openfoam/tutorials/combustion/engineFoam/kivaTest/system/fvSchemes

82 lines
2.1 KiB
C++

/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default Euler;
}
gradSchemes
{
default Gauss linear;
}
divSchemes
{
default none;
div(phi,U) Gauss upwind;
div(phi,K) Gauss upwind;
div(phid,p) Gauss upwind;
div(meshPhi,p) Gauss upwind;
div(phiv,p) Gauss upwind;
div(phi,k) Gauss upwind;
div(phi,epsilon) Gauss upwind;
div(phi,R) Gauss upwind;
div(R) Gauss linear;
div(phiXi,Xi) Gauss upwind;
div(phiXi,Su) Gauss upwind;
div(phiSt,b) Gauss limitedLinear01 1;
div(phi,ft_b_ha_hau) Gauss multivariateSelection
{
fu limitedLinear01 1;
ft limitedLinear01 1;
b limitedLinear01 1;
ha limitedLinear 1;
hau limitedLinear 1;
ea limitedLinear 1;
eau limitedLinear 1;
};
div(U) Gauss linear;
div((Su*grad(b))) Gauss linear;
div((U+((Su*Xi)*grad(b)))) Gauss linear;
div((muEff*dev2(T(grad(U))))) Gauss linear;
}
laplacianSchemes
{
default Gauss linear limited corrected 0.5;
}
interpolationSchemes
{
default linear;
}
snGradSchemes
{
default limited corrected 0.5;
}
fluxRequired
{
default no;
p ;
}
// ************************************************************************* //