[praveen]

I am having some problem with a NACA0012 test case using rhoCentralFoam. The freestream mach is 0.75 and there is a shock. I have attached some pictures. There is something wrong with the bcs.

Some of the input options are listed below. Other input files are same as here

http://gfoam.svn.sourceforge.net/vie...12_7k_M075_a2/

Hope somebody can point out the mistakes.

0/p

internalField   uniform 85418.9;

boundaryField
{
    inlet-outlet
    {
        type            fixedValue;
        value           uniform 85418.9;
    }

    body            
    {
        //type            slip;
        type            zeroGradient;
    }

    defaultFaces    
    {
        type            empty;
    }
}

0/T

internalField   uniform 260;

boundaryField
{
    inlet-outlet
    {
        type            fixedValue;
        value           uniform 260;
    }

    body            
    {
        //type            slip;
        type            zeroGradient;
    }

    defaultFaces    
    {
        type            empty;
    }
}

0/U

internalField   uniform (242.284 8.46075 0);

boundaryField
{
    inlet-outlet
    {
        type            fixedValue;
        value           uniform (242.284 8.46075 0);
    }

    body            
    {
        type            slip;
    }

    defaultFaces    
    {
        type            empty;
    }
}

constant/thermophysicalProperties

thermoType      ePsiThermo<pureMixture<constTransport<specieThermo<eConstThermo<perfectGas>>>>>;

mixture         air 1 28.965 717.625 0 0 0.72;