foam-extend4.1-coherent-io/tutorials/compressible/sonicFoam/ras/nacaAirfoil/0/U

/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM Extend Project: Open Source CFD        |
|  \\    /   O peration     | Version:  1.6-ext                               |
|   \\  /    A nd           | Web:      www.extend-project.de                 |
|    \\/     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            fixedValue;
        value           uniform (0 0 0);
    }
}

// ************************************************************************* //