INSFVBodyForce

This object implements both the functionalities as FVBodyForce and FVCoupledForce but it's dedicated to use in the Navier-Stokes momentum equation.

A body force in the momentum equation can be a momentum source, like a pump, or a momentum sink, like a volumetric friction term. Friction terms may also be modeled with PINSFVMomentumFriction.

Example input syntax

In this example, the INSFVBodyForce is used to apply a forcing function to the momentum equation in a method of manufactured solution study.

[FVKernels]
  [mass]
    type = INSFVMassAdvection
    variable = pressure
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
  []
  [mass_forcing]
    type = FVBodyForce
    variable = pressure
    function = forcing_p
  []

  [u_advection]
    type = INSFVMomentumAdvection
    variable = u
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = INSFVMomentumDiffusion
    variable = u
    mu = ${mu}
    momentum_component = 'x'
  []
  [u_pressure]
    type = INSFVMomentumPressure
    variable = u
    momentum_component = 'x'
    pressure = pressure
  []
  [u_forcing]
    type = INSFVBodyForce
    variable = u
    functor = forcing_u
    momentum_component = 'x'
  []

  [v_advection]
    type = INSFVMomentumAdvection
    variable = v
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = v
    mu = ${mu}
    momentum_component = 'y'
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = v
    momentum_component = 'y'
    pressure = pressure
  []
  [v_forcing]
    type = INSFVBodyForce
    variable = v
    functor = forcing_v
    momentum_component = 'y'
  []
[]

Input Parameters

momentum_componentThe component of the momentum equation that this kernel applies to.
C++ Type:MooseEnum
Options:x, y, z
Controllable:No
Description:The component of the momentum equation that this kernel applies to.
rhie_chow_user_objectThe rhie-chow user-object
C++ Type:UserObjectName
Controllable:No
Description:The rhie-chow user-object
variableThe name of the variable that this residual object operates on
C++ Type:NonlinearVariableName
Controllable:No
Description:The name of the variable that this residual object operates on

Required Parameters

blockThe list of blocks (ids or names) that this object will be applied
C++ Type:std::vector<SubdomainName>
Controllable:No
Description:The list of blocks (ids or names) that this object will be applied
functor1A functor that describes the body force
Default:1
C++ Type:MooseFunctorName
Controllable:No
Description:A functor that describes the body force
postprocessor1A postprocessor whose value is multiplied by the body force
Default:1
C++ Type:PostprocessorName
Controllable:No
Description:A postprocessor whose value is multiplied by the body force
prop_getter_suffixAn optional suffix parameter that can be appended to any attempt to retrieve/get material properties. The suffix will be prepended with a '_' character.
C++ Type:MaterialPropertyName
Controllable:No
Description:An optional suffix parameter that can be appended to any attempt to retrieve/get material properties. The suffix will be prepended with a '_' character.
scaling_factor1Coefficient to multiply by the body force term
Default:1
C++ Type:double
Controllable:Yes
Description:Coefficient to multiply by the body force term

Optional Parameters

absolute_value_vector_tagsThe tags for the vectors this residual object should fill with the absolute value of the residual contribution
C++ Type:std::vector<TagName>
Controllable:No
Description:The tags for the vectors this residual object should fill with the absolute value of the residual contribution
extra_matrix_tagsThe extra tags for the matrices this Kernel should fill
C++ Type:std::vector<TagName>
Controllable:No
Description:The extra tags for the matrices this Kernel should fill
extra_vector_tagsThe extra tags for the vectors this Kernel should fill
C++ Type:std::vector<TagName>
Controllable:No
Description:The extra tags for the vectors this Kernel should fill
matrix_tagssystemThe tag for the matrices this Kernel should fill
Default:system
C++ Type:MultiMooseEnum
Options:nontime, system
Controllable:No
Description:The tag for the matrices this Kernel should fill
vector_tagsnontimeThe tag for the vectors this Kernel should fill
Default:nontime
C++ Type:MultiMooseEnum
Options:nontime, time
Controllable:No
Description:The tag for the vectors this Kernel should fill

Tagging Parameters

control_tagsAdds user-defined labels for accessing object parameters via control logic.
C++ Type:std::vector<std::string>
Controllable:No
Description:Adds user-defined labels for accessing object parameters via control logic.
enableTrueSet the enabled status of the MooseObject.
Default:True
C++ Type:bool
Controllable:Yes
Description:Set the enabled status of the MooseObject.
implicitTrueDetermines whether this object is calculated using an implicit or explicit form
Default:True
C++ Type:bool
Controllable:No
Description:Determines whether this object is calculated using an implicit or explicit form
seed0The seed for the master random number generator
Default:0
C++ Type:unsigned int
Controllable:No
Description:The seed for the master random number generator
use_displaced_meshFalseWhether or not this object should use the displaced mesh for computation. Note that in the case this is true but no displacements are provided in the Mesh block the undisplaced mesh will still be used.
Default:False
C++ Type:bool
Controllable:No
Description:Whether or not this object should use the displaced mesh for computation. Note that in the case this is true but no displacements are provided in the Mesh block the undisplaced mesh will still be used.

Advanced Parameters

ghost_layers1The number of layers of elements to ghost.
Default:1
C++ Type:unsigned short
Controllable:No
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
Controllable:No
Description:Whether to use point neighbors, which introduces additional ghosting to that used for simple face neighbors.

Parallel Ghosting Parameters

(moose/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
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
  []
[]

[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}
    rho = ${rho}
  []
  [mass_forcing]
    type = FVBodyForce
    variable = pressure
    function = forcing_p
  []

  [u_advection]
    type = INSFVMomentumAdvection
    variable = u
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = INSFVMomentumDiffusion
    variable = u
    mu = ${mu}
    momentum_component = 'x'
  []
  [u_pressure]
    type = INSFVMomentumPressure
    variable = u
    momentum_component = 'x'
    pressure = pressure
  []
  [u_forcing]
    type = INSFVBodyForce
    variable = u
    functor = forcing_u
    momentum_component = 'x'
  []

  [v_advection]
    type = INSFVMomentumAdvection
    variable = v
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = v
    mu = ${mu}
    momentum_component = 'y'
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = v
    momentum_component = 'y'
    pressure = pressure
  []
  [v_forcing]
    type = INSFVBodyForce
    variable = v
    functor = forcing_v
    momentum_component = 'y'
  []
[]

[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'
  []
[]

[Functions]
  [exact_u]
    type = ParsedFunction
    expression = 'sin((1/2)*y*pi)*cos((1/2)*x*pi)'
  []
  [exact_rhou]
    type = ParsedFunction
    expression = 'rho*sin((1/2)*y*pi)*cos((1/2)*x*pi)'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
  [forcing_u]
    type = ParsedFunction
    expression = '(1/2)*pi^2*mu*sin((1/2)*y*pi)*cos((1/2)*x*pi) - '
            '1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi) + '
            '(1/2)*pi*rho*sin((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)^2 - '
            'pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi) - '
            '1/4*pi*sin((1/4)*x*pi)*sin((3/2)*y*pi)'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [exact_v]
    type = ParsedFunction
    expression = 'sin((1/4)*x*pi)*cos((1/2)*y*pi)'
  []
  [exact_rhov]
    type = ParsedFunction
    expression = 'rho*sin((1/4)*x*pi)*cos((1/2)*y*pi)'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
  [forcing_v]
    type = ParsedFunction
    expression = '(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)'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [exact_p]
    type = ParsedFunction
    expression = 'sin((3/2)*y*pi)*cos((1/4)*x*pi)'
  []
  [forcing_p]
    type = ParsedFunction
    expression = '-1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi) - '
            '1/2*pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type -pc_factor_mat_solver_type'
  petsc_options_value = 'lu       NONZERO               superlu_dist'
  nl_rel_tol = 1e-12
[]

[Outputs]
  csv = true
[]

[Postprocessors]
  [h]
    type = AverageElementSize
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2u]
    type = ElementL2FunctorError
    approximate = u
    exact = exact_u
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2v]
    type = ElementL2FunctorError
    approximate = v
    exact = exact_v
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2p]
    type = ElementL2FunctorError
    approximate = pressure
    exact = exact_p
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
[]

Example input syntax
Input Parameters