/*---------------------------------------------------------------------------*\ ========= | \\ / F ield | foam-extend: Open Source CFD \\ / O peration | Version: 4.0 \\ / A nd | Web: http://www.foam-extend.org \\/ M anipulation | For copyright notice see file Copyright ------------------------------------------------------------------------------- License This file is part of foam-extend. foam-extend is free software: you can redistribute it and/or modify it under the terms of the GNU General Public License as published by the Free Software Foundation, either version 3 of the License, or (at your option) any later version. foam-extend is distributed in the hope that it will be useful, but WITHOUT ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License for more details. You should have received a copy of the GNU General Public License along with foam-extend. If not, see . Class Foam::compressible::RASModels::PDRkEpsilon Description Standard k-epsilon turbulence model with additional source terms corresponding to PDR basic drag model (\link basic.H \endlink) The default model coefficients correspond to the following: @verbatim kEpsilonCoeffs { Cmu 0.09; C1 1.44; C2 1.92; C3 -0.33; // only for compressible sigmak 1.0; // only for compressible sigmaEps 1.3; Prt 1.0; // only for compressible } @endverbatim The turbulence source term \f$ G_{R} \f$ appears in the \f$ \kappa-\epsilon \f$ equation for the generation of turbulence due to interaction with unresolved obstacles. In the \f$ \epsilon \f$ equation \f$ C_{1} G_{R} \f$ is added as a source term. In the \f$ \kappa \f$ equation \f$ G_{R} \f$ is added as a source term. SourceFiles PDRkEpsilon.C PDRkEpsilonCorrect.C \*---------------------------------------------------------------------------*/ #ifndef compressiblePDRkEpsilon_H #define compressiblePDRkEpsilon_H #include "RASModel.H" // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // namespace Foam { namespace compressible { namespace RASModels { /*---------------------------------------------------------------------------*\ Class PDRkEpsilon Declaration \*---------------------------------------------------------------------------*/ class PDRkEpsilon : public RASModel { // Private data // Model coefficients dimensionedScalar Cmu_; dimensionedScalar C1_; dimensionedScalar C2_; dimensionedScalar sigmak_; dimensionedScalar sigmaEps_; dimensionedScalar Prt_; // Fields volScalarField k_; volScalarField epsilon_; volScalarField mut_; volScalarField alphat_; public: //- Runtime type information TypeName("PDRkEpsilon"); // Constructors //- Construct from components PDRkEpsilon ( const volScalarField& rho, const volVectorField& U, const surfaceScalarField& phi, const basicThermo& thermophysicalModel ); //- Destructor virtual ~PDRkEpsilon() {} // Member Functions tmp mut() const { return mut_; } //- Return the effective diffusivity for k tmp DkEff() const { return tmp ( new volScalarField("DkEff", mut_/sigmak_ + mu()) ); } //- Return the effective diffusivity for epsilon tmp DepsilonEff() const { return tmp ( new volScalarField("DepsilonEff", mut_/sigmaEps_ + mu()) ); } //- Return the effective turbulent thermal diffusivity tmp alphaEff() const { return tmp ( new volScalarField("alphaEff", alphat_ + alpha()) ); } //- Return the turbulence kinetic energy tmp k() const { return k_; } //- Return the turbulence kinetic energy dissipation rate tmp epsilon() const { return epsilon_; } //- Return the Reynolds stress tensor tmp R() const; //- Return the effective stress tensor including the laminar stress tmp devRhoReff() const; //- Return the source term for the momentum equation tmp divDevRhoReff() const; //- Solve the turbulence equations and correct the turbulence viscosity void correct(); //- Read turbulenceProperties dictionary bool read(); }; // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // } // End namespace RASModels } // End namespace compressible } // End namespace Foam // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // #endif // ************************************************************************* //