[mechkween]

Hi all,
I'm trying to modify and build a version of k-omega SST (compressible) where I need to compute temperature gradients to evaluate and construct a new turbulent Prandtl number. I'm not sure how to get the turbulence solver to read in the temperature field to perform the processing. I tried adding T using:

 

rhoKOmegaSSTAlt
        (   
            const volScalarField& rho,
            const volVectorField& U,
            const surfaceScalarField& phi,
            const volScalarField& T,
            const fluidThermo& thermophysicalModel,
            const word& turbulenceModelName = turbulenceModel::typeName,
            const word& modelName = typeName
        );

but the compilation fails saying no matching function call which leads me to RASModel.H where the T line doesn't exist. I could modify that as well but seems like a complicated thing. Is there a simpler way to read the temperature field into the solver?


Thanks