619f1c55d8
See tutorials/compressible/rhoSimpleFoam/squareBend
SIMPLE
{
nNonOrthogonalCorrectors 0;
rhoMin 0.1;
rhoMax 1.0;
transonic yes;
consistent yes;
residualControl
{
p 1e-3;
U 1e-4;
e 1e-3;
// possibly check turbulence fields
"(k|epsilon|omega)" 1e-3;
}
}
relaxationFactors
{
fields
{
p 1;
rho 1;
}
equations
{
p 1;
U 0.9;
e 0.9;
k 0.9;
epsilon 0.9;
}
}
65 lines
1.6 KiB
C++
65 lines
1.6 KiB
C++
/*--------------------------------*- C++ -*----------------------------------*\
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| ========= | |
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| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
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| \\ / O peration | Version: dev |
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| \\ / A nd | Web: www.OpenFOAM.org |
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| \\/ M anipulation | |
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\*---------------------------------------------------------------------------*/
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FoamFile
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{
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version 2.0;
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format ascii;
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class dictionary;
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location "system";
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object fvSchemes;
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}
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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ddtSchemes
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{
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default steadyState;
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}
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gradSchemes
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{
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default Gauss linear;
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}
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divSchemes
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{
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default none;
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div(phi,U) bounded Gauss upwind;
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div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;
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div(phi,e) bounded Gauss upwind;
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div(phi,epsilon) bounded Gauss upwind;
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div(phi,k) bounded Gauss upwind;
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div(phid,p) Gauss upwind;
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div(phi,Ekp) bounded Gauss upwind;
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div((phi|interpolate(rho)),p) Gauss upwind;
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}
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laplacianSchemes
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{
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default Gauss linear corrected;
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}
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interpolationSchemes
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{
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default linear;
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}
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snGradSchemes
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{
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default corrected;
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}
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fluxRequired
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{
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default no;
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p;
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pCorr;
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}
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// ************************************************************************* //
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