RAS turbulenceModels - document default coefficients for doxygen

- removed stray 'sourceFiles'
This commit is contained in:
Mark Olesen
2008-06-18 11:23:00 +02:00
parent 1efdd657bd
commit b2b498dbaf
18 changed files with 261 additions and 6 deletions

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@ -29,6 +29,24 @@ Description
Launder, Reece and Rodi Reynolds-stress turbulence model for
compressible flows.
The default model coefficients correspond to the following:
@verbatim
LRRCoeffs
{
Cmu 0.09;
Clrr1 1.8;
Clrr2 0.6;
C1 1.44;
C2 1.92;
Cs 0.25;
Ceps 0.15;
alphah 1.0; // only for compressible
alphaEps 0.76923;
alphaR 1.22; // only for compressible
couplingFactor 0.0; // only for incompressible
}
@endverbatim
SourceFiles
LRR.C
LRRcorrect.C

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@ -28,6 +28,26 @@ Class
Description
Launder-Gibson Reynolds stress turbulence model for compressible flows.
The default model coefficients correspond to the following:
@verbatim
LaunderGibsonRSTMCoeffs
{
Cmu 0.09;
Clg1 1.8;
Clg2 0.6;
C1 1.44;
C2 1.92;
C1Ref 0.5;
C2Ref 0.3;
Cs 0.25;
Ceps 0.15;
alphah 1.0; // only for compressible
alphaEps 0.76923;
alphaR 1.22;
couplingFactor 0.0;
}
@endverbatim
SourceFiles
LaunderGibsonRSTM.C
LaunderGibsonRSTMcorrect.C

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@ -29,6 +29,20 @@ Description
Launder and Sharma low-Reynolds k-epsilon turbulence model for
compressible and combusting flows.
The default model coefficients correspond to the following:
@verbatim
LaunderSharmaKECoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
C3 -0.33;
alphah 1.0; // only for compressible
alphahk 1.0; // only for compressible
alphaEps 0.76923;
}
@endverbatim
SourceFiles
LaunderSharmaKE.C
LaunderSharmaKECorrect.C

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@ -1,2 +0,0 @@
SOURCE = \
$(EXE_SRC)/RNGkEpsilon.C

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@ -28,6 +28,22 @@ Class
Description
Renormalisation group k-epsilon turbulence model for compressible flows.
The default model coefficients correspond to the following:
@verbatim
RNGkEpsilonCoeffs
{
Cmu 0.0845;
C1 1.42;
C2 1.68;
C3 -0.33; // only for compressible
alphah 1.0; // only for compressible
alphak 1.39;
alphaEps 1.39;
eta0 4.38;
beta 0.012;
}
@endverbatim
SourceFiles
RNGkEpsilon.C
RNGkEpsilonCorrect.C

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@ -1,2 +0,0 @@
SOURCE = \
$(EXE_SRC)/RNGkEpsilon.C

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@ -44,6 +44,21 @@ Description
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;
alphaNut 1.5;
alphah 1.0; // only for compressible
}
@endverbatim
SourceFiles
SpalartAllmaras.C
SpalartAllmarasCorrect.C

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@ -28,6 +28,20 @@ Class
Description
Standard k-epsilon turbulence model for compressible flows
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
alphak 1.0; // only for compressible
alphaEps 0.76923;
alphah 1.0; // only for compressible
}
@endverbatim
SourceFiles
kEpsilon.C
kEpsilonCorrect.C

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@ -39,7 +39,7 @@ Description
Note that this implementation is written in terms of alpha diffusion
coefficients rather than the more traditional sigma (alpha = 1/sigma) so
that the blending can be applied to all coefficuients in a consistent
manner. The paper suggests that sigma is blended but this woulf not be
manner. The paper suggests that sigma is blended but this would not be
consistent with the blending of the k-epsilon and k-omega models.
Also note that the error in the last term of equation (2) relating to
@ -52,6 +52,26 @@ Description
uncertainty in their origin, range of applicability and that is y+ becomes
sufficiently small blending u_tau in this manner clearly becomes nonsense.
The default model coefficients correspond to the following:
@verbatim
kOmegaSST
{
Cmu 0.09;
alphaK1 0.85034;
alphaK2 1.0;
alphaOmega1 0.5;
alphaOmega2 0.85616;
alphah 1.0; // only for compressible
beta1 0.075;
beta2 0.0828;
betaStar 0.09;
gamma1 0.5532;
gamma2 0.4403;
a1 0.31;
c1 10.0;
}
@endverbatim
SourceFiles
kOmegaSST.C
kOmegaWallFunctionsI.H

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@ -37,7 +37,20 @@ Description
Jiang Zhu
Computers and Fluids Vol. 24, No. 3, pp. 227-238, 1995
@endverbatim
The default model coefficients correspond to the following:
@verbatim
realizableKE
{
Cmu 0.09;
A0 4.0;
C2 1.9;
alphak 1.0;
alphaEps 0.833333;
alphah 1.0; // only for compressible
}
@endverbatim
SourceFiles
realizableKE.C

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@ -29,6 +29,24 @@ Description
Launder, Reece and Rodi Reynolds-stress turbulence model for
incompressible flows.
The default model coefficients correspond to the following:
@verbatim
LRRCoeffs
{
Cmu 0.09;
Clrr1 1.8;
Clrr2 0.6;
C1 1.44;
C2 1.92;
Cs 0.25;
Ceps 0.15;
alphah 1.0; // only for compressible
alphaEps 0.76923;
alphaR 1.22; // only for compressible
couplingFactor 0.0; // only for incompressible
}
@endverbatim
SourceFiles
LRR.C

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@ -28,6 +28,26 @@ Class
Description
Launder-Gibson Reynolds stress turbulence model for incompressible flows.
The default model coefficients correspond to the following:
@verbatim
LaunderGibsonRSTMCoeffs
{
Cmu 0.09;
Clg1 1.8;
Clg2 0.6;
C1 1.44;
C2 1.92;
C1Ref 0.5;
C2Ref 0.3;
Cs 0.25;
Ceps 0.15;
alphah 1.0; // only for compressible
alphaEps 0.76923;
alphaR 1.22;
couplingFactor 0.0;
}
@endverbatim
SourceFiles
LaunderGibsonRSTM.C

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@ -29,6 +29,20 @@ Description
Launder and Sharma low-Reynolds k-epsilon turbulence model for
incompressible flows.
The default model coefficients correspond to the following:
@verbatim
LaunderSharmaKECoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
C3 -0.33;
alphah 1.0; // only for compressible
alphahk 1.0; // only for compressible
alphaEps 0.76923;
}
@endverbatim
SourceFiles
LaunderSharmaKE.C

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@ -28,6 +28,22 @@ Class
Description
Renormalisation group k-epsilon turbulence model for incompressible flows.
The default model coefficients correspond to the following:
@verbatim
RNGkEpsilonCoeffs
{
Cmu 0.0845;
C1 1.42;
C2 1.68;
C3 -0.33; // only for compressible
alphah 1.0; // only for compressible
alphak 1.39;
alphaEps 1.39;
eta0 4.38;
beta 0.012;
}
@endverbatim
SourceFiles
RNGkEpsilon.C

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@ -42,7 +42,22 @@ Description
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;
alphaNut 1.5;
alphah 1.0; // only for compressible
}
@endverbatim
SourceFiles
SpalartAllmaras.C

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@ -28,6 +28,20 @@ Class
Description
Standard k-epsilon turbulence model for incompressible flows.
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
alphak 1.0; // only for compressible
alphaEps 0.76923;
alphah 1.0; // only for compressible
}
@endverbatim
SourceFiles
kEpsilon.C

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@ -53,6 +53,26 @@ Description
uncertainty in their origin, range of applicability and that is y+ becomes
sufficiently small blending u_tau in this manner clearly becomes nonsense.
The default model coefficients correspond to the following:
@verbatim
kOmegaSST
{
Cmu 0.09;
alphaK1 0.85034;
alphaK2 1.0;
alphaOmega1 0.5;
alphaOmega2 0.85616;
alphah 1.0; // only for compressible
beta1 0.075;
beta2 0.0828;
betaStar 0.09;
gamma1 0.5532;
gamma2 0.4403;
a1 0.31;
c1 10.0;
}
@endverbatim
SourceFiles
kOmegaSST.C
kOmegaWallFunctionsI.H

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@ -37,8 +37,20 @@ Description
Jiang Zhu
Computers and Fluids Vol. 24, No. 3, pp. 227-238, 1995
@verbatim
@endverbatim
The default model coefficients correspond to the following:
@verbatim
realizableKE
{
Cmu 0.09;
A0 4.0;
C2 1.9;
alphak 1.0;
alphaEps 0.833333;
alphah 1.0; // only for compressible
}
@endverbatim
SourceFiles
realizableKE.C