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foam-extend4.1-coherent-io/validationAndVerificationSuite/validation/overset/NACA4412-airfoil/implicitConservativeOverset/0/omega

90 lines
2 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 | For copyright notice see file Copyright |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object omega;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 -1 0 0 0 0];
internalField uniform 0.42797;
boundaryField
{
OversetFaces
{
type overset;
value uniform 0.42797;
coupledFringe yes;
setHoleCellValue yes;
holeCellValue 0.42797;
}
Inflow
{
type fixedValue;
value uniform 0.42797;
}
Outflow
{
type inletOutlet;
inletValue uniform 0.42797;
value uniform 0.42797;
}
Lower
{
type fixedValue;
value uniform 0.42797;
}
Upper
{
type inletOutlet;
inletValue uniform 0.42797;
value uniform 0.42797;
}
frontAndBack
{
type empty;
}
airfoil
{
type omegaWallFunction;
refValue uniform 0;
value uniform 0.42797;
Cmu 0.09;
kappa 0.41;
E 9.8;
beta1 0.075;
}
OversetMiddle
{
type emptyOverset;
value uniform 0.42797;
}
OversetFront
{
type emptyOverset;
value uniform 0.42797;
}
}
// ************************************************************************* //