HeatStructure2DCoupler

This component couples two 2D heat structures via a heat transfer coefficient.

Usage

This component has the following restrictions:

  • The coupled heat structures must be 2D heat structures.

  • The coupled heat structures must be of the same type.

  • Only one boundary name may be provided in each of the "primary_boundary" and "secondary_boundary" parameters.

  • The meshes along the coupled boundaries must be coincident, i.e., each node on each side must be at an identical location as a node on the other side.

Input Parameters

  • heat_transfer_coefficientHeat transfer coefficient function [W/(m^2-K)]

    C++ Type:FunctionName

    Controllable:No

    Description:Heat transfer coefficient function [W/(m^2-K)]

  • primary_boundaryThe boundary of the first heat structure to couple

    C++ Type:BoundaryName

    Controllable:No

    Description:The boundary of the first heat structure to couple

  • primary_heat_structureThe first heat structure to couple

    C++ Type:std::string

    Controllable:No

    Description:The first heat structure to couple

  • secondary_boundaryThe boundary of the second heat structure to couple

    C++ Type:BoundaryName

    Controllable:No

    Description:The boundary of the second heat structure to couple

  • secondary_heat_structureThe second heat structure to couple

    C++ Type:std::string

    Controllable:No

    Description:The second heat structure to couple

Required 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:No

    Description:Set the enabled status of the MooseObject.

Advanced Parameters

Formulation

The heat conduction equation is the following: where

  • is density,

  • is specific heat capacity,

  • is thermal conductivity,

  • is temperature, and

  • is a volumetric heat source.

Multiplying by a test function and integrating by parts over the domain gives where is the boundary of the domain .

For Neumann boundary conditions on the boundary , is replaced with a known incoming heat flux function :

For the heat structure , the incoming boundary heat flux is computed as

where

  • is the heat transfer coefficient,

  • is the surface temperature of the heat structure , and

  • is the surface temperature of the coupled heat structure .

Input Files