FoamFile
{
    version     2.0;
    format      ascii;
    class       volVectorField;
    object      U;
}

dimensions      [0 1 -1 0 0 0 0];

Uinf		0.05;
aoa		45;

radAoa		#eval {degToRad($aoa)};

internalField   uniform (#eval{$Uinf * cos($radAoa)} #eval{$Uinf * sin($radAoa)} 0);

boundaryField
{
    inlet
    {
        type            fixedValue;
        value           $internalField;
    }
    outlet
    {
        type            zeroGradient;
    }

    flap
    {
        type            movingWallVelocity;
	value		uniform (0 0 0);
    }

    airfoil
    {
        type            noSlip;
    }

    defaultFaces
    {
        type            empty;
    }
}
