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RAS turbulenceModels - document default coefficients for doxygen
- removed stray 'sourceFiles'
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@ -29,6 +29,24 @@ Description
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Launder, Reece and Rodi Reynolds-stress turbulence model for
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compressible flows.
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The default model coefficients correspond to the following:
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@verbatim
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LRRCoeffs
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{
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Cmu 0.09;
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Clrr1 1.8;
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Clrr2 0.6;
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C1 1.44;
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C2 1.92;
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Cs 0.25;
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Ceps 0.15;
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alphah 1.0; // only for compressible
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alphaEps 0.76923;
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alphaR 1.22; // only for compressible
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couplingFactor 0.0; // only for incompressible
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}
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@endverbatim
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SourceFiles
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LRR.C
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LRRcorrect.C
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@ -28,6 +28,26 @@ Class
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Description
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Launder-Gibson Reynolds stress turbulence model for compressible flows.
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The default model coefficients correspond to the following:
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@verbatim
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LaunderGibsonRSTMCoeffs
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{
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Cmu 0.09;
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Clg1 1.8;
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Clg2 0.6;
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C1 1.44;
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C2 1.92;
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C1Ref 0.5;
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C2Ref 0.3;
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Cs 0.25;
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Ceps 0.15;
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alphah 1.0; // only for compressible
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alphaEps 0.76923;
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alphaR 1.22;
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couplingFactor 0.0;
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}
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@endverbatim
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SourceFiles
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LaunderGibsonRSTM.C
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LaunderGibsonRSTMcorrect.C
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@ -29,6 +29,20 @@ Description
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Launder and Sharma low-Reynolds k-epsilon turbulence model for
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compressible and combusting flows.
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The default model coefficients correspond to the following:
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@verbatim
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LaunderSharmaKECoeffs
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{
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Cmu 0.09;
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C1 1.44;
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C2 1.92;
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C3 -0.33;
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alphah 1.0; // only for compressible
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alphahk 1.0; // only for compressible
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alphaEps 0.76923;
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}
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@endverbatim
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SourceFiles
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LaunderSharmaKE.C
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LaunderSharmaKECorrect.C
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@ -1,2 +0,0 @@
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SOURCE = \
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$(EXE_SRC)/RNGkEpsilon.C
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@ -28,6 +28,22 @@ Class
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Description
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Renormalisation group k-epsilon turbulence model for compressible flows.
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The default model coefficients correspond to the following:
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@verbatim
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RNGkEpsilonCoeffs
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{
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Cmu 0.0845;
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C1 1.42;
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C2 1.68;
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C3 -0.33; // only for compressible
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alphah 1.0; // only for compressible
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alphak 1.39;
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alphaEps 1.39;
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eta0 4.38;
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beta 0.012;
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}
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@endverbatim
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SourceFiles
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RNGkEpsilon.C
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RNGkEpsilonCorrect.C
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@ -1,2 +0,0 @@
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SOURCE = \
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$(EXE_SRC)/RNGkEpsilon.C
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@ -44,6 +44,21 @@ Description
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Ph.D. thesis, University of Michigan, 1996.
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@endverbatim
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The default model coefficients correspond to the following:
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@verbatim
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SpalartAllmarasCoeffs
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{
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Cb1 0.1355;
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Cb2 0.622;
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Cw2 0.3;
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Cw3 2.0;
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Cv1 7.1;
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Cv2 5.0;
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alphaNut 1.5;
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alphah 1.0; // only for compressible
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}
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@endverbatim
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SourceFiles
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SpalartAllmaras.C
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SpalartAllmarasCorrect.C
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@ -28,6 +28,20 @@ Class
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Description
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Standard k-epsilon turbulence model for compressible flows
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The default model coefficients correspond to the following:
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@verbatim
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kEpsilonCoeffs
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{
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Cmu 0.09;
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C1 1.44;
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C2 1.92;
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C3 -0.33; // only for compressible
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alphak 1.0; // only for compressible
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alphaEps 0.76923;
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alphah 1.0; // only for compressible
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}
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@endverbatim
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SourceFiles
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kEpsilon.C
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kEpsilonCorrect.C
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@ -39,7 +39,7 @@ Description
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Note that this implementation is written in terms of alpha diffusion
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coefficients rather than the more traditional sigma (alpha = 1/sigma) so
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that the blending can be applied to all coefficuients in a consistent
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manner. The paper suggests that sigma is blended but this woulf not be
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manner. The paper suggests that sigma is blended but this would not be
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consistent with the blending of the k-epsilon and k-omega models.
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Also note that the error in the last term of equation (2) relating to
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@ -52,6 +52,26 @@ Description
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uncertainty in their origin, range of applicability and that is y+ becomes
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sufficiently small blending u_tau in this manner clearly becomes nonsense.
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The default model coefficients correspond to the following:
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@verbatim
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kOmegaSST
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{
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Cmu 0.09;
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alphaK1 0.85034;
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alphaK2 1.0;
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alphaOmega1 0.5;
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alphaOmega2 0.85616;
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alphah 1.0; // only for compressible
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beta1 0.075;
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beta2 0.0828;
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betaStar 0.09;
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gamma1 0.5532;
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gamma2 0.4403;
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a1 0.31;
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c1 10.0;
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}
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@endverbatim
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SourceFiles
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kOmegaSST.C
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kOmegaWallFunctionsI.H
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@ -37,7 +37,20 @@ Description
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Jiang Zhu
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Computers and Fluids Vol. 24, No. 3, pp. 227-238, 1995
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@endverbatim
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The default model coefficients correspond to the following:
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@verbatim
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realizableKE
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{
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Cmu 0.09;
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A0 4.0;
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C2 1.9;
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alphak 1.0;
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alphaEps 0.833333;
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alphah 1.0; // only for compressible
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}
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@endverbatim
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SourceFiles
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realizableKE.C
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@ -29,6 +29,24 @@ Description
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Launder, Reece and Rodi Reynolds-stress turbulence model for
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incompressible flows.
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The default model coefficients correspond to the following:
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@verbatim
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LRRCoeffs
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{
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Cmu 0.09;
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Clrr1 1.8;
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Clrr2 0.6;
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C1 1.44;
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C2 1.92;
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Cs 0.25;
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Ceps 0.15;
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alphah 1.0; // only for compressible
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alphaEps 0.76923;
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alphaR 1.22; // only for compressible
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couplingFactor 0.0; // only for incompressible
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}
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@endverbatim
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SourceFiles
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LRR.C
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@ -28,6 +28,26 @@ Class
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Description
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Launder-Gibson Reynolds stress turbulence model for incompressible flows.
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The default model coefficients correspond to the following:
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@verbatim
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LaunderGibsonRSTMCoeffs
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{
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Cmu 0.09;
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Clg1 1.8;
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Clg2 0.6;
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C1 1.44;
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C2 1.92;
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C1Ref 0.5;
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C2Ref 0.3;
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Cs 0.25;
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Ceps 0.15;
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alphah 1.0; // only for compressible
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alphaEps 0.76923;
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alphaR 1.22;
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couplingFactor 0.0;
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}
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@endverbatim
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SourceFiles
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LaunderGibsonRSTM.C
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@ -29,6 +29,20 @@ Description
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Launder and Sharma low-Reynolds k-epsilon turbulence model for
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incompressible flows.
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The default model coefficients correspond to the following:
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@verbatim
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LaunderSharmaKECoeffs
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{
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Cmu 0.09;
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C1 1.44;
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C2 1.92;
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C3 -0.33;
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alphah 1.0; // only for compressible
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alphahk 1.0; // only for compressible
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alphaEps 0.76923;
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}
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@endverbatim
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SourceFiles
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LaunderSharmaKE.C
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@ -28,6 +28,22 @@ Class
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Description
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Renormalisation group k-epsilon turbulence model for incompressible flows.
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The default model coefficients correspond to the following:
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@verbatim
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RNGkEpsilonCoeffs
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{
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Cmu 0.0845;
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C1 1.42;
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C2 1.68;
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C3 -0.33; // only for compressible
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alphah 1.0; // only for compressible
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alphak 1.39;
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alphaEps 1.39;
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eta0 4.38;
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beta 0.012;
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}
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@endverbatim
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SourceFiles
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RNGkEpsilon.C
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@ -42,7 +42,22 @@ Description
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for High Reynolds Number Compressible Flows"
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G.A. Ashford,
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Ph.D. thesis, University of Michigan, 1996.
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@endverbatim
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The default model coefficients correspond to the following:
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@verbatim
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SpalartAllmarasCoeffs
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{
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Cb1 0.1355;
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Cb2 0.622;
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Cw2 0.3;
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Cw3 2.0;
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Cv1 7.1;
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Cv2 5.0;
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alphaNut 1.5;
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alphah 1.0; // only for compressible
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}
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@endverbatim
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SourceFiles
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SpalartAllmaras.C
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@ -28,6 +28,20 @@ Class
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Description
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Standard k-epsilon turbulence model for incompressible flows.
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The default model coefficients correspond to the following:
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@verbatim
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kEpsilonCoeffs
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{
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Cmu 0.09;
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C1 1.44;
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C2 1.92;
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C3 -0.33; // only for compressible
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alphak 1.0; // only for compressible
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alphaEps 0.76923;
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alphah 1.0; // only for compressible
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}
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@endverbatim
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SourceFiles
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kEpsilon.C
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@ -53,6 +53,26 @@ Description
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uncertainty in their origin, range of applicability and that is y+ becomes
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sufficiently small blending u_tau in this manner clearly becomes nonsense.
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The default model coefficients correspond to the following:
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@verbatim
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kOmegaSST
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{
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Cmu 0.09;
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alphaK1 0.85034;
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alphaK2 1.0;
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alphaOmega1 0.5;
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alphaOmega2 0.85616;
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alphah 1.0; // only for compressible
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beta1 0.075;
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beta2 0.0828;
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betaStar 0.09;
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gamma1 0.5532;
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gamma2 0.4403;
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a1 0.31;
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c1 10.0;
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}
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@endverbatim
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SourceFiles
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kOmegaSST.C
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kOmegaWallFunctionsI.H
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@ -37,8 +37,20 @@ Description
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Jiang Zhu
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Computers and Fluids Vol. 24, No. 3, pp. 227-238, 1995
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@verbatim
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@endverbatim
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The default model coefficients correspond to the following:
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@verbatim
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realizableKE
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{
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Cmu 0.09;
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A0 4.0;
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C2 1.9;
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alphak 1.0;
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alphaEps 0.833333;
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alphah 1.0; // only for compressible
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}
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@endverbatim
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SourceFiles
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realizableKE.C
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