- 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
- sort_byWhat to sort the samples by
C++ Type:MooseEnum
Controllable:No
Description:What to sort the samples by
- variableThe names of the variables that this VectorPostprocessor operates on
C++ Type:std::vector<VariableName>
Unit:(no unit assumed)
Controllable:No
Description:The names of the variables that this VectorPostprocessor operates on
SideValueSampler
Sample variable(s) along a sideset, internal or external.
The data output to CSV is output with the columns listed below. The declared vectors use the same names.
the id of the element that the quadrature point, on the side, belongs to.
the values of the requested variables, with a column named after each variable. On internal sidesets, finite volume variables use an inverse distance weighted average to determine the face value.
the X, Y, Z coordinates of the quadrature points on the side. In case of finite volume variables this is the cell centroid of the face.
commentnote:General sampling
The SideValueSampler samples variables on the specified boundary on element side quadrature points. For more flexible sampling, use the PositionsFunctorValueSampler.
Example input syntax
In this example, variable u and v are the solutions of two boundary value diffusion problems. Their value along the top boundary and along the center internal sidesets are reported using two SideValueSampler. The rows in the CSV output are sorted according the x coordinate along the boundary for the former, and the element id for the latter.
[VectorPostprocessors<<<{"href": "../../syntax/VectorPostprocessors/index.html"}>>>]
inactive<<<{"description": "If specified blocks matching these identifiers will be skipped."}>>> = 'internal_sample'
[side_sample]
type = SideValueSampler<<<{"description": "Sample variable(s) along a sideset, internal or external.", "href": "SideValueSampler.html"}>>>
variable<<<{"description": "The names of the variables that this VectorPostprocessor operates on"}>>> = 'u v'
boundary<<<{"description": "The list of boundary IDs from the mesh where this object applies"}>>> = top
sort_by<<<{"description": "What to sort the samples by"}>>> = x
[]
[internal_sample]
type = SideValueSampler<<<{"description": "Sample variable(s) along a sideset, internal or external.", "href": "SideValueSampler.html"}>>>
variable<<<{"description": "The names of the variables that this VectorPostprocessor operates on"}>>> = 'u v'
boundary<<<{"description": "The list of boundary IDs from the mesh where this object applies"}>>> = center
sort_by<<<{"description": "What to sort the samples by"}>>> = 'id'
[]
[]Input Parameters
- _auto_broadcastFalse
Default:False
C++ Type:bool
Controllable:No
- contains_complete_historyFalseSet this flag to indicate that the values in all vectors declared by this VPP represent a time history (e.g. with each invocation, new values are added and old values are never removed). This changes the output so that only a single file is output and updated with each invocation
Default:False
C++ Type:bool
Controllable:No
Description:Set this flag to indicate that the values in all vectors declared by this VPP represent a time history (e.g. with each invocation, new values are added and old values are never removed). This changes the output so that only a single file is output and updated with each invocation
- parallel_typeREPLICATEDSet how the data is represented within the VectorPostprocessor (VPP); 'distributed' indicates that data within the VPP is distributed and no auto communication is performed, this setting will result in parallel output within the CSV output; 'replicated' indicates that the data within the VPP is correct on processor 0, the data will automatically be broadcast to all processors unless the '_auto_broadcast' param is set to false within the validParams function.
Default:REPLICATED
C++ Type:MooseEnum
Options:DISTRIBUTED, REPLICATED
Controllable:No
Description:Set how the data is represented within the VectorPostprocessor (VPP); 'distributed' indicates that data within the VPP is distributed and no auto communication is performed, this setting will result in parallel output within the CSV output; 'replicated' indicates that the data within the VPP is correct on processor 0, the data will automatically be broadcast to all processors unless the '_auto_broadcast' param is set to false within the validParams function.
Optional Parameters
- allow_duplicate_execution_on_initialFalseIn the case where this UserObject is depended upon by an initial condition, allow it to be executed twice during the initial setup (once before the IC and again after mesh adaptivity (if applicable).
Default:False
C++ Type:bool
Controllable:No
Description:In the case where this UserObject is depended upon by an initial condition, allow it to be executed twice during the initial setup (once before the IC and again after mesh adaptivity (if applicable).
- execute_onTIMESTEP_ENDThe list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html.
Default:TIMESTEP_END
C++ Type:ExecFlagEnum
Options:XFEM_MARK, FORWARD, ADJOINT, HOMOGENEOUS_FORWARD, ADJOINT_TIMESTEP_BEGIN, ADJOINT_TIMESTEP_END, NONE, INITIAL, LINEAR, LINEAR_CONVERGENCE, NONLINEAR, NONLINEAR_CONVERGENCE, POSTCHECK, TIMESTEP_END, TIMESTEP_BEGIN, MULTIAPP_FIXED_POINT_END, MULTIAPP_FIXED_POINT_BEGIN, MULTIAPP_FIXED_POINT_CONVERGENCE, FINAL, CUSTOM
Controllable:No
Description:The list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html.
- execution_order_group0Execution order groups are executed in increasing order (e.g., the lowest number is executed first). Note that negative group numbers may be used to execute groups before the default (0) group. Please refer to the user object documentation for ordering of user object execution within a group.
Default:0
C++ Type:int
Controllable:No
Description:Execution order groups are executed in increasing order (e.g., the lowest number is executed first). Note that negative group numbers may be used to execute groups before the default (0) group. Please refer to the user object documentation for ordering of user object execution within a group.
- force_postauxFalseForces the UserObject to be executed in POSTAUX
Default:False
C++ Type:bool
Controllable:No
Description:Forces the UserObject to be executed in POSTAUX
- force_preauxFalseForces the UserObject to be executed in PREAUX
Default:False
C++ Type:bool
Controllable:No
Description:Forces the UserObject to be executed in PREAUX
- force_preicFalseForces the UserObject to be executed in PREIC during initial setup
Default:False
C++ Type:bool
Controllable:No
Description:Forces the UserObject to be executed in PREIC during initial setup
Execution Scheduling 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.
- outputsVector of output names where you would like to restrict the output of variables(s) associated with this object
C++ Type:std::vector<OutputName>
Controllable:No
Description:Vector of output names where you would like to restrict the output of variables(s) associated with this object
- use_displaced_meshFalseWhether or not this object should use the displaced mesh for computation. Note that in the case this is true but no displacements are provided in the Mesh block the undisplaced mesh will still be used.
Default:False
C++ Type:bool
Controllable:No
Description:Whether or not this object should use the displaced mesh for computation. Note that in the case this is true but no displacements are provided in the Mesh block the undisplaced mesh will still be used.
Advanced Parameters
- prop_getter_suffixAn optional suffix parameter that can be appended to any attempt to retrieve/get material properties. The suffix will be prepended with a '_' character.
C++ Type:MaterialPropertyName
Unit:(no unit assumed)
Controllable:No
Description:An optional suffix parameter that can be appended to any attempt to retrieve/get material properties. The suffix will be prepended with a '_' character.
- use_interpolated_stateFalseFor the old and older state use projected material properties interpolated at the quadrature points. To set up projection use the ProjectedStatefulMaterialStorageAction.
Default:False
C++ Type:bool
Controllable:No
Description:For the old and older state use projected material properties interpolated at the quadrature points. To set up projection use the ProjectedStatefulMaterialStorageAction.
Material Property Retrieval Parameters
Input Files
- (test/tests/vectorpostprocessors/side_value_sampler/side_value_sampler.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/turbulence/bfs/segregated/BFS_ERCOFTAC.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/linear-segregated/lid-driven-turb-std-wall.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/segregated/lid-driven-turb-linear-wall.i)
- (modules/porous_flow/test/tests/dirackernels/theis2.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/turbulence/bfs/linear-segregated-transient/BFS_ERCOFTAC.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/segregated/lid-driven-turb-non-eq-bulk.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/segregated/lid-driven-turb-energy-wall.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/newton_physics/lid-driven-turb-capped-physics.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/newton_physics/lid-driven-turb-std-wall-nonlinear-physics.i)
- (modules/thermal_hydraulics/test/tests/components/heat_structure_base/inner_radial_boundary.i)
- (test/tests/userobjects/layered_side_average_functor/layered_side_average_functor.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/linear-segregated/lid-driven-turb-non-eq-wall.i)
- (test/tests/userobjects/nearest_point_layered_side_average_functor/nearest_point_layered_side_average_functor.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/segregated/lid-driven-turb-energy.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/segregated/lid-driven-turb-no-wall.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/segregated/lid-driven-turb-non-eq-wall.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/turbulence/channel/segregated/channel_ERCOFTAC.i)
- (test/tests/userobjects/layered_side_integral_functor/layered_side_integral_functor.i)
- (modules/porous_flow/test/tests/dirackernels/theis1.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/segregated/lid-driven-turb-inc-wall.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/segregated/lid-driven-turb-capped.i)
- (test/tests/vectorpostprocessors/side_value_sampler/side_value_sampler_fv.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/turbulence/bfs/linear-segregated/BFS_ERCOFTAC.i)
- (test/tests/userobjects/nearest_point_layered_side_integral_functor/nearest_point_layered_side_integral_functor.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/turbulence/channel/linear-segregated/channel_ERCOFTAC.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/newton_physics/lid-driven-turb-energy-wall-physics.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/turbulence/channel/linear-segregated-transient/channel_ERCOFTAC.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/segregated/lid-driven-turb-std-wall.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/newton/lid-driven-turb-std-wall-nonlinear.i)
(test/tests/vectorpostprocessors/side_value_sampler/side_value_sampler.i)
[Mesh]
[mesh]
type = CartesianMeshGenerator
dim = 2
dx = '0.5 0.5'
dy = '1'
ix = '5 5'
iy = '10'
subdomain_id = '1 1'
[]
# Limited to 1 side to avoid inconsistencies in parallel
[internal_sideset]
type = ParsedGenerateSideset
combinatorial_geometry = 'y<0.51 & y>0.49 & x<0.11'
new_sideset_name = 'center'
input = 'mesh'
[]
# this keeps numbering continuous so tests dont fail on different ids in CSV
allow_renumbering = false
[]
[Variables]
[u]
[]
[v]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[diff_v]
type = Diffusion
variable = v
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[left_v]
type = DirichletBC
variable = v
boundary = left
value = 1
[]
[right_v]
type = DirichletBC
variable = v
boundary = right
value = 0
[]
[]
[VectorPostprocessors]
inactive = 'internal_sample'
[side_sample]
type = SideValueSampler
variable = 'u v'
boundary = top
sort_by = x
[]
[internal_sample]
type = SideValueSampler
variable = 'u v'
boundary = center
sort_by = 'id'
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
[vpp_csv]
type = CSV
[]
[]
(test/tests/vectorpostprocessors/side_value_sampler/side_value_sampler.i)
[Mesh]
[mesh]
type = CartesianMeshGenerator
dim = 2
dx = '0.5 0.5'
dy = '1'
ix = '5 5'
iy = '10'
subdomain_id = '1 1'
[]
# Limited to 1 side to avoid inconsistencies in parallel
[internal_sideset]
type = ParsedGenerateSideset
combinatorial_geometry = 'y<0.51 & y>0.49 & x<0.11'
new_sideset_name = 'center'
input = 'mesh'
[]
# this keeps numbering continuous so tests dont fail on different ids in CSV
allow_renumbering = false
[]
[Variables]
[u]
[]
[v]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[diff_v]
type = Diffusion
variable = v
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[left_v]
type = DirichletBC
variable = v
boundary = left
value = 1
[]
[right_v]
type = DirichletBC
variable = v
boundary = right
value = 0
[]
[]
[VectorPostprocessors]
inactive = 'internal_sample'
[side_sample]
type = SideValueSampler
variable = 'u v'
boundary = top
sort_by = x
[]
[internal_sample]
type = SideValueSampler
variable = 'u v'
boundary = center
sort_by = 'id'
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
[vpp_csv]
type = CSV
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/turbulence/bfs/segregated/BFS_ERCOFTAC.i)
##########################################################
# ERCOFTAC test case foe BFS
# Case Number: 031
# Author: Dr. Mauricio Tano
# Last Update: November, 2023
# Turbulent model using:
# k-epsilon model
# Equilibrium + Newton wall treatement
# SIMPLE solve
##########################################################
Re = 5100
rho = 1.0
bulk_u = 1.0
H = 1.0
mu = '${fparse rho * bulk_u * H/ Re}'
advected_interp_method = 'upwind'
pressure_tag = "pressure_grad"
### k-epsilon Closure Parameters ###
sigma_k = 1.0
sigma_eps = 1.3
C1_eps = 1.44
C2_eps = 1.92
C_mu = 0.09
### Initial and Boundary Conditions ###
intensity = 0.01
k_init = '${fparse 1.5*(intensity * bulk_u)^2}'
eps_init = '${fparse C_mu^0.75 * k_init^1.5 / H}'
### Modeling parameters ###
bulk_wall_treatment = false
walls = 'bottom wall-side top'
wall_treatment = 'eq_incremental' # Options: eq_newton, eq_incremental, eq_linearized, neq
[Mesh]
[gen]
type = CartesianMeshGenerator
dim = 2
dx = '${fparse 10.0*H} ${fparse 20.0*H}'
dy = '${H} ${fparse 5*H}'
ix = '8 16'
iy = '2 8'
subdomain_id = '
2 1
1 1
'
[]
[corner_walls]
type = SideSetsBetweenSubdomainsGenerator
input = gen
primary_block ='1'
paired_block ='2'
new_boundary = 'wall-side'
[]
[delete_bottom]
type = BlockDeletionGenerator
input = corner_walls
block ='2'
[]
# Prevent test diffing on distributed parallel element numbering
allow_renumbering = false
[]
[Problem]
nl_sys_names = 'u_system v_system pressure_system TKE_system TKED_system'
previous_nl_solution_required = true
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolatorSegregated
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = ${bulk_u}
solver_sys = u_system
two_term_boundary_expansion = false
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 0
solver_sys = v_system
two_term_boundary_expansion = false
[]
[pressure]
type = INSFVPressureVariable
initial_condition = 1e-8
solver_sys = pressure_system
two_term_boundary_expansion = false
[]
[TKE]
type = INSFVEnergyVariable
solver_sys = TKE_system
initial_condition = ${k_init}
two_term_boundary_expansion = false
[]
[TKED]
type = INSFVEnergyVariable
solver_sys = TKED_system
initial_condition = ${eps_init}
two_term_boundary_expansion = false
[]
[]
[FVKernels]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = ${mu}
momentum_component = 'x'
[]
[u_viscosity_turbulent]
type = INSFVMomentumDiffusion
variable = vel_x
mu = 'mu_t'
momentum_component = 'x'
complete_expansion = true
u = vel_x
v = vel_y
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
extra_vector_tags = ${pressure_tag}
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = ${mu}
momentum_component = 'y'
[]
[v_viscosity_turbulent]
type = INSFVMomentumDiffusion
variable = vel_y
mu = 'mu_t'
momentum_component = 'y'
complete_expansion = true
u = vel_x
v = vel_y
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
extra_vector_tags = ${pressure_tag}
[]
[p_diffusion]
type = FVAnisotropicDiffusion
variable = pressure
coeff = "Ainv"
coeff_interp_method = 'average'
[]
[p_source]
type = FVDivergence
variable = pressure
vector_field = "HbyA"
force_boundary_execution = true
[]
[TKE_advection]
type = INSFVTurbulentAdvection
variable = TKE
rho = ${rho}
[]
[TKE_diffusion]
type = INSFVTurbulentDiffusion
variable = TKE
coeff = ${mu}
[]
[TKE_diffusion_turbulent]
type = INSFVTurbulentDiffusion
variable = TKE
coeff = 'mu_t'
scaling_coef = ${sigma_k}
[]
[TKE_source_sink]
type = INSFVTKESourceSink
variable = TKE
u = vel_x
v = vel_y
epsilon = TKED
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
walls = ${walls}
wall_treatment = ${wall_treatment}
[]
[TKED_advection]
type = INSFVTurbulentAdvection
variable = TKED
rho = ${rho}
walls = ${walls}
[]
[TKED_diffusion]
type = INSFVTurbulentDiffusion
variable = TKED
coeff = ${mu}
walls = ${walls}
[]
[TKED_diffusion_turbulent]
type = INSFVTurbulentDiffusion
variable = TKED
coeff = 'mu_t'
scaling_coef = ${sigma_eps}
walls = ${walls}
[]
[TKED_source_sink]
type = INSFVTKEDSourceSink
variable = TKED
u = vel_x
v = vel_y
tke = TKE
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
C1_eps = ${C1_eps}
C2_eps = ${C2_eps}
walls = ${walls}
wall_treatment = ${wall_treatment}
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_x
functor = '${bulk_u}'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_y
functor = 0
[]
[inlet_TKE]
type = INSFVInletIntensityTKEBC
boundary = 'left'
variable = TKE
u = vel_x
v = vel_y
intensity = ${intensity}
[]
[inlet_TKED]
type = INSFVMixingLengthTKEDBC
boundary = 'left'
variable = TKED
tke = TKE
characteristic_length = '${fparse 2*H}'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
functor = 0
[]
[walls-u]
type = FVDirichletBC
boundary = ${walls}
variable = vel_x
value = 0
[]
[walls-v]
type = FVDirichletBC
boundary = ${walls}
variable = vel_y
value = 0
[]
[walls_mu_t]
type = INSFVTurbulentViscosityWallFunction
boundary = ${walls}
variable = mu_t
u = vel_x
v = vel_y
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
tke = TKE
wall_treatment = ${wall_treatment}
[]
[]
[AuxVariables]
[mu_t]
type = MooseVariableFVReal
initial_condition = '${fparse rho * C_mu * ${k_init}^2 / eps_init}'
two_term_boundary_expansion = false
[]
[]
[AuxKernels]
[compute_mu_t]
type = kEpsilonViscosityAux
variable = mu_t
C_mu = ${C_mu}
tke = TKE
epsilon = TKED
mu = ${mu}
rho = ${rho}
u = vel_x
v = vel_y
bulk_wall_treatment = ${bulk_wall_treatment}
walls = ${walls}
wall_treatment = ${wall_treatment}
execute_on = 'NONLINEAR'
[]
[]
[Executioner]
type = SIMPLENonlinearAssembly
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
turbulence_systems = 'TKED_system TKE_system'
pressure_gradient_tag = ${pressure_tag}
momentum_equation_relaxation = 0.7
pressure_variable_relaxation = 0.3
turbulence_equation_relaxation = '0.3 0.3'
num_iterations = 500
pressure_absolute_tolerance = 1e-12
momentum_absolute_tolerance = 1e-12
turbulence_absolute_tolerance = '1e-12 1e-12'
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
momentum_l_abs_tol = 1e-14
pressure_l_abs_tol = 1e-14
turbulence_l_abs_tol = 1e-14
momentum_l_max_its = 30
pressure_l_max_its = 30
momentum_l_tol = 0.0
pressure_l_tol = 0.0
turbulence_l_tol = 0.0
print_fields = false
continue_on_max_its = true
[]
[Outputs]
csv = true
[console]
type = Console
outlier_variable_norms = false
[]
[]
[VectorPostprocessors]
[side_bottom]
type = SideValueSampler
boundary = 'bottom'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_top]
type = SideValueSampler
boundary = 'top'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[line_entry_channel_wall]
type = LineValueSampler
start_point = '${fparse 0.5 * H} ${fparse 1.00001 * H} 0'
end_point = '${fparse 29.5 * H} ${fparse 1.00001 * H} 0'
num_points = 24
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[line_quarter_entry_channel]
type = LineValueSampler
start_point = '${fparse 0.5 * H} ${fparse 2.25001 * H} 0'
end_point = '${fparse 29.5 * H} ${fparse 2.25001 * H} 0'
num_points = 24
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/linear-segregated/lid-driven-turb-std-wall.i)
### Thermophysical Properties ###
mu = 1e-3
rho = 1.0
### Operation Conditions ###
lid_velocity = 1.0
side_length = 0.1
### Initial Conditions ###
intensity = 0.01
k_init = '${fparse 1.5*(intensity * lid_velocity)^2}'
eps_init = '${fparse C_mu^0.75 * k_init^1.5 / side_length}'
### k-epsilon Closure Parameters ###
sigma_k = 1.0
sigma_eps = 1.3
C1_eps = 1.44
C2_eps = 1.92
C_mu = 0.09
### Modeling parameters ###
bulk_wall_treatment = false
walls = 'left top right bottom'
wall_treatment = 'eq_newton' # Options: eq_newton, eq_incremental, eq_linearized, neq
[GlobalParams]
rhie_chow_user_object = 'rc'
advected_interp_method = 'upwind'
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${side_length}
ymin = 0
ymax = ${side_length}
nx = 12
ny = 12
[]
# Prevent test diffing on distributed parallel element numbering
allow_renumbering = false
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system TKE_system TKED_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 = ${lid_velocity}
solver_sys = u_system
[]
[vel_y]
type = MooseLinearVariableFVReal
initial_condition = 0
solver_sys = v_system
[]
[pressure]
type = MooseLinearVariableFVReal
initial_condition = 1e-8
solver_sys = pressure_system
[]
[TKE]
type = MooseLinearVariableFVReal
solver_sys = TKE_system
initial_condition = ${k_init}
[]
[TKED]
type = MooseLinearVariableFVReal
solver_sys = TKED_system
initial_condition = ${eps_init}
[]
[]
[LinearFVKernels]
[u_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_x
mu = 'mu_t'
u = vel_x
v = vel_y
momentum_component = 'x'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = true
use_deviatoric_terms = yes
[]
[u_diffusion]
type = LinearFVDiffusion
variable = vel_x
diffusion_coeff = ${mu}
use_nonorthogonal_correction = true
[]
[u_pressure]
type = LinearFVMomentumPressure
variable = vel_x
pressure = pressure
momentum_component = 'x'
[]
[v_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_y
mu = 'mu_t'
u = vel_x
v = vel_y
momentum_component = 'y'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = true
use_deviatoric_terms = yes
[]
[v_diffusion]
type = LinearFVDiffusion
variable = vel_y
diffusion_coeff = ${mu}
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
[]
[TKE_advection]
type = LinearFVTurbulentAdvection
variable = TKE
[]
[TKE_diffusion]
type = LinearFVTurbulentDiffusion
variable = TKE
diffusion_coeff = ${mu}
use_nonorthogonal_correction = true
[]
[TKE_turb_diffusion]
type = LinearFVTurbulentDiffusion
variable = TKE
diffusion_coeff = 'mu_t'
scaling_coeff = ${sigma_k}
use_nonorthogonal_correction = true
[]
[TKE_source_sink]
type = LinearFVTKESourceSink
variable = TKE
u = vel_x
v = vel_y
epsilon = TKED
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
walls = ${walls}
wall_treatment = ${wall_treatment}
C_pl = 1e10
[]
[TKED_advection]
type = LinearFVTurbulentAdvection
variable = TKED
walls = ${walls}
[]
[TKED_diffusion]
type = LinearFVTurbulentDiffusion
variable = TKED
diffusion_coeff = ${mu}
use_nonorthogonal_correction = true
walls = ${walls}
[]
[TKED_turb_diffusion]
type = LinearFVTurbulentDiffusion
variable = TKED
diffusion_coeff = 'mu_t'
scaling_coeff = ${sigma_eps}
use_nonorthogonal_correction = true
walls = ${walls}
[]
[TKED_source_sink]
type = LinearFVTKEDSourceSink
variable = TKED
u = vel_x
v = vel_y
tke = TKE
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
C1_eps = ${C1_eps}
C2_eps = ${C2_eps}
walls = ${walls}
wall_treatment = ${wall_treatment}
C_pl = 1e10
[]
[]
[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
[]
[walls_mu_t]
type = LinearFVTurbulentViscosityWallFunctionBC
boundary = ${walls}
variable = 'mu_t'
u = vel_x
v = vel_y
rho = ${rho}
mu = ${mu}
tke = TKE
wall_treatment = ${wall_treatment}
[]
[]
[AuxVariables]
[mu_t]
type = MooseLinearVariableFVReal
initial_condition = '${fparse rho * C_mu * ${k_init}^2 / eps_init}'
[]
[yplus]
type = MooseLinearVariableFVReal
[]
[mu_eff]
type = MooseLinearVariableFVReal
initial_condition = '${fparse rho * C_mu * ${k_init}^2 / eps_init}'
[]
[]
[AuxKernels]
[compute_mu_t]
type = kEpsilonViscosityAux
variable = mu_t
C_mu = ${C_mu}
tke = TKE
epsilon = TKED
mu = ${mu}
rho = ${rho}
u = vel_x
v = vel_y
bulk_wall_treatment = ${bulk_wall_treatment}
walls = ${walls}
wall_treatment = ${wall_treatment}
execute_on = 'NONLINEAR'
mu_t_ratio_max = 1e20
[]
[compute_y_plus]
type = RANSYPlusAux
variable = yplus
tke = TKE
mu = ${mu}
rho = ${rho}
u = vel_x
v = vel_y
walls = ${walls}
wall_treatment = ${wall_treatment}
execute_on = 'NONLINEAR'
[]
[compute_mu_eff]
type = ParsedAux
variable = 'mu_eff'
coupled_variables = 'mu_t'
expression = 'mu_t + ${mu}'
execute_on = 'NONLINEAR'
[]
[]
[Executioner]
type = SIMPLE
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
turbulence_systems = 'TKE_system TKED_system'
momentum_l_abs_tol = 1e-14
pressure_l_abs_tol = 1e-14
turbulence_l_abs_tol = 1e-14
momentum_l_tol = 1e-14
pressure_l_tol = 1e-14
turbulence_l_tol = 1e-14
momentum_equation_relaxation = 0.7
pressure_variable_relaxation = 0.3
turbulence_equation_relaxation = '0.5 0.5'
num_iterations = 1000
pressure_absolute_tolerance = 1e-12
momentum_absolute_tolerance = 1e-12
turbulence_absolute_tolerance = '1e-12 1e-12'
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
turbulence_petsc_options_iname = '-pc_type -pc_hypre_type'
turbulence_petsc_options_value = 'hypre boomeramg'
print_fields = false
continue_on_max_its = true
pin_pressure = true
pressure_pin_value = 0.0
pressure_pin_point = '0.01 0.099 0.0'
[]
[Outputs]
csv = true
perf_graph = false
print_nonlinear_residuals = false
print_linear_residuals = true
[]
[VectorPostprocessors]
[side_bottom]
type = SideValueSampler
boundary = 'bottom'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_top]
type = SideValueSampler
boundary = 'top'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_left]
type = SideValueSampler
boundary = 'left'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[side_right]
type = SideValueSampler
boundary = 'right'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[horizontal_center]
type = LineValueSampler
start_point = '${fparse 0.01 * side_length} ${fparse 0.499 * side_length} 0'
end_point = '${fparse 0.99 * side_length} ${fparse 0.499 * side_length} 0'
num_points = ${Mesh/gen/nx}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[vertical_center]
type = LineValueSampler
start_point = '${fparse 0.499 * side_length} ${fparse 0.01 * side_length} 0'
end_point = '${fparse 0.499 * side_length} ${fparse 0.99 * side_length} 0'
num_points = ${Mesh/gen/ny}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/segregated/lid-driven-turb-linear-wall.i)
##########################################################
# Lid-driven cavity test
# Reynolds: 5,000
# Author: Dr. Mauricio Tano
# Last Update: November, 2023
# Turbulent model using:
# k-epsilon model
# Linear wall function formulation (faster runs)
# SIMPLE Solve
##########################################################
### Thermophysical Properties ###
mu = 2e-5
rho = 1.0
### Operation Conditions ###
lid_velocity = 1.0
side_length = 0.1
### Initial Conditions ###
intensity = 0.01
k_init = '${fparse 1.5*(intensity * lid_velocity)^2}'
eps_init = '${fparse C_mu^0.75 * k_init^1.5 / side_length}'
### k-epsilon Closure Parameters ###
sigma_k = 1.0
sigma_eps = 1.3
C1_eps = 1.44
C2_eps = 1.92
C_mu = 0.09
### Modeling parameters ###
bulk_wall_treatment = false
walls = 'left top right bottom'
wall_treatment = 'eq_linearized' # Options: eq_newton, eq_incremental, eq_linearized, neq
pressure_tag = "pressure_grad"
[GlobalParams]
rhie_chow_user_object = 'rc'
advected_interp_method = 'upwind'
velocity_interp_method = 'rc'
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${side_length}
ymin = 0
ymax = ${side_length}
nx = 12
ny = 12
[]
# Prevent test diffing on distributed parallel element numbering
allow_renumbering = false
[]
[Problem]
nl_sys_names = 'u_system v_system pressure_system TKE_system TKED_system'
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolatorSegregated
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = 0.0
solver_sys = u_system
two_term_boundary_expansion = false
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 0.0
solver_sys = v_system
two_term_boundary_expansion = false
[]
[pressure]
type = INSFVPressureVariable
solver_sys = pressure_system
initial_condition = 0.2
two_term_boundary_expansion = false
[]
[TKE]
type = INSFVEnergyVariable
solver_sys = TKE_system
initial_condition = ${k_init}
two_term_boundary_expansion = false
[]
[TKED]
type = INSFVEnergyVariable
solver_sys = TKED_system
initial_condition = ${eps_init}
two_term_boundary_expansion = false
[]
[]
[FVKernels]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = ${mu}
momentum_component = 'x'
[]
[u_viscosity_turbulent]
type = INSFVMomentumDiffusion
variable = vel_x
mu = 'mu_t'
momentum_component = 'x'
complete_expansion = true
u = vel_x
v = vel_y
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
extra_vector_tags = ${pressure_tag}
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = ${mu}
momentum_component = 'y'
[]
[v_viscosity_turbulent]
type = INSFVMomentumDiffusion
variable = vel_y
mu = 'mu_t'
momentum_component = 'y'
complete_expansion = true
u = vel_x
v = vel_y
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
extra_vector_tags = ${pressure_tag}
[]
[p_diffusion]
type = FVAnisotropicDiffusion
variable = pressure
coeff = "Ainv"
coeff_interp_method = 'average'
[]
[p_source]
type = FVDivergence
variable = pressure
vector_field = "HbyA"
force_boundary_execution = true
[]
[TKE_advection]
type = INSFVTurbulentAdvection
variable = TKE
rho = ${rho}
[]
[TKE_diffusion]
type = INSFVTurbulentDiffusion
variable = TKE
coeff = ${mu}
[]
[TKE_diffusion_turbulent]
type = INSFVTurbulentDiffusion
variable = TKE
coeff = 'mu_t'
scaling_coef = ${sigma_k}
[]
[TKE_source_sink]
type = INSFVTKESourceSink
variable = TKE
u = vel_x
v = vel_y
epsilon = TKED
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
walls = ${walls}
wall_treatment = ${wall_treatment}
[]
[TKED_advection]
type = INSFVTurbulentAdvection
variable = TKED
rho = ${rho}
walls = ${walls}
[]
[TKED_diffusion]
type = INSFVTurbulentDiffusion
variable = TKED
coeff = ${mu}
walls = ${walls}
[]
[TKED_diffusion_turbulent]
type = INSFVTurbulentDiffusion
variable = TKED
coeff = 'mu_t'
scaling_coef = ${sigma_eps}
walls = ${walls}
[]
[TKED_source_sink]
type = INSFVTKEDSourceSink
variable = TKED
u = vel_x
v = vel_y
k = TKE
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
C1_eps = ${C1_eps}
C2_eps = ${C2_eps}
walls = ${walls}
wall_treatment = ${wall_treatment}
[]
[]
[FVBCs]
[top_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'top'
function = ${lid_velocity}
[]
[no_slip_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'left right bottom'
function = 0
[]
[no_slip_y]
type = INSFVNoSlipWallBC
variable = vel_y
boundary = 'left right top bottom'
function = 0
[]
[walls_mu_t]
type = INSFVTurbulentViscosityWallFunction
boundary = 'left right top bottom'
variable = mu_t
u = vel_x
v = vel_y
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
k = TKE
wall_treatment = ${wall_treatment}
[]
[]
[AuxVariables]
[mu_t]
type = MooseVariableFVReal
initial_condition = '${fparse rho * C_mu * ${k_init}^2 / eps_init}'
two_term_boundary_expansion = false
[]
[]
[AuxKernels]
[compute_mu_t]
type = kEpsilonViscosityAux
variable = mu_t
C_mu = ${C_mu}
k = TKE
epsilon = TKED
mu = ${mu}
rho = ${rho}
u = vel_x
v = vel_y
bulk_wall_treatment = ${bulk_wall_treatment}
walls = ${walls}
wall_treatment = ${wall_treatment}
execute_on = 'NONLINEAR'
[]
[]
[Executioner]
type = SIMPLENonlinearAssembly
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
turbulence_systems = 'TKED_system TKE_system'
pressure_gradient_tag = ${pressure_tag}
momentum_equation_relaxation = 0.8
pressure_variable_relaxation = 0.5
turbulence_equation_relaxation = '0.8 0.8'
num_iterations = 500
pressure_absolute_tolerance = 1e-12
momentum_absolute_tolerance = 1e-12
turbulence_absolute_tolerance = '1e-12 1e-12'
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
momentum_l_abs_tol = 1e-14
pressure_l_abs_tol = 1e-14
turbulence_l_abs_tol = 1e-14
momentum_l_max_its = 30
pressure_l_max_its = 30
momentum_l_tol = 0.0
pressure_l_tol = 0.0
turbulence_l_tol = 0.0
print_fields = false
continue_on_max_its = true
pin_pressure = true
pressure_pin_value = 0.0
pressure_pin_point = '0.01 0.099 0.0'
[]
[Outputs]
csv = true
perf_graph = false
print_nonlinear_residuals = false
print_linear_residuals = true
[]
[VectorPostprocessors]
[side_bottom]
type = SideValueSampler
boundary = 'bottom'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_top]
type = SideValueSampler
boundary = 'top'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_left]
type = SideValueSampler
boundary = 'left'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[side_right]
type = SideValueSampler
boundary = 'right'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[horizontal_center]
type = LineValueSampler
start_point = '${fparse 0.01 * side_length} ${fparse 0.499 * side_length} 0'
end_point = '${fparse 0.99 * side_length} ${fparse 0.499 * side_length} 0'
num_points = ${Mesh/gen/nx}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[vertical_center]
type = LineValueSampler
start_point = '${fparse 0.499 * side_length} ${fparse 0.01 * side_length} 0'
end_point = '${fparse 0.499 * side_length} ${fparse 0.99 * side_length} 0'
num_points = ${Mesh/gen/ny}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[]
(modules/porous_flow/test/tests/dirackernels/theis2.i)
# Theis problem: Flow to single sink
# Constant rate injection between 200 and 1000 s.
# Cartesian mesh with logarithmic distribution in x and y.
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
bias_x = 1.1
bias_y = 1.1
ymax = 100
xmax = 100
# To get consistent ordering of results with distributed meshes
allow_renumbering = false
[]
[GlobalParams]
PorousFlowDictator = dictator
compute_enthalpy = false
compute_internal_energy = false
[]
[Variables]
[pp]
[]
[]
[Kernels]
[mass0]
type = PorousFlowMassTimeDerivative
fluid_component = 0
variable = pp
[]
[flux]
type = PorousFlowAdvectiveFlux
variable = pp
gravity = '0 0 0'
fluid_component = 0
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureVG
m = 0.5
alpha = 1e-7
[]
[]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 2e9
density0 = 1000
viscosity = 0.001
thermal_expansion = 0
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pp
capillary_pressure = pc
[]
[massfrac]
type = PorousFlowMassFraction
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[porosity]
type = PorousFlowPorosityConst
porosity = 0.2
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1E-14 0 0 0 1E-14 0 0 0 1E-14'
[]
[relperm]
type = PorousFlowRelativePermeabilityCorey
n = 0
phase = 0
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = Newton
dt = 200
end_time = 1000
nl_abs_tol = 1e-10
[]
[Outputs]
perf_graph = true
file_base = theis2
[csv]
type = CSV
execute_on = final
[]
[]
[ICs]
[PressureIC]
variable = pp
type = ConstantIC
value = 20e6
[]
[]
[DiracKernels]
[sink]
type = PorousFlowSquarePulsePointSource
start_time = 200
end_time = 1000
point = '0 0 0'
mass_flux = -0.04
variable = pp
[]
[]
[BCs]
[right]
type = DirichletBC
variable = pp
value = 20e6
boundary = right
[]
[top]
type = DirichletBC
variable = pp
value = 20e6
boundary = top
[]
[]
[VectorPostprocessors]
[pressure]
type = SideValueSampler
variable = pp
sort_by = x
execute_on = timestep_end
boundary = bottom
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/turbulence/bfs/linear-segregated-transient/BFS_ERCOFTAC.i)
Re = 5100
rho = 1.0
bulk_u = 1.0
H = 1.0
mu = '${fparse rho * bulk_u * H / Re}'
advected_interp_method = 'upwind'
### k-epsilon Closure Parameters ###
sigma_k = 1.0
sigma_eps = 1.3
C1_eps = 1.44
C2_eps = 1.92
C_mu = 0.09
### Initial and Boundary Conditions ###
intensity = 0.01
k_init = '${fparse 1.5*(intensity * bulk_u)^2}'
eps_init = '${fparse C_mu^0.75 * k_init^1.5 / H}'
### Modeling parameters ###
bulk_wall_treatment = false
walls = 'bottom wall-side top'
wall_treatment = 'neq' # Options: eq_newton, eq_incremental, eq_linearized, neq
[Mesh]
[gen]
type = CartesianMeshGenerator
dim = 2
dx = '${fparse 10.0*H} ${fparse 20.0*H}'
dy = '${H} ${fparse 5*H}'
ix = '8 16'
iy = '2 8'
subdomain_id = '
2 1
1 1
'
[]
[corner_walls]
type = SideSetsBetweenSubdomainsGenerator
input = gen
primary_block ='1'
paired_block ='2'
new_boundary = 'wall-side'
[]
[delete_bottom]
type = BlockDeletionGenerator
input = corner_walls
block ='2'
[]
# Prevent test diffing on distributed parallel element numbering
allow_renumbering = false
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system TKE_system TKED_system'
previous_nl_solution_required = true
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
advected_interp_method = ${advected_interp_method}
[]
[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 = ${bulk_u}
solver_sys = u_system
[]
[vel_y]
type = MooseLinearVariableFVReal
initial_condition = 0
solver_sys = v_system
[]
[pressure]
type = MooseLinearVariableFVReal
initial_condition = 1e-8
solver_sys = pressure_system
[]
[TKE]
type = MooseLinearVariableFVReal
solver_sys = TKE_system
initial_condition = ${k_init}
[]
[TKED]
type = MooseLinearVariableFVReal
solver_sys = TKED_system
initial_condition = ${eps_init}
[]
[]
[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_t'
u = vel_x
v = vel_y
momentum_component = 'x'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
use_deviatoric_terms = yes
[]
[u_diffusion]
type = LinearFVDiffusion
variable = vel_x
diffusion_coeff = ${mu}
use_nonorthogonal_correction = false
[]
[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_t'
u = vel_x
v = vel_y
momentum_component = 'y'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
use_deviatoric_terms = yes
[]
[v_diffusion]
type = LinearFVDiffusion
variable = vel_y
diffusion_coeff = ${mu}
use_nonorthogonal_correction = false
[]
[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
[]
[TKE_time]
type = LinearFVTimeDerivative
variable = TKE
factor = ${rho}
[]
[TKE_advection]
type = LinearFVTurbulentAdvection
variable = TKE
[]
[TKE_diffusion]
type = LinearFVTurbulentDiffusion
variable = TKE
diffusion_coeff = ${mu}
use_nonorthogonal_correction = false
[]
[TKE_turb_diffusion]
type = LinearFVTurbulentDiffusion
variable = TKE
diffusion_coeff = 'mu_t'
scaling_coeff = ${sigma_k}
use_nonorthogonal_correction = false
[]
[TKE_source_sink]
type = LinearFVTKESourceSink
variable = TKE
u = vel_x
v = vel_y
epsilon = TKED
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
walls = ${walls}
wall_treatment = ${wall_treatment}
C_pl = 1e10
[]
[TKED_time]
type = LinearFVTimeDerivative
variable = TKED
factor = ${rho}
[]
[TKED_advection]
type = LinearFVTurbulentAdvection
variable = TKED
walls = ${walls}
[]
[TKED_diffusion]
type = LinearFVTurbulentDiffusion
variable = TKED
diffusion_coeff = ${mu}
use_nonorthogonal_correction = false
walls = ${walls}
[]
[TKED_turb_diffusion]
type = LinearFVTurbulentDiffusion
variable = TKED
diffusion_coeff = 'mu_t'
scaling_coeff = ${sigma_eps}
use_nonorthogonal_correction = false
walls = ${walls}
[]
[TKED_source_sink]
type = LinearFVTKEDSourceSink
variable = TKED
u = vel_x
v = vel_y
tke = TKE
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
C1_eps = ${C1_eps}
C2_eps = ${C2_eps}
walls = ${walls}
wall_treatment = ${wall_treatment}
C_pl = 1e10
[]
[]
[LinearFVBCs]
[inlet-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_x
functor = '${bulk_u}'
[]
[inlet-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_y
functor = '0.0'
[]
[inlet_TKE]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = TKE
functor = '${k_init}'
[]
[inlet_TKED]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = TKED
functor = '${eps_init}'
[]
[outlet_p]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'right'
variable = pressure
functor = 0.0
[]
[outlet_u]
type = LinearFVAdvectionDiffusionOutflowBC
boundary = 'right'
variable = vel_x
use_two_term_expansion = false
[]
[outlet_v]
type = LinearFVAdvectionDiffusionOutflowBC
boundary = 'right'
variable = vel_y
use_two_term_expansion = false
[]
[outlet_TKE]
type = LinearFVAdvectionDiffusionOutflowBC
boundary = 'right'
variable = TKE
use_two_term_expansion = false
[]
[outlet_TKED]
type = LinearFVAdvectionDiffusionOutflowBC
boundary = 'right'
variable = TKED
use_two_term_expansion = false
[]
[walls-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = ${walls}
variable = vel_x
functor = 0.0
[]
[walls-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = ${walls}
variable = vel_y
functor = 0.0
[]
[walls_mu_t]
type = LinearFVTurbulentViscosityWallFunctionBC
boundary = ${walls}
variable = 'mu_t'
u = vel_x
v = vel_y
rho = ${rho}
mu = ${mu}
tke = TKE
wall_treatment = ${wall_treatment}
[]
[]
[AuxVariables]
[mu_t]
type = MooseLinearVariableFVReal
initial_condition = '${fparse rho * C_mu * ${k_init}^2 / eps_init}'
[]
[yplus]
type = MooseLinearVariableFVReal
[]
[mu_eff]
type = MooseLinearVariableFVReal
initial_condition = '${fparse rho * C_mu * ${k_init}^2 / eps_init + mu}'
[]
[]
[AuxKernels]
[compute_mu_t]
type = kEpsilonViscosityAux
variable = mu_t
C_mu = ${C_mu}
tke = TKE
epsilon = TKED
mu = ${mu}
rho = ${rho}
u = vel_x
v = vel_y
bulk_wall_treatment = ${bulk_wall_treatment}
walls = ${walls}
wall_treatment = ${wall_treatment}
execute_on = 'NONLINEAR'
mu_t_ratio_max = 1e20
[]
[compute_y_plus]
type = RANSYPlusAux
variable = yplus
tke = TKE
mu = ${mu}
rho = ${rho}
u = vel_x
v = vel_y
walls = ${walls}
wall_treatment = ${wall_treatment}
execute_on = 'NONLINEAR'
[]
[compute_mu_eff]
type = ParsedAux
variable = 'mu_eff'
coupled_variables = 'mu_t'
expression = 'mu_t + ${mu}'
execute_on = 'NONLINEAR'
[]
[]
[Executioner]
type = PIMPLE
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
turbulence_systems = 'TKE_system TKED_system'
momentum_l_abs_tol = 1e-14
pressure_l_abs_tol = 1e-14
turbulence_l_abs_tol = 1e-14
momentum_l_tol = 1e-14
pressure_l_tol = 1e-14
turbulence_l_tol = 1e-14
momentum_equation_relaxation = 0.7
pressure_variable_relaxation = 0.3
turbulence_equation_relaxation = '0.5 0.5'
num_iterations = 20
pressure_absolute_tolerance = 1e-6
momentum_absolute_tolerance = 1e-6
turbulence_absolute_tolerance = '1e-6 1e-6'
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
turbulence_petsc_options_iname = '-pc_type -pc_hypre_type'
turbulence_petsc_options_value = 'hypre boomeramg'
print_fields = false
continue_on_max_its = true
dt = 10.0
num_steps = 10
num_piso_iterations = 2
[]
[Outputs]
csv = true
[]
[VectorPostprocessors]
[side_bottom]
type = SideValueSampler
boundary = 'bottom'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_top]
type = SideValueSampler
boundary = 'top'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[line_entry_channel_wall]
type = LineValueSampler
start_point = '${fparse 0.5 * H} ${fparse 1.00001 * H} 0'
end_point = '${fparse 29.5 * H} ${fparse 1.00001 * H} 0'
num_points = 24
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[line_quarter_entry_channel]
type = LineValueSampler
start_point = '${fparse 0.5 * H} ${fparse 2.25001 * H} 0'
end_point = '${fparse 29.5 * H} ${fparse 2.25001 * H} 0'
num_points = 24
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/segregated/lid-driven-turb-non-eq-bulk.i)
##########################################################
# Lid-driven cavity test
# Reynolds: 5,000
# Author: Dr. Mauricio Tano
# Last Update: November, 2023
# Turbulent model using:
# Standard wall functions with non-equilibrium bulk formaultion
# No wall functions
# SIMPLE Solve
##########################################################
### Thermophysical Properties ###
mu = 2e-5
rho = 1.0
### Operation Conditions ###
lid_velocity = 1.0
side_length = 0.1
### Initial Conditions ###
intensity = 0.01
k_init = '${fparse 1.5*(intensity * lid_velocity)^2}'
eps_init = '${fparse C_mu^0.75 * k_init^1.5 / side_length}'
### k-epsilon Closure Parameters ###
sigma_k = 1.0
sigma_eps = 1.3
C1_eps = 1.44
C2_eps = 1.92
C_mu = 0.09
### Modeling parameters ###
bulk_wall_treatment = false
walls = 'left top right bottom'
wall_treatment = 'eq_newton' # Options: eq_newton, eq_incremental, eq_linearized, neq
pressure_tag = "pressure_grad"
[GlobalParams]
rhie_chow_user_object = 'rc'
advected_interp_method = 'upwind'
velocity_interp_method = 'rc'
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${side_length}
ymin = 0
ymax = ${side_length}
nx = 12
ny = 12
[]
# Prevent test diffing on distributed parallel element numbering
allow_renumbering = false
[]
[Problem]
nl_sys_names = 'u_system v_system pressure_system TKE_system TKED_system'
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolatorSegregated
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = 0.0
solver_sys = u_system
two_term_boundary_expansion = false
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 0.0
solver_sys = v_system
two_term_boundary_expansion = false
[]
[pressure]
type = INSFVPressureVariable
solver_sys = pressure_system
initial_condition = 0.2
two_term_boundary_expansion = false
[]
[TKE]
type = INSFVEnergyVariable
solver_sys = TKE_system
initial_condition = ${k_init}
two_term_boundary_expansion = false
[]
[TKED]
type = INSFVEnergyVariable
solver_sys = TKED_system
initial_condition = ${eps_init}
two_term_boundary_expansion = false
[]
[]
[FVKernels]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = ${mu}
momentum_component = 'x'
[]
[u_viscosity_turbulent]
type = INSFVMomentumDiffusion
variable = vel_x
mu = 'mu_t'
momentum_component = 'x'
complete_expansion = true
u = vel_x
v = vel_y
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
extra_vector_tags = ${pressure_tag}
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = ${mu}
momentum_component = 'y'
[]
[v_viscosity_turbulent]
type = INSFVMomentumDiffusion
variable = vel_y
mu = 'mu_t'
momentum_component = 'y'
complete_expansion = true
u = vel_x
v = vel_y
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
extra_vector_tags = ${pressure_tag}
[]
[p_diffusion]
type = FVAnisotropicDiffusion
variable = pressure
coeff = "Ainv"
coeff_interp_method = 'average'
[]
[p_source]
type = FVDivergence
variable = pressure
vector_field = "HbyA"
force_boundary_execution = true
[]
[TKE_advection]
type = INSFVTurbulentAdvection
variable = TKE
rho = ${rho}
[]
[TKE_diffusion]
type = INSFVTurbulentDiffusion
variable = TKE
coeff = ${mu}
[]
[TKE_diffusion_turbulent]
type = INSFVTurbulentDiffusion
variable = TKE
coeff = 'mu_t'
scaling_coef = ${sigma_k}
[]
[TKE_source_sink]
type = INSFVTKESourceSink
variable = TKE
u = vel_x
v = vel_y
epsilon = TKED
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
walls = ${walls}
wall_treatment = ${wall_treatment}
[]
[TKED_advection]
type = INSFVTurbulentAdvection
variable = TKED
rho = ${rho}
walls = ${walls}
[]
[TKED_diffusion]
type = INSFVTurbulentDiffusion
variable = TKED
coeff = ${mu}
walls = ${walls}
[]
[TKED_diffusion_turbulent]
type = INSFVTurbulentDiffusion
variable = TKED
coeff = 'mu_t'
scaling_coef = ${sigma_eps}
walls = ${walls}
[]
[TKED_source_sink]
type = INSFVTKEDSourceSink
variable = TKED
u = vel_x
v = vel_y
k = TKE
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
C1_eps = ${C1_eps}
C2_eps = ${C2_eps}
walls = ${walls}
wall_treatment = ${wall_treatment}
[]
[]
[FVBCs]
[top_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'top'
function = ${lid_velocity}
[]
[no_slip_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'left right bottom'
function = 0
[]
[no_slip_y]
type = INSFVNoSlipWallBC
variable = vel_y
boundary = 'left right top bottom'
function = 0
[]
[walls_mu_t]
type = INSFVTurbulentViscosityWallFunction
boundary = 'left right top bottom'
variable = mu_t
u = vel_x
v = vel_y
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
k = TKE
wall_treatment = ${wall_treatment}
[]
[]
[AuxVariables]
[mu_t]
type = MooseVariableFVReal
initial_condition = '${fparse rho * C_mu * ${k_init}^2 / eps_init}'
two_term_boundary_expansion = false
[]
[]
[AuxKernels]
[compute_mu_t]
type = kEpsilonViscosityAux
variable = mu_t
C_mu = ${C_mu}
k = TKE
epsilon = TKED
mu = ${mu}
rho = ${rho}
u = vel_x
v = vel_y
bulk_wall_treatment = ${bulk_wall_treatment}
walls = ${walls}
wall_treatment = ${wall_treatment}
execute_on = 'NONLINEAR'
[]
[]
[Executioner]
type = SIMPLENonlinearAssembly
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
turbulence_systems = 'TKED_system TKE_system'
pressure_gradient_tag = ${pressure_tag}
momentum_equation_relaxation = 0.8
pressure_variable_relaxation = 0.5
turbulence_equation_relaxation = '0.8 0.8'
num_iterations = 500
pressure_absolute_tolerance = 1e-12
momentum_absolute_tolerance = 1e-12
turbulence_absolute_tolerance = '1e-12 1e-12'
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
momentum_l_abs_tol = 1e-14
pressure_l_abs_tol = 1e-14
turbulence_l_abs_tol = 1e-14
momentum_l_max_its = 30
pressure_l_max_its = 30
momentum_l_tol = 0.0
pressure_l_tol = 0.0
turbulence_l_tol = 0.0
print_fields = false
continue_on_max_its = true
pin_pressure = true
pressure_pin_value = 0.0
pressure_pin_point = '0.01 0.099 0.0'
[]
[Outputs]
csv = true
perf_graph = false
print_nonlinear_residuals = false
print_linear_residuals = true
[]
[VectorPostprocessors]
[side_bottom]
type = SideValueSampler
boundary = 'bottom'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_top]
type = SideValueSampler
boundary = 'top'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_left]
type = SideValueSampler
boundary = 'left'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[side_right]
type = SideValueSampler
boundary = 'right'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[horizontal_center]
type = LineValueSampler
start_point = '${fparse 0.01 * side_length} ${fparse 0.499 * side_length} 0'
end_point = '${fparse 0.99 * side_length} ${fparse 0.499 * side_length} 0'
num_points = ${Mesh/gen/nx}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[vertical_center]
type = LineValueSampler
start_point = '${fparse 0.499 * side_length} ${fparse 0.01 * side_length} 0'
end_point = '${fparse 0.499 * side_length} ${fparse 0.99 * side_length} 0'
num_points = ${Mesh/gen/ny}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/segregated/lid-driven-turb-energy-wall.i)
##########################################################
# Lid-driven cavity test
# Reynolds: 5,000
# Author: Dr. Mauricio Tano
# Last Update: November, 2023
# Turbulent model using:
# k-epsilon model
# Standard wall functions with temperature wall functions
# SIMPLE Solve
##########################################################
### Thermophysical Properties ###
mu = 2e-5
rho = 1.0
k = 0.01
cp = 10.0
Pr_t = 0.9
### Operation Conditions ###
lid_velocity = 1.0
side_length = 0.1
### Initial Conditions ###
intensity = 0.01
k_init = '${fparse 1.5*(intensity * lid_velocity)^2}'
eps_init = '${fparse C_mu^0.75 * k_init^1.5 / side_length}'
### k-epsilon Closure Parameters ###
sigma_k = 1.0
sigma_eps = 1.3
C1_eps = 1.44
C2_eps = 1.92
C_mu = 0.09
### Modeling parameters ###
bulk_wall_treatment = false
walls = 'left top right bottom'
wall_treatment_v = 'eq_newton' # Options: eq_newton, eq_incremental, eq_linearized, neq
wall_treatment_T = 'eq_linearized' # Options: eq_newton, eq_incremental, eq_linearized, neq
pressure_tag = "pressure_grad"
[GlobalParams]
rhie_chow_user_object = 'rc'
advected_interp_method = 'upwind'
velocity_interp_method = 'rc'
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${side_length}
ymin = 0
ymax = ${side_length}
nx = 12
ny = 12
[]
# Prevent test diffing on distributed parallel element numbering
allow_renumbering = false
[]
[Problem]
nl_sys_names = 'u_system v_system pressure_system energy_system TKE_system TKED_system'
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolatorSegregated
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = 0.0
solver_sys = u_system
two_term_boundary_expansion = false
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 0.0
solver_sys = v_system
two_term_boundary_expansion = false
[]
[pressure]
type = INSFVPressureVariable
solver_sys = pressure_system
initial_condition = 0.2
two_term_boundary_expansion = false
[]
[T_fluid]
type = INSFVEnergyVariable
solver_sys = energy_system
initial_condition = 1.0
two_term_boundary_expansion = false
[]
[TKE]
type = INSFVEnergyVariable
solver_sys = TKE_system
initial_condition = ${k_init}
two_term_boundary_expansion = false
[]
[TKED]
type = INSFVEnergyVariable
solver_sys = TKED_system
initial_condition = ${eps_init}
two_term_boundary_expansion = false
[]
[]
[FVKernels]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = ${mu}
momentum_component = 'x'
[]
[u_viscosity_turbulent]
type = INSFVMomentumDiffusion
variable = vel_x
mu = 'mu_t'
momentum_component = 'x'
complete_expansion = true
u = vel_x
v = vel_y
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
extra_vector_tags = ${pressure_tag}
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = ${mu}
momentum_component = 'y'
[]
[v_viscosity_turbulent]
type = INSFVMomentumDiffusion
variable = vel_y
mu = 'mu_t'
momentum_component = 'y'
complete_expansion = true
u = vel_x
v = vel_y
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
extra_vector_tags = ${pressure_tag}
[]
[p_diffusion]
type = FVAnisotropicDiffusion
variable = pressure
coeff = "Ainv"
coeff_interp_method = 'average'
[]
[p_source]
type = FVDivergence
variable = pressure
vector_field = "HbyA"
force_boundary_execution = true
[]
[temp_advection]
type = INSFVEnergyAdvection
variable = T_fluid
[]
[temp_conduction]
type = FVDiffusion
coeff = ${k}
variable = T_fluid
[]
[temp_turb_conduction]
type = FVDiffusion
coeff = 'k_t'
variable = T_fluid
[]
[TKE_advection]
type = INSFVTurbulentAdvection
variable = TKE
rho = ${rho}
[]
[TKE_diffusion]
type = INSFVTurbulentDiffusion
variable = TKE
coeff = ${mu}
[]
[TKE_diffusion_turbulent]
type = INSFVTurbulentDiffusion
variable = TKE
coeff = 'mu_t'
scaling_coef = ${sigma_k}
[]
[TKE_source_sink]
type = INSFVTKESourceSink
variable = TKE
u = vel_x
v = vel_y
epsilon = TKED
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
walls = ${walls}
wall_treatment = ${wall_treatment_v}
[]
[TKED_advection]
type = INSFVTurbulentAdvection
variable = TKED
rho = ${rho}
walls = ${walls}
[]
[TKED_diffusion]
type = INSFVTurbulentDiffusion
variable = TKED
coeff = ${mu}
walls = ${walls}
[]
[TKED_diffusion_turbulent]
type = INSFVTurbulentDiffusion
variable = TKED
coeff = 'mu_t'
scaling_coef = ${sigma_eps}
walls = ${walls}
[]
[TKED_source_sink]
type = INSFVTKEDSourceSink
variable = TKED
u = vel_x
v = vel_y
k = TKE
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
C1_eps = ${C1_eps}
C2_eps = ${C2_eps}
walls = ${walls}
wall_treatment = ${wall_treatment_v}
[]
[]
[FVBCs]
[top_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'top'
function = ${lid_velocity}
[]
[no_slip_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'left right bottom'
function = 0
[]
[no_slip_y]
type = INSFVNoSlipWallBC
variable = vel_y
boundary = 'left right top bottom'
function = 0
[]
[T_hot]
type = INSFVTurbulentTemperatureWallFunction
variable = T_fluid
boundary = 'top'
T_w = 1
u = vel_x
v = vel_y
rho = ${rho}
mu = ${mu}
cp = ${cp}
kappa = ${k}
k = TKE
wall_treatment = ${wall_treatment_T}
[]
[T_cold]
type = INSFVTurbulentTemperatureWallFunction
variable = T_fluid
boundary = 'bottom'
T_w = 0
u = vel_x
v = vel_y
rho = ${rho}
mu = ${mu}
cp = ${cp}
kappa = ${k}
k = TKE
wall_treatment = ${wall_treatment_T}
[]
[walls_mu_t]
type = INSFVTurbulentViscosityWallFunction
boundary = 'left right top bottom'
variable = mu_t
u = vel_x
v = vel_y
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
k = TKE
wall_treatment = ${wall_treatment_v}
[]
[]
[AuxVariables]
[mu_t]
type = MooseVariableFVReal
initial_condition = '${fparse rho * C_mu * ${k_init}^2 / eps_init}'
two_term_boundary_expansion = false
[]
[k_t]
type = MooseVariableFVReal
initial_condition = 1.0
[]
[]
[AuxKernels]
[compute_mu_t]
type = kEpsilonViscosityAux
variable = mu_t
C_mu = ${C_mu}
k = TKE
epsilon = TKED
mu = ${mu}
rho = ${rho}
u = vel_x
v = vel_y
bulk_wall_treatment = ${bulk_wall_treatment}
walls = ${walls}
wall_treatment = ${wall_treatment_v}
execute_on = 'NONLINEAR'
[]
[compute_k_t]
type = TurbulentConductivityAux
variable = k_t
Pr_t = ${Pr_t}
cp = ${cp}
mu_t = 'mu_t'
execute_on = 'NONLINEAR'
[]
[]
[FunctorMaterials]
[ins_fv]
type = INSFVEnthalpyFunctorMaterial
temperature = 'T_fluid'
rho = ${rho}
cp = ${cp}
[]
[]
[Executioner]
type = SIMPLENonlinearAssembly
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
energy_system = 'energy_system'
turbulence_systems = 'TKED_system TKE_system'
pressure_gradient_tag = ${pressure_tag}
momentum_equation_relaxation = 0.8
pressure_variable_relaxation = 0.5
energy_equation_relaxation = 0.9
turbulence_equation_relaxation = '0.8 0.8'
num_iterations = 500
pressure_absolute_tolerance = 1e-12
momentum_absolute_tolerance = 1e-12
energy_absolute_tolerance = 1e-12
turbulence_absolute_tolerance = '1e-12 1e-12'
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
energy_petsc_options_iname = '-pc_type -pc_hypre_type'
energy_petsc_options_value = 'hypre boomeramg'
momentum_l_abs_tol = 1e-14
energy_l_abs_tol = 1e-14
pressure_l_abs_tol = 1e-14
turbulence_l_abs_tol = 1e-14
momentum_l_max_its = 30
pressure_l_max_its = 30
momentum_l_tol = 0.0
energy_l_tol = 0.0
pressure_l_tol = 0.0
turbulence_l_tol = 0.0
print_fields = false
pin_pressure = true
pressure_pin_value = 0.0
pressure_pin_point = '0.01 0.099 0.0'
continue_on_max_its = true
[]
[Outputs]
csv = true
perf_graph = false
print_nonlinear_residuals = false
print_linear_residuals = true
[]
[VectorPostprocessors]
[side_bottom]
type = SideValueSampler
boundary = 'bottom'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_top]
type = SideValueSampler
boundary = 'top'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_left]
type = SideValueSampler
boundary = 'left'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[side_right]
type = SideValueSampler
boundary = 'right'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[horizontal_center]
type = LineValueSampler
start_point = '${fparse 0.01 * side_length} ${fparse 0.499 * side_length} 0'
end_point = '${fparse 0.99 * side_length} ${fparse 0.499 * side_length} 0'
num_points = ${Mesh/gen/nx}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[vertical_center]
type = LineValueSampler
start_point = '${fparse 0.499 * side_length} ${fparse 0.01 * side_length} 0'
end_point = '${fparse 0.499 * side_length} ${fparse 0.99 * side_length} 0'
num_points = ${Mesh/gen/ny}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/newton_physics/lid-driven-turb-capped-physics.i)
##########################################################
# Lid-driven cavity test
# Reynolds: 5,000
# Author: Dr. Mauricio Tano
# Last Update: May, 2024
# Turbulent model using:
# k-epsilon model with capped mixing length
# Standard wall functions
# SIMPLE Solve
##########################################################
### Thermophysical Properties ###
mu = 2e-5
rho = 1.0
### Operation Conditions ###
lid_velocity = 1.0
side_length = 0.1
### k-epsilon Closure Parameters ###
sigma_k = 1.0
sigma_eps = 1.3
C1_eps = 1.44
C2_eps = 1.92
C_mu = 0.09
C_pl = 0.1
### Initial Conditions ###
intensity = 0.01
k_init = '${fparse 1.5*(intensity * lid_velocity)^2}'
eps_init = '${fparse C_mu^0.75 * k_init^1.5 / side_length}'
mu_t_init = '${fparse rho * C_mu * k_init * k_init / eps_init}'
### Modeling parameters ###
walls = 'left top right bottom'
bulk_wall_treatment = false
wall_treatment = 'eq_newton' # Options: eq_newton, eq_incremental, eq_linearized, neq
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${side_length}
ymin = 0
ymax = ${side_length}
nx = 12
ny = 12
[]
[break_symmetries]
type = ParsedNodeTransformGenerator
input = gen
constant_names = 'side_length'
constant_expressions = '${side_length}'
x_function = 'if(x<side_length*1.001 / 2 & x > side_length * 0.999 / 2, x * 1.05, x)'
y_function = 'if(y<side_length*1.001 / 2 & y > side_length * 0.999 / 2, y * 1.05, y)'
[]
# Prevent test diffing on distributed parallel element numbering
allow_renumbering = false
[]
[Physics]
[NavierStokes]
[Flow]
[flow]
compressibility = 'incompressible'
density = ${rho}
dynamic_viscosity = ${mu}
initial_pressure = 0.2
initial_velocity = 'ini_vx ini_vy 0'
wall_boundaries = 'top left right bottom'
momentum_wall_types = 'noslip noslip noslip noslip'
momentum_wall_functors = '${lid_velocity} 0; 0 0; 0 0; 0 0'
pin_pressure = true
pinned_pressure_type = point-value
pinned_pressure_value = 0
pinned_pressure_point = '0.01 0.099 0.0'
momentum_two_term_bc_expansion = false
pressure_two_term_bc_expansion = false
[]
[]
[Turbulence]
[keps]
turbulence_handling = 'k-epsilon'
tke_name = TKE
tked_name = TKED
# Initialization
initial_tke = ${k_init}
initial_tked = ${eps_init}
initial_mu_t = ${mu_t_init}
# Model parameters
C1_eps = ${C1_eps}
C2_eps = ${C2_eps}
C_mu = ${C_mu}
C_pl = ${C_pl}
sigma_k = ${sigma_k}
sigma_eps = ${sigma_eps}
# Wall parameters
turbulence_walls = ${walls}
bulk_wall_treatment = ${bulk_wall_treatment}
wall_treatment_eps = ${wall_treatment}
# Numerical parameters
turbulent_viscosity_two_term_bc_expansion = false
mu_t_as_aux_variable = true
tke_two_term_bc_expansion = false
tked_two_term_bc_expansion = false
[]
[]
[]
[]
[Functions]
[ini_vx]
type = ParsedFunction
expression = 'if(y>0.09, 0.1, -0.0001)'
[]
[ini_vy]
type = ParsedFunction
expression = 'if(x>0.05, -0.001, 0.001)'
[]
[]
[AuxVariables]
[dummy]
type = MooseVariableConstMonomial
[]
[]
[Bounds]
[min_tke]
type = ConstantBounds
variable = dummy
bound_value = 1e-8
bounded_variable = TKE
bound_type = lower
[]
[min_eps]
type = ConstantBounds
variable = dummy
bound_value = 1e-8
bounded_variable = TKED
bound_type = lower
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_shift_type -snes_type'
petsc_options_value = 'lu NONZERO vinewtonrsls '
nl_abs_tol = 1e-7
nl_rel_tol = 1e-8
nl_max_its = 100
line_search = none
automatic_scaling = true
[]
[Outputs]
csv = true
perf_graph = false
print_nonlinear_residuals = true
print_linear_residuals = false
[]
[VectorPostprocessors]
[side_bottom]
type = SideValueSampler
boundary = 'bottom'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_top]
type = SideValueSampler
boundary = 'top'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_left]
type = SideValueSampler
boundary = 'left'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[side_right]
type = SideValueSampler
boundary = 'right'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[horizontal_center]
type = LineValueSampler
start_point = '${fparse 0.01 * side_length} ${fparse 0.499 * side_length} 0'
end_point = '${fparse 0.99 * side_length} ${fparse 0.499 * side_length} 0'
num_points = ${Mesh/gen/nx}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[vertical_center]
type = LineValueSampler
start_point = '${fparse 0.499 * side_length} ${fparse 0.01 * side_length} 0'
end_point = '${fparse 0.499 * side_length} ${fparse 0.99 * side_length} 0'
num_points = ${Mesh/gen/ny}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/newton_physics/lid-driven-turb-std-wall-nonlinear-physics.i)
##########################################################
# Lid-driven cavity test
# Reynolds: 5,000
# Author: Dr. Mauricio Tano
# Last Update: May, 2024
# Turbulent model using:
# k-epsilon model
# No wall functions
# Newton Solve
##########################################################
### Thermophysical Properties ###
mu = 2e-5
rho = 1.0
### Operation Conditions ###
lid_velocity = 1.0
side_length = 0.1
### Initial Conditions ###
intensity = 0.01
k_init = '${fparse 1.5*(intensity * lid_velocity)^2}'
eps_init = '${fparse C_mu^0.75 * k_init^1.5 / side_length}'
### k-epsilon Closure Parameters ###
sigma_k = 1.0
sigma_eps = 1.3
C1_eps = 1.44
C2_eps = 1.92
C_mu = 0.09
### Modeling parameters ###
walls = '' # no walls for turbulence, to get 'standard' walls
bulk_wall_treatment = false
wall_treatment = 'eq_newton' # Options: eq_newton, eq_incremental, eq_linearized, neq
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${side_length}
ymin = 0
ymax = ${side_length}
nx = 10
ny = 10
[]
[]
[Problem]
previous_nl_solution_required = true
[]
[Physics]
[NavierStokes]
[Flow]
[flow]
compressibility = 'incompressible'
density = ${rho}
dynamic_viscosity = ${mu}
initial_pressure = 0.2
initial_velocity = '1e-10 1e-10 0'
wall_boundaries = 'left right top bottom'
momentum_wall_types = 'noslip noslip noslip noslip'
momentum_wall_functors = '0 0; 0 0; ${lid_velocity} 0; 0 0'
pin_pressure = true
pinned_pressure_type = average
pinned_pressure_value = 0
mu_interp_method = 'average'
[]
[]
[Turbulence]
[keps]
turbulence_handling = 'k-epsilon'
# only needed for comparing input syntax with DumpObjectsProblem
transient = true
tke_name = TKE
tked_name = TKED
# Initialization
initial_tke = ${k_init}
initial_tked = ${eps_init}
# Model parameters
C1_eps = ${C1_eps}
C2_eps = ${C2_eps}
C_mu = ${C_mu}
sigma_k = ${sigma_k}
sigma_eps = ${sigma_eps}
# Wall parameters
turbulence_walls = ${walls}
bulk_wall_treatment = ${bulk_wall_treatment}
wall_treatment_eps = ${wall_treatment}
# Numerical parameters
turbulent_viscosity_two_term_bc_expansion = false
turbulent_viscosity_interp_method = 'average'
mu_t_as_aux_variable = false
output_mu_t = false
tke_two_term_bc_expansion = false
tked_two_term_bc_expansion = false
[]
[]
[]
[]
[FVBCs]
[walls_TKE]
type = FVDirichletBC
boundary = 'left right top bottom'
variable = TKE
value = ${k_init}
[]
[walls_TKED]
type = FVDirichletBC
boundary = 'left right top bottom'
variable = TKED
value = ${eps_init}
[]
[]
[Executioner]
type = Transient
end_time = 200
dt = 0.01
# To force it to end on the same step as the gold file
num_steps = 160
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_shift_type -snes_linesearch_damping'
petsc_options_value = 'lu NONZERO 0.5'
nl_abs_tol = 1e-8
nl_rel_tol = 1e-8
nl_max_its = 50
line_search = none
[]
[Outputs]
csv = true
perf_graph = false
print_nonlinear_residuals = true
print_linear_residuals = false
[]
[VectorPostprocessors]
[side_bottom]
type = SideValueSampler
boundary = 'bottom'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_top]
type = SideValueSampler
boundary = 'top'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_left]
type = SideValueSampler
boundary = 'left'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[side_right]
type = SideValueSampler
boundary = 'right'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[horizontal_center]
type = LineValueSampler
start_point = '${fparse 0.01 * side_length} ${fparse 0.499 * side_length} 0'
end_point = '${fparse 0.99 * side_length} ${fparse 0.499 * side_length} 0'
num_points = ${Mesh/gen/nx}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[vertical_center]
type = LineValueSampler
start_point = '${fparse 0.499 * side_length} ${fparse 0.01 * side_length} 0'
end_point = '${fparse 0.499 * side_length} ${fparse 0.99 * side_length} 0'
num_points = ${Mesh/gen/ny}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[]
(modules/thermal_hydraulics/test/tests/components/heat_structure_base/inner_radial_boundary.i)
# Used for testing that the inner radial boundaries of a heat structure are
# created correctly. A SideValueSampler VPP samples a variable along an inner
# radial boundary and the test verifies that the correct space points and
# variable values are recovered.
[Functions]
[initial_T_fn_ax_x]
type = PiecewiseLinear
axis = x
x = '0 5 10'
y = '300 500 1000'
[]
[initial_T_fn_ax_y]
type = PiecewiseLinear
axis = y
x = '0 0.75 1.0 4.0 6.0'
y = '0 0 1.0 1.5 2.0'
[]
[initial_T_fn]
type = CompositeFunction
functions = 'initial_T_fn_ax_x initial_T_fn_ax_y'
[]
[]
[SolidProperties]
[hs_mat]
type = ThermalFunctionSolidProperties
k = 1
cp = 1
rho = 1
[]
[]
[Components]
[hs]
type = HeatStructureCylindrical
position = '0 0 0'
orientation = '1 0 0'
length = 10.0
n_elems = 20
names = 'region1 region2 region3'
widths = '1.0 3.0 2.0'
n_part_elems = '2 6 8'
solid_properties = 'hs_mat hs_mat hs_mat'
solid_properties_T_ref = '300 300 300'
initial_T = initial_T_fn
[]
[]
[VectorPostprocessors]
[test_vpp]
type = SideValueSampler
variable = T_solid
boundary = 'hs:region1:region2'
sort_by = x
execute_on = 'INITIAL'
[]
[]
[Preconditioning]
[pc]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
num_steps = 0
[]
[Outputs]
csv = true
execute_on = 'INITIAL'
[]
(test/tests/userobjects/layered_side_average_functor/layered_side_average_functor.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 40
ny = 10
nz = 10
allow_renumbering = false
[]
[Materials]
[u_mat]
type = GenericFunctorMaterial
prop_names = 'u'
prop_values = 'u_fn'
[]
[]
[AuxVariables]
[u_layered_average]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[u_layered_average_kern]
type = SpatialUserObjectAux
variable = u_layered_average
user_object = nplaf
boundary = 'bottom top'
execute_on = 'INITIAL'
[]
[]
[Functions]
[u_fn]
type = ParsedFunction
expression = 'x + y + z'
[]
[]
[UserObjects]
[nplaf]
type = LayeredSideAverageFunctor
direction = x
num_layers = 10
functor = u
boundary = 'bottom top'
execute_on = 'INITIAL'
[]
[]
[VectorPostprocessors]
[test_vpp]
type = SideValueSampler
variable = u_layered_average
boundary = 'bottom top'
sort_by = id
execute_on = 'INITIAL'
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
execute_on = 'INITIAL'
[]
(modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/linear-segregated/lid-driven-turb-non-eq-wall.i)
### Thermophysical Properties ###
mu = 1e-3
rho = 1.0
### Operation Conditions ###
lid_velocity = 1.0
side_length = 0.1
### Initial Conditions ###
intensity = 0.01
k_init = '${fparse 1.5*(intensity * lid_velocity)^2}'
eps_init = '${fparse C_mu^0.75 * k_init^1.5 / side_length}'
### k-epsilon Closure Parameters ###
sigma_k = 1.0
sigma_eps = 1.3
C1_eps = 1.44
C2_eps = 1.92
C_mu = 0.09
### Modeling parameters ###
bulk_wall_treatment = false
walls = 'left top right bottom'
wall_treatment = 'neq' # Options: eq_newton, eq_incremental, eq_linearized, neq
[GlobalParams]
rhie_chow_user_object = 'rc'
advected_interp_method = 'upwind'
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${side_length}
ymin = 0
ymax = ${side_length}
nx = 12
ny = 12
[]
# Prevent test diffing on distributed parallel element numbering
allow_renumbering = false
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system TKE_system TKED_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 = ${lid_velocity}
solver_sys = u_system
[]
[vel_y]
type = MooseLinearVariableFVReal
initial_condition = 0
solver_sys = v_system
[]
[pressure]
type = MooseLinearVariableFVReal
initial_condition = 1e-8
solver_sys = pressure_system
[]
[TKE]
type = MooseLinearVariableFVReal
solver_sys = TKE_system
initial_condition = ${k_init}
[]
[TKED]
type = MooseLinearVariableFVReal
solver_sys = TKED_system
initial_condition = ${eps_init}
[]
[]
[LinearFVKernels]
[u_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_x
mu = 'mu_t'
u = vel_x
v = vel_y
momentum_component = 'x'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
use_deviatoric_terms = yes
[]
[u_diffusion]
type = LinearFVDiffusion
variable = vel_x
diffusion_coeff = ${mu}
use_nonorthogonal_correction = false
[]
[u_pressure]
type = LinearFVMomentumPressure
variable = vel_x
pressure = pressure
momentum_component = 'x'
[]
[v_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_y
mu = 'mu_t'
u = vel_x
v = vel_y
momentum_component = 'y'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
use_deviatoric_terms = yes
[]
[v_diffusion]
type = LinearFVDiffusion
variable = vel_y
diffusion_coeff = ${mu}
use_nonorthogonal_correction = false
[]
[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
[]
[TKE_advection]
type = LinearFVTurbulentAdvection
variable = TKE
[]
[TKE_diffusion]
type = LinearFVTurbulentDiffusion
variable = TKE
diffusion_coeff = ${mu}
use_nonorthogonal_correction = false
[]
[TKE_turb_diffusion]
type = LinearFVTurbulentDiffusion
variable = TKE
diffusion_coeff = 'mu_t'
scaling_coeff = ${sigma_k}
use_nonorthogonal_correction = false
[]
[TKE_source_sink]
type = LinearFVTKESourceSink
variable = TKE
u = vel_x
v = vel_y
epsilon = TKED
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
walls = ${walls}
wall_treatment = ${wall_treatment}
C_pl = 1e10
[]
[TKED_advection]
type = LinearFVTurbulentAdvection
variable = TKED
walls = ${walls}
[]
[TKED_diffusion]
type = LinearFVTurbulentDiffusion
variable = TKED
diffusion_coeff = ${mu}
use_nonorthogonal_correction = false
walls = ${walls}
[]
[TKED_turb_diffusion]
type = LinearFVTurbulentDiffusion
variable = TKED
diffusion_coeff = 'mu_t'
scaling_coeff = ${sigma_eps}
use_nonorthogonal_correction = false
walls = ${walls}
[]
[TKED_source_sink]
type = LinearFVTKEDSourceSink
variable = TKED
u = vel_x
v = vel_y
tke = TKE
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
C1_eps = ${C1_eps}
C2_eps = ${C2_eps}
walls = ${walls}
wall_treatment = ${wall_treatment}
C_pl = 1e10
[]
[]
[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
[]
[walls_mu_t]
type = LinearFVTurbulentViscosityWallFunctionBC
boundary = 'bottom top'
variable = 'mu_t'
u = vel_x
v = vel_y
rho = ${rho}
mu = ${mu}
tke = TKE
wall_treatment = ${wall_treatment}
[]
[]
[AuxVariables]
[mu_t]
type = MooseLinearVariableFVReal
initial_condition = '${fparse rho * C_mu * ${k_init}^2 / eps_init}'
[]
[yplus]
type = MooseLinearVariableFVReal
[]
[mu_eff]
type = MooseLinearVariableFVReal
initial_condition = '${fparse rho * C_mu * ${k_init}^2 / eps_init}'
[]
[]
[AuxKernels]
[compute_mu_t]
type = kEpsilonViscosityAux
variable = mu_t
C_mu = ${C_mu}
tke = TKE
epsilon = TKED
mu = ${mu}
rho = ${rho}
u = vel_x
v = vel_y
bulk_wall_treatment = ${bulk_wall_treatment}
walls = ${walls}
wall_treatment = ${wall_treatment}
execute_on = 'NONLINEAR'
mu_t_ratio_max = 1e20
[]
[compute_y_plus]
type = RANSYPlusAux
variable = yplus
tke = TKE
mu = ${mu}
rho = ${rho}
u = vel_x
v = vel_y
walls = ${walls}
wall_treatment = ${wall_treatment}
execute_on = 'NONLINEAR'
[]
[compute_mu_eff]
type = ParsedAux
variable = 'mu_eff'
coupled_variables = 'mu_t'
expression = 'mu_t + ${mu}'
execute_on = 'NONLINEAR'
[]
[]
[Executioner]
type = SIMPLE
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
turbulence_systems = 'TKE_system TKED_system'
momentum_l_abs_tol = 1e-14
pressure_l_abs_tol = 1e-14
turbulence_l_abs_tol = 1e-14
momentum_l_tol = 1e-14
pressure_l_tol = 1e-14
turbulence_l_tol = 1e-14
momentum_equation_relaxation = 0.7
pressure_variable_relaxation = 0.3
turbulence_equation_relaxation = '0.5 0.5'
num_iterations = 1000
pressure_absolute_tolerance = 1e-12
momentum_absolute_tolerance = 1e-12
turbulence_absolute_tolerance = '1e-12 1e-12'
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
turbulence_petsc_options_iname = '-pc_type -pc_hypre_type'
turbulence_petsc_options_value = 'hypre boomeramg'
print_fields = false
continue_on_max_its = true
pin_pressure = true
pressure_pin_value = 0.0
pressure_pin_point = '0.01 0.099 0.0'
[]
[Outputs]
csv = true
perf_graph = false
print_nonlinear_residuals = false
print_linear_residuals = true
[]
[VectorPostprocessors]
[side_bottom]
type = SideValueSampler
boundary = 'bottom'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_top]
type = SideValueSampler
boundary = 'top'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_left]
type = SideValueSampler
boundary = 'left'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[side_right]
type = SideValueSampler
boundary = 'right'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[horizontal_center]
type = LineValueSampler
start_point = '${fparse 0.01 * side_length} ${fparse 0.499 * side_length} 0'
end_point = '${fparse 0.99 * side_length} ${fparse 0.499 * side_length} 0'
num_points = ${Mesh/gen/nx}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[vertical_center]
type = LineValueSampler
start_point = '${fparse 0.499 * side_length} ${fparse 0.01 * side_length} 0'
end_point = '${fparse 0.499 * side_length} ${fparse 0.99 * side_length} 0'
num_points = ${Mesh/gen/ny}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[]
(test/tests/userobjects/nearest_point_layered_side_average_functor/nearest_point_layered_side_average_functor.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 40
ny = 10
nz = 10
allow_renumbering = false
[]
[Materials]
[u_mat]
type = GenericFunctorMaterial
prop_names = 'u'
prop_values = 'u_fn'
[]
[]
[AuxVariables]
[u_layered_average]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[u_layered_average_kern]
type = SpatialUserObjectAux
variable = u_layered_average
user_object = nplaf
boundary = 'bottom top'
execute_on = 'INITIAL'
[]
[]
[Functions]
[u_fn]
type = ParsedFunction
expression = 'x + y + z'
[]
[]
[UserObjects]
[nplaf]
type = NearestPointLayeredSideAverageFunctor
direction = x
points='
0.25 0 0.25
0.75 0 0.25
0.25 0 0.75
0.75 0 0.75'
num_layers = 10
functor = u
boundary = 'bottom top'
execute_on = 'INITIAL'
[]
[]
[VectorPostprocessors]
[test_vpp]
type = SideValueSampler
variable = u_layered_average
boundary = 'bottom top'
sort_by = id
execute_on = 'INITIAL'
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
execute_on = 'INITIAL'
[]
(modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/segregated/lid-driven-turb-energy.i)
##########################################################
# Lid-driven cavity test
# Reynolds: 5,000
# Author: Dr. Mauricio Tano
# Last Update: November, 2023
# Turbulent model using:
# k-epsilon model with energy transport
# Standard wall functions without temperature wall functions
# SIMPLE Solve
##########################################################
### Thermophysical Properties ###
mu = 2e-5
rho = 1.0
k = 0.01
cp = 10.0
Pr_t = 0.9
### Operation Conditions ###
lid_velocity = 1.0
side_length = 0.1
### Initial Conditions ###
intensity = 0.01
k_init = '${fparse 1.5*(intensity * lid_velocity)^2}'
eps_init = '${fparse C_mu^0.75 * k_init^1.5 / side_length}'
### k-epsilon Closure Parameters ###
sigma_k = 1.0
sigma_eps = 1.3
C1_eps = 1.44
C2_eps = 1.92
C_mu = 0.09
### Modeling parameters ###
bulk_wall_treatment = false
walls = 'left top right bottom'
wall_treatment = 'eq_newton' # Options: eq_newton, eq_incremental, eq_linearized, neq
pressure_tag = "pressure_grad"
[GlobalParams]
rhie_chow_user_object = 'rc'
advected_interp_method = 'upwind'
velocity_interp_method = 'rc'
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${side_length}
ymin = 0
ymax = ${side_length}
nx = 12
ny = 12
[]
# Prevent test diffing on distributed parallel element numbering
allow_renumbering = false
[]
[Problem]
nl_sys_names = 'u_system v_system pressure_system energy_system TKE_system TKED_system'
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolatorSegregated
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = 0.0
solver_sys = u_system
two_term_boundary_expansion = false
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 0.0
solver_sys = v_system
two_term_boundary_expansion = false
[]
[pressure]
type = INSFVPressureVariable
solver_sys = pressure_system
initial_condition = 0.2
two_term_boundary_expansion = false
[]
[T_fluid]
type = INSFVEnergyVariable
solver_sys = energy_system
initial_condition = 1.0
two_term_boundary_expansion = false
[]
[TKE]
type = INSFVEnergyVariable
solver_sys = TKE_system
initial_condition = ${k_init}
two_term_boundary_expansion = false
[]
[TKED]
type = INSFVEnergyVariable
solver_sys = TKED_system
initial_condition = ${eps_init}
two_term_boundary_expansion = false
[]
[]
[FVKernels]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = ${mu}
momentum_component = 'x'
[]
[u_viscosity_turbulent]
type = INSFVMomentumDiffusion
variable = vel_x
mu = 'mu_t'
momentum_component = 'x'
complete_expansion = true
u = vel_x
v = vel_y
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
extra_vector_tags = ${pressure_tag}
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = ${mu}
momentum_component = 'y'
[]
[v_viscosity_turbulent]
type = INSFVMomentumDiffusion
variable = vel_y
mu = 'mu_t'
momentum_component = 'y'
complete_expansion = true
u = vel_x
v = vel_y
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
extra_vector_tags = ${pressure_tag}
[]
[p_diffusion]
type = FVAnisotropicDiffusion
variable = pressure
coeff = "Ainv"
coeff_interp_method = 'average'
[]
[p_source]
type = FVDivergence
variable = pressure
vector_field = "HbyA"
force_boundary_execution = true
[]
[temp_advection]
type = INSFVEnergyAdvection
variable = T_fluid
[]
[temp_conduction]
type = FVDiffusion
coeff = ${k}
variable = T_fluid
[]
[temp_turb_conduction]
type = FVDiffusion
coeff = 'k_t'
variable = T_fluid
[]
[TKE_advection]
type = INSFVTurbulentAdvection
variable = TKE
rho = ${rho}
[]
[TKE_diffusion]
type = INSFVTurbulentDiffusion
variable = TKE
coeff = ${mu}
[]
[TKE_diffusion_turbulent]
type = INSFVTurbulentDiffusion
variable = TKE
coeff = 'mu_t'
scaling_coef = ${sigma_k}
[]
[TKE_source_sink]
type = INSFVTKESourceSink
variable = TKE
u = vel_x
v = vel_y
epsilon = TKED
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
walls = ${walls}
wall_treatment = ${wall_treatment}
[]
[TKED_advection]
type = INSFVTurbulentAdvection
variable = TKED
rho = ${rho}
walls = ${walls}
[]
[TKED_diffusion]
type = INSFVTurbulentDiffusion
variable = TKED
coeff = ${mu}
walls = ${walls}
[]
[TKED_diffusion_turbulent]
type = INSFVTurbulentDiffusion
variable = TKED
coeff = 'mu_t'
scaling_coef = ${sigma_eps}
walls = ${walls}
[]
[TKED_source_sink]
type = INSFVTKEDSourceSink
variable = TKED
u = vel_x
v = vel_y
k = TKE
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
C1_eps = ${C1_eps}
C2_eps = ${C2_eps}
walls = ${walls}
wall_treatment = ${wall_treatment}
[]
[]
[FVBCs]
[top_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'top'
function = ${lid_velocity}
[]
[no_slip_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'left right bottom'
function = 0
[]
[no_slip_y]
type = INSFVNoSlipWallBC
variable = vel_y
boundary = 'left right top bottom'
function = 0
[]
[T_hot]
type = FVDirichletBC
variable = T_fluid
boundary = 'top'
value = 1
[]
[T_cold]
type = FVDirichletBC
variable = T_fluid
boundary = 'bottom'
value = 0
[]
[walls_mu_t]
type = INSFVTurbulentViscosityWallFunction
boundary = 'left right top bottom'
variable = mu_t
u = vel_x
v = vel_y
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
k = TKE
wall_treatment = ${wall_treatment}
[]
[]
[AuxVariables]
[mu_t]
type = MooseVariableFVReal
initial_condition = '${fparse rho * C_mu * ${k_init}^2 / eps_init}'
two_term_boundary_expansion = false
[]
[]
[AuxKernels]
[compute_mu_t]
type = kEpsilonViscosityAux
variable = mu_t
C_mu = ${C_mu}
k = TKE
epsilon = TKED
mu = ${mu}
rho = ${rho}
u = vel_x
v = vel_y
bulk_wall_treatment = ${bulk_wall_treatment}
walls = ${walls}
wall_treatment = ${wall_treatment}
execute_on = 'NONLINEAR'
[]
[]
[FunctorMaterials]
[ins_fv]
type = INSFVEnthalpyFunctorMaterial
temperature = 'T_fluid'
rho = ${rho}
cp = ${cp}
[]
[k_t]
type = ADParsedFunctorMaterial
expression = 'mu_t * cp / Pr_t'
functor_names = 'mu_t ${cp} ${Pr_t}'
functor_symbols = 'mu_t cp Pr_t'
property_name = 'k_t'
[]
[]
[Executioner]
type = SIMPLENonlinearAssembly
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
energy_system = 'energy_system'
turbulence_systems = 'TKED_system TKE_system'
pressure_gradient_tag = ${pressure_tag}
momentum_equation_relaxation = 0.8
pressure_variable_relaxation = 0.5
energy_equation_relaxation = 0.9
turbulence_equation_relaxation = '0.8 0.8'
num_iterations = 500
pressure_absolute_tolerance = 1e-12
momentum_absolute_tolerance = 1e-12
energy_absolute_tolerance = 1e-12
turbulence_absolute_tolerance = '1e-12 1e-12'
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
energy_petsc_options_iname = '-pc_type -pc_hypre_type'
energy_petsc_options_value = 'hypre boomeramg'
momentum_l_abs_tol = 1e-14
energy_l_abs_tol = 1e-14
pressure_l_abs_tol = 1e-14
turbulence_l_abs_tol = 1e-14
momentum_l_max_its = 30
pressure_l_max_its = 30
momentum_l_tol = 0.0
energy_l_tol = 0.0
pressure_l_tol = 0.0
turbulence_l_tol = 0.0
print_fields = false
pin_pressure = true
pressure_pin_value = 0.0
pressure_pin_point = '0.01 0.099 0.0'
continue_on_max_its = true
[]
[Outputs]
csv = true
perf_graph = false
print_nonlinear_residuals = false
print_linear_residuals = true
[]
[VectorPostprocessors]
[side_bottom]
type = SideValueSampler
boundary = 'bottom'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_top]
type = SideValueSampler
boundary = 'top'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_left]
type = SideValueSampler
boundary = 'left'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[side_right]
type = SideValueSampler
boundary = 'right'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[horizontal_center]
type = LineValueSampler
start_point = '${fparse 0.01 * side_length} ${fparse 0.499 * side_length} 0'
end_point = '${fparse 0.99 * side_length} ${fparse 0.499 * side_length} 0'
num_points = ${Mesh/gen/nx}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[vertical_center]
type = LineValueSampler
start_point = '${fparse 0.499 * side_length} ${fparse 0.01 * side_length} 0'
end_point = '${fparse 0.499 * side_length} ${fparse 0.99 * side_length} 0'
num_points = ${Mesh/gen/ny}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/segregated/lid-driven-turb-no-wall.i)
##########################################################
# Lid-driven cavity test
# Reynolds: 5,000
# Author: Dr. Mauricio Tano
# Last Update: November, 2023
# Turbulent model using:
# k-epsilon model
# No wall functions
# SIMPLE Solve
##########################################################
### Thermophysical Properties ###
mu = 2e-5
rho = 1.0
### Operation Conditions ###
lid_velocity = 1.0
side_length = 0.1
### Initial Conditions ###
intensity = 0.01
k_init = '${fparse 1.5*(intensity * lid_velocity)^2}'
eps_init = '${fparse C_mu^0.75 * k_init^1.5 / side_length}'
### k-epsilon Closure Parameters ###
sigma_k = 1.0
sigma_eps = 1.3
C1_eps = 1.44
C2_eps = 1.92
C_mu = 0.09
### Modeling parameters ###
bulk_wall_treatment = false
walls = ''
wall_treatment = 'eq_newton' # Options: eq_newton, eq_incremental, eq_linearized, neq
pressure_tag = "pressure_grad"
[GlobalParams]
rhie_chow_user_object = 'rc'
advected_interp_method = 'upwind'
velocity_interp_method = 'rc'
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${side_length}
ymin = 0
ymax = ${side_length}
nx = 12
ny = 12
[]
# Prevent test diffing on distributed parallel element numbering
allow_renumbering = false
[]
[Problem]
nl_sys_names = 'u_system v_system pressure_system TKE_system TKED_system'
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolatorSegregated
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = 0.0
solver_sys = u_system
two_term_boundary_expansion = false
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 0.0
solver_sys = v_system
two_term_boundary_expansion = false
[]
[pressure]
type = INSFVPressureVariable
solver_sys = pressure_system
initial_condition = 0.2
two_term_boundary_expansion = false
[]
[TKE]
type = INSFVEnergyVariable
solver_sys = TKE_system
initial_condition = ${k_init}
two_term_boundary_expansion = false
[]
[TKED]
type = INSFVEnergyVariable
solver_sys = TKED_system
initial_condition = ${eps_init}
two_term_boundary_expansion = false
[]
[]
[FVKernels]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = ${mu}
momentum_component = 'x'
[]
[u_viscosity_turbulent]
type = INSFVMomentumDiffusion
variable = vel_x
mu = 'mu_t'
momentum_component = 'x'
complete_expansion = true
u = vel_x
v = vel_y
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
extra_vector_tags = ${pressure_tag}
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = ${mu}
momentum_component = 'y'
[]
[v_viscosity_turbulent]
type = INSFVMomentumDiffusion
variable = vel_y
mu = 'mu_t'
momentum_component = 'y'
complete_expansion = true
u = vel_x
v = vel_y
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
extra_vector_tags = ${pressure_tag}
[]
[p_diffusion]
type = FVAnisotropicDiffusion
variable = pressure
coeff = "Ainv"
coeff_interp_method = 'average'
[]
[p_source]
type = FVDivergence
variable = pressure
vector_field = "HbyA"
force_boundary_execution = true
[]
[TKE_advection]
type = INSFVTurbulentAdvection
variable = TKE
rho = ${rho}
[]
[TKE_diffusion]
type = INSFVTurbulentDiffusion
variable = TKE
coeff = ${mu}
[]
[TKE_diffusion_turbulent]
type = INSFVTurbulentDiffusion
variable = TKE
coeff = 'mu_t'
scaling_coef = ${sigma_k}
[]
[TKE_source_sink]
type = INSFVTKESourceSink
variable = TKE
u = vel_x
v = vel_y
epsilon = TKED
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
walls = ${walls}
wall_treatment = ${wall_treatment}
[]
[TKED_advection]
type = INSFVTurbulentAdvection
variable = TKED
rho = ${rho}
walls = ${walls}
[]
[TKED_diffusion]
type = INSFVTurbulentDiffusion
variable = TKED
coeff = ${mu}
walls = ${walls}
[]
[TKED_diffusion_turbulent]
type = INSFVTurbulentDiffusion
variable = TKED
coeff = 'mu_t'
scaling_coef = ${sigma_eps}
walls = ${walls}
[]
[TKED_source_sink]
type = INSFVTKEDSourceSink
variable = TKED
u = vel_x
v = vel_y
k = TKE
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
C1_eps = ${C1_eps}
C2_eps = ${C2_eps}
walls = ${walls}
wall_treatment = ${wall_treatment}
[]
[]
[FVBCs]
[top_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'top'
function = ${lid_velocity}
[]
[no_slip_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'left right bottom'
function = 0
[]
[no_slip_y]
type = INSFVNoSlipWallBC
variable = vel_y
boundary = 'left right top bottom'
function = 0
[]
[walls_mu_t]
type = INSFVTurbulentViscosityWallFunction
boundary = 'left right top bottom'
variable = mu_t
u = vel_x
v = vel_y
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
k = TKE
wall_treatment = ${wall_treatment}
[]
[walls_TKED]
type = INSFVTKEDWallFunctionBC
boundary = 'left right top bottom'
variable = TKED
u = vel_x
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
k = TKE
[]
[walls_TKE]
type = FVDirichletBC
boundary = 'left right top bottom'
variable = TKE
value = ${k_init}
[]
[]
[AuxVariables]
[mu_t]
type = MooseVariableFVReal
initial_condition = '${fparse rho * C_mu * ${k_init}^2 / eps_init}'
two_term_boundary_expansion = false
[]
[]
[AuxKernels]
[compute_mu_t]
type = kEpsilonViscosityAux
variable = mu_t
C_mu = ${C_mu}
k = TKE
epsilon = TKED
mu = ${mu}
rho = ${rho}
u = vel_x
v = vel_y
bulk_wall_treatment = ${bulk_wall_treatment}
walls = ${walls}
wall_treatment = ${wall_treatment}
execute_on = 'NONLINEAR'
[]
[]
[Executioner]
type = SIMPLENonlinearAssembly
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
turbulence_systems = 'TKED_system TKE_system'
pressure_gradient_tag = ${pressure_tag}
momentum_equation_relaxation = 0.7
pressure_variable_relaxation = 0.5
turbulence_equation_relaxation = '0.9 0.9'
num_iterations = 1000
pressure_absolute_tolerance = 1e-12
momentum_absolute_tolerance = 1e-12
turbulence_absolute_tolerance = '1e-12 1e-12'
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
momentum_l_abs_tol = 1e-14
pressure_l_abs_tol = 1e-14
turbulence_l_abs_tol = 1e-14
momentum_l_max_its = 30
pressure_l_max_its = 30
momentum_l_tol = 0.0
pressure_l_tol = 0.0
turbulence_l_tol = 0.0
print_fields = false
continue_on_max_its = true
pin_pressure = true
pressure_pin_value = 0.0
pressure_pin_point = '0.01 0.099 0.0'
[]
[Outputs]
csv = true
perf_graph = false
print_nonlinear_residuals = false
print_linear_residuals = true
[]
[VectorPostprocessors]
[side_bottom]
type = SideValueSampler
boundary = 'bottom'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_top]
type = SideValueSampler
boundary = 'top'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_left]
type = SideValueSampler
boundary = 'left'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[side_right]
type = SideValueSampler
boundary = 'right'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[horizontal_center]
type = LineValueSampler
start_point = '${fparse 0.01 * side_length} ${fparse 0.499 * side_length} 0'
end_point = '${fparse 0.99 * side_length} ${fparse 0.499 * side_length} 0'
num_points = ${Mesh/gen/nx}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[vertical_center]
type = LineValueSampler
start_point = '${fparse 0.499 * side_length} ${fparse 0.01 * side_length} 0'
end_point = '${fparse 0.499 * side_length} ${fparse 0.99 * side_length} 0'
num_points = ${Mesh/gen/ny}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/segregated/lid-driven-turb-non-eq-wall.i)
##########################################################
# Lid-driven cavity test
# Reynolds: 5,000
# Author: Dr. Mauricio Tano
# Last Update: November, 2023
# Turbulent model using:
# Standard wall functions with non-equilibrium wall formulation
# No wall functions
# SIMPLE Solve
##########################################################
### Thermophysical Properties ###
mu = 2e-5
rho = 1.0
### Operation Conditions ###
lid_velocity = 1.0
side_length = 0.1
### Initial Conditions ###
intensity = 0.01
k_init = '${fparse 1.5*(intensity * lid_velocity)^2}'
eps_init = '${fparse C_mu^0.75 * k_init^1.5 / side_length}'
### k-epsilon Closure Parameters ###
sigma_k = 1.0
sigma_eps = 1.3
C1_eps = 1.44
C2_eps = 1.92
C_mu = 0.09
### Modeling parameters ###
bulk_wall_treatment = false
walls = 'left top right bottom'
wall_treatment = 'neq' # Options: eq_newton, eq_incremental, eq_linearized, neq
pressure_tag = "pressure_grad"
[GlobalParams]
rhie_chow_user_object = 'rc'
advected_interp_method = 'upwind'
velocity_interp_method = 'rc'
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${side_length}
ymin = 0
ymax = ${side_length}
nx = 12
ny = 12
[]
# Prevent test diffing on distributed parallel element numbering
allow_renumbering = false
[]
[Problem]
nl_sys_names = 'u_system v_system pressure_system TKE_system TKED_system'
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolatorSegregated
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = 0.0
solver_sys = u_system
two_term_boundary_expansion = false
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 0.0
solver_sys = v_system
two_term_boundary_expansion = false
[]
[pressure]
type = INSFVPressureVariable
solver_sys = pressure_system
initial_condition = 0.2
two_term_boundary_expansion = false
[]
[TKE]
type = INSFVEnergyVariable
solver_sys = TKE_system
initial_condition = ${k_init}
two_term_boundary_expansion = false
[]
[TKED]
type = INSFVEnergyVariable
solver_sys = TKED_system
initial_condition = ${eps_init}
two_term_boundary_expansion = false
[]
[]
[FVKernels]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = ${mu}
momentum_component = 'x'
[]
[u_viscosity_turbulent]
type = INSFVMomentumDiffusion
variable = vel_x
mu = 'mu_t'
momentum_component = 'x'
complete_expansion = true
u = vel_x
v = vel_y
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
extra_vector_tags = ${pressure_tag}
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = ${mu}
momentum_component = 'y'
[]
[v_viscosity_turbulent]
type = INSFVMomentumDiffusion
variable = vel_y
mu = 'mu_t'
momentum_component = 'y'
complete_expansion = true
u = vel_x
v = vel_y
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
extra_vector_tags = ${pressure_tag}
[]
[p_diffusion]
type = FVAnisotropicDiffusion
variable = pressure
coeff = "Ainv"
coeff_interp_method = 'average'
[]
[p_source]
type = FVDivergence
variable = pressure
vector_field = "HbyA"
force_boundary_execution = true
[]
[TKE_advection]
type = INSFVTurbulentAdvection
variable = TKE
rho = ${rho}
[]
[TKE_diffusion]
type = INSFVTurbulentDiffusion
variable = TKE
coeff = ${mu}
[]
[TKE_diffusion_turbulent]
type = INSFVTurbulentDiffusion
variable = TKE
coeff = 'mu_t'
scaling_coef = ${sigma_k}
[]
[TKE_source_sink]
type = INSFVTKESourceSink
variable = TKE
u = vel_x
v = vel_y
epsilon = TKED
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
walls = ${walls}
wall_treatment = ${wall_treatment}
[]
[TKED_advection]
type = INSFVTurbulentAdvection
variable = TKED
rho = ${rho}
walls = ${walls}
[]
[TKED_diffusion]
type = INSFVTurbulentDiffusion
variable = TKED
coeff = ${mu}
walls = ${walls}
[]
[TKED_diffusion_turbulent]
type = INSFVTurbulentDiffusion
variable = TKED
coeff = 'mu_t'
scaling_coef = ${sigma_eps}
walls = ${walls}
[]
[TKED_source_sink]
type = INSFVTKEDSourceSink
variable = TKED
u = vel_x
v = vel_y
k = TKE
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
C1_eps = ${C1_eps}
C2_eps = ${C2_eps}
walls = ${walls}
wall_treatment = ${wall_treatment}
[]
[]
[FVBCs]
[top_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'top'
function = ${lid_velocity}
[]
[no_slip_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'left right bottom'
function = 0
[]
[no_slip_y]
type = INSFVNoSlipWallBC
variable = vel_y
boundary = 'left right top bottom'
function = 0
[]
[walls_mu_t]
type = INSFVTurbulentViscosityWallFunction
boundary = 'left right top bottom'
variable = mu_t
u = vel_x
v = vel_y
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
k = TKE
wall_treatment = ${wall_treatment}
[]
[]
[AuxVariables]
[mu_t]
type = MooseVariableFVReal
initial_condition = '${fparse rho * C_mu * ${k_init}^2 / eps_init}'
two_term_boundary_expansion = false
[]
[]
[AuxKernels]
[compute_mu_t]
type = kEpsilonViscosityAux
variable = mu_t
C_mu = ${C_mu}
k = TKE
epsilon = TKED
mu = ${mu}
rho = ${rho}
u = vel_x
v = vel_y
bulk_wall_treatment = ${bulk_wall_treatment}
walls = ${walls}
wall_treatment = ${wall_treatment}
execute_on = 'NONLINEAR'
[]
[]
[Executioner]
type = SIMPLENonlinearAssembly
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
turbulence_systems = 'TKED_system TKE_system'
pressure_gradient_tag = ${pressure_tag}
momentum_equation_relaxation = 0.8
pressure_variable_relaxation = 0.5
turbulence_equation_relaxation = '0.8 0.8'
num_iterations = 500
pressure_absolute_tolerance = 1e-12
momentum_absolute_tolerance = 1e-12
turbulence_absolute_tolerance = '1e-12 1e-12'
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
momentum_l_abs_tol = 1e-14
pressure_l_abs_tol = 1e-14
turbulence_l_abs_tol = 1e-14
momentum_l_max_its = 30
pressure_l_max_its = 30
momentum_l_tol = 0.0
pressure_l_tol = 0.0
turbulence_l_tol = 0.0
print_fields = false
continue_on_max_its = true
pin_pressure = true
pressure_pin_value = 0.0
pressure_pin_point = '0.01 0.099 0.0'
[]
[Outputs]
csv = true
perf_graph = false
print_nonlinear_residuals = false
print_linear_residuals = true
[]
[VectorPostprocessors]
[side_bottom]
type = SideValueSampler
boundary = 'bottom'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_top]
type = SideValueSampler
boundary = 'top'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_left]
type = SideValueSampler
boundary = 'left'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[side_right]
type = SideValueSampler
boundary = 'right'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[horizontal_center]
type = LineValueSampler
start_point = '${fparse 0.01 * side_length} ${fparse 0.499 * side_length} 0'
end_point = '${fparse 0.99 * side_length} ${fparse 0.499 * side_length} 0'
num_points = ${Mesh/gen/nx}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[vertical_center]
type = LineValueSampler
start_point = '${fparse 0.499 * side_length} ${fparse 0.01 * side_length} 0'
end_point = '${fparse 0.499 * side_length} ${fparse 0.99 * side_length} 0'
num_points = ${Mesh/gen/ny}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/turbulence/channel/segregated/channel_ERCOFTAC.i)
##########################################################
# ERCOFTAC test case foe turbulent channel flow
# Case Number: 032
# Author: Dr. Mauricio Tano
# Last Update: November, 2023
# Turbulent model using:
# k-epsilon model
# Equilibrium + Newton wall treatement
# SIMPLE solve
##########################################################
H = 1 #halfwidth of the channel
L = 100
Re = 13700
rho = 1
bulk_u = 1
mu = '${fparse rho * bulk_u * 2 * H / Re}'
advected_interp_method = 'upwind'
pressure_tag = "pressure_grad"
### k-epsilon Closure Parameters ###
sigma_k = 1.0
sigma_eps = 1.3
C1_eps = 1.44
C2_eps = 1.92
C_mu = 0.09
### Initial and Boundary Conditions ###
intensity = 0.01
k_init = '${fparse 1.5*(intensity * bulk_u)^2}'
eps_init = '${fparse C_mu^0.75 * k_init^1.5 / (2*H)}'
### Modeling parameters ###
bulk_wall_treatment = false
walls = 'top bottom'
wall_treatment = 'eq_newton' # Options: eq_newton, eq_incremental, eq_linearized, neq
[Mesh]
[block_1]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${L}
ymin = 0
ymax = ${H}
nx = 4
ny = 3
bias_y = 0.7
[]
[block_2]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${L}
ymin = ${fparse -H}
ymax = 0
nx = 4
ny = 3
bias_y = ${fparse 1/0.7}
[]
[smg]
type = StitchedMeshGenerator
inputs = 'block_1 block_2'
clear_stitched_boundary_ids = true
stitch_boundaries_pairs = 'bottom top'
merge_boundaries_with_same_name = true
[]
# Prevent test diffing on distributed parallel element numbering
allow_renumbering = false
[]
[Problem]
nl_sys_names = 'u_system v_system pressure_system TKE_system TKED_system'
previous_nl_solution_required = true
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolatorSegregated
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = ${bulk_u}
solver_sys = u_system
two_term_boundary_expansion = false
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 0
solver_sys = v_system
two_term_boundary_expansion = false
[]
[pressure]
type = INSFVPressureVariable
initial_condition = 1e-8
solver_sys = pressure_system
two_term_boundary_expansion = false
[]
[TKE]
type = INSFVEnergyVariable
solver_sys = TKE_system
initial_condition = ${k_init}
two_term_boundary_expansion = false
[]
[TKED]
type = INSFVEnergyVariable
solver_sys = TKED_system
initial_condition = ${eps_init}
two_term_boundary_expansion = false
[]
[]
[FVKernels]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = ${mu}
momentum_component = 'x'
[]
[u_viscosity_turbulent]
type = INSFVMomentumDiffusion
variable = vel_x
mu = 'mu_t'
momentum_component = 'x'
complete_expansion = no
u = vel_x
v = vel_y
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
extra_vector_tags = ${pressure_tag}
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = ${mu}
momentum_component = 'y'
[]
[v_viscosity_turbulent]
type = INSFVMomentumDiffusion
variable = vel_y
mu = 'mu_t'
momentum_component = 'y'
complete_expansion = no
u = vel_x
v = vel_y
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
extra_vector_tags = ${pressure_tag}
[]
[p_diffusion]
type = FVAnisotropicDiffusion
variable = pressure
coeff = "Ainv"
coeff_interp_method = 'average'
[]
[p_source]
type = FVDivergence
variable = pressure
vector_field = "HbyA"
force_boundary_execution = true
[]
[TKE_advection]
type = INSFVTurbulentAdvection
variable = TKE
rho = ${rho}
[]
[TKE_diffusion]
type = INSFVTurbulentDiffusion
variable = TKE
coeff = ${mu}
[]
[TKE_diffusion_turbulent]
type = INSFVTurbulentDiffusion
variable = TKE
coeff = 'mu_t'
scaling_coef = ${sigma_k}
[]
[TKE_source_sink]
type = INSFVTKESourceSink
variable = TKE
u = vel_x
v = vel_y
epsilon = TKED
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
walls = ${walls}
wall_treatment = ${wall_treatment}
C_pl = 1e10
[]
[TKED_advection]
type = INSFVTurbulentAdvection
variable = TKED
rho = ${rho}
walls = ${walls}
[]
[TKED_diffusion]
type = INSFVTurbulentDiffusion
variable = TKED
coeff = ${mu}
walls = ${walls}
[]
[TKED_diffusion_turbulent]
type = INSFVTurbulentDiffusion
variable = TKED
coeff = 'mu_t'
scaling_coef = ${sigma_eps}
walls = ${walls}
[]
[TKED_source_sink]
type = INSFVTKEDSourceSink
variable = TKED
u = vel_x
v = vel_y
k = TKE
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
C1_eps = ${C1_eps}
C2_eps = ${C2_eps}
walls = ${walls}
wall_treatment = ${wall_treatment}
C_pl = 1e10
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_x
function = '${bulk_u}'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_y
function = 0
[]
[walls-u]
type = FVDirichletBC
boundary = 'bottom top'
variable = vel_x
value = 0
[]
[walls-v]
type = FVDirichletBC
boundary = 'bottom top'
variable = vel_y
value = 0
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 0
[]
[inlet_TKE]
type = FVDirichletBC
boundary = 'left'
variable = TKE
value = '${k_init}'
[]
[inlet_TKED]
type = FVDirichletBC
boundary = 'left'
variable = TKED
value = '${eps_init}'
[]
[walls_mu_t]
type = INSFVTurbulentViscosityWallFunction
boundary = 'bottom top'
variable = mu_t
u = vel_x
v = vel_y
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
k = TKE
wall_treatment = ${wall_treatment}
[]
[]
[AuxVariables]
[mu_t]
type = MooseVariableFVReal
initial_condition = '${fparse rho * C_mu * ${k_init}^2 / eps_init}'
two_term_boundary_expansion = false
[]
[yplus]
type = MooseVariableFVReal
two_term_boundary_expansion = false
[]
[]
[AuxKernels]
[compute_mu_t]
type = kEpsilonViscosityAux
variable = mu_t
C_mu = ${C_mu}
k = TKE
epsilon = TKED
mu = ${mu}
rho = ${rho}
u = vel_x
v = vel_y
bulk_wall_treatment = ${bulk_wall_treatment}
walls = ${walls}
wall_treatment = ${wall_treatment}
execute_on = 'NONLINEAR'
mu_t_ratio_max = 1e20
[]
[compute_y_plus]
type = RANSYPlusAux
variable = yplus
k = TKE
mu = ${mu}
rho = ${rho}
u = vel_x
v = vel_y
walls = ${walls}
wall_treatment = ${wall_treatment}
execute_on = 'NONLINEAR'
[]
[]
[Executioner]
type = SIMPLENonlinearAssembly
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
turbulence_systems = 'TKE_system TKED_system'
pressure_gradient_tag = ${pressure_tag}
momentum_equation_relaxation = 0.7
pressure_variable_relaxation = 0.3
turbulence_equation_relaxation = '0.2 0.2'
num_iterations = 1000
pressure_absolute_tolerance = 1e-12
momentum_absolute_tolerance = 1e-12
turbulence_absolute_tolerance = '1e-12 1e-12'
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
momentum_l_abs_tol = 1e-14
pressure_l_abs_tol = 1e-14
turbulence_l_abs_tol = 1e-14
momentum_l_max_its = 30
pressure_l_max_its = 30
momentum_l_tol = 0.0
pressure_l_tol = 0.0
turbulence_l_tol = 0.0
print_fields = false
continue_on_max_its = true
[]
[Outputs]
csv = true
[]
[VectorPostprocessors]
[side_bottom]
type = SideValueSampler
boundary = 'bottom'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_top]
type = SideValueSampler
boundary = 'top'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[line_center_channel]
type = LineValueSampler
start_point = '${fparse 0.125 * L} ${fparse 0.0001} 0'
end_point = '${fparse 0.875 * L} ${fparse 0.0001} 0'
num_points = ${Mesh/block_1/nx}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[line_quarter_radius_channel]
type = LineValueSampler
start_point = '${fparse 0.125 * L} ${fparse 0.5 * H} 0'
end_point = '${fparse 0.875 * L} ${fparse 0.5 * H} 0'
num_points = ${Mesh/block_1/nx}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[]
(test/tests/userobjects/layered_side_integral_functor/layered_side_integral_functor.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 40
ny = 10
nz = 10
allow_renumbering = false
[]
[Materials]
[u_mat]
type = GenericFunctorMaterial
prop_names = 'u'
prop_values = 'u_fn'
[]
[]
[AuxVariables]
[u_layered_average]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[u_layered_average_kern]
type = SpatialUserObjectAux
variable = u_layered_average
user_object = nplaf
boundary = 'bottom top'
execute_on = 'INITIAL'
[]
[]
[Functions]
[u_fn]
type = ParsedFunction
expression = 'x + y + z'
[]
[]
[UserObjects]
[nplaf]
type = LayeredSideIntegralFunctor
direction = x
num_layers = 10
functor = u
boundary = 'bottom top'
execute_on = 'INITIAL'
[]
[]
[VectorPostprocessors]
[test_vpp]
type = SideValueSampler
variable = u_layered_average
boundary = 'bottom top'
sort_by = id
execute_on = 'INITIAL'
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
execute_on = 'INITIAL'
[]
(modules/porous_flow/test/tests/dirackernels/theis1.i)
# Theis problem: Flow to single sink
# SinglePhase
# Cartesian mesh with logarithmic distribution in x and y.
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
bias_x = 1.1
bias_y = 1.1
ymax = 100
xmax = 100
# To get consistent ordering of results with distributed meshes
allow_renumbering = false
[]
[GlobalParams]
PorousFlowDictator = dictator
compute_enthalpy = false
compute_internal_energy = false
[]
[Variables]
[pp]
[]
[]
[Kernels]
[mass0]
type = PorousFlowMassTimeDerivative
fluid_component = 0
variable = pp
[]
[flux]
type = PorousFlowAdvectiveFlux
variable = pp
gravity = '0 0 0'
fluid_component = 0
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureVG
m = 0.5
alpha = 1e-7
[]
[]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 2e9
density0 = 1000
viscosity = 0.001
thermal_expansion = 0
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pp
capillary_pressure = pc
[]
[massfrac]
type = PorousFlowMassFraction
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[porosity]
type = PorousFlowPorosityConst
porosity = 0.2
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1E-14 0 0 0 1E-14 0 0 0 1E-14'
[]
[relperm]
type = PorousFlowRelativePermeabilityCorey
n = 0
phase = 0
[]
[]
[Postprocessors]
[porepressure]
type = PointValue
point = '0 0 0'
variable = pp
execute_on = 'initial timestep_end'
[]
[total_mass]
type = PorousFlowFluidMass
execute_on = 'initial timestep_end'
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = Newton
dt = 200
end_time = 1E3
nl_abs_tol = 1e-10
[]
[Outputs]
perf_graph = true
file_base = theis1
[csv]
type = CSV
execute_on = final
[]
[]
[ICs]
[PressureIC]
variable = pp
type = ConstantIC
value = 20e6
[]
[]
[DiracKernels]
[sink]
type = PorousFlowSquarePulsePointSource
end_time = 1000
point = '0 0 0'
mass_flux = -0.04
variable = pp
[]
[]
[BCs]
[right]
type = DirichletBC
variable = pp
value = 20e6
boundary = right
[]
[top]
type = DirichletBC
variable = pp
value = 20e6
boundary = top
[]
[]
[VectorPostprocessors]
[pressure]
type = SideValueSampler
variable = pp
sort_by = x
execute_on = timestep_end
boundary = bottom
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/segregated/lid-driven-turb-inc-wall.i)
##########################################################
# Lid-driven cavity test
# Reynolds: 5,000
# Author: Dr. Mauricio Tano
# Last Update: November, 2023
# Turbulent model using:
# k-epsilon model
# Incremental wall function formulation (similar to OpenFOAM)
# SIMPLE Solve
##########################################################
### Thermophysical Properties ###
mu = 2e-5
rho = 1.0
### Operation Conditions ###
lid_velocity = 1.0
side_length = 0.1
### Initial Conditions ###
intensity = 0.01
k_init = '${fparse 1.5*(intensity * lid_velocity)^2}'
eps_init = '${fparse C_mu^0.75 * k_init^1.5 / side_length}'
### k-epsilon Closure Parameters ###
sigma_k = 1.0
sigma_eps = 1.3
C1_eps = 1.44
C2_eps = 1.92
C_mu = 0.09
### Modeling parameters ###
bulk_wall_treatment = false
walls = 'left top right bottom'
wall_treatment = 'eq_incremental' # Options: eq_newton, eq_incremental, eq_linearized, neq
pressure_tag = "pressure_grad"
[GlobalParams]
rhie_chow_user_object = 'rc'
advected_interp_method = 'upwind'
velocity_interp_method = 'rc'
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${side_length}
ymin = 0
ymax = ${side_length}
nx = 12
ny = 12
[]
# Prevent test diffing on distributed parallel element numbering
allow_renumbering = false
[]
[Problem]
nl_sys_names = 'u_system v_system pressure_system TKE_system TKED_system'
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolatorSegregated
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = 0.0
solver_sys = u_system
two_term_boundary_expansion = false
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 0.0
solver_sys = v_system
two_term_boundary_expansion = false
[]
[pressure]
type = INSFVPressureVariable
solver_sys = pressure_system
initial_condition = 0.2
two_term_boundary_expansion = false
[]
[TKE]
type = INSFVEnergyVariable
solver_sys = TKE_system
initial_condition = ${k_init}
two_term_boundary_expansion = false
[]
[TKED]
type = INSFVEnergyVariable
solver_sys = TKED_system
initial_condition = ${eps_init}
two_term_boundary_expansion = false
[]
[]
[FVKernels]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = ${mu}
momentum_component = 'x'
[]
[u_viscosity_turbulent]
type = INSFVMomentumDiffusion
variable = vel_x
mu = 'mu_t'
momentum_component = 'x'
complete_expansion = true
u = vel_x
v = vel_y
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
extra_vector_tags = ${pressure_tag}
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = ${mu}
momentum_component = 'y'
[]
[v_viscosity_turbulent]
type = INSFVMomentumDiffusion
variable = vel_y
mu = 'mu_t'
momentum_component = 'y'
complete_expansion = true
u = vel_x
v = vel_y
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
extra_vector_tags = ${pressure_tag}
[]
[p_diffusion]
type = FVAnisotropicDiffusion
variable = pressure
coeff = "Ainv"
coeff_interp_method = 'average'
[]
[p_source]
type = FVDivergence
variable = pressure
vector_field = "HbyA"
force_boundary_execution = true
[]
[TKE_advection]
type = INSFVTurbulentAdvection
variable = TKE
rho = ${rho}
[]
[TKE_diffusion]
type = INSFVTurbulentDiffusion
variable = TKE
coeff = ${mu}
[]
[TKE_diffusion_turbulent]
type = INSFVTurbulentDiffusion
variable = TKE
coeff = 'mu_t'
scaling_coef = ${sigma_k}
[]
[TKE_source_sink]
type = INSFVTKESourceSink
variable = TKE
u = vel_x
v = vel_y
epsilon = TKED
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
walls = ${walls}
wall_treatment = ${wall_treatment}
[]
[TKED_advection]
type = INSFVTurbulentAdvection
variable = TKED
rho = ${rho}
walls = ${walls}
[]
[TKED_diffusion]
type = INSFVTurbulentDiffusion
variable = TKED
coeff = ${mu}
walls = ${walls}
[]
[TKED_diffusion_turbulent]
type = INSFVTurbulentDiffusion
variable = TKED
coeff = 'mu_t'
scaling_coef = ${sigma_eps}
walls = ${walls}
[]
[TKED_source_sink]
type = INSFVTKEDSourceSink
variable = TKED
u = vel_x
v = vel_y
k = TKE
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
C1_eps = ${C1_eps}
C2_eps = ${C2_eps}
walls = ${walls}
wall_treatment = ${wall_treatment}
[]
[]
[FVBCs]
[top_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'top'
function = ${lid_velocity}
[]
[no_slip_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'left right bottom'
function = 0
[]
[no_slip_y]
type = INSFVNoSlipWallBC
variable = vel_y
boundary = 'left right top bottom'
function = 0
[]
[walls_mu_t]
type = INSFVTurbulentViscosityWallFunction
boundary = 'left right top bottom'
variable = mu_t
u = vel_x
v = vel_y
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
k = TKE
wall_treatment = ${wall_treatment}
[]
[]
[AuxVariables]
[mu_t]
type = MooseVariableFVReal
initial_condition = '${fparse rho * C_mu * ${k_init}^2 / eps_init}'
two_term_boundary_expansion = false
[]
[]
[AuxKernels]
[compute_mu_t]
type = kEpsilonViscosityAux
variable = mu_t
C_mu = ${C_mu}
k = TKE
epsilon = TKED
mu = ${mu}
rho = ${rho}
u = vel_x
v = vel_y
bulk_wall_treatment = ${bulk_wall_treatment}
walls = ${walls}
wall_treatment = ${wall_treatment}
execute_on = 'NONLINEAR'
[]
[]
[Executioner]
type = SIMPLENonlinearAssembly
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
turbulence_systems = 'TKED_system TKE_system'
pressure_gradient_tag = ${pressure_tag}
momentum_equation_relaxation = 0.8
pressure_variable_relaxation = 0.5
turbulence_equation_relaxation = '0.8 0.8'
num_iterations = 500
pressure_absolute_tolerance = 1e-12
momentum_absolute_tolerance = 1e-12
turbulence_absolute_tolerance = '1e-12 1e-12'
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
momentum_l_abs_tol = 1e-14
pressure_l_abs_tol = 1e-14
turbulence_l_abs_tol = 1e-14
momentum_l_max_its = 30
pressure_l_max_its = 30
momentum_l_tol = 0.0
pressure_l_tol = 0.0
turbulence_l_tol = 0.0
print_fields = false
continue_on_max_its = true
pin_pressure = true
pressure_pin_value = 0.0
pressure_pin_point = '0.01 0.099 0.0'
[]
[Outputs]
csv = true
perf_graph = false
print_nonlinear_residuals = false
print_linear_residuals = true
[]
[VectorPostprocessors]
[side_bottom]
type = SideValueSampler
boundary = 'bottom'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_top]
type = SideValueSampler
boundary = 'top'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_left]
type = SideValueSampler
boundary = 'left'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[side_right]
type = SideValueSampler
boundary = 'right'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[horizontal_center]
type = LineValueSampler
start_point = '${fparse 0.01 * side_length} ${fparse 0.499 * side_length} 0'
end_point = '${fparse 0.99 * side_length} ${fparse 0.499 * side_length} 0'
num_points = ${Mesh/gen/nx}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[vertical_center]
type = LineValueSampler
start_point = '${fparse 0.499 * side_length} ${fparse 0.01 * side_length} 0'
end_point = '${fparse 0.499 * side_length} ${fparse 0.99 * side_length} 0'
num_points = ${Mesh/gen/ny}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/segregated/lid-driven-turb-capped.i)
##########################################################
# Lid-driven cavity test
# Reynolds: 5,000
# Author: Dr. Mauricio Tano
# Last Update: November, 2023
# Turbulent model using:
# k-epsilon model with capped mixing length
# Standard wall functions
# SIMPLE Solve
##########################################################
### Thermophysical Properties ###
mu = 2e-5
rho = 1.0
### Operation Conditions ###
lid_velocity = 1.0
side_length = 0.1
### Initial Conditions ###
intensity = 0.01
k_init = '${fparse 1.5*(intensity * lid_velocity)^2}'
eps_init = '${fparse C_mu^0.75 * k_init^1.5 / side_length}'
### k-epsilon Closure Parameters ###
sigma_k = 1.0
sigma_eps = 1.3
C1_eps = 1.44
C2_eps = 1.92
C_mu = 0.09
C_pl = 0.1
### Modeling parameters ###
bulk_wall_treatment = false
walls = 'left top right bottom'
wall_treatment = 'eq_newton' # Options: eq_newton, eq_incremental, eq_linearized, neq
pressure_tag = "pressure_grad"
[GlobalParams]
rhie_chow_user_object = 'rc'
advected_interp_method = 'upwind'
velocity_interp_method = 'rc'
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${side_length}
ymin = 0
ymax = ${side_length}
nx = 12
ny = 12
[]
[break_symmetries]
type = ParsedNodeTransformGenerator
input = gen
constant_names = 'side_length'
constant_expressions = '${side_length}'
x_function = 'if(x<side_length*1.001 / 2 & x > side_length * 0.999 / 2, x * 1.05, x)'
y_function = 'if(y<side_length*1.001 / 2 & y > side_length * 0.999 / 2, y * 1.05, y)'
[]
# Prevent test diffing on distributed parallel element numbering
allow_renumbering = false
[]
[Problem]
nl_sys_names = 'u_system v_system pressure_system TKE_system TKED_system'
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolatorSegregated
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
solver_sys = u_system
two_term_boundary_expansion = false
[]
[vel_y]
type = INSFVVelocityVariable
solver_sys = v_system
two_term_boundary_expansion = false
[]
[pressure]
type = INSFVPressureVariable
solver_sys = pressure_system
initial_condition = 0.2
two_term_boundary_expansion = false
[]
[TKE]
type = INSFVEnergyVariable
solver_sys = TKE_system
initial_condition = ${k_init}
two_term_boundary_expansion = false
[]
[TKED]
type = INSFVEnergyVariable
solver_sys = TKED_system
initial_condition = ${eps_init}
two_term_boundary_expansion = false
[]
[]
[ICs]
[vx]
type = FunctionIC
variable = vel_x
function = 'if(y>0.09, 0.1, -0.001)'
[]
[vy]
type = FunctionIC
variable = vel_y
function = 'if(x>0.05, -0.001, 0.001)'
[]
[]
[FVKernels]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = ${mu}
momentum_component = 'x'
[]
[u_viscosity_turbulent]
type = INSFVMomentumDiffusion
variable = vel_x
mu = 'mu_t'
momentum_component = 'x'
complete_expansion = true
u = vel_x
v = vel_y
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
extra_vector_tags = ${pressure_tag}
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = ${mu}
momentum_component = 'y'
[]
[v_viscosity_turbulent]
type = INSFVMomentumDiffusion
variable = vel_y
mu = 'mu_t'
momentum_component = 'y'
complete_expansion = true
u = vel_x
v = vel_y
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
extra_vector_tags = ${pressure_tag}
[]
[p_diffusion]
type = FVAnisotropicDiffusion
variable = pressure
coeff = "Ainv"
coeff_interp_method = 'average'
[]
[p_source]
type = FVDivergence
variable = pressure
vector_field = "HbyA"
force_boundary_execution = true
[]
[TKE_advection]
type = INSFVTurbulentAdvection
variable = TKE
rho = ${rho}
[]
[TKE_diffusion]
type = INSFVTurbulentDiffusion
variable = TKE
coeff = ${mu}
[]
[TKE_diffusion_turbulent]
type = INSFVTurbulentDiffusion
variable = TKE
coeff = 'mu_t'
scaling_coef = ${sigma_k}
[]
[TKE_source_sink]
type = INSFVTKESourceSink
variable = TKE
u = vel_x
v = vel_y
epsilon = TKED
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
C_pl = ${C_pl}
walls = ${walls}
wall_treatment = ${wall_treatment}
[]
[TKED_advection]
type = INSFVTurbulentAdvection
variable = TKED
rho = ${rho}
walls = ${walls}
[]
[TKED_diffusion]
type = INSFVTurbulentDiffusion
variable = TKED
coeff = ${mu}
walls = ${walls}
[]
[TKED_diffusion_turbulent]
type = INSFVTurbulentDiffusion
variable = TKED
coeff = 'mu_t'
scaling_coef = ${sigma_eps}
walls = ${walls}
[]
[TKED_source_sink]
type = INSFVTKEDSourceSink
variable = TKED
u = vel_x
v = vel_y
k = TKE
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
C1_eps = ${C1_eps}
C2_eps = ${C2_eps}
C_pl = ${C_pl}
walls = ${walls}
wall_treatment = ${wall_treatment}
[]
[]
[FVBCs]
[top_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'top'
function = ${lid_velocity}
[]
[no_slip_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'left right bottom'
function = 0
[]
[no_slip_y]
type = INSFVNoSlipWallBC
variable = vel_y
boundary = 'left right top bottom'
function = 0
[]
[walls_mu_t]
type = INSFVTurbulentViscosityWallFunction
boundary = 'left right top bottom'
variable = mu_t
u = vel_x
v = vel_y
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
k = TKE
wall_treatment = ${wall_treatment}
[]
[]
[AuxVariables]
[mu_t]
type = MooseVariableFVReal
initial_condition = '${fparse rho * C_mu * ${k_init}^2 / eps_init}'
two_term_boundary_expansion = false
[]
[]
[AuxKernels]
[compute_mu_t]
type = kEpsilonViscosityAux
variable = mu_t
C_mu = ${C_mu}
k = TKE
epsilon = TKED
mu = ${mu}
rho = ${rho}
u = vel_x
v = vel_y
bulk_wall_treatment = ${bulk_wall_treatment}
walls = ${walls}
wall_treatment = ${wall_treatment}
execute_on = 'NONLINEAR'
[]
[]
[Executioner]
type = SIMPLENonlinearAssembly
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
turbulence_systems = 'TKED_system TKE_system'
pressure_gradient_tag = ${pressure_tag}
momentum_equation_relaxation = 0.8
pressure_variable_relaxation = 0.5
turbulence_equation_relaxation = '0.8 0.8'
num_iterations = 500
pressure_absolute_tolerance = 1e-12
momentum_absolute_tolerance = 1e-12
turbulence_absolute_tolerance = '1e-12 1e-12'
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
momentum_l_abs_tol = 1e-14
pressure_l_abs_tol = 1e-14
turbulence_l_abs_tol = 1e-14
momentum_l_max_its = 30
pressure_l_max_its = 30
momentum_l_tol = 0.0
pressure_l_tol = 0.0
turbulence_l_tol = 0.0
print_fields = false
pin_pressure = true
pressure_pin_value = 0.0
pressure_pin_point = '0.01 0.099 0.0'
continue_on_max_its = true
[]
[Outputs]
csv = true
perf_graph = false
print_nonlinear_residuals = false
print_linear_residuals = true
[]
[VectorPostprocessors]
[side_bottom]
type = SideValueSampler
boundary = 'bottom'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_top]
type = SideValueSampler
boundary = 'top'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_left]
type = SideValueSampler
boundary = 'left'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[side_right]
type = SideValueSampler
boundary = 'right'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[horizontal_center]
type = LineValueSampler
start_point = '${fparse 0.01 * side_length} ${fparse 0.499 * side_length} 0'
end_point = '${fparse 0.99 * side_length} ${fparse 0.499 * side_length} 0'
num_points = ${Mesh/gen/nx}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[vertical_center]
type = LineValueSampler
start_point = '${fparse 0.499 * side_length} ${fparse 0.01 * side_length} 0'
end_point = '${fparse 0.499 * side_length} ${fparse 0.99 * side_length} 0'
num_points = ${Mesh/gen/ny}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[]
(test/tests/vectorpostprocessors/side_value_sampler/side_value_sampler_fv.i)
[Mesh]
[mesh]
type = CartesianMeshGenerator
dim = 2
dx = '0.5 0.5'
dy = '1'
ix = '5 5'
iy = '10'
subdomain_id = '1 1'
[]
# Limited to 1 side to avoid inconsistencies in parallel
[internal_sideset]
type = ParsedGenerateSideset
combinatorial_geometry = 'y<0.51 & y>0.49 & x<0.11'
new_sideset_name = 'center'
input = 'mesh'
[]
# this keeps numbering continuous so tests dont fail on different ids in CSV
allow_renumbering = false
[]
[Problem]
nl_sys_names = 'u_sys'
linear_sys_names = 'v_sys'
[]
[Variables]
[u]
type = MooseVariableFVReal
solver_sys = u_sys
[]
[v]
type = MooseLinearVariableFVReal
solver_sys = v_sys
[]
[]
[FVKernels]
[diff]
type = FVDiffusion
variable = u
coeff = 1.0
[]
[]
[LinearFVKernels]
[diff]
type = LinearFVDiffusion
variable = v
[]
[]
[FVBCs]
[all]
type = FVFunctorDirichletBC
variable = u
boundary = 'top bottom left right'
functor = linear_x
[]
[]
[LinearFVBCs]
[all]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = v
boundary = 'top bottom left right'
functor = linear_x
[]
[]
[Functions]
[linear_x]
type = ParsedFunction
expression = '5*x'
[]
[]
[VectorPostprocessors]
[side_sample]
type = SideValueSampler
variable = 'u v'
boundary = top
sort_by = x
[]
[internal_sample]
type = SideValueSampler
variable = 'u v'
boundary = center
sort_by = 'id'
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
system_names = 'u_sys v_sys'
l_tol = 1e-8
[]
[Outputs]
execute_on = 'timestep_end'
[vpp_csv]
type = CSV
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/turbulence/bfs/linear-segregated/BFS_ERCOFTAC.i)
Re = 5100
rho = 1.0
bulk_u = 1.0
H = 1.0
mu = '${fparse rho * bulk_u * H / Re}'
advected_interp_method = 'upwind'
### k-epsilon Closure Parameters ###
sigma_k = 1.0
sigma_eps = 1.3
C1_eps = 1.44
C2_eps = 1.92
C_mu = 0.09
### Initial and Boundary Conditions ###
intensity = 0.01
k_init = '${fparse 1.5*(intensity * bulk_u)^2}'
eps_init = '${fparse C_mu^0.75 * k_init^1.5 / H}'
### Modeling parameters ###
bulk_wall_treatment = false
walls = 'bottom wall-side top'
wall_treatment = 'eq_incremental' # Options: eq_newton, eq_incremental, eq_linearized, neq
[Mesh]
[gen]
type = CartesianMeshGenerator
dim = 2
dx = '${fparse 10.0*H} ${fparse 20.0*H}'
dy = '${H} ${fparse 5*H}'
ix = '8 16'
iy = '2 8'
subdomain_id = '
2 1
1 1
'
[]
[corner_walls]
type = SideSetsBetweenSubdomainsGenerator
input = gen
primary_block = '1'
paired_block = '2'
new_boundary = 'wall-side'
[]
[delete_bottom]
type = BlockDeletionGenerator
input = corner_walls
block = '2'
[]
# Prevent test diffing on distributed parallel element numbering
allow_renumbering = false
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system TKE_system TKED_system'
previous_nl_solution_required = true
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
advected_interp_method = ${advected_interp_method}
[]
[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 = ${bulk_u}
solver_sys = u_system
[]
[vel_y]
type = MooseLinearVariableFVReal
initial_condition = 0
solver_sys = v_system
[]
[pressure]
type = MooseLinearVariableFVReal
initial_condition = 1e-8
solver_sys = pressure_system
[]
[TKE]
type = MooseLinearVariableFVReal
solver_sys = TKE_system
initial_condition = ${k_init}
[]
[TKED]
type = MooseLinearVariableFVReal
solver_sys = TKED_system
initial_condition = ${eps_init}
[]
[]
[LinearFVKernels]
[u_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_x
advected_interp_method = ${advected_interp_method}
mu = 'mu_t'
u = vel_x
v = vel_y
momentum_component = 'x'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
use_deviatoric_terms = yes
[]
[u_diffusion]
type = LinearFVDiffusion
variable = vel_x
diffusion_coeff = ${mu}
use_nonorthogonal_correction = false
[]
[u_pressure]
type = LinearFVMomentumPressure
variable = vel_x
pressure = pressure
momentum_component = 'x'
[]
[v_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_y
advected_interp_method = ${advected_interp_method}
mu = 'mu_t'
u = vel_x
v = vel_y
momentum_component = 'y'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
use_deviatoric_terms = yes
[]
[v_diffusion]
type = LinearFVDiffusion
variable = vel_y
diffusion_coeff = ${mu}
use_nonorthogonal_correction = false
[]
[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
[]
[TKE_advection]
type = LinearFVTurbulentAdvection
variable = TKE
[]
[TKE_diffusion]
type = LinearFVTurbulentDiffusion
variable = TKE
diffusion_coeff = ${mu}
use_nonorthogonal_correction = false
[]
[TKE_turb_diffusion]
type = LinearFVTurbulentDiffusion
variable = TKE
diffusion_coeff = 'mu_t'
scaling_coeff = ${sigma_k}
use_nonorthogonal_correction = false
[]
[TKE_source_sink]
type = LinearFVTKESourceSink
variable = TKE
u = vel_x
v = vel_y
epsilon = TKED
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
walls = ${walls}
wall_treatment = ${wall_treatment}
C_pl = 1e10
[]
[TKED_advection]
type = LinearFVTurbulentAdvection
variable = TKED
walls = ${walls}
[]
[TKED_diffusion]
type = LinearFVTurbulentDiffusion
variable = TKED
diffusion_coeff = ${mu}
use_nonorthogonal_correction = false
walls = ${walls}
[]
[TKED_turb_diffusion]
type = LinearFVTurbulentDiffusion
variable = TKED
diffusion_coeff = 'mu_t'
scaling_coeff = ${sigma_eps}
use_nonorthogonal_correction = false
walls = ${walls}
[]
[TKED_source_sink]
type = LinearFVTKEDSourceSink
variable = TKED
u = vel_x
v = vel_y
tke = TKE
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
C1_eps = ${C1_eps}
C2_eps = ${C2_eps}
walls = ${walls}
wall_treatment = ${wall_treatment}
C_pl = 1e10
[]
[]
[LinearFVBCs]
[inlet-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_x
functor = '${bulk_u}'
[]
[inlet-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_y
functor = '0.0'
[]
[inlet_TKE]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = TKE
functor = '${k_init}'
[]
[inlet_TKED]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = TKED
functor = '${eps_init}'
[]
[outlet_p]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'right'
variable = pressure
functor = 0.0
[]
[outlet_u]
type = LinearFVAdvectionDiffusionOutflowBC
boundary = 'right'
variable = vel_x
use_two_term_expansion = false
[]
[outlet_v]
type = LinearFVAdvectionDiffusionOutflowBC
boundary = 'right'
variable = vel_y
use_two_term_expansion = false
[]
[outlet_TKE]
type = LinearFVAdvectionDiffusionOutflowBC
boundary = 'right'
variable = TKE
use_two_term_expansion = false
[]
[outlet_TKED]
type = LinearFVAdvectionDiffusionOutflowBC
boundary = 'right'
variable = TKED
use_two_term_expansion = false
[]
[walls-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = ${walls}
variable = vel_x
functor = 0.0
[]
[walls-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = ${walls}
variable = vel_y
functor = 0.0
[]
[walls_mu_t]
type = LinearFVTurbulentViscosityWallFunctionBC
boundary = ${walls}
variable = 'mu_t'
u = vel_x
v = vel_y
rho = ${rho}
mu = ${mu}
tke = TKE
wall_treatment = ${wall_treatment}
[]
[]
[AuxVariables]
[mu_t]
type = MooseLinearVariableFVReal
initial_condition = '${fparse rho * C_mu * ${k_init}^2 / eps_init}'
[]
[yplus]
type = MooseLinearVariableFVReal
[]
[mu_eff]
type = MooseLinearVariableFVReal
initial_condition = '${fparse rho * C_mu * ${k_init}^2 / eps_init + mu}'
[]
[]
[AuxKernels]
[compute_mu_t]
type = kEpsilonViscosityAux
variable = mu_t
C_mu = ${C_mu}
tke = TKE
epsilon = TKED
mu = ${mu}
rho = ${rho}
u = vel_x
v = vel_y
bulk_wall_treatment = ${bulk_wall_treatment}
walls = ${walls}
wall_treatment = ${wall_treatment}
execute_on = 'NONLINEAR'
mu_t_ratio_max = 1e20
[]
[compute_y_plus]
type = RANSYPlusAux
variable = yplus
tke = TKE
mu = ${mu}
rho = ${rho}
u = vel_x
v = vel_y
walls = ${walls}
wall_treatment = ${wall_treatment}
execute_on = 'NONLINEAR'
[]
[compute_mu_eff]
type = ParsedAux
variable = 'mu_eff'
coupled_variables = 'mu_t'
expression = 'mu_t + ${mu}'
execute_on = 'NONLINEAR'
[]
[]
[Executioner]
type = SIMPLE
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
turbulence_systems = 'TKE_system TKED_system'
momentum_l_abs_tol = 1e-14
pressure_l_abs_tol = 1e-14
turbulence_l_abs_tol = 1e-14
momentum_l_tol = 1e-14
pressure_l_tol = 1e-14
turbulence_l_tol = 1e-14
momentum_equation_relaxation = 0.7
pressure_variable_relaxation = 0.3
turbulence_equation_relaxation = '0.5 0.5'
num_iterations = 1000
pressure_absolute_tolerance = 1e-12
momentum_absolute_tolerance = 1e-12
turbulence_absolute_tolerance = '1e-12 1e-12'
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
turbulence_petsc_options_iname = '-pc_type -pc_hypre_type'
turbulence_petsc_options_value = 'hypre boomeramg'
print_fields = false
continue_on_max_its = true
[]
[Outputs]
csv = true
[console]
type = Console
outlier_variable_norms = false
[]
[]
[VectorPostprocessors]
[side_bottom]
type = SideValueSampler
boundary = 'bottom'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_top]
type = SideValueSampler
boundary = 'top'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[line_entry_channel_wall]
type = LineValueSampler
start_point = '${fparse 0.5 * H} ${fparse 1.00001 * H} 0'
end_point = '${fparse 29.5 * H} ${fparse 1.00001 * H} 0'
num_points = 24
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[line_quarter_entry_channel]
type = LineValueSampler
start_point = '${fparse 0.5 * H} ${fparse 2.25001 * H} 0'
end_point = '${fparse 29.5 * H} ${fparse 2.25001 * H} 0'
num_points = 24
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[]
(test/tests/userobjects/nearest_point_layered_side_integral_functor/nearest_point_layered_side_integral_functor.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 40
ny = 10
nz = 10
allow_renumbering = false
[]
[Materials]
[u_mat]
type = GenericFunctorMaterial
prop_names = 'u'
prop_values = 'u_fn'
[]
[]
[AuxVariables]
[u_layered_integral]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[u_layered_integral_kern]
type = SpatialUserObjectAux
variable = u_layered_integral
user_object = nplaf
boundary = 'bottom top'
execute_on = 'INITIAL'
[]
[]
[Functions]
[u_fn]
type = ParsedFunction
expression = 'x + y + z'
[]
[]
[UserObjects]
[nplaf]
type = NearestPointLayeredSideIntegralFunctor
direction = x
points='
0.25 0 0.25
0.75 0 0.25
0.25 0 0.75
0.75 0 0.75'
# Each layer has exactly 4 elements in the x direction. Note that to avoid inconsistent
# results, we should always avoid aligning layer edges with element centroids.
num_layers = 10
functor = u
boundary = 'bottom top'
execute_on = 'INITIAL'
[]
[]
[VectorPostprocessors]
[test_vpp]
type = SideValueSampler
variable = u_layered_integral
boundary = 'bottom top'
sort_by = id
execute_on = 'INITIAL'
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
execute_on = 'INITIAL'
[]
(modules/navier_stokes/test/tests/finite_volume/ins/turbulence/channel/linear-segregated/channel_ERCOFTAC.i)
H = 1 #halfwidth of the channel
L = 100
Re = 13700
rho = 1
bulk_u = 1
mu = '${fparse rho * bulk_u * 2 * H / Re}'
advected_interp_method = 'upwind'
### k-epsilon Closure Parameters ###
sigma_k = 1.0
sigma_eps = 1.3
C1_eps = 1.44
C2_eps = 1.92
C_mu = 0.09
### Initial and Boundary Conditions ###
intensity = ${fparse 0.16*Re^(-1./8.)}
k_init = '${fparse 1.5*(intensity * bulk_u)^2}'
eps_init = '${fparse C_mu^0.75 * k_init^1.5 / (2*H)}'
### Modeling parameters ###
bulk_wall_treatment = false
walls = 'top bottom'
wall_treatment = 'eq_newton' # Options: eq_newton, eq_incremental, eq_linearized, neq
[Mesh]
[block_1]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${L}
ymin = 0
ymax = ${H}
nx = 4
ny = 4
bias_y = 0.7
[]
[block_2]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${L}
ymin = ${fparse -H}
ymax = 0
nx = 4
ny = 4
bias_y = ${fparse 1/0.7}
[]
[smg]
type = StitchedMeshGenerator
inputs = 'block_1 block_2'
clear_stitched_boundary_ids = true
stitch_boundaries_pairs = 'bottom top'
merge_boundaries_with_same_name = true
[]
# Prevent test diffing on distributed parallel element numbering
allow_renumbering = false
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system TKE_system TKED_system'
previous_nl_solution_required = true
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
advected_interp_method = ${advected_interp_method}
[]
[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 = ${bulk_u}
solver_sys = u_system
[]
[vel_y]
type = MooseLinearVariableFVReal
initial_condition = 0
solver_sys = v_system
[]
[pressure]
type = MooseLinearVariableFVReal
initial_condition = 1e-8
solver_sys = pressure_system
[]
[TKE]
type = MooseLinearVariableFVReal
solver_sys = TKE_system
initial_condition = ${k_init}
[]
[TKED]
type = MooseLinearVariableFVReal
solver_sys = TKED_system
initial_condition = ${eps_init}
[]
[]
[LinearFVKernels]
[u_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_x
advected_interp_method = ${advected_interp_method}
mu = 'mu_t'
u = vel_x
v = vel_y
momentum_component = 'x'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
use_deviatoric_terms = yes
[]
[u_diffusion]
type = LinearFVDiffusion
variable = vel_x
diffusion_coeff = ${mu}
use_nonorthogonal_correction = false
[]
[u_pressure]
type = LinearFVMomentumPressure
variable = vel_x
pressure = pressure
momentum_component = 'x'
[]
[v_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_y
advected_interp_method = ${advected_interp_method}
mu = 'mu_t'
u = vel_x
v = vel_y
momentum_component = 'y'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
use_deviatoric_terms = yes
[]
[v_diffusion]
type = LinearFVDiffusion
variable = vel_y
diffusion_coeff = ${mu}
use_nonorthogonal_correction = false
[]
[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
[]
[TKE_advection]
type = LinearFVTurbulentAdvection
variable = TKE
[]
[TKE_diffusion]
type = LinearFVTurbulentDiffusion
variable = TKE
diffusion_coeff = ${mu}
use_nonorthogonal_correction = false
[]
[TKE_turb_diffusion]
type = LinearFVTurbulentDiffusion
variable = TKE
diffusion_coeff = 'mu_t'
scaling_coeff = ${sigma_k}
use_nonorthogonal_correction = false
[]
[TKE_source_sink]
type = LinearFVTKESourceSink
variable = TKE
u = vel_x
v = vel_y
epsilon = TKED
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
walls = ${walls}
wall_treatment = ${wall_treatment}
C_pl = 1e10
[]
[TKED_advection]
type = LinearFVTurbulentAdvection
variable = TKED
walls = ${walls}
[]
[TKED_diffusion]
type = LinearFVTurbulentDiffusion
variable = TKED
diffusion_coeff = ${mu}
use_nonorthogonal_correction = false
walls = ${walls}
[]
[TKED_turb_diffusion]
type = LinearFVTurbulentDiffusion
variable = TKED
diffusion_coeff = 'mu_t'
scaling_coeff = ${sigma_eps}
use_nonorthogonal_correction = false
walls = ${walls}
[]
[TKED_source_sink]
type = LinearFVTKEDSourceSink
variable = TKED
u = vel_x
v = vel_y
tke = TKE
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
C1_eps = ${C1_eps}
C2_eps = ${C2_eps}
walls = ${walls}
wall_treatment = ${wall_treatment}
C_pl = 1e10
[]
[]
[LinearFVBCs]
[inlet-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_x
functor = '${bulk_u}'
[]
[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_u]
type = LinearFVAdvectionDiffusionOutflowBC
boundary = 'right'
variable = vel_x
use_two_term_expansion = false
[]
[outlet_v]
type = LinearFVAdvectionDiffusionOutflowBC
boundary = 'right'
variable = vel_y
use_two_term_expansion = false
[]
[outlet_p]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'right'
variable = pressure
functor = 0.0
[]
[inlet_TKE]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = TKE
functor = '${k_init}'
[]
[outlet_TKE]
type = LinearFVAdvectionDiffusionOutflowBC
boundary = 'right'
variable = TKE
use_two_term_expansion = false
[]
[inlet_TKED]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = TKED
functor = '${eps_init}'
[]
[outlet_TKED]
type = LinearFVAdvectionDiffusionOutflowBC
boundary = 'right'
variable = TKED
use_two_term_expansion = false
[]
[walls_mu_t]
type = LinearFVTurbulentViscosityWallFunctionBC
boundary = 'bottom top'
variable = 'mu_t'
u = vel_x
v = vel_y
rho = ${rho}
mu = ${mu}
tke = TKE
wall_treatment = ${wall_treatment}
[]
[]
[AuxVariables]
[mu_t]
type = MooseLinearVariableFVReal
initial_condition = '${fparse rho * C_mu * ${k_init}^2 / eps_init}'
[]
[yplus]
type = MooseLinearVariableFVReal
[]
[]
[AuxKernels]
[compute_mu_t]
type = kEpsilonViscosityAux
variable = mu_t
C_mu = ${C_mu}
tke = TKE
epsilon = TKED
mu = ${mu}
rho = ${rho}
u = vel_x
v = vel_y
bulk_wall_treatment = ${bulk_wall_treatment}
walls = ${walls}
wall_treatment = ${wall_treatment}
execute_on = 'NONLINEAR'
mu_t_ratio_max = 1e20
[]
[compute_y_plus]
type = RANSYPlusAux
variable = yplus
tke = TKE
mu = ${mu}
rho = ${rho}
u = vel_x
v = vel_y
walls = ${walls}
wall_treatment = ${wall_treatment}
execute_on = 'NONLINEAR'
[]
[]
[Executioner]
type = SIMPLE
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
turbulence_systems = 'TKE_system TKED_system'
momentum_l_abs_tol = 1e-14
pressure_l_abs_tol = 1e-14
turbulence_l_abs_tol = 1e-14
momentum_l_tol = 1e-14
pressure_l_tol = 1e-14
turbulence_l_tol = 1e-14
momentum_equation_relaxation = 0.7
pressure_variable_relaxation = 0.3
turbulence_equation_relaxation = '0.2 0.2'
turbulence_field_relaxation = '0.2 0.2'
num_iterations = 1000
pressure_absolute_tolerance = 1e-12
momentum_absolute_tolerance = 1e-12
turbulence_absolute_tolerance = '1e-12 1e-12'
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
turbulence_petsc_options_iname = '-pc_type -pc_hypre_type'
turbulence_petsc_options_value = 'hypre boomeramg'
print_fields = false
continue_on_max_its = true
[]
[Outputs]
csv = true
[]
[VectorPostprocessors]
[side_bottom]
type = SideValueSampler
boundary = 'bottom'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_top]
type = SideValueSampler
boundary = 'top'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[line_center_channel]
type = LineValueSampler
start_point = '${fparse 0.125 * L} ${fparse 0.0001} 0'
end_point = '${fparse 0.875 * L} ${fparse 0.0001} 0'
num_points = ${Mesh/block_1/nx}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[line_quarter_radius_channel]
type = LineValueSampler
start_point = '${fparse 0.125 * L} ${fparse 0.5 * H} 0'
end_point = '${fparse 0.875 * L} ${fparse 0.5 * H} 0'
num_points = ${Mesh/block_1/nx}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/newton_physics/lid-driven-turb-energy-wall-physics.i)
##########################################################
# Lid-driven cavity test
# Reynolds: 5,000
# Author: Dr. Mauricio Tano & Guillaume Giudicelli
# Last Update: July 2024
# Turbulent model using:
# k-epsilon model
# Standard wall functions with temperature wall functions
# Physics-based syntax
# Fully coupled solve
##########################################################
# Note:
# - in the original input k_t is lagged
### Thermophysical Properties ###
mu = 2e-5
rho = 1.0
k = 0.01
cp = 10.0
Pr_t = 0.9
### Operation Conditions ###
lid_velocity = 1.0
side_length = 0.1
### k-epsilon Closure Parameters ###
sigma_k = 1.0
sigma_eps = 1.3
C1_eps = 1.44
C2_eps = 1.92
C_mu = 0.09
### Initial Conditions ###
intensity = 0.01
k_init = '${fparse 1.5*(intensity * lid_velocity)^2}'
eps_init = '${fparse C_mu^0.75 * k_init^1.5 / side_length}'
mu_t_init = '${fparse rho * C_mu * k_init * k_init / eps_init}'
### Modeling parameters ###
bulk_wall_treatment = false
walls = 'left top right bottom'
wall_treatment_eps = 'eq_newton' # Options: eq_newton, eq_incremental, eq_linearized, neq
wall_treatment_tem = 'eq_linearized' # Options: eq_newton, eq_incremental, eq_linearized, neq
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${side_length}
ymin = 0
ymax = ${side_length}
nx = 12
ny = 12
[]
# Prevent test diffing on distributed parallel element numbering
allow_renumbering = false
[]
[Physics]
[NavierStokes]
[Flow]
[flow]
compressibility = 'incompressible'
# Material properties
density = ${rho}
dynamic_viscosity = ${mu}
# Initial conditions
initial_pressure = 0.2
# Need a non-zero starting velocity to avoid
# sparsity pattern + Newton error
initial_velocity = '1e-10 1e-10 0'
wall_boundaries = 'left right bottom top'
momentum_wall_types = 'noslip noslip noslip noslip'
momentum_wall_functors = '0 0; 0 0; 0 0; ${lid_velocity} 0'
pin_pressure = true
pinned_pressure_type = point-value
pinned_pressure_value = 0
pinned_pressure_point = '0.01 0.099 0.0'
# Numerical parameters
momentum_two_term_bc_expansion = false
pressure_two_term_bc_expansion = false
[]
[]
[FluidHeatTransfer]
[energy]
coupled_flow_physics = flow
thermal_conductivity = ${k}
specific_heat = ${cp}
initial_temperature = '1'
# Energy turbulent boundary conditions are specified in
# the turbulence block
energy_wall_types = 'heatflux heatflux wallfunction wallfunction'
energy_wall_functors = '0 0 0 1'
# Numerical parameters
energy_advection_interpolation = 'average'
energy_two_term_bc_expansion = false
[]
[]
[Turbulence]
[keps]
fluid_heat_transfer_physics = energy
turbulence_handling = 'k-epsilon'
tke_name = TKE
tked_name = TKED
# Initialization
initial_tke = ${k_init}
initial_tked = ${eps_init}
initial_mu_t = ${mu_t_init}
# Fluid properties
Pr_t = ${Pr_t}
# Model parameters
C1_eps = ${C1_eps}
C2_eps = ${C2_eps}
C_mu = ${C_mu}
sigma_k = ${sigma_k}
sigma_eps = ${sigma_eps}
# Wall parameters
turbulence_walls = ${walls}
bulk_wall_treatment = ${bulk_wall_treatment}
wall_treatment_eps = ${wall_treatment_eps}
wall_treatment_T = ${wall_treatment_tem}
# Numerical parameters
turbulent_viscosity_two_term_bc_expansion = false
mu_t_as_aux_variable = true
k_t_as_aux_variable = true
# this case requires it for convergence
linearize_sink_sources = true
neglect_advection_derivatives = true
# needed for non-negative face values
tke_two_term_bc_expansion = false
tked_two_term_bc_expansion = false
[]
[]
[]
[]
[AuxVariables]
[dummy]
type = MooseVariableConstMonomial
[]
[]
[Bounds]
[min_tke]
type = ConstantBounds
variable = dummy
bound_value = 1e-8
bounded_variable = TKE
bound_type = lower
[]
[min_eps]
type = ConstantBounds
variable = dummy
bound_value = 1e-8
bounded_variable = TKED
bound_type = lower
[]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_factor_shift_type -snes_type'
petsc_options_value = 'lu NONZERO vinewtonrsls'
nl_rel_tol = 1e-10
nl_abs_tol = 5e-8
nl_max_its = 100
# Necessary for these cases
snesmf_reuse_base = false
line_search = none
[]
[Outputs]
csv = true
exodus = true
perf_graph = false
print_nonlinear_residuals = true
print_linear_residuals = false
[]
[VectorPostprocessors]
[side_bottom]
type = SideValueSampler
boundary = 'bottom'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_top]
type = SideValueSampler
boundary = 'top'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_left]
type = SideValueSampler
boundary = 'left'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[side_right]
type = SideValueSampler
boundary = 'right'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[horizontal_center]
type = LineValueSampler
start_point = '${fparse 0.01 * side_length} ${fparse 0.499 * side_length} 0'
end_point = '${fparse 0.99 * side_length} ${fparse 0.499 * side_length} 0'
num_points = ${Mesh/gen/nx}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[vertical_center]
type = LineValueSampler
start_point = '${fparse 0.499 * side_length} ${fparse 0.01 * side_length} 0'
end_point = '${fparse 0.499 * side_length} ${fparse 0.99 * side_length} 0'
num_points = ${Mesh/gen/ny}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/turbulence/channel/linear-segregated-transient/channel_ERCOFTAC.i)
H = 1 #halfwidth of the channel
L = 100
Re = 13700
rho = 1
bulk_u = 1
mu = '${fparse rho * bulk_u * 2 * H / Re}'
advected_interp_method = 'upwind'
### k-epsilon Closure Parameters ###
sigma_k =1.0
sigma_eps = 1.3
C1_eps = 1.44
C2_eps = 1.92
C_mu = 0.09
### Initial and Boundary Conditions ###
intensity = 0.01
k_init = '${fparse 1.5*(intensity * bulk_u)^2}'
eps_init = '${fparse C_mu^0.75 * k_init^1.5 / (2*H)}'
### Modeling parameters ###
bulk_wall_treatment = false
walls = 'top bottom'
wall_treatment = 'eq_newton' # Options: eq_newton, eq_incremental, eq_linearized, neq
[Mesh]
[block_1]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${L}
ymin = 0
ymax = ${H}
nx = 4
ny = 3
bias_y = 0.7
[]
[block_2]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${L}
ymin = ${fparse -H}
ymax = 0
nx = 4
ny = 3
bias_y = ${fparse 1/0.7}
[]
[smg]
type = StitchedMeshGenerator
inputs = 'block_1 block_2'
clear_stitched_boundary_ids = true
stitch_boundaries_pairs = 'bottom top'
merge_boundaries_with_same_name = true
[]
# Prevent test diffing on distributed parallel element numbering
allow_renumbering = false
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system TKE_system TKED_system'
previous_nl_solution_required = true
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
advected_interp_method = ${advected_interp_method}
[]
[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 = ${bulk_u}
solver_sys = u_system
[]
[vel_y]
type = MooseLinearVariableFVReal
initial_condition = 0
solver_sys = v_system
[]
[pressure]
type = MooseLinearVariableFVReal
initial_condition = 1e-8
solver_sys = pressure_system
[]
[TKE]
type = MooseLinearVariableFVReal
solver_sys = TKE_system
initial_condition = ${k_init}
[]
[TKED]
type = MooseLinearVariableFVReal
solver_sys = TKED_system
initial_condition = ${eps_init}
[]
[]
[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_t'
u = vel_x
v = vel_y
momentum_component = 'x'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
use_deviatoric_terms = yes
[]
[u_diffusion]
type = LinearFVDiffusion
variable = vel_x
diffusion_coeff = ${mu}
use_nonorthogonal_correction = false
[]
[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_t'
u = vel_x
v = vel_y
momentum_component = 'y'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
use_deviatoric_terms = yes
[]
[v_diffusion]
type = LinearFVDiffusion
variable = vel_y
diffusion_coeff = ${mu}
use_nonorthogonal_correction = false
[]
[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
[]
[TKE_time]
type = LinearFVTimeDerivative
variable = TKE
factor = ${rho}
[]
[TKE_advection]
type = LinearFVTurbulentAdvection
variable = TKE
[]
[TKE_diffusion]
type = LinearFVTurbulentDiffusion
variable = TKE
diffusion_coeff = ${mu}
use_nonorthogonal_correction = false
[]
[TKE_turb_diffusion]
type = LinearFVTurbulentDiffusion
variable = TKE
diffusion_coeff = 'mu_t'
scaling_coeff = ${sigma_k}
use_nonorthogonal_correction = false
[]
[TKE_source_sink]
type = LinearFVTKESourceSink
variable = TKE
u = vel_x
v = vel_y
epsilon = TKED
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
walls = ${walls}
wall_treatment = ${wall_treatment}
C_pl = 1e10
[]
[TKED_time]
type = LinearFVTimeDerivative
variable = TKED
factor = ${rho}
[]
[TKED_advection]
type = LinearFVTurbulentAdvection
variable = TKED
walls = ${walls}
[]
[TKED_diffusion]
type = LinearFVTurbulentDiffusion
variable = TKED
diffusion_coeff = ${mu}
use_nonorthogonal_correction = false
walls = ${walls}
[]
[TKED_turb_diffusion]
type = LinearFVTurbulentDiffusion
variable = TKED
diffusion_coeff = 'mu_t'
scaling_coeff = ${sigma_eps}
use_nonorthogonal_correction = false
walls = ${walls}
[]
[TKED_source_sink]
type = LinearFVTKEDSourceSink
variable = TKED
u = vel_x
v = vel_y
tke = TKE
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
C1_eps = ${C1_eps}
C2_eps = ${C2_eps}
walls = ${walls}
wall_treatment = ${wall_treatment}
C_pl = 1e10
[]
[]
[LinearFVBCs]
[inlet-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_x
functor = '${bulk_u}'
[]
[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_u]
type = LinearFVAdvectionDiffusionOutflowBC
boundary = 'right'
variable = vel_x
use_two_term_expansion = false
[]
[outlet_v]
type = LinearFVAdvectionDiffusionOutflowBC
boundary = 'right'
variable = vel_y
use_two_term_expansion = false
[]
[outlet_p]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'right'
variable = pressure
functor = 0.0
[]
[inlet_TKE]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = TKE
functor = '${k_init}'
[]
[outlet_TKE]
type = LinearFVAdvectionDiffusionOutflowBC
boundary = 'right'
variable = TKE
use_two_term_expansion = false
[]
[inlet_TKED]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = TKED
functor = '${eps_init}'
[]
[outlet_TKED]
type = LinearFVAdvectionDiffusionOutflowBC
boundary = 'right'
variable = TKED
use_two_term_expansion = false
[]
[walls_mu_t]
type = LinearFVTurbulentViscosityWallFunctionBC
boundary = 'bottom top'
variable = 'mu_t'
u = vel_x
v = vel_y
rho = ${rho}
mu = ${mu}
tke = TKE
wall_treatment = ${wall_treatment}
[]
[]
[AuxVariables]
[mu_t]
type = MooseLinearVariableFVReal
initial_condition = '${fparse rho * C_mu * ${k_init}^2 / eps_init}'
[]
[yplus]
type = MooseLinearVariableFVReal
[]
[mu_eff]
type = MooseLinearVariableFVReal
initial_condition = '${fparse rho * C_mu * ${k_init}^2 / eps_init}'
[]
[]
[AuxKernels]
[compute_mu_t]
type = kEpsilonViscosityAux
variable = mu_t
C_mu = ${C_mu}
tke = TKE
epsilon = TKED
mu = ${mu}
rho = ${rho}
u = vel_x
v = vel_y
bulk_wall_treatment = ${bulk_wall_treatment}
walls = ${walls}
wall_treatment = ${wall_treatment}
execute_on = 'NONLINEAR'
mu_t_ratio_max = 1e20
[]
[compute_y_plus]
type = RANSYPlusAux
variable = yplus
tke = TKE
mu = ${mu}
rho = ${rho}
u = vel_x
v = vel_y
walls = ${walls}
wall_treatment = ${wall_treatment}
execute_on = 'NONLINEAR'
[]
[compute_mu_eff]
type = ParsedAux
variable = 'mu_eff'
coupled_variables = 'mu_t'
expression = 'mu_t + ${mu}'
execute_on = 'NONLINEAR'
[]
[]
[Executioner]
type = PIMPLE
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
turbulence_systems = 'TKE_system TKED_system'
momentum_l_abs_tol = 1e-14
pressure_l_abs_tol = 1e-14
turbulence_l_abs_tol = 1e-14
momentum_l_tol = 1e-14
pressure_l_tol = 1e-14
turbulence_l_tol = 1e-14
momentum_equation_relaxation = 0.7
pressure_variable_relaxation = 0.3
turbulence_equation_relaxation = '0.25 0.25'
num_iterations = 1000
pressure_absolute_tolerance = 1e-12
momentum_absolute_tolerance = 1e-12
turbulence_absolute_tolerance = '1e-12 1e-12'
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
turbulence_petsc_options_iname = '-pc_type -pc_hypre_type'
turbulence_petsc_options_value = 'hypre boomeramg'
print_fields = false
continue_on_max_its = true
dt = 1.0
num_steps = 2
[]
[Outputs]
csv = true
[]
[VectorPostprocessors]
[side_bottom]
type = SideValueSampler
boundary = 'bottom'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_top]
type = SideValueSampler
boundary = 'top'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[line_center_channel]
type = LineValueSampler
start_point = '${fparse 0.125 * L} ${fparse 0.0001} 0'
end_point = '${fparse 0.875 * L} ${fparse 0.0001} 0'
num_points = ${Mesh/block_1/nx}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[line_quarter_radius_channel]
type = LineValueSampler
start_point = '${fparse 0.125 * L} ${fparse 0.5 * H} 0'
end_point = '${fparse 0.875 * L} ${fparse 0.5 * H} 0'
num_points = ${Mesh/block_1/nx}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/segregated/lid-driven-turb-std-wall.i)
##########################################################
# Lid-driven cavity test
# Reynolds: 5,000
# Author: Dr. Mauricio Tano
# Last Update: November, 2023
# Turbulent model using:
# k-epsilon model
# Standard wall functions
# SIMPLE Solve
##########################################################
### Thermophysical Properties ###
mu = 1e-3
rho = 1.0
### Operation Conditions ###
lid_velocity = 1.0
side_length = 0.1
### Initial Conditions ###
intensity = 0.01
k_init = '${fparse 1.5*(intensity * lid_velocity)^2}'
eps_init = '${fparse C_mu^0.75 * k_init^1.5 / side_length}'
### k-epsilon Closure Parameters ###
sigma_k = 1.0
sigma_eps = 1.3
C1_eps = 1.44
C2_eps = 1.92
C_mu = 0.09
### Modeling parameters ###
bulk_wall_treatment = false
walls = 'left top right bottom'
wall_treatment = 'eq_newton' # Options: eq_newton, eq_incremental, eq_linearized, neq
pressure_tag = "pressure_grad"
[GlobalParams]
rhie_chow_user_object = 'rc'
advected_interp_method = 'upwind'
velocity_interp_method = 'rc'
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${side_length}
ymin = 0
ymax = ${side_length}
nx = 12
ny = 12
[]
# Prevent test diffing on distributed parallel element numbering
allow_renumbering = false
[]
[Problem]
nl_sys_names = 'u_system v_system pressure_system TKE_system TKED_system'
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolatorSegregated
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = 0.0
solver_sys = u_system
two_term_boundary_expansion = false
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 0.0
solver_sys = v_system
two_term_boundary_expansion = false
[]
[pressure]
type = INSFVPressureVariable
solver_sys = pressure_system
initial_condition = 0.2
two_term_boundary_expansion = false
[]
[TKE]
type = INSFVEnergyVariable
solver_sys = TKE_system
initial_condition = ${k_init}
two_term_boundary_expansion = false
[]
[TKED]
type = INSFVEnergyVariable
solver_sys = TKED_system
initial_condition = ${eps_init}
two_term_boundary_expansion = false
[]
[]
[FVKernels]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = ${mu}
momentum_component = 'x'
[]
[u_viscosity_turbulent]
type = INSFVMomentumDiffusion
variable = vel_x
mu = 'mu_t'
momentum_component = 'x'
complete_expansion = true
u = vel_x
v = vel_y
mu_interp_method = 'average'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
extra_vector_tags = ${pressure_tag}
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = ${mu}
momentum_component = 'y'
[]
[v_viscosity_turbulent]
type = INSFVMomentumDiffusion
variable = vel_y
mu = 'mu_t'
momentum_component = 'y'
complete_expansion = true
u = vel_x
v = vel_y
mu_interp_method = 'average'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
extra_vector_tags = ${pressure_tag}
[]
[p_diffusion]
type = FVAnisotropicDiffusion
variable = pressure
coeff = "Ainv"
coeff_interp_method = 'average'
[]
[p_source]
type = FVDivergence
variable = pressure
vector_field = "HbyA"
force_boundary_execution = true
[]
[TKE_advection]
type = INSFVTurbulentAdvection
variable = TKE
rho = ${rho}
[]
[TKE_diffusion]
type = INSFVTurbulentDiffusion
variable = TKE
coeff = ${mu}
[]
[TKE_diffusion_turbulent]
type = INSFVTurbulentDiffusion
variable = TKE
coeff = 'mu_t'
scaling_coef = ${sigma_k}
coeff_interp_method = 'average'
[]
[TKE_source_sink]
type = INSFVTKESourceSink
variable = TKE
u = vel_x
v = vel_y
epsilon = TKED
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
walls = ${walls}
wall_treatment = ${wall_treatment}
[]
[TKED_advection]
type = INSFVTurbulentAdvection
variable = TKED
rho = ${rho}
walls = ${walls}
[]
[TKED_diffusion]
type = INSFVTurbulentDiffusion
variable = TKED
coeff = ${mu}
walls = ${walls}
[]
[TKED_diffusion_turbulent]
type = INSFVTurbulentDiffusion
variable = TKED
coeff = 'mu_t'
scaling_coef = ${sigma_eps}
walls = ${walls}
coeff_interp_method = 'average'
[]
[TKED_source_sink]
type = INSFVTKEDSourceSink
variable = TKED
u = vel_x
v = vel_y
k = TKE
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
C1_eps = ${C1_eps}
C2_eps = ${C2_eps}
walls = ${walls}
wall_treatment = ${wall_treatment}
[]
[]
[FVBCs]
[top_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'top'
function = ${lid_velocity}
[]
[no_slip_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'left right bottom'
function = 0
[]
[no_slip_y]
type = INSFVNoSlipWallBC
variable = vel_y
boundary = 'left right top bottom'
function = 0
[]
[walls_mu_t]
type = INSFVTurbulentViscosityWallFunction
boundary = 'left right top bottom'
variable = mu_t
u = vel_x
v = vel_y
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
k = TKE
wall_treatment = ${wall_treatment}
[]
[]
[AuxVariables]
[mu_t]
type = MooseVariableFVReal
initial_condition = '${fparse rho * C_mu * ${k_init}^2 / eps_init}'
two_term_boundary_expansion = false
[]
[]
[AuxKernels]
[compute_mu_t]
type = kEpsilonViscosityAux
variable = mu_t
C_mu = ${C_mu}
k = TKE
epsilon = TKED
mu = ${mu}
rho = ${rho}
u = vel_x
v = vel_y
bulk_wall_treatment = ${bulk_wall_treatment}
walls = ${walls}
execute_on = 'NONLINEAR'
[]
[]
[Executioner]
type = SIMPLENonlinearAssembly
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
turbulence_systems = 'TKED_system TKE_system'
pressure_gradient_tag = ${pressure_tag}
momentum_equation_relaxation = 0.8
pressure_variable_relaxation = 0.5
turbulence_equation_relaxation = '0.8 0.8'
num_iterations = 500
pressure_absolute_tolerance = 1e-12
momentum_absolute_tolerance = 1e-12
turbulence_absolute_tolerance = '1e-12 1e-12'
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
continue_on_max_its = true
momentum_l_abs_tol = 1e-14
pressure_l_abs_tol = 1e-14
turbulence_l_abs_tol = 1e-14
momentum_l_max_its = 30
pressure_l_max_its = 30
momentum_l_tol = 0.0
pressure_l_tol = 0.0
turbulence_l_tol = 0.0
print_fields = false
pin_pressure = true
pressure_pin_value = 0.0
pressure_pin_point = '0.01 0.099 0.0'
[]
[Outputs]
csv = true
perf_graph = false
print_nonlinear_residuals = false
print_linear_residuals = true
[]
[VectorPostprocessors]
[side_bottom]
type = SideValueSampler
boundary = 'bottom'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_top]
type = SideValueSampler
boundary = 'top'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_left]
type = SideValueSampler
boundary = 'left'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[side_right]
type = SideValueSampler
boundary = 'right'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[horizontal_center]
type = LineValueSampler
start_point = '${fparse 0.01 * side_length} ${fparse 0.499 * side_length} 0'
end_point = '${fparse 0.99 * side_length} ${fparse 0.499 * side_length} 0'
num_points = ${Mesh/gen/nx}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[vertical_center]
type = LineValueSampler
start_point = '${fparse 0.499 * side_length} ${fparse 0.01 * side_length} 0'
end_point = '${fparse 0.499 * side_length} ${fparse 0.99 * side_length} 0'
num_points = ${Mesh/gen/ny}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/newton/lid-driven-turb-std-wall-nonlinear.i)
##########################################################
# Lid-driven cavity test
# Reynolds: 5,000
# Author: Dr. Mauricio Tano
# Last Update: November, 2023
# Turbulent model using:
# k-epsilon model
# No wall functions
# Newton Solve
##########################################################
### Thermophysical Properties ###
mu = 2e-5
rho = 1.0
### Operation Conditions ###
lid_velocity = 1.0
side_length = 0.1
### Initial Conditions ###
intensity = 0.01
k_init = '${fparse 1.5*(intensity * lid_velocity)^2}'
eps_init = '${fparse C_mu^0.75 * k_init^1.5 / side_length}'
### k-epsilon Closure Parameters ###
sigma_k = 1.0
sigma_eps = 1.3
C1_eps = 1.44
C2_eps = 1.92
C_mu = 0.09
### Modeling parameters ###
walls = ''
linearized_model = false
[GlobalParams]
rhie_chow_user_object = 'rc'
advected_interp_method = 'upwind'
velocity_interp_method = 'rc'
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${side_length}
ymin = 0
ymax = ${side_length}
nx = 10
ny = 10
[]
# Prevent test diffing on distributed parallel element numbering
allow_renumbering = false
[]
[Problem]
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = 1e-10
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 1e-10
[]
[pressure]
type = INSFVPressureVariable
initial_condition = 0.2
[]
[TKE]
type = INSFVEnergyVariable
initial_condition = ${k_init}
two_term_boundary_expansion = false
[]
[TKED]
type = INSFVEnergyVariable
initial_condition = ${eps_init}
two_term_boundary_expansion = false
[]
[lambda]
family = SCALAR
order = FIRST
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
rho = ${rho}
[]
[mean_zero_pressure]
type = FVIntegralValueConstraint
variable = pressure
lambda = lambda
[]
[u_time]
type = INSFVMomentumTimeDerivative
variable = vel_x
rho = ${rho}
momentum_component = 'x'
[]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = ${mu}
momentum_component = 'x'
mu_interp_method = average
[]
[u_viscosity_turbulent]
type = INSFVMomentumDiffusion
variable = vel_x
mu = 'mu_t'
momentum_component = 'x'
complete_expansion = true
u = vel_x
v = vel_y
mu_interp_method = average
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
rho = ${rho}
momentum_component = 'y'
[]
[v_time]
type = INSFVMomentumTimeDerivative
variable = vel_y
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = ${mu}
momentum_component = 'y'
mu_interp_method = average
[]
[v_viscosity_turbulent]
type = INSFVMomentumDiffusion
variable = vel_y
mu = 'mu_t'
momentum_component = 'y'
complete_expansion = true
u = vel_x
v = vel_y
mu_interp_method = average
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
[]
[TKE_time]
type = FVFunctorTimeKernel
variable = TKE
[]
[TKE_advection]
type = INSFVTurbulentAdvection
variable = TKE
rho = ${rho}
[]
[TKE_diffusion]
type = INSFVTurbulentDiffusion
variable = TKE
coeff = ${mu}
[]
[TKE_diffusion_turbulent]
type = INSFVTurbulentDiffusion
variable = TKE
coeff = 'mu_t'
scaling_coef = ${sigma_k}
coeff_interp_method = average
[]
[TKE_source_sink]
type = INSFVTKESourceSink
variable = TKE
u = vel_x
v = vel_y
epsilon = TKED
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
walls = ${walls}
linearized_model = ${linearized_model}
[]
[TKED_time]
type = FVFunctorTimeKernel
variable = TKED
[]
[TKED_advection]
type = INSFVTurbulentAdvection
variable = TKED
rho = ${rho}
walls = ${walls}
[]
[TKED_diffusion]
type = INSFVTurbulentDiffusion
variable = TKED
coeff = ${mu}
walls = ${walls}
[]
[TKED_diffusion_turbulent]
type = INSFVTurbulentDiffusion
variable = TKED
coeff = 'mu_t'
scaling_coef = ${sigma_eps}
walls = ${walls}
coeff_interp_method = average
[]
[TKED_source_sink]
type = INSFVTKEDSourceSink
variable = TKED
u = vel_x
v = vel_y
tke = TKE
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
C1_eps = ${C1_eps}
C2_eps = ${C2_eps}
walls = ${walls}
linearized_model = ${linearized_model}
[]
[]
[FVBCs]
[top_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'top'
function = ${lid_velocity}
[]
[no_slip_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'left right bottom'
function = 0
[]
[no_slip_y]
type = INSFVNoSlipWallBC
variable = vel_y
boundary = 'left right top bottom'
function = 0
[]
[walls_TKE]
type = FVDirichletBC
boundary = 'left right top bottom'
variable = TKE
value = ${k_init}
[]
[walls_TKED]
type = FVDirichletBC
boundary = 'left right top bottom'
variable = TKED
value = ${eps_init}
[]
[]
[FunctorMaterials]
[mu_t_material]
type = INSFVkEpsilonViscosityFunctorMaterial
tke = TKE
epsilon = TKED
rho = ${rho}
[]
[]
[Executioner]
type = Transient
end_time = 200
dt = 0.01
steady_state_detection = true
steady_state_tolerance = 1e-3
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_shift_type -snes_linesearch_damping'
petsc_options_value = 'lu NONZERO 0.5'
nl_abs_tol = 1e-8
nl_rel_tol = 1e-8
nl_max_its = 50
line_search = none
[]
[Outputs]
csv = true
perf_graph = false
print_nonlinear_residuals = true
print_linear_residuals = false
[]
[VectorPostprocessors]
[side_bottom]
type = SideValueSampler
boundary = 'bottom'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_top]
type = SideValueSampler
boundary = 'top'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_left]
type = SideValueSampler
boundary = 'left'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[side_right]
type = SideValueSampler
boundary = 'right'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[horizontal_center]
type = LineValueSampler
start_point = '${fparse 0.01 * side_length} ${fparse 0.499 * side_length} 0'
end_point = '${fparse 0.99 * side_length} ${fparse 0.499 * side_length} 0'
num_points = ${Mesh/gen/nx}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[vertical_center]
type = LineValueSampler
start_point = '${fparse 0.499 * side_length} ${fparse 0.01 * side_length} 0'
end_point = '${fparse 0.499 * side_length} ${fparse 0.99 * side_length} 0'
num_points = ${Mesh/gen/ny}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[]