- variableThe name of the variable that this residual object operates on
C++ Type:NonlinearVariableName
Unit:(no unit assumed)
Controllable:No
Description:The name of the variable that this residual object operates on
INSADEnergySUPG
This object adds stabilization to the incompressible energy equation in the form of where is the stabilization parameter, is the velocity vector and is the strong residual of the momentum equation. is calculated based on the advection velocity, thermal conductivity, density, heat capacity, time step size, and mesh size. This term adds additional (consistent) streamline diffusion such that higher Reynolds numbers can be simulated without producing crippling oscillations.
Adds the supg stabilization to the INS temperature/energy equation
Input Parameters
- 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
- displacementsThe displacements
C++ Type:std::vector<VariableName>
Unit:(no unit assumed)
Controllable:No
Description:The displacements
- material_velocityA material property describing the velocity
C++ Type:MaterialPropertyName
Unit:(no unit assumed)
Controllable:No
Description:A material property describing the velocity
- matrix_onlyFalseWhether this object is only doing assembly to matrices (no vectors)
Default:False
C++ Type:bool
Controllable:No
Description:Whether this object is only doing assembly to matrices (no vectors)
- tau_nametau_energyThe name of the stabilization parameter tau.
Default:tau_energy
C++ Type:MaterialPropertyName
Unit:(no unit assumed)
Controllable:No
Description:The name of the stabilization parameter tau.
- velocityThe velocity variable.
C++ Type:std::vector<VariableName>
Unit:(no unit assumed)
Controllable:No
Description:The velocity variable.
Optional Parameters
- absolute_value_vector_tagsThe tags for the vectors this residual object should fill with the absolute value of the residual contribution
C++ Type:std::vector<TagName>
Controllable:No
Description:The tags for the vectors this residual object should fill with the absolute value of the residual contribution
- extra_matrix_tagsThe extra tags for the matrices this Kernel should fill
C++ Type:std::vector<TagName>
Controllable:No
Description:The extra tags for the matrices this Kernel should fill
- extra_vector_tagsThe extra tags for the vectors this Kernel should fill
C++ Type:std::vector<TagName>
Controllable:No
Description:The extra tags for the vectors this Kernel should fill
- matrix_tagssystemThe tag for the matrices this Kernel should fill
Default:system
C++ Type:MultiMooseEnum
Options:nontime, system
Controllable:No
Description:The tag for the matrices this Kernel should fill
- vector_tagsnontimeThe tag for the vectors this Kernel should fill
Default:nontime
C++ Type:MultiMooseEnum
Options:nontime, time
Controllable:No
Description:The tag for the vectors this Kernel should fill
Contribution To Tagged Field Data Parameters
- control_tagsAdds user-defined labels for accessing object parameters via control logic.
C++ Type:std::vector<std::string>
Controllable:No
Description:Adds user-defined labels for accessing object parameters via control logic.
- diag_save_inThe name of auxiliary variables to save this Kernel's diagonal Jacobian contributions to. Everything about that variable must match everything about this variable (the type, what blocks it's on, etc.)
C++ Type:std::vector<AuxVariableName>
Unit:(no unit assumed)
Controllable:No
Description:The name of auxiliary variables to save this Kernel's diagonal Jacobian contributions to. Everything about that variable must match everything about this variable (the type, what blocks it's on, etc.)
- 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
- save_inThe name of auxiliary variables to save this Kernel's residual contributions to. Everything about that variable must match everything about this variable (the type, what blocks it's on, etc.)
C++ Type:std::vector<AuxVariableName>
Unit:(no unit assumed)
Controllable:No
Description:The name of auxiliary variables to save this Kernel's residual contributions to. Everything about that variable must match everything about this variable (the type, what blocks it's on, etc.)
- 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
- 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/combined/examples/stochastic/laser_welding_dimred/physics_objects.i)
- (modules/navier_stokes/examples/laser-welding/2d.i)
- (modules/navier_stokes/test/tests/finite_element/ins/energy-conservation/q2q1.i)
- (modules/navier_stokes/test/tests/finite_element/ins/energy_source/steady.i)
- (modules/fsi/test/tests/2d-finite-strain-steady/thermal-me.i)
- (modules/navier_stokes/test/tests/finite_element/ins/energy_source/steady-var.i)
- (modules/navier_stokes/test/tests/finite_element/ins/boussinesq/benchmark/benchmark.i)
- (modules/navier_stokes/test/tests/finite_element/ins/lid_driven/ad_lid_driven_stabilized_with_temp.i)
- (modules/navier_stokes/test/tests/finite_element/ins/wall_convection/steady.i)
- (modules/navier_stokes/examples/laser-welding/3d.i)
- (modules/navier_stokes/test/tests/finite_element/ins/boussinesq/boussinesq_stabilized.i)
- (modules/navier_stokes/test/tests/finite_element/ins/lid_driven/mixed-transient-steady/mixed.i)
- (modules/navier_stokes/test/tests/finite_element/ins/lid_driven/ad_lid_driven_stabilized_with_temp_transient.i)
- (modules/navier_stokes/test/tests/finite_element/ins/energy-conservation/q1q1.i)
(modules/combined/examples/stochastic/laser_welding_dimred/physics_objects.i)
[ICs]
[T]
type = FunctionIC
variable = T
function = '(${surfacetemp} - 300) / ${thickness} * y + ${surfacetemp}'
[]
[]
[Kernels]
[disp_x]
type = Diffusion
variable = disp_x
[]
[disp_y]
type = Diffusion
variable = disp_y
[]
[mass]
type = INSADMass
variable = p
use_displaced_mesh = true
[]
[mass_pspg]
type = INSADMassPSPG
variable = p
use_displaced_mesh = true
[]
[momentum_time]
type = INSADMomentumTimeDerivative
variable = vel
use_displaced_mesh = true
[]
[momentum_advection]
type = INSADMomentumAdvection
variable = vel
use_displaced_mesh = true
[]
[momentum_mesh_advection]
type = INSADMomentumMeshAdvection
variable = vel
disp_x = disp_x
disp_y = disp_y
use_displaced_mesh = true
[]
[momentum_viscous]
type = INSADMomentumViscous
variable = vel
use_displaced_mesh = true
[]
[momentum_pressure]
type = INSADMomentumPressure
variable = vel
pressure = p
integrate_p_by_parts = true
use_displaced_mesh = true
[]
[momentum_supg]
type = INSADMomentumSUPG
variable = vel
material_velocity = relative_velocity
use_displaced_mesh = true
[]
[temperature_time]
type = INSADHeatConductionTimeDerivative
variable = T
use_displaced_mesh = true
[]
[temperature_advection]
type = INSADEnergyAdvection
variable = T
use_displaced_mesh = true
[]
[temperature_mesh_advection]
type = INSADEnergyMeshAdvection
variable = T
disp_x = disp_x
disp_y = disp_y
use_displaced_mesh = true
[]
[temperature_conduction]
type = ADHeatConduction
variable = T
thermal_conductivity = 'k'
use_displaced_mesh = true
[]
[temperature_supg]
type = INSADEnergySUPG
variable = T
velocity = vel
use_displaced_mesh = true
[]
[]
[BCs]
[x_no_disp]
type = DirichletBC
variable = disp_x
boundary = 'bottom'
value = 0
[]
[y_no_disp]
type = DirichletBC
variable = disp_y
boundary = 'bottom'
value = 0
[]
[no_slip]
type = ADVectorFunctionDirichletBC
variable = vel
boundary = 'bottom right left'
[]
[T_cold]
type = DirichletBC
variable = T
boundary = 'bottom'
value = 300
[]
[radiation_flux]
type = FunctionRadiativeBC
variable = T
boundary = 'top'
emissivity_function = '1'
Tinfinity = 300
stefan_boltzmann_constant = 5.67e-8
use_displaced_mesh = true
[]
[weld_flux]
type = GaussianEnergyFluxBC
variable = T
boundary = 'top'
P0 = ${power}
R = ${R}
x_beam_coord = '${scanning_speed}*t'
y_beam_coord = '0'
use_displaced_mesh = true
[]
[vapor_recoil]
type = INSADVaporRecoilPressureMomentumFluxBC
variable = vel
boundary = 'top'
use_displaced_mesh = true
[]
[surface_tension]
type = INSADSurfaceTensionBC
variable = vel
boundary = 'top'
use_displaced_mesh = true
[]
[displace_x_top]
type = INSADDisplaceBoundaryBC
boundary = 'top'
variable = 'disp_x'
velocity = 'vel'
component = 0
associated_subdomain = 0
[]
[displace_y_top]
type = INSADDisplaceBoundaryBC
boundary = 'top'
variable = 'disp_y'
velocity = 'vel'
component = 1
associated_subdomain = 0
[]
[displace_x_top_dummy]
type = INSADDummyDisplaceBoundaryIntegratedBC
boundary = 'top'
variable = 'disp_x'
velocity = 'vel'
component = 0
[]
[displace_y_top_dummy]
type = INSADDummyDisplaceBoundaryIntegratedBC
boundary = 'top'
variable = 'disp_y'
velocity = 'vel'
component = 1
[]
[]
[Materials]
[ins_mat]
type = INSADStabilized3Eqn
velocity = vel
pressure = p
temperature = T
use_displaced_mesh = true
[]
[steel]
type = LaserWeld316LStainlessSteel
temperature = T
use_displaced_mesh = true
[]
[steel_boundary]
type = LaserWeld316LStainlessSteelBoundary
boundary = 'top'
temperature = T
use_displaced_mesh = true
[]
[const]
type = GenericConstantMaterial
prop_names = 'abs sb_constant'
prop_values = '1 5.67e-8'
use_displaced_mesh = true
[]
[]
(modules/navier_stokes/examples/laser-welding/2d.i)
endtime=5e-4 # s
timestep=${fparse endtime/100} # s
surfacetemp=300 # K
power=190 # W
R=1.8257418583505537e-4 # m
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -.45e-3 # m
xmax = 0.45e-3 # m
ymin = -.9e-4 # m
ymax = 0
nx = 25
ny = 5
displacements = 'disp_x disp_y'
[]
[GlobalParams]
temperature = T
[]
[Variables]
[vel]
family = LAGRANGE_VEC
[]
[T]
[]
[p]
[]
[disp_x]
[]
[disp_y]
[]
[]
[AuxVariables]
[vel_x_aux]
[InitialCondition]
type = ConstantIC
value = 1e-15
[]
[]
[vel_y_aux]
[InitialCondition]
type = ConstantIC
value = 1e-15
[]
[]
[]
[AuxKernels]
[vel_x_value]
type = VectorVariableComponentAux
variable = vel_x_aux
vector_variable = vel
component = x
[]
[vel_y_value]
type = VectorVariableComponentAux
variable = vel_y_aux
vector_variable = vel
component = y
[]
[]
[ICs]
[T]
type = FunctionIC
variable = T
function = '(${surfacetemp} - 300) / .7e-3 * y + ${surfacetemp}'
[]
[]
[Kernels]
[disp_x]
type = Diffusion
variable = disp_x
[]
[disp_y]
type = Diffusion
variable = disp_y
[]
[mass]
type = INSADMass
variable = p
use_displaced_mesh = true
[]
[mass_pspg]
type = INSADMassPSPG
variable = p
use_displaced_mesh = true
[]
[momentum_time]
type = INSADMomentumTimeDerivative
variable = vel
use_displaced_mesh = true
[]
[momentum_advection]
type = INSADMomentumAdvection
variable = vel
use_displaced_mesh = true
[]
[momentum_mesh_advection]
type = INSADMomentumMeshAdvection
variable = vel
disp_x = disp_x
disp_y = disp_y
use_displaced_mesh = true
[]
[momentum_viscous]
type = INSADMomentumViscous
variable = vel
use_displaced_mesh = true
[]
[momentum_pressure]
type = INSADMomentumPressure
variable = vel
pressure = p
integrate_p_by_parts = true
use_displaced_mesh = true
[]
[momentum_supg]
type = INSADMomentumSUPG
variable = vel
material_velocity = relative_velocity
use_displaced_mesh = true
[]
[temperature_time]
type = INSADHeatConductionTimeDerivative
variable = T
use_displaced_mesh = true
[]
[temperature_advection]
type = INSADEnergyAdvection
variable = T
use_displaced_mesh = true
[]
[temperature_mesh_advection]
type = INSADEnergyMeshAdvection
variable = T
disp_x = disp_x
disp_y = disp_y
use_displaced_mesh = true
[]
[temperature_conduction]
type = ADHeatConduction
variable = T
thermal_conductivity = 'k'
use_displaced_mesh = true
[]
[temperature_supg]
type = INSADEnergySUPG
variable = T
velocity = vel
use_displaced_mesh = true
[]
[]
[BCs]
[x_no_disp]
type = DirichletBC
variable = disp_x
boundary = 'bottom'
value = 0
[]
[y_no_disp]
type = DirichletBC
variable = disp_y
boundary = 'bottom'
value = 0
[]
[no_slip]
type = ADVectorFunctionDirichletBC
variable = vel
boundary = 'bottom right left'
[]
[T_cold]
type = DirichletBC
variable = T
boundary = 'bottom'
value = 300
[]
[radiation_flux]
type = FunctionRadiativeBC
variable = T
boundary = 'top'
emissivity_function = '1'
Tinfinity = 300
stefan_boltzmann_constant = 5.67e-8
use_displaced_mesh = true
[]
[weld_flux]
type = GaussianEnergyFluxBC
variable = T
boundary = 'top'
P0 = ${power}
R = ${R}
x_beam_coord = '-0.35e-3 +0.7e-3*t/${endtime}'
y_beam_coord = '0'
use_displaced_mesh = true
[]
[vapor_recoil]
type = INSADVaporRecoilPressureMomentumFluxBC
variable = vel
boundary = 'top'
use_displaced_mesh = true
[]
[surface_tension]
type = INSADSurfaceTensionBC
variable = vel
boundary = 'top'
use_displaced_mesh = true
include_gradient_terms = true
[]
[displace_x_top]
type = INSADDisplaceBoundaryBC
boundary = 'top'
variable = 'disp_x'
velocity = 'vel'
component = 0
associated_subdomain = 0
[]
[displace_y_top]
type = INSADDisplaceBoundaryBC
boundary = 'top'
variable = 'disp_y'
velocity = 'vel'
component = 1
associated_subdomain = 0
[]
[displace_x_top_dummy]
type = INSADDummyDisplaceBoundaryIntegratedBC
boundary = 'top'
variable = 'disp_x'
velocity = 'vel'
component = 0
[]
[displace_y_top_dummy]
type = INSADDummyDisplaceBoundaryIntegratedBC
boundary = 'top'
variable = 'disp_y'
velocity = 'vel'
component = 1
[]
[]
[Materials]
[ins_mat]
type = INSADStabilized3Eqn
velocity = vel
pressure = p
temperature = T
use_displaced_mesh = true
[]
[steel]
type = AriaLaserWeld304LStainlessSteel
temperature = T
beta = 1e7
use_displaced_mesh = true
[]
[steel_boundary]
type = AriaLaserWeld304LStainlessSteelBoundary
boundary = 'top'
temperature = T
use_displaced_mesh = true
[]
[const]
type = GenericConstantMaterial
prop_names = 'abs sb_constant'
prop_values = '1 5.67e-8'
use_displaced_mesh = true
[]
[]
[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
end_time = ${endtime}
dtmin = 1e-8
dtmax = ${timestep}
petsc_options = '-snes_converged_reason -ksp_converged_reason -options_left'
solve_type = 'NEWTON'
line_search = 'none'
nl_max_its = 12
l_max_its = 100
[TimeStepper]
type = IterationAdaptiveDT
optimal_iterations = 7
dt = ${timestep}
linear_iteration_ratio = 1e6
growth_factor = 1.5
[]
[]
[Outputs]
[exodus]
type = Exodus
output_material_properties = true
show_material_properties = 'mu'
[]
checkpoint = true
perf_graph = true
[]
[Debug]
show_var_residual_norms = true
[]
[Adaptivity]
marker = combo
max_h_level = 4
[Indicators]
[error_T]
type = GradientJumpIndicator
variable = T
[]
[error_dispz]
type = GradientJumpIndicator
variable = disp_y
[]
[]
[Markers]
[errorfrac_T]
type = ErrorFractionMarker
refine = 0.4
coarsen = 0.2
indicator = error_T
[]
[errorfrac_dispz]
type = ErrorFractionMarker
refine = 0.4
coarsen = 0.2
indicator = error_dispz
[]
[combo]
type = ComboMarker
markers = 'errorfrac_T errorfrac_dispz'
[]
[]
[]
[Postprocessors]
[num_dofs]
type = NumDOFs
system = 'NL'
[]
[nl]
type = NumNonlinearIterations
[]
[tot_nl]
type = CumulativeValuePostprocessor
postprocessor = 'nl'
[]
[]
(modules/navier_stokes/test/tests/finite_element/ins/energy-conservation/q2q1.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
nx = 10
ny = 10
dim = 2
[]
[subdomain]
type = SubdomainBoundingBoxGenerator
bottom_left = '0.5 0 0'
top_right = '1 1 0'
block_id = 1
input = gen
[]
[break_boundary]
input = subdomain
type = BreakBoundaryOnSubdomainGenerator
boundaries = 'bottom top'
[]
[sideset]
type = SideSetsBetweenSubdomainsGenerator
input = break_boundary
primary_block = '1'
paired_block = '0'
new_boundary = 'fluid_left'
[]
coord_type = RZ
second_order = true
[]
[Variables]
[T]
order = SECOND
[]
[velocity]
family = LAGRANGE_VEC
order = SECOND
block = 1
[]
[pressure]
block = 1
[]
[]
[Kernels]
[mass]
type = INSADMass
variable = pressure
block = 1
[]
[momentum_convection]
type = INSADMomentumAdvection
variable = velocity
block = 1
[]
[momentum_viscous]
type = INSADMomentumViscous
variable = velocity
block = 1
[]
[momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = pressure
integrate_p_by_parts = true
block = 1
[]
[momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
block = 1
[]
[temperature_advection]
type = INSADEnergyAdvection
variable = T
block = 1
[]
[temperature_supg]
type = INSADEnergySUPG
variable = T
velocity = velocity
block = 1
[]
[temperature_conduction]
type = ADHeatConduction
variable = T
thermal_conductivity = 'k'
[]
[heat_source]
type = BodyForce
variable = T
block = 0
function = 'x + y'
[]
[]
[BCs]
[velocity_inlet]
type = VectorFunctionDirichletBC
variable = velocity
function_y = 1
boundary = 'bottom_to_1'
[]
[wall]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'fluid_left right'
[]
[convective_heat_transfer]
type = ConvectiveHeatFluxBC
variable = T
T_infinity = 0
heat_transfer_coefficient = 1
boundary = 'right'
[]
[]
[Materials]
[constant]
type = ADGenericConstantMaterial
prop_names = 'cp rho k mu'
prop_values = '1 1 1 1'
[]
[ins]
type = INSADStabilized3Eqn
pressure = pressure
velocity = velocity
temperature = T
block = 1
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
[]
[Outputs]
csv = true
[]
[Postprocessors]
[convective_heat_transfer]
type = ConvectiveHeatTransferSideIntegral
T_solid = T
T_fluid = 0
htc = 1
boundary = 'right'
[]
[advection]
type = INSADElementIntegralEnergyAdvection
temperature = T
velocity = velocity
cp = cp
rho = rho
block = 1
[]
[source]
type = FunctionElementIntegral
function = 'x + y'
block = 0
[]
[energy_balance]
type = ParsedPostprocessor
expression = 'convective_heat_transfer + advection - source'
pp_names = 'convective_heat_transfer advection source'
[]
[]
(modules/navier_stokes/test/tests/finite_element/ins/energy_source/steady.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
nx = 16
ny = 16
[]
[./corner_node]
type = ExtraNodesetGenerator
new_boundary = 'pinned_node'
nodes = '0'
input = gen
[../]
[]
[Variables]
[./velocity]
family = LAGRANGE_VEC
[../]
[./p]
[../]
[temperature][]
[]
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[./mass_pspg]
type = INSADMassPSPG
variable = p
[../]
[./momentum_convection]
type = INSADMomentumAdvection
variable = velocity
[../]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
integrate_p_by_parts = true
[../]
[./momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[../]
[./temperature_advection]
type = INSADEnergyAdvection
variable = temperature
[../]
[./temperature_conduction]
type = ADHeatConduction
variable = temperature
thermal_conductivity = 'k'
[../]
[temperature_source]
type = INSADEnergySource
variable = temperature
source_function = 1
[]
[temperature_supg]
type = INSADEnergySUPG
variable = temperature
velocity = velocity
[]
[]
[BCs]
[./no_slip]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom right left'
[../]
[./lid]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'top'
function_x = 'lid_function'
[../]
[./pressure_pin]
type = DirichletBC
variable = p
boundary = 'pinned_node'
value = 0
[../]
[./temperature_hot]
type = DirichletBC
variable = temperature
boundary = 'bottom'
value = 1
[../]
[./temperature_cold]
type = DirichletBC
variable = temperature
boundary = 'top'
value = 0
[../]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu cp k'
prop_values = '1 1 1 .01'
[../]
[ins_mat]
type = INSADStabilized3Eqn
velocity = velocity
pressure = p
temperature = temperature
[]
[]
[Functions]
[./lid_function]
# We pick a function that is exactly represented in the velocity
# space so that the Dirichlet conditions are the same regardless
# of the mesh spacing.
type = ParsedFunction
expression = '4*x*(1-x)'
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_levels -ksp_gmres_restart'
petsc_options_value = 'asm 6 200'
line_search = 'none'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
exodus = true
[]
(modules/fsi/test/tests/2d-finite-strain-steady/thermal-me.i)
# Units: specific_heat_capacity--cp--J/(kg.K); density--rho--kg/(cm^3);
# dynamic_viscosity--mu--kg/(cm.s); thermal_conductivity--k--W/(cm.K);
# pressure--kg/(cm.s^2); force--kg.cm/s^2
outlet_pressure = 0
inlet_velocity = 150 # cm/s
ini_temp = 593 # K
heat_transfer_coefficient = 9 # W/(cm2.K)
g = -981 # cm/s2
alpha_fluid = 2e-4 # thermal expansion coefficient of fluid used in INSADBoussinesqBodyForce
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
file = '2layers_2d_midline.msh'
[]
[Variables]
[velocity]
family = LAGRANGE_VEC
order = FIRST
block = 'fluid'
[]
[p]
family = LAGRANGE
order = FIRST
block = 'fluid'
[]
[Tf]
family = LAGRANGE
order = FIRST
block = 'fluid'
[]
[Ts]
family = LAGRANGE
order = FIRST
block = 'solid'
[]
[disp_x]
family = LAGRANGE
order = FIRST
block = 'solid fluid'
[]
[disp_y]
family = LAGRANGE
order = FIRST
block = 'solid fluid'
[]
[]
[AuxVariables]
[heat_source]
family = MONOMIAL
order = FIRST
block = 'solid'
[]
[]
[ICs]
[initial_velocity]
type = VectorConstantIC
variable = velocity
x_value = 0
y_value = ${inlet_velocity}
z_value = 0
[]
[initial_p]
type = FunctionIC
variable = p
function = ini_p
[]
[initial_Tf]
type = ConstantIC
variable = Tf
value = ${ini_temp}
[]
[initial_Ts]
type = ConstantIC
variable = Ts
value = ${ini_temp}
[]
[]
[Kernels]
[fluid_mass]
type = INSADMass
variable = p
use_displaced_mesh = true
[]
[fluid_mass_pspg]
type = INSADMassPSPG
variable = p
use_displaced_mesh = true
[]
[fluid_momentum_time]
type = INSADMomentumTimeDerivative
variable = velocity
use_displaced_mesh = true
[]
[fluid_momentum_convection]
type = INSADMomentumAdvection
variable = velocity
use_displaced_mesh = true
[]
[fluid_momentum_viscous]
type = INSADMomentumViscous
variable = velocity
use_displaced_mesh = true
[]
[fluid_momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
integrate_p_by_parts = true
use_displaced_mesh = true
[]
[fluid_momentum_gravity]
type = INSADGravityForce
variable = velocity
gravity = '0 ${g} 0'
use_displaced_mesh = true
[]
[fluid_momentum_buoyancy]
type = INSADBoussinesqBodyForce
variable = velocity
gravity = '0 ${g} 0'
alpha_name = 'alpha_fluid'
ref_temp = 'T_ref'
temperature = Tf
use_displaced_mesh = true
[]
[fluid_momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
use_displaced_mesh = true
[]
[fluid_temperature_time]
type = INSADHeatConductionTimeDerivative
variable = Tf
use_displaced_mesh = true
[]
[fluid_temperature_conduction]
type = ADHeatConduction
variable = Tf
thermal_conductivity = 'k'
use_displaced_mesh = true
[]
[fluid_temperature_advection]
type = INSADEnergyAdvection
variable = Tf
use_displaced_mesh = true
[]
[fluid_temperature_supg]
type = INSADEnergySUPG
variable = Tf
velocity = velocity
use_displaced_mesh = true
[]
[solid_temperature_time]
type = ADHeatConductionTimeDerivative
variable = Ts
density_name = 'rho'
specific_heat = 'cp'
block = 'solid'
use_displaced_mesh = true
[]
[solid_temperature_conduction]
type = ADHeatConduction
variable = Ts
thermal_conductivity = 'k'
block = 'solid'
use_displaced_mesh = true
[]
[heat_source]
type = ADCoupledForce
variable = Ts
v = heat_source
block = 'solid'
use_displaced_mesh = true
[]
[disp_x_smooth]
type = Diffusion
variable = disp_x
block = fluid
[]
[disp_y_smooth]
type = Diffusion
variable = disp_y
block = fluid
[]
[]
[Physics/SolidMechanics/QuasiStatic]
strain = FINITE
material_output_order = FIRST
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx strain_yy strain_zz'
[solid]
block = 'solid'
temperature = Ts
automatic_eigenstrain_names = true
[]
[]
[InterfaceKernels]
[convection_heat_transfer]
type = ConjugateHeatTransfer
variable = Tf
T_fluid = Tf
neighbor_var = 'Ts'
boundary = 'solid_wall'
htc = 'htc'
use_displaced_mesh = true
[]
[]
[AuxKernels]
[heat_source_distribution_auxk]
type = FunctionAux
variable = heat_source
function = heat_source_distribution_function
block = 'solid'
use_displaced_mesh = true
execute_on = 'INITIAL TIMESTEP_BEGIN'
[]
[]
[BCs]
[no_slip]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'solid_wall'
use_displaced_mesh = true
[]
[inlet_velocity]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'fluid_bottom'
function_y = ${inlet_velocity}
use_displaced_mesh = true
[]
[symmetry]
type = ADVectorFunctionDirichletBC
variable = velocity
boundary = 'fluid_wall'
function_x = 0
set_x_comp = true
set_y_comp = false
set_z_comp = false
use_displaced_mesh = true
[]
[outlet_p]
type = DirichletBC
variable = p
boundary = 'fluid_top'
value = ${outlet_pressure}
use_displaced_mesh = true
[]
[inlet_T]
type = DirichletBC
variable = Tf
boundary = 'fluid_bottom'
value = ${ini_temp}
use_displaced_mesh = true
[]
[pin1_y]
type = DirichletBC
variable = disp_y
boundary = 'pin1'
value = 0
use_displaced_mesh = true
[]
[pin1_x]
type = DirichletBC
variable = disp_x
boundary = 'pin1'
value = 0
use_displaced_mesh = true
[]
[top_and_bottom_y]
type = DirichletBC
variable = disp_y
boundary = 'solid_bottom solid_top fluid_top fluid_bottom'
value = 0
use_displaced_mesh = true
[]
[left_and_right_x]
type = DirichletBC
variable = disp_x
boundary = 'fluid_wall fluid_bottom'
value = 0
use_displaced_mesh = true
[]
[]
[Materials]
[rho_solid]
type = ADParsedMaterial
property_name = rho
expression = '0.0110876 * pow(9.9672e-1 + 1.179e-5 * Ts - 2.429e-9 * pow(Ts,2) + 1.219e-12 * pow(Ts,3),-3)'
coupled_variables = 'Ts'
block = 'solid'
use_displaced_mesh = true
[]
[cp_solid]
type = ADParsedMaterial
property_name = cp
expression = '0.76 * ((302.27 * pow((548.68 / Ts),2) * exp(548.68 / Ts)) / pow((exp(548.68 / Ts) - 1),2) + 2 * 8.463e-3 * Ts + 8.741e7 * 18531.7 * exp(-18531.7 / Ts) / pow(Ts,2)) + 0.24 * ((322.49 * pow((587.41/Ts),2) * exp(587.41 / Ts)) / pow((exp(587.41 / Ts) - 1),2) + 2 * 1.4679e-2 * Ts)'
coupled_variables = 'Ts'
block = 'solid'
use_displaced_mesh = true
[]
[k_solid]
type = ADParsedMaterial
property_name = k
expression = '1.158/(7.5408 + 17.692 * (Ts / 1000) + 3.6142 * pow((Ts/1000),2)) + 74.105 * pow((Ts / 1000),-2.5) * exp(-16.35 / (Ts / 1000))'
coupled_variables = 'Ts'
block = 'solid'
use_displaced_mesh = true
[]
[rho_fluid]
type = ADParsedMaterial
property_name = rho
expression = '(11096 - 1.3236 * Tf) * 1e-6'
coupled_variables = 'Tf'
block = 'fluid'
use_displaced_mesh = true
[]
[cp_fluid]
type = ADParsedMaterial
property_name = cp
expression = '159 - 2.72e-2 * Tf + 7.12e-6 * pow(Tf,2)'
coupled_variables = 'Tf'
block = 'fluid'
use_displaced_mesh = true
[]
[k_fluid]
type = ADParsedMaterial
property_name = k
expression = '(3.61 + 1.517e-2 * Tf - 1.741e-6 * pow(Tf,2)) * 1e-2'
coupled_variables = 'Tf'
block = 'fluid'
use_displaced_mesh = true
[]
[mu_fluid]
type = ADParsedMaterial
property_name = mu
expression = '4.94e-6 * exp(754.1/Tf)'
coupled_variables = 'Tf'
block = 'fluid'
use_displaced_mesh = true
[]
[buoyancy_thermal_expansion_coefficient_fluid]
type = ADGenericConstantMaterial
prop_names = 'alpha_fluid'
prop_values = '${alpha_fluid}'
block = 'fluid'
use_displaced_mesh = true
[]
[buoyancy_reference_temperature_fluid]
type = GenericConstantMaterial
prop_names = 'T_ref'
prop_values = '${ini_temp}'
block = 'fluid'
use_displaced_mesh = true
[]
[ins_mat_fluid]
type = INSADStabilized3Eqn
velocity = velocity
pressure = p
temperature = Tf
block = 'fluid'
use_displaced_mesh = true
[]
[htc]
type = ADGenericFunctionMaterial
prop_names = htc
prop_values = htc_function
use_displaced_mesh = true
[]
[elasticity_solid]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 2e7
poissons_ratio = 0.32
block = 'solid'
use_displaced_mesh = true
[]
[thermal_expansion_solid]
type = ComputeThermalExpansionEigenstrain
temperature = Ts
thermal_expansion_coeff = 2e-4
stress_free_temperature = 593
eigenstrain_name = thermal_expansion
block = 'solid'
use_displaced_mesh = true
[]
[stress_solid]
type = ComputeFiniteStrainElasticStress
block = 'solid'
[]
[]
[Functions]
[htc_function]
type = ParsedFunction
expression = ${heat_transfer_coefficient}
[]
[ini_p]
type = ParsedFunction
expression = '0.010302 * 981 * (10 - y)'
[]
[heat_source_distribution_function]
type = ParsedFunction
expression = '300 * sin(pi * y / 10)'
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
solve_type = 'PJFNK'
[]
[]
[Executioner]
type = Transient
end_time = 1e4
solve_type = 'NEWTON'
petsc_options = '-snes_converged_reason -ksp_converged_reason -snes_linesearch_monitor'
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
line_search = 'none'
nl_max_its = 30
l_max_its = 100
automatic_scaling = true
compute_scaling_once = true
off_diagonals_in_auto_scaling = true
dtmin = 1
nl_abs_tol = 1e-12
[TimeStepper]
type = IterationAdaptiveDT
optimal_iterations = 6
growth_factor = 1.5
dt = 1
[]
[]
[Outputs]
[csv]
type = CSV
file_base = 'thermal-me'
execute_on = 'final'
[]
[]
[Postprocessors]
[average_solid_Ts]
type = ElementAverageValue
variable = Ts
block = 'solid'
use_displaced_mesh = true
[]
[average_fluid_Tf]
type = ElementAverageValue
variable = Tf
block = 'fluid'
use_displaced_mesh = true
[]
[max_solid_Ts]
type = ElementExtremeValue
variable = Ts
value_type = max
block = 'solid'
use_displaced_mesh = true
[]
[max_fluid_Tf]
type = ElementExtremeValue
variable = Tf
value_type = max
block = 'fluid'
use_displaced_mesh = true
[]
[min_solid_Ts]
type = ElementExtremeValue
variable = Ts
value_type = min
block = 'solid'
use_displaced_mesh = true
[]
[min_fluid_Tf]
type = ElementExtremeValue
variable = Tf
value_type = min
block = 'fluid'
use_displaced_mesh = true
[]
[]
[Debug]
show_var_residual_norms = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/energy_source/steady-var.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
nx = 16
ny = 16
[]
[./corner_node]
type = ExtraNodesetGenerator
new_boundary = 'pinned_node'
nodes = '0'
input = gen
[../]
[]
[AuxVariables]
[u]
initial_condition = 1
[]
[]
[Variables]
[./velocity]
family = LAGRANGE_VEC
[../]
[./p]
[../]
[temperature][]
[]
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[./mass_pspg]
type = INSADMassPSPG
variable = p
[../]
[./momentum_convection]
type = INSADMomentumAdvection
variable = velocity
[../]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
integrate_p_by_parts = true
[../]
[./momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[../]
[./temperature_advection]
type = INSADEnergyAdvection
variable = temperature
[../]
[./temperature_conduction]
type = ADHeatConduction
variable = temperature
thermal_conductivity = 'k'
[../]
[temperature_source]
type = INSADEnergySource
variable = temperature
source_variable = u
[]
[temperature_supg]
type = INSADEnergySUPG
variable = temperature
velocity = velocity
[]
[]
[BCs]
[./no_slip]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom right left'
[../]
[./lid]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'top'
function_x = 'lid_function'
[../]
[./pressure_pin]
type = DirichletBC
variable = p
boundary = 'pinned_node'
value = 0
[../]
[./temperature_hot]
type = DirichletBC
variable = temperature
boundary = 'bottom'
value = 1
[../]
[./temperature_cold]
type = DirichletBC
variable = temperature
boundary = 'top'
value = 0
[../]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu cp k'
prop_values = '1 1 1 .01'
[../]
[ins_mat]
type = INSADStabilized3Eqn
velocity = velocity
pressure = p
temperature = temperature
[]
[]
[Functions]
[./lid_function]
# We pick a function that is exactly represented in the velocity
# space so that the Dirichlet conditions are the same regardless
# of the mesh spacing.
type = ParsedFunction
expression = '4*x*(1-x)'
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_levels -ksp_gmres_restart'
petsc_options_value = 'asm 6 200'
line_search = 'none'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
[out]
type = Exodus
hide = 'u'
[]
[]
(modules/navier_stokes/test/tests/finite_element/ins/boussinesq/benchmark/benchmark.i)
rayleigh=1e3
hot_temp=${rayleigh}
temp_ref=${fparse hot_temp / 2.}
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 100
ny = 100
[]
[./bottom_left]
type = ExtraNodesetGenerator
new_boundary = corner
coord = '0 0'
input = gen
[../]
[]
[Preconditioning]
[./Newton_SMP]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-12
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_shift_type -ksp_gmres_restart'
petsc_options_value = 'bjacobi lu NONZERO 200'
[]
[Debug]
show_var_residual_norms = true
[]
[Outputs]
[out]
type = Exodus
[]
[]
[Variables]
[velocity]
family = LAGRANGE_VEC
[]
[p][]
[temp]
initial_condition = 340
scaling = 1e-4
[]
[]
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[BCs]
[./velocity_dirichlet]
type = VectorDirichletBC
boundary = 'left right bottom top'
variable = velocity
# The third entry is to satisfy RealVectorValue
values = '0 0 0'
[../]
# Even though we are integrating by parts, because there are no integrated
# boundary conditions on the velocity p doesn't appear in the system of
# equations. Thus we must pin the pressure somewhere in order to ensure a
# unique solution
[./p_zero]
type = DirichletBC
boundary = corner
variable = p
value = 0
[../]
[./hot]
type = DirichletBC
variable = temp
boundary = left
value = ${hot_temp}
[../]
[./cold]
type = DirichletBC
variable = temp
boundary = right
value = 0
[../]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[mass_pspg]
type = INSADMassPSPG
variable = p
[]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[momentum_advection]
type = INSADMomentumAdvection
variable = velocity
[]
[momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
integrate_p_by_parts = true
[]
[./buoyancy]
type = INSADBoussinesqBodyForce
variable = velocity
temperature = temp
gravity = '0 -1 0'
[../]
[./gravity]
type = INSADGravityForce
variable = velocity
gravity = '0 -1 0'
[../]
[supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[]
[temp_advection]
type = INSADEnergyAdvection
variable = temp
[]
[temp_conduction]
type = ADHeatConduction
variable = temp
thermal_conductivity = 'k'
[../]
[temp_supg]
type = INSADEnergySUPG
variable = temp
velocity = velocity
[]
[]
[Materials]
[./ad_const]
type = ADGenericConstantMaterial
# alpha = coefficient of thermal expansion where rho = rho0 -alpha * rho0 * delta T
prop_names = 'mu rho alpha k cp'
prop_values = '1 1 1 1 1'
[../]
[./const]
type = GenericConstantMaterial
prop_names = 'temp_ref'
prop_values = '${temp_ref}'
[../]
[ins_mat]
type = INSADStabilized3Eqn
velocity = velocity
pressure = p
temperature = temp
[]
[]
(modules/navier_stokes/test/tests/finite_element/ins/lid_driven/ad_lid_driven_stabilized_with_temp.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
nx = 16
ny = 16
[]
[./corner_node]
type = ExtraNodesetGenerator
new_boundary = 'pinned_node'
nodes = '0'
input = gen
[../]
[]
[Variables]
[./velocity]
family = LAGRANGE_VEC
[../]
[./p]
[../]
[temperature][]
[]
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[./mass_pspg]
type = INSADMassPSPG
variable = p
[../]
[./momentum_convection]
type = INSADMomentumAdvection
variable = velocity
[../]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
integrate_p_by_parts = true
[../]
[./momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[../]
[./temperature_advection]
type = INSADEnergyAdvection
variable = temperature
[../]
[./temperature_conduction]
type = ADHeatConduction
variable = temperature
thermal_conductivity = 'k'
[../]
[temperature_supg]
type = INSADEnergySUPG
variable = temperature
velocity = velocity
[]
[]
[BCs]
[./no_slip]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom right left'
[../]
[./lid]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'top'
function_x = 'lid_function'
[../]
[./pressure_pin]
type = DirichletBC
variable = p
boundary = 'pinned_node'
value = 0
[../]
[./temperature_hot]
type = DirichletBC
variable = temperature
boundary = 'bottom'
value = 1
[../]
[./temperature_cold]
type = DirichletBC
variable = temperature
boundary = 'top'
value = 0
[../]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu cp k'
prop_values = '1 1 1 .01'
[../]
[ins_mat]
type = INSADStabilized3Eqn
velocity = velocity
pressure = p
temperature = temperature
[]
[]
[Functions]
[./lid_function]
# We pick a function that is exactly represented in the velocity
# space so that the Dirichlet conditions are the same regardless
# of the mesh spacing.
type = ParsedFunction
expression = '4*x*(1-x)'
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_levels -ksp_gmres_restart'
petsc_options_value = 'asm 6 200'
line_search = 'none'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/wall_convection/steady.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
nx = 16
ny = 16
[]
[./corner_node]
type = ExtraNodesetGenerator
new_boundary = 'pinned_node'
nodes = '0'
input = gen
[../]
[]
[Variables]
[./velocity]
family = LAGRANGE_VEC
[../]
[./p]
[../]
[temperature][]
[]
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[./mass_pspg]
type = INSADMassPSPG
variable = p
[../]
[./momentum_convection]
type = INSADMomentumAdvection
variable = velocity
[../]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
integrate_p_by_parts = true
[../]
[./momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[../]
[./temperature_advection]
type = INSADEnergyAdvection
variable = temperature
[../]
[./temperature_conduction]
type = ADHeatConduction
variable = temperature
thermal_conductivity = 'k'
[../]
[temperature_ambient_convection]
type = INSADEnergyAmbientConvection
variable = temperature
alpha = 1
T_ambient = 0.5
[]
[temperature_supg]
type = INSADEnergySUPG
variable = temperature
velocity = velocity
[]
[]
[BCs]
[./no_slip]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom right left'
[../]
[./lid]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'top'
function_x = 'lid_function'
[../]
[./pressure_pin]
type = DirichletBC
variable = p
boundary = 'pinned_node'
value = 0
[../]
[./temperature_hot]
type = DirichletBC
variable = temperature
boundary = 'bottom'
value = 1
[../]
[./temperature_cold]
type = DirichletBC
variable = temperature
boundary = 'top'
value = 0
[../]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu cp k'
prop_values = '1 1 1 .01'
[../]
[ins_mat]
type = INSADStabilized3Eqn
velocity = velocity
pressure = p
temperature = temperature
[]
[]
[Functions]
[./lid_function]
# We pick a function that is exactly represented in the velocity
# space so that the Dirichlet conditions are the same regardless
# of the mesh spacing.
type = ParsedFunction
expression = '4*x*(1-x)'
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_levels -ksp_gmres_restart'
petsc_options_value = 'asm 6 200'
line_search = 'none'
nl_rel_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/examples/laser-welding/3d.i)
period=1.25e-3
endtime=${period}
timestep=1.25e-5
surfacetemp=300
sb=5.67e-8
[GlobalParams]
temperature = T
[]
[Mesh]
type = GeneratedMesh
dim = 3
xmin = -.35e-3
xmax = 0.35e-3
ymin = -.35e-3
ymax = .35e-3
zmin = -.7e-3
zmax = 0
nx = 2
ny = 2
nz = 2
displacements = 'disp_x disp_y disp_z'
uniform_refine = 2
[]
[Variables]
[vel]
family = LAGRANGE_VEC
[]
[T]
[]
[p]
[]
[disp_x]
[]
[disp_y]
[]
[disp_z]
[]
[]
[ICs]
[T]
type = FunctionIC
variable = T
function = '(${surfacetemp} - 300) / .7e-3 * z + ${surfacetemp}'
[]
[]
[Kernels]
[disp_x]
type = Diffusion
variable = disp_x
[]
[disp_y]
type = Diffusion
variable = disp_y
[]
[disp_z]
type = Diffusion
variable = disp_z
[]
[mass]
type = INSADMass
variable = p
use_displaced_mesh = true
[]
[mass_pspg]
type = INSADMassPSPG
variable = p
use_displaced_mesh = true
[]
[momentum_time]
type = INSADMomentumTimeDerivative
variable = vel
use_displaced_mesh = true
[]
[momentum_advection]
type = INSADMomentumAdvection
variable = vel
use_displaced_mesh = true
[]
[momentum_mesh_advection]
type = INSADMomentumMeshAdvection
variable = vel
disp_x = disp_x
disp_y = disp_y
disp_z = disp_z
use_displaced_mesh = true
[]
[momentum_viscous]
type = INSADMomentumViscous
variable = vel
use_displaced_mesh = true
[]
[momentum_pressure]
type = INSADMomentumPressure
variable = vel
pressure = p
integrate_p_by_parts = true
use_displaced_mesh = true
[]
[momentum_supg]
type = INSADMomentumSUPG
variable = vel
material_velocity = relative_velocity
use_displaced_mesh = true
[]
[temperature_time]
type = INSADHeatConductionTimeDerivative
variable = T
use_displaced_mesh = true
[]
[temperature_advection]
type = INSADEnergyAdvection
variable = T
use_displaced_mesh = true
[]
[temperature_mesh_advection]
type = INSADEnergyMeshAdvection
variable = T
disp_x = disp_x
disp_y = disp_y
disp_z = disp_z
use_displaced_mesh = true
[]
[temperature_conduction]
type = ADHeatConduction
variable = T
thermal_conductivity = 'k'
use_displaced_mesh = true
[]
[temperature_supg]
type = INSADEnergySUPG
variable = T
velocity = vel
use_displaced_mesh = true
[]
[]
[BCs]
[x_no_disp]
type = DirichletBC
variable = disp_x
boundary = 'back'
value = 0
[]
[y_no_disp]
type = DirichletBC
variable = disp_y
boundary = 'back'
value = 0
[]
[z_no_disp]
type = DirichletBC
variable = disp_z
boundary = 'back'
value = 0
[]
[no_slip]
type = ADVectorFunctionDirichletBC
variable = vel
boundary = 'bottom right left top back'
[]
[T_cold]
type = DirichletBC
variable = T
boundary = 'back'
value = 300
[]
[radiation_flux]
type = FunctionRadiativeBC
variable = T
boundary = 'front'
emissivity_function = '1'
Tinfinity = 300
stefan_boltzmann_constant = ${sb}
use_displaced_mesh = true
[]
[weld_flux]
type = GaussianEnergyFluxBC
variable = T
boundary = 'front'
P0 = 159.96989792079225
R = 1.8257418583505537e-4
x_beam_coord = '2e-4 * cos(t * 2 * pi / ${period})'
y_beam_coord = '2e-4 * sin(t * 2 * pi / ${period})'
z_beam_coord = 0
use_displaced_mesh = true
[]
[vapor_recoil]
type = INSADVaporRecoilPressureMomentumFluxBC
variable = vel
boundary = 'front'
use_displaced_mesh = true
[]
[surface_tension]
type = INSADSurfaceTensionBC
variable = vel
boundary = 'front'
use_displaced_mesh = true
[]
[displace_x_top]
type = INSADDisplaceBoundaryBC
boundary = 'front'
variable = 'disp_x'
velocity = 'vel'
component = 0
associated_subdomain = 0
[]
[displace_y_top]
type = INSADDisplaceBoundaryBC
boundary = 'front'
variable = 'disp_y'
velocity = 'vel'
component = 1
associated_subdomain = 0
[]
[displace_z_top]
type = INSADDisplaceBoundaryBC
boundary = 'front'
variable = 'disp_z'
velocity = 'vel'
component = 2
associated_subdomain = 0
[]
[displace_x_top_dummy]
type = INSADDummyDisplaceBoundaryIntegratedBC
boundary = 'front'
variable = 'disp_x'
velocity = 'vel'
component = 0
[]
[displace_y_top_dummy]
type = INSADDummyDisplaceBoundaryIntegratedBC
boundary = 'front'
variable = 'disp_y'
velocity = 'vel'
component = 1
[]
[displace_z_top_dummy]
type = INSADDummyDisplaceBoundaryIntegratedBC
boundary = 'front'
variable = 'disp_z'
velocity = 'vel'
component = 2
[]
[]
[Materials]
[ins_mat]
type = INSADStabilized3Eqn
velocity = vel
pressure = p
temperature = T
use_displaced_mesh = true
[]
[steel]
type = AriaLaserWeld304LStainlessSteel
temperature = T
beta = 1e7
use_displaced_mesh = true
[]
[steel_boundary]
type = AriaLaserWeld304LStainlessSteelBoundary
boundary = 'front'
temperature = T
use_displaced_mesh = true
[]
[const]
type = GenericConstantMaterial
prop_names = 'abs sb_constant'
prop_values = '1 ${sb}'
use_displaced_mesh = true
[]
[]
[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
end_time = ${endtime}
dtmin = 1e-8
dtmax = ${timestep}
petsc_options = '-snes_converged_reason -ksp_converged_reason -options_left'
solve_type = 'NEWTON'
line_search = 'none'
nl_max_its = 12
l_max_its = 100
[TimeStepper]
type = IterationAdaptiveDT
optimal_iterations = 7
dt = ${timestep}
linear_iteration_ratio = 1e6
growth_factor = 1.5
[]
[]
[Outputs]
[exodus]
type = Exodus
output_material_properties = true
show_material_properties = 'mu'
[]
checkpoint = true
perf_graph = true
[]
[Debug]
show_var_residual_norms = true
[]
[Adaptivity]
marker = combo
max_h_level = 4
[Indicators]
[error_T]
type = GradientJumpIndicator
variable = T
[]
[error_dispz]
type = GradientJumpIndicator
variable = disp_z
[]
[]
[Markers]
[errorfrac_T]
type = ErrorFractionMarker
refine = 0.4
coarsen = 0.2
indicator = error_T
[]
[errorfrac_dispz]
type = ErrorFractionMarker
refine = 0.4
coarsen = 0.2
indicator = error_dispz
[]
[combo]
type = ComboMarker
markers = 'errorfrac_T errorfrac_dispz'
[]
[]
[]
[Postprocessors]
[num_dofs]
type = NumDOFs
system = 'NL'
[]
[nl]
type = NumNonlinearIterations
[]
[tot_nl]
type = CumulativeValuePostprocessor
postprocessor = 'nl'
[]
[]
(modules/navier_stokes/test/tests/finite_element/ins/boussinesq/boussinesq_stabilized.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmax = .05
ymax = .05
nx = 20
ny = 20
elem_type = QUAD9
[]
[./bottom_left]
type = ExtraNodesetGenerator
new_boundary = corner
coord = '0 0'
input = gen
[../]
[]
[Preconditioning]
[./Newton_SMP]
type = SMP
full = true
solve_type = 'NEWTON'
[../]
[]
[Executioner]
type = Steady
nl_rel_tol = 1e-12
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_shift_type -ksp_gmres_restart'
petsc_options_value = 'bjacobi lu NONZERO 200'
[]
[Debug]
show_var_residual_norms = true
[]
[Outputs]
[out]
type = Exodus
execute_on = 'final'
[]
[]
[Variables]
[velocity]
family = LAGRANGE_VEC
[]
[p][]
[temp]
initial_condition = 340
scaling = 1e-4
[]
[]
[ICs]
[velocity]
type = VectorConstantIC
x_value = 1e-15
y_value = 1e-15
variable = velocity
[]
[]
[BCs]
[./velocity_dirichlet]
type = VectorDirichletBC
boundary = 'left right bottom top'
variable = velocity
# The third entry is to satisfy RealVectorValue
values = '0 0 0'
[../]
# Even though we are integrating by parts, because there are no integrated
# boundary conditions on the velocity p doesn't appear in the system of
# equations. Thus we must pin the pressure somewhere in order to ensure a
# unique solution
[./p_zero]
type = DirichletBC
boundary = corner
variable = p
value = 0
[../]
[./cold]
type = DirichletBC
variable = temp
boundary = left
value = 300
[../]
[./hot]
type = DirichletBC
variable = temp
boundary = right
value = 400
[../]
[]
[Kernels]
[./mass]
type = INSADMass
variable = p
[../]
[mass_pspg]
type = INSADMassPSPG
variable = p
[]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[momentum_advection]
type = INSADMomentumAdvection
variable = velocity
[]
[momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
integrate_p_by_parts = true
[]
[./buoyancy]
type = INSADBoussinesqBodyForce
variable = velocity
temperature = temp
gravity = '0 -9.81 0'
[../]
[./gravity]
type = INSADGravityForce
variable = velocity
gravity = '0 -9.81 0'
[../]
[supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[]
[temp_advection]
type = INSADEnergyAdvection
variable = temp
[]
[temp_conduction]
type = ADHeatConduction
variable = temp
thermal_conductivity = 'k'
[../]
[temp_supg]
type = INSADEnergySUPG
variable = temp
velocity = velocity
[]
[]
[Materials]
[./ad_const]
type = ADGenericConstantMaterial
# alpha = coefficient of thermal expansion where rho = rho0 -alpha * rho0 * delta T
prop_names = 'mu rho alpha k cp'
prop_values = '30.74e-6 .5757 2.9e-3 46.38e-3 1054'
[../]
[./const]
type = GenericConstantMaterial
prop_names = 'temp_ref'
prop_values = '900'
[../]
[ins_mat]
type = INSADStabilized3Eqn
velocity = velocity
pressure = p
temperature = temp
[]
[]
(modules/navier_stokes/test/tests/finite_element/ins/lid_driven/mixed-transient-steady/mixed.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
nx = 16
ny = 16
[]
[./corner_node]
type = ExtraNodesetGenerator
new_boundary = 'pinned_node'
nodes = '0'
input = gen
[../]
[]
[Variables]
[./velocity]
family = LAGRANGE_VEC
[../]
[./p]
[../]
[temperature]
[InitialCondition]
type = ConstantIC
value = 1.0
[]
[]
[]
[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_convection]
type = INSADMomentumAdvection
variable = velocity
[../]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
integrate_p_by_parts = true
[../]
[./momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[../]
[./temperature_advection]
type = INSADEnergyAdvection
variable = temperature
[../]
[./temperature_conduction]
type = ADHeatConduction
variable = temperature
thermal_conductivity = 'k'
[../]
[temperature_supg]
type = INSADEnergySUPG
variable = temperature
velocity = velocity
[]
[]
[BCs]
[./no_slip]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom right left'
[../]
[./lid]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'top'
function_x = 'lid_function'
[../]
[./pressure_pin]
type = DirichletBC
variable = p
boundary = 'pinned_node'
value = 0
[../]
[./temperature_hot]
type = DirichletBC
variable = temperature
boundary = 'bottom'
value = 1
[../]
[./temperature_cold]
type = DirichletBC
variable = temperature
boundary = 'top'
value = 0
[../]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu cp k'
prop_values = '1 1 1 .01'
[../]
[ins_mat]
type = INSADStabilized3Eqn
velocity = velocity
pressure = p
temperature = temperature
[]
[]
[Functions]
[./lid_function]
# We pick a function that is exactly represented in the velocity
# space so that the Dirichlet conditions are the same regardless
# of the mesh spacing.
type = ParsedFunction
expression = '4*x*(1-x)'
[../]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
# Run for 100+ timesteps to reach steady state.
num_steps = 5
dt = .5
dtmin = .5
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_abs_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/lid_driven/ad_lid_driven_stabilized_with_temp_transient.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1.0
ymin = 0
ymax = 1.0
nx = 16
ny = 16
[]
[./corner_node]
type = ExtraNodesetGenerator
new_boundary = 'pinned_node'
nodes = '0'
input = gen
[../]
[]
[Variables]
[./velocity]
family = LAGRANGE_VEC
[../]
[./p]
[../]
[temperature]
[InitialCondition]
type = ConstantIC
value = 1.0
[]
[]
[]
[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_convection]
type = INSADMomentumAdvection
variable = velocity
[../]
[./momentum_viscous]
type = INSADMomentumViscous
variable = velocity
[../]
[./momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = p
integrate_p_by_parts = true
[../]
[./momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
[../]
[./temperature_advection]
type = INSADEnergyAdvection
variable = temperature
[../]
[temperature_time]
type = INSADHeatConductionTimeDerivative
variable = temperature
[]
[./temperature_conduction]
type = ADHeatConduction
variable = temperature
thermal_conductivity = 'k'
[../]
[temperature_supg]
type = INSADEnergySUPG
variable = temperature
velocity = velocity
[]
[]
[BCs]
[./no_slip]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'bottom right left'
[../]
[./lid]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'top'
function_x = 'lid_function'
[../]
[./pressure_pin]
type = DirichletBC
variable = p
boundary = 'pinned_node'
value = 0
[../]
[./temperature_hot]
type = DirichletBC
variable = temperature
boundary = 'bottom'
value = 1
[../]
[./temperature_cold]
type = DirichletBC
variable = temperature
boundary = 'top'
value = 0
[../]
[]
[Materials]
[./const]
type = ADGenericConstantMaterial
prop_names = 'rho mu cp k'
prop_values = '1 1 1 .01'
[../]
[ins_mat]
type = INSADStabilized3Eqn
velocity = velocity
pressure = p
temperature = temperature
[]
[]
[Functions]
[./lid_function]
# We pick a function that is exactly represented in the velocity
# space so that the Dirichlet conditions are the same regardless
# of the mesh spacing.
type = ParsedFunction
expression = '4*x*(1-x)'
[../]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
# Run for 100+ timesteps to reach steady state.
num_steps = 5
dt = .5
dtmin = .5
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_abs_tol = 1e-12
nl_max_its = 6
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_element/ins/energy-conservation/q1q1.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
nx = 10
ny = 10
dim = 2
[]
[subdomain]
type = SubdomainBoundingBoxGenerator
bottom_left = '0.5 0 0'
top_right = '1 1 0'
block_id = 1
input = gen
[]
[break_boundary]
input = subdomain
type = BreakBoundaryOnSubdomainGenerator
boundaries = 'bottom top'
[]
[sideset]
type = SideSetsBetweenSubdomainsGenerator
input = break_boundary
primary_block = '1'
paired_block = '0'
new_boundary = 'fluid_left'
[]
coord_type = RZ
[]
[Variables]
[T][]
[velocity]
family = LAGRANGE_VEC
block = 1
[]
[pressure]
block = 1
[]
[]
[Kernels]
[mass]
type = INSADMass
variable = pressure
block = 1
[]
[pspg]
type = INSADMassPSPG
variable = pressure
block = 1
[]
[momentum_convection]
type = INSADMomentumAdvection
variable = velocity
block = 1
[]
[momentum_viscous]
type = INSADMomentumViscous
variable = velocity
block = 1
[]
[momentum_pressure]
type = INSADMomentumPressure
variable = velocity
pressure = pressure
integrate_p_by_parts = true
block = 1
[]
[momentum_supg]
type = INSADMomentumSUPG
variable = velocity
velocity = velocity
block = 1
[]
[temperature_advection]
type = INSADEnergyAdvection
variable = T
block = 1
[]
[temperature_supg]
type = INSADEnergySUPG
variable = T
velocity = velocity
block = 1
[]
[temperature_conduction]
type = ADHeatConduction
variable = T
thermal_conductivity = 'k'
[]
[heat_source]
type = BodyForce
variable = T
block = 0
function = 'x + y'
[]
[]
[BCs]
[velocity_inlet]
type = VectorFunctionDirichletBC
variable = velocity
function_y = 1
boundary = 'bottom_to_1'
[]
[wall]
type = VectorFunctionDirichletBC
variable = velocity
boundary = 'fluid_left right'
[]
[convective_heat_transfer]
type = ConvectiveHeatFluxBC
variable = T
T_infinity = 0
heat_transfer_coefficient = 1
boundary = 'right'
[]
[]
[Materials]
[constant]
type = ADGenericConstantMaterial
prop_names = 'cp rho k mu'
prop_values = '1 1 1 1'
[]
[ins]
type = INSADStabilized3Eqn
pressure = pressure
velocity = velocity
temperature = T
block = 1
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
[]
[Outputs]
csv = true
[]
[Postprocessors]
[convective_heat_transfer]
type = ConvectiveHeatTransferSideIntegral
T_solid = T
T_fluid = 0
htc = 1
boundary = 'right'
[]
[advection]
type = INSADElementIntegralEnergyAdvection
temperature = T
velocity = velocity
cp = cp
rho = rho
block = 1
[]
[source]
type = FunctionElementIntegral
function = 'x + y'
block = 0
[]
[energy_balance]
type = ParsedPostprocessor
expression = 'convective_heat_transfer + advection - source'
pp_names = 'convective_heat_transfer advection source'
[]
[]