/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | foam-extend: Open Source CFD |
| \\ / O peration | Version: 3.2 |
| \\ / 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
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;
fluxRequired
default no;
p;
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)
// ************************************************************************* //