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foam-extend4.1-coherent-io/validationAndVerificationSuite/validation/overset/NACA4412-airfoil/oversetMeshes/middleMesh/system/fvSchemes

70 lines
1.8 KiB
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;
location "system";
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default steadyState;
}
gradSchemes
{
default Gauss linear;
grad(k) cellLimited Gauss linear 1;
grad(omega) cellLimited Gauss linear 1;
}
divSchemes
{
default none;
div(phi,U) bounded Gauss linearUpwind grad(U);//bounded Gauss limitedLinearV 1;
div((nuEff*dev(T(grad(U))))) Gauss linear;
div(phi,nuTilda) bounded Gauss upwind;//limitedLinear 1;
div(phi,k) bounded Gauss upwind;//limitedLinear 1;
div(phi,omega) bounded Gauss upwind;//limitedLinear 1;
div(phid,p) Gauss upwind;
div(phi,Ekp) bounded Gauss upwind;
div((phi|interpolate(rho)),p) Gauss upwind;
div(tauMC) Gauss linear;
}
laplacianSchemes
{
default Gauss linear corrected;
}
interpolationSchemes
{
default linear;
}
snGradSchemes
{
default corrected;
}
fluxRequired
{
default no;
p;
pCorr;
}
// ************************************************************************* //