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Commit 88b67a32 authored by henry's avatar henry
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New simpleFoam tutorial

parent 6ddfb349
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tutorials/simpleFoam/airFoil2D/0/U 0 → 100644
View file @ 88b67a32
/*--------------------------------*- 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;
}
}
// ************************************************************************* //
tutorials/simpleFoam/airFoil2D/0/nuTilda 0 → 100644
View file @ 88b67a32
/*--------------------------------*- 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;
}
}
// ************************************************************************* //
tutorials/simpleFoam/airFoil2D/0/nut 0 → 100644
View file @ 88b67a32
/*--------------------------------*- 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;
}
}
// ************************************************************************* //
tutorials/simpleFoam/airFoil2D/0/p 0 → 100644
View file @ 88b67a32
/*--------------------------------*- 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;
}
}
// ************************************************************************* //
tutorials/simpleFoam/airFoil2D/constant/RASProperties 0 → 100644
View file @ 88b67a32
/*--------------------------------*- 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;
}
// ************************************************************************* //
tutorials/simpleFoam/airFoil2D/constant/polyMesh/boundary 0 → 100644
View file @ 88b67a32
/*--------------------------------*- 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;
}
)
// ************************************************************************* //
tutorials/simpleFoam/airFoil2D/constant/polyMesh/cells 0 → 100644
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tutorials/simpleFoam/airFoil2D/constant/polyMesh/faces 0 → 100644
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tutorials/simpleFoam/airFoil2D/constant/polyMesh/neighbour 0 → 100644
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tutorials/simpleFoam/airFoil2D/constant/polyMesh/owner 0 → 100644
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tutorials/simpleFoam/airFoil2D/constant/polyMesh/points 0 → 100644
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This diff is collapsed.
tutorials/simpleFoam/airFoil2D/constant/transportProperties 0 → 100644
View file @ 88b67a32
/*--------------------------------*- 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;
}
// ************************************************************************* //
tutorials/simpleFoam/airFoil2D/constant/turbulenceProperties 0 → 100644
View file @ 88b67a32
/*--------------------------------*- 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