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

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/*--------------------------------*- 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 volVectorField;
location "0";
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (26.3389 0 6.5036);
boundaryField
{
OversetFaces
{
type overset;
value uniform (0 0 0);
coupledFringe yes;
setHoleCellValue yes;
holeCellValue (0 0 0);
}
Inflow
{
type fixedValue;
value uniform (26.3389 0 6.5036);
}
Outflow
{
type inletOutlet;
inletValue uniform (0 0 0);
value uniform (0 0 0);
}
Lower
{
type fixedValue;
value uniform (26.3389 0 6.5036);
}
Upper
{
type inletOutlet;
inletValue uniform (0 0 0);
value uniform (0 0 0);
}
airfoil
{
type fixedValue;
value uniform (0 0 0);
}
frontAndBack
{
type empty;
}
OversetMiddle
{
type emptyOverset;
value uniform (0 0 0);
}
OversetFront
{
type emptyOverset;
value uniform (0 0 0);
}
}
// ************************************************************************* //