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sonicFoam: Update tutorials

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This commit is contained in:
Henry
2012-10-12 11:16:25 +01:00
parent 9b1ed88057
commit 657863b007
4 changed files with 8 additions and 15 deletions
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10
tutorials/compressible/sonicFoam/laminar/forwardStep/system/fvSchemes
View File

@ -23,8 +23,6 @@ ddtSchemes
gradSchemes
{
default Gauss linear;
grad(p) Gauss linear;
grad(U) Gauss linear;
}
divSchemes
@ -33,16 +31,14 @@ divSchemes
div(phi,U) Gauss upwind;
div(phid,p) Gauss limitedLinear 1;
div(phi,e) Gauss limitedLinear 1;
div(phi,Ekp) Gauss limitedLinear 1;
div(phi,K) Gauss limitedLinear 1;
div(phiv,p) Gauss limitedLinear 1;
div((muEff*dev2(T(grad(U))))) Gauss linear 1;
}
laplacianSchemes
{
default none;
laplacian(Dp,p) Gauss linear corrected;
laplacian(muEff,U) Gauss linear corrected;
laplacian(alphaEff,e) Gauss linear corrected;
default Gauss linear corrected;
}
interpolationSchemes

7
tutorials/compressible/sonicFoam/laminar/shockTube/system/fvSchemes
View File

@ -23,8 +23,6 @@ ddtSchemes
gradSchemes
{
default Gauss linear;
grad(p) Gauss linear;
grad(U) Gauss linear;
}
divSchemes
@ -40,10 +38,7 @@ divSchemes
laplacianSchemes
{
default none;
laplacian(Dp,p) Gauss linear orthogonal;
laplacian(muEff,U) Gauss linear orthogonal;
laplacian(alphaEff,e) Gauss linear orthogonal;
default Gauss linear orthogonal;
}
interpolationSchemes

3
tutorials/compressible/sonicFoam/ras/nacaAirfoil/system/fvSchemes
View File

@ -30,8 +30,9 @@ divSchemes
default none;
div(phi,U) Gauss limitedLinearV 1;
div(phi,e) Gauss limitedLinear 1;
div(phi,Ekp) Gauss limitedLinear 1;
div(phid,p) Gauss limitedLinear 1;
div(phi,K) Gauss limitedLinear 1;
div(phiv,p) Gauss limitedLinear 1;
div(phi,k) Gauss upwind;
div(phi,epsilon) Gauss upwind;
div((muEff*dev2(T(grad(U))))) Gauss linear;

3
tutorials/compressible/sonicFoam/ras/prism/system/fvSchemes
View File

@ -30,8 +30,9 @@ divSchemes
default none;
div(phi,U) Gauss limitedLinearV 1;
div(phi,e) Gauss limitedLinear 1;
div(phi,Ekp) Gauss limitedLinear 1;
div(phid,p) Gauss limitedLinear 1;
div(phi,K) Gauss limitedLinear 1;
div(phiv,p) Gauss limitedLinear 1;
div(phi,k) Gauss upwind;
div(phi,epsilon) Gauss upwind;
div((muEff*dev2(T(grad(U))))) Gauss linear;