tutorials: Removed 0.orig directories in favor of <field>.orig
The new automated <field>.orig reading has made 0.orig directories and associated scripting redundant.
This commit is contained in:
Henry Weller
@ -4,11 +4,12 @@ cd ${0%/*} || exit 1 # Run from this directory
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# Source tutorial clean functions
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. $WM_PROJECT_DIR/bin/tools/CleanFunctions
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# remove surface
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# Remove surface
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rm -f constant/triSurface/propellerTip.obj.gz > /dev/null 2>&1
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cleanCase
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rm -rf 0 > /dev/null 2>&1
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rm -rf constant/extendedFeatureEdgeMesh > /dev/null 2>&1
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rm -f constant/triSurface/*.eMesh* > /dev/null 2>&1
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#------------------------------------------------------------------------------
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@ -11,3 +11,5 @@ runApplication decomposePar
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runParallel `getApplication`
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runApplication reconstructPar
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#------------------------------------------------------------------------------
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@ -30,5 +30,4 @@ runApplication createPatch -overwrite
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# - test by running moveDynamicMes
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#runApplication moveDynamicMesh -checkAMI
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# - set the initial fields
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cp -rf 0.orig 0
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#------------------------------------------------------------------------------
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@ -9,8 +9,9 @@ cleanCase
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cd ../wingMotion2D_simpleFoam
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cleanCase
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rm -rf 0
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cd ../wingMotion2D_pimpleFoam
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cleanCase
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rm -rf 0
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rm -f 0/p 0/nut 0/k 0/omega 0/U 0/pointDisplacement
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#------------------------------------------------------------------------------
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@ -13,16 +13,14 @@ runApplication snappyHexMesh -overwrite
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cd ../wingMotion2D_simpleFoam
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runApplication extrudeMesh
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runApplication createPatch -overwrite
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cp -r 0.orig 0
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runApplication simpleFoam
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# Copy the mesh from the steady state case and map the results to a
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# mesh motion case, then solve transient.
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cd ../wingMotion2D_pimpleFoam
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cp -r ../wingMotion2D_simpleFoam/constant/polyMesh constant
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cp -r 0.orig 0
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runApplication mapFields ../wingMotion2D_simpleFoam -sourceTime latestTime -consistent
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mv 0/pointDisplacement.unmapped 0/pointDisplacement
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cp pointDisplacement 0/pointDisplacement
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runApplication decomposePar
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runParallel `getApplication`
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runApplication reconstructPar
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@ -1,45 +0,0 @@
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/*--------------------------------*- C++ -*----------------------------------*\
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| ========= | |
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| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
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| \\ / O peration | Version: dev |
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| \\ / A nd | Web: www.OpenFOAM.org |
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| \\/ M anipulation | |
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\*---------------------------------------------------------------------------*/
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FoamFile
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{
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version 2.0;
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format ascii;
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class volVectorField;
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location "0";
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object U;
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}
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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#include "include/initialConditions"
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dimensions [0 1 -1 0 0 0 0];
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internalField uniform $flowVelocity;
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boundaryField
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{
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#include "include/fixedInlet"
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outlet
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{
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type inletOutlet;
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inletValue uniform (0 0 0);
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value $internalField;
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}
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wing
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{
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type movingWallVelocity;
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value uniform (0 0 0);
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}
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#include "include/frontBackTopBottomPatches"
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}
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// ************************************************************************* //
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@ -1,44 +0,0 @@
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/*--------------------------------*- C++ -*----------------------------------*\
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| ========= | |
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| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
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| \\ / O peration | Version: dev |
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| \\ / A nd | Web: www.OpenFOAM.org |
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| \\/ M anipulation | |
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\*---------------------------------------------------------------------------*/
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FoamFile
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{
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version 2.0;
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format ascii;
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class volScalarField;
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object k;
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}
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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#include "include/initialConditions"
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dimensions [0 2 -2 0 0 0 0];
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internalField uniform $turbulentKE;
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boundaryField
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{
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#include "include/fixedInlet"
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outlet
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{
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type inletOutlet;
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inletValue $internalField;
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value $internalField;
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}
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wing
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{
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type kqRWallFunction;
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value $internalField;
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}
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#include "include/frontBackTopBottomPatches"
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}
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// ************************************************************************* //
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@ -1,38 +0,0 @@
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/*--------------------------------*- C++ -*----------------------------------*\
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| ========= | |
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| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
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| \\ / O peration | Version: dev |
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| \\ / A nd | Web: www.OpenFOAM.org |
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| \\/ M anipulation | |
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\*---------------------------------------------------------------------------*/
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FoamFile
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{
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version 2.0;
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format ascii;
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class volScalarField;
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location "0";
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object nut;
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}
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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dimensions [0 2 -1 0 0 0 0];
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internalField uniform 0;
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boundaryField
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{
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wing
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{
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type nutkWallFunction;
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value uniform 0;
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}
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"(front|back|topAndBottom|inlet|outlet)"
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{
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type calculated;
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value uniform 0;
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}
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}
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// ************************************************************************* //
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@ -1,44 +0,0 @@
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/*--------------------------------*- C++ -*----------------------------------*\
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| ========= | |
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| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
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| \\ / O peration | Version: dev |
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| \\ / A nd | Web: www.OpenFOAM.org |
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| \\/ M anipulation | |
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\*---------------------------------------------------------------------------*/
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FoamFile
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{
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version 2.0;
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format ascii;
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class volScalarField;
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object epsilon;
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}
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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#include "include/initialConditions"
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dimensions [0 0 -1 0 0 0 0];
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internalField uniform $turbulentOmega;
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boundaryField
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{
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#include "include/fixedInlet"
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outlet
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{
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type inletOutlet;
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inletValue $internalField;
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value $internalField;
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}
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wing
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{
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type omegaWallFunction;
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value $internalField;
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}
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#include "include/frontBackTopBottomPatches"
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}
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// ************************************************************************* //
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@ -1,44 +0,0 @@
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/*--------------------------------*- C++ -*----------------------------------*\
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| ========= | |
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| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
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| \\ / O peration | Version: dev |
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| \\ / A nd | Web: www.OpenFOAM.org |
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| \\/ M anipulation | |
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\*---------------------------------------------------------------------------*/
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FoamFile
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{
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version 2.0;
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format ascii;
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class volScalarField;
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object p;
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}
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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#include "include/initialConditions"
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dimensions [0 2 -2 0 0 0 0];
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internalField uniform $pressure;
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boundaryField
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{
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inlet
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{
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type zeroGradient;
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}
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outlet
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{
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type fixedValue;
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value $internalField;
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}
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wing
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{
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type zeroGradient;
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}
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#include "include/frontBackTopBottomPatches"
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}
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// ************************************************************************* //
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@ -4,11 +4,9 @@ cd ${0%/*} || exit 1 # Run from this directory
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# Source tutorial clean functions
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. $WM_PROJECT_DIR/bin/tools/CleanFunctions
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# remove surface
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# Remove surface
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rm -f constant/triSurface/motorBike.obj.gz
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rm -rf 0 > /dev/null 2>&1
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cleanCase
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# Reset decomposeParDict
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@ -7,21 +7,15 @@ cd ${0%/*} || exit 1 # Run from this directory
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# copy motorbike surface from resources directory
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cp $FOAM_TUTORIALS/resources/geometry/motorBike.obj.gz constant/triSurface/
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# Make dummy 0 directory
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mkdir 0
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runApplication blockMesh
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cp system/decomposeParDict.hierarchical system/decomposeParDict
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runApplication decomposePar
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runApplication decomposePar -copyZero
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cp system/decomposeParDict.ptscotch system/decomposeParDict
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runParallel snappyHexMesh -overwrite
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find . -type f -iname "*level*" -exec rm {} \;
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ls -d processor* | xargs -I {} rm -rf ./{}/0
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ls -d processor* | xargs -I {} cp -r 0.orig ./{}/0
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runParallel renumberMesh -overwrite
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runParallel potentialFoam -initialiseUBCs
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@ -4,8 +4,6 @@ cd ${0%/*} || exit 1 # Run from this directory
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# Source tutorial clean functions
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. $WM_PROJECT_DIR/bin/tools/CleanFunctions
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rm -rf 0 > /dev/null 2>&1
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cleanCase
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# Remove decomposeParDict
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@ -4,20 +4,15 @@ cd ${0%/*} || exit 1 # Run from this directory
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# Source tutorial run functions
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. $WM_PROJECT_DIR/bin/tools/RunFunctions
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# Make dummy 0 directory
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mkdir 0
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runApplication blockMesh
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cp system/decomposeParDict.hierarchical system/decomposeParDict
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runApplication decomposePar
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runApplication decomposePar -copyZero
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cp system/decomposeParDict.ptscotch system/decomposeParDict
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runParallel snappyHexMesh -overwrite
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find . -type f -iname "*level*" -exec rm {} \;
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ls -d processor* | xargs -I {} cp -r 0.orig ./{}/0
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runParallel topoSet
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runParallel `getApplication`
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Reference in New Issue
Block a user