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foam-extend4.1-coherent-io/tutorials/incompressible/MRFSimpleFoam/axialTurbine_mixingPlane/system/fvSolution
2017-08-11 20:22:17 +01:00

67 lines
1.8 KiB
C++

/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | foam-extend: Open Source CFD |
| \\ / O peration | Version: 4.0 |
| \\ / A nd | Web: http://www.foam-extend.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
// For meshes with
// disparities in angle span across the mixingPlane interface, a
// solver for asymmetrical matrices is required, like BiCGStab. When
// in doubt, just select a solver for asymmetrical matrices for p.
p
{
solver BiCGStab;
preconditioner DILU;
tolerance 1e-08;
relTol 0.05;
}
U
{
solver BiCGStab;
preconditioner DILU;
tolerance 1e-07;
relTol 0.1;
}
k
{
solver BiCGStab;
preconditioner DILU;
tolerance 1e-07;
relTol 0.1;
}
epsilon
{
solver BiCGStab;
preconditioner DILU;
tolerance 1e-07;
relTol 0.1;
}
}
SIMPLE
{
nNonOrthogonalCorrectors 0;
}
relaxationFactors
{
p 0.3;
U 0.7;
k 0.7;
epsilon 0.7;
}
// ************************************************************************* //