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Corrected for new BCs.

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This commit is contained in:
henry
2009-08-18 17:18:05 +01:00
parent dc183f3011
commit a1bf420f52
5 changed files with 120 additions and 21 deletions
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47
tutorials/compressible/sonicFoam/ras/nacaAirfoil/0/alphat Normal file
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@ -0,0 +1,47 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object alphat;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
INLE1
{
type calculated;
value uniform 0;
}
OUTL2
{
type calculated;
value uniform 0;
}
SYMP3
{
type empty;
}
WALL10
{
type alphatWallFunction;
Prt 0.85;
value uniform 0;
}
}
// ************************************************************************* //

23
tutorials/compressible/sonicFoam/ras/nacaAirfoil/0/epsilon
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@ -1,8 +1,8 @@
/*--------------------------------*- C++ -*----------------------------------*\ /*--------------------------------*- C++ -*----------------------------------*\
| ========= | | | ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 | | \\ / O peration | Version: dev |
| \\ / A nd | Web: http://www.OpenFOAM.org | | \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | | | \\/ M anipulation | |
\*---------------------------------------------------------------------------*/ \*---------------------------------------------------------------------------*/
FoamFile FoamFile
@ -10,6 +10,7 @@ FoamFile
version 2.0; version 2.0;
format ascii; format ascii;
class volScalarField; class volScalarField;
location "0";
object epsilon; object epsilon;
} }
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
@ -20,29 +21,31 @@ internalField uniform 25000;
boundaryField boundaryField
{ {
INLE1 INLE1
{ {
type inletOutlet; type inletOutlet;
inletValue uniform 25000; inletValue uniform 25000;
value uniform 25000; value uniform 25000;
} }
OUTL2
OUTL2
{ {
type inletOutlet; type inletOutlet;
inletValue uniform 25000; inletValue uniform 25000;
value uniform 25000; value uniform 25000;
} }
SYMP3
SYMP3
{ {
type empty; type empty;
} }
WALL10
WALL10
{ {
type zeroGradient; type compressible::epsilonWallFunction;
Cmu 0.09;
kappa 0.41;
E 9.8;
value uniform 25000;
} }
} }
// ************************************************************************* // // ************************************************************************* //

20
tutorials/compressible/sonicFoam/ras/nacaAirfoil/0/k
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@ -1,8 +1,8 @@
/*--------------------------------*- C++ -*----------------------------------*\ /*--------------------------------*- C++ -*----------------------------------*\
| ========= | | | ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 | | \\ / O peration | Version: dev |
| \\ / A nd | Web: http://www.OpenFOAM.org | | \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | | | \\/ M anipulation | |
\*---------------------------------------------------------------------------*/ \*---------------------------------------------------------------------------*/
FoamFile FoamFile
@ -10,6 +10,7 @@ FoamFile
version 2.0; version 2.0;
format ascii; format ascii;
class volScalarField; class volScalarField;
location "0";
object k; object k;
} }
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
@ -20,29 +21,28 @@ internalField uniform 1000;
boundaryField boundaryField
{ {
INLE1 INLE1
{ {
type inletOutlet; type inletOutlet;
inletValue uniform 1000; inletValue uniform 1000;
value uniform 1000; value uniform 1000;
} }
OUTL2
OUTL2
{ {
type inletOutlet; type inletOutlet;
inletValue uniform 1000; inletValue uniform 1000;
value uniform 1000; value uniform 1000;
} }
SYMP3
SYMP3
{ {
type empty; type empty;
} }
WALL10
WALL10
{ {
type zeroGradient; type compressible::kqRWallFunction;
value uniform 1000;
} }
} }
// ************************************************************************* // // ************************************************************************* //

49
tutorials/compressible/sonicFoam/ras/nacaAirfoil/0/mut Normal file
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@ -0,0 +1,49 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object mut;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
INLE1
{
type calculated;
value uniform 0;
}
OUTL2
{
type calculated;
value uniform 0;
}
SYMP3
{
type empty;
}
WALL10
{
type mutkWallFunction;
Cmu 0.09;
kappa 0.41;
E 9.8;
value uniform 0;
}
}
// ************************************************************************* //

2
tutorials/compressible/sonicFoam/ras/nacaAirfoil/constant/polyMesh/boundary
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@ -1,7 +1,7 @@
/*--------------------------------*- C++ -*----------------------------------*\ /*--------------------------------*- C++ -*----------------------------------*\
| ========= | | | ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 | | \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org | | \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | | | \\/ M anipulation | |
\*---------------------------------------------------------------------------*/ \*---------------------------------------------------------------------------*/