
block = 0
[]
[]
[Variables]
[vel_x]
type = MooseLinearVariableFVReal
initial_condition = 0.1
solver_sys = u_system
block = 0
[]
[vel_y]
type = MooseLinearVariableFVReal
solver_sys = v_system
initial_condition = 0.01
block = 0
[]
[pressure]
type = MooseLinearVariableFVReal
solver_sys = pressure_system
initial_condition = 0.2
block = 0
[]
[T_fluid]
type = MooseLinearVariableFVReal
solver_sys = energy_system
initial_condition = 300
block = 0
[]
[T_solid]
type = MooseLinearVariableFVReal
solver_sys = solid_energy_system
initial_condition = 500
block = 1
[]
[]
[LinearFVKernels]
[u_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_x
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'x'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = true
[]
[v_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_y
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'y'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = true
[]
[u_pressure]
type = LinearFVMomentumPressure
variable = vel_x
pressure = pressure
momentum_component = 'x'
[]
[v_pressure]
type = LinearFVMomentumPressure
variable = vel_y
pressure = pressure
momentum_component = 'y'
[]
[p_diffusion]
type = LinearFVAnisotropicDiffusion
variable = pressure
diffusion_tensor = Ainv
use_nonorthogonal_correction = true
[]
[HbyA_divergence]
type = LinearFVDivergence
variable = pressure
face_flux = HbyA
force_boundary_execution = true
[]
[h_advection]
type = LinearFVEnergyAdvection
variable = T_fluid
advected_quantity = temperature
cp = ${cp}
advected_interp_method = ${advected_interp_method}
rhie_chow_user_object = 'rc'
[]
[conduction]
type = LinearFVDiffusion
variable = T_fluid
diffusion_coeff = ${k}
use_nonorthogonal_correction = true
[]
[solid-conduction]
type = LinearFVDiffusion
variable = T_solid
diffusion_coeff = ${k_s}
use_nonorthogonal_correction = true
[]
[solid-source]
type = LinearFVSource
variable = T_solid
source_density = ${power_density}
[]
[]
[LinearFVBCs]
[inlet-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_x
functor = '0.1'
[]
[inlet-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_y
functor = '0.0'
[]
[walls-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom interface'
variable = vel_x
functor = 0.0
[]
[walls-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom interface'
variable = vel_y
functor = 0.0
[]
[outlet_p]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'right'
variable = pressure
functor = 1.4
[]
[outlet_u]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_x
use_two_term_expansion = false
boundary = right
[]
[outlet_v]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_y
use_two_term_expansion = false
boundary = right
[]
[inlet_T]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = T_fluid
functor = 300
boundary = 'left'
[]
[walls_T]
type = LinearFVAdvectionDiffusionFunctorNeumannBC
variable = T_fluid
functor = 0.0
boundary = 'top bottom'
[]
[outlet_T]
type = LinearFVAdvectionDiffusionOutflowBC
variable = T_fluid
use_two_term_expansion = false
boundary = right
[]
[fluid_solid]
type = LinearFVConvectiveHeatTransferBC
variable = T_fluid
T_solid = T_solid
T_fluid = T_fluid
boundary = interface
h = ${h_conv}
[]
[solid_fluid]
type = LinearFVConvectiveHeatTransferBC
variable = T_solid
T_solid = T_solid
T_fluid = T_fluid
boundary = interface
h = ${h_conv}
[]
[]
[FunctorMaterials]
[rhocpT]
property_name = 'rhocpT'
type = ParsedFunctorMaterial
functor_names = 'T_fluid'
expression = '${rho}*${cp}*T_fluid'
[]
[]
[Postprocessors]
[h_in]
type = VolumetricFlowRate
boundary = left
vel_x = vel_x
vel_y = vel_y
rhie_chow_user_object = rc
advected_quantity = 'rhocpT'
subtract_mesh_velocity = false
[]
[h_out]
type = VolumetricFlowRate
boundary = right
vel_x = vel_x
vel_y = vel_y
rhie_chow_user_object = rc
advected_quantity = 'rhocpT'
advected_interp_method = upwind
subtract_mesh_velocity = false
[]
[power]
type = ElementIntegralFunctorPostprocessor
functor = ${power_density}
block = 1
[]
[]
[Executioner]
type = SIMPLE
momentum_l_abs_tol = 1e-13
pressure_l_abs_tol = 1e-13
energy_l_abs_tol = 1e-13
solid_energy_l_abs_tol = 1e-13
momentum_l_tol = 0
pressure_l_tol = 0
energy_l_tol = 0
solid_energy_l_tol = 0
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
energy_system = 'energy_system'
solid_energy_system = 'solid_energy_system'
momentum_equation_relaxation = 0.8
energy_equation_relaxation = 1.0
pressure_variable_relaxation = 0.3
num_iterations = 1000
pressure_absolute_tolerance = 1e-10
momentum_absolute_tolerance = 1e-10
energy_absolute_tolerance = 1e-10
solid_energy_absolute_tolerance = 1e-10
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
energy_petsc_options_iname = '-pc_type -pc_hypre_type'
energy_petsc_options_value = 'hypre boomeramg'
solid_energy_petsc_options_iname = '-pc_type -pc_hypre_type'
solid_energy_petsc_options_value = 'hypre boomeramg'
print_fields = false
continue_on_max_its = true
[]
[Outputs]
exodus = true
execute_on = timestep_end
[]
(test/tests/multiapps/linearfv_nonlinearfv/linearfv.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
nx = 6
[]
[]
[Problem]
linear_sys_names = 'u_sys'
[]
[Variables]
[u]
type = MooseLinearVariableFVReal
solver_sys = 'u_sys'
initial_condition = 1.0
[]
[]
[AuxVariables]
[diff_var]
type = MooseVariableFVReal
initial_condition = 2.0
[]
[]
[LinearFVKernels]
[diffusion]
type = LinearFVDiffusion
variable = u
diffusion_coeff = diff_var
[]
[source]
type = LinearFVSource
variable = u
source_density = 1
[]
[]
[LinearFVBCs]
[dir]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = u
boundary = "left right"
functor = 1
[]
[]
[MultiApps]
inactive = 'nonlinear'
[nonlinear]
type = FullSolveMultiApp
input_files = nonlinearfv.i
execute_on = timestep_begin
no_restore = true
[]
[]
[Transfers]
inactive = 'from_nonlinear to_nonlinear'
[from_nonlinear]
type = MultiAppCopyTransfer
from_multi_app = nonlinear
source_variable = 'v'
variable = 'diff_var'
execute_on = timestep_begin
[]
[to_nonlinear]
type = MultiAppCopyTransfer
to_multi_app = nonlinear
source_variable = 'u'
variable = 'diff_var'
execute_on = timestep_begin
[]
[]
[Executioner]
type = Steady
system_names = u_sys
l_tol = 1e-10
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu mumps'
fixed_point_rel_tol = 1e-10
[]
[Outputs]
exodus = true
execute_on = timestep_end
[]
(modules/navier_stokes/test/tests/finite_volume/wcns/enthalpy_equation/enthalpy_equation.i)
H = 0.015 #halfwidth of the channel, 10 cm of channel height
L = 1
bulk_u = 0.01
p_ref = 101325.0
advected_interp_method = 'upwind'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${L}
ymin = -${H}
ymax = ${H}
nx = 30
ny = 15
[]
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system energy_system'
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = RhieChowMassFlux
u = vel_x
v = vel_y
pressure = pressure
rho = 'rho'
p_diffusion_kernel = p_diffusion
[]
[]
[Variables]
[vel_x]
type = MooseLinearVariableFVReal
solver_sys = u_system
initial_condition = ${bulk_u}
[]
[vel_y]
type = MooseLinearVariableFVReal
solver_sys = v_system
initial_condition = 0
[]
[pressure]
type = MooseLinearVariableFVReal
solver_sys = pressure_system
initial_condition = ${p_ref}
[]
[h]
type = MooseLinearVariableFVReal
solver_sys = energy_system
initial_condition = 44000 # 1900 is an approx of cp(T)
[]
[]
[AuxVariables]
[rho_var]
type = MooseLinearVariableFVReal
[]
[cp_var]
type = MooseLinearVariableFVReal
[]
[mu_var]
type = MooseLinearVariableFVReal
[]
[k_var]
type = MooseLinearVariableFVReal
[]
[T]
type = MooseLinearVariableFVReal
initial_condition = 777.
[]
[]
[LinearFVKernels]
[u_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_x
mu = 'mu'
momentum_component = 'x'
use_nonorthogonal_correction = false
advected_interp_method = ${advected_interp_method}
rhie_chow_user_object = 'rc'
u = vel_x
v = vel_y
[]
[u_pressure]
type = LinearFVMomentumPressure
variable = vel_x
pressure = pressure
momentum_component = 'x'
[]
[v_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_y
mu = 'mu'
momentum_component = 'y'
use_nonorthogonal_correction = false
advected_interp_method = ${advected_interp_method}
rhie_chow_user_object = 'rc'
u = vel_x
v = vel_y
[]
[v_pressure]
type = LinearFVMomentumPressure
variable = vel_y
pressure = pressure
momentum_component = 'y'
[]
[p_diffusion]
type = LinearFVAnisotropicDiffusion
variable = pressure
diffusion_tensor = Ainv
use_nonorthogonal_correction = false
[]
[HbyA_divergence]
type = LinearFVDivergence
variable = pressure
face_flux = HbyA
force_boundary_execution = true
[]
[temp_conduction]
type = LinearFVDiffusion
diffusion_coeff = 'alpha'
variable = h
[]
[temp_advection]
type = LinearFVEnergyAdvection
variable = h
advected_interp_method = ${advected_interp_method}
rhie_chow_user_object = 'rc'
[]
[]
[LinearFVBCs]
[inlet_u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_x
functor = ${bulk_u} #${bulk_u} #'fully_developed_velocity'
[]
[inlet-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_y
functor = 0
[]
[inlet_h]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = h
boundary = 'left'
functor = h_from_p_T # ${fparse 1900.*860.}
[]
[inlet_T]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = T
boundary = 'left'
functor = 860.
[]
[walls-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = vel_x
boundary = 'top bottom'
functor = 0.
[]
[walls-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = vel_y
boundary = 'top bottom'
functor = 0.
[]
[walls_h]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = h
boundary = 'top bottom'
functor = h_from_p_T # ${fparse 1900. * 950}
[]
[walls_T]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = T
boundary = 'top bottom'
functor = 950.
[]
[walls_p]
type = LinearFVExtrapolatedPressureBC
boundary = 'top bottom'
variable = pressure
use_two_term_expansion = false
[]
[outlet_p]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'right'
variable = pressure
functor = ${p_ref}
[]
[outlet_h]
type = LinearFVAdvectionDiffusionOutflowBC
variable = h
use_two_term_expansion = false
boundary = 'right'
[]
[outlet_u]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_x
use_two_term_expansion = false
boundary = right
[]
[outlet_v]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_y
use_two_term_expansion = false
boundary = right
[]
[]
[FluidProperties]
[lead]
type = LeadFluidProperties
[]
[]
[FunctorMaterials]
[fluid_props_to_mat_props]
type = GeneralFunctorFluidProps
fp = lead
pressure = ${p_ref}
T_fluid = 'T'
speed = 1
porosity = 1
characteristic_length = 1
[]
[alpha]
type = ADParsedFunctorMaterial
property_name = 'alpha'
functor_names = 'k cp'
expression = 'k/cp'
[]
[enthalpy_material]
type = LinearFVEnthalpyFunctorMaterial
pressure = ${p_ref}
T_fluid = T
h = h
fp = lead
[]
[]
[AuxKernels]
[rho_out]
type = FunctorAux
functor = 'rho'
variable = 'rho_var'
execute_on = 'NONLINEAR'
[]
[cp_out]
type = FunctorAux
functor = 'cp'
variable = 'cp_var'
execute_on = 'NONLINEAR'
[]
[mu_out]
type = FunctorAux
functor = 'mu'
variable = 'mu_var'
execute_on = 'NONLINEAR'
[]
[k_out]
type = FunctorAux
functor = 'k'
variable = 'k_var'
execute_on = 'NONLINEAR'
[]
[T_from_h_functor]
type = FunctorAux
functor = 'T_from_p_h'
variable = 'T'
execute_on = 'NONLINEAR'
[]
[]
[Executioner]
type = SIMPLE
momentum_l_abs_tol = 1e-6
pressure_l_abs_tol = 1e-6
energy_l_abs_tol = 1e-8
momentum_l_tol = 0
pressure_l_tol = 0
energy_l_tol = 0
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
energy_system = 'energy_system'
momentum_equation_relaxation = 0.7
pressure_variable_relaxation = 0.3
energy_equation_relaxation = 0.9
num_iterations = 200
pressure_absolute_tolerance = 1e-6
momentum_absolute_tolerance = 1e-6
energy_absolute_tolerance = 1e-6
print_fields = false
momentum_l_max_its = 1000
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
energy_petsc_options_iname = '-pc_type -pc_hypre_type'
energy_petsc_options_value = 'hypre boomeramg'
continue_on_max_its = true
[]
[Outputs]
exodus = true
execute_on = 'TIMESTEP_BEGIN FINAL'
[]
(test/tests/time_integrators/implicit-euler/ie-linearfv.i)
###########################################################
# This is a simple test with a time-dependent problem
# demonstrating the use of the TimeIntegrator system.
#
# Testing a solution that is second order in space
# and first order in time
#
# @Requirement F1.30
###########################################################
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 10
ny = 10
[]
[Problem]
linear_sys_names = 'u_sys'
[]
[Variables]
[u]
type = MooseLinearVariableFVReal
solver_sys = 'u_sys'
initial_condition = 0.0
[]
[]
[Functions]
[forcing_fn]
type = ParsedFunction
expression = ((x*x)+(y*y))-(4*t)
[]
[exact_fn]
type = ParsedFunction
expression = t*((x*x)+(y*y))
[]
[]
[LinearFVKernels]
[ie]
type = LinearFVTimeDerivative
variable = u
[]
[diff]
type = LinearFVDiffusion
variable = u
[]
[source]
type = LinearFVSource
variable = u
source_density = forcing_fn
[]
[]
[LinearFVBCs]
[all]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = u
boundary = '0 1 2 3'
functor = exact_fn
[]
[]
[Postprocessors]
[l2_err]
type = ElementL2Error
variable = u
function = exact_fn
[]
[]
[Executioner]
type = Transient
system_names = u_sys
l_tol = 1e-10
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
# Test of the TimeIntegrator System
scheme = 'implicit-euler'
start_time = 0.0
num_steps = 5
dt = 0.25
[]
[Outputs]
exodus = true
[]
(test/tests/variables/linearfv/diffusion-1d-pp.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
nx = 50
[]
[]
[Problem]
linear_sys_names = 'u_sys'
[]
[Variables]
[u]
type = MooseLinearVariableFVReal
solver_sys = 'u_sys'
initial_condition = 1.0
[]
[]
[LinearFVKernels]
[diffusion]
type = LinearFVDiffusion
variable = u
diffusion_coeff = coeff_func
[]
[source]
type = LinearFVSource
variable = u
source_density = source_func
[]
[]
[LinearFVBCs]
[dir]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = u
boundary = "left right"
functor = analytic_solution
[]
[]
[Functions]
[coeff_func]
type = ParsedFunction
expression = '0.5*x'
[]
[source_func]
type = ParsedFunction
expression = '2*x'
[]
[analytic_solution]
type = ParsedFunction
expression = '1-x*x'
[]
[]
[Postprocessors]
[average]
type = ElementAverageValue
variable = u
execute_on = TIMESTEP_END
outputs = csv
[]
[min]
type = ElementExtremeValue
variable = u
value_type = min
execute_on = TIMESTEP_END
outputs = csv
[]
[max]
type = ElementExtremeValue
variable = u
value_type = max
execute_on = TIMESTEP_END
outputs = csv
[]
[num_dofs]
type = NumDOFs
execute_on = TIMESTEP_END
outputs = csv
[]
[elem_value]
type = ElementalVariableValue
variable = u
elementid = 10
execute_on = TIMESTEP_END
outputs = csv
[]
[point_value]
type = PointValue
variable = u
point = '0.33333 0 0'
execute_on = TIMESTEP_END
outputs = csv
[]
[]
[VectorPostprocessors]
[line-sample]
type = LineValueSampler
variable = u
start_point = '0.13333 0 0'
end_point = '0.766666 0 0'
num_points = 9
sort_by = x
execute_on = TIMESTEP_END
outputs = vpp_csv
[]
[]
[Executioner]
type = Steady
system_names = u_sys
l_tol = 1e-10
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
[csv]
type = CSV
execute_on = TIMESTEP_END
[]
[vpp_csv]
type = CSV
execute_on = TIMESTEP_END
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/lid-driven/linear-segregated/lid-driven-segregated.i)
mu = .01
rho = 1
advected_interp_method = 'average'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = .1
ymin = 0
ymax = .1
nx = 3
ny = 3
[]
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system'
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = RhieChowMassFlux
u = vel_x
v = vel_y
pressure = pressure
rho = ${rho}
p_diffusion_kernel = p_diffusion
[]
[]
[Variables]
[vel_x]
type = MooseLinearVariableFVReal
initial_condition = 0.0
solver_sys = u_system
[]
[vel_y]
type = MooseLinearVariableFVReal
initial_condition = 0.0
solver_sys = v_system
[]
[pressure]
type = MooseLinearVariableFVReal
solver_sys = pressure_system
initial_condition = 0.2
[]
[]
[LinearFVKernels]
[u_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_x
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'x'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[v_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_y
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'y'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[u_pressure]
type = LinearFVMomentumPressure
variable = vel_x
pressure = pressure
momentum_component = 'x'
[]
[v_pressure]
type = LinearFVMomentumPressure
variable = vel_y
pressure = pressure
momentum_component = 'y'
[]
[p_diffusion]
type = LinearFVAnisotropicDiffusion
variable = pressure
diffusion_tensor = Ainv
use_nonorthogonal_correction = false
[]
[HbyA_divergence]
type = LinearFVDivergence
variable = pressure
face_flux = HbyA
force_boundary_execution = true
[]
[]
[LinearFVBCs]
[top_x]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = vel_x
boundary = 'top'
functor = 1
[]
[no_slip_x]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = vel_x
boundary = 'left right bottom'
functor = 0
[]
[no_slip_y]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = vel_y
boundary = 'left right top bottom'
functor = 0
[]
[pressure-extrapolation]
type = LinearFVExtrapolatedPressureBC
boundary = 'left right top bottom'
variable = pressure
use_two_term_expansion = true
[]
[]
[Executioner]
type = SIMPLE
momentum_l_abs_tol = 1e-10
pressure_l_abs_tol = 1e-10
momentum_l_tol = 0
pressure_l_tol = 0
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
momentum_equation_relaxation = 0.8
pressure_variable_relaxation = 0.3
num_iterations = 500
pressure_absolute_tolerance = 1e-10
momentum_absolute_tolerance = 1e-10
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
print_fields = false
pin_pressure = true
pressure_pin_value = 0.0
pressure_pin_point = '0.05 0.05 0.0'
[]
[Outputs]
exodus = true
csv = false
perf_graph = false
print_nonlinear_residuals = false
print_linear_residuals = true
[]
(test/tests/postprocessors/side_diffusive_flux_integral/side_diffusive_flux_integral_linear_fv.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Problem]
linear_sys_names = 'u_sys'
[]
[Variables]
[u]
solver_sys = 'u_sys'
type = MooseLinearVariableFVReal
[]
[]
[LinearFVKernels]
[diff]
type = LinearFVDiffusion
variable = u
diffusion_coeff = diffusivity
[]
[]
[LinearFVBCs]
[left]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = u
boundary = left
functor = 0
[]
[right]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = u
boundary = right
functor = 1
[]
[]
[FunctorMaterials]
[mat_props]
type = GenericFunctorMaterial
prop_names = diffusivity
prop_values = 1
[]
[]
[AuxVariables]
[grad]
family = MONOMIAL_VEC
order = CONSTANT
[]
[]
[AuxKernels]
[grad]
variable = grad
functor = u
type = FunctorElementalGradientAux
[]
[]
[Postprocessors]
[avg_left]
type = SideAverageValue
variable = u
boundary = left
[]
[avg_right]
type = SideAverageValue
variable = u
boundary = right
[]
[avg_flux_left]
type = SideDiffusiveFluxAverage
variable = u
boundary = left
functor_diffusivity = diffusivity
[]
[avg_flux_right]
type = SideDiffusiveFluxAverage
variable = u
boundary = right
functor_diffusivity = diffusivity
[]
[]
[Executioner]
type = Steady
system_names = u_sys
l_tol = 1e-10
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[]
(test/tests/linearfvkernels/diffusion/diffusion-1d.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
nx = 2
[]
[]
[Problem]
linear_sys_names = 'u_sys'
[]
[Variables]
[u]
type = MooseLinearVariableFVReal
solver_sys = 'u_sys'
initial_condition = 1.0
[]
[]
[LinearFVKernels]
[diffusion]
type = LinearFVDiffusion
variable = u
diffusion_coeff = coeff_func
[]
[source]
type = LinearFVSource
variable = u
source_density = source_func
[]
[]
[LinearFVBCs]
[dir]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = u
boundary = "left right"
functor = analytic_solution
[]
[]
[Functions]
[coeff_func]
type = ParsedFunction
expression = '0.5*x'
[]
[source_func]
type = ParsedFunction
expression = '2*x'
[]
[analytic_solution]
type = ParsedFunction
expression = '1-x*x'
[]
[]
[Postprocessors]
[h]
type = AverageElementSize
execute_on = FINAL
[]
[error]
type = ElementL2FunctorError
approximate = u
exact = analytic_solution
execute_on = FINAL
[]
[]
[Executioner]
type = Steady
system_names = u_sys
l_tol = 1e-10
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
[csv]
type = CSV
execute_on = FINAL
[]
[]
(test/tests/linearfvkernels/diffusion-reaction-advection/advection-diffusion-reaction-2d.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 1
ymax = 0.5
[]
[]
[Problem]
linear_sys_names = 'u_sys'
[]
[Variables]
[u]
type = MooseLinearVariableFVReal
solver_sys = 'u_sys'
initial_condition = 1.0
[]
[]
[LinearFVKernels]
[diffusion]
type = LinearFVDiffusion
variable = u
diffusion_coeff = diff_coeff_func
use_nonorthogonal_correction = false
[]
[advection]
type = LinearFVAdvection
variable = u
velocity = "0.5 0 0"
advected_interp_method = average
[]
[reaction]
type = LinearFVReaction
variable = u
coeff = coeff_func
[]
[source]
type = LinearFVSource
variable = u
source_density = source_func
[]
[]
[LinearFVBCs]
inactive = "outflow neumann"
[dir]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = u
boundary = "left right top bottom"
functor = analytic_solution
[]
[outflow]
type = LinearFVAdvectionDiffusionOutflowBC
variable = u
boundary = "right"
use_two_term_expansion = true
[]
[neumann]
type = LinearFVAdvectionDiffusionFunctorNeumannBC
variable = u
boundary = "top"
functor = analytic_solution_neumann_top
diffusion_coeff = diff_coeff_func
[]
[]
[Functions]
[diff_coeff_func]
type = ParsedFunction
expression = '1.0+0.5*x*y'
[]
[coeff_func]
type = ParsedFunction
expression = '1.0+1.0/(1+x*y)'
[]
[source_func]
type = ParsedFunction
expression = '-1.0*x*pi*sin((1/2)*x*pi)*cos(2*y*pi) - 0.25*y*pi*sin(2*y*pi)*cos((1/2)*x*pi) + (1.0 + 1.0/(x*y + 1))*(sin((1/2)*x*pi)*sin(2*y*pi) + 1.5) + (17/4)*pi^2*(0.5*x*y + 1.0)*sin((1/2)*x*pi)*sin(2*y*pi) + 0.25*pi*sin(2*y*pi)*cos((1/2)*x*pi)'
[]
[analytic_solution]
type = ParsedFunction
expression = 'sin((1/2)*x*pi)*sin(2*y*pi) + 1.5'
[]
[analytic_solution_neumann_top]
type = ParsedFunction
expression = '(1.0+0.5*x*y)*sin((1/2)*x*pi)*cos(2*y*pi)*2*pi'
[]
[]
[Postprocessors]
[h]
type = AverageElementSize
execute_on = FINAL
[]
[error]
type = ElementL2FunctorError
approximate = u
exact = analytic_solution
execute_on = FINAL
[]
[]
[Convergence]
[linear]
type = IterationCountConvergence
max_iterations = 1
converge_at_max_iterations = true
[]
[]
[Executioner]
type = Steady
system_names = u_sys
l_tol = 1e-10
multi_system_fixed_point=true
multi_system_fixed_point_convergence=linear
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
[csv]
type = CSV
execute_on = FINAL
[]
[]
(test/tests/transfers/multiapp_copy_transfer/linear_sys_to_aux/linear_sub.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
nx = 10
[]
[]
[Problem]
linear_sys_names = 'u_sys'
[]
[Variables]
[u]
type = MooseLinearVariableFVReal
solver_sys = 'u_sys'
initial_condition = 1.0
[]
[]
[LinearFVKernels]
[diffusion]
type = LinearFVDiffusion
variable = u
diffusion_coeff = coeff_func
[]
[source]
type = LinearFVSource
variable = u
source_density = source_func
[]
[]
[LinearFVBCs]
[dir]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = u
boundary = "left right"
functor = analytic_solution
[]
[]
[Functions]
[coeff_func]
type = ParsedFunction
expression = '0.5*x'
[]
[source_func]
type = ParsedFunction
expression = '2*x'
[]
[analytic_solution]
type = ParsedFunction
expression = '1-x*x'
[]
[]
[Executioner]
type = Steady
system_names = u_sys
l_tol = 1e-10
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
execute_on = TIMESTEP_END
[]
(test/tests/linearfvkernels/block-restriction/block-restricted-diffusion-react.i)
source=1
diff_coeff=2
reac_coeff=3
[Mesh]
[cmg]
type = CartesianMeshGenerator
dim = 1
dx = '0.5 0.5'
ix = '20 20'
subdomain_id = '1 2'
[]
[]
[Problem]
linear_sys_names = 'u_sys'
[]
[Variables]
[u]
type = MooseLinearVariableFVReal
solver_sys = 'u_sys'
initial_condition = 1.0
[]
[]
[LinearFVKernels]
[diffusion]
type = LinearFVDiffusion
variable = u
diffusion_coeff = ${diff_coeff}
use_nonorthogonal_correction = false
block = 1
[]
[reaction]
type = LinearFVReaction
variable = u
coeff = ${reac_coeff}
block = 2
[]
[source]
type = LinearFVSource
variable = u
source_density = ${source}
[]
[]
[LinearFVBCs]
[dir]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = u
boundary = "left"
functor = 0
[]
[]
[Functions]
[analytic_solution]
type = ParsedFunction
expression = 'if(x<0.5, -x*x*S/2/D+(S/C+0.5*0.5/2/D*S)/0.5*x, S/C)'
symbol_names = 'S D C'
symbol_values = '${source} ${diff_coeff} ${reac_coeff}'
[]
[]
[Postprocessors]
[h]
type = AverageElementSize
execute_on = TIMESTEP_END
block = 2
[]
[error]
type = ElementL2FunctorError
approximate = u
exact = analytic_solution
execute_on = TIMESTEP_END
block = 2
[]
[]
[Convergence]
[linear]
type = IterationCountConvergence
max_iterations = 1
converge_at_max_iterations = true
[]
[]
[Executioner]
type = Steady
system_names = u_sys
multi_system_fixed_point=true
multi_system_fixed_point_convergence=linear
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_rtol'
petsc_options_value = 'hypre boomeramg 1e-10'
[]
[Outputs]
[csv]
type = CSV
execute_on = TIMESTEP_END
[]
[]
(test/tests/linearfvkernels/diffusion/diffusion-2d_neumann.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 1
ymax = 0.5
[]
[]
[Problem]
linear_sys_names = 'u_sys'
[]
[Variables]
[u]
type = MooseLinearVariableFVReal
solver_sys = 'u_sys'
initial_condition = 1.0
[]
[]
[LinearFVKernels]
[diffusion]
type = LinearFVDiffusion
variable = u
diffusion_coeff = coeff_func
use_nonorthogonal_correction = false
[]
[source]
type = LinearFVSource
variable = u
source_density = source_func
[]
[]
[LinearFVBCs]
[dir]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = u
boundary = "left right"
functor = analytic_solution
[]
[neu_bottom]
type = LinearFVAdvectionDiffusionFunctorNeumannBC
variable = u
boundary = "bottom"
functor = analytic_solution_neumann_bottom
diffusion_coeff = coeff_func
[]
[neu_top]
type = LinearFVAdvectionDiffusionFunctorNeumannBC
variable = u
boundary = "top"
functor = analytic_solution_neumann_top
diffusion_coeff = coeff_func
[]
[]
[Functions]
[coeff_func]
type = ParsedFunction
expression = '1+0.5*x*y'
[]
[source_func]
type = ParsedFunction
expression = '2*(1.5-y*y)+2*x*y*(1.5-y*y)+2*(1.5-x*x)+2*x*y*(1.5-x*x)'
[]
[analytic_solution]
type = ParsedFunction
expression = '(1.5-x*x)*(1.5-y*y)'
[]
[analytic_solution_neumann_bottom]
type = ParsedFunction
expression = '-(1+0.5*x*y)*(1.5-x*x)*(-2*y)'
[]
[analytic_solution_neumann_top]
type = ParsedFunction
expression = '(1+0.5*x*y)*(1.5-x*x)*(-2*y)'
[]
[]
[Postprocessors]
[h]
type = AverageElementSize
execute_on = FINAL
[]
[error]
type = ElementL2FunctorError
approximate = u
exact = analytic_solution
execute_on = FINAL
[]
[]
[Convergence]
[linear]
type = IterationCountConvergence
max_iterations = 1
converge_at_max_iterations = true
[]
[]
[Executioner]
type = Steady
system_names = u_sys
l_tol = 1e-10
multi_system_fixed_point=true
multi_system_fixed_point_convergence=linear
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
[csv]
type = CSV
execute_on = FINAL
[]
[]
(test/tests/time_steppers/iteration_adaptive/adapt_linear_systems.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 50
ny = 2
xmax = 5
[]
[Problem]
linear_sys_names = 'u_sys'
[]
[Variables]
[u]
type = MooseLinearVariableFVReal
solver_sys = 'u_sys'
initial_condition = 1.0
[]
[]
[LinearFVKernels]
[time]
type = LinearFVTimeDerivative
variable = 'u'
[]
[diffusion]
type = LinearFVDiffusion
variable = u
diffusion_coeff = 5
[]
[source]
type = LinearFVSource
variable = u
source_density = 2
[]
[]
[LinearFVBCs]
[dir]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = u
boundary = "left right"
functor = 12
[]
[]
[Executioner]
type = Transient
system_names = u_sys
start_time = 0.0
end_time = 19
n_startup_steps = 2
dtmax = 6.0
[TimeStepper]
type = IterationAdaptiveDT
optimal_iterations = 8
dt = 1.0
[]
verbose = true
linear_convergence = much_logic
[]
[Convergence]
[force_grow]
type = IterationCountConvergence
min_iterations = 0
max_iterations = 4
converge_at_max_iterations = true
[]
[force_shrink]
type = IterationCountConvergence
min_iterations = 12
max_iterations = 13
converge_at_max_iterations = true
[]
[much_logic]
type = ParsedConvergence
convergence_expression = 'if(time < 5, force_grow, force_shrink)'
symbol_names = 'time force_grow force_shrink'
symbol_values = 'time force_grow force_shrink'
[]
[]
[Postprocessors]
[_dt]
type = TimestepSize
[]
[time]
type = TimePostprocessor
[]
[]
[Outputs]
csv = true
[]
(test/tests/linearfvkernels/diffusion/diffusion-2d.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 1
ymax = 0.5
[]
[]
[Problem]
linear_sys_names = 'u_sys'
[]
[Variables]
[u]
type = MooseLinearVariableFVReal
solver_sys = 'u_sys'
initial_condition = 1.0
[]
[]
[LinearFVKernels]
[diffusion]
type = LinearFVDiffusion
variable = u
diffusion_coeff = coeff_func
use_nonorthogonal_correction = false
[]
[source]
type = LinearFVSource
variable = u
source_density = source_func
[]
[]
[LinearFVBCs]
[dir]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = u
boundary = "left right top bottom"
functor = analytic_solution
[]
[]
[Functions]
[coeff_func]
type = ParsedFunction
expression = '1+0.5*x*y'
[]
[source_func]
type = ParsedFunction
expression = '2*(1.5-y*y)+2*x*y*(1.5-y*y)+2*(1.5-x*x)+2*x*y*(1.5-x*x)'
[]
[analytic_solution]
type = ParsedFunction
expression = '(1.5-x*x)*(1.5-y*y)'
[]
[]
[Postprocessors]
[h]
type = AverageElementSize
execute_on = FINAL
[]
[error]
type = ElementL2FunctorError
approximate = u
exact = analytic_solution
execute_on = FINAL
[]
[]
[Convergence]
[linear]
type = IterationCountConvergence
max_iterations = 1
converge_at_max_iterations = true
[]
[]
[Executioner]
type = Steady
system_names = u_sys
l_tol = 1e-10
multi_system_fixed_point=true
multi_system_fixed_point_convergence=linear
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
[csv]
type = CSV
execute_on = FINAL
[]
[]
(modules/navier_stokes/test/tests/finite_volume/wcns/enthalpy_equation/1d_test_h_fp.i)
L = 30
nx = 600
bulk_u = 0.01
p_ref = 101325.0
T_in = 860.
q_source = 20000.
advected_interp_method = 'upwind'
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
xmin = 0
xmax = ${L}
nx = ${nx}
[]
allow_renumbering = false
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
advected_interp_method = ${advected_interp_method}
u = vel_x
[]
[Problem]
linear_sys_names = 'u_system pressure_system energy_system'
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = RhieChowMassFlux
u = vel_x
pressure = pressure
rho = 'rho'
p_diffusion_kernel = p_diffusion
[]
[]
[Variables]
[vel_x]
type = MooseLinearVariableFVReal
solver_sys = u_system
initial_condition = ${bulk_u}
[]
[pressure]
type = MooseLinearVariableFVReal
solver_sys = pressure_system
initial_condition = ${p_ref}
[]
[h]
type = MooseLinearVariableFVReal
solver_sys = energy_system
initial_condition = ${fparse 860.*240.}
[]
[]
[AuxVariables]
[rho_var]
type = MooseLinearVariableFVReal
[]
[cp_var]
type = MooseLinearVariableFVReal
[]
[mu_var]
type = MooseLinearVariableFVReal
[]
[k_var]
type = MooseLinearVariableFVReal
[]
[alpha_var]
type = MooseLinearVariableFVReal
[]
[T]
type = MooseLinearVariableFVReal
initial_condition = ${T_in}
[]
[h_aux]
type = MooseLinearVariableFVReal
[]
[]
[LinearFVKernels]
[u_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_x
mu = 'mu'
momentum_component = 'x'
use_nonorthogonal_correction = false
[]
[u_pressure]
type = LinearFVMomentumPressure
variable = vel_x
pressure = pressure
momentum_component = 'x'
[]
[p_diffusion]
type = LinearFVAnisotropicDiffusion
variable = pressure
diffusion_tensor = Ainv
use_nonorthogonal_correction = false
[]
[HbyA_divergence]
type = LinearFVDivergence
variable = pressure
face_flux = HbyA
force_boundary_execution = true
[]
[temp_advection]
type = LinearFVEnergyAdvection
variable = h
[]
[source]
type = LinearFVSource
variable = h
source_density = source_func
[]
[]
[LinearFVBCs]
[inlet_u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_x
functor = ${bulk_u}
[]
[inlet_h]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = h
boundary = 'left'
functor = 'h_from_p_T'
[]
[inlet_T]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = T
boundary = 'left'
functor = ${T_in}
[]
[outlet_p]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'right'
variable = pressure
functor = ${p_ref}
[]
[outlet_h]
type = LinearFVAdvectionDiffusionOutflowBC
variable = h
use_two_term_expansion = false
boundary = 'right'
[]
[outlet_u]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_x
use_two_term_expansion = false
boundary = 'right'
[]
[]
[FluidProperties]
[lead]
type = LeadFluidProperties
[]
[]
[FunctorMaterials]
[enthalpy_material]
type = LinearFVEnthalpyFunctorMaterial
pressure = ${p_ref}
T_fluid = T
h = h
fp = lead
[]
[fluid_props_to_mat_props]
type = GeneralFunctorFluidProps
fp = lead
pressure = ${p_ref}
T_fluid = 'T'
speed = 1
porosity = 1
characteristic_length = 1
[]
[source_func]
type = ADParsedFunctorMaterial
property_name = source_func
functor_names = 'rho'
expression = ${q_source}
[]
[]
[AuxKernels]
[rho_out]
type = FunctorAux
functor = 'rho'
variable = 'rho_var'
execute_on = 'NONLINEAR'
[]
[cp_out]
type = FunctorAux
functor = 'cp'
variable = 'cp_var'
execute_on = 'NONLINEAR'
[]
[mu_out]
type = FunctorAux
functor = 'mu'
variable = 'mu_var'
execute_on = 'NONLINEAR'
[]
[k_out]
type = FunctorAux
functor = 'k'
variable = 'k_var'
execute_on = 'NONLINEAR'
[]
[T_from_h_functor_aux]
type = FunctorAux
functor = 'T_from_p_h'
variable = 'T'
execute_on = 'NONLINEAR'
[]
[h_from_T_functor_aux]
type = FunctorAux
functor = 'h_from_p_T'
variable = 'h_aux'
execute_on = 'NONLINEAR'
[]
[]
[Postprocessors]
[T_out_sim]
type = ElementalVariableValue
variable = T
elementid = ${fparse nx-1}
[]
[]
[Executioner]
type = SIMPLE
momentum_l_abs_tol = 1e-12
pressure_l_abs_tol = 1e-12
energy_l_abs_tol = 1e-12
momentum_l_tol = 0
pressure_l_tol = 0
energy_l_tol = 0
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system'
pressure_system = 'pressure_system'
energy_system = 'energy_system'
momentum_equation_relaxation = 0.7
pressure_variable_relaxation = 0.3
energy_equation_relaxation = 0.95
num_iterations = 100
pressure_absolute_tolerance = 1e-8
momentum_absolute_tolerance = 1e-8
energy_absolute_tolerance = 1e-6
print_fields = false
momentum_l_max_its = 200
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
energy_petsc_options_iname = '-pc_type -pc_hypre_type'
energy_petsc_options_value = 'hypre boomeramg'
continue_on_max_its = true
[]
[Outputs]
[out]
type = CSV
[]
[]
(test/tests/linearfvkernels/advection/advection-2d.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny= 1
ymax = 0.5
[]
[]
[Problem]
linear_sys_names = 'u_sys'
[]
[Variables]
[u]
type = MooseLinearVariableFVReal
solver_sys = 'u_sys'
initial_condition = 1.0
[]
[]
[LinearFVKernels]
[advection]
type = LinearFVAdvection
variable = u
velocity = "0.5 0 0"
advected_interp_method = upwind
[]
[source]
type = LinearFVSource
variable = u
source_density = source_func
[]
[]
[LinearFVBCs]
[inflow]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = u
boundary = "left top bottom"
functor = analytic_solution
[]
[outflow]
type = LinearFVAdvectionDiffusionOutflowBC
variable = u
boundary = "right"
use_two_term_expansion = false
[]
[]
[Functions]
[source_func]
type = ParsedFunction
expression = '0.5*pi*sin(2*y*pi)*cos(x*pi)'
[]
[analytic_solution]
type = ParsedFunction
expression = 'sin(x*pi)*sin(2*y*pi) + 1.5'
[]
[]
[Postprocessors]
[error]
type = ElementL2FunctorError
approximate = u
exact = analytic_solution
execute_on = FINAL
[]
[h]
type = AverageElementSize
execute_on = FINAL
[]
[]
[Convergence]
[linear]
type = IterationCountConvergence
max_iterations = 1
converge_at_max_iterations = true
[]
[]
[Executioner]
type = Steady
system_names = u_sys
l_tol = 1e-10
multi_system_fixed_point=true
multi_system_fixed_point_convergence=linear
petsc_options_iname = '-pc_type -pc_factor_shift_type -pc_factor_shift_amount'
petsc_options_value = 'lu NONZERO 1e-10'
[]
[Outputs]
[csv]
type = CSV
execute_on = FINAL
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/SIMPLEC/2d/2d-velocity-pressure.i)
mu = 2.6
rho = 1.0
advected_interp_method = 'average'
[Mesh]
[mesh]
type = CartesianMeshGenerator
dim = 2
dx = '1.0'
dy = '0.1'
ix = '20'
iy = '3'
[]
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system'
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = RhieChowMassFlux
u = vel_x
v = vel_y
pressure = pressure
rho = ${rho}
p_diffusion_kernel = p_diffusion
pressure_projection_method = consistent
[]
[]
[Variables]
[vel_x]
type = MooseLinearVariableFVReal
initial_condition = 0.5
solver_sys = u_system
[]
[vel_y]
type = MooseLinearVariableFVReal
solver_sys = v_system
initial_condition = 0.0
[]
[pressure]
type = MooseLinearVariableFVReal
solver_sys = pressure_system
initial_condition = 0.2
[]
[]
[LinearFVKernels]
[u_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_x
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'x'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[v_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_y
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'y'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[u_pressure]
type = LinearFVMomentumPressure
variable = vel_x
pressure = pressure
momentum_component = 'x'
[]
[v_pressure]
type = LinearFVMomentumPressure
variable = vel_y
pressure = pressure
momentum_component = 'y'
[]
[p_diffusion]
type = LinearFVAnisotropicDiffusion
variable = pressure
diffusion_tensor = Ainv
use_nonorthogonal_correction = false
[]
[HbyA_divergence]
type = LinearFVDivergence
variable = pressure
face_flux = HbyA
force_boundary_execution = true
[]
[]
[LinearFVBCs]
[inlet-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_x
functor = '1.1'
[]
[inlet-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_y
functor = '0.0'
[]
[walls-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom'
variable = vel_x
functor = 0.0
[]
[walls-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom'
variable = vel_y
functor = 0.0
[]
[outlet_p]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'right'
variable = pressure
functor = 1.4
[]
[outlet_u]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_x
use_two_term_expansion = false
boundary = right
[]
[outlet_v]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_y
use_two_term_expansion = false
boundary = right
[]
[]
[Executioner]
type = SIMPLE
momentum_l_abs_tol = 1e-10
pressure_l_abs_tol = 1e-10
momentum_l_tol = 0
pressure_l_tol = 0
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
momentum_equation_relaxation = 0.8
pressure_variable_relaxation = 1.0
num_iterations = 100
pressure_absolute_tolerance = 1e-10
momentum_absolute_tolerance = 1e-10
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
print_fields = false
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/linear-segregated/steady-transient-compare/common-blocks.i)
mu = 2.6
rho = 1.0
advected_interp_method = 'average'
cp = 300
k = 20
alpha_b = 1e-4
[Mesh]
[mesh]
type = CartesianMeshGenerator
dim = 2
dx = '1.'
dy = '0.2'
ix = '10'
iy = '5'
[]
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system energy_system'
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = RhieChowMassFlux
u = vel_x
v = vel_y
pressure = pressure
rho = ${rho}
p_diffusion_kernel = p_diffusion
[]
[]
[Variables]
[vel_x]
type = MooseLinearVariableFVReal
initial_condition = 0.5
solver_sys = u_system
[]
[vel_y]
type = MooseLinearVariableFVReal
solver_sys = v_system
initial_condition = 0.0
[]
[pressure]
type = MooseLinearVariableFVReal
solver_sys = pressure_system
initial_condition = 0.2
[]
[T]
type = MooseLinearVariableFVReal
solver_sys = energy_system
initial_condition = 300
[]
[]
[LinearFVKernels]
[u_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_x
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'x'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[v_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_y
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'y'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[u_pressure]
type = LinearFVMomentumPressure
variable = vel_x
pressure = pressure
momentum_component = 'x'
[]
[v_pressure]
type = LinearFVMomentumPressure
variable = vel_y
pressure = pressure
momentum_component = 'y'
[]
[u_boussinesq]
type = LinearFVMomentumBoussinesq
variable = vel_x
rho = ${rho}
gravity = '0 -9.81 0'
alpha_name = ${alpha_b}
ref_temperature = 300.0
T_fluid = T
momentum_component = 'x'
[]
[v_boussinesq]
type = LinearFVMomentumBoussinesq
variable = vel_y
rho = ${rho}
gravity = '0 -9.81 0'
alpha_name = ${alpha_b}
ref_temperature = 300.0
T_fluid = T
momentum_component = 'y'
[]
[p_diffusion]
type = LinearFVAnisotropicDiffusion
variable = pressure
diffusion_tensor = Ainv
use_nonorthogonal_correction = false
[]
[HbyA_divergence]
type = LinearFVDivergence
variable = pressure
face_flux = HbyA
force_boundary_execution = true
[]
[h_advection]
type = LinearFVEnergyAdvection
variable = T
advected_quantity = temperature
cp = ${cp}
advected_interp_method = ${advected_interp_method}
rhie_chow_user_object = 'rc'
[]
[conduction]
type = LinearFVDiffusion
variable = T
diffusion_coeff = ${k}
use_nonorthogonal_correction = false
[]
[]
[FunctorMaterials]
[constant_functors]
type = GenericFunctorMaterial
prop_names = 'cp alpha_b'
prop_values = '${cp} ${alpha_b}'
[]
[]
[LinearFVBCs]
[inlet-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_x
functor = '1.1'
[]
[inlet-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_y
functor = '0.0'
[]
[walls-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom'
variable = vel_x
functor = 0.0
[]
[walls-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom'
variable = vel_y
functor = 0.0
[]
[outlet_p]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'right'
variable = pressure
functor = 1.4
[]
[outlet_u]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_x
use_two_term_expansion = false
boundary = right
[]
[outlet_v]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_y
use_two_term_expansion = false
boundary = right
[]
[inlet_top_T]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = T
functor = ${fparse 300.0}
boundary = 'left top'
[]
[bottom_T]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = T
functor = ${fparse 350.0}
boundary = bottom
[]
[outlet_T]
type = LinearFVAdvectionDiffusionOutflowBC
variable = T
use_two_term_expansion = false
boundary = right
[]
[]
[Outputs]
exodus = true
execute_on = FINAL
[]
(test/tests/linearfvkernels/advection/advection-2d-rz.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny= 1
ymax = 0.5
[]
coord_type = RZ
rz_coord_axis = Y
[]
[Problem]
linear_sys_names = 'u_sys'
[]
[Variables]
[u]
type = MooseLinearVariableFVReal
solver_sys = 'u_sys'
initial_condition = 1.0
[]
[]
[LinearFVKernels]
[advection]
type = LinearFVAdvection
variable = u
velocity = "0.0 0.5 0"
advected_interp_method = average
[]
[source]
type = LinearFVSource
variable = u
source_density = source_func
[]
[]
[LinearFVBCs]
[inflow]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = u
boundary = "left right bottom"
functor = analytic_solution
[]
[outflow]
type = LinearFVAdvectionDiffusionOutflowBC
variable = u
boundary = "top"
use_two_term_expansion = true
[]
[]
[Functions]
[source_func]
type = ParsedFunction
expression = '1.0*pi*sin(x*pi)*cos(2*y*pi)'
[]
[analytic_solution]
type = ParsedFunction
expression = 'sin(x*pi)*sin(2*y*pi) + 1.5'
[]
[]
[Postprocessors]
[error]
type = ElementL2FunctorError
approximate = u
exact = analytic_solution
execute_on = FINAL
[]
[h]
type = AverageElementSize
execute_on = FINAL
[]
[]
[Convergence]
[linear]
type = IterationCountConvergence
max_iterations = 10
converge_at_max_iterations = true
[]
[]
[Executioner]
type = Steady
system_names = u_sys
l_tol = 1e-10
multi_system_fixed_point=true
multi_system_fixed_point_convergence=linear
petsc_options_iname = '-pc_type -pc_factor_shift_type -pc_factor_shift_amount'
petsc_options_value = 'lu NONZERO 1e-10'
[]
[Outputs]
[csv]
type = CSV
execute_on = FINAL
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/natural_convection/linear_segregated/2d/diff_heated_cavity_linear_segregated.i)
################################################################################
# MATERIAL PROPERTIES
################################################################################
rho = 3279.
T_0 = 875.0
mu = 1.
k_cond = 38.0
cp = 640.
alpha = 3.26e-4
walls = 'right left top bottom'
[GlobalParams]
rhie_chow_user_object = 'ins_rhie_chow_interpolator'
advected_interp_method = 'upwind'
u = superficial_vel_x
v = superficial_vel_y
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system energy_system'
previous_nl_solution_required = true
[]
################################################################################
# GEOMETRY
################################################################################
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 30
ny = 30
[]
[]
################################################################################
# EQUATIONS: VARIABLES, KERNELS & BCS
################################################################################
[UserObjects]
[ins_rhie_chow_interpolator]
type = RhieChowMassFlux
u = superficial_vel_x
v = superficial_vel_y
pressure = pressure
rho = ${rho}
p_diffusion_kernel = p_diffusion
[]
[]
[Variables]
[superficial_vel_x]
type = MooseLinearVariableFVReal
solver_sys = u_system
[]
[superficial_vel_y]
type = MooseLinearVariableFVReal
solver_sys = v_system
[]
[pressure]
type = MooseLinearVariableFVReal
initial_condition = 0
solver_sys = pressure_system
[]
[T_fluid]
type = MooseLinearVariableFVReal
solver_sys = energy_system
initial_condition = 875
[]
[]
[LinearFVKernels]
[u_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = superficial_vel_x
mu = ${mu}
momentum_component = 'x'
use_nonorthogonal_correction = true
[]
[u_pressure]
type = LinearFVMomentumPressure
variable = superficial_vel_x
pressure = pressure
momentum_component = 'x'
[]
[u_buoyancy]
type = LinearFVMomentumBoussinesq
variable = superficial_vel_x
T_fluid = T_fluid
gravity = '0 -9.81 0'
rho = ${rho}
ref_temperature = ${T_0}
alpha_name = ${alpha}
momentum_component = 'x'
[]
[v_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = superficial_vel_y
mu = ${mu}
momentum_component = 'y'
use_nonorthogonal_correction = true
[]
[v_pressure]
type = LinearFVMomentumPressure
variable = superficial_vel_y
pressure = pressure
momentum_component = 'y'
[]
[v_buoyancy]
type = LinearFVMomentumBoussinesq
variable = superficial_vel_y
T_fluid = T_fluid
gravity = '0 -9.81 0'
rho = ${rho}
ref_temperature = ${T_0}
alpha_name = ${alpha}
momentum_component = 'y'
[]
[p_diffusion]
type = LinearFVAnisotropicDiffusion
variable = pressure
diffusion_tensor = Ainv
use_nonorthogonal_correction = true
[]
[HbyA_divergence]
type = LinearFVDivergence
variable = pressure
face_flux = HbyA
force_boundary_execution = true
[]
####### FUEL ENERGY EQUATION #######
[heat_advection]
type = LinearFVEnergyAdvection
variable = T_fluid
advected_quantity = temperature
cp = ${cp}
[]
[conduction]
type = LinearFVDiffusion
variable = T_fluid
diffusion_coeff = ${fparse k_cond}
[]
[]
[LinearFVBCs]
[no-slip-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = superficial_vel_x
boundary = ${walls}
functor = 0
[]
[no-slip-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = superficial_vel_y
boundary = ${walls}
functor = 0
[]
[T_cold]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = T_fluid
boundary = 'right'
functor = 870.0
[]
[T_hot]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = T_fluid
boundary = 'left'
functor = 880.0
[]
[T_all]
type = LinearFVAdvectionDiffusionExtrapolatedBC
variable = T_fluid
boundary = 'top bottom'
use_two_term_expansion = false
[]
[pressure-extrapolation]
type = LinearFVExtrapolatedPressureBC
boundary = ${walls}
variable = pressure
use_two_term_expansion = false
[]
[]
[FunctorMaterials]
[constant_functors]
type = GenericFunctorMaterial
prop_names = 'cp alpha_b'
prop_values = '${cp} ${alpha}'
[]
[]
################################################################################
# EXECUTION / SOLVE
################################################################################
[Executioner]
type = SIMPLE
momentum_l_abs_tol = 1e-11
pressure_l_abs_tol = 1e-11
energy_l_abs_tol = 1e-11
momentum_l_tol = 0
pressure_l_tol = 0
energy_l_tol = 0
rhie_chow_user_object = 'ins_rhie_chow_interpolator'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
energy_system = 'energy_system'
momentum_equation_relaxation = 0.3
pressure_variable_relaxation = 0.7
energy_equation_relaxation = 0.95
num_iterations = 3000
pressure_absolute_tolerance = 1e-8
momentum_absolute_tolerance = 1e-8
energy_absolute_tolerance = 1e-8
print_fields = false
momentum_l_max_its = 300
pin_pressure = true
pressure_pin_value = 0.0
pressure_pin_point = '0.5 0.0 0.0'
# momentum_petsc_options = '-ksp_monitor'
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
energy_petsc_options_iname = '-pc_type -pc_hypre_type'
energy_petsc_options_value = 'hypre boomeramg'
[]
################################################################################
# SIMULATION OUTPUTS
################################################################################
[Outputs]
exodus = true
[]
(test/tests/linearfvkernels/block-restriction/block-restricted-adr.i)
[Mesh]
[cmg]
type = CartesianMeshGenerator
dim = 2
dx = '0.1 1 0.1'
dy = '0.1 0.5 0.1'
ix = '1 2 1'
iy = '1 1 1'
subdomain_id = '1 1 1 1 2 3 1 1 1'
[]
[transform]
type = TransformGenerator
input = cmg
transform = TRANSLATE
vector_value = '-0.1 -0.1 0.0'
[]
[create_sides]
type = SideSetsBetweenSubdomainsGenerator
input = transform
new_boundary = sides
primary_block = 2
paired_block = 1
[]
[create_outlet]
type = SideSetsBetweenSubdomainsGenerator
input = create_sides
new_boundary = outlet
primary_block = 2
paired_block = 3
[]
[]
[Problem]
linear_sys_names = 'u_sys'
[]
[Variables]
[u]
type = MooseLinearVariableFVReal
solver_sys = 'u_sys'
initial_condition = 1.0
block = 2
[]
[]
[LinearFVKernels]
[diffusion]
type = LinearFVDiffusion
variable = u
diffusion_coeff = diff_coeff_func
use_nonorthogonal_correction = false
[]
[advection]
type = LinearFVAdvection
variable = u
velocity = "0.5 0 0"
advected_interp_method = average
[]
[reaction]
type = LinearFVReaction
variable = u
coeff = coeff_func
[]
[source]
type = LinearFVSource
variable = u
source_density = source_func
[]
[]
[LinearFVBCs]
inactive = "outflow"
[dir]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = u
boundary = "sides outlet"
functor = analytic_solution
[]
[outflow]
type = LinearFVAdvectionDiffusionOutflowBC
variable = u
boundary = "right"
use_two_term_expansion = true
[]
[]
[Functions]
[diff_coeff_func]
type = ParsedFunction
expression = '1.0+0.5*x*y'
[]
[coeff_func]
type = ParsedFunction
expression = '1.0+1.0/(1+x*y)'
[]
[source_func]
type = ParsedFunction
expression = '-1.0*x*pi*sin((1/2)*x*pi)*cos(2*y*pi) - 0.25*y*pi*sin(2*y*pi)*cos((1/2)*x*pi) + (1.0 + 1.0/(x*y + 1))*(sin((1/2)*x*pi)*sin(2*y*pi) + 1.5) + (17/4)*pi^2*(0.5*x*y + 1.0)*sin((1/2)*x*pi)*sin(2*y*pi) + 0.25*pi*sin(2*y*pi)*cos((1/2)*x*pi)'
[]
[analytic_solution]
type = ParsedFunction
expression = 'sin((1/2)*x*pi)*sin(2*y*pi) + 1.5'
[]
[]
[Postprocessors]
[h]
type = AverageElementSize
execute_on = FINAL
block = 2
[]
[error]
type = ElementL2FunctorError
approximate = u
exact = analytic_solution
execute_on = FINAL
block = 2
[]
[]
[Convergence]
[linear]
type = IterationCountConvergence
max_iterations = 1
converge_at_max_iterations = true
[]
[]
[Executioner]
type = Steady
system_names = u_sys
l_tol = 1e-10
multi_system_fixed_point=true
multi_system_fixed_point_convergence=linear
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
[csv]
type = CSV
execute_on = FINAL
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/cht/flow-around-square-linear-fluidonly.i)
mu = 0.01
rho = 1.1
k = 0.0005
cp = 10
h_conv = 5
advected_interp_method = 'upwind'
[Mesh]
[generated_mesh]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
xmin = 0
ymin = 0
ymax = 0.1
xmax = 0.1
[]
[subdomain1]
type = SubdomainBoundingBoxGenerator
input = generated_mesh
block_name = subdomain1
bottom_left = '0.04 0.04 0'
block_id = 1
top_right = '0.06 0.06 0'
[]
[interface]
type = SideSetsBetweenSubdomainsGenerator
input = subdomain1
primary_block = 0
paired_block = 1
new_boundary = interface
[]
[delete]
type = BlockDeletionGenerator
input = interface
block = 1
[]
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system energy_system'
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = RhieChowMassFlux
u = vel_x
v = vel_y
pressure = pressure
rho = ${rho}
p_diffusion_kernel = p_diffusion
block = 0
[]
[]
[Variables]
[vel_x]
type = MooseLinearVariableFVReal
initial_condition = 0.1
solver_sys = u_system
block = 0
[]
[vel_y]
type = MooseLinearVariableFVReal
solver_sys = v_system
initial_condition = 0.01
block = 0
[]
[pressure]
type = MooseLinearVariableFVReal
solver_sys = pressure_system
initial_condition = 0.2
block = 0
[]
[T_fluid]
type = MooseLinearVariableFVReal
solver_sys = energy_system
initial_condition = 300
block = 0
[]
[]
[LinearFVKernels]
[u_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_x
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'x'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = true
[]
[v_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_y
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'y'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = true
[]
[u_pressure]
type = LinearFVMomentumPressure
variable = vel_x
pressure = pressure
momentum_component = 'x'
[]
[v_pressure]
type = LinearFVMomentumPressure
variable = vel_y
pressure = pressure
momentum_component = 'y'
[]
[p_diffusion]
type = LinearFVAnisotropicDiffusion
variable = pressure
diffusion_tensor = Ainv
use_nonorthogonal_correction = true
[]
[HbyA_divergence]
type = LinearFVDivergence
variable = pressure
face_flux = HbyA
force_boundary_execution = true
[]
[h_advection]
type = LinearFVEnergyAdvection
variable = T_fluid
advected_quantity = temperature
cp = ${cp}
advected_interp_method = ${advected_interp_method}
rhie_chow_user_object = 'rc'
[]
[conduction]
type = LinearFVDiffusion
variable = T_fluid
diffusion_coeff = ${k}
use_nonorthogonal_correction = true
[]
[]
[LinearFVBCs]
[inlet-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_x
functor = '0.1'
[]
[inlet-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_y
functor = '0.0'
[]
[walls-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom interface'
variable = vel_x
functor = 0.0
[]
[walls-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom interface'
variable = vel_y
functor = 0.0
[]
[outlet_p]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'right'
variable = pressure
functor = 1.4
[]
[outlet_u]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_x
use_two_term_expansion = false
boundary = right
[]
[outlet_v]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_y
use_two_term_expansion = false
boundary = right
[]
[inlet_T]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = T_fluid
functor = 300
boundary = 'left'
[]
[walls_T]
type = LinearFVAdvectionDiffusionFunctorNeumannBC
variable = T_fluid
functor = 0.0
boundary = 'top bottom'
[]
[outlet_T]
type = LinearFVAdvectionDiffusionOutflowBC
variable = T_fluid
use_two_term_expansion = false
boundary = right
[]
[fluid_solid]
type = LinearFVConvectiveHeatTransferBC
variable = T_fluid
T_solid = boundary_value
T_fluid = T_fluid
boundary = interface
h = ${h_conv}
[]
[]
[FunctorMaterials]
[rhocpT]
property_name = 'rhocpT'
type = ParsedFunctorMaterial
functor_names = 'T_fluid'
expression = '${rho}*${cp}*T_fluid'
[]
[]
[Functions]
[boundary_value]
type = ConstantFunction
value = 350
[]
[]
[Executioner]
type = SIMPLE
momentum_l_abs_tol = 1e-13
pressure_l_abs_tol = 1e-13
energy_l_abs_tol = 1e-13
momentum_l_tol = 0
pressure_l_tol = 0
energy_l_tol = 0
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
energy_system = 'energy_system'
momentum_equation_relaxation = 0.8
energy_equation_relaxation = 1.0
pressure_variable_relaxation = 0.3
num_iterations = 1000
pressure_absolute_tolerance = 1e-10
momentum_absolute_tolerance = 1e-10
energy_absolute_tolerance = 1e-10
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
energy_petsc_options_iname = '-pc_type -pc_hypre_type'
energy_petsc_options_value = 'hypre boomeramg'
print_fields = false
continue_on_max_its = true
[]
[Outputs]
exodus = true
execute_on = timestep_end
[]
(modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/segregated/channel-drift-flux.i)
mu = 1.0
rho = 10.0
mu_d = 0.1
rho_d = 1.0
l = 2
# 'average' leads to slight oscillations, upwind may be preferred
# This method is selected for consistency with the original nonlinear input
advected_interp_method = 'average'
# TODO remove need for those
cp = 1
k = 1
cp_d = 1
k_d = 1
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = '${fparse l * 5}'
ymin = '${fparse -l / 2}'
ymax = '${fparse l / 2}'
nx = 10
ny = 4
[]
uniform_refine = 0
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system phi_system'
previous_nl_solution_required = true
[]
[Variables]
[vel_x]
type = MooseLinearVariableFVReal
solver_sys = u_system
initial_condition = 1
[]
[vel_y]
type = MooseLinearVariableFVReal
solver_sys = v_system
[]
[pressure]
type = MooseLinearVariableFVReal
solver_sys = pressure_system
[]
[phase_2]
type = MooseLinearVariableFVReal
solver_sys = phi_system
[]
[]
[LinearFVKernels]
[flow_p_diffusion]
type = LinearFVAnisotropicDiffusion
diffusion_tensor = Ainv
use_nonorthogonal_correction = false
variable = pressure
[]
[flow_HbyA_divergence]
type = LinearFVDivergence
face_flux = HbyA
force_boundary_execution = true
variable = pressure
[]
[flow_ins_momentum_flux_x]
type = LinearWCNSFVMomentumFlux
advected_interp_method = ${advected_interp_method}
momentum_component = x
mu = mu_mixture
rhie_chow_user_object = ins_rhie_chow_interpolator
u = vel_x
use_deviatoric_terms = false
use_nonorthogonal_correction = false
v = vel_y
variable = vel_x
[]
[flow_ins_momentum_flux_y]
type = LinearWCNSFVMomentumFlux
advected_interp_method = ${advected_interp_method}
momentum_component = y
mu = mu_mixture
rhie_chow_user_object = ins_rhie_chow_interpolator
u = vel_x
use_deviatoric_terms = false
use_nonorthogonal_correction = false
v = vel_y
variable = vel_y
[]
[mixture_drift_flux_x]
type = LinearWCNSFV2PMomentumDriftFlux
density_interp_method = average
fraction_dispersed = phase_2
momentum_component = x
rhie_chow_user_object = ins_rhie_chow_interpolator
rho_d = ${rho_d}
u_slip = vel_slip_x
v_slip = vel_slip_y
variable = vel_x
[]
[mixture_drift_flux_y]
type = LinearWCNSFV2PMomentumDriftFlux
density_interp_method = average
fraction_dispersed = phase_2
momentum_component = y
rhie_chow_user_object = ins_rhie_chow_interpolator
rho_d = ${rho_d}
u_slip = vel_slip_x
v_slip = vel_slip_y
variable = vel_y
[]
[flow_ins_momentum_pressure_x]
type = LinearFVMomentumPressure
momentum_component = x
pressure = pressure
variable = vel_x
[]
[flow_ins_momentum_pressure_y]
type = LinearFVMomentumPressure
momentum_component = y
pressure = pressure
variable = vel_y
[]
[flow_momentum_friction_0_x]
type = LinearFVMomentumFriction
Darcy_name = Darcy_coefficient_vec
momentum_component = x
mu = mu_mixture
variable = vel_x
[]
[flow_momentum_friction_0_y]
type = LinearFVMomentumFriction
Darcy_name = Darcy_coefficient_vec
momentum_component = y
mu = mu_mixture
variable = vel_y
[]
# Mixture phase equation
[mixture_ins_phase_2_advection]
type = LinearFVScalarAdvection
advected_interp_method = upwind
rhie_chow_user_object = ins_rhie_chow_interpolator
u_slip = vel_slip_x
v_slip = vel_slip_y
variable = phase_2
[]
[mixture_phase_interface_reaction]
type = LinearFVReaction
coeff = 0.1
variable = phase_2
[]
[mixture_phase_interface_source]
type = LinearFVSource
scaling_factor = 0.1
source_density = phase_1
variable = phase_2
[]
[]
[LinearFVBCs]
[vel_x_left]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = left
functor = 1
variable = vel_x
[]
[vel_y_left]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = left
functor = 0
variable = vel_y
[]
[pressure_extrapolation_inlet_left]
type = LinearFVExtrapolatedPressureBC
boundary = left
use_two_term_expansion = true
variable = pressure
[]
[vel_x_right]
type = LinearFVAdvectionDiffusionOutflowBC
boundary = right
use_two_term_expansion = true
variable = vel_x
[]
[vel_y_right]
type = LinearFVAdvectionDiffusionOutflowBC
boundary = right
use_two_term_expansion = true
variable = vel_y
[]
[pressure_right]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = right
functor = 0
variable = pressure
[]
[vel_x_bottom]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = bottom
functor = 0
variable = vel_x
[]
[vel_y_bottom]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = bottom
functor = 0
variable = vel_y
[]
[vel_x_top]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = top
functor = 0
variable = vel_x
[]
[vel_y_top]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = top
functor = 0
variable = vel_y
[]
[pressure_extrapolation_top_bottom]
type = LinearFVExtrapolatedPressureBC
boundary = 'top bottom'
use_two_term_expansion = true
variable = pressure
[]
[phase_2_left]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = left
functor = 0.1
variable = phase_2
[]
[phase_2_right]
type = LinearFVAdvectionDiffusionOutflowBC
boundary = right
use_two_term_expansion = true
variable = phase_2
[]
[]
[FunctorMaterials]
[flow_ins_speed_material]
type = ADVectorMagnitudeFunctorMaterial
execute_on = ALWAYS
outputs = none
vector_magnitude_name = speed
x_functor = vel_x
y_functor = vel_y
[]
[mixture_phase_1_fraction]
type = ParsedFunctorMaterial
execute_on = ALWAYS
expression = '1 - phase_2'
functor_names = phase_2
output_properties = phase_1
outputs = all
property_name = phase_1
[]
[mixture_mixture_material]
type = WCNSLinearFVMixtureFunctorMaterial
execute_on = ALWAYS
limit_phase_fraction = true
outputs = all
phase_1_fraction = phase_2
phase_1_names = '${rho_d} ${mu_d} ${cp_d} ${k_d}'
phase_2_names = '${rho} ${mu} ${cp} ${k}'
prop_names = 'rho_mixture mu_mixture cp_mixture k_mixture'
[]
[mixture_slip_x]
type = WCNSFV2PSlipVelocityFunctorMaterial
execute_on = ALWAYS
gravity = '0 0 0'
linear_coef_name = Darcy_coefficient
momentum_component = x
mu = mu_mixture
outputs = all
particle_diameter = 0.01
rho = ${rho}
rho_d = ${rho_d}
slip_velocity_name = vel_slip_x
u = vel_x
v = vel_y
[]
[mixture_slip_y]
type = WCNSFV2PSlipVelocityFunctorMaterial
execute_on = ALWAYS
gravity = '0 0 0'
linear_coef_name = Darcy_coefficient
momentum_component = y
mu = mu_mixture
outputs = all
particle_diameter = 0.01
rho = ${rho}
rho_d = ${rho_d}
slip_velocity_name = vel_slip_y
u = vel_x
v = vel_y
[]
[mixture_dispersed_drag]
type = NSFVDispersePhaseDragFunctorMaterial
drag_coef_name = Darcy_coefficient
execute_on = ALWAYS
mu = mu_mixture
outputs = all
particle_diameter = 0.01
rho = rho_mixture
u = vel_x
v = vel_y
[]
[]
[UserObjects]
[ins_rhie_chow_interpolator]
type = RhieChowMassFlux
p_diffusion_kernel = flow_p_diffusion
pressure = pressure
rho = rho_mixture
u = vel_x
v = vel_y
[]
[]
[Executioner]
type = SIMPLE
rhie_chow_user_object = 'ins_rhie_chow_interpolator'
# Systems
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
active_scalar_systems = 'phi_system'
momentum_equation_relaxation = 0.8
active_scalar_equation_relaxation = '0.7'
pressure_variable_relaxation = 0.3
# We need to converge the problem to show conservation
num_iterations = 200
pressure_absolute_tolerance = 1e-10
momentum_absolute_tolerance = 1e-10
active_scalar_absolute_tolerance = '1e-10'
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
active_scalar_petsc_options_iname = '-pc_type -pc_hypre_type'
active_scalar_petsc_options_value = 'hypre boomeramg'
momentum_l_abs_tol = 1e-13
pressure_l_abs_tol = 1e-13
active_scalar_l_abs_tol = 1e-13
momentum_l_tol = 0
pressure_l_tol = 0
active_scalar_l_tol = 0
# print_fields = true
continue_on_max_its = true
[]
[Outputs]
csv = true
[]
[Postprocessors]
[Re]
type = ParsedPostprocessor
expression = '10.0 * 2 * 1'
[]
[average_phase2]
type = ElementAverageValue
variable = phase_2
[]
[dp]
type = PressureDrop
boundary = 'left right'
downstream_boundary = right
pressure = pressure
upstream_boundary = left
[]
[max_phase2]
type = ElementExtremeValue
variable = phase_2
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/linear-segregated/2d/2d-boussinesq.i)
mu = 2.6
rho = 1.0
advected_interp_method = 'average'
cp = 300
k = 20
alpha_b = 1e-4
[Mesh]
[mesh]
type = CartesianMeshGenerator
dim = 2
dx = '1.'
dy = '0.2'
ix = '10'
iy = '5'
[]
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system energy_system'
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = RhieChowMassFlux
u = vel_x
v = vel_y
pressure = pressure
rho = ${rho}
p_diffusion_kernel = p_diffusion
[]
[]
[Variables]
[vel_x]
type = MooseLinearVariableFVReal
initial_condition = 0.5
solver_sys = u_system
[]
[vel_y]
type = MooseLinearVariableFVReal
solver_sys = v_system
initial_condition = 0.0
[]
[pressure]
type = MooseLinearVariableFVReal
solver_sys = pressure_system
initial_condition = 0.2
[]
[T]
type = MooseLinearVariableFVReal
solver_sys = energy_system
initial_condition = 300
[]
[]
[LinearFVKernels]
[u_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_x
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'x'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[v_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_y
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'y'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[u_pressure]
type = LinearFVMomentumPressure
variable = vel_x
pressure = pressure
momentum_component = 'x'
[]
[v_pressure]
type = LinearFVMomentumPressure
variable = vel_y
pressure = pressure
momentum_component = 'y'
[]
[u_boussinesq]
type = LinearFVMomentumBoussinesq
variable = vel_x
rho = ${rho}
gravity = '0 -9.81 0'
alpha_name = ${alpha_b}
ref_temperature = 300.0
T_fluid = T
momentum_component = 'x'
[]
[v_boussinesq]
type = LinearFVMomentumBoussinesq
variable = vel_y
rho = ${rho}
gravity = '0 -9.81 0'
alpha_name = ${alpha_b}
ref_temperature = 300.0
T_fluid = T
momentum_component = 'y'
[]
[p_diffusion]
type = LinearFVAnisotropicDiffusion
variable = pressure
diffusion_tensor = Ainv
use_nonorthogonal_correction = false
[]
[HbyA_divergence]
type = LinearFVDivergence
variable = pressure
face_flux = HbyA
force_boundary_execution = true
[]
[h_advection]
type = LinearFVEnergyAdvection
variable = T
advected_quantity = temperature
cp = ${cp}
advected_interp_method = ${advected_interp_method}
rhie_chow_user_object = 'rc'
[]
[conduction]
type = LinearFVDiffusion
variable = T
diffusion_coeff = ${k}
use_nonorthogonal_correction = false
[]
[]
[FunctorMaterials]
[constant_functors]
type = GenericFunctorMaterial
prop_names = 'cp alpha_b'
prop_values = '${cp} ${alpha_b}'
[]
[]
[LinearFVBCs]
[inlet-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_x
functor = '1.1'
[]
[inlet-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_y
functor = '0.0'
[]
[walls-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom'
variable = vel_x
functor = 0.0
[]
[walls-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom'
variable = vel_y
functor = 0.0
[]
[outlet_p]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'right'
variable = pressure
functor = 1.4
[]
[outlet_u]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_x
use_two_term_expansion = false
boundary = right
[]
[outlet_v]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_y
use_two_term_expansion = false
boundary = right
[]
[inlet_top_T]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = T
functor = ${fparse 300.0}
boundary = 'left top'
[]
[bottom_T]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = T
functor = ${fparse 350.0}
boundary = bottom
[]
[outlet_T]
type = LinearFVAdvectionDiffusionOutflowBC
variable = T
use_two_term_expansion = false
boundary = right
[]
[]
[Executioner]
type = SIMPLE
momentum_l_abs_tol = 1e-10
pressure_l_abs_tol = 1e-10
energy_l_abs_tol = 1e-10
momentum_l_tol = 0
pressure_l_tol = 0
energy_l_tol = 0
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
energy_system = 'energy_system'
momentum_equation_relaxation = 0.8
energy_equation_relaxation = 0.9
pressure_variable_relaxation = 0.3
num_iterations = 200
pressure_absolute_tolerance = 1e-10
momentum_absolute_tolerance = 1e-10
energy_absolute_tolerance = 1e-10
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
energy_petsc_options_iname = '-pc_type -pc_hypre_type'
energy_petsc_options_value = 'hypre boomeramg'
print_fields = false
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/linear-segregated/2d-heated/fluid.i)
mu = 2.6
rho = 1.0
advected_interp_method = 'upwind'
cp = 1000
k = 1
[Mesh]
[mesh]
type = CartesianMeshGenerator
dim = 2
dx = '0.25 0.25'
dy = '0.2'
ix = '5 5'
iy = '5'
subdomain_id = '0 1'
[]
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system energy_system'
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = RhieChowMassFlux
u = vel_x
v = vel_y
pressure = pressure
rho = ${rho}
p_diffusion_kernel = p_diffusion
[]
[]
[Variables]
[vel_x]
type = MooseLinearVariableFVReal
initial_condition = 0.5
solver_sys = u_system
[]
[vel_y]
type = MooseLinearVariableFVReal
solver_sys = v_system
initial_condition = 0.0
[]
[pressure]
type = MooseLinearVariableFVReal
solver_sys = pressure_system
initial_condition = 0.2
[]
[T_fluid]
type = MooseLinearVariableFVReal
solver_sys = energy_system
initial_condition = 300
[]
[]
[LinearFVKernels]
[u_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_x
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'x'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[v_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_y
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'y'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[u_pressure]
type = LinearFVMomentumPressure
variable = vel_x
pressure = pressure
momentum_component = 'x'
[]
[v_pressure]
type = LinearFVMomentumPressure
variable = vel_y
pressure = pressure
momentum_component = 'y'
[]
[p_diffusion]
type = LinearFVAnisotropicDiffusion
variable = pressure
diffusion_tensor = Ainv
use_nonorthogonal_correction = false
[]
[HbyA_divergence]
type = LinearFVDivergence
variable = pressure
face_flux = HbyA
force_boundary_execution = true
[]
[h_advection]
type = LinearFVEnergyAdvection
variable = T_fluid
advected_quantity = temperature
cp = ${cp}
advected_interp_method = ${advected_interp_method}
rhie_chow_user_object = 'rc'
[]
[conduction]
type = LinearFVDiffusion
variable = T_fluid
diffusion_coeff = ${k}
use_nonorthogonal_correction = false
[]
[heat_exchange]
type = LinearFVVolumetricHeatTransfer
variable = T_fluid
h_solid_fluid = 100
T_fluid = T_fluid
T_solid = T_solid
is_solid = false
block = 1
[]
[]
[FunctorMaterials]
[constant_functors]
type = GenericFunctorMaterial
prop_names = 'cp'
prop_values = '${cp}'
[]
[]
[LinearFVBCs]
[inlet-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_x
functor = '1.1'
[]
[inlet-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_y
functor = '0.0'
[]
[walls-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom'
variable = vel_x
functor = 0.0
[]
[walls-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom'
variable = vel_y
functor = 0.0
[]
[outlet_p]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'right'
variable = pressure
functor = 1.4
[]
[outlet_u]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_x
use_two_term_expansion = false
boundary = right
[]
[outlet_v]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_y
use_two_term_expansion = false
boundary = right
[]
[inlet_wall_T]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = T_fluid
functor = 300
boundary = 'left top bottom'
[]
[outlet_T]
type = LinearFVAdvectionDiffusionOutflowBC
variable = T_fluid
use_two_term_expansion = false
boundary = right
[]
[]
[AuxVariables]
[T_solid]
type = MooseLinearVariableFVReal
initial_condition = 300
block = 1
[]
[]
[MultiApps]
inactive = 'solid'
[solid]
type = FullSolveMultiApp
input_files = solid.i
execute_on = timestep_begin
no_restore = true
[]
[]
[Transfers]
inactive = 'from_solid to_solid'
[from_solid]
type = MultiAppGeneralFieldShapeEvaluationTransfer
from_multi_app = solid
source_variable = 'T_solid'
variable = 'T_solid'
execute_on = timestep_begin
from_blocks = 1
[]
[to_solid]
type = MultiAppGeneralFieldShapeEvaluationTransfer
to_multi_app = solid
source_variable = 'T_fluid'
variable = 'T_fluid'
execute_on = timestep_begin
to_blocks = 1
[]
[]
[Executioner]
type = SIMPLE
momentum_l_abs_tol = 1e-13
pressure_l_abs_tol = 1e-13
energy_l_abs_tol = 1e-13
momentum_l_tol = 0
pressure_l_tol = 0
energy_l_tol = 0
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
energy_system = 'energy_system'
momentum_equation_relaxation = 0.8
energy_equation_relaxation = 0.9
pressure_variable_relaxation = 0.3
num_iterations = 20
pressure_absolute_tolerance = 1e-10
momentum_absolute_tolerance = 1e-10
energy_absolute_tolerance = 1e-10
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
energy_petsc_options_iname = '-pc_type -pc_hypre_type'
energy_petsc_options_value = 'hypre boomeramg'
print_fields = false
continue_on_max_its = true
[]
[Outputs]
exodus = true
execute_on = timestep_end
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/segregated-comparison/segregated-linear.i)
mu = 2.6
rho = 1.0
advected_interp_method = 'average'
[Mesh]
[mesh]
type = CartesianMeshGenerator
dim = 2
dx = '0.3'
dy = '0.3'
ix = '3'
iy = '3'
[]
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system'
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = RhieChowMassFlux
u = vel_x
v = vel_y
pressure = pressure
rho = ${rho}
p_diffusion_kernel = p_diffusion
[]
[]
[Variables]
[vel_x]
type = MooseLinearVariableFVReal
initial_condition = 0.5
solver_sys = u_system
[]
[vel_y]
type = MooseLinearVariableFVReal
solver_sys = v_system
initial_condition = 0.0
[]
[pressure]
type = MooseLinearVariableFVReal
solver_sys = pressure_system
initial_condition = 0.2
[]
[]
[LinearFVKernels]
[u_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_x
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'x'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[v_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_y
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'y'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[u_pressure]
type = LinearFVMomentumPressure
variable = vel_x
pressure = pressure
momentum_component = 'x'
[]
[v_pressure]
type = LinearFVMomentumPressure
variable = vel_y
pressure = pressure
momentum_component = 'y'
[]
[p_diffusion]
type = LinearFVAnisotropicDiffusion
variable = pressure
diffusion_tensor = Ainv
use_nonorthogonal_correction = false
[]
[HbyA_divergence]
type = LinearFVDivergence
variable = pressure
face_flux = HbyA
force_boundary_execution = true
[]
[]
[LinearFVBCs]
[inlet-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_x
functor = '1.1'
[]
[inlet-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_y
functor = '0.0'
[]
[walls-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom'
variable = vel_x
functor = 0.0
[]
[walls-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom'
variable = vel_y
functor = 0.0
[]
[outlet_p]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'right'
variable = pressure
functor = 1.4
[]
[outlet_u]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_x
use_two_term_expansion = false
boundary = right
[]
[outlet_v]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_y
use_two_term_expansion = false
boundary = right
[]
[]
[Executioner]
type = SIMPLE
momentum_l_abs_tol = 1e-10
pressure_l_abs_tol = 1e-10
momentum_l_tol = 0
pressure_l_tol = 0
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
momentum_equation_relaxation = 0.8
pressure_variable_relaxation = 0.3
num_iterations = 2
pressure_absolute_tolerance = 1e-10
momentum_absolute_tolerance = 1e-10
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
print_fields = false
[]
[Outputs]
exodus = true
execute_on = TIMESTEP_END
[]
(test/tests/linearfvkernels/anisotropic-diffusion/anisotropic-diffusion-2d.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 1
ymax = 0.5
[]
[]
[Problem]
linear_sys_names = 'u_sys'
[]
[Variables]
[u]
type = MooseLinearVariableFVReal
solver_sys = 'u_sys'
initial_condition = 1.0
[]
[]
[LinearFVKernels]
[diffusion]
type = LinearFVAnisotropicDiffusion
variable = u
diffusion_tensor = diffusivity_tensor
use_nonorthogonal_correction = false
[]
[source]
type = LinearFVSource
variable = u
source_density = source_func
[]
[]
[LinearFVBCs]
[dir]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = u
boundary = "left right top bottom"
functor = analytic_solution
[]
[]
[FunctorMaterials]
[diff_tensor]
type = GenericVectorFunctorMaterial
prop_names = diffusivity_tensor
prop_values = 'coeff_func_x coeff_func_y 0.0'
[]
[]
[Functions]
[coeff_func_x]
type = ParsedFunction
expression = '1+0.5*x*y'
[]
[coeff_func_y]
type = ParsedFunction
expression = '1+x*y'
[]
[source_func]
type = ParsedFunction
expression = '(1.5-y*y)*(2+2*x*y)+(1.5-x*x)*(2+4*x*y)'
[]
[analytic_solution]
type = ParsedFunction
expression = '(1.5-x*x)*(1.5-y*y)'
[]
[]
[Postprocessors]
[h]
type = AverageElementSize
execute_on = FINAL
[]
[error]
type = ElementL2FunctorError
approximate = u
exact = analytic_solution
execute_on = FINAL
[]
[]
[Convergence]
[linear]
type = IterationCountConvergence
max_iterations = 1
converge_at_max_iterations = true
[]
[]
[Executioner]
type = Steady
system_names = u_sys
l_tol = 1e-10
multi_system_fixed_point=true
multi_system_fixed_point_convergence=linear
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
[csv]
type = CSV
execute_on = FINAL
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/linear-segregated/2d-scalar/channel.i)
mu = 2.6
rho = 1.0
advected_interp_method = 'upwind'
k1 = 0.1
k2 = 0.2
[Mesh]
[mesh]
type = CartesianMeshGenerator
dim = 2
dx = '0.25 0.25'
dy = '0.2'
ix = '5 5'
iy = '5'
subdomain_id = '0 1'
[]
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system s1_system s2_system'
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = RhieChowMassFlux
u = vel_x
v = vel_y
pressure = pressure
rho = ${rho}
p_diffusion_kernel = p_diffusion
[]
[]
[Variables]
[vel_x]
type = MooseLinearVariableFVReal
initial_condition = 0.5
solver_sys = u_system
[]
[vel_y]
type = MooseLinearVariableFVReal
solver_sys = v_system
initial_condition = 0.0
[]
[pressure]
type = MooseLinearVariableFVReal
solver_sys = pressure_system
initial_condition = 0.2
[]
[scalar1]
type = MooseLinearVariableFVReal
solver_sys = s1_system
initial_condition = 1.1
[]
[scalar2]
type = MooseLinearVariableFVReal
solver_sys = s2_system
initial_condition = 3
[]
[]
[LinearFVKernels]
[u_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_x
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'x'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[v_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_y
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'y'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[u_pressure]
type = LinearFVMomentumPressure
variable = vel_x
pressure = pressure
momentum_component = 'x'
[]
[v_pressure]
type = LinearFVMomentumPressure
variable = vel_y
pressure = pressure
momentum_component = 'y'
[]
[p_diffusion]
type = LinearFVAnisotropicDiffusion
variable = pressure
diffusion_tensor = Ainv
use_nonorthogonal_correction = false
[]
[HbyA_divergence]
type = LinearFVDivergence
variable = pressure
face_flux = HbyA
force_boundary_execution = true
[]
[s1_advection]
type = LinearFVScalarAdvection
variable = scalar1
advected_interp_method = ${advected_interp_method}
rhie_chow_user_object = 'rc'
[]
[s1_diffusion]
type = LinearFVDiffusion
variable = scalar1
diffusion_coeff = ${k1}
use_nonorthogonal_correction = false
[]
[s2_diffusion]
type = LinearFVScalarAdvection
variable = scalar2
advected_interp_method = ${advected_interp_method}
rhie_chow_user_object = 'rc'
[]
[s2_conduction]
type = LinearFVDiffusion
variable = scalar2
diffusion_coeff = ${k2}
use_nonorthogonal_correction = false
[]
[]
[LinearFVBCs]
[inlet-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_x
functor = '1.1'
[]
[inlet-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_y
functor = '0.0'
[]
[walls-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom'
variable = vel_x
functor = 0.0
[]
[walls-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom'
variable = vel_y
functor = 0.0
[]
[outlet_p]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'right'
variable = pressure
functor = 1.4
[]
[outlet_u]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_x
use_two_term_expansion = false
boundary = right
[]
[outlet_v]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_y
use_two_term_expansion = false
boundary = right
[]
[inlet_wall_scalar1]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = scalar1
functor = 1
boundary = 'left'
[]
[outlet_scalar1]
type = LinearFVAdvectionDiffusionOutflowBC
variable = scalar1
use_two_term_expansion = false
boundary = right
[]
[inlet_wall_scalar2]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = scalar2
functor = 2
boundary = 'left'
[]
[outlet_scalar2]
type = LinearFVAdvectionDiffusionOutflowBC
variable = scalar2
use_two_term_expansion = false
boundary = right
[]
[]
[Executioner]
type = SIMPLE
momentum_l_abs_tol = 1e-13
pressure_l_abs_tol = 1e-13
passive_scalar_l_abs_tol = 1e-13
momentum_l_tol = 0
pressure_l_tol = 0
passive_scalar_l_tol = 0
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
passive_scalar_systems = 's1_system s2_system'
momentum_equation_relaxation = 0.8
passive_scalar_equation_relaxation = '0.9 0.9'
pressure_variable_relaxation = 0.3
# We need to converge the problem to show conservation
num_iterations = 200
pressure_absolute_tolerance = 1e-10
momentum_absolute_tolerance = 1e-10
# The solution being flat, the normalization factor based on fluxes goes to
# 0. The convergence criteria being multiplied by said factor, we won't do any
# better than this. For a non-flat solution, use tighter tolerances
passive_scalar_absolute_tolerance = '1e-2 1e-2'
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
passive_scalar_petsc_options_iname = '-pc_type -pc_hypre_type'
passive_scalar_petsc_options_value = 'hypre boomeramg'
print_fields = false
continue_on_max_its = true
[]
[Outputs]
exodus = true
execute_on = timestep_end
hide = 'pressure vel_x vel_y'
[]
(modules/navier_stokes/test/tests/finite_volume/ins/mms/linear-segregated/2d-vortex/2d-vortex.i)
mu = 1
rho = 1
advected_interp_method = 'average'
[Problem]
linear_sys_names = 'u_system v_system pressure_system'
previous_nl_solution_required = true
[]
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 2
[]
[]
[UserObjects]
[rc]
type = RhieChowMassFlux
u = vel_x
v = vel_y
pressure = pressure
rho = ${rho}
p_diffusion_kernel = p_diffusion
[]
[]
[Variables]
[vel_x]
type = MooseLinearVariableFVReal
initial_condition = 0.0
solver_sys = u_system
[]
[vel_y]
type = MooseLinearVariableFVReal
solver_sys = v_system
initial_condition = 0.0
[]
[pressure]
type = MooseLinearVariableFVReal
solver_sys = pressure_system
initial_condition = 0
[]
[]
[LinearFVKernels]
[u_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_x
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'x'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[v_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_y
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'y'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[u_pressure]
type = LinearFVMomentumPressure
variable = vel_x
pressure = pressure
momentum_component = 'x'
[]
[v_pressure]
type = LinearFVMomentumPressure
variable = vel_y
pressure = pressure
momentum_component = 'y'
[]
[u_forcing]
type = LinearFVSource
variable = vel_x
source_density = forcing_u
[]
[v_forcing]
type = LinearFVSource
variable = vel_y
source_density = forcing_v
[]
[p_diffusion]
type = LinearFVAnisotropicDiffusion
variable = pressure
diffusion_tensor = Ainv
use_nonorthogonal_correction = false
use_nonorthogonal_correction_on_boundary = false
[]
[HbyA_divergence]
type = LinearFVDivergence
variable = pressure
face_flux = HbyA
force_boundary_execution = true
[]
[]
[LinearFVBCs]
[no-slip-wall-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left right top bottom'
variable = vel_x
functor = '0'
[]
[no-slip-wall-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left right top bottom'
variable = vel_y
functor = '0'
[]
[pressure-extrapolation]
type = LinearFVExtrapolatedPressureBC
boundary = 'left right top bottom'
variable = pressure
use_two_term_expansion = true
[]
[]
[Functions]
[exact_u]
type = ParsedFunction
expression = 'x^2*(1-x)^2*(2*y-6*y^2+4*y^3)'
[]
[exact_v]
type = ParsedFunction
expression = '-y^2*(1-y)^2*(2*x-6*x^2+4*x^3)'
[]
[exact_p]
type = ParsedFunction
expression = 'x*(1-x)'
[]
[forcing_u]
type = ParsedFunction
expression = '-4*mu*(-1+2*y)*(y^2-6*x*y^2+6*x^2*y^2-y+6*x*y-6*x^2*y+3*x^2-6*x^3+3*x^4)+1-2*x+rho*4*x^3'
'*y^2*(2*y^2-2*y+1)*(y-1)^2*(-1+2*x)*(x-1)^3'
symbol_names = 'mu rho'
symbol_values = '${mu} ${rho}'
[]
[forcing_v]
type = ParsedFunction
expression = '4*mu*(-1+2*x)*(x^2-6*y*x^2+6*x^2*y^2-x+6*x*y-6*x*y^2+3*y^2-6*y^3+3*y^4)+rho*4*y^3*x^2*(2'
'*x^2-2*x+1)*(x-1)^2*(-1+2*y)*(y-1)^3'
symbol_names = 'mu rho'
symbol_values = '${mu} ${rho}'
[]
[]
[Executioner]
type = SIMPLE
momentum_l_abs_tol = 1e-8
pressure_l_abs_tol = 1e-8
momentum_l_tol = 0
pressure_l_tol = 0
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
momentum_equation_relaxation = 0.8
pressure_variable_relaxation = 0.3
num_iterations = 2000
pressure_absolute_tolerance = 1e-8
momentum_absolute_tolerance = 1e-8
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
print_fields = false
pin_pressure = true
pressure_pin_value = 0.25
pressure_pin_point = '0.5 0.5 0.0'
[]
[Outputs]
exodus = true
[csv]
type = CSV
execute_on = FINAL
[]
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'csv'
execute_on = FINAL
[]
[L2u]
type = ElementL2FunctorError
approximate = vel_x
exact = exact_u
outputs = 'csv'
execute_on = FINAL
[]
[L2v]
type = ElementL2FunctorError
approximate = vel_y
exact = exact_v
outputs = 'csv'
execute_on = FINAL
[]
[L2p]
approximate = pressure
exact = exact_p
type = ElementL2FunctorError
outputs = 'csv'
execute_on = FINAL
[]
[]
(modules/navier_stokes/examples/flow-over-circle/flow_over_circle_linearfv.i)
[Problem]
linear_sys_names = 'u_system v_system pressure_system'
previous_nl_solution_required = true
[]
[Functions]
[inlet_function]
type = ParsedFunction
expression = '4*U*(y-ymin)*(ymax-y)/(ymax-ymin)/(ymax-ymin)'
symbol_names = 'U ymax ymin'
symbol_values = '${inlet_velocity} ${y_max} ${y_min}'
[]
[]
[UserObjects]
[rc]
type = RhieChowMassFlux
u = vel_x
v = vel_y
pressure = pressure
rho = ${rho}
p_diffusion_kernel = p_diffusion
[]
[]
[Variables]
[vel_x]
type = MooseLinearVariableFVReal
solver_sys = u_system
[]
[vel_y]
type = MooseLinearVariableFVReal
solver_sys = v_system
[]
[pressure]
type = MooseLinearVariableFVReal
initial_condition = 0
solver_sys = pressure_system
[]
[]
[LinearFVKernels]
[u_time]
type = LinearFVTimeDerivative
variable = vel_x
factor = ${rho}
[]
[u_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_x
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'x'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = true
[]
[u_pressure]
type = LinearFVMomentumPressure
variable = vel_x
pressure = pressure
momentum_component = 'x'
[]
[v_time]
type = LinearFVTimeDerivative
variable = vel_y
factor = ${rho}
[]
[v_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_y
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'y'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = true
[]
[v_pressure]
type = LinearFVMomentumPressure
variable = vel_y
pressure = pressure
momentum_component = 'y'
[]
[p_diffusion]
type = LinearFVAnisotropicDiffusion
variable = pressure
diffusion_tensor = Ainv
use_nonorthogonal_correction = true
[]
[HbyA_divergence]
type = LinearFVDivergence
variable = pressure
face_flux = HbyA
force_boundary_execution = true
[]
[]
[LinearFVBCs]
[inlet_x]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = vel_x
boundary = 'left_boundary'
functor = 'inlet_function'
[]
[inlet_y]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = vel_y
boundary = 'left_boundary'
functor = 0
[]
[circle_x]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = vel_x
boundary = 'circle'
functor = 0
[]
[circle_y]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = vel_y
boundary = 'circle'
functor = 0
[]
[walls_x]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = vel_x
boundary = 'top_boundary bottom_boundary'
functor = 0
[]
[walls_y]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = vel_y
boundary = 'top_boundary bottom_boundary'
functor = 0
[]
[outlet_p]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'right_boundary'
variable = pressure
functor = 0
[]
[outlet_u]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_x
use_two_term_expansion = false
boundary = 'right_boundary'
[]
[outlet_v]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_y
use_two_term_expansion = false
boundary = 'right_boundary'
[]
[]
[Postprocessors]
[drag_force]
type = IntegralDirectedSurfaceForce
vel_x = vel_x
vel_y = vel_y
mu = ${mu}
pressure = pressure
principal_direction = '1 0 0'
boundary = 'circle'
outputs = none
execute_on = 'INITIAL TIMESTEP_END'
[]
[drag_coeff]
type = ParsedPostprocessor
expression = '2*drag_force/rho/(avgvel*avgvel)/D'
constant_names = 'rho avgvel D'
constant_expressions = '${rho} ${fparse 2/3*inlet_velocity} ${fparse 2*circle_radius}'
pp_names = 'drag_force'
execute_on = 'INITIAL TIMESTEP_END'
[]
[lift_force]
type = IntegralDirectedSurfaceForce
vel_x = vel_x
vel_y = vel_y
mu = ${mu}
pressure = pressure
principal_direction = '0 1 0'
boundary = 'circle'
outputs = none
execute_on = 'INITIAL TIMESTEP_END'
[]
[lift_coeff]
type = ParsedPostprocessor
expression = '2*lift_force/rho/(avgvel*avgvel)/D'
constant_names = 'rho avgvel D'
constant_expressions = '${rho} ${fparse 2/3*inlet_velocity} ${fparse 2*circle_radius}'
pp_names = 'lift_force'
execute_on = 'INITIAL TIMESTEP_END'
[]
[]
[Executioner]
type = PIMPLE
momentum_l_abs_tol = 1e-12
pressure_l_abs_tol = 1e-12
momentum_l_tol = 1e-12
pressure_l_tol = 1e-12
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
momentum_equation_relaxation = 0.90
pressure_variable_relaxation = 0.4
num_iterations = 100
pressure_absolute_tolerance = 1e-10
momentum_absolute_tolerance = 1e-10
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
print_fields = false
continue_on_max_its = true
dt = 0.01
num_steps = 500
[]
[Outputs]
exodus = true
csv = true
[]
(test/tests/linearfvkernels/diffusion/diffusion-2d-rz.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 1
ymax = 0.5
[]
coord_type = RZ
rz_coord_axis = Y
[]
[Problem]
linear_sys_names = 'u_sys'
[]
[Variables]
[u]
type = MooseLinearVariableFVReal
solver_sys = 'u_sys'
initial_condition = 1.0
[]
[]
[LinearFVKernels]
[diffusion]
type = LinearFVDiffusion
variable = u
diffusion_coeff = coeff_func
use_nonorthogonal_correction = true
[]
[source]
type = LinearFVSource
variable = u
source_density = source_func
[]
[]
[LinearFVBCs]
[dir]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = u
boundary = "left right top bottom"
functor = analytic_solution
[]
[]
[Functions]
[coeff_func]
type = ParsedFunction
expression = '1+0.5*x*y'
[]
[source_func]
type = ParsedFunction
expression = '-(-1.0*x^2*y*(1.5 - x^2) + x*(1.5 - x^2)*(-1.0*x*y - 2))/x - (-1.0*x^2*y*(1.5 - y^2) - 4*x*(1.5 - y^2)*(0.5*x*y + 1))/x'
[]
[analytic_solution]
type = ParsedFunction
expression = '(1.5-x*x)*(1.5-y*y)'
[]
[]
[Postprocessors]
[h]
type = AverageElementSize
execute_on = FINAL
[]
[error]
type = ElementL2FunctorError
approximate = u
exact = analytic_solution
execute_on = FINAL
[]
[]
[Convergence]
[linear]
type = IterationCountConvergence
max_iterations = 1
converge_at_max_iterations = true
[]
[]
[Executioner]
type = Steady
system_names = u_sys
l_tol = 1e-10
multi_system_fixed_point=true
multi_system_fixed_point_convergence=linear
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
[csv]
type = CSV
execute_on = FINAL
[]
[exo]
type = Exodus
execute_on = FINAL
[]
[]
(test/tests/linearfvkernels/advection/advection-1d.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
nx = 2
[]
[]
[Problem]
linear_sys_names = 'u_sys'
[]
[Variables]
[u]
type = MooseLinearVariableFVReal
solver_sys = 'u_sys'
initial_condition = 1.0
[]
[]
[LinearFVKernels]
[advection]
type = LinearFVAdvection
variable = u
velocity = "0.5 0 0"
advected_interp_method = upwind
[]
[source]
type = LinearFVSource
variable = u
source_density = source_func
[]
[]
[LinearFVBCs]
[inflow]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = u
boundary = "left"
functor = analytic_solution
[]
[outflow]
type = LinearFVAdvectionDiffusionOutflowBC
variable = u
boundary = "right"
use_two_term_expansion = false
[]
[]
[Functions]
[source_func]
type = ParsedFunction
expression = '0.5*x'
[]
[analytic_solution]
type = ParsedFunction
expression = '0.5+0.5*x*x'
[]
[]
[Postprocessors]
[error]
type = ElementL2FunctorError
approximate = u
exact = analytic_solution
execute_on = FINAL
[]
[h]
type = AverageElementSize
execute_on = FINAL
[]
[]
[Convergence]
[linear]
type = IterationCountConvergence
max_iterations = 1
converge_at_max_iterations = true
[]
[]
[Executioner]
type = Steady
system_names = u_sys
l_tol = 1e-10
multi_system_fixed_point=true
multi_system_fixed_point_convergence=linear
[]
[Outputs]
[csv]
type = CSV
execute_on = FINAL
[]
[]
(test/tests/outputs/debug/show_execution_linear_fv_flux.i)
[Mesh]
[gen_mesh]
type = GeneratedMeshGenerator
dim = 1
xmin = 0
xmax = 10
nx = 50
[]
[left]
type = ParsedSubdomainMeshGenerator
input = 'gen_mesh'
combinatorial_geometry = 'x < 0.5'
block_id = '1'
[]
[]
[Problem]
linear_sys_names = 'u_sys'
[]
[Variables]
[u]
type = MooseLinearVariableFVReal
solver_sys = 'u_sys'
[]
[]
[LinearFVKernels]
[diffusion_1]
type = LinearFVDiffusion
variable = u
diffusion_coeff = 1.5
block = 0
[]
[diffusion_2]
type = LinearFVDiffusion
variable = u
diffusion_coeff = 2.5
block = 1
[]
[source_1]
type = LinearFVSource
variable = u
source_density = 3.5
block = 0
[]
[source_2]
type = LinearFVSource
variable = u
source_density = 4.5
block = 1
[]
[]
[LinearFVBCs]
[left_bc]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = u
boundary = 'left right'
functor = 0
[]
[]
[Executioner]
type = Steady
system_names = u_sys
l_tol = 1e-10
[]
[Debug]
show_execution_order = 'NONLINEAR'
[]
(test/tests/multisystem/picard/linearfv_nonlinearfv/same_input.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
nx = 6
[]
[]
[Problem]
nl_sys_names = 'v_sys'
linear_sys_names = 'u_sys'
[]
[Variables]
[v]
type = MooseVariableFVReal
initial_condition = 2.0
solver_sys = v_sys
[]
[u]
type = MooseLinearVariableFVReal
solver_sys = 'u_sys'
initial_condition = 1.0
[]
[]
[FVKernels]
[diffusion]
type = FVDiffusion
variable = v
coeff = u
[]
[source]
type = FVBodyForce
variable = v
function = 3
[]
[]
[LinearFVKernels]
[diffusion]
type = LinearFVDiffusion
variable = u
diffusion_coeff = v
[]
[source]
type = LinearFVSource
variable = u
source_density = 1
[]
[]
[FVBCs]
[dir]
type = FVFunctorDirichletBC
variable = v
boundary = "left right"
functor = 2
[]
[]
[LinearFVBCs]
[dir]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = u
boundary = "left right"
functor = 1
[]
[]
[Convergence]
[linear]
type = IterationCountConvergence
max_iterations = 6
converge_at_max_iterations = true
[]
[]
[Executioner]
type = Steady
system_names = 'v_sys u_sys'
l_abs_tol = 1e-12
l_tol = 1e-10
nl_abs_tol = 1e-10
multi_system_fixed_point=true
multi_system_fixed_point_convergence=linear
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
execute_on = timestep_end
[]
(test/tests/tag/tag-linearfv.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
nx = 3
[]
[]
[Problem]
linear_sys_names = 'u_sys v_sys'
extra_tag_matrices = 'mat_tag_u; mat_tag_v'
extra_tag_vectors = 'vec_tag_u; vec_tag_v'
[]
[Variables]
[u]
type = MooseLinearVariableFVReal
initial_condition = 1.0
solver_sys = u_sys
[]
[v]
type = MooseLinearVariableFVReal
initial_condition = 0.5
solver_sys = v_sys
[]
[]
[LinearFVKernels]
[diffusion]
type = LinearFVDiffusion
variable = u
diffusion_coeff = 2.0
[]
[reaction]
type = LinearFVReaction
variable = u
coeff = 3.0
matrix_tags = 'system mat_tag_u'
[]
[source]
type = LinearFVSource
variable = u
source_density = 60.0
vector_tags = 'rhs vec_tag_u'
[]
[diffusion_v]
type = LinearFVDiffusion
variable = v
diffusion_coeff = 1.0
[]
[reaction_v]
type = LinearFVReaction
variable = v
coeff = 1.5
matrix_tags = 'system mat_tag_v'
[]
[source_v]
type = LinearFVSource
variable = v
source_density = 20.0
vector_tags = 'rhs vec_tag_v'
[]
[]
[LinearFVBCs]
[left_u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = u
boundary = left
functor = 1.0
[]
[right_u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = u
boundary = right
functor = 3.0
[]
[left_v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = v
boundary = left
functor = 1.0
[]
[right_v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = v
boundary = right
functor = 3.0
[]
[]
[AuxVariables]
[soln_u_dof]
type = MooseLinearVariableFVReal
[]
[soln_u]
type = MooseLinearVariableFVReal
[]
[rhs_u_dof]
type = MooseLinearVariableFVReal
[]
[rhs_u]
type = MooseLinearVariableFVReal
[]
[vector_tag_u]
type = MooseLinearVariableFVReal
[]
[matrix_u_diag]
type = MooseLinearVariableFVReal
[]
[soln_v_dof]
type = MooseLinearVariableFVReal
[]
[soln_v]
type = MooseLinearVariableFVReal
[]
[rhs_v_dof]
type = MooseLinearVariableFVReal
[]
[rhs_v]
type = MooseLinearVariableFVReal
[]
[vector_tag_v]
type = MooseLinearVariableFVReal
[]
[matrix_v_diag]
type = MooseLinearVariableFVReal
[]
[]
[AuxKernels]
[soln_u_dof]
type = TagVectorDofValueAux
variable = soln_u_dof
v = u
vector_tag = 'solution'
[]
[soln_u]
type = TagVectorAux
variable = soln_u
v = u
vector_tag = 'solution'
[]
[rhs_u_dof]
type = TagVectorDofValueAux
variable = rhs_u_dof
v = u
vector_tag = 'rhs'
[]
[rhs_u]
type = TagVectorAux
variable = rhs_u
v = u
vector_tag = 'rhs'
[]
[extra_vector_u_dof]
type = TagVectorDofValueAux
variable = vector_tag_u
v = u
vector_tag = 'vec_tag_u'
[]
[extra_vector_u]
type = TagVectorAux
variable = vector_tag_u
v = u
vector_tag = 'vec_tag_u'
[]
[extra_matrix_u]
type = TagMatrixAux
variable = matrix_u_diag
v = u
matrix_tag = 'mat_tag_u'
[]
[soln_v_dof]
type = TagVectorDofValueAux
variable = soln_v_dof
v = v
vector_tag = 'solution'
[]
[soln_v]
type = TagVectorAux
variable = soln_v
v = v
vector_tag = 'solution'
[]
[rhs_v_dof]
type = TagVectorDofValueAux
variable = rhs_v_dof
v = v
vector_tag = 'rhs'
[]
[rhs_v]
type = TagVectorAux
variable = rhs_v
v = v
vector_tag = 'rhs'
[]
[extra_vector_v_dof]
type = TagVectorDofValueAux
variable = vector_tag_v
v = v
vector_tag = 'vec_tag_v'
[]
[extra_vector_v]
type = TagVectorAux
variable = vector_tag_v
v = v
vector_tag = 'vec_tag_v'
[]
[extra_matrix_v]
type = TagMatrixAux
variable = matrix_v_diag
v = v
matrix_tag = 'mat_tag_v'
[]
[]
[Executioner]
type = Steady
solve_type = 'LINEAR'
system_names = 'u_sys v_sys'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
execute_on = timestep_end
[]
(modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/segregated/rayleigh-bernard-two-phase-physics.i)
mu = 1.0
rho = 1e3
mu_d = 0.3
rho_d = 1.0
dp = 0.01
U_lid = 0.0
g = -9.81
advected_interp_method = 'upwind'
# Currently required
k = 1
k_d = 1
cp = 1
cp_d = 1
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = .1
ymin = 0
ymax = .1
nx = 11
ny = 11
[]
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system phi_system'
[]
[Physics]
[NavierStokes]
[FlowSegregated]
[flow]
compressibility = 'incompressible'
density = 'rho_mixture'
dynamic_viscosity = 'mu_mixture'
gravity = '0 ${g} 0'
# Initial conditions
initial_velocity = '1e-12 1e-12 0'
initial_pressure = 0.2
wall_boundaries = 'top left right bottom'
momentum_wall_types = 'noslip noslip noslip noslip'
momentum_wall_functors = '${U_lid} 0; 0 0; 0 0; 0 0'
orthogonality_correction = false
pressure_two_term_bc_expansion = true
momentum_advection_interpolation = ${advected_interp_method}
[]
[]
[TwoPhaseMixtureSegregated]
[mixture]
system_names = 'phi_system'
phase_1_fraction_name = 'phase_1'
phase_2_fraction_name = 'phase_2'
add_phase_transport_equation = true
phase_advection_interpolation = '${advected_interp_method}'
phase_fraction_diffusivity = 1e-3
# We could consider adding fixed-value-yet-not-an-inlet
# boundary conditions to the TwoPhaseMixture physics
# Base phase material properties
phase_1_density_name = ${rho}
phase_1_viscosity_name = ${mu}
phase_1_specific_heat_name = ${cp}
phase_1_thermal_conductivity_name = ${k}
# Other phase material properties
phase_2_density_name = ${rho_d}
phase_2_viscosity_name = ${mu_d}
phase_2_specific_heat_name = ${cp_d}
phase_2_thermal_conductivity_name = ${k_d}
output_all_properties = true
# Friction model, not actually used!
use_dispersed_phase_drag_model = true
particle_diameter = ${dp}
add_advection_slip_term = false
# To match Rayleigh Bernard nonlinear test setup
add_gravity_term_in_slip_velocity = false
[]
[]
[]
[]
[LinearFVBCs]
[botttom-phase-2]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'bottom'
variable = phase_2
functor = '1'
[]
[top-phase-2]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top'
variable = phase_2
functor = '0'
[]
[]
[Executioner]
type = PIMPLE
rhie_chow_user_object = 'ins_rhie_chow_interpolator'
end_time = 1e8
[TimeStepper]
type = IterationAdaptiveDT
optimal_iterations = 10
iteration_window = 2
growth_factor = 2
cutback_factor = 0.5
dt = 1e-3
[]
# Systems
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
active_scalar_systems = 'phi_system'
momentum_equation_relaxation = 0.8
active_scalar_equation_relaxation = '0.7'
pressure_variable_relaxation = 0.3
# We need to converge the problem to show conservation
num_iterations = 200
pressure_absolute_tolerance = 1e-10
momentum_absolute_tolerance = 1e-10
active_scalar_absolute_tolerance = '1e-10'
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
active_scalar_petsc_options_iname = '-pc_type -pc_factor_shift_type' # -pc_hypre_type'
active_scalar_petsc_options_value = 'lu NONZERO'
momentum_l_abs_tol = 1e-13
pressure_l_abs_tol = 1e-13
active_scalar_l_abs_tol = 1e-13
momentum_l_tol = 0
pressure_l_tol = 0
active_scalar_l_tol = 0
# print_fields = true
continue_on_max_its = true
pin_pressure = true
pressure_pin_value = 0.0
pressure_pin_point = '0.0 0.0 0.0'
[]
[Outputs]
exodus = false
[out]
type = CSV
execute_on = 'FINAL'
[]
[]
[AuxVariables]
[U]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[]
[Postprocessors]
[average_void]
type = ElementAverageValue
variable = 'phase_2'
[]
[max_y_velocity]
type = ElementExtremeValue
variable = 'vel_y'
value_type = max
[]
[min_y_velocity]
type = ElementExtremeValue
variable = 'vel_y'
value_type = min
[]
[max_x_velocity]
type = ElementExtremeValue
variable = 'vel_x'
value_type = max
[]
[min_x_velocity]
type = ElementExtremeValue
variable = 'vel_x'
value_type = min
[]
[max_x_slip_velocity]
type = ElementExtremeFunctorValue
functor = 'vel_slip_x'
value_type = max
[]
[max_y_slip_velocity]
type = ElementExtremeFunctorValue
functor = 'vel_slip_y'
value_type = max
[]
[max_drag_coefficient_x]
type = ElementExtremeFunctorValue
functor = 'Darcy_coefficient_vec_out_x'
value_type = max
[]
[max_drag_coefficient_y]
type = ElementExtremeFunctorValue
functor = 'Darcy_coefficient_vec_out_y'
value_type = max
[]
[]
(modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/segregated/lid-driven-two-phase-physics.i)
mu = 1.0
rho = 1.0e3
mu_d = 0.3
rho_d = 5e2
dp = 0.01
U_lid = 0.1
advected_interp_method = 'upwind'
k = 1
k_d = 1
cp = 1
cp_d = 1
[Mesh]
inactive = 'make_skew'
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = .1
ymin = 0
ymax = .1
nx = 10
ny = 10
[]
[make_skew]
type = MoveNodeGenerator
input = 'gen'
node_id = 0
shift_position = '0.007 0.0021 0'
[]
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system phi_system'
[]
[Physics]
[NavierStokes]
[FlowSegregated]
[flow]
compressibility = 'incompressible'
density = 'rho_mixture'
dynamic_viscosity = 'mu_mixture'
# Initial conditions
initial_velocity = '1e-12 1e-12 0'
initial_pressure = 0.2
wall_boundaries = 'top left right bottom'
momentum_wall_types = 'noslip noslip noslip noslip'
momentum_wall_functors = '${U_lid} 0; 0 0; 0 0; 0 0'
orthogonality_correction = false
pressure_two_term_bc_expansion = true
momentum_advection_interpolation = ${advected_interp_method}
[]
[]
[TwoPhaseMixtureSegregated]
[mixture]
system_names = 'phi_system'
phase_1_fraction_name = 'phase_1'
phase_2_fraction_name = 'phase_2'
add_phase_transport_equation = true
phase_advection_interpolation = '${advected_interp_method}'
phase_fraction_diffusivity = 1e-3
# We could consider adding fixed-value-yet-not-an-inlet
# boundary conditions to the TwoPhaseMixture physics
# Base phase material properties
phase_1_density_name = ${rho}
phase_1_viscosity_name = ${mu}
phase_1_specific_heat_name = ${cp}
phase_1_thermal_conductivity_name = ${k}
# Other phase material properties
phase_2_density_name = ${rho_d}
phase_2_viscosity_name = ${mu_d}
phase_2_specific_heat_name = ${cp_d}
phase_2_thermal_conductivity_name = ${k_d}
output_all_properties = true
# Friction model, not actually used!
use_dispersed_phase_drag_model = true
particle_diameter = ${dp}
add_advection_slip_term = false
[]
[]
[]
[]
[LinearFVBCs]
[botttom-phase-2]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'bottom'
variable = phase_2
functor = '0'
[]
[top-phase-2]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top'
variable = phase_2
functor = '1'
[]
[]
[Executioner]
type = PIMPLE
rhie_chow_user_object = 'ins_rhie_chow_interpolator'
dt = 1
end_time = 10
# Systems
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
active_scalar_systems = 'phi_system'
momentum_equation_relaxation = 0.8
active_scalar_equation_relaxation = '0.7'
pressure_variable_relaxation = 0.3
# We need to converge the problem to show conservation
num_iterations = 200
pressure_absolute_tolerance = 1e-10
momentum_absolute_tolerance = 1e-10
active_scalar_absolute_tolerance = '1e-10'
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
active_scalar_petsc_options_iname = '-pc_type -pc_factor_shift_type' # -pc_hypre_type'
active_scalar_petsc_options_value = 'lu NONZERO'
momentum_l_abs_tol = 1e-13
pressure_l_abs_tol = 1e-13
active_scalar_l_abs_tol = 1e-13
momentum_l_tol = 0
pressure_l_tol = 0
active_scalar_l_tol = 0
# print_fields = true
continue_on_max_its = true
pin_pressure = true
pressure_pin_value = 0.0
pressure_pin_point = '0.05 0.05 0.0'
[]
[Outputs]
exodus = true
[out]
type = CSV
execute_on = 'FINAL'
[]
[]
[AuxVariables]
[drag_coefficient]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[populate_cd]
type = FunctorAux
variable = drag_coefficient
functor = 'Darcy_coefficient'
execute_on = 'TIMESTEP_END'
[]
[]
[Postprocessors]
[average_void]
type = ElementAverageValue
variable = 'phase_2'
[]
[max_y_velocity]
type = ElementExtremeValue
variable = 'vel_y'
value_type = max
[]
[min_y_velocity]
type = ElementExtremeValue
variable = 'vel_y'
value_type = min
[]
[max_x_velocity]
type = ElementExtremeValue
variable = 'vel_x'
value_type = max
[]
[min_x_velocity]
type = ElementExtremeValue
variable = 'vel_x'
value_type = min
[]
[max_x_slip_velocity]
type = ElementExtremeFunctorValue
functor = 'vel_slip_x'
value_type = max
[]
[max_y_slip_velocity]
type = ElementExtremeFunctorValue
functor = 'vel_slip_y'
value_type = max
[]
[max_drag_coefficient]
type = ElementExtremeFunctorValue
functor = 'drag_coefficient'
value_type = max
[]
[]