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Tried to sort out the scripts in the tutorials but found it is messed up. Will start again from a new version from Mattijs

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henry
2008-06-13 13:46:55 +01:00
parent 91c2d7743b
commit 9ad914ca0b
1061 changed files with 0 additions and 533232 deletions
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55
tutorials/boundaryFoam/boundaryWallFunctions/0/R
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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class volSymmTensorField;
object R;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform (0 0 0 0 0 0);
boundaryField
{
lowerWall
{
type zeroGradient;
}
upperWall
{
type zeroGradient;
}
frontBack
{
type cyclic;
}
defaultFaces
{
type empty;
}
}
// ************************************************************************* //

57
tutorials/boundaryFoam/boundaryWallFunctions/0/U
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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class volVectorField;
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
lowerWall
{
type fixedValue;
value uniform (0 0 0);
}
upperWall
{
type fixedValue;
value uniform (0 0 0);
}
frontBack
{
type cyclic;
}
defaultFaces
{
type empty;
}
}
// ************************************************************************* //

55
tutorials/boundaryFoam/boundaryWallFunctions/0/epsilon
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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class volScalarField;
object epsilon;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -3 0 0 0 0];
internalField uniform 1e-08;
boundaryField
{
lowerWall
{
type zeroGradient;
}
upperWall
{
type zeroGradient;
}
frontBack
{
type cyclic;
}
defaultFaces
{
type empty;
}
}
// ************************************************************************* //

55
tutorials/boundaryFoam/boundaryWallFunctions/0/k
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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class volScalarField;
object k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 1e-10;
boundaryField
{
lowerWall
{
type zeroGradient;
}
upperWall
{
type zeroGradient;
}
frontBack
{
type cyclic;
}
defaultFaces
{
type empty;
}
}
// ************************************************************************* //

80
tutorials/boundaryFoam/boundaryWallFunctions/0/nu.xy
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55
tutorials/boundaryFoam/boundaryWallFunctions/0/nuTilda
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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class volScalarField;
object nuTilda;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
lowerWall
{
type zeroGradient;
}
upperWall
{
type zeroGradient;
}
frontBack
{
type cyclic;
}
defaultFaces
{
type empty;
}
}
// ************************************************************************* //

80
tutorials/boundaryFoam/boundaryWallFunctions/constant/gammaDot.xy
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@ -1,80 +0,0 @@
-0.049375 8000
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79
tutorials/boundaryFoam/boundaryWallFunctions/constant/polyMesh/blockMeshDict
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@ -1,79 +0,0 @@
/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class dictionary;
object blockMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
convertToMeters 0.05;
vertices
(
(0 -1 0)
(0 0 0)
(0 1 0)
(0.1 -1 0)
(0.1 0 0)
(0.1 1 0)
(0 -1 0.1)
(0 0 0.1)
(0 1 0.1)
(0.1 -1 0.1)
(0.1 0 0.1)
(0.1 1 0.1)
);
blocks
(
hex (0 3 4 1 6 9 10 7) (1 40 1) simpleGrading (1 1 1)
hex (1 4 5 2 7 10 11 8) (1 40 1) simpleGrading (1 1 1)
);
edges
(
);
patches
(
wall lowerWall
(
(0 3 9 6)
)
wall upperWall
(
(2 8 11 5)
)
cyclic frontBack
(
(0 6 7 1)
(1 7 8 2)
(9 3 4 10)
(10 4 5 11)
)
);
mergePatchPairs
(
);
// ************************************************************************* //

58
tutorials/boundaryFoam/boundaryWallFunctions/constant/polyMesh/boundary
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@ -1,58 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4.1 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "/home/dm2/henry/OpenFOAM/OpenFOAM-1.4.1/tutorials/boundaryFoam";
case "boundaryWallFunctions";
instance "constant";
local "polyMesh";
class polyBoundaryMesh;
object boundary;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
4
(
lowerWall
{
type wall;
physicalType wallFunctions;
nFaces 1;
startFace 79;
}
upperWall
{
type wall;
physicalType wallFunctions;
nFaces 1;
startFace 80;
}
frontBack
{
type cyclic;
nFaces 160;
startFace 81;
}
defaultFaces
{
type empty;
nFaces 160;
startFace 241;
}
)
// ************************************************************************* //

62
tutorials/boundaryFoam/boundaryWallFunctions/constant/transportProperties
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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class dictionary;
object transportProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// Ubar
Ubar Ubar [0 1 -1 0 0 0 0] (10 0 0);
// Laminar incompressible transport model
transportModel Newtonian;
// nu
nu nu [0 2 -1 0 0 0 0] 1e-05;
// Coefficients for Cross's Power Law
CrossPowerLawCoeffs
{
// nu0
nu0 nu0 [0 2 -1 0 0 0 0] 1e-06;
// nuInf
nuInf nuInf [0 2 -1 0 0 0 0] 1e-06;
// m
m m [0 0 1 0 0 0 0] 1;
// n
n n [0 0 0 0 0 0 0] 1;
}
// Coefficients for Bird-Carreau Law
BirdCarreauCoeffs
{
// nu0
nu0 nu0 [0 2 -1 0 0 0 0] 1e-06;
// nuInf
nuInf nuInf [0 2 -1 0 0 0 0] 1e-06;
// k
k k [0 0 1 0 0 0 0] 0;
// n
n n [0 0 0 0 0 0 0] 1;
}
// ************************************************************************* //

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tutorials/boundaryFoam/boundaryWallFunctions/constant/turbulenceProperties
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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class dictionary;
object turbulenceProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// Turbulence model selection
turbulenceModel kEpsilon;
// Do you wish to calculate turbulence?
turbulence on;
// Laminar model coefficients
laminarCoeffs
{
}
// Standard k-epsilon model coefficients
kEpsilonCoeffs
{
// Cmu
Cmu Cmu [0 0 0 0 0 0 0] 0.09;
// C1
C1 C1 [0 0 0 0 0 0 0] 1.44;
// C2
C2 C2 [0 0 0 0 0 0 0] 1.92;
// alphaEps
alphaEps alphaEps [0 0 0 0 0 0 0] 0.76923;
}
// RNG k-epsilon model coefficients
RNGkEpsilonCoeffs
{
// Cmu
Cmu Cmu [0 0 0 0 0 0 0] 0.0845;
// C1
C1 C1 [0 0 0 0 0 0 0] 1.42;
// C2
C2 C2 [0 0 0 0 0 0 0] 1.68;
// alphak
alphak alphaK [0 0 0 0 0 0 0] 1.39;
// alphaEps
alphaEps alphaEps [0 0 0 0 0 0 0] 1.39;
// eta0
eta0 eta0 [0 0 0 0 0 0 0] 4.38;
// beta
beta beta [0 0 0 0 0 0 0] 0.012;
}
// k-omega-SST model coefficients
kOmegaSSTCoeffs
{
alphaK1 alphaK1 [0 0 0 0 0 0 0] 0.85034;
alphaK2 alphaK1 [0 0 0 0 0 0 0] 1.0;
alphaOmega1 alphaOmega1 [0 0 0 0 0 0 0] 0.5;
alphaOmega2 alphaOmega2 [0 0 0 0 0 0 0] 0.85616;
gamma1 gamma1 [0 0 0 0 0 0 0] 0.5532;
gamma2 gamma2 [0 0 0 0 0 0 0] 0.4403;
beta1 beta1 [0 0 0 0 0 0 0] 0.0750;
beta2 beta2 [0 0 0 0 0 0 0] 0.0828;
betaStar betaStar [0 0 0 0 0 0 0] 0.09;
a1 a1 [0 0 0 0 0 0 0] 0.31;
c1 c1 [0 0 0 0 0 0 0] 10;
Cmu Cmu [0 0 0 0 0 0 0] 0.09;
}
// Shih non-Linear k-epsilon model coefficients
NonlinearKEShihCoeffs
{
// Cmu
Cmu Cmu [0 0 0 0 0 0 0] 0.09;
// C1
C1 C1 [0 0 0 0 0 0 0] 1.44;
// C2
C2 C2 [0 0 0 0 0 0 0] 1.92;
// alphak
alphak alphak [0 0 0 0 0 0 0] 1;
// alphaEps
alphaEps alphaEps [0 0 0 0 0 0 0] 0.76932;
// A1
A1 A1 [0 0 0 0 0 0 0] 1.25;
// A2
A2 A2 [0 0 0 0 0 0 0] 1000;
// Ctau1
Ctau1 Ctau1 [0 0 0 0 0 0 0] -4;
// Ctau2
Ctau2 Ctau2 [0 0 0 0 0 0 0] 13;
// Ctau3
Ctau3 Ctau3 [0 0 0 0 0 0 0] -2;
// alphaKsi
alphaKsi alphaKsi [0 0 0 0 0 0 0] 0.9;
}
// Lien non-Linear cubic k-epsilon model coefficients
LienCubicKECoeffs
{
// C1
C1 C1 [0 0 0 0 0 0 0] 1.44;
// C2
C2 C2 [0 0 0 0 0 0 0] 1.92;
// alphak
alphak alphak [0 0 0 0 0 0 0] 1;
// alphaEps
alphaEps alphaEps [0 0 0 0 0 0 0] 0.76923;
// A1
A1 A1 [0 0 0 0 0 0 0] 1.25;
// A2
A2 A2 [0 0 0 0 0 0 0] 1000;
// Ctau1
Ctau1 Ctau1 [0 0 0 0 0 0 0] -4;
// Ctau2
Ctau2 Ctau2 [0 0 0 0 0 0 0] 13;
// Ctau3
Ctau3 Ctau3 [0 0 0 0 0 0 0] -2;
// alphaKsi
alphaKsi alphaKsi [0 0 0 0 0 0 0] 0.9;
}
// Gibson's q-zeta low Reynolds number k-epsilon model coefficients
QZetaCoeffs
{
// Cmu
Cmu Cmu [0 0 0 0 0 0 0] 0.09;
// C1
C1 C1 [0 0 0 0 0 0 0] 1.44;
// C2
C2 C2 [0 0 0 0 0 0 0] 1.92;
// alphaZeta
alphaZeta alphaZeta [0 0 0 0 0 0 0] 0.76923;
// anisotropic?
anisotropic no;
}
// Launder-Sharma low Reynolds number k-epsilon model coefficients
LaunderSharmaKECoeffs
{
// Cmu
Cmu Cmu [0 0 0 0 0 0 0] 0.09;
// C1
C1 C1 [0 0 0 0 0 0 0] 1.44;
// C2
C2 C2 [0 0 0 0 0 0 0] 1.92;
// alphaEps
alphaEps alphaEps [0 0 0 0 0 0 0] 0.76923;
}
// Lam-Bremhorst low Reynolds number k-Epsilon model coefficients
LamBremhorstKECoeffs
{
// Cmu
Cmu Cmu [0 0 0 0 0 0 0] 0.09;
// C1
C1 C1 [0 0 0 0 0 0 0] 1.44;
// C2
C2 C2 [0 0 0 0 0 0 0] 1.92;
// alphaEps
alphaEps alphaEps [0 0 0 0 0 0 0] 0.76923;
}
// Lien-Leschziner low Reynolds number cubic k-epsilon model coefficients
LienCubicKELowReCoeffs
{
// Cmu
Cmu Cmu [0 0 0 0 0 0 0] 0.09;
// C1
C1 C1 [0 0 0 0 0 0 0] 1.44;
// C2
C2 C2 [0 0 0 0 0 0 0] 1.92;
// alphak
alphak alphak [0 0 0 0 0 0 0] 1;
// alphaEps
alphaEps alphaEps [0 0 0 0 0 0 0] 0.76923;
// A1
A1 A1 [0 0 0 0 0 0 0] 1.25;
// A2
A2 A2 [0 0 0 0 0 0 0] 1000;
// Ctau1
Ctau1 Ctau1 [0 0 0 0 0 0 0] -4;
// Ctau2
Ctau2 Ctau2 [0 0 0 0 0 0 0] 13;
// Ctau3
Ctau3 Ctau3 [0 0 0 0 0 0 0] -2;
// alphaKsi
alphaKsi alphaKsi [0 0 0 0 0 0 0] 0.9;
// Am
Am Am [0 0 0 0 0 0 0] 0.016;
// Aepsilon
Aepsilon Aepsilon [0 0 0 0 0 0 0] 0.263;
// Amu
Amu Amu [0 0 0 0 0 0 0] 0.00222;
}
// Lien-Leschziner low Reynolds number cubic k-epsilon model coefficients
LienLeschzinerLowReCoeffs
{
// Cmu
Cmu Cmu [0 0 0 0 0 0 0] 0.09;
// C1
C1 C1 [0 0 0 0 0 0 0] 1.44;
// C2
C2 C2 [0 0 0 0 0 0 0] 1.92;
// alphak
alphak alphak [0 0 0 0 0 0 0] 1;
// alphaEps
alphaEps alphaEps [0 0 0 0 0 0 0] 0.76923;
// Am
Am Am [0 0 0 0 0 0 0] 0.016;
// Aepsilon
Aepsilon Aepsilon [0 0 0 0 0 0 0] 0.263;
// Amu
Amu Amu [0 0 0 0 0 0 0] 0.00222;
}
// Launder-Reece-Rodi RSTM with wall functions model coefficients
LRRCoeffs
{
// Cmu
Cmu Cmu [0 0 0 0 0 0 0] 0.09;
// Clrr1
Clrr1 Clrr1 [0 0 0 0 0 0 0] 1.8;
// Clrr2
Clrr2 Clrr2 [0 0 0 0 0 0 0] 0.6;
// C1
C1 C1 [0 0 0 0 0 0 0] 1.44;
// C2
C2 C2 [0 0 0 0 0 0 0] 1.92;
// Cs
Cs Cs [0 0 0 0 0 0 0] 0.25;
// Ceps
Ceps Ceps [0 0 0 0 0 0 0] 0.15;
// alphaEps
alphaEps alphaEps [0 0 0 0 0 0 0] 0.76923;
}
// Launder-Gibson RSTM with wall reflection and wall functions model coefficients
LaunderGibsonRSTMCoeffs
{
// Cmu
Cmu Cmu [0 0 0 0 0 0 0] 0.09;
// Clg1
Clg1 Clg1 [0 0 0 0 0 0 0] 1.8;
// Clg2
Clg2 Clg2 [0 0 0 0 0 0 0] 0.6;
// C1
C1 C1 [0 0 0 0 0 0 0] 1.44;
// C2
C2 C2 [0 0 0 0 0 0 0] 1.92;
// C1Ref
C1Ref C1Ref [0 0 0 0 0 0 0] 0.5;
// C2Ref
C2Ref C2Ref [0 0 0 0 0 0 0] 0.3;
// Cs
Cs Cs [0 0 0 0 0 0 0] 0.25;
// Ceps
Ceps Ceps [0 0 0 0 0 0 0] 0.15;
// alphaEps
alphaEps alphaEps [0 0 0 0 0 0 0] 0.76923;
// alphaR
alphaR alphaR [0 0 0 0 0 0 0] 1.22;
}
// Standard Spalart-Allmaras model coefficients
SpalartAllmarasCoeffs
{
// alphaNut
alphaNut alphaNut [0 0 0 0 0 0 0] 1.5;
// Cb1
Cb1 Cb1 [0 0 0 0 0 0 0] 0.1355;
// Cb2
Cb2 Cb2 [0 0 0 0 0 0 0] 0.622;
// Cw2
Cw2 Cw2 [0 0 0 0 0 0 0] 0.3;
// Cw3
Cw3 Cw3 [0 0 0 0 0 0 0] 2;
// Cv1
Cv1 Cv1 [0 0 0 0 0 0 0] 7.1;
Cv2 Cv2 [0 0 0 0 0 0 0] 5.0;
}
// Wall function coefficients
wallFunctionCoeffs
{
// kappa
kappa kappa [0 0 0 0 0 0 0] 0.4187;
// E
E E [0 0 0 0 0 0 0] 9;
}
// ************************************************************************* //

74
tutorials/boundaryFoam/boundaryWallFunctions/system/controlDict
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@ -1,74 +0,0 @@
/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class dictionary;
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// Foam Application Class
application boundaryFoam;
// Start point of run
startFrom startTime;
// Calculation start time
startTime 0;
// End point of run
stopAt endTime;
// Calculation end time
endTime 1000;
// Calculation time step
deltaT 1;
// Type of write output control
writeControl timeStep;
// Interval with which the results are output
writeInterval 100;
// Limits number of time directories before overwriting
purgeWrite 0;
// Write Format
writeFormat ascii;
// Significant figures of written ASCII data
writePrecision 6;
// Write Compression
writeCompression uncompressed;
// Time directories name format
timeFormat general;
// Decimal precision of time directory names
timePrecision 6;
// Can parameters be modified during run time?
runTimeModifiable yes;
// Output format for graphs
graphFormat raw;
// ************************************************************************* //

78
tutorials/boundaryFoam/boundaryWallFunctions/system/fvSchemes
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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class dictionary;
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// Time derivative discretisation schemes
ddtSchemes
{
// Default scheme
default steadyState;
}
// Gradient discretisation schemes
gradSchemes
{
// Default gradient scheme
default Gauss linear;
}
// Convection discretisation schemes
divSchemes
{
// Default scheme
default none;
div(phi,k) Gauss linear;
div(phi,epsilon) Gauss linear;
div(phi,R) Gauss linear;
div(phi,nuTilda) Gauss linear;
div((nuEff*dev(grad(U).T()))) Gauss linear;
}
// Laplacian discretisation schemes
laplacianSchemes
{
// Default scheme
default none;
laplacian(nuEff,U) Gauss linear corrected;
laplacian(DkEff,k) Gauss linear corrected;
laplacian(DepsilonEff,epsilon) Gauss linear corrected;
laplacian(DREff,R) Gauss linear corrected;
laplacian(DnuTildaEff,nuTilda) Gauss linear corrected;
}
// Interpolation schemes
interpolationSchemes
{
// Default scheme
default linear;
}
// Surface normal gradient schemes
snGradSchemes
{
// Default scheme
default corrected;
}
// ************************************************************************* //

91
tutorials/boundaryFoam/boundaryWallFunctions/system/fvSolution
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@ -1,91 +0,0 @@
/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class dictionary;
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
// Solver for the U equation
U PCG
{
preconditioner DIC;
tolerance 1e-06;
relTol 0;
};
// Solver for the k equation
k PBiCG
{
preconditioner DILU;
tolerance 1e-06;
relTol 0;
};
// Solver for the epsilon equation
epsilon PBiCG
{
preconditioner DILU;
tolerance 1e-06;
relTol 0;
};
// Solver for the R equation
R PBiCG
{
preconditioner DILU;
tolerance 1e-06;
relTol 0;
};
// Solver for the nuTilda equation
nuTilda PBiCG
{
preconditioner DILU;
tolerance 1e-06;
relTol 0;
};
}
PISO
{
// Number of PISO correctors
nCorrectors 2;
// Number of non-orthogonal correctors
nNonOrthogonalCorrectors 0;
// momentumPredictor?
momentumPredictor yes;
// fluxGradp?
fluxGradp no;
}
relaxationFactors
{
// U
U 0.5;
// k
k 0.7;
// epsilon
epsilon 0.7;
// R
R 0.7;
// nuTilda
nuTilda 0.7;
}
// ************************************************************************* //