SpalartAllmaras.H

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Class
    Foam::compressible::RASModels::SpalartAllmaras

Description
    Spalart-Allmaras one-eqn mixing-length model for compressible
    external flows.

    Reference:
    @verbatim
        "A One-Equation Turbulence Model for Aerodynamic Flows"
        P.R. Spalart,
        S.R. Allmaras,
        La Recherche Aerospatiale, No. 1, 1994, pp. 5--21.

        Extended according to:

        "An Unstructured Grid Generation and Adaptive Solution Technique
        for High Reynolds Number Compressible Flows"
        G.A. Ashford,
        Ph.D. thesis, University of Michigan, 1996.
    @endverbatim

    The default model coefficients correspond to the following:
    @verbatim
        SpalartAllmarasCoeffs
        {
            Cb1         0.1355;
            Cb2         0.622;
            Cw2         0.3;
            Cw3         2.0;
            Cv1         7.1;
            Cv2         5.0;
            sigmaNut    0.66666;
            Prt         1.0;    // only for compressible
            kappa       0.41;
        }
    @endverbatim

SourceFiles
    SpalartAllmaras.C
    SpalartAllmarasCorrect.C

\*---------------------------------------------------------------------------*/

#ifndef compressibleSpalartAllmaras_H
#define combressibleSpalartAllmaras_H

#include <compressibleRASModels/RASModel.H>
#include <finiteVolume/wallDist.H>

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

namespace Foam
{
namespace compressible
{
namespace RASModels
{

/*---------------------------------------------------------------------------*\
                      Class SpalartAllmaras Declaration
\*---------------------------------------------------------------------------*/

class SpalartAllmaras
:
    public RASModel
{
    // Private data

        // Model coefficients

            dimensionedScalar sigmaNut_;
            dimensionedScalar kappa_;
            dimensionedScalar Prt_;

            dimensionedScalar Cb1_;
            dimensionedScalar Cb2_;
            dimensionedScalar Cw1_;
            dimensionedScalar Cw2_;
            dimensionedScalar Cw3_;
            dimensionedScalar Cv1_;
            dimensionedScalar Cv2_;


        // Fields

            volScalarField nuTilda_;
            volScalarField mut_;
            volScalarField alphat_;


        //- Wall distance
        wallDist d_;


    // Private member functions

        tmp<volScalarField> chi() const;
        tmp<volScalarField> fv1(const volScalarField& chi) const;
        tmp<volScalarField> fv2
        (
            const volScalarField& chi,
            const volScalarField& fv1
        ) const;
        tmp<volScalarField> fv3
        (
            const volScalarField& chi,
            const volScalarField& fv1
        ) const;
        tmp<volScalarField> fw(const volScalarField& Stilda) const;


public:

    //- Runtime type information
    TypeName("SpalartAllmaras");


    // Constructors

        //- Construct from components
        SpalartAllmaras
        (
            const volScalarField& rho,
            const volVectorField& U,
            const surfaceScalarField& phi,
            const basicThermo& thermophysicalModel
        );


    //- Destructor
    virtual ~SpalartAllmaras()
    {}


    // Member Functions

        //- Return the effective diffusivity for nuTilda
        tmp<volScalarField> DnuTildaEff() const
        {
            return tmp<volScalarField>
            (
                new volScalarField
                (
                    "DnuTildaEff",
                    rho_*nuTilda_/sigmaNut_ + mu()
                )
            );
        }

        //- Return the turbulence viscosity
        virtual tmp<volScalarField> mut() const
        {
            return mut_;
        }

        //- Return the effective turbulent thermal diffusivity
        virtual tmp<volScalarField> alphaEff() const
        {
            return tmp<volScalarField>
            (
                new volScalarField("alphaEff", alphat_ + alpha())
            );
        }

        //- Return the turbulence kinetic energy
        virtual tmp<volScalarField> k() const
        {
            return tmp<volScalarField>
            (
                new volScalarField
                (
                    IOobject
                    (
                        "k",
                        runTime_.timeName(),
                        mesh_
                    ),
                    mesh_,
                    dimensionedScalar("0", dimensionSet(0, 2, -2, 0, 0), 0)
                )
            );
        }

        //- Return the turbulence kinetic energy dissipation rate
        virtual tmp<volScalarField> epsilon() const
        {
            return tmp<volScalarField>
            (
                new volScalarField
                (
                    IOobject
                    (
                        "epslion",
                        runTime_.timeName(),
                        mesh_
                    ),
                    mesh_,
                    dimensionedScalar("0", dimensionSet(0, 2, -3, 0, 0), 0)
                )
            );
        }

        //- Return the Reynolds stress tensor
        virtual tmp<volSymmTensorField> R() const;

        //- Return the effective stress tensor including the laminar stress
        virtual tmp<volSymmTensorField> devRhoReff() const;

        //- Return the source term for the momentum equation
        virtual tmp<fvVectorMatrix> divDevRhoReff(volVectorField& U) const;

        //- Solve the turbulence equations and correct the turbulence viscosity
        virtual void correct();

        //- Read RASProperties dictionary
        virtual bool read();
};


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

} // End namespace RASModels
} // End namespace compressible
} // End namespace Foam

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

#endif

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