openfoam/tutorials/mesh/snappyHexMesh/aerofoilNACA0012_directionalRefinement/system/fvSolution
2021-06-08 20:14:09 +00:00

67 lines
1.5 KiB
C++

/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: v2012 |
| \\ / A nd | Website: www.openfoam.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
p
{
solver GAMG;
smoother GaussSeidel;
tolerance 1e-6;
relTol 0.01;
}
"(U|k|omega|e)"
{
solver PBiCGStab;
preconditioner DILU;
tolerance 1e-6;
relTol 0.1;
}
}
SIMPLE
{
residualControl
{
p 1e-4;
U 1e-4;
"(k|omega|e)" 1e-4;
}
nNonOrthogonalCorrectors 0;
pMinFactor 0.1;
pMaxFactor 2;
}
relaxationFactors
{
fields
{
p 0.7;
rho 0.01;
}
equations
{
U 0.3;
e 0.7;
"(k|omega)" 0.7;
}
}
// ************************************************************************* //