- muThe viscosity
C++ Type:MaterialPropertyName
Description:The viscosity
- pressureThe pressure variable.
C++ Type:std::vector<VariableName>
Description:The pressure variable.
- rhoThe value for the density
C++ Type:double
Description:The value for the density
- uThe velocity in the x direction.
C++ Type:std::vector<VariableName>
Description:The velocity in the x direction.
- variableThe name of the finite volume variable this kernel applies to
C++ Type:NonlinearVariableName
Description:The name of the finite volume variable this kernel applies to
- veladvection velocity
C++ Type:MaterialPropertyName
Description:advection velocity
INSFVMomentumAdvection
This object implements the component terms of the incompressible Navier Stokes momentum equation. An average or Rhie-Chow interpolation can be used for the advecting velocity interpolation. An average or upwind interpolation can be used for the advected quantity, which in this case is the momentum component where denotes the x, y, or z component of the velocity in Cartesian coordinates, or the r or z component of the velocity in RZ coordinates.
Input Parameters
- advected_interp_methodupwindThe interpolation to use for the advected quantity. Options are 'upwind' and 'average', with the default being 'upwind'.
Default:upwind
C++ Type:MooseEnum
Options:average, upwind
Description:The interpolation to use for the advected quantity. Options are 'upwind' and 'average', with the default being 'upwind'.
- advected_quantityAn optional parameter for specifying an advected quantity from a material property. If this is not specified, then the advected quantity will simply be the variable that this object is acting on
C++ Type:MaterialPropertyName
Options:
Description:An optional parameter for specifying an advected quantity from a material property. If this is not specified, then the advected quantity will simply be the variable that this object is acting on
- blockThe list of block ids (SubdomainID) that this object will be applied
C++ Type:std::vector<SubdomainName>
Options:
Description:The list of block ids (SubdomainID) that this object will be applied
- boundaries_to_forceThe set of boundaries to force execution of this FVFluxKernel on.
C++ Type:std::vector<BoundaryName>
Options:
Description:The set of boundaries to force execution of this FVFluxKernel on.
- boundaries_to_not_forceThe set of boundaries to not force execution of this FVFluxKernel on.
C++ Type:std::vector<BoundaryName>
Options:
Description:The set of boundaries to not force execution of this FVFluxKernel on.
- force_boundary_executionFalseWhether to force execution of this object on the boundary.
Default:False
C++ Type:bool
Options:
Description:Whether to force execution of this object on the boundary.
- ghost_layers2The number of layers of elements to ghost.
Default:2
C++ Type:unsigned short
Options:
Description:The number of layers of elements to ghost.
- use_point_neighborsFalseWhether to use point neighbors, which introduces additional ghosting to that used for simple face neighbors.
Default:False
C++ Type:bool
Options:
Description:Whether to use point neighbors, which introduces additional ghosting to that used for simple face neighbors.
- vThe velocity in the y direction.
C++ Type:std::vector<VariableName>
Options:
Description:The velocity in the y direction.
- velocity_interp_methodrcThe interpolation to use for the velocity. Options are 'average' and 'rc' which stands for Rhie-Chow. The default is Rhie-Chow.
Default:rc
C++ Type:MooseEnum
Options:average, rc
Description:The interpolation to use for the velocity. Options are 'average' and 'rc' which stands for Rhie-Chow. The default is Rhie-Chow.
- wThe velocity in the z direction.
C++ Type:std::vector<VariableName>
Options:
Description:The velocity in the z direction.
Optional Parameters
- control_tagsAdds user-defined labels for accessing object parameters via control logic.
C++ Type:std::vector<std::string>
Options:
Description:Adds user-defined labels for accessing object parameters via control logic.
- enableTrueSet the enabled status of the MooseObject.
Default:True
C++ Type:bool
Options:
Description:Set the enabled status of the MooseObject.
- implicitTrueDetermines whether this object is calculated using an implicit or explicit form
Default:True
C++ Type:bool
Options:
Description:Determines whether this object is calculated using an implicit or explicit form
- 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
Options:
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
- extra_matrix_tagsThe extra tags for the matrices this Kernel should fill
C++ Type:std::vector<TagName>
Options:
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>
Options:
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
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
Description:The tag for the vectors this Kernel should fill
Tagging Parameters
Input Files
- (modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/2d-average.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/1d-rc.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/block_restriction/2d-rc.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-rc-friction.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/boussinesq/boussinesq.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/lid-driven/lid-driven-with-energy.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/lid-driven/transient-lid-driven-with-energy.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/cylindrical/diverging.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/2d-average-with-temp.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/2d-rc.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/cylindrical/2d-rc-slip.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-scalar-transport.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/1d-average.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-mixing-length.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/mms/rc.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/3d-rc-no-slip.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/cylindrical/2d-average.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-rc-no-slip-extrapolated-outlet-pressure.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/lid-driven/lid-driven.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-rc-no-slip.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/plane-poiseuille-flow.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/cylindrical/2d-average-no-slip.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/rotated/rotated-pp-flow.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/cylindrical/2d-average-with-temp.i)
- (modules/navier_stokes/test/tests/postprocessors/conservation_INSFV.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-rc-ambient-convection.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/3d-rc.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-rc-no-slip-outflow-bcs.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/cylindrical/2d-rc.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-rc.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/mms/cylindrical/2d-rc.i)
- (modules/navier_stokes/examples/pipe_mixing_length/pipe_mixing_length.i)
Child Objects
(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/2d-average.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='average'
force_boundary_execution=true
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 2
ymin = -1
ymax = 1
nx = 2
ny = 2
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
two_term_boundary_expansion = false
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
two_term_boundary_expansion = false
[]
[pressure]
type = INSFVPressureVariable
two_term_boundary_expansion = false
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
vel = 'velocity'
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[u_forcing]
type = FVBodyForce
variable = u
function = forcing_u
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_quantity = 'rhov'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[v_viscosity]
type = FVDiffusion
variable = v
coeff = ${mu}
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
p = pressure
[]
[v_forcing]
type = FVBodyForce
variable = v
function = forcing_v
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = 'exact_u'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = 'exact_v'
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = u
function = 'exact_u'
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = v
function = 'exact_v'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 'exact_p'
[]
[]
[Materials]
[ins_fv]
type = INSFVMaterial
u = 'u'
v = 'v'
pressure = 'pressure'
rho = ${rho}
[]
[]
[Functions]
[exact_u]
type = ParsedFunction
value = 'sin((1/2)*y*pi)*cos((1/2)*x*pi)'
[]
[exact_rhou]
type = ParsedFunction
value = 'rho*sin((1/2)*y*pi)*cos((1/2)*x*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_u]
type = ParsedFunction
value = '(1/2)*pi^2*mu*sin((1/2)*y*pi)*cos((1/2)*x*pi) - 1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi) + (1/2)*pi*rho*sin((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)^2 - pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi) - 1/4*pi*sin((1/4)*x*pi)*sin((3/2)*y*pi)'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_v]
type = ParsedFunction
value = 'sin((1/4)*x*pi)*cos((1/2)*y*pi)'
[]
[exact_rhov]
type = ParsedFunction
value = 'rho*sin((1/4)*x*pi)*cos((1/2)*y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_v]
type = ParsedFunction
value = '(5/16)*pi^2*mu*sin((1/4)*x*pi)*cos((1/2)*y*pi) - pi*rho*sin((1/4)*x*pi)^2*sin((1/2)*y*pi)*cos((1/2)*y*pi) - 1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*y*pi) + (1/4)*pi*rho*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi) + (3/2)*pi*cos((1/4)*x*pi)*cos((3/2)*y*pi)'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_p]
type = ParsedFunction
value = 'sin((3/2)*y*pi)*cos((1/4)*x*pi)'
[]
[forcing_p]
type = ParsedFunction
value = '-1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi) - 1/2*pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[./L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2v]
type = ElementL2Error
variable = v
function = exact_v
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2p]
variable = pressure
function = exact_p
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/1d-rc.i)
mu=1.1
rho=1.1
advected_interp_method='upwind'
velocity_interp_method='rc'
[Mesh]
[mesh]
type = CartesianMeshGenerator
dim = 1
dx = '1 1'
ix = '30 30'
subdomain_id = '1 2'
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
vel = 'velocity'
pressure = pressure
u = u
mu = ${mu}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
mu = ${mu}
rho = ${rho}
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = '1'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 1
[]
[]
[Materials]
[ins_fv]
type = INSFVMaterial
u = 'u'
pressure = 'pressure'
rho = ${rho}
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Postprocessors]
[inlet_p]
type = SideAverageValue
variable = 'pressure'
boundary = 'left'
[]
[outlet-u]
type = SideIntegralVariablePostprocessor
variable = u
boundary = 'right'
[]
[]
[Outputs]
exodus = true
csv = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/block_restriction/2d-rc.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'
restricted_blocks = '1'
[GlobalParams]
two_term_boundary_expansion = true
[]
[Mesh]
parallel_type = 'replicated'
[mesh]
type = CartesianMeshGenerator
dim = 2
dx = '1 1'
dy = '1'
ix = '7 7'
iy = 10
subdomain_id = '1 2'
[]
[mid]
type = SideSetsBetweenSubdomainsGenerator
primary_block = 1
paired_block = 2
input = mesh
new_boundary = 'middle'
[]
[break_top]
type = PatchSidesetGenerator
boundary = 'top'
n_patches = 2
input = mid
[]
[break_bottom]
type = PatchSidesetGenerator
boundary = 'bottom'
n_patches = 2
input = break_top
[]
[]
[Problem]
kernel_coverage_check = false
fv_bcs_integrity_check = true
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
block = ${restricted_blocks}
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
block = ${restricted_blocks}
[]
[pressure]
type = INSFVPressureVariable
block = ${restricted_blocks}
[]
[temperature]
type = INSFVEnergyVariable
block = ${restricted_blocks}
[]
[scalar]
type = INSFVScalarFieldVariable
block = ${restricted_blocks}
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
vel = 'velocity'
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_quantity = 'rhov'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[v_viscosity]
type = FVDiffusion
variable = v
coeff = ${mu}
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
p = pressure
[]
[energy_advection]
type = INSFVEnergyAdvection
variable = temperature
vel = 'velocity'
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[energy_diffusion]
type = FVDiffusion
coeff = 1.1
variable = temperature
[]
[energy_loss]
type = FVBodyForce
variable = temperature
value = -0.1
[]
[scalar_advection]
type = INSFVScalarFieldAdvection
variable = scalar
vel = 'velocity'
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[scalar_diffusion]
type = FVDiffusion
coeff = 1
variable = scalar
[]
[scalar_src]
type = FVBodyForce
variable = scalar
value = 0.1
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = 0
[]
[top-wall-u]
type = INSFVNoSlipWallBC
boundary = 'top_0'
variable = u
function = 0
[]
[top-wall-v]
type = INSFVNoSlipWallBC
boundary = 'top_0'
variable = v
function = 0
[]
[bottom-wall-u]
type = INSFVSymmetryVelocityBC
boundary = 'bottom_0'
variable = u
mu = ${mu}
u = u
v = v
momentum_component = 'x'
[]
[bottom-wall-v]
type = INSFVSymmetryVelocityBC
boundary = 'bottom_0'
variable = v
mu = ${mu}
u = u
v = v
momentum_component = 'y'
[]
[bottom-wall-p]
type = INSFVSymmetryPressureBC
boundary = 'bottom_0'
variable = pressure
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'middle'
variable = pressure
function = 0
[]
[inlet_t]
type = FVDirichletBC
boundary = 'left'
variable = temperature
value = 1
[]
[outlet_scalar]
type = FVDirichletBC
boundary = 'middle'
variable = scalar
value = 1
[]
[]
[Materials]
[ins_fv]
type = INSFVMaterial
u = 'u'
v = 'v'
pressure = 'pressure'
temperature = 'temperature'
rho = ${rho}
block = ${restricted_blocks}
[]
[const]
type = ADGenericConstantMaterial
prop_names = 'cp'
prop_values = '2'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-rc-friction.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'
[GlobalParams]
two_term_boundary_expansion = true
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 5
ymin = -1
ymax = 1
nx = 50
ny = 10
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[FVKernels]
inactive='u_friction_quad v_friction_quad'
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
vel = 'velocity'
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[u_friction_linear]
type = NSFVMomentumFriction
variable = u
linear_coef_name = friction_coefficient
[]
[u_friction_quad]
type = NSFVMomentumFriction
variable = u
quadratic_coef_name = friction_coefficient
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_quantity = 'rhov'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[v_viscosity]
type = FVDiffusion
variable = v
coeff = ${mu}
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
p = pressure
[]
[v_friction_linear]
type = NSFVMomentumFriction
variable = v
linear_coef_name = friction_coefficient
[]
[v_friction_quad]
type = NSFVMomentumFriction
variable = v
quadratic_coef_name = friction_coefficient
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = '0'
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = u
function = 0
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = v
function = 0
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = '0'
[]
[]
[Materials]
[ins_fv]
type = INSFVMaterial
u = 'u'
v = 'v'
pressure = 'pressure'
rho = ${rho}
[]
[friction_coefficient]
type = ADGenericConstantMaterial
prop_names = 'friction_coefficient'
prop_values = '25'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 200 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/boussinesq/boussinesq.i)
mu = 1
rho = 1
k = 1
cp = 1
alpha = 1
vel = 'velocity'
velocity_interp_method = 'rc'
advected_interp_method = 'upwind'
rayleigh=1e3
hot_temp=${rayleigh}
temp_ref=${fparse hot_temp / 2.}
[GlobalParams]
two_term_boundary_expansion = true
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 32
ny = 32
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
[]
[v]
type = INSFVVelocityVariable
[]
[pressure]
type = INSFVPressureVariable
[]
[T]
type = INSFVEnergyVariable
scaling = 1e-4
[]
[lambda]
family = SCALAR
order = FIRST
[]
[]
[AuxVariables]
[U]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[vel_x]
order = FIRST
family = MONOMIAL
[]
[vel_y]
order = FIRST
family = MONOMIAL
[]
[viz_T]
order = FIRST
family = MONOMIAL
[]
[]
[AuxKernels]
[mag]
type = VectorMagnitudeAux
variable = U
x = u
y = v
execute_on = 'initial timestep_end'
[]
[vel_x]
type = ParsedAux
variable = vel_x
function = 'u'
execute_on = 'initial timestep_end'
args = 'u'
[]
[vel_y]
type = ParsedAux
variable = vel_y
function = 'v'
execute_on = 'initial timestep_end'
args = 'v'
[]
[viz_T]
type = ParsedAux
variable = viz_T
function = 'T'
execute_on = 'initial timestep_end'
args = 'T'
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
vel = ${vel}
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
u = u
v = v
pressure = pressure
mu = ${mu}
rho = ${rho}
[]
[mean_zero_pressure]
type = FVScalarLagrangeMultiplier
variable = pressure
lambda = lambda
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
vel = ${vel}
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[u_buoyancy]
type = INSFVMomentumBoussinesq
variable = u
temperature = T
gravity = '0 -1 0'
rho = ${rho}
ref_temperature = ${temp_ref}
momentum_component = 'x'
[]
[u_gravity]
type = INSFVMomentumGravity
variable = u
gravity = '0 -1 0'
rho = ${rho}
momentum_component = 'x'
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_quantity = 'rhov'
vel = ${vel}
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[v_viscosity]
type = FVDiffusion
variable = v
coeff = ${mu}
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
p = pressure
[]
[v_buoyancy]
type = INSFVMomentumBoussinesq
variable = v
temperature = T
gravity = '0 -1 0'
rho = ${rho}
ref_temperature = ${temp_ref}
momentum_component = 'y'
[]
[v_gravity]
type = INSFVMomentumGravity
variable = v
gravity = '0 -1 0'
rho = ${rho}
momentum_component = 'y'
[]
[temp_conduction]
type = FVDiffusion
coeff = 'k'
variable = T
[]
[temp_advection]
type = INSFVEnergyAdvection
variable = T
vel = ${vel}
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[]
[FVBCs]
[top_x]
type = INSFVNoSlipWallBC
variable = u
boundary = 'top'
function = 'lid_function'
[]
[no_slip_x]
type = INSFVNoSlipWallBC
variable = u
boundary = 'left right bottom'
function = 0
[]
[no_slip_y]
type = INSFVNoSlipWallBC
variable = v
boundary = 'left right top bottom'
function = 0
[]
[T_hot]
type = FVDirichletBC
variable = T
boundary = left
value = ${hot_temp}
[]
[T_cold]
type = FVDirichletBC
variable = T
boundary = right
value = 0
[]
[]
[Materials]
[const]
type = ADGenericConstantMaterial
prop_names = 'k cp alpha'
prop_values = '${k} ${cp} ${alpha}'
[]
[ins_fv]
type = INSFVMaterial
u = 'u'
v = 'v'
pressure = 'pressure'
temperature = 'T'
rho = ${rho}
[]
[]
[Functions]
[lid_function]
type = ParsedFunction
value = '4*x*(1-x)'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 300 lu NONZERO'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/lid-driven/lid-driven-with-energy.i)
mu = 1
rho = 1
k = .01
cp = 1
vel = 'velocity'
velocity_interp_method = 'rc'
advected_interp_method = 'average'
[GlobalParams]
two_term_boundary_expansion = true
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 32
ny = 32
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
[]
[v]
type = INSFVVelocityVariable
[]
[pressure]
type = INSFVPressureVariable
[]
[T]
type = INSFVEnergyVariable
[]
[lambda]
family = SCALAR
order = FIRST
[]
[]
[AuxVariables]
[U]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[]
[AuxKernels]
[mag]
type = VectorMagnitudeAux
variable = U
x = u
y = v
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
vel = ${vel}
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
u = u
v = v
pressure = pressure
mu = ${mu}
rho = ${rho}
[]
[mean_zero_pressure]
type = FVScalarLagrangeMultiplier
variable = pressure
lambda = lambda
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
vel = ${vel}
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_quantity = 'rhov'
vel = ${vel}
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[v_viscosity]
type = FVDiffusion
variable = v
coeff = ${mu}
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
p = pressure
[]
[temp-condution]
type = FVDiffusion
coeff = 'k'
variable = T
[]
[temp_advection]
type = INSFVEnergyAdvection
variable = T
vel = ${vel}
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[]
[FVBCs]
[top_x]
type = INSFVNoSlipWallBC
variable = u
boundary = 'top'
function = 'lid_function'
[]
[no_slip_x]
type = INSFVNoSlipWallBC
variable = u
boundary = 'left right bottom'
function = 0
[]
[no_slip_y]
type = INSFVNoSlipWallBC
variable = v
boundary = 'left right top bottom'
function = 0
[]
[T_hot]
type = FVDirichletBC
variable = T
boundary = 'bottom'
value = 1
[]
[T_cold]
type = FVDirichletBC
variable = T
boundary = 'top'
value = 0
[]
[]
[Materials]
[const]
type = ADGenericConstantMaterial
prop_names = 'k cp'
prop_values = '${k} ${cp}'
[]
[ins_fv]
type = INSFVMaterial
u = 'u'
v = 'v'
pressure = 'pressure'
temperature = 'T'
rho = ${rho}
[]
[]
[Functions]
[lid_function]
type = ParsedFunction
value = '4*x*(1-x)'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 300 lu NONZERO'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/lid-driven/transient-lid-driven-with-energy.i)
mu = 1
rho = 1
k = .01
cp = 1
vel = 'velocity'
velocity_interp_method = 'rc'
advected_interp_method = 'average'
[GlobalParams]
two_term_boundary_expansion = true
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 32
ny = 32
[]
[pin]
type = ExtraNodesetGenerator
input = gen
new_boundary = 'pin'
nodes = '0'
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
[]
[v]
type = INSFVVelocityVariable
[]
[pressure]
type = INSFVPressureVariable
[]
[T]
type = INSFVEnergyVariable
[]
[lambda]
family = SCALAR
order = FIRST
[]
[]
[ICs]
[T]
type = ConstantIC
variable = T
value = 1
[]
[]
[AuxVariables]
[U]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[]
[AuxKernels]
[mag]
type = VectorMagnitudeAux
variable = U
x = u
y = v
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
vel = ${vel}
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
u = u
v = v
pressure = pressure
mu = ${mu}
rho = ${rho}
[]
[mean_zero_pressure]
type = FVScalarLagrangeMultiplier
variable = pressure
lambda = lambda
[]
[u_time]
type = INSFVMomentumTimeDerivative
variable = 'u'
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
vel = ${vel}
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[v_time]
type = INSFVMomentumTimeDerivative
variable = v
rho = ${rho}
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_quantity = 'rhov'
vel = ${vel}
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[v_viscosity]
type = FVDiffusion
variable = v
coeff = ${mu}
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
p = pressure
[]
[temp_time]
type = INSFVEnergyTimeDerivative
variable = T
rho = ${rho}
[]
[temp_conduction]
type = FVDiffusion
coeff = 'k'
variable = T
[]
[temp_advection]
type = INSFVEnergyAdvection
variable = T
vel = ${vel}
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[]
[FVBCs]
[top_x]
type = INSFVNoSlipWallBC
variable = u
boundary = 'top'
function = 'lid_function'
[]
[no_slip_x]
type = INSFVNoSlipWallBC
variable = u
boundary = 'left right bottom'
function = 0
[]
[no_slip_y]
type = INSFVNoSlipWallBC
variable = v
boundary = 'left right top bottom'
function = 0
[]
[T_hot]
type = FVDirichletBC
variable = T
boundary = 'bottom'
value = 1
[]
[T_cold]
type = FVDirichletBC
variable = T
boundary = 'top'
value = 0
[]
[]
[Materials]
[const]
type = ADGenericConstantMaterial
prop_names = 'k cp'
prop_values = '${k} ${cp}'
[]
[ins_fv]
type = INSFVMaterial
u = 'u'
v = 'v'
pressure = 'pressure'
temperature = 'T'
rho = ${rho}
[]
[]
[Functions]
[lid_function]
type = ParsedFunction
value = '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_type -sub_pc_factor_shift_type -ksp_gmres_restart'
petsc_options_value = 'asm lu NONZERO 200'
line_search = 'none'
nl_rel_tol = 1e-12
nl_max_its = 6
l_max_its = 200
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/cylindrical/diverging.i)
mu=1
rho=1
advected_interp_method='average'
velocity_interp_method='rc'
[GlobalParams]
two_term_boundary_expansion = true
[]
[Mesh]
file = diverging.msh
uniform_refine = 2
[]
[Problem]
fv_bcs_integrity_check = true
coord_type = 'RZ'
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1e-15
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1e-15
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
vel = 'velocity'
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_quantity = 'rhov'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
# we can think of the axis as a slip wall boundary, no normal velocity and no viscous shear
[]
[v_viscosity]
type = FVDiffusion
variable = v
coeff = ${mu}
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
p = pressure
[]
[]
[FVBCs]
active = 'inlet-u inlet-v free-slip-wall-u free-slip-wall-v outlet-p axis-u axis-v'
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = u
function = 0
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = v
function = 1
[]
[free-slip-wall-u]
type = INSFVNaturalFreeSlipBC
boundary = 'right'
variable = u
[]
[free-slip-wall-v]
type = INSFVNaturalFreeSlipBC
boundary = 'right'
variable = v
[]
[no-slip-wall-u]
type = INSFVNoSlipWallBC
boundary = 'right'
variable = u
function = 0
[]
[no-slip-wall-v]
type = INSFVNoSlipWallBC
boundary = 'right'
variable = v
function = 0
[]
[outlet-p]
type = INSFVOutletPressureBC
boundary = 'top'
variable = pressure
function = 0
[]
[axis-u]
type = INSFVSymmetryVelocityBC
boundary = 'left'
variable = u
u = u
v = v
mu = ${mu}
momentum_component = x
[]
[axis-v]
type = INSFVSymmetryVelocityBC
boundary = 'left'
variable = v
u = u
v = v
mu = ${mu}
momentum_component = y
[]
[axis-p]
type = INSFVSymmetryPressureBC
boundary = 'left'
variable = pressure
[]
[]
[Materials]
[ins_fv]
type = INSFVMaterial
u = 'u'
v = 'v'
pressure = 'pressure'
rho = ${rho}
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options = '-options_left'
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_shift_type -ksp_gmres_restart'
petsc_options_value = 'asm lu NONZERO 200'
line_search = 'none'
[]
[Debug]
show_var_residual_norms = true
[]
[Postprocessors]
[in]
type = SideIntegralVariablePostprocessor
variable = v
boundary = 'bottom'
[]
[out]
type = SideIntegralVariablePostprocessor
variable = v
boundary = 'top'
[]
[num_lin]
type = NumLinearIterations
outputs = 'console'
[]
[num_nl]
type = NumNonlinearIterations
outputs = 'console'
[]
[cum_lin]
type = CumulativeValuePostprocessor
outputs = 'console'
postprocessor = 'num_lin'
[]
[cum_nl]
type = CumulativeValuePostprocessor
outputs = 'console'
postprocessor = 'num_nl'
[]
[]
[Outputs]
exodus = true
csv = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/2d-average-with-temp.i)
mu=1.1
rho=1.1
k=1.1
cp=1.1
advected_interp_method='average'
velocity_interp_method='average'
velocity='velocity'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 2
ymin = -1
ymax = 1
nx = 2
ny = 2
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
two_term_boundary_expansion = false
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
two_term_boundary_expansion = false
[]
[pressure]
type = INSFVPressureVariable
two_term_boundary_expansion = false
[]
[temperature]
type = INSFVEnergyVariable
two_term_boundary_expansion = false
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
vel = ${velocity}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
vel = ${velocity}
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[u_forcing]
type = FVBodyForce
variable = u
function = forcing_u
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_quantity = 'rhov'
vel = ${velocity}
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[v_viscosity]
type = FVDiffusion
variable = v
coeff = ${mu}
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
p = pressure
[]
[v_forcing]
type = FVBodyForce
variable = v
function = forcing_v
[]
[temp_conduction]
type = FVDiffusion
coeff = 'k'
variable = temperature
[]
[temp_advection]
type = INSFVEnergyAdvection
vel = ${velocity}
variable = temperature
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[temp_forcing]
type = FVBodyForce
variable = temperature
function = forcing_t
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = 'exact_u'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = 'exact_v'
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = u
function = 'exact_u'
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = v
function = 'exact_v'
[]
[inlet-and-walls-t]
type = FVFunctionDirichletBC
boundary = 'left top bottom'
variable = temperature
function = 'exact_t'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 'exact_p'
[]
[]
[Materials]
[const]
type = ADGenericConstantMaterial
prop_names = 'k cp'
prop_values = '${k} ${cp}'
[]
[ins_fv]
type = INSFVMaterial
u = 'u'
v = 'v'
pressure = 'pressure'
temperature = 'temperature'
rho = ${rho}
[]
[]
[Functions]
[exact_u]
type = ParsedFunction
value = 'sin((1/2)*y*pi)*cos((1/2)*x*pi)'
[]
[exact_rhou]
type = ParsedFunction
value = 'rho*sin((1/2)*y*pi)*cos((1/2)*x*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_u]
type = ParsedFunction
value = '(1/2)*pi^2*mu*sin((1/2)*y*pi)*cos((1/2)*x*pi) - 1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi) + (1/2)*pi*rho*sin((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)^2 - pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi) - 1/4*pi*sin((1/4)*x*pi)*sin((3/2)*y*pi)'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_v]
type = ParsedFunction
value = 'sin((1/4)*x*pi)*cos((1/2)*y*pi)'
[]
[exact_rhov]
type = ParsedFunction
value = 'rho*sin((1/4)*x*pi)*cos((1/2)*y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_v]
type = ParsedFunction
value = '(5/16)*pi^2*mu*sin((1/4)*x*pi)*cos((1/2)*y*pi) - pi*rho*sin((1/4)*x*pi)^2*sin((1/2)*y*pi)*cos((1/2)*y*pi) - 1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*y*pi) + (1/4)*pi*rho*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi) + (3/2)*pi*cos((1/4)*x*pi)*cos((3/2)*y*pi)'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_p]
type = ParsedFunction
value = 'sin((3/2)*y*pi)*cos((1/4)*x*pi)'
[]
[forcing_p]
type = ParsedFunction
value = '-1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi) - 1/2*pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[exact_t]
type = ParsedFunction
value = 'sin((1/4)*x*pi)*cos((1/2)*y*pi)'
[]
[forcing_t]
type = ParsedFunction
value = '-pi*cp*rho*sin((1/4)*x*pi)^2*sin((1/2)*y*pi)*cos((1/2)*y*pi) - 1/2*pi*cp*rho*sin((1/4)*x*pi)*sin((1/2)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*y*pi) + (1/4)*pi*cp*rho*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi) + (5/16)*pi^2*k*sin((1/4)*x*pi)*cos((1/2)*y*pi)'
vars = 'k rho cp'
vals = '${k} ${rho} ${cp}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[./L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2v]
type = ElementL2Error
variable = v
function = exact_v
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2p]
variable = pressure
function = exact_p
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2t]
variable = temperature
function = exact_t
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/2d-rc.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 2
ymin = -1
ymax = 1
nx = 2
ny = 2
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
vel = 'velocity'
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[u_forcing]
type = FVBodyForce
variable = u
function = forcing_u
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_quantity = 'rhov'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[v_viscosity]
type = FVDiffusion
variable = v
coeff = ${mu}
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
p = pressure
[]
[v_forcing]
type = FVBodyForce
variable = v
function = forcing_v
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = 'exact_u'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = 'exact_v'
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = u
function = 'exact_u'
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = v
function = 'exact_v'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 'exact_p'
[]
[]
[Materials]
[ins_fv]
type = INSFVMaterial
u = 'u'
v = 'v'
pressure = 'pressure'
rho = ${rho}
[]
[]
[Functions]
[exact_u]
type = ParsedFunction
value = 'sin((1/2)*y*pi)*cos((1/2)*x*pi)'
[]
[exact_rhou]
type = ParsedFunction
value = 'rho*sin((1/2)*y*pi)*cos((1/2)*x*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_u]
type = ParsedFunction
value = '(1/2)*pi^2*mu*sin((1/2)*y*pi)*cos((1/2)*x*pi) - 1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi) + (1/2)*pi*rho*sin((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)^2 - pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi) - 1/4*pi*sin((1/4)*x*pi)*sin((3/2)*y*pi)'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_v]
type = ParsedFunction
value = 'sin((1/4)*x*pi)*cos((1/2)*y*pi)'
[]
[exact_rhov]
type = ParsedFunction
value = 'rho*sin((1/4)*x*pi)*cos((1/2)*y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_v]
type = ParsedFunction
value = '(5/16)*pi^2*mu*sin((1/4)*x*pi)*cos((1/2)*y*pi) - pi*rho*sin((1/4)*x*pi)^2*sin((1/2)*y*pi)*cos((1/2)*y*pi) - 1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*y*pi) + (1/4)*pi*rho*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi) + (3/2)*pi*cos((1/4)*x*pi)*cos((3/2)*y*pi)'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_p]
type = ParsedFunction
value = 'sin((3/2)*y*pi)*cos((1/4)*x*pi)'
[]
[forcing_p]
type = ParsedFunction
value = '-1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi) - 1/2*pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[./L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2v]
type = ElementL2Error
variable = v
function = exact_v
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2p]
type = ElementL2Error
variable = pressure
function = exact_p
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/cylindrical/2d-rc-slip.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 2
ymin = 0
ymax = 10
nx = 10
ny = 50
[]
[]
[Problem]
fv_bcs_integrity_check = true
coord_type = 'RZ'
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
vel = 'velocity'
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_quantity = 'rhov'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[v_viscosity]
type = FVDiffusion
variable = v
coeff = ${mu}
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
p = pressure
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = u
function = 0
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = v
function = 1
[]
[free-slip-wall-u]
type = INSFVNaturalFreeSlipBC
boundary = 'right'
variable = u
[]
[free-slip-wall-v]
type = INSFVNaturalFreeSlipBC
boundary = 'right'
variable = v
[]
[outlet-p]
type = INSFVOutletPressureBC
boundary = 'top'
variable = pressure
function = 0
[]
[axis-u]
type = INSFVSymmetryVelocityBC
boundary = 'left'
variable = u
u = u
v = v
mu = ${mu}
momentum_component = x
[]
[axis-v]
type = INSFVSymmetryVelocityBC
boundary = 'left'
variable = v
u = u
v = v
mu = ${mu}
momentum_component = y
[]
[axis-p]
type = INSFVSymmetryPressureBC
boundary = 'left'
variable = pressure
[]
[]
[Materials]
[ins_fv]
type = INSFVMaterial
u = 'u'
v = 'v'
pressure = 'pressure'
rho = ${rho}
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
[]
[Outputs]
exodus = true
csv = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-scalar-transport.i)
mu=1
rho=1
k=1e-3
diff=1e-3
cp=1
advected_interp_method='average'
velocity_interp_method='rc'
[GlobalParams]
two_term_boundary_expansion = true
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 10
ymin = -1
ymax = 1
nx = 100
ny = 20
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[temperature]
type = INSFVEnergyVariable
[]
[scalar]
type = INSFVScalarFieldVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
vel = 'velocity'
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_quantity = 'rhov'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[v_viscosity]
type = FVDiffusion
variable = v
coeff = ${mu}
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
p = pressure
[]
[energy_advection]
type = INSFVEnergyAdvection
variable = temperature
vel = 'velocity'
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[energy_diffusion]
type = FVDiffusion
coeff = ${k}
variable = temperature
[]
[scalar_advection]
type = INSFVScalarFieldAdvection
variable = scalar
vel = 'velocity'
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[scalar_diffusion]
type = FVDiffusion
coeff = ${diff}
variable = scalar
[]
[scalar_src]
type = FVBodyForce
variable = scalar
value = 0.1
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = 0
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = u
function = 0
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = v
function = 0
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 0
[]
[inlet_t]
type = FVDirichletBC
boundary = 'left'
variable = temperature
value = 1
[]
[inlet_scalar]
type = FVDirichletBC
boundary = 'left'
variable = scalar
value = 1
[]
[]
[Materials]
[const]
type = ADGenericConstantMaterial
prop_names = 'cp'
prop_values = '${cp}'
[]
[ins_fv]
type = INSFVMaterial
u = 'u'
v = 'v'
pressure = 'pressure'
rho = ${rho}
temperature = 'temperature'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/1d-average.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='average'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
xmin = 0
xmax = 1
nx = 2
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
two_term_boundary_expansion = false
[]
[pressure]
type = INSFVPressureVariable
two_term_boundary_expansion = false
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
vel = 'velocity'
pressure = pressure
u = u
mu = ${mu}
rho = ${rho}
flow_boundaries = 'left right'
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
mu = ${mu}
rho = ${rho}
flow_boundaries = 'left right'
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[u_forcing]
type = FVBodyForce
variable = u
function = forcing_u
[]
[]
[FVBCs]
[inlet_u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = 'exact_u'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 'exact_p'
[]
[]
[Materials]
[ins_fv]
type = INSFVMaterial
u = 'u'
pressure = 'pressure'
rho = ${rho}
[]
[]
[Functions]
[exact_u]
type = ParsedFunction
value = 'sin((1/2)*x*pi)'
[]
[exact_rhou]
type = ParsedFunction
value = 'rho*sin((1/2)*x*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_u]
type = ParsedFunction
value = '(1/4)*pi^2*mu*sin((1/2)*x*pi) + pi*rho*sin((1/2)*x*pi)*cos((1/2)*x*pi) - 1/2*pi*sin((1/2)*x*pi)'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_p]
type = ParsedFunction
value = 'cos((1/2)*x*pi)'
[]
[forcing_p]
type = ParsedFunction
value = '(1/2)*pi*rho*cos((1/2)*x*pi)'
vars = 'rho'
vals = '${rho}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[./L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2p]
variable = pressure
function = exact_p
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-mixing-length.i)
Re = 1e4
von_karman_const = 0.2
D = 1
rho = 1
bulk_u = 1
mu = ${fparse rho * bulk_u * D / Re}
advected_interp_method='upwind'
velocity_interp_method='rc'
[GlobalParams]
two_term_boundary_expansion = true
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 5
ymin = 0
ymax = ${fparse 0.5 * D}
nx = 20
ny = 10
bias_y = ${fparse 1 / 1.2}
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[scalar]
type = INSFVScalarFieldVariable
[]
[]
[AuxVariables]
[mixing_len]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
vel = 'velocity'
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
[]
[u_viscosity_rans]
type = INSFVMixingLengthReynoldsStress
variable = u
rho = ${rho}
mixing_length = mixing_len
momentum_component = 'x'
u = u
v = v
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_quantity = 'rhov'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[v_viscosity]
type = FVDiffusion
variable = v
coeff = ${mu}
[]
[v_viscosity_rans]
type = INSFVMixingLengthReynoldsStress
variable = v
rho = ${rho}
mixing_length = mixing_len
momentum_component = 'y'
u = u
v = v
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
p = pressure
[]
[scalar_advection]
type = INSFVScalarFieldAdvection
variable = scalar
vel = 'velocity'
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[scalar_diffusion_rans]
type = INSFVMixingLengthScalarDiffusion
variable = scalar
mixing_length = mixing_len
u = u
v = v
schmidt_number = 1.0
[]
[scalar_src]
type = FVBodyForce
variable = scalar
value = 0.1
[]
[]
[AuxKernels]
[mixing_len]
type = WallDistanceMixingLengthAux
walls = 'top bottom'
variable = mixing_len
execute_on = 'initial'
von_karman_const = ${von_karman_const}
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = '0'
[]
[inlet_scalar]
type = FVDirichletBC
boundary = 'left'
variable = scalar
value = 1
[]
[wall-u]
type = INSFVNoSlipWallBC
boundary = 'top'
variable = u
function = 0
[]
[wall-v]
type = INSFVNoSlipWallBC
boundary = 'top'
variable = v
function = 0
[]
[sym-u]
type = INSFVSymmetryVelocityBC
boundary = 'bottom'
variable = u
u = u
v = v
mu = ${mu}
momentum_component = x
[]
[sym-v]
type = INSFVSymmetryVelocityBC
boundary = 'bottom'
variable = v
u = u
v = v
mu = ${mu}
momentum_component = y
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = '0'
[]
[]
[Materials]
[ins_fv]
type = INSFVMaterial
u = 'u'
v = 'v'
pressure = 'pressure'
rho = ${rho}
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 200 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/mms/rc.i)
mu=1.1
rho=1.1
velocity_interp_method='rc'
[GlobalParams]
force_boundary_execution = false
two_term_boundary_expansion = false
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 2
ny = 2
[]
[]
[Problem]
fv_bcs_integrity_check = false
error_on_jacobian_nonzero_reallocation = true
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[lambda]
family = SCALAR
order = FIRST
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = 'average'
velocity_interp_method = ${velocity_interp_method}
vel = 'velocity'
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[mean_zero_pressure]
type = FVScalarLagrangeMultiplier
variable = pressure
lambda = lambda
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
vel = 'velocity'
advected_interp_method = 'average'
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[u_forcing]
type = FVBodyForce
variable = u
function = forcing_u
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_quantity = 'rhov'
vel = 'velocity'
advected_interp_method = 'average'
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[v_viscosity]
type = FVDiffusion
variable = v
coeff = ${mu}
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
p = pressure
[]
[v_forcing]
type = FVBodyForce
variable = v
function = forcing_v
[]
[]
[FVBCs]
[no-slip-wall-u]
type = INSFVNoSlipWallBC
boundary = 'left right top bottom'
variable = u
function = 'exact_u'
[]
[no-slip-wall-v]
type = INSFVNoSlipWallBC
boundary = 'left right top bottom'
variable = v
function = 'exact_v'
[]
[]
[Materials]
[ins_fv]
type = INSFVMaterial
u = 'u'
v = 'v'
pressure = 'pressure'
rho = ${rho}
[]
[]
[Functions]
[exact_u]
type = ParsedFunction
value = 'sin(y)*cos((1/2)*x*pi)'
[]
[exact_rhou]
type = ParsedFunction
value = 'rho*sin(y)*cos((1/2)*x*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_u]
type = ParsedFunction
value = 'mu*sin(y)*cos((1/2)*x*pi) + (1/4)*pi^2*mu*sin(y)*cos((1/2)*x*pi) - 1/2*pi*rho*sin(x)*sin(y)*sin((1/2)*y*pi)*cos((1/2)*x*pi) + rho*sin(x)*cos(y)*cos((1/2)*x*pi)*cos((1/2)*y*pi) - pi*rho*sin(y)^2*sin((1/2)*x*pi)*cos((1/2)*x*pi) + sin(y)*cos(x)'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_v]
type = ParsedFunction
value = 'sin(x)*cos((1/2)*y*pi)'
[]
[exact_rhov]
type = ParsedFunction
value = 'rho*sin(x)*cos((1/2)*y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_v]
type = ParsedFunction
value = 'mu*sin(x)*cos((1/2)*y*pi) + (1/4)*pi^2*mu*sin(x)*cos((1/2)*y*pi) - pi*rho*sin(x)^2*sin((1/2)*y*pi)*cos((1/2)*y*pi) - 1/2*pi*rho*sin(x)*sin(y)*sin((1/2)*x*pi)*cos((1/2)*y*pi) + rho*sin(y)*cos(x)*cos((1/2)*x*pi)*cos((1/2)*y*pi) + sin(x)*cos(y)'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_p]
type = ParsedFunction
value = 'sin(x)*sin(y)'
[]
[forcing_p]
type = ParsedFunction
value = '-1/2*pi*rho*sin(x)*sin((1/2)*y*pi) - 1/2*pi*rho*sin(y)*sin((1/2)*x*pi)'
vars = 'rho'
vals = '${rho}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 30 lu NONZERO'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[./L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2v]
variable = v
function = exact_v
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2p]
variable = pressure
function = exact_p
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/3d-rc-no-slip.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
xmin = 0
xmax = 10
ymin = -1
ymax = 1
zmin = -1
zmax = 1
nx = 20
ny = 4
nz = 4
elem_type = TET4
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1e-15
[]
[w]
type = INSFVVelocityVariable
initial_condition = 1e-15
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
vel = 'velocity'
pressure = pressure
u = u
v = v
w = w
mu = ${mu}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
w = w
mu = ${mu}
rho = ${rho}
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_quantity = 'rhov'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
w = w
mu = ${mu}
rho = ${rho}
[]
[v_viscosity]
type = FVDiffusion
variable = v
coeff = ${mu}
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
p = pressure
[]
[w_advection]
type = INSFVMomentumAdvection
variable = v
advected_quantity = 'rhow'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
w = w
mu = ${mu}
rho = ${rho}
[]
[w_viscosity]
type = FVDiffusion
variable = w
coeff = ${mu}
[]
[w_pressure]
type = INSFVMomentumPressure
variable = w
momentum_component = 'z'
p = pressure
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = '0'
[]
[inlet-w]
type = INSFVInletVelocityBC
boundary = 'left'
variable = w
function = '0'
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom front back'
variable = u
function = 0
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom front back'
variable = v
function = 0
[]
[walls-w]
type = INSFVNoSlipWallBC
boundary = 'top bottom front back'
variable = w
function = 0
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = '0'
[]
[]
[Materials]
[ins_fv]
type = INSFVMaterial
u = 'u'
v = 'v'
w = 'w'
pressure = 'pressure'
rho = ${rho}
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type -pc_factor_shift_type'
petsc_options_value = 'lu mumps NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[dof]
type = DOFMap
execute_on = 'initial'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/cylindrical/2d-average.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='average'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
[]
[]
[Problem]
kernel_coverage_check = false
fv_bcs_integrity_check = true
coord_type = 'RZ'
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
two_term_boundary_expansion = false
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
two_term_boundary_expansion = false
[]
[pressure]
type = INSFVPressureVariable
two_term_boundary_expansion = false
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
vel = 'velocity'
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[u_forcing]
type = FVBodyForce
variable = u
function = forcing_u
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_quantity = 'rhov'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[v_viscosity]
type = FVDiffusion
variable = v
coeff = ${mu}
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
p = pressure
[]
[v_forcing]
type = FVBodyForce
variable = v
function = forcing_v
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = u
function = 'exact_u'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = v
function = 'exact_v'
[]
[no-slip-wall-u]
type = INSFVNoSlipWallBC
boundary = 'right'
variable = u
function = 'exact_u'
[]
[no-slip-wall-v]
type = INSFVNoSlipWallBC
boundary = 'right'
variable = v
function = 'exact_v'
[]
[outlet-p]
type = INSFVOutletPressureBC
boundary = 'top'
variable = pressure
function = 'exact_p'
[]
[axis-u]
type = INSFVSymmetryVelocityBC
boundary = 'left'
variable = u
u = u
v = v
mu = ${mu}
momentum_component = x
[]
[axis-v]
type = INSFVSymmetryVelocityBC
boundary = 'left'
variable = v
u = u
v = v
mu = ${mu}
momentum_component = y
[]
[axis-p]
type = INSFVSymmetryPressureBC
boundary = 'left'
variable = pressure
[]
[]
[Materials]
[ins_fv]
type = INSFVMaterial
u = 'u'
v = 'v'
pressure = 'pressure'
rho = ${rho}
[]
[]
[Functions]
[exact_u]
type = ParsedFunction
value = 'sin(x*pi)*sin((1/2)*y*pi)'
[]
[exact_rhou]
type = ParsedFunction
value = 'rho*sin(x*pi)*sin((1/2)*y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_u]
type = ParsedFunction
value = '(1/4)*pi^2*mu*sin(x*pi)*sin((1/2)*y*pi) - pi*sin(x*pi)*cos((1/2)*y*pi) - (-x*pi^2*mu*sin(x*pi)*sin((1/2)*y*pi) + pi*mu*sin((1/2)*y*pi)*cos(x*pi))/x + (2*x*pi*rho*sin(x*pi)*sin((1/2)*y*pi)^2*cos(x*pi) + rho*sin(x*pi)^2*sin((1/2)*y*pi)^2)/x + (-x*pi*rho*sin(x*pi)*sin((1/2)*y*pi)*sin(y*pi)*cos(x*pi) + (1/2)*x*pi*rho*sin(x*pi)*cos(x*pi)*cos((1/2)*y*pi)*cos(y*pi))/x'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_v]
type = ParsedFunction
value = 'cos(x*pi)*cos(y*pi)'
[]
[exact_rhov]
type = ParsedFunction
value = 'rho*cos(x*pi)*cos(y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_v]
type = ParsedFunction
value = 'pi^2*mu*cos(x*pi)*cos(y*pi) - 2*pi*rho*sin(y*pi)*cos(x*pi)^2*cos(y*pi) - 1/2*pi*sin((1/2)*y*pi)*cos(x*pi) - (-x*pi^2*mu*cos(x*pi)*cos(y*pi) - pi*mu*sin(x*pi)*cos(y*pi))/x + (-x*pi*rho*sin(x*pi)^2*sin((1/2)*y*pi)*cos(y*pi) + x*pi*rho*sin((1/2)*y*pi)*cos(x*pi)^2*cos(y*pi) + rho*sin(x*pi)*sin((1/2)*y*pi)*cos(x*pi)*cos(y*pi))/x'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_p]
type = ParsedFunction
value = 'cos(x*pi)*cos((1/2)*y*pi)'
[]
[forcing_p]
type = ParsedFunction
value = '-pi*rho*sin(y*pi)*cos(x*pi) + (x*pi*rho*sin((1/2)*y*pi)*cos(x*pi) + rho*sin(x*pi)*sin((1/2)*y*pi))/x'
vars = 'rho'
vals = '${rho}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
[]
[Outputs]
exodus = true
csv = true
[dof]
type = DOFMap
execute_on = 'initial'
[]
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[./L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2v]
type = ElementL2Error
variable = v
function = exact_v
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2p]
variable = pressure
function = exact_p
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-rc-no-slip-extrapolated-outlet-pressure.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'
[GlobalParams]
two_term_boundary_expansion = true
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 10
ymin = -1
ymax = 1
nx = 100
ny = 20
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[lambda]
family = SCALAR
order = FIRST
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
vel = 'velocity'
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[mean_zero_pressure]
type = FVScalarLagrangeMultiplier
variable = pressure
lambda = lambda
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_quantity = 'rhov'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[v_viscosity]
type = FVDiffusion
variable = v
coeff = ${mu}
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
p = pressure
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = '0'
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = u
function = 0
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = v
function = 0
[]
[outlet_u]
type = INSFVMomentumAdvectionOutflowBC
variable = u
advected_quantity = 'rhou'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
u = u
v = v
boundary = 'right'
[]
[outlet_v]
type = INSFVMomentumAdvectionOutflowBC
variable = v
advected_quantity = 'rhov'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
u = u
v = v
boundary = 'right'
[]
[outlet_p]
type = INSFVMassAdvectionOutflowBC
boundary = 'right'
variable = pressure
u = u
v = v
rho = ${rho}
[]
[]
[Materials]
[ins_fv]
type = INSFVMaterial
u = 'u'
v = 'v'
pressure = 'pressure'
rho = ${rho}
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 200 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[dof]
type = DOFMap
execute_on = 'initial'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/lid-driven/lid-driven.i)
mu=.01
rho=1
[GlobalParams]
vel = 'velocity'
velocity_interp_method = 'rc'
advected_interp_method = 'average'
two_term_boundary_expansion = true
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = .1
ymin = 0
ymax = .1
nx = 20
ny = 20
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
[]
[v]
type = INSFVVelocityVariable
[]
[pressure]
type = INSFVPressureVariable
[]
[lambda]
family = SCALAR
order = FIRST
[]
[]
[AuxVariables]
[U]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[]
[AuxKernels]
[mag]
type = VectorMagnitudeAux
variable = U
x = u
y = v
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[mean_zero_pressure]
type = FVScalarLagrangeMultiplier
variable = pressure
lambda = lambda
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_quantity = 'rhov'
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[v_viscosity]
type = FVDiffusion
variable = v
coeff = ${mu}
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
p = pressure
[]
[]
[FVBCs]
[top_x]
type = INSFVNoSlipWallBC
variable = u
boundary = 'top'
function = 1
[]
[no_slip_x]
type = INSFVNoSlipWallBC
variable = u
boundary = 'left right bottom'
function = 0
[]
[no_slip_y]
type = INSFVNoSlipWallBC
variable = v
boundary = 'left right top bottom'
function = 0
[]
[]
[Materials]
[ins_fv]
type = INSFVMaterial
u = 'u'
v = 'v'
pressure = 'pressure'
rho = ${rho}
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-rc-no-slip.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'
[GlobalParams]
two_term_boundary_expansion = true
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 10
ymin = -1
ymax = 1
nx = 100
ny = 20
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
vel = 'velocity'
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_quantity = 'rhov'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[v_viscosity]
type = FVDiffusion
variable = v
coeff = ${mu}
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
p = pressure
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = '0'
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = u
function = 0
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = v
function = 0
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = '0'
[]
[]
[Materials]
[ins_fv]
type = INSFVMaterial
u = 'u'
v = 'v'
pressure = 'pressure'
rho = ${rho}
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 200 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/plane-poiseuille-flow.i)
mu=0.5
rho=1.1
advected_interp_method='average'
velocity_interp_method='average'
two_term_boundary_expansion=true
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 10
ymin = -1
ymax = 1
nx = 10
ny = 2
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
two_term_boundary_expansion = ${two_term_boundary_expansion}
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
two_term_boundary_expansion = ${two_term_boundary_expansion}
[]
[pressure]
type = INSFVPressureVariable
two_term_boundary_expansion = ${two_term_boundary_expansion}
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
vel = 'velocity'
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[u_forcing]
type = FVBodyForce
variable = u
function = forcing_u
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_quantity = 'rhov'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[v_viscosity]
type = FVDiffusion
variable = v
coeff = ${mu}
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
p = pressure
[]
[v_forcing]
type = FVBodyForce
variable = v
function = forcing_v
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = 'exact_u'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = 'exact_v'
[]
[walls-u]
type = INSFVNoSlipWallBC
variable = u
boundary = 'top bottom'
function = 'exact_u'
[]
[walls-v]
type = INSFVNoSlipWallBC
variable = v
boundary = 'top bottom'
function = 'exact_v'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 'exact_p'
[]
[]
[Materials]
[ins_fv]
type = INSFVMaterial
u = 'u'
v = 'v'
pressure = 'pressure'
rho = ${rho}
[]
[]
[Functions]
[exact_u]
type = ParsedFunction
value = '0.5*(1.0 - y^2)/mu'
vars = 'mu'
vals = '${mu}'
[]
[exact_rhou]
type = ParsedFunction
value = '0.5*rho*(1.0 - y^2)/mu'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[forcing_u]
type = ParsedFunction
value = '0'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_v]
type = ParsedFunction
value = '0.0'
[]
[exact_rhov]
type = ParsedFunction
value = '0'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[forcing_v]
type = ParsedFunction
value = '0'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_p]
type = ParsedFunction
value = '10.0 - x'
[]
[forcing_p]
type = ParsedFunction
value = '0'
vars = 'rho mu'
vals = '${rho} ${mu}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[./L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2v]
type = ElementL2Error
variable = v
function = exact_v
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2p]
variable = pressure
function = exact_p
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/cylindrical/2d-average-no-slip.i)
mu=1
rho=1
advected_interp_method='average'
velocity_interp_method='average'
[GlobalParams]
two_term_boundary_expansion = true
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 4
nx = 10
ny = 40
[]
[]
[Problem]
fv_bcs_integrity_check = true
coord_type = 'RZ'
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
vel = 'velocity'
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_quantity = 'rhov'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[v_viscosity]
type = FVDiffusion
variable = v
coeff = ${mu}
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
p = pressure
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = u
function = 0
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = v
function = 1
[]
[no-slip-wall-u]
type = INSFVNoSlipWallBC
boundary = 'right'
variable = u
function = 0
[]
[no-slip-wall-v]
type = INSFVNoSlipWallBC
boundary = 'right'
variable = v
function = 0
[]
[outlet-p]
type = INSFVOutletPressureBC
boundary = 'top'
variable = pressure
function = 0
[]
[axis-u]
type = INSFVSymmetryVelocityBC
boundary = 'left'
variable = u
u = u
v = v
mu = ${mu}
momentum_component = x
[]
[axis-v]
type = INSFVSymmetryVelocityBC
boundary = 'left'
variable = v
u = u
v = v
mu = ${mu}
momentum_component = y
[]
[axis-p]
type = INSFVSymmetryPressureBC
boundary = 'left'
variable = pressure
[]
[]
[Materials]
[ins_fv]
type = INSFVMaterial
u = 'u'
v = 'v'
pressure = 'pressure'
rho = ${rho}
[]
[]
[Postprocessors]
[in]
type = SideIntegralVariablePostprocessor
variable = v
boundary = 'bottom'
[]
[out]
type = SideIntegralVariablePostprocessor
variable = v
boundary = 'top'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/rotated/rotated-pp-flow.i)
mu=0.5
rho=1.1
advected_interp_method='average'
velocity_interp_method='average'
two_term_boundary_expansion=true
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 10
ymin = -1
ymax = 1
nx = 10
ny = 2
[]
[rotate]
type = TransformGenerator
input = gen
transform = 'rotate'
vector_value = '45 0 0'
[]
[]
[Problem]
kernel_coverage_check = false
fv_bcs_integrity_check = true
[]
[AuxVariables]
[vel_exact_x][]
[vel_exact_y][]
[p_exact][]
[]
[AuxKernels]
[u_exact]
type = FunctionAux
variable = vel_exact_x
function = exact_u
[]
[v_exact]
type = FunctionAux
variable = vel_exact_y
function = exact_v
[]
[p_exact]
type = FunctionAux
variable = p_exact
function = exact_p
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
two_term_boundary_expansion = ${two_term_boundary_expansion}
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
two_term_boundary_expansion = ${two_term_boundary_expansion}
[]
[pressure]
type = INSFVPressureVariable
two_term_boundary_expansion = ${two_term_boundary_expansion}
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
vel = 'velocity'
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[u_forcing]
type = FVBodyForce
variable = u
function = forcing_u
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_quantity = 'rhov'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[v_viscosity]
type = FVDiffusion
variable = v
coeff = ${mu}
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
p = pressure
[]
[v_forcing]
type = FVBodyForce
variable = v
function = forcing_v
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = 'exact_u'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = 'exact_v'
[]
[walls-u]
type = INSFVNoSlipWallBC
variable = u
boundary = 'top bottom'
function = 'exact_u'
[]
[walls-v]
type = INSFVNoSlipWallBC
variable = v
boundary = 'top bottom'
function = 'exact_v'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 'exact_p'
[]
[]
[Materials]
[ins_fv]
type = INSFVMaterial
u = 'u'
v = 'v'
pressure = 'pressure'
rho = ${rho}
[]
[]
[Functions]
[exact_u]
type = ParsedFunction
value = '0.25*sqrt(2)*(1.0 - 1/2*(-x + y)^2)/mu'
vars = 'mu'
vals = '${mu}'
[]
[exact_rhou]
type = ParsedFunction
value = '0.25*sqrt(2)*rho*(1.0 - 1/2*(-x + y)^2)/mu'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[forcing_u]
type = ParsedFunction
value = '0'
[]
[exact_v]
type = ParsedFunction
value = '0.25*sqrt(2)*(1.0 - 1/2*(-x + y)^2)/mu'
vars = 'mu'
vals = '${mu}'
[]
[exact_rhov]
type = ParsedFunction
value = '0.25*sqrt(2)*rho*(1.0 - 1/2*(-x + y)^2)/mu'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[forcing_v]
type = ParsedFunction
value = '0'
[]
[exact_p]
type = ParsedFunction
value = '-1/2*sqrt(2)*(x + y) + 10.0'
[]
[forcing_p]
type = ParsedFunction
value = '0'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
[]
[Outputs]
exodus = true
csv = true
[dof]
type = DOFMap
execute_on = 'initial'
[]
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[./L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2v]
type = ElementL2Error
variable = v
function = exact_v
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2p]
variable = pressure
function = exact_p
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/cylindrical/2d-average-with-temp.i)
mu=1.1
rho=1.1
k=1.1
cp=1.1
advected_interp_method='average'
velocity_interp_method='average'
velocity='velocity'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
[]
[]
[Problem]
kernel_coverage_check = false
fv_bcs_integrity_check = true
coord_type = 'RZ'
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
two_term_boundary_expansion = false
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
two_term_boundary_expansion = false
[]
[pressure]
type = INSFVPressureVariable
two_term_boundary_expansion = false
[]
[temperature]
type = INSFVEnergyVariable
two_term_boundary_expansion = false
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
vel = ${velocity}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
vel = ${velocity}
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[u_forcing]
type = FVBodyForce
variable = u
function = forcing_u
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_quantity = 'rhov'
vel = ${velocity}
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[v_viscosity]
type = FVDiffusion
variable = v
coeff = ${mu}
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
p = pressure
[]
[v_forcing]
type = FVBodyForce
variable = v
function = forcing_v
[]
[temp_conduction]
type = FVDiffusion
coeff = 'k'
variable = temperature
[]
[temp_advection]
type = INSFVEnergyAdvection
vel = ${velocity}
variable = temperature
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[temp_forcing]
type = FVBodyForce
variable = temperature
function = forcing_t
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = u
function = 'exact_u'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = v
function = 'exact_v'
[]
[no-slip-wall-u]
type = INSFVNoSlipWallBC
boundary = 'right'
variable = u
function = 'exact_u'
[]
[no-slip-wall-v]
type = INSFVNoSlipWallBC
boundary = 'right'
variable = v
function = 'exact_v'
[]
[outlet-p]
type = INSFVOutletPressureBC
boundary = 'top'
variable = pressure
function = 'exact_p'
[]
[axis-u]
type = INSFVSymmetryVelocityBC
boundary = 'left'
variable = u
u = u
v = v
mu = ${mu}
momentum_component = x
[]
[axis-v]
type = INSFVSymmetryVelocityBC
boundary = 'left'
variable = v
u = u
v = v
mu = ${mu}
momentum_component = y
[]
[axis-p]
type = INSFVSymmetryPressureBC
boundary = 'left'
variable = pressure
[]
[axis-inlet-wall-t]
type = FVFunctionDirichletBC
boundary = 'left bottom right'
variable = temperature
function = 'exact_t'
[]
[]
[Materials]
[const]
type = ADGenericConstantMaterial
prop_names = 'k cp'
prop_values = '${k} ${cp}'
[]
[ins_fv]
type = INSFVMaterial
u = 'u'
v = 'v'
pressure = 'pressure'
temperature = 'temperature'
rho = ${rho}
[]
[]
[Functions]
[exact_u]
type = ParsedFunction
value = 'sin(x*pi)*sin((1/2)*y*pi)'
[]
[exact_rhou]
type = ParsedFunction
value = 'rho*sin(x*pi)*sin((1/2)*y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_u]
type = ParsedFunction
value = '(1/4)*pi^2*mu*sin(x*pi)*sin((1/2)*y*pi) - pi*sin(x*pi)*cos((1/2)*y*pi) - (-x*pi^2*mu*sin(x*pi)*sin((1/2)*y*pi) + pi*mu*sin((1/2)*y*pi)*cos(x*pi))/x + (2*x*pi*rho*sin(x*pi)*sin((1/2)*y*pi)^2*cos(x*pi) + rho*sin(x*pi)^2*sin((1/2)*y*pi)^2)/x + (-x*pi*rho*sin(x*pi)*sin((1/2)*y*pi)*sin(y*pi)*cos(x*pi) + (1/2)*x*pi*rho*sin(x*pi)*cos(x*pi)*cos((1/2)*y*pi)*cos(y*pi))/x'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_v]
type = ParsedFunction
value = 'cos(x*pi)*cos(y*pi)'
[]
[exact_rhov]
type = ParsedFunction
value = 'rho*cos(x*pi)*cos(y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_v]
type = ParsedFunction
value = 'pi^2*mu*cos(x*pi)*cos(y*pi) - 2*pi*rho*sin(y*pi)*cos(x*pi)^2*cos(y*pi) - 1/2*pi*sin((1/2)*y*pi)*cos(x*pi) - (-x*pi^2*mu*cos(x*pi)*cos(y*pi) - pi*mu*sin(x*pi)*cos(y*pi))/x + (-x*pi*rho*sin(x*pi)^2*sin((1/2)*y*pi)*cos(y*pi) + x*pi*rho*sin((1/2)*y*pi)*cos(x*pi)^2*cos(y*pi) + rho*sin(x*pi)*sin((1/2)*y*pi)*cos(x*pi)*cos(y*pi))/x'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_p]
type = ParsedFunction
value = 'cos(x*pi)*cos((1/2)*y*pi)'
[]
[forcing_p]
type = ParsedFunction
value = '-pi*rho*sin(y*pi)*cos(x*pi) + (x*pi*rho*sin((1/2)*y*pi)*cos(x*pi) + rho*sin(x*pi)*sin((1/2)*y*pi))/x'
vars = 'rho'
vals = '${rho}'
[]
[exact_t]
type = ParsedFunction
value = 'sin(x*pi)*sin((1/2)*y*pi)'
[]
[forcing_t]
type = ParsedFunction
value = '(1/4)*pi^2*k*sin(x*pi)*sin((1/2)*y*pi) - (-x*pi^2*k*sin(x*pi)*sin((1/2)*y*pi) + pi*k*sin((1/2)*y*pi)*cos(x*pi))/x + (2*x*pi*cp*rho*sin(x*pi)*sin((1/2)*y*pi)^2*cos(x*pi) + cp*rho*sin(x*pi)^2*sin((1/2)*y*pi)^2)/x + (-x*pi*cp*rho*sin(x*pi)*sin((1/2)*y*pi)*sin(y*pi)*cos(x*pi) + (1/2)*x*pi*cp*rho*sin(x*pi)*cos(x*pi)*cos((1/2)*y*pi)*cos(y*pi))/x'
vars = 'k rho cp'
vals = '${k} ${rho} ${cp}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
[]
[Outputs]
exodus = true
csv = true
[dof]
type = DOFMap
execute_on = 'initial'
[]
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[./L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2v]
type = ElementL2Error
variable = v
function = exact_v
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2p]
variable = pressure
function = exact_p
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2t]
variable = temperature
function = exact_t
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[]
(modules/navier_stokes/test/tests/postprocessors/conservation_INSFV.i)
mu=1.1
rho=1
advected_interp_method='average'
velocity_interp_method='average'
[GlobalParams]
two_term_boundary_expansion = true
[]
[Mesh]
inactive = 'mesh internal_boundary_bot internal_boundary_top'
[mesh]
type = CartesianMeshGenerator
dim = 2
dx = '1'
dy = '1 1 1'
ix = '5'
iy = '5 5 5'
subdomain_id = '1
2
3'
[]
[internal_boundary_bot]
type = SideSetsBetweenSubdomainsGenerator
input = mesh
new_boundary = 'internal_bot'
primary_block = 1
paired_block = 2
[]
[internal_boundary_top]
type = SideSetsBetweenSubdomainsGenerator
input = internal_boundary_bot
new_boundary = 'internal_top'
primary_block = 2
paired_block = 3
[]
[diverging_mesh]
type = FileMeshGenerator
file = 'expansion_quad.e'
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 0
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[temperature]
type = INSFVEnergyVariable
[]
[]
[AuxVariables]
[advected_density]
order = CONSTANT
family = MONOMIAL
fv = true
initial_condition = ${rho}
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
vel = 'velocity'
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
force_boundary_execution = true
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_quantity = 'rhov'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[v_viscosity]
type = FVDiffusion
variable = v
coeff = ${mu}
force_boundary_execution = true
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
p = pressure
[]
[temp_advection]
type = INSFVEnergyAdvection
vel = 'velocity'
variable = temperature
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[temp_source]
type = FVBodyForce
variable = temperature
function = 10
block = 1
[]
[]
[FVBCs]
inactive = 'noslip-u noslip-v'
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = u
function = 0
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = v
function = 1
[]
[noslip-u]
type = INSFVNoSlipWallBC
boundary = 'right'
variable = u
function = 0
[]
[noslip-v]
type = INSFVNoSlipWallBC
boundary = 'right'
variable = v
function = 0
[]
[free-slip-u]
type = INSFVNaturalFreeSlipBC
boundary = 'right'
variable = u
[]
[free-slip-v]
type = INSFVNaturalFreeSlipBC
boundary = 'right'
variable = v
[]
[axis-u]
type = INSFVSymmetryVelocityBC
boundary = 'left'
variable = u
u = u
v = v
mu = ${mu}
momentum_component = x
[]
[axis-v]
type = INSFVSymmetryVelocityBC
boundary = 'left'
variable = v
u = u
v = v
mu = ${mu}
momentum_component = y
[]
[axis-p]
type = INSFVSymmetryPressureBC
boundary = 'left'
variable = pressure
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'top'
variable = pressure
function = 0
[]
[inlet_temp]
type = FVNeumannBC
boundary = 'bottom'
variable = temperature
value = 300
[]
[]
[Materials]
[ins_fv]
type = INSFVMaterial
u = 'u'
v = 'v'
pressure = 'pressure'
temperature = 'temperature'
rho = ${rho}
[]
[advected_material_property]
type = ADGenericConstantMaterial
prop_names = 'advected_rho cp'
prop_values ='${rho} 1'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 200 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Postprocessors]
[inlet_mass_variable]
type = VolumetricFlowRate
boundary = bottom
vel_x = u
vel_y = v
advected_variable = advected_density
fv = true
advected_interp_method = ${advected_interp_method}
[]
[inlet_mass_constant]
type = VolumetricFlowRate
boundary = bottom
vel_x = u
vel_y = v
advected_variable = ${rho}
fv = true
advected_interp_method = ${advected_interp_method}
[]
[inlet_mass_matprop]
type = VolumetricFlowRate
boundary = bottom
vel_x = u
vel_y = v
advected_mat_prop = 'advected_rho'
fv = true
[]
[mid1_mass]
type = InternalVolumetricFlowRate
boundary = internal_bot
vel_x = u
vel_y = v
fv = true
advected_interp_method = ${advected_interp_method}
[]
[mid2_mass]
type = InternalVolumetricFlowRate
boundary = internal_top
vel_x = u
vel_y = v
fv = true
advected_interp_method = ${advected_interp_method}
[]
[outlet_mass]
type = VolumetricFlowRate
boundary = top
vel_x = u
vel_y = v
fv = true
advected_interp_method = ${advected_interp_method}
[]
[inlet_momentum_x]
type = VolumetricFlowRate
boundary = bottom
vel_x = u
vel_y = v
advected_variable = u
fv = true
advected_interp_method = ${advected_interp_method}
[]
[mid1_momentum_x]
type = InternalVolumetricFlowRate
boundary = internal_bot
vel_x = u
vel_y = v
advected_variable = u
fv = true
advected_interp_method = ${advected_interp_method}
[]
[mid2_momentum_x]
type = InternalVolumetricFlowRate
boundary = internal_top
vel_x = u
vel_y = v
advected_variable = u
fv = true
advected_interp_method = ${advected_interp_method}
[]
[outlet_momentum_x]
type = VolumetricFlowRate
boundary = top
vel_x = u
vel_y = v
advected_variable = u
fv = true
advected_interp_method = ${advected_interp_method}
[]
[inlet_momentum_y]
type = VolumetricFlowRate
boundary = bottom
vel_x = u
vel_y = v
advected_variable = v
fv = true
advected_interp_method = ${advected_interp_method}
[]
[mid1_momentum_y]
type = InternalVolumetricFlowRate
boundary = internal_bot
vel_x = u
vel_y = v
advected_variable = v
fv = true
advected_interp_method = ${advected_interp_method}
[]
[mid2_momentum_y]
type = InternalVolumetricFlowRate
boundary = internal_top
vel_x = u
vel_y = v
advected_variable = v
fv = true
advected_interp_method = ${advected_interp_method}
[]
[outlet_momentum_y]
type = VolumetricFlowRate
boundary = top
vel_x = u
vel_y = v
advected_variable = v
fv = true
advected_interp_method = ${advected_interp_method}
[]
[inlet_advected_energy]
type = VolumetricFlowRate
boundary = bottom
vel_x = u
vel_y = v
advected_mat_prop = 'rho_cp_temp'
fv = true
[]
[mid1_advected_energy]
type = InternalVolumetricFlowRate
boundary = internal_bot
vel_x = u
vel_y = v
advected_mat_prop = 'rho_cp_temp'
fv = true
advected_interp_method = ${advected_interp_method}
[]
[mid2_advected_energy]
type = InternalVolumetricFlowRate
boundary = internal_top
vel_x = u
vel_y = v
advected_mat_prop = 'rho_cp_temp'
fv = true
advected_interp_method = ${advected_interp_method}
[]
[outlet_advected_energy]
type = VolumetricFlowRate
boundary = top
vel_x = u
vel_y = v
advected_mat_prop = 'rho_cp_temp'
fv = true
[]
[]
[Outputs]
exodus = false
csv = true
inactive = 'console_mass console_momentum_x console_momentum_y console_energy'
[console_mass]
type = Console
start_step = 1
show = 'inlet_mass_variable inlet_mass_constant inlet_mass_matprop mid1_mass mid2_mass outlet_mass'
[]
[console_momentum_x]
type = Console
start_step = 1
show = 'inlet_momentum_x mid1_momentum_x mid2_momentum_x outlet_momentum_x'
[]
[console_momentum_y]
type = Console
start_step = 1
show = 'inlet_momentum_y mid1_momentum_y mid2_momentum_y outlet_momentum_y'
[]
[console_energy]
type = Console
start_step = 1
show = 'inlet_advected_energy mid1_advected_energy mid2_advected_energy outlet_advected_energy'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-rc-ambient-convection.i)
mu=1
rho=1
k=1e-3
cp=1
advected_interp_method='average'
velocity_interp_method='rc'
[GlobalParams]
two_term_boundary_expansion = true
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 5
ymin = -1
ymax = 1
nx = 50
ny = 16
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[temperature]
type = INSFVEnergyVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
vel = 'velocity'
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_quantity = 'rhov'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[v_viscosity]
type = FVDiffusion
variable = v
coeff = ${mu}
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
p = pressure
[]
[energy_advection]
type = INSFVEnergyAdvection
variable = temperature
vel = 'velocity'
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[energy_diffusion]
type = FVDiffusion
coeff = ${k}
variable = temperature
[]
[ambient_convection]
type = NSFVEnergyAmbientConvection
variable = temperature
T_ambient = 100
alpha = 'alpha'
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = 0
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = u
function = 0
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = v
function = 0
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 0
[]
[inlet_t]
type = FVDirichletBC
boundary = 'left'
variable = temperature
value = 1
[]
[]
[Materials]
[const]
type = ADGenericConstantMaterial
prop_names = 'cp alpha'
prop_values = '${cp} 1'
[]
[ins_fv]
type = INSFVMaterial
u = 'u'
v = 'v'
pressure = 'pressure'
rho = ${rho}
temperature = 'temperature'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/3d-rc.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
xmin = 0
xmax = 10
ymin = -1
ymax = 1
zmin = -1
zmax = 1
nx = 21
ny = 7
nz = 7
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1e-6
[]
[w]
type = INSFVVelocityVariable
initial_condition = 1e-6
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
vel = 'velocity'
pressure = pressure
u = u
v = v
w = w
mu = ${mu}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
w = w
mu = ${mu}
rho = ${rho}
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_quantity = 'rhov'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
w = w
mu = ${mu}
rho = ${rho}
[]
[v_viscosity]
type = FVDiffusion
variable = v
coeff = ${mu}
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
p = pressure
[]
[w_advection]
type = INSFVMomentumAdvection
variable = w
advected_quantity = 'rhow'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
w = w
mu = ${mu}
rho = ${rho}
[]
[w_viscosity]
type = FVDiffusion
variable = w
coeff = ${mu}
[]
[w_pressure]
type = INSFVMomentumPressure
variable = w
momentum_component = 'z'
p = pressure
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = 0
[]
[inlet-w]
type = INSFVInletVelocityBC
boundary = 'left'
variable = w
function = 0
[]
[walls-u]
type = INSFVNaturalFreeSlipBC
boundary = 'top bottom front back'
variable = u
[]
[walls-v]
type = INSFVNaturalFreeSlipBC
boundary = 'top bottom front back'
variable = v
[]
[walls-w]
type = INSFVNaturalFreeSlipBC
boundary = 'top bottom front back'
variable = w
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 0
[]
[]
[Materials]
[ins_fv]
type = INSFVMaterial
u = 'u'
v = 'v'
w = 'w'
pressure = 'pressure'
rho = ${rho}
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_abs_tol = 1e-13
[]
[Outputs]
exodus = true
csv = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-rc-no-slip-outflow-bcs.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'
[GlobalParams]
two_term_boundary_expansion = true
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 10
ymin = -1
ymax = 1
nx = 100
ny = 20
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
vel = 'velocity'
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_quantity = 'rhov'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[v_viscosity]
type = FVDiffusion
variable = v
coeff = ${mu}
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
p = pressure
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = '0'
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = u
function = 0
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = v
function = 0
[]
[outlet_u]
type = INSFVMomentumAdvectionOutflowBC
variable = u
advected_quantity = 'rhou'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
u = u
v = v
boundary = 'right'
[]
[outlet_v]
type = INSFVMomentumAdvectionOutflowBC
variable = v
advected_quantity = 'rhov'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
u = u
v = v
boundary = 'right'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = '0'
[]
[]
[Materials]
[ins_fv]
type = INSFVMaterial
u = 'u'
v = 'v'
pressure = 'pressure'
rho = ${rho}
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 200 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[dof]
type = DOFMap
execute_on = 'initial'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/cylindrical/2d-rc.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
[]
[]
[Problem]
kernel_coverage_check = false
fv_bcs_integrity_check = true
coord_type = 'RZ'
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
vel = 'velocity'
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[u_forcing]
type = FVBodyForce
variable = u
function = forcing_u
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_quantity = 'rhov'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[v_viscosity]
type = FVDiffusion
variable = v
coeff = ${mu}
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
p = pressure
[]
[v_forcing]
type = FVBodyForce
variable = v
function = forcing_v
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = u
function = 'exact_u'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'bottom'
variable = v
function = 'exact_v'
[]
[no-slip-wall-u]
type = INSFVNoSlipWallBC
boundary = 'right'
variable = u
function = 'exact_u'
[]
[no-slip-wall-v]
type = INSFVNoSlipWallBC
boundary = 'right'
variable = v
function = 'exact_v'
[]
[outlet-p]
type = INSFVOutletPressureBC
boundary = 'top'
variable = pressure
function = 'exact_p'
[]
[axis-u]
type = INSFVSymmetryVelocityBC
boundary = 'left'
variable = u
u = u
v = v
mu = ${mu}
momentum_component = x
[]
[axis-v]
type = INSFVSymmetryVelocityBC
boundary = 'left'
variable = v
u = u
v = v
mu = ${mu}
momentum_component = y
[]
[axis-p]
type = INSFVSymmetryPressureBC
boundary = 'left'
variable = pressure
[]
[]
[Materials]
[ins_fv]
type = INSFVMaterial
u = 'u'
v = 'v'
pressure = 'pressure'
rho = ${rho}
[]
[]
[Functions]
[exact_u]
type = ParsedFunction
value = 'sin(x*pi)*sin((1/2)*y*pi)'
[]
[exact_rhou]
type = ParsedFunction
value = 'rho*sin(x*pi)*sin((1/2)*y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_u]
type = ParsedFunction
value = '(1/4)*pi^2*mu*sin(x*pi)*sin((1/2)*y*pi) - pi*sin(x*pi)*cos((1/2)*y*pi) - (-x*pi^2*mu*sin(x*pi)*sin((1/2)*y*pi) + pi*mu*sin((1/2)*y*pi)*cos(x*pi))/x + (2*x*pi*rho*sin(x*pi)*sin((1/2)*y*pi)^2*cos(x*pi) + rho*sin(x*pi)^2*sin((1/2)*y*pi)^2)/x + (-x*pi*rho*sin(x*pi)*sin((1/2)*y*pi)*sin(y*pi)*cos(x*pi) + (1/2)*x*pi*rho*sin(x*pi)*cos(x*pi)*cos((1/2)*y*pi)*cos(y*pi))/x'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_v]
type = ParsedFunction
value = 'cos(x*pi)*cos(y*pi)'
[]
[exact_rhov]
type = ParsedFunction
value = 'rho*cos(x*pi)*cos(y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_v]
type = ParsedFunction
value = 'pi^2*mu*cos(x*pi)*cos(y*pi) - 2*pi*rho*sin(y*pi)*cos(x*pi)^2*cos(y*pi) - 1/2*pi*sin((1/2)*y*pi)*cos(x*pi) - (-x*pi^2*mu*cos(x*pi)*cos(y*pi) - pi*mu*sin(x*pi)*cos(y*pi))/x + (-x*pi*rho*sin(x*pi)^2*sin((1/2)*y*pi)*cos(y*pi) + x*pi*rho*sin((1/2)*y*pi)*cos(x*pi)^2*cos(y*pi) + rho*sin(x*pi)*sin((1/2)*y*pi)*cos(x*pi)*cos(y*pi))/x'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_p]
type = ParsedFunction
value = 'cos(x*pi)*cos((1/2)*y*pi)'
[]
[forcing_p]
type = ParsedFunction
value = '-pi*rho*sin(y*pi)*cos(x*pi) + (x*pi*rho*sin((1/2)*y*pi)*cos(x*pi) + rho*sin(x*pi)*sin((1/2)*y*pi))/x'
vars = 'rho'
vals = '${rho}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 200 lu NONZERO'
line_search = 'none'
[]
[Outputs]
exodus = true
csv = true
[dof]
type = DOFMap
execute_on = 'initial'
[]
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[./L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2v]
type = ElementL2Error
variable = v
function = exact_v
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2p]
variable = pressure
function = exact_p
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-rc.i)
mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 10
ymin = -1
ymax = 1
nx = 100
ny = 20
[]
[]
[Problem]
fv_bcs_integrity_check = true
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
vel = 'velocity'
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_quantity = 'rhov'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[v_viscosity]
type = FVDiffusion
variable = v
coeff = ${mu}
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
p = pressure
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = 0
[]
[walls-u]
type = INSFVNaturalFreeSlipBC
boundary = 'top bottom'
variable = u
[]
[walls-v]
type = INSFVNaturalFreeSlipBC
boundary = 'top bottom'
variable = v
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 0
[]
[]
[Materials]
[ins_fv]
type = INSFVMaterial
u = 'u'
v = 'v'
pressure = 'pressure'
rho = ${rho}
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 100 lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/mms/cylindrical/2d-rc.i)
mu=1.1
rho=1.1
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 1
xmax = 3
ymin = -1
ymax = 1
nx = 2
ny = 2
[]
[]
[Problem]
coord_type = 'RZ'
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[lambda]
family = SCALAR
order = FIRST
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = 'average'
velocity_interp_method = 'rc'
vel = 'velocity'
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
no_slip_wall_boundaries = 'left right top bottom'
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[mean_zero_pressure]
type = FVScalarLagrangeMultiplier
variable = pressure
lambda = lambda
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
vel = 'velocity'
advected_interp_method = 'average'
velocity_interp_method = 'rc'
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
no_slip_wall_boundaries = 'left right top bottom'
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[u_forcing]
type = FVBodyForce
variable = u
function = forcing_u
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_quantity = 'rhov'
vel = 'velocity'
advected_interp_method = 'average'
velocity_interp_method = 'rc'
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
no_slip_wall_boundaries = 'left right top bottom'
[]
[v_viscosity]
type = FVDiffusion
variable = v
coeff = ${mu}
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
p = pressure
[]
[v_forcing]
type = FVBodyForce
variable = v
function = forcing_v
[]
[]
[FVBCs]
[no-slip-wall-u]
type = INSFVNoSlipWallBC
boundary = 'left right top bottom'
variable = u
function = 'exact_u'
[]
[no-slip-wall-v]
type = INSFVNoSlipWallBC
boundary = 'left right top bottom'
variable = v
function = 'exact_v'
[]
[]
[Materials]
[ins_fv]
type = INSFVMaterial
u = u
v = v
pressure = 'pressure'
rho = ${rho}
[]
[]
[Functions]
[exact_u]
type = ParsedFunction
value = 'sin(y)*sin(x*pi)'
[]
[exact_rhou]
type = ParsedFunction
value = 'rho*sin(y)*sin(x*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_u]
type = ParsedFunction
value = 'mu*sin(y)*sin(x*pi) - (-x*pi^2*mu*sin(y)*sin(x*pi) + pi*mu*sin(y)*cos(x*pi))/x + (2*x*pi*rho*sin(y)^2*sin(x*pi)*cos(x*pi) + rho*sin(y)^2*sin(x*pi)^2)/x + (-1/2*x*pi*rho*sin(x)*sin(y)*sin(x*pi)*sin((1/2)*y*pi) + x*rho*sin(x)*sin(x*pi)*cos(y)*cos((1/2)*y*pi))/x'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_v]
type = ParsedFunction
value = 'sin(x)*cos((1/2)*y*pi)'
[]
[exact_rhov]
type = ParsedFunction
value = 'rho*sin(x)*cos((1/2)*y*pi)'
vars = 'rho'
vals = '${rho}'
[]
[forcing_v]
type = ParsedFunction
value = '(1/4)*pi^2*mu*sin(x)*cos((1/2)*y*pi) - pi*rho*sin(x)^2*sin((1/2)*y*pi)*cos((1/2)*y*pi) + cos(y) - (-x*mu*sin(x)*cos((1/2)*y*pi) + mu*cos(x)*cos((1/2)*y*pi))/x + (x*pi*rho*sin(x)*sin(y)*cos(x*pi)*cos((1/2)*y*pi) + x*rho*sin(y)*sin(x*pi)*cos(x)*cos((1/2)*y*pi) + rho*sin(x)*sin(y)*sin(x*pi)*cos((1/2)*y*pi))/x'
vars = 'mu rho'
vals = '${mu} ${rho}'
[]
[exact_p]
type = ParsedFunction
value = 'sin(y)'
[]
[forcing_p]
type = ParsedFunction
value = '-1/2*pi*rho*sin(x)*sin((1/2)*y*pi) + (x*pi*rho*sin(y)*cos(x*pi) + rho*sin(y)*sin(x*pi))/x'
vars = 'rho'
vals = '${rho}'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm 30 lu NONZERO'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[./L2u]
type = ElementL2Error
variable = u
function = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2v]
type = ElementL2Error
variable = v
function = exact_v
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[./L2p]
variable = pressure
function = exact_p
type = ElementL2Error
outputs = 'console csv'
execute_on = 'timestep_end'
[../]
[]
(modules/navier_stokes/examples/pipe_mixing_length/pipe_mixing_length.i)
# This example demonstrates how the mixing length model can be tuned to match an
# established correlation for pressure drop in a smooth circular pipe.
# The primary input parameters for this example are the system Reynolds number
# and the von Karman constant for the mixing length model. These two parameters
# can be changed here:
Re = 1e5
von_karman_const = 0.22
# Note that for this model (using the wall-distance mixing length for the entire
# pipe) different von Karman constants are optimal for different Reynolds
# numbers.
# This model has been non-dimensionalized. The diameter (D), density (rho), and
# bulk velocity (bulk_u) are all considered unity.
D = 1
total_len = ${fparse 40 * D}
rho = 1
bulk_u = 1
# With those parameters set, the viscosity is then computed in order to reach
# the desired Reynolds number.
mu = ${fparse rho * bulk_u * D / Re}
# Here the DeltaP will be evaluted by using a postprocessor to find the pressure
# at a point that is 10 diameters away from the outlet. (The outlet pressure is
# set to zero.)
L = ${fparse 10 * D}
# We will use the McAdams correlation to find the Darcy friction factor. Note
# that this correlation is valid for fully developed flow in smooth circular
# tubes at 3e4 < Re < 1e6.
f = ${fparse 0.316 * Re^(-0.25)}
# The DeltaP can then be computed using this friction factor as,
ref_delta_P = ${fparse f * L / D * rho * bulk_u^2 / 2}
# The upwind and Rhie-Chow interpolation schemes are used here.
advected_interp_method='upwind'
velocity_interp_method='rc'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${total_len}
ymin = 0
ymax = ${fparse 0.5 * D}
nx = 200
ny = 40
bias_y = ${fparse 1 / 1.2}
[]
[rename1]
type = RenameBoundaryGenerator
input = gen
old_boundary = 'left'
new_boundary = 'inlet'
[]
[rename2]
type = RenameBoundaryGenerator
input = rename1
old_boundary = 'right'
new_boundary = 'outlet'
[]
[rename3]
type = RenameBoundaryGenerator
input = rename2
old_boundary = 'bottom'
new_boundary = 'symmetry'
[]
[rename4]
type = RenameBoundaryGenerator
input = rename3
old_boundary = 'top'
new_boundary = 'wall'
[]
[]
[Outputs]
exodus = true
[]
[Problem]
kernel_coverage_check = false
fv_bcs_integrity_check = true
coord_type = 'RZ'
rz_coord_axis = 'X'
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1e-6
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1e-6
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[AuxVariables]
[mixing_len]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
vel = 'velocity'
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
advected_quantity = 'rhou'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[u_viscosity]
type = FVDiffusion
variable = u
coeff = ${mu}
[]
[u_viscosity_rans]
type = INSFVMixingLengthReynoldsStress
variable = u
rho = ${rho}
mixing_length = mixing_len
momentum_component = 'x'
u = u
v = v
[]
[u_pressure]
type = INSFVMomentumPressure
variable = u
momentum_component = 'x'
p = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
advected_quantity = 'rhov'
vel = 'velocity'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
pressure = pressure
u = u
v = v
mu = ${mu}
rho = ${rho}
[]
[v_viscosity]
type = FVDiffusion
variable = v
coeff = ${mu}
[]
[v_viscosity_rans]
type = INSFVMixingLengthReynoldsStress
variable = v
rho = ${rho}
mixing_length = mixing_len
momentum_component = 'y'
u = u
v = v
[]
[v_pressure]
type = INSFVMomentumPressure
variable = v
momentum_component = 'y'
p = pressure
[]
[]
[AuxKernels]
[mixing_len]
type = WallDistanceMixingLengthAux
walls = 'wall'
variable = mixing_len
execute_on = 'initial'
von_karman_const = ${von_karman_const}
[]
[]
[FVBCs]
[inlet_u]
type = INSFVInletVelocityBC
boundary = 'inlet'
variable = u
function = ${bulk_u}
[]
[inlet_v]
type = INSFVInletVelocityBC
boundary = 'inlet'
variable = v
function = '0'
[]
[walls_u]
type = INSFVNoSlipWallBC
boundary = 'wall'
variable = u
function = 0
[]
[walls_v]
type = INSFVNoSlipWallBC
boundary = 'wall'
variable = v
function = 0
[]
[sym_u]
type = INSFVSymmetryVelocityBC
boundary = 'symmetry'
variable = u
u = u
v = v
mu = ${mu}
momentum_component = x
[]
[sym_v]
type = INSFVSymmetryVelocityBC
boundary = 'symmetry'
variable = v
u = u
v = v
mu = ${mu}
momentum_component = y
[]
[sym_p]
type = INSFVSymmetryPressureBC
boundary = 'symmetry'
variable = pressure
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'outlet'
variable = pressure
function = '0'
[]
[]
[Materials]
[ins_fv]
type = INSFVMaterial
u = 'u'
v = 'v'
pressure = 'pressure'
rho = ${rho}
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
line_search = 'none'
nl_rel_tol = 1e-12
nl_abs_tol = 1e-12
[]
[Postprocessors]
[delta_P]
type = PointValue
variable = 'pressure'
point = '${fparse total_len - L} 0 0'
[]
[reference_delta_P]
type = Receiver
default = ${ref_delta_P}
[]
[]
(modules/navier_stokes/include/fvkernels/INSFVMassAdvection.h)
// This file is part of the MOOSE framework
// https://www.mooseframework.org
//
// All rights reserved, see COPYRIGHT for full restrictions
// https://github.com/idaholab/moose/blob/master/COPYRIGHT
//
// Licensed under LGPL 2.1, please see LICENSE for details
// https://www.gnu.org/licenses/lgpl-2.1.html
#pragma once
#include "INSFVMomentumAdvection.h"
/**
* A flux kernel transporting mass across cell faces
*/
class INSFVMassAdvection : public INSFVMomentumAdvection
{
public:
static InputParameters validParams();
INSFVMassAdvection(const InputParameters & params);
protected:
ADReal computeQpResidual() override;
};
(modules/navier_stokes/include/fvkernels/INSFVScalarFieldAdvection.h)
// This file is part of the MOOSE framework
// https://www.mooseframework.org
//
// All rights reserved, see COPYRIGHT for full restrictions
// https://github.com/idaholab/moose/blob/master/COPYRIGHT
//
// Licensed under LGPL 2.1, please see LICENSE for details
// https://www.gnu.org/licenses/lgpl-2.1.html
#pragma once
#include "INSFVMomentumAdvection.h"
/**
* An advection kernel that implements interpolation schemes specific to Navier-Stokes flow
* physics and that advects arbitrary scalar quantities
*/
class INSFVScalarFieldAdvection : public INSFVMomentumAdvection
{
public:
static InputParameters validParams();
INSFVScalarFieldAdvection(const InputParameters & params);
};
(modules/navier_stokes/include/fvkernels/INSFVEnergyAdvection.h)
// This file is part of the MOOSE framework
// https://www.mooseframework.org
//
// All rights reserved, see COPYRIGHT for full restrictions
// https://github.com/idaholab/moose/blob/master/COPYRIGHT
//
// Licensed under LGPL 2.1, please see LICENSE for details
// https://www.gnu.org/licenses/lgpl-2.1.html
#pragma once
#include "INSFVMomentumAdvection.h"
/**
* An advection kernel that implements interpolation schemes specific to Navier-Stokes flow
* physics
*/
class INSFVEnergyAdvection : public INSFVMomentumAdvection
{
public:
static InputParameters validParams();
INSFVEnergyAdvection(const InputParameters & params);
};
(modules/navier_stokes/include/fvkernels/PINSFVMomentumAdvection.h)
// This file is part of the MOOSE framework
// https://www.mooseframework.org
//
// All rights reserved, see COPYRIGHT for full restrictions
// https://github.com/idaholab/moose/blob/master/COPYRIGHT
//
// Licensed under LGPL 2.1, please see LICENSE for details
// https://www.gnu.org/licenses/lgpl-2.1.html
#pragma once
#include "MooseVariableFV.h"
#include "INSFVMomentumAdvection.h"
/**
* A flux kernel transporting momentum in porous media across cell faces
*/
class PINSFVMomentumAdvection : public INSFVMomentumAdvection
{
public:
static InputParameters validParams();
PINSFVMomentumAdvection(const InputParameters & params);
protected:
/**
* interpolation overload for the velocity
*/
void interpolate(Moose::FV::InterpMethod m,
ADRealVectorValue & interp_v,
const ADRealVectorValue & elem_v,
const ADRealVectorValue & neighbor_v) override;
virtual ADReal computeQpResidual() override;
VectorValue<ADReal> coeffCalculator(const Elem & elem, const ADReal & mu) const override;
/// porosity variable to compute gradients
const MooseVariableFV<Real> * const _eps_var;
/// porosity in the current element
const VariableValue & _eps;
/// porosity in the neighbor element
const VariableValue & _eps_neighbor;
/// Whether the porosity field is smooth or has discontinuities
const bool _smooth_porosity;
};