songtianlun/openfoam
1
0
Fork 0
Code Issues Pull Requests Actions Packages Projects Releases Wiki Activity

New simpleFoam tutorial

Browse Source
This commit is contained in:
henry 2008-07-29 08:45:25 +01:00
parent 6ddfb3490c
commit 88b67a3263
17 changed files with 140820 additions and 0 deletions
Show Stats Download Patch File Download Diff File Expand all files Collapse all files

BIN
tutorials/simpleFoam/airFoil2D/.preGuise.gz Normal file
View File

Binary file not shown.

47
tutorials/simpleFoam/airFoil2D/0/U Normal file
View File

@ -0,0 +1,47 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volVectorField;
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (25.75 3.62 0);
boundaryField
{
inlet
{
type freestream;
freestreamValue uniform (25.75 3.62 0);
}
outlet
{
type freestream;
freestreamValue uniform (25.75 3.62 0);
}
wall
{
type fixedValue;
value uniform (0 0 0);
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

47
tutorials/simpleFoam/airFoil2D/0/nuTilda Normal file
View File

@ -0,0 +1,47 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object nuTilda;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -1 0 0 0 0];
internalField uniform 0.14;
boundaryField
{
inlet
{
type freestream;
freestreamValue uniform 0.14;
}
outlet
{
type freestream;
freestreamValue uniform 0.14;
}
wall
{
type fixedValue;
value uniform 0;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

47
tutorials/simpleFoam/airFoil2D/0/nut Normal file
View File

@ -0,0 +1,47 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object nut;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -1 0 0 0 0];
internalField uniform 0.14;
boundaryField
{
inlet
{
type freestream;
freestreamValue uniform 0.14;
}
outlet
{
type freestream;
freestreamValue uniform 0.14;
}
wall
{
type nutWallFunction;
value uniform 0;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

44
tutorials/simpleFoam/airFoil2D/0/p Normal file
View File

@ -0,0 +1,44 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object p;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 0;
boundaryField
{
inlet
{
type freestreamPressure;
}
outlet
{
type freestreamPressure;
}
wall
{
type zeroGradient;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

173
tutorials/simpleFoam/airFoil2D/constant/RASProperties Normal file
View File

@ -0,0 +1,173 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object RASProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
RASModel SpalartAllmaras; //kEpsilon;
turbulence on;
laminarCoeffs
{
}
kEpsilonCoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphaEps 0.76923;
}
RNGkEpsilonCoeffs
{
Cmu 0.0845;
C1 1.42;
C2 1.68;
alphak 1.39;
alphaEps 1.39;
eta0 4.38;
beta 0.012;
}
NonlinearKEShihCoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphak 1;
alphaEps 0.76932;
A1 1.25;
A2 1000;
Ctau1 -4;
Ctau2 13;
Ctau3 -2;
alphaKsi 0.9;
}
LienCubicKECoeffs
{
C1 1.44;
C2 1.92;
alphak 1;
alphaEps 0.76923;
A1 1.25;
A2 1000;
Ctau1 -4;
Ctau2 13;
Ctau3 -2;
alphaKsi 0.9;
}
QZetaCoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphaZeta 0.76923;
anisotropic no;
}
LaunderSharmaKECoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphaEps 0.76923;
}
LamBremhorstKECoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphaEps 0.76923;
}
LienCubicKELowReCoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphak 1;
alphaEps 0.76923;
A1 1.25;
A2 1000;
Ctau1 -4;
Ctau2 13;
Ctau3 -2;
alphaKsi 0.9;
Am 0.016;
Aepsilon 0.263;
Amu 0.00222;
}
LienLeschzinerLowReCoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphak 1;
alphaEps 0.76923;
Am 0.016;
Aepsilon 0.263;
Amu 0.00222;
}
LRRCoeffs
{
Cmu 0.09;
Clrr1 1.8;
Clrr2 0.6;
C1 1.44;
C2 1.92;
Cs 0.25;
Ceps 0.15;
alphaEps 0.76923;
}
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;
alphaEps 0.76923;
alphaR 1.22;
}
SpalartAllmarasCoeffs
{
alphaNut 1.5;
Cb1 0.1355;
Cb2 0.622;
Cw2 0.3;
Cw3 2;
Cv1 7.1;
//Next line Modified vorticity factor by Ashford 1996
Cv2 5.0;
}
wallFunctionCoeffs
{
kappa 0.4187;
E 9;
}
// ************************************************************************* //

51
tutorials/simpleFoam/airFoil2D/constant/polyMesh/boundary Normal file
View File

@ -0,0 +1,51 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class polyBoundaryMesh;
object boundary;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
4
(
inlet
{
type patch;
physicalType inlet;
nFaces 134;
startFace 21254;
}
outlet
{
type patch;
physicalType outlet;
nFaces 160;
startFace 21388;
}
wall
{
type wall;
physicalType wall;
nFaces 78;
startFace 21548;
}
frontAndBack
{
type empty;
physicalType empty;
nFaces 21440;
startFace 21626;
}
)
// ************************************************************************* //

10741
tutorials/simpleFoam/airFoil2D/constant/polyMesh/cells Normal file
View File

File diff suppressed because it is too large Load Diff

43087
tutorials/simpleFoam/airFoil2D/constant/polyMesh/faces Normal file
View File

File diff suppressed because it is too large Load Diff

21275
tutorials/simpleFoam/airFoil2D/constant/polyMesh/neighbour Normal file
View File

File diff suppressed because it is too large Load Diff

43087
tutorials/simpleFoam/airFoil2D/constant/polyMesh/owner Normal file
View File

File diff suppressed because it is too large Load Diff

21833
tutorials/simpleFoam/airFoil2D/constant/polyMesh/points Normal file
View File

File diff suppressed because it is too large Load Diff

38
tutorials/simpleFoam/airFoil2D/constant/transportProperties Normal file
View File

@ -0,0 +1,38 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object transportProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
transportModel Newtonian;
rho rho [1 -3 0 0 0 0 0] 1.0;
nu nu [0 2 -1 0 0 0 0] 1e-05;
CrossPowerLawCoeffs
{
nu0 nu0 [0 2 -1 0 0 0 0] 1e-06;
nuInf nuInf [0 2 -1 0 0 0 0] 1e-06;
m m [0 0 1 0 0 0 0] 1;
n n [0 0 0 0 0 0 0] 1;
}
BirdCarreauCoeffs
{
nu0 nu0 [0 2 -1 0 0 0 0] 1e-06;
nuInf nuInf [0 2 -1 0 0 0 0] 1e-06;
k k [0 0 1 0 0 0 0] 0;
n n [0 0 0 0 0 0 0] 1;
}
// ************************************************************************* //

173
tutorials/simpleFoam/airFoil2D/constant/turbulenceProperties Normal file
View File

@ -0,0 +1,173 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object turbulenceProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
turbulenceModel SpalartAllmaras; //kEpsilon;
turbulence on;
laminarCoeffs
{
}
kEpsilonCoeffs
{
Cmu Cmu [0 0 0 0 0 0 0] 0.09;
C1 C1 [0 0 0 0 0 0 0] 1.44;
C2 C2 [0 0 0 0 0 0 0] 1.92;
alphaEps alphaEps [0 0 0 0 0 0 0] 0.76923;
}
RNGkEpsilonCoeffs
{
Cmu Cmu [0 0 0 0 0 0 0] 0.0845;
C1 C1 [0 0 0 0 0 0 0] 1.42;
C2 C2 [0 0 0 0 0 0 0] 1.68;
alphak alphaK [0 0 0 0 0 0 0] 1.39;
alphaEps alphaEps [0 0 0 0 0 0 0] 1.39;
eta0 eta0 [0 0 0 0 0 0 0] 4.38;
beta beta [0 0 0 0 0 0 0] 0.012;
}
NonlinearKEShihCoeffs
{
Cmu Cmu [0 0 0 0 0 0 0] 0.09;
C1 C1 [0 0 0 0 0 0 0] 1.44;
C2 C2 [0 0 0 0 0 0 0] 1.92;
alphak alphak [0 0 0 0 0 0 0] 1;
alphaEps alphaEps [0 0 0 0 0 0 0] 0.76932;
A1 A1 [0 0 0 0 0 0 0] 1.25;
A2 A2 [0 0 0 0 0 0 0] 1000;
Ctau1 Ctau1 [0 0 0 0 0 0 0] -4;
Ctau2 Ctau2 [0 0 0 0 0 0 0] 13;
Ctau3 Ctau3 [0 0 0 0 0 0 0] -2;
alphaKsi alphaKsi [0 0 0 0 0 0 0] 0.9;
}
LienCubicKECoeffs
{
C1 C1 [0 0 0 0 0 0 0] 1.44;
C2 C2 [0 0 0 0 0 0 0] 1.92;
alphak alphak [0 0 0 0 0 0 0] 1;
alphaEps alphaEps [0 0 0 0 0 0 0] 0.76923;
A1 A1 [0 0 0 0 0 0 0] 1.25;
A2 A2 [0 0 0 0 0 0 0] 1000;
Ctau1 Ctau1 [0 0 0 0 0 0 0] -4;
Ctau2 Ctau2 [0 0 0 0 0 0 0] 13;
Ctau3 Ctau3 [0 0 0 0 0 0 0] -2;
alphaKsi alphaKsi [0 0 0 0 0 0 0] 0.9;
}
QZetaCoeffs
{
Cmu Cmu [0 0 0 0 0 0 0] 0.09;
C1 C1 [0 0 0 0 0 0 0] 1.44;
C2 C2 [0 0 0 0 0 0 0] 1.92;
alphaZeta alphaZeta [0 0 0 0 0 0 0] 0.76923;
anisotropic no;
}
LaunderSharmaKECoeffs
{
Cmu Cmu [0 0 0 0 0 0 0] 0.09;
C1 C1 [0 0 0 0 0 0 0] 1.44;
C2 C2 [0 0 0 0 0 0 0] 1.92;
alphaEps alphaEps [0 0 0 0 0 0 0] 0.76923;
}
LamBremhorstKECoeffs
{
Cmu Cmu [0 0 0 0 0 0 0] 0.09;
C1 C1 [0 0 0 0 0 0 0] 1.44;
C2 C2 [0 0 0 0 0 0 0] 1.92;
alphaEps alphaEps [0 0 0 0 0 0 0] 0.76923;
}
LienCubicKELowReCoeffs
{
Cmu Cmu [0 0 0 0 0 0 0] 0.09;
C1 C1 [0 0 0 0 0 0 0] 1.44;
C2 C2 [0 0 0 0 0 0 0] 1.92;
alphak alphak [0 0 0 0 0 0 0] 1;
alphaEps alphaEps [0 0 0 0 0 0 0] 0.76923;
A1 A1 [0 0 0 0 0 0 0] 1.25;
A2 A2 [0 0 0 0 0 0 0] 1000;
Ctau1 Ctau1 [0 0 0 0 0 0 0] -4;
Ctau2 Ctau2 [0 0 0 0 0 0 0] 13;
Ctau3 Ctau3 [0 0 0 0 0 0 0] -2;
alphaKsi alphaKsi [0 0 0 0 0 0 0] 0.9;
Am Am [0 0 0 0 0 0 0] 0.016;
Aepsilon Aepsilon [0 0 0 0 0 0 0] 0.263;
Amu Amu [0 0 0 0 0 0 0] 0.00222;
}
LienLeschzinerLowReCoeffs
{
Cmu Cmu [0 0 0 0 0 0 0] 0.09;
C1 C1 [0 0 0 0 0 0 0] 1.44;
C2 C2 [0 0 0 0 0 0 0] 1.92;
alphak alphak [0 0 0 0 0 0 0] 1;
alphaEps alphaEps [0 0 0 0 0 0 0] 0.76923;
Am Am [0 0 0 0 0 0 0] 0.016;
Aepsilon Aepsilon [0 0 0 0 0 0 0] 0.263;
Amu Amu [0 0 0 0 0 0 0] 0.00222;
}
LRRCoeffs
{
Cmu Cmu [0 0 0 0 0 0 0] 0.09;
Clrr1 Clrr1 [0 0 0 0 0 0 0] 1.8;
Clrr2 Clrr2 [0 0 0 0 0 0 0] 0.6;
C1 C1 [0 0 0 0 0 0 0] 1.44;
C2 C2 [0 0 0 0 0 0 0] 1.92;
Cs Cs [0 0 0 0 0 0 0] 0.25;
Ceps Ceps [0 0 0 0 0 0 0] 0.15;
alphaEps alphaEps [0 0 0 0 0 0 0] 0.76923;
}
LaunderGibsonRSTMCoeffs
{
Cmu Cmu [0 0 0 0 0 0 0] 0.09;
Clg1 Clg1 [0 0 0 0 0 0 0] 1.8;
Clg2 Clg2 [0 0 0 0 0 0 0] 0.6;
C1 C1 [0 0 0 0 0 0 0] 1.44;
C2 C2 [0 0 0 0 0 0 0] 1.92;
C1Ref C1Ref [0 0 0 0 0 0 0] 0.5;
C2Ref C2Ref [0 0 0 0 0 0 0] 0.3;
Cs Cs [0 0 0 0 0 0 0] 0.25;
Ceps Ceps [0 0 0 0 0 0 0] 0.15;
alphaEps alphaEps [0 0 0 0 0 0 0] 0.76923;
alphaR alphaR [0 0 0 0 0 0 0] 1.22;
}
SpalartAllmarasCoeffs
{
alphaNut alphaNut [0 0 0 0 0 0 0] 1.5;
Cb1 Cb1 [0 0 0 0 0 0 0] 0.1355;
Cb2 Cb2 [0 0 0 0 0 0 0] 0.622;
Cw2 Cw2 [0 0 0 0 0 0 0] 0.3;
Cw3 Cw3 [0 0 0 0 0 0 0] 2;
Cv1 Cv1 [0 0 0 0 0 0 0] 7.1;
//Next line Modified vorticity factor by Ashford 1996
Cv2 Cv2 [0 0 0 0 0 0 0] 5.0;
}
wallFunctionCoeffs
{
kappa kappa [0 0 0 0 0 0 0] 0.4187;
E E [0 0 0 0 0 0 0] 9;
}
// ************************************************************************* //

47
tutorials/simpleFoam/airFoil2D/system/controlDict Normal file
View File

@ -0,0 +1,47 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application simpleFoam;
startFrom latestTime;
startTime 0;
stopAt endTime;
endTime 500;
deltaT 1;
writeControl timeStep;
writeInterval 50;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
writeCompression uncompressed;
timeFormat general;
timePrecision 6;
runTimeModifiable yes;
// ************************************************************************* //

64
tutorials/simpleFoam/airFoil2D/system/fvSchemes Normal file
View File

@ -0,0 +1,64 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default steadyState;
}
gradSchemes
{
default Gauss linear;
grad(p) Gauss linear;
grad(U) Gauss linear;
}
divSchemes
{
default none;
div(phi,U) Gauss linearUpwind Gauss linear;
div(phi,nuTilda) Gauss linearUpwind Gauss linear;
div((nuEff*dev(grad(U).T()))) Gauss linear;
}
laplacianSchemes
{
default none;
laplacian(nuEff,U) Gauss linear corrected;
laplacian((1|A(U)),p) Gauss linear corrected;
laplacian(DnuTildaEff,nuTilda) Gauss linear corrected;
laplacian(1,p) Gauss linear corrected;
}
interpolationSchemes
{
default linear;
interpolate(U) linear;
}
snGradSchemes
{
default corrected;
}
fluxRequired
{
default no;
p;
}
// ************************************************************************* //

66
tutorials/simpleFoam/airFoil2D/system/fvSolution Normal file
View File

@ -0,0 +1,66 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
p GAMG
{
tolerance 1e-6;
relTol 0.1;
smoother GaussSeidel;
nPreSweeps 0;
nPostSweeps 2;
cacheAgglomeration true;
nCellsInCoarsestLevel 10;
agglomerator faceAreaPair;
mergeLevels 1;
};
U smoothSolver
{
smoother GaussSeidel;
nSweeps 2;
tolerance 1e-8;
relTol 0.1;
};
nuTilda smoothSolver
{
smoother GaussSeidel;
nSweeps 2;
tolerance 1e-8;
relTol 0.1;
};
}
SIMPLE
{
nNonOrthogonalCorrectors 0;
pRefCell 0;
pRefValue 0;
}
relaxationFactors
{
p 0.3;
U 0.7;
nuTilda 0.7;
}
// ************************************************************************* //