Files
openfoam/tutorials/compressible/sonicFoam/ras/nacaAirfoil/0/U

52 lines
1.4 KiB
C++

/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volVectorField;
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (600 148.16 0);
boundaryField
{
INLE1
{
type supersonicFreestream;
pInf 100000;
TInf 300;
UInf (600 148.16 0);
gamma 1.4;
value uniform (600 148.16 0);
}
OUTL2
{
type inletOutlet;
inletValue uniform (600 148.16 0);
value uniform (600 148.16 0);
}
SYMP3
{
type empty;
}
WALL10
{
type noSlip;
}
}
// ************************************************************************* //