- pressureThe pressure
C++ Type:std::vector<VariableName>
Unit:(no unit assumed)
Controllable:No
Description:The pressure
- velocityThe velocity
C++ Type:std::vector<VariableName>
Unit:(no unit assumed)
Controllable:No
Description:The velocity
INSADTauMaterial
This object computes the stabilization parameter for use in pressure-stabilized and streamline-upwind kernels.
This is the material class used to compute the stabilization parameter tau.
Input Parameters
- alpha1Multiplicative factor on the stabilization parameter tau.
Default:1
C++ Type:double
Unit:(no unit assumed)
Controllable:No
Description:Multiplicative factor on the stabilization parameter tau.
- blockThe list of blocks (ids or names) that this object will be applied
C++ Type:std::vector<SubdomainName>
Controllable:No
Description:The list of blocks (ids or names) that this object will be applied
- boundaryThe list of boundaries (ids or names) from the mesh where this object applies
C++ Type:std::vector<BoundaryName>
Controllable:No
Description:The list of boundaries (ids or names) from the mesh where this object applies
- computeTrueWhen false, MOOSE will not call compute methods on this material. The user must call computeProperties() after retrieving the MaterialBase via MaterialBasePropertyInterface::getMaterialBase(). Non-computed MaterialBases are not sorted for dependencies.
Default:True
C++ Type:bool
Controllable:No
Description:When false, MOOSE will not call compute methods on this material. The user must call computeProperties() after retrieving the MaterialBase via MaterialBasePropertyInterface::getMaterialBase(). Non-computed MaterialBases are not sorted for dependencies.
- constant_onNONEWhen ELEMENT, MOOSE will only call computeQpProperties() for the 0th quadrature point, and then copy that value to the other qps.When SUBDOMAIN, MOOSE will only call computeQpProperties() for the 0th quadrature point, and then copy that value to the other qps. Evaluations on element qps will be skipped
Default:NONE
C++ Type:MooseEnum
Options:NONE, ELEMENT, SUBDOMAIN
Controllable:No
Description:When ELEMENT, MOOSE will only call computeQpProperties() for the 0th quadrature point, and then copy that value to the other qps.When SUBDOMAIN, MOOSE will only call computeQpProperties() for the 0th quadrature point, and then copy that value to the other qps. Evaluations on element qps will be skipped
- declare_suffixAn optional suffix parameter that can be appended to any declared 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 declared properties. The suffix will be prepended with a '_' character.
- mu_namemuThe name of the dynamic viscosity
Default:mu
C++ Type:MaterialPropertyName
Unit:(no unit assumed)
Controllable:No
Description:The name of the dynamic viscosity
- rho_namerhoThe name of the density
Default:rho
C++ Type:MaterialPropertyName
Unit:(no unit assumed)
Controllable:No
Description:The name of the density
Optional Parameters
- control_tagsAdds user-defined labels for accessing object parameters via control logic.
C++ Type:std::vector<std::string>
Controllable:No
Description:Adds user-defined labels for accessing object parameters via control logic.
- enableTrueSet the enabled status of the MooseObject.
Default:True
C++ Type:bool
Controllable:Yes
Description:Set the enabled status of the MooseObject.
- implicitTrueDetermines whether this object is calculated using an implicit or explicit form
Default:True
C++ Type:bool
Controllable:No
Description:Determines whether this object is calculated using an implicit or explicit form
- search_methodnearest_node_connected_sidesChoice of search algorithm. All options begin by finding the nearest node in the primary boundary to a query point in the secondary boundary. In the default nearest_node_connected_sides algorithm, primary boundary elements are searched iff that nearest node is one of their nodes. This is fast to determine via a pregenerated node-to-elem map and is robust on conforming meshes. In the optional all_proximate_sides algorithm, primary boundary elements are searched iff they touch that nearest node, even if they are not topologically connected to it. This is more CPU-intensive but is necessary for robustness on any boundary surfaces which has disconnections (such as Flex IGA meshes) or non-conformity (such as hanging nodes in adaptively h-refined meshes).
Default:nearest_node_connected_sides
C++ Type:MooseEnum
Options:nearest_node_connected_sides, all_proximate_sides
Controllable:No
Description:Choice of search algorithm. All options begin by finding the nearest node in the primary boundary to a query point in the secondary boundary. In the default nearest_node_connected_sides algorithm, primary boundary elements are searched iff that nearest node is one of their nodes. This is fast to determine via a pregenerated node-to-elem map and is robust on conforming meshes. In the optional all_proximate_sides algorithm, primary boundary elements are searched iff they touch that nearest node, even if they are not topologically connected to it. This is more CPU-intensive but is necessary for robustness on any boundary surfaces which has disconnections (such as Flex IGA meshes) or non-conformity (such as hanging nodes in adaptively h-refined meshes).
- seed0The seed for the master random number generator
Default:0
C++ Type:unsigned int
Controllable:No
Description:The seed for the master random number generator
- 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
- output_propertiesList of material properties, from this material, to output (outputs must also be defined to an output type)
C++ Type:std::vector<std::string>
Controllable:No
Description:List of material properties, from this material, to output (outputs must also be defined to an output type)
- outputsnone Vector of output names where you would like to restrict the output of variables(s) associated with this object
Default:none
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
Outputs 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
- (modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/ad-rz-displacements.i)
- (modules/navier_stokes/test/tests/finite_element/ins/rz-x-axial-coord/pipe-flow.i)
- (modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/ad_rz_cone_stab_jac_test.i)
- (modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/ad_rz_cone_no_parts_steady_stabilized_second_order.i)
- (modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/ad_rz_cone_by_parts_traction_steady_stabilized.i)
- (modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/ad_rz_cone_by_parts_steady_stabilized_second_order.i)
- (modules/navier_stokes/test/tests/finite_element/ins/lid_driven/ad_lid_driven_stabilized.i)
- (modules/navier_stokes/test/tests/finite_element/ins/rz-x-axial-coord/pipe-flow-natural-bc.i)
- (modules/navier_stokes/test/tests/finite_element/ins/coupled-force/gravity-object.i)
- (modules/fsi/test/tests/newmark-beta/test_ALE.i)
- (modules/navier_stokes/test/tests/finite_element/ins/velocity_channel/ad-traction-supg.i)
- (modules/fsi/test/tests/2d-small-strain-transient/ad-fsi-flat-channel.i)
- (modules/navier_stokes/test/tests/finite_element/ins/coupled-force/gravity-through-coupled-force.i)
- (modules/navier_stokes/test/tests/finite_element/ins/coupled-force/steady.i)
- (modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/ad_rz_cone_no_parts_steady_stabilized.i)
- (modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/ad_rz_cone_by_parts_steady_stabilized.i)
- (modules/navier_stokes/test/tests/finite_element/ins/lid_driven/steady_vector_fsp_al.i)
- (modules/combined/test/tests/phase_field_contact_angle/contact_angle.i)
- (modules/navier_stokes/test/tests/finite_element/ins/coupled-force/steady-function.i)
(modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/ad-rz-displacements.i)
[GlobalParams]
order = FIRST
integrate_p_by_parts = true
use_displaced_mesh = true
[]
[Mesh]
file = '2d_cone.msh'
displacements = 'disp_x disp_y'
coord_type = RZ
[]
[AuxVariables]
[vel_x][]
[vel_y][]
[disp_x]
order = SECOND
[]
[disp_y]
order = SECOND
[]
[]
[AuxKernels]
[vel_x]
type = VectorVariableComponentAux
variable = vel_x
vector_variable = velocity
component = 'x'
[]
[vel_y]
type = VectorVariableComponentAux
variable = vel_y
vector_variable = velocity
component = 'y'
[]
[]
[Variables]
[velocity]
family = LAGRANGE_VEC
[]
[p]
[]
[]
# Need to set a non-zero initial condition because we have a velocity norm in
# the denominator for the tau coefficient of the stabilization term
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[Kernels]
[mass]
type = INSADMass
variable = p
[]
[mass_pspg]
type = INSADMassPSPG
variable = p
[]
[momentum_advection]
type = INSADMomentumAdvection
variable = velocity
[]
[momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[]
[momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
[]
[momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[]
[]
[BCs]
[inlet]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom'
function_x = 0
function_y = 'inlet_func'
[]
[wall]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'right'
function_x = 0
function_y = 0
[]
[axis]
type = ADVectorFunctionDirichletBC
variable = velocity
boundary = 'left'
set_y_comp = false
function_x = 0
[]
[]
[Functions]
[inlet_func]
type = ParsedFunction
expression = '-4 * x^2 + 1'
[]
[]
[Materials]
[const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '1 1'
[]
[ins_mat]
type = INSADTauMaterial
velocity = velocity
pressure = p
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
solve_type = 'NEWTON'
[]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = 'bjacobi ilu 4'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
csv = true
[out]
type = Exodus
hide = 'disp_x disp_y'
[]
[]
[Postprocessors]
[flow_in]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'bottom'
execute_on = 'timestep_end'
[]
[flow_out]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'top'
execute_on = 'timestep_end'
[]
[]
(modules/navier_stokes/test/tests/finite_element/ins/rz-x-axial-coord/pipe-flow.i)
mu=1
rho=1
pipe_length=10 # m
pipe_radius=1 # m
u_inlet=1
[GlobalParams]
integrate_p_by_parts = false
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${pipe_length}
ymin = 0
ymax = ${pipe_radius}
nx = 50
ny = 5
[]
coord_type = 'RZ'
rz_coord_axis = x
[]
[Variables]
[velocity]
family = LAGRANGE_VEC
[]
[p][]
[]
[Kernels]
[mass]
type = INSADMass
variable = p
[]
[mass_pspg]
type = INSADMassPSPG
variable = p
[]
[momentum_convection]
type = INSADMomentumAdvection
variable = velocity
[]
[momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[]
[momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
[]
[momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[]
[]
[Functions]
[vel_x_inlet]
type = ParsedFunction
expression = '${u_inlet} * (${pipe_radius}^2 - y^2)'
[]
[]
[BCs]
[inlet]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'left'
function_x = vel_x_inlet
function_y = 0
[../]
[wall]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'top'
function_x = 0
function_y = 0
[]
[axis]
type = ADVectorFunctionDirichletBC
variable = velocity
boundary = 'bottom'
set_x_comp = false
function_y = 0
[]
# pressure is not integrated by parts so we cannot remove the nullspace through a natural condition
[p_corner]
type = DirichletBC
boundary = 'right'
value = 0
variable = p
[]
[]
[Materials]
[const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '${rho} ${mu}'
[]
[ins_mat]
type = INSADTauMaterial
velocity = velocity
pressure = p
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
nl_rel_tol = 1e-12
nl_abs_tol = 1e-12
line_search = 'none'
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/ad_rz_cone_stab_jac_test.i)
[GlobalParams]
order = SECOND
integrate_p_by_parts = true
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 2
xmin = 0
xmax = 1.1
ymin = -1.1
ymax = 1.1
elem_type = QUAD9
[]
[./corner_node]
type = ExtraNodesetGenerator
new_boundary = 'pinned_node'
nodes = '0'
input = gen
[../]
coord_type = RZ
[]
[Preconditioning]
[./SMP_PJFNK]
type = SMP
full = true
solve_type = NEWTON
[../]
[]
[Executioner]
type = Transient
num_steps = 1
dt = 1.1
[]
[Variables]
[./velocity]
family = LAGRANGE_VEC
[../]
[./p]
order = FIRST
[../]
[]
# Need to set a non-zero initial condition because we have a velocity norm in
# the denominator for the tau coefficient of the stabilization term
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[mass_pspg]
type = INSADMassPSPG
variable = p
[]
[momentum_time]
type = INSADMomentumTimeDerivative
variable = velocity
[]
[momentum_advection]
type = INSADMomentumAdvection
variable = velocity
[]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
[../]
[momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[]
[]
[BCs]
[inlet]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom'
function_x = 0
function_y = 1
[../]
[wall]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'right'
function_x = 0
function_y = 0
[]
[axis]
type = ADVectorFunctionDirichletBC
variable = velocity
boundary = 'left'
set_y_comp = false
function_x = 0
[]
[outlet]
type = INSADMomentumNoBCBC
variable = velocity
pressure = p
boundary = 'top'
[]
# When the NoBCBC is applied on the outlet boundary then there is nothing
# constraining the pressure. Thus we must pin the pressure somewhere to ensure
# that the problem is not singular. If the below BC is not applied then
# -pc_type svd -pc_svd_monitor reveals a singular value
[p_corner]
type = DirichletBC
boundary = pinned_node
value = 0
variable = p
[]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '1.1 1.1'
[../]
[ins_mat]
type = INSADTauMaterial
velocity = velocity
pressure = p
[]
[]
(modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/ad_rz_cone_no_parts_steady_stabilized_second_order.i)
[GlobalParams]
order = SECOND
integrate_p_by_parts = false
[]
[Mesh]
file = '2d_cone.msh'
coord_type = RZ
[]
[AuxVariables]
[vel_x]
[]
[vel_y]
[]
[]
[AuxKernels]
[vel_x]
type = VectorVariableComponentAux
variable = vel_x
vector_variable = velocity
component = 'x'
[]
[vel_y]
type = VectorVariableComponentAux
variable = vel_y
vector_variable = velocity
component = 'y'
[]
[]
[Variables]
[./velocity]
family = LAGRANGE_VEC
[../]
[./p]
order = FIRST
[../]
[]
# Need to set a non-zero initial condition because we have a velocity norm in
# the denominator for the tau coefficient of the stabilization term
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[mass_pspg]
type = INSADMassPSPG
variable = p
[]
[momentum_advection]
type = INSADMomentumAdvection
variable = velocity
[]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
[../]
[momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[]
[]
[BCs]
[p_corner]
type = DirichletBC
boundary = top_right
value = 0
variable = p
[]
[inlet]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom'
function_x = 0
function_y = 'inlet_func'
[../]
[wall]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'right'
function_x = 0
function_y = 0
[]
[axis]
type = ADVectorFunctionDirichletBC
variable = velocity
boundary = 'left'
set_y_comp = false
function_x = 0
[]
[]
[Functions]
[./inlet_func]
type = ParsedFunction
expression = '-4 * x^2 + 1'
[../]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[ins_mat]
type = INSADTauMaterial
velocity = velocity
pressure = p
[]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = 'bjacobi ilu 4'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
console = true
[./out]
type = Exodus
[../]
[]
[Postprocessors]
[./flow_in]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'bottom'
execute_on = 'timestep_end'
[../]
[./flow_out]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'top'
execute_on = 'timestep_end'
[../]
[]
(modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/ad_rz_cone_by_parts_traction_steady_stabilized.i)
[GlobalParams]
order = FIRST
integrate_p_by_parts = true
viscous_form = 'traction'
[]
[Mesh]
file = '2d_cone.msh'
coord_type = RZ
[]
[AuxVariables]
[vel_x]
[]
[vel_y]
[]
[]
[AuxKernels]
[vel_x]
type = VectorVariableComponentAux
variable = vel_x
vector_variable = velocity
component = 'x'
[]
[vel_y]
type = VectorVariableComponentAux
variable = vel_y
vector_variable = velocity
component = 'y'
[]
[]
[Variables]
[./velocity]
family = LAGRANGE_VEC
[../]
[./p]
[../]
[]
# Need to set a non-zero initial condition because we have a velocity norm in
# the denominator for the tau coefficient of the stabilization term
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[mass_pspg]
type = INSADMassPSPG
variable = p
[]
[momentum_advection]
type = INSADMomentumAdvection
variable = velocity
[]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
[../]
[momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[]
[]
[BCs]
[inlet]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom'
function_x = 0
function_y = 'inlet_func'
[../]
[wall]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'right'
function_x = 0
function_y = 0
[]
[axis]
type = ADVectorFunctionDirichletBC
variable = velocity
boundary = 'left'
set_y_comp = false
function_x = 0
[]
[]
[Functions]
[./inlet_func]
type = ParsedFunction
expression = '-4 * x^2 + 1'
[../]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[ins_mat]
type = INSADTauMaterial
velocity = velocity
pressure = p
[]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = 'bjacobi ilu 4'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
console = true
[./out]
type = Exodus
[../]
[]
[Postprocessors]
[./flow_in]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'bottom'
execute_on = 'timestep_end'
[../]
[./flow_out]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'top'
execute_on = 'timestep_end'
[../]
[]
(modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/ad_rz_cone_by_parts_steady_stabilized_second_order.i)
[GlobalParams]
order = SECOND
integrate_p_by_parts = true
[]
[Mesh]
file = '2d_cone.msh'
coord_type = RZ
[]
[AuxVariables]
[vel_x]
[]
[vel_y]
[]
[]
[AuxKernels]
[vel_x]
type = VectorVariableComponentAux
variable = vel_x
vector_variable = velocity
component = 'x'
[]
[vel_y]
type = VectorVariableComponentAux
variable = vel_y
vector_variable = velocity
component = 'y'
[]
[]
[Variables]
[./velocity]
family = LAGRANGE_VEC
[../]
[./p]
order = FIRST
[../]
[]
# Need to set a non-zero initial condition because we have a velocity norm in
# the denominator for the tau coefficient of the stabilization term
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[mass_pspg]
type = INSADMassPSPG
variable = p
[]
[momentum_advection]
type = INSADMomentumAdvection
variable = velocity
[]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
[../]
[momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[]
[]
[BCs]
[inlet]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom'
function_x = 0
function_y = 'inlet_func'
[../]
[wall]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'right'
function_x = 0
function_y = 0
[]
[axis]
type = ADVectorFunctionDirichletBC
variable = velocity
boundary = 'left'
set_y_comp = false
function_x = 0
[]
[]
[Functions]
[./inlet_func]
type = ParsedFunction
expression = '-4 * x^2 + 1'
[../]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[ins_mat]
type = INSADTauMaterial
velocity = velocity
pressure = p
[]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = 'bjacobi ilu 4'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
console = true
[./out]
type = Exodus
[../]
[]
[Postprocessors]
[./flow_in]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'bottom'
execute_on = 'timestep_end'
[../]
[./flow_out]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'top'
execute_on = 'timestep_end'
[../]
[]
(modules/navier_stokes/test/tests/finite_element/ins/lid_driven/ad_lid_driven_stabilized.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
nx = 64
ny = 64
[]
[./corner_node]
type = ExtraNodesetGenerator
new_boundary = 'pinned_node'
nodes = '0'
input = gen
[../]
[]
[AuxVariables]
[vel_x]
[]
[vel_y]
[]
[]
[AuxKernels]
[vel_x]
type = VectorVariableComponentAux
variable = vel_x
vector_variable = velocity
component = 'x'
[]
[vel_y]
type = VectorVariableComponentAux
variable = vel_y
vector_variable = velocity
component = 'y'
[]
[]
[Variables]
[./velocity]
family = LAGRANGE_VEC
[../]
[./p]
[../]
[]
[ICs]
[velocity]
type = VectorConstantIC
x_value = 0
y_value = 0
variable = velocity
[]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[./mass_pspg]
type = INSADMassPSPG
variable = p
[../]
[./momentum_convection]
type = INSADMomentumAdvection
variable = velocity
[../]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
integrate_p_by_parts = true
[../]
[./momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[../]
[]
[BCs]
[./no_slip]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom right left'
[../]
[./lid]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'top'
function_x = 'lid_function'
[../]
[./pressure_pin]
type = DirichletBC
variable = p
boundary = 'pinned_node'
value = 0
[../]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[ins_mat]
type = INSADTauMaterial
velocity = velocity
pressure = p
alpha = .1
[]
[]
[Functions]
[./lid_function]
# We pick a function that is exactly represented in the velocity
# space so that the Dirichlet conditions are the same regardless
# of the mesh spacing.
type = ParsedFunction
expression = '4*x*(1-x)'
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
line_search = 'none'
nl_rel_tol = 1e-12
nl_abs_tol = 1e-13
nl_max_its = 6
l_tol = 1e-6
l_max_its = 500
[]
[Outputs]
exodus = true
file_base = lid_driven_stabilized_out
[]
[Postprocessors]
[lin]
type = NumLinearIterations
[]
[nl]
type = NumNonlinearIterations
[]
[lin_tot]
type = CumulativeValuePostprocessor
postprocessor = 'lin'
[]
[nl_tot]
type = CumulativeValuePostprocessor
postprocessor = 'nl'
[]
[]
(modules/navier_stokes/test/tests/finite_element/ins/rz-x-axial-coord/pipe-flow-natural-bc.i)
mu=1
rho=1
pipe_length=10 # m
pipe_radius=1 # m
u_inlet=1
[GlobalParams]
integrate_p_by_parts = true
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${pipe_length}
ymin = 0
ymax = ${pipe_radius}
nx = 50
ny = 5
[]
coord_type = 'RZ'
rz_coord_axis = x
[]
[Variables]
[velocity]
family = LAGRANGE_VEC
[]
[p][]
[]
[Kernels]
[mass]
type = INSADMass
variable = p
[]
[mass_pspg]
type = INSADMassPSPG
variable = p
[]
[momentum_convection]
type = INSADMomentumAdvection
variable = velocity
[]
[momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[]
[momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
[]
[momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[]
[]
[Functions]
[vel_x_inlet]
type = ParsedFunction
expression = '${u_inlet} * (${pipe_radius}^2 - y^2)'
[]
[]
[BCs]
[inlet]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'left'
function_x = vel_x_inlet
function_y = 0
[../]
[wall]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'top'
function_x = 0
function_y = 0
[]
[axis]
type = ADVectorFunctionDirichletBC
variable = velocity
boundary = 'bottom'
set_x_comp = false
function_y = 0
[]
[]
[Materials]
[const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '${rho} ${mu}'
[]
[ins_mat]
type = INSADTauMaterial
velocity = velocity
pressure = p
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
nl_rel_tol = 1e-12
nl_abs_tol = 1e-12
line_search = 'none'
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/coupled-force/gravity-object.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
nx = 16
ny = 16
[]
[./corner_node]
type = ExtraNodesetGenerator
new_boundary = 'pinned_node'
nodes = '0'
input = gen
[../]
[]
[Variables]
[./velocity]
family = LAGRANGE_VEC
[../]
[./p]
[../]
[u]
family = LAGRANGE_VEC
[]
[]
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[./mass_pspg]
type = INSADMassPSPG
variable = p
[../]
[./momentum_convection]
type = INSADMomentumAdvection
variable = velocity
[../]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
integrate_p_by_parts = true
[../]
[momentum_coupled_force]
type = INSADMomentumCoupledForce
variable = velocity
coupled_vector_var = u
[]
[gravity]
type = INSADGravityForce
variable = velocity
gravity = '0 -9.81 0'
[]
[./momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[../]
[u_diff]
type = VectorDiffusion
variable = u
[]
[]
[BCs]
[./no_slip]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom right left top'
[../]
[./pressure_pin]
type = DirichletBC
variable = p
boundary = 'pinned_node'
value = 0
[../]
[u_left]
type = VectorFunctionDirichletBC
variable = u
boundary = 'left'
function_x = 1
function_y = 1
[]
[u_right]
type = VectorFunctionDirichletBC
variable = u
boundary = 'right'
function_x = -1
function_y = -1
[]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[ins_mat]
type = INSADTauMaterial
velocity = velocity
pressure = p
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_levels -ksp_gmres_restart'
petsc_options_value = 'asm 6 200'
line_search = 'none'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
exodus = true
[]
(modules/fsi/test/tests/newmark-beta/test_ALE.i)
beta = 0.25
gamma = 0.5
eta = 19.63
zeta = 0.000025
youngs_modulus = 1e8
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
[file]
type = FileMeshGenerator
file = tmesh_HR.msh
[]
[convert]
type = ElementOrderConversionGenerator
input = file
conversion_type = FIRST_ORDER
[]
[matrix_side_interface]
type = SideSetsBetweenSubdomainsGenerator
input = convert
new_boundary = interface_matrix_side
paired_block = 'inclusion'
primary_block = 'matrix'
[]
[]
[Variables]
[disp_x]
scaling = '${fparse 1/youngs_modulus}'
[]
[disp_y]
scaling = '${fparse 1/youngs_modulus}'
[]
[vel]
family = LAGRANGE_VEC
block = 'matrix'
[]
[p]
block = 'matrix'
[]
[lambda]
family = SCALAR
block = 'matrix'
[]
[]
[AuxVariables]
[accel_x]
block = 'inclusion'
[]
[accel_y]
block = 'inclusion'
[]
[vel_x_solid]
block = 'inclusion'
[]
[vel_y_solid]
block = 'inclusion'
[]
[vel_x_fluid]
block = 'matrix'
[]
[vel_y_fluid]
block = 'matrix'
[]
[]
[AuxKernels]
[accel_x] # Calculates and stores acceleration at the end of time step
type = NewmarkAccelAux
variable = accel_x
displacement = disp_x
velocity = vel_x_solid
beta = ${beta}
execute_on = timestep_end
block = 'inclusion'
[]
[accel_y] # Calculates and stores acceleration at the end of time step
type = NewmarkAccelAux
variable = accel_y
displacement = disp_y
velocity = vel_y_solid
beta = ${beta}
execute_on = timestep_end
block = 'inclusion'
[]
[vel_x_solid]
type = NewmarkVelAux
variable = vel_x_solid
acceleration = accel_x
gamma = ${gamma}
execute_on = timestep_end
block = 'inclusion'
[]
[vel_y_solid]
type = NewmarkVelAux
variable = vel_y_solid
acceleration = accel_y
gamma = ${gamma}
execute_on = timestep_end
block = 'inclusion'
[]
[vel_x_fluid]
type = VectorVariableComponentAux
variable = vel_x_fluid
vector_variable = vel
execute_on = timestep_end
component = 'x'
[]
[vel_y_fluid]
type = VectorVariableComponentAux
variable = vel_y_fluid
vector_variable = vel
execute_on = timestep_end
component = 'y'
[]
[]
[ScalarKernels]
[mean_zero_pressure_lm]
type = AverageValueConstraint
variable = lambda
pp_name = pressure_integral
value = 0
[]
[]
[Kernels]
[mat_disp_x]
type = MatDiffusion
variable = disp_x
block = 'matrix'
use_displaced_mesh = false
diffusivity = ${youngs_modulus}
[]
[mat_disp_y]
type = MatDiffusion
variable = disp_y
block = 'matrix'
use_displaced_mesh = false
diffusivity = ${youngs_modulus}
[]
[mass]
type = INSADMass
variable = p
use_displaced_mesh = true
block = 'matrix'
[]
[mass_pspg]
type = INSADMassPSPG
variable = p
use_displaced_mesh = true
block = 'matrix'
[]
[momentum_time]
type = INSADMomentumTimeDerivative
variable = vel
block = 'matrix'
[]
[momentum_convection]
type = INSADMomentumAdvection
variable = vel
block = 'matrix'
[]
[momentum_viscous]
type = INSADMomentumViscous
variable = vel
use_displaced_mesh = true
block = 'matrix'
[]
[momentum_pressure]
type = INSADMomentumPressure
variable = vel
pressure = p
integrate_p_by_parts = true
use_displaced_mesh = true
block = 'matrix'
[]
[momentum_supg]
type = INSADMomentumSUPG
variable = vel
material_velocity = relative_velocity
block = 'matrix'
use_displaced_mesh = true
[]
[momentum_mesh_advection]
type = INSADMomentumMeshAdvection
variable = vel
disp_x = 'disp_x'
disp_y = 'disp_y'
use_displaced_mesh = true
block = 'matrix'
[]
[mean_zero_pressure]
type = ScalarLagrangeMultiplier
variable = p
lambda = lambda
block = 'matrix'
[]
# zeta*K*vel + K * disp
[dynamic_stress_x]
type = DynamicStressDivergenceTensors
block = inclusion
component = 0
variable = disp_x
zeta = ${zeta}
[]
[dynamic_stress_y]
type = DynamicStressDivergenceTensors
block = inclusion
component = 1
variable = disp_y
zeta = ${zeta}
[]
# M*accel + eta*M*vel
[inertia_x]
type = InertialForce
variable = disp_x
velocity = vel_x_solid
acceleration = accel_x
beta = ${beta} # Newmark time integration
gamma = ${gamma} # Newmark time integration
eta = ${eta}
block = 'inclusion'
[]
[inertia_y]
type = InertialForce
variable = disp_y
velocity = vel_y_solid
acceleration = accel_y
beta = ${beta}
gamma = ${gamma}
eta = ${eta}
block = 'inclusion'
[]
[]
[InterfaceKernels]
[penalty]
type = ADPenaltyVelocityContinuityNewmarkBeta
variable = vel
fluid_velocity = vel
displacements = 'disp_x disp_y'
solid_velocities = 'vel_x_solid vel_y_solid'
solid_accelerations = 'accel_x accel_y'
boundary = 'interface_matrix_side'
penalty = ${youngs_modulus}
beta = ${beta}
gamma = ${gamma}
[]
[]
[Materials]
[viscous_mat]
type = ADGenericConstantMaterial
block = 'matrix'
prop_names = 'rho mu'
prop_values = '1 1'
[]
[ins_mat]
type = INSADTauMaterial
velocity = vel
pressure = p
block = 'matrix'
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = ${youngs_modulus}
poissons_ratio = 0.3
block = 'inclusion'
[]
[strain]
type = ComputeFiniteStrain
displacements = 'disp_x disp_y'
block = 'inclusion'
[]
[small_stress]
type = ComputeFiniteStrainElasticStress
block = 'inclusion'
[]
[density]
type = GenericConstantMaterial
block = 'inclusion'
prop_names = density
prop_values = 3 # kg/m3
[]
[]
[BCs] # mesh boundaries remain still so I dont think we need to use deformed mesh for vel
[no_disp_x]
type = DirichletBC
variable = disp_x
boundary = 'bottom top left right'
value = 0
[]
[no_disp_y]
type = DirichletBC
variable = disp_y
boundary = 'bottom top left right'
value = 0
[]
[shear_top_x]
type = ADVectorFunctionDirichletBC
boundary = top
variable = vel
function_x = '-0.001'
[]
[shear_bottom_x]
type = ADVectorFunctionDirichletBC
boundary = 'bottom'
variable = vel
function_x = '0.001'
[]
[Periodic]
[vel]
variable = vel
primary = 'left'
secondary = 'right'
translation = '1 0 0'
[]
[x_p]
variable = p
primary = 'left'
secondary = 'right'
translation = '1 0 0'
[]
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
petsc_options_iname = '-pc_type -pc_factor_shift_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu NONZERO strumpack'
[]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
end_time = 100.0
nl_abs_tol = 1e-12
[TimeStepper]
type = IterationAdaptiveDT
optimal_iterations = 5
dt = 0.005
growth_factor = 1.5
cutback_factor = 0.9
[]
[]
[Postprocessors]
[pressure_integral]
type = ElementIntegralVariablePostprocessor
variable = p
execute_on = linear
block = 'matrix'
[]
[max_vel_y]
type = ElementExtremeValue
variable = vel_y_fluid
block = 'matrix'
value_type = max
[]
[min_vel_y]
type = ElementExtremeValue
variable = vel_y_fluid
block = 'matrix'
value_type = min
[]
[]
[Outputs]
hide = 'pressure_integral lambda'
[csv]
type = CSV
execute_on = 'final'
[]
[]
(modules/navier_stokes/test/tests/finite_element/ins/velocity_channel/ad-traction-supg.i)
# This input file tests outflow boundary conditions for the incompressible NS equations.
[GlobalParams]
integrate_p_by_parts = true
viscous_form = traction
[]
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 3.0
ymin = 0
ymax = 1.0
nx = 30
ny = 10
elem_type = QUAD9
[]
[Variables]
[vel]
order = SECOND
family = LAGRANGE_VEC
[]
[p]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
[mass]
type = INSADMass
variable = p
[]
[momentum_convection]
type = INSADMomentumAdvection
variable = vel
[]
[momentum_viscous]
type = INSADMomentumViscous
variable = vel
[]
[momentum_pressure]
type = INSADMomentumPressure
variable = vel
pressure = p
[]
[momentum_supg]
type = INSADMomentumSUPG
variable = vel
velocity = vel
[]
[]
[BCs]
[wall]
type = VectorFunctionDirichletBC
variable = vel
boundary = 'top bottom'
function_x = 0
function_y = 0
[]
[inlet]
type = VectorFunctionDirichletBC
variable = vel
boundary = 'left'
function_x = inlet_func
function_y = 0
[]
[]
[Materials]
[const]
type = ADGenericConstantMaterial
block = 0
prop_names = 'rho mu'
prop_values = '1 1'
[]
[ins_mat]
type = INSADTauMaterial
velocity = vel
pressure = p
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
solve_type = NEWTON
[]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
line_search = none
nl_rel_tol = 1e-12
[]
[Outputs]
[out]
type = Exodus
[]
[]
[Functions]
[inlet_func]
type = ParsedFunction
expression = '-4 * (y - 0.5)^2 + 1'
[]
[]
(modules/fsi/test/tests/2d-small-strain-transient/ad-fsi-flat-channel.i)
[GlobalParams]
displacements = 'disp_x disp_y'
order = FIRST
preset = false
use_displaced_mesh = true
[]
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 3.0
ymin = 0
ymax = 1.0
nx = 10
ny = 15
elem_type = QUAD4
[]
[subdomain1]
type = SubdomainBoundingBoxGenerator
bottom_left = '0.0 0.5 0'
block_id = 1
top_right = '3.0 1.0 0'
input = gmg
[]
[interface]
type = SideSetsBetweenSubdomainsGenerator
primary_block = '0'
paired_block = '1'
new_boundary = 'master0_interface'
input = subdomain1
[]
[break_boundary]
type = BreakBoundaryOnSubdomainGenerator
input = interface
[]
[]
[Variables]
[vel]
block = 0
family = LAGRANGE_VEC
[]
[p]
block = 0
order = FIRST
[]
[disp_x]
[]
[disp_y]
[]
[vel_x_solid]
block = 1
[]
[vel_y_solid]
block = 1
[]
[]
[Kernels]
[mass]
type = INSADMass
variable = p
block = 0
[]
[mass_pspg]
type = INSADMassPSPG
variable = p
block = 0
[]
[momentum_time]
type = INSADMomentumTimeDerivative
variable = vel
block = 0
[]
[momentum_convection]
type = INSADMomentumAdvection
variable = vel
block = 0
[]
[momentum_viscous]
type = INSADMomentumViscous
variable = vel
block = 0
[]
[momentum_pressure]
type = INSADMomentumPressure
variable = vel
pressure = p
integrate_p_by_parts = true
block = 0
[]
[momentum_supg]
type = INSADMomentumSUPG
variable = vel
material_velocity = relative_velocity
block = 0
[]
[momentum_mesh]
type = INSADMomentumMeshAdvection
variable = vel
disp_x = 'disp_x'
disp_y = 'disp_y'
block = 0
[]
[disp_x_fluid]
type = Diffusion
variable = disp_x
block = 0
use_displaced_mesh = false
[]
[disp_y_fluid]
type = Diffusion
variable = disp_y
block = 0
use_displaced_mesh = false
[]
[accel_tensor_x]
type = CoupledTimeDerivative
variable = disp_x
v = vel_x_solid
block = 1
use_displaced_mesh = false
[]
[accel_tensor_y]
type = CoupledTimeDerivative
variable = disp_y
v = vel_y_solid
block = 1
use_displaced_mesh = false
[]
[vxs_time_derivative_term]
type = CoupledTimeDerivative
variable = vel_x_solid
v = disp_x
block = 1
use_displaced_mesh = false
[]
[vys_time_derivative_term]
type = CoupledTimeDerivative
variable = vel_y_solid
v = disp_y
block = 1
use_displaced_mesh = false
[]
[source_vxs]
type = MatReaction
variable = vel_x_solid
block = 1
reaction_rate = 1
use_displaced_mesh = false
[]
[source_vys]
type = MatReaction
variable = vel_y_solid
block = 1
reaction_rate = 1
use_displaced_mesh = false
[]
[]
[InterfaceKernels]
[penalty]
type = ADPenaltyVelocityContinuity
variable = vel
fluid_velocity = vel
displacements = 'disp_x disp_y'
solid_velocities = 'vel_x_solid vel_y_solid'
boundary = master0_interface
penalty = 1e6
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[solid_domain]
strain = SMALL
incremental = false
# generate_output = 'strain_xx strain_yy strain_zz' ## Not at all necessary, but nice
block = '1'
[]
[]
[Materials]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e2
poissons_ratio = 0.3
block = '1'
use_displaced_mesh = false
[]
[small_stress]
type = ComputeLinearElasticStress
block = 1
[]
[const]
type = ADGenericConstantMaterial
block = 0
prop_names = 'rho mu'
prop_values = '1 1'
[]
[ins_mat]
type = INSADTauMaterial
velocity = vel
pressure = p
block = 0
[]
[]
[BCs]
[fluid_bottom]
type = ADVectorFunctionDirichletBC
variable = vel
boundary = 'bottom'
function_x = 0
function_y = 0
[]
[fluid_left]
type = ADVectorFunctionDirichletBC
variable = vel
boundary = 'left_to_0'
function_x = 'inlet_func'
function_y = 0
# The displacements actually affect the result of the function evaluation so in order to eliminate the impact
# on the Jacobian we set 'use_displaced_mesh = false' here
use_displaced_mesh = false
[]
[no_disp_x]
type = DirichletBC
variable = disp_x
boundary = 'bottom top left_to_1 right_to_1 left_to_0 right_to_0'
value = 0
[]
[no_disp_y]
type = DirichletBC
variable = disp_y
boundary = 'bottom top left_to_1 right_to_1 left_to_0 right_to_0'
value = 0
[]
[solid_x_no_slip]
type = DirichletBC
variable = vel_x_solid
boundary = 'top left_to_1 right_to_1'
value = 0.0
[]
[solid_y_no_slip]
type = DirichletBC
variable = vel_y_solid
boundary = 'top left_to_1 right_to_1'
value = 0.0
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
num_steps = 5
# num_steps = 60
dt = 0.1
dtmin = 0.1
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
line_search = none
nl_rel_tol = 1e-50
nl_abs_tol = 1e-10
[]
[Outputs]
exodus = true
[]
[Functions]
[inlet_func]
type = ParsedFunction
expression = '(-16 * (y - 0.25)^2 + 1) * (1 + cos(t))'
[]
[]
(modules/navier_stokes/test/tests/finite_element/ins/coupled-force/gravity-through-coupled-force.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
nx = 16
ny = 16
[]
[./corner_node]
type = ExtraNodesetGenerator
new_boundary = 'pinned_node'
nodes = '0'
input = gen
[../]
[]
[Variables]
[./velocity]
family = LAGRANGE_VEC
[../]
[./p]
[../]
[u]
family = LAGRANGE_VEC
[]
[]
[AuxVariables]
[gravity]
family = LAGRANGE_VEC
[]
[]
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[gravity]
type = VectorConstantIC
x_value = '0'
y_value = '-9.81'
variable = gravity
[]
[]
[Kernels]
inactive = 'momentum_coupled_forces_two_vars momentum_coupled_forces_two_funcs'
[./mass]
type = INSADMass
variable = p
[../]
[./mass_pspg]
type = INSADMassPSPG
variable = p
[../]
[./momentum_convection]
type = INSADMomentumAdvection
variable = velocity
[../]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
integrate_p_by_parts = true
[../]
[momentum_coupled_forces_var_and_func]
type = INSADMomentumCoupledForce
variable = velocity
coupled_vector_var = u
vector_function = 'vector_gravity_func'
[]
[momentum_coupled_forces_two_vars]
type = INSADMomentumCoupledForce
variable = velocity
coupled_vector_var = 'u gravity'
[]
[momentum_coupled_forces_two_funcs]
type = INSADMomentumCoupledForce
variable = velocity
vector_function = 'vector_func vector_gravity_func'
[]
[./momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[../]
[u_diff]
type = VectorDiffusion
variable = u
[]
[]
[BCs]
[./no_slip]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom right left top'
[../]
[./pressure_pin]
type = DirichletBC
variable = p
boundary = 'pinned_node'
value = 0
[../]
[u_left]
type = VectorFunctionDirichletBC
variable = u
boundary = 'left'
function_x = 1
function_y = 1
[]
[u_right]
type = VectorFunctionDirichletBC
variable = u
boundary = 'right'
function_x = -1
function_y = -1
[]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[ins_mat]
type = INSADTauMaterial
velocity = velocity
pressure = p
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_levels -ksp_gmres_restart'
petsc_options_value = 'asm 6 200'
line_search = 'none'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
[out]
type = Exodus
hide = 'gravity'
[]
[]
[Functions]
[vector_func]
type = ParsedVectorFunction
expression_x = '-2*x + 1'
expression_y = '-2*x + 1'
[]
[vector_gravity_func]
type = ParsedVectorFunction
expression_x = '0'
expression_y = '-9.81'
[]
[]
(modules/navier_stokes/test/tests/finite_element/ins/coupled-force/steady.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
nx = 16
ny = 16
[]
[./corner_node]
type = ExtraNodesetGenerator
new_boundary = 'pinned_node'
nodes = '0'
input = gen
[../]
[]
[Variables]
[./velocity]
family = LAGRANGE_VEC
[../]
[./p]
[../]
[u]
family = LAGRANGE_VEC
[]
[]
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[./mass_pspg]
type = INSADMassPSPG
variable = p
[../]
[./momentum_convection]
type = INSADMomentumAdvection
variable = velocity
[../]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
integrate_p_by_parts = true
[../]
[momentum_coupled_force]
type = INSADMomentumCoupledForce
variable = velocity
coupled_vector_var = u
[]
[./momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[../]
[u_diff]
type = VectorDiffusion
variable = u
[]
[]
[BCs]
[./no_slip]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom right left top'
[../]
[./pressure_pin]
type = DirichletBC
variable = p
boundary = 'pinned_node'
value = 0
[../]
[u_left]
type = VectorFunctionDirichletBC
variable = u
boundary = 'left'
function_x = 1
function_y = 1
[]
[u_right]
type = VectorFunctionDirichletBC
variable = u
boundary = 'right'
function_x = -1
function_y = -1
[]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[ins_mat]
type = INSADTauMaterial
velocity = velocity
pressure = p
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_levels -ksp_gmres_restart'
petsc_options_value = 'asm 6 200'
line_search = 'none'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/ad_rz_cone_no_parts_steady_stabilized.i)
[GlobalParams]
order = FIRST
integrate_p_by_parts = false
[]
[Mesh]
file = '2d_cone.msh'
coord_type = RZ
[]
[AuxVariables]
[vel_x]
[]
[vel_y]
[]
[]
[AuxKernels]
[vel_x]
type = VectorVariableComponentAux
variable = vel_x
vector_variable = velocity
component = 'x'
[]
[vel_y]
type = VectorVariableComponentAux
variable = vel_y
vector_variable = velocity
component = 'y'
[]
[]
[Variables]
[./velocity]
family = LAGRANGE_VEC
[../]
[./p]
[../]
[]
# Need to set a non-zero initial condition because we have a velocity norm in
# the denominator for the tau coefficient of the stabilization term
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[mass_pspg]
type = INSADMassPSPG
variable = p
[]
[momentum_advection]
type = INSADMomentumAdvection
variable = velocity
[]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
[../]
[momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[]
[]
[BCs]
[p_corner]
type = DirichletBC
boundary = top_right
value = 0
variable = p
[]
[inlet]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom'
function_x = 0
function_y = 'inlet_func'
[../]
[wall]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'right'
function_x = 0
function_y = 0
[]
[axis]
type = ADVectorFunctionDirichletBC
variable = velocity
boundary = 'left'
set_y_comp = false
function_x = 0
[]
[]
[Functions]
[./inlet_func]
type = ParsedFunction
expression = '-4 * x^2 + 1'
[../]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[ins_mat]
type = INSADTauMaterial
velocity = velocity
pressure = p
[]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = 'bjacobi ilu 4'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
console = true
[./out]
type = Exodus
[../]
[]
[Postprocessors]
[./flow_in]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'bottom'
execute_on = 'timestep_end'
[../]
[./flow_out]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'top'
execute_on = 'timestep_end'
[../]
[]
(modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/ad_rz_cone_by_parts_steady_stabilized.i)
[GlobalParams]
order = FIRST
integrate_p_by_parts = true
[]
[Mesh]
file = '2d_cone.msh'
coord_type = RZ
[]
[AuxVariables]
[vel_x]
[]
[vel_y]
[]
[]
[AuxKernels]
[vel_x]
type = VectorVariableComponentAux
variable = vel_x
vector_variable = velocity
component = 'x'
[]
[vel_y]
type = VectorVariableComponentAux
variable = vel_y
vector_variable = velocity
component = 'y'
[]
[]
[Variables]
[./velocity]
family = LAGRANGE_VEC
[../]
[./p]
[../]
[]
# Need to set a non-zero initial condition because we have a velocity norm in
# the denominator for the tau coefficient of the stabilization term
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[mass_pspg]
type = INSADMassPSPG
variable = p
[]
[momentum_advection]
type = INSADMomentumAdvection
variable = velocity
[]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
[../]
[momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[]
[]
[BCs]
[inlet]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom'
function_x = 0
function_y = 'inlet_func'
[../]
[wall]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'right'
function_x = 0
function_y = 0
[]
[axis]
type = ADVectorFunctionDirichletBC
variable = velocity
boundary = 'left'
set_y_comp = false
function_x = 0
[]
[]
[Functions]
[./inlet_func]
type = ParsedFunction
expression = '-4 * x^2 + 1'
[../]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[ins_mat]
type = INSADTauMaterial
velocity = velocity
pressure = p
[]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = 'bjacobi ilu 4'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
console = true
[./out]
type = Exodus
[../]
[]
[Postprocessors]
[./flow_in]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'bottom'
execute_on = 'timestep_end'
[../]
[./flow_out]
type = VolumetricFlowRate
vel_x = vel_x
vel_y = vel_y
boundary = 'top'
execute_on = 'timestep_end'
[../]
[]
(modules/navier_stokes/test/tests/finite_element/ins/lid_driven/steady_vector_fsp_al.i)
rho=1
mu=1e-3
U=1
l=1
prefactor=${fparse 1/(l/2)^2}
n=8
gamma=${U}
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${l}
ymin = 0
ymax = ${l}
nx = ${n}
ny = ${n}
elem_type = QUAD4
[]
second_order = true
[]
[Variables]
[vel]
order = SECOND
family = LAGRANGE_VEC
[]
[p]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
[mass]
type = INSADMass
variable = p
[]
[mass_kernel]
type = MassMatrix
variable = p
matrix_tags = 'mass'
density = ${fparse -1/(gamma + mu)}
[]
[momentum_advection]
type = INSADMomentumAdvection
variable = vel
[]
[momentum_viscous]
type = INSADMomentumViscous
variable = vel
[]
[momentum_pressure]
type = INSADMomentumPressure
variable = vel
pressure = p
integrate_p_by_parts = true
[]
[momentum_graddiv]
type = INSADMomentumGradDiv
variable = vel
gamma = ${gamma}
[]
[]
[BCs]
[no_slip]
type = ADVectorFunctionDirichletBC
variable = vel
boundary = 'bottom right left'
preset = true
[]
[lid]
type = ADVectorFunctionDirichletBC
variable = vel
boundary = 'top'
function_x = 'lid_function'
preset = true
[]
[]
[Materials]
[const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '${rho} ${mu}'
[]
[insad]
type = INSADTauMaterial
velocity = vel
pressure = p
[]
[]
[Functions]
[lid_function]
# We pick a function that is exactly represented in the velocity
# space so that the Dirichlet conditions are the same regardless
# of the mesh spacing.
type = ParsedFunction
expression = '${prefactor}*${U}*x*(${l}-x)'
[]
[]
[Problem]
type = NavierStokesProblem
mass_matrix = 'mass'
extra_tag_matrices = 'mass'
use_pressure_mass_matrix = true
[]
[Preconditioning]
[FSP]
type = FSP
topsplit = 'up'
[up]
splitting = 'u p'
splitting_type = schur
petsc_options_iname = '-pc_fieldsplit_schur_fact_type -pc_fieldsplit_schur_precondition -ksp_gmres_restart -ksp_type -ksp_pc_side -ksp_rtol'
petsc_options_value = 'full self 300 fgmres right 1e-4'
[]
[u]
vars = 'vel'
petsc_options = '-ksp_converged_reason'
petsc_options_iname = '-pc_type -ksp_type -ksp_rtol -ksp_gmres_restart -ksp_pc_side -pc_factor_mat_solver_type'
petsc_options_value = 'ilu gmres 1e-2 300 right strumpack'
[]
[p]
vars = 'p'
petsc_options = '-ksp_converged_reason'
petsc_options_iname = '-ksp_type -ksp_gmres_restart -ksp_rtol -pc_type -ksp_pc_side'
petsc_options_value = 'gmres 300 1e-2 ilu right'
[]
[]
[]
[Postprocessors]
[pavg]
type = ElementAverageValue
variable = p
[]
[]
[Correctors]
[set_pressure]
type = NSPressurePin
pin_type = 'average'
variable = p
pressure_average = 'pavg'
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
nl_rel_tol = 1e-12
[]
[Outputs]
print_linear_residuals = false
[exo]
type = Exodus
execute_on = 'final'
hide = 'pavg'
[]
[]
(modules/combined/test/tests/phase_field_contact_angle/contact_angle.i)
sigma = 25e-3 #10e-3 #25e-3 #surface tension coefficient
epsilon = 1e-6 #width parameter
nu = 1e-4#mobility parameter
contactangle = 2.61799#0.523599#1.0472
lambda = ${fparse 3*sigma*epsilon/(2*sqrt(2))}
prefactor_phi = ${fparse nu*lambda/(epsilon*epsilon)}
prefactor_psi = ${fparse -epsilon*epsilon}
coeff = ${fparse lambda/(epsilon*epsilon)}
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 0.2e-3
ymin = 0
ymax = 0.2e-3
nx = 20
ny = 20
elem_type = QUAD9
[]
[]
[ICs]
[pf_ic]
type = BoundingBoxIC
variable = pf
x1 = 0.1e-3
y1 = -0.1e-3
x2 = 0.3e-03
y2 = 0.3e-3
inside = 1
outside = -1
int_width = ${fparse 2*sqrt(2)*epsilon}
[]
[velocity]
type = VectorConstantIC
x_value = 0.0
y_value = 0.0
variable = velocity
[]
[]
[Variables]
[pf]
family = LAGRANGE
order = second
[]
[auxpf]
family = LAGRANGE
order = second
[]
[velocity]
family = LAGRANGE_VEC
[]
[p]
[]
[]
[Kernels]
[mass]
type = INSADMass
variable = p
[]
[mass_pspg]
type = INSADMassPSPG
variable = p
[]
[momentum_viscous]
type = INSADMomentumViscous
variable = velocity
viscous_form = 'traction'
mu_name = 'mu'
[]
[momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
integrate_p_by_parts = false
[]
[surface_tension]
type = ADPhaseFieldTwoPhaseSurfaceTension
variable = velocity
pf = pf
auxpf = auxpf
coeff = ${coeff}
[]
[phasefield_timederivative]
type = ADTimeDerivative
variable = pf
[]
[phasefield_supg]
type = ADPhaseFieldTimeDerivativeSUPG
velocity = velocity
variable = pf
[]
[phasefield_laplacian]
type=ADPrefactorLaplacianSplit
variable = pf
c = auxpf
prefactor = ${prefactor_phi}
[]
[Auxphasefield_firstorder]
type=ADReaction
variable = auxpf
rate = 1.0
[]
[Auxphasefield_laplacian]
type=ADPrefactorLaplacianSplit
variable = auxpf
c = pf
prefactor=${prefactor_psi}
[]
[Auxphasefield_doublewell]
type=ADPhaseFieldCoupledDoubleWellPotential
variable = auxpf
c = pf
prefactor=-1.0
[]
[]
[BCs]
[no_slip]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'top bottom'
[]
[velocity_L]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'left'
[]
[velocity_R]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'right'
[]
[ContactangleBC]
type=ADPhaseFieldContactAngleBC
variable = auxpf
pf = pf
epsilon = ${epsilon}
lambda=${lambda}
sigma=${sigma}
contactangle=${contactangle}
boundary = 'top bottom'
[]
[]
[Materials]
[rho]
type = ADPhaseFieldTwoPhaseMaterial
prop_name = rho
prop_value_1 = 1000
prop_value_2 = 840
pf = pf
# outputs = exodus
[]
[mu]
type = ADPhaseFieldTwoPhaseMaterial
prop_name = mu
prop_value_1 = 1e-3
prop_value_2 = 7.6e-3
pf = pf
# outputs = exodus
[]
[ins_mat]
type = INSADTauMaterial
velocity = velocity
pressure = p
alpha = .1
[]
[]
[Postprocessors]
[contact_angle_top]
type = ObtainAvgContactAngle
boundary = top
pf=pf
execute_on = 'timestep_end'
[]
[x_position]
type = FindValueOnLine
start_point = '0 0.0001 0'
end_point ='0.0002 0.0001 0'
v = pf
target = 0.0
tol = 1e-6
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[Adaptivity]
initial_steps = 2
initial_marker = phase_marker
marker = phase_marker
max_h_level = 4
[Markers]
[phase_marker]
type = ValueRangeMarker
lower_bound = -0.99
upper_bound = 0.99
variable = pf
[]
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
start_time = 0
num_steps = 5
dtmax = 0.25
[TimeStepper]
type = IterationAdaptiveDT
dt = 1e-10
iteration_window = 2
optimal_iterations = 10
growth_factor = 2
cutback_factor = 0.5
[]
# petsc_options_iname = '-pc_type -ksp_gmres_restart -pc_factor_mat_solver_type -pc_factor_shift_type -pc_factor_shift_amount'
# petsc_options_value = 'lu 50 superlu_dist NONZERO 1e-15'
#petsc_options_iname = '-pc_type'
#petsc_options_value = 'lu '
petsc_options_iname = '-pc_type -pc_factor_shift_type -pc_factor_shift_amount'
petsc_options_value = 'lu NONZERO 1e-15 '
line_search = 'none'
nl_rel_tol = 1e-6
nl_abs_tol = 1e-8
nl_max_its = 20
nl_forced_its = 3
l_tol = 1e-6
l_max_its = 20
[]
[Outputs]
[csv]
type = CSV
time_step_interval = 1
[]
[]
(modules/navier_stokes/test/tests/finite_element/ins/coupled-force/steady-function.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
nx = 16
ny = 16
[]
[./corner_node]
type = ExtraNodesetGenerator
new_boundary = 'pinned_node'
nodes = '0'
input = gen
[../]
[]
[Variables]
[./velocity]
family = LAGRANGE_VEC
[../]
[./p]
[../]
[u]
family = LAGRANGE_VEC
[]
[]
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[./mass_pspg]
type = INSADMassPSPG
variable = p
[../]
[./momentum_convection]
type = INSADMomentumAdvection
variable = velocity
[../]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
integrate_p_by_parts = true
[../]
[momentum_coupled_force]
type = INSADMomentumCoupledForce
variable = velocity
vector_function = 'vector_func'
[]
[./momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[../]
[u_diff]
type = VectorDiffusion
variable = u
[]
[]
[BCs]
[./no_slip]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom right left top'
[../]
[./pressure_pin]
type = DirichletBC
variable = p
boundary = 'pinned_node'
value = 0
[../]
[u_left]
type = VectorFunctionDirichletBC
variable = u
boundary = 'left'
function_x = 1
function_y = 1
[]
[u_right]
type = VectorFunctionDirichletBC
variable = u
boundary = 'right'
function_x = -1
function_y = -1
[]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu'
prop_values = '1 1'
[../]
[ins_mat]
type = INSADTauMaterial
velocity = velocity
pressure = p
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_levels -ksp_gmres_restart'
petsc_options_value = 'asm 6 200'
line_search = 'none'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
exodus = true
[]
[Functions]
[vector_func]
type = ParsedVectorFunction
expression_x = '-2*x + 1'
expression_y = '-2*x + 1'
[]
[]