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foam-extend4.1-coherent-io/tutorials/incompressible/MRFSimpleFoam/axialTurbine_mixingPlane/system/fvSchemes
2018-06-01 18:11:37 +02:00

71 lines
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C++

/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | foam-extend: Open Source CFD |
| \\ / O peration | Version: 4.1 |
| \\ / A nd | Web: http://www.foam-extend.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default steadyState;
}
gradSchemes
{
default Gauss linear;
grad(p) Gauss linear;
grad(U) Gauss linear;
}
divSchemes
{
default none;
div(phi,U) Gauss limitedLinearV 1;
div(phi,k) Gauss limitedLinear 1;
div(phi,epsilon) Gauss limitedLinear 1;
div((nuEff*dev(T(grad(U))))) Gauss linear;
}
laplacianSchemes
{
default none;
laplacian(nuEff,U) Gauss linear corrected;
laplacian((1|A(U)),p) Gauss linear corrected;
laplacian(DkEff,k) Gauss linear corrected;
laplacian(DepsilonEff,epsilon) Gauss linear corrected;
}
interpolationSchemes
{
default linear;
interpolate(U) linear;
}
snGradSchemes
{
default corrected;
}
mixingPlane
{
default areaAveraging;
U areaAveraging;
p areaAveraging;
k fluxAveraging; //Transported variable
epsilon fluxAveraging; //Transported variable
//NOTE: Ideally, tangential velocity components should also be
//fluxAveraged, while keeping areaAveraging for normal velocity
//component (to preserve perfect mass conservation)
}
// ************************************************************************* //