Skip to content
GitLab
Projects
Groups
Snippets
/
Help
Help
Support
Community forum
Keyboard shortcuts
?
Submit feedback
Contribute to GitLab
Sign in / Register
Toggle navigation
Menu
Open sidebar
Development
openfoam
Commits
6a8880a9
Commit
6a8880a9
authored
Jun 18, 2008
by
Mark Olesen
Committed by
graham
Jun 18, 2008
Browse files
RAS turbulenceModels - document default coefficients for doxygen
- removed stray 'sourceFiles'
parent
5c957aa0
Changes
18
Hide whitespace changes
Inline
Side-by-side
src/turbulenceModels/RAS/compressible/LRR/LRR.H
View file @
6a8880a9
...
...
@@ -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
...
...
src/turbulenceModels/RAS/compressible/LaunderGibsonRSTM/LaunderGibsonRSTM.H
View file @
6a8880a9
...
...
@@ -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
...
...
src/turbulenceModels/RAS/compressible/LaunderSharmaKE/LaunderSharmaKE.H
View file @
6a8880a9
...
...
@@ -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
...
...
src/turbulenceModels/RAS/compressible/LaunderSharmaKE/sourceFiles
deleted
100644 → 0
View file @
5c957aa0
SOURCE = \
$(EXE_SRC)/RNGkEpsilon.C
src/turbulenceModels/RAS/compressible/RNGkEpsilon/RNGkEpsilon.H
View file @
6a8880a9
...
...
@@ -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
...
...
src/turbulenceModels/RAS/compressible/RNGkEpsilon/sourceFiles
deleted
100644 → 0
View file @
5c957aa0
SOURCE = \
$(EXE_SRC)/RNGkEpsilon.C
src/turbulenceModels/RAS/compressible/SpalartAllmaras/SpalartAllmaras.H
View file @
6a8880a9
...
...
@@ -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
...
...
src/turbulenceModels/RAS/compressible/kEpsilon/kEpsilon.H
View file @
6a8880a9
...
...
@@ -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
...
...
src/turbulenceModels/RAS/compressible/kOmegaSST/kOmegaSST.H
View file @
6a8880a9
...
...
@@ -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 woul
f
not be
manner. The paper suggests that sigma is blended but this woul
d
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
...
...
src/turbulenceModels/RAS/compressible/realizableKE/realizableKE.H
View file @
6a8880a9
...
...
@@ -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
...
...
src/turbulenceModels/RAS/incompressible/LRR/LRR.H
View file @
6a8880a9
...
...
@@ -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
...
...
src/turbulenceModels/RAS/incompressible/LaunderGibsonRSTM/LaunderGibsonRSTM.H
View file @
6a8880a9
...
...
@@ -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
...
...
src/turbulenceModels/RAS/incompressible/LaunderSharmaKE/LaunderSharmaKE.H
View file @
6a8880a9
...
...
@@ -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
...
...
src/turbulenceModels/RAS/incompressible/RNGkEpsilon/RNGkEpsilon.H
View file @
6a8880a9
...
...
@@ -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
...
...
src/turbulenceModels/RAS/incompressible/SpalartAllmaras/SpalartAllmaras.H
View file @
6a8880a9
...
...
@@ -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
...
...
src/turbulenceModels/RAS/incompressible/kEpsilon/kEpsilon.H
View file @
6a8880a9
...
...
@@ -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
...
...
src/turbulenceModels/RAS/incompressible/kOmegaSST/kOmegaSST.H
View file @
6a8880a9
...
...
@@ -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
...
...
src/turbulenceModels/RAS/incompressible/realizableKE/realizableKE.H
View file @
6a8880a9
...
...
@@ -37,8 +37,20 @@ Description
Jiang Zhu
Computers and Fluids Vol. 24, No. 3, pp. 227-238, 1995
@verbatim
@
end
verbatim
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
...
...
Write
Preview
Supports
Markdown
0%
Try again
or
attach a new file
.
Cancel
You are about to add
0
people
to the discussion. Proceed with caution.
Finish editing this message first!
Cancel
Please
register
or
sign in
to comment