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.

tutorials/combustion/reactingFoam/RAS/SandiaD_LTS/Allclean

@@ -1,11 +0,0 @@
-#!/bin/sh
-cd ${0%/*} || exit 1    # Run from this directory
-
-# Source tutorial clean functions
-. $WM_PROJECT_DIR/bin/tools/CleanFunctions
-
-cleanCase
-
-rm -rf 0
-
-#------------------------------------------------------------------------------

tutorials/combustion/reactingFoam/RAS/SandiaD_LTS/Allrun

@@ -7,9 +7,6 @@ cd ${0%/*} || exit 1    # Run from this directory
 # Set application name
 application=`getApplication`
 
-rm -f 0
-cp -r 0.orig 0
-
 runApplication chemkinToFoam \
                chemkin/grimech30.dat chemkin/thermo30.dat chemkin/transportProperties \
                constant/reactionsGRI constant/thermo.compressibleGasGRI

tutorials/combustion/reactingFoam/RAS/SandiaD_LTS/constant/chemistryProperties

@@ -20,7 +20,7 @@ chemistryType
     method          TDAC;
 }
 
-chemistry       on;
+chemistry       off;
 
 importantSpecies
 {

tutorials/combustion/reactingFoam/RAS/SandiaD_LTS/system/controlDict

@@ -7,13 +7,12 @@
 \*---------------------------------------------------------------------------*/
 FoamFile
 {
-    version         2.0;
+    version         2;
     format          ascii;
     class           dictionary;
     location        "system";
     object          controlDict;
 }
-// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
 
 application     reactingFoam;
 
@@ -23,13 +22,13 @@ startTime       0;
 
 stopAt          endTime;
 
-endTime         6000;
+endTime         1500;
 
 deltaT          1;
 
 writeControl    runTime;
 
-writeInterval   100;
+writeInterval   1500;
 
 purgeWrite      0;
 

tutorials/compressible/rhoCentralFoam/shockTube/Allclean

@@ -1,12 +0,0 @@
-#!/bin/sh
-cd ${0%/*} || exit 1    # Run from this directory
-
-# Source tutorial clean functions
-. $WM_PROJECT_DIR/bin/tools/CleanFunctions
-
-rm -rf 0
-cp -r 0.orig 0
-cleanCase
-cleanSamples
-
-#------------------------------------------------------------------------------

tutorials/compressible/rhoCentralFoam/shockTube/system/setFieldsDict

@@ -15,9 +15,25 @@ FoamFile
 }
 // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
 
-defaultFieldValues ( volVectorFieldValue U (0 0 0) volScalarFieldValue T 348.432 volScalarFieldValue p 100000 );
+defaultFieldValues
+(
+    volVectorFieldValue U (0 0 0)
+    volScalarFieldValue T 348.432
+    volScalarFieldValue p 100000
+);
 
-regions         ( boxToCell { box (0 -1 -1) (5 1 1) ; fieldValues ( volScalarFieldValue T 278.746 volScalarFieldValue p 10000 ) ; } );
+regions
+(
+    boxToCell
+    {
+        box (0 -1 -1) (5 1 1);
+        fieldValues
+        (
+            volScalarFieldValue T 278.746
+            volScalarFieldValue p 10000
+        );
+    }
+);
 
 
 // ************************************************************************* //

tutorials/compressible/sonicFoam/laminar/shockTube/0.orig/T

@@ -1,34 +0,0 @@
-/*--------------------------------*- 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;
-    object      T;
-}
-// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
-
-dimensions      [0 0 0 1 0 0 0];
-
-internalField   uniform 1;
-
-boundaryField
-{
-    sides
-    {
-        type            zeroGradient;
-    }
-
-    empty
-    {
-        type            empty;
-    }
-}
-
-// ************************************************************************* //

tutorials/compressible/sonicFoam/laminar/shockTube/0.orig/U

@@ -1,34 +0,0 @@
-/*--------------------------------*- 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       volVectorField;
-    object      U;
-}
-// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
-
-dimensions      [0 1 -1 0 0 0 0];
-
-internalField   uniform (0 0 0);
-
-boundaryField
-{
-    sides
-    {
-        type            zeroGradient;
-    }
-
-    empty
-    {
-        type            empty;
-    }
-}
-
-// ************************************************************************* //

tutorials/compressible/sonicFoam/laminar/shockTube/0.orig/p

@@ -1,34 +0,0 @@
-/*--------------------------------*- 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;
-    object      p;
-}
-// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
-
-dimensions      [1 -1 -2 0 0 0 0];
-
-internalField   uniform 0;
-
-boundaryField
-{
-    sides
-    {
-        type            zeroGradient;
-    }
-
-    empty
-    {
-        type            empty;
-    }
-}
-
-// ************************************************************************* //

tutorials/compressible/sonicFoam/laminar/shockTube/0/T

@@ -1,34 +0,0 @@
-/*--------------------------------*- 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;
-    object      T;
-}
-// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
-
-dimensions      [0 0 0 1 0 0 0];
-
-internalField   uniform 1;
-
-boundaryField
-{
-    sides
-    {
-        type            zeroGradient;
-    }
-
-    empty
-    {
-        type            empty;
-    }
-}
-
-// ************************************************************************* //

tutorials/compressible/sonicFoam/laminar/shockTube/0/U

@@ -1,34 +0,0 @@
-/*--------------------------------*- 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       volVectorField;
-    object      U;
-}
-// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
-
-dimensions      [0 1 -1 0 0 0 0];
-
-internalField   uniform (0 0 0);
-
-boundaryField
-{
-    sides
-    {
-        type            zeroGradient;
-    }
-
-    empty
-    {
-        type            empty;
-    }
-}
-
-// ************************************************************************* //

tutorials/compressible/sonicFoam/laminar/shockTube/0/p

@@ -1,34 +0,0 @@
-/*--------------------------------*- 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;
-    object      p;
-}
-// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
-
-dimensions      [1 -1 -2 0 0 0 0];
-
-internalField   uniform 0;
-
-boundaryField
-{
-    sides
-    {
-        type            zeroGradient;
-    }
-
-    empty
-    {
-        type            empty;
-    }
-}
-
-// ************************************************************************* //

tutorials/compressible/sonicFoam/laminar/shockTube/Allclean

@@ -1,12 +0,0 @@
-#!/bin/sh
-cd ${0%/*} || exit 1    # Run from this directory
-
-# Source tutorial clean functions
-. $WM_PROJECT_DIR/bin/tools/CleanFunctions
-
-cleanCase
-rm -rf 0
-cp -r 0.orig 0
-cleanSamples
-
-#------------------------------------------------------------------------------

tutorials/incompressible/pimpleFoam/RAS/propeller/Allclean

@@ -4,11 +4,12 @@ cd ${0%/*} || exit 1    # Run from this directory
 # Source tutorial clean functions
 . $WM_PROJECT_DIR/bin/tools/CleanFunctions
 
-# remove surface
+# Remove surface
 rm -f constant/triSurface/propellerTip.obj.gz > /dev/null 2>&1
 
 cleanCase
 
-rm -rf 0 > /dev/null 2>&1
 rm -rf constant/extendedFeatureEdgeMesh > /dev/null 2>&1
 rm -f constant/triSurface/*.eMesh* > /dev/null 2>&1
+
+#------------------------------------------------------------------------------

tutorials/incompressible/pimpleFoam/RAS/propeller/Allrun

@@ -11,3 +11,5 @@ runApplication decomposePar
 runParallel `getApplication`
 
 runApplication reconstructPar
+
+#------------------------------------------------------------------------------

tutorials/incompressible/pimpleFoam/RAS/propeller/Allrun.pre

@@ -30,5 +30,4 @@ runApplication createPatch -overwrite
 # - test by running moveDynamicMes
 #runApplication moveDynamicMesh -checkAMI
 
-# - set the initial fields
+#------------------------------------------------------------------------------
-cp -rf 0.orig 0

tutorials/incompressible/pimpleFoam/RAS/wingMotion/Allclean

@@ -9,8 +9,9 @@ cleanCase
 
 cd ../wingMotion2D_simpleFoam
 cleanCase
-rm -rf 0
 
 cd ../wingMotion2D_pimpleFoam
 cleanCase
-rm -rf 0
+rm -f 0/p 0/nut 0/k 0/omega 0/U 0/pointDisplacement
+
+#------------------------------------------------------------------------------

tutorials/incompressible/pimpleFoam/RAS/wingMotion/Allrun

@@ -13,16 +13,14 @@ runApplication snappyHexMesh -overwrite
 cd ../wingMotion2D_simpleFoam
 runApplication extrudeMesh
 runApplication createPatch -overwrite
-cp -r 0.orig 0
 runApplication simpleFoam
 
 # Copy the mesh from the steady state case and map the results to a
 # mesh motion case, then solve transient.
 cd ../wingMotion2D_pimpleFoam
 cp -r ../wingMotion2D_simpleFoam/constant/polyMesh constant
-cp -r 0.orig 0
 runApplication mapFields ../wingMotion2D_simpleFoam -sourceTime latestTime -consistent
-mv 0/pointDisplacement.unmapped 0/pointDisplacement
+cp pointDisplacement 0/pointDisplacement
 runApplication decomposePar
 runParallel `getApplication`
 runApplication reconstructPar

tutorials/incompressible/pimpleFoam/RAS/wingMotion/wingMotion2D_pimpleFoam/0.orig/U

@@ -1,45 +0,0 @@
-/*--------------------------------*- 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       volVectorField;
-    location    "0";
-    object      U;
-}
-// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
-
-#include        "include/initialConditions"
-
-dimensions      [0 1 -1 0 0 0 0];
-
-internalField   uniform $flowVelocity;
-
-boundaryField
-{
-    #include "include/fixedInlet"
-
-    outlet
-    {
-        type            inletOutlet;
-        inletValue      uniform (0 0 0);
-        value           $internalField;
-    }
-
-    wing
-    {
-        type            movingWallVelocity;
-        value           uniform (0 0 0);
-    }
-
-    #include "include/frontBackTopBottomPatches"
-}
-
-
-// ************************************************************************* //

tutorials/incompressible/pimpleFoam/RAS/wingMotion/wingMotion2D_simpleFoam/0.orig/k

@@ -1,44 +0,0 @@
-/*--------------------------------*- 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;
-    object      k;
-}
-// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
-
-#include        "include/initialConditions"
-
-dimensions      [0 2 -2 0 0 0 0];
-
-internalField   uniform $turbulentKE;
-
-boundaryField
-{
-    #include "include/fixedInlet"
-
-    outlet
-    {
-        type            inletOutlet;
-        inletValue      $internalField;
-        value           $internalField;
-    }
-
-    wing
-    {
-        type            kqRWallFunction;
-        value           $internalField;
-    }
-
-    #include "include/frontBackTopBottomPatches"
-}
-
-
-// ************************************************************************* //

tutorials/incompressible/pimpleFoam/RAS/wingMotion/wingMotion2D_simpleFoam/0.orig/nut

@@ -1,38 +0,0 @@
-/*--------------------------------*- 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      nut;
-}
-// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
-
-dimensions      [0 2 -1 0 0 0 0];
-
-internalField   uniform 0;
-
-boundaryField
-{
-    wing
-    {
-        type            nutkWallFunction;
-        value           uniform 0;
-    }
-
-    "(front|back|topAndBottom|inlet|outlet)"
-    {
-        type            calculated;
-        value           uniform 0;
-    }
-}
-
-
-// ************************************************************************* //

tutorials/incompressible/pimpleFoam/RAS/wingMotion/wingMotion2D_simpleFoam/0.orig/omega

@@ -1,44 +0,0 @@
-/*--------------------------------*- 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;
-    object      epsilon;
-}
-// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
-
-#include        "include/initialConditions"
-
-dimensions      [0 0 -1 0 0 0 0];
-
-internalField   uniform $turbulentOmega;
-
-boundaryField
-{
-    #include "include/fixedInlet"
-
-    outlet
-    {
-        type            inletOutlet;
-        inletValue      $internalField;
-        value           $internalField;
-    }
-
-    wing
-    {
-        type            omegaWallFunction;
-        value           $internalField;
-    }
-
-    #include "include/frontBackTopBottomPatches"
-}
-
-
-// ************************************************************************* //

tutorials/incompressible/pimpleFoam/RAS/wingMotion/wingMotion2D_simpleFoam/0.orig/p

@@ -1,44 +0,0 @@
-/*--------------------------------*- 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;
-    object      p;
-}
-// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
-
-#include        "include/initialConditions"
-
-dimensions      [0 2 -2 0 0 0 0];
-
-internalField   uniform $pressure;
-
-boundaryField
-{
-    inlet
-    {
-        type            zeroGradient;
-    }
-
-    outlet
-    {
-        type            fixedValue;
-        value           $internalField;
-    }
-
-    wing
-    {
-        type            zeroGradient;
-    }
-
-    #include "include/frontBackTopBottomPatches"
-}
-
-// ************************************************************************* //

tutorials/incompressible/pisoFoam/LES/motorBike/motorBike/Allclean

@@ -4,11 +4,9 @@ cd ${0%/*} || exit 1    # Run from this directory
 # Source tutorial clean functions
 . $WM_PROJECT_DIR/bin/tools/CleanFunctions
 
-# remove surface
+# Remove surface
 rm -f constant/triSurface/motorBike.obj.gz
 
-rm -rf 0 > /dev/null 2>&1
-
 cleanCase
 
 # Reset decomposeParDict

tutorials/incompressible/pisoFoam/LES/motorBike/motorBike/Allrun

@@ -7,21 +7,15 @@ cd ${0%/*} || exit 1    # Run from this directory
 # copy motorbike surface from resources directory
 cp $FOAM_TUTORIALS/resources/geometry/motorBike.obj.gz constant/triSurface/
 
-# Make dummy 0 directory
-mkdir 0
-
 runApplication blockMesh
 cp system/decomposeParDict.hierarchical system/decomposeParDict
-runApplication decomposePar
+runApplication decomposePar -copyZero
 
 cp system/decomposeParDict.ptscotch system/decomposeParDict
 runParallel snappyHexMesh -overwrite
 
 find . -type f -iname "*level*" -exec rm {} \;
 
-ls -d processor* | xargs -I {} rm -rf ./{}/0
-ls -d processor* | xargs -I {} cp -r 0.orig ./{}/0
-
 runParallel renumberMesh -overwrite
 
 runParallel potentialFoam -initialiseUBCs

tutorials/incompressible/simpleFoam/turbineSiting/Allclean

@@ -4,8 +4,6 @@ cd ${0%/*} || exit 1    # Run from this directory
 # Source tutorial clean functions
 . $WM_PROJECT_DIR/bin/tools/CleanFunctions
 
-rm -rf 0 > /dev/null 2>&1
-
 cleanCase
 
 # Remove decomposeParDict

tutorials/incompressible/simpleFoam/turbineSiting/Allrun

@@ -4,20 +4,15 @@ cd ${0%/*} || exit 1    # Run from this directory
 # Source tutorial run functions
 . $WM_PROJECT_DIR/bin/tools/RunFunctions
 
-# Make dummy 0 directory
-mkdir 0
-
 runApplication blockMesh
 cp system/decomposeParDict.hierarchical system/decomposeParDict
-runApplication decomposePar
+runApplication decomposePar -copyZero
 
 cp system/decomposeParDict.ptscotch system/decomposeParDict
 runParallel snappyHexMesh -overwrite
 
 find . -type f -iname "*level*" -exec rm {} \;
 
-ls -d processor* | xargs -I {} cp -r 0.orig ./{}/0
-
 runParallel topoSet
 runParallel `getApplication`
 

tutorials/lagrangian/reactingParcelFoam/cylinder/Allclean

@@ -7,7 +7,6 @@ cd ${0%/*} || exit 1    # Run from this directory
 cleanCase
 
 rm -rf constant/wallFilmRegion
-rm -rf 0
 rm -f *.obj
 
 #------------------------------------------------------------------------------

tutorials/lagrangian/reactingParcelFoam/cylinder/Allrun

@@ -8,3 +8,5 @@ cd ${0%/*} || exit 1    # Run from this directory
 application=`getApplication`
 
 runApplication $application
+
+#------------------------------------------------------------------------------

tutorials/lagrangian/reactingParcelFoam/cylinder/Allrun.pre

@@ -1,7 +1,6 @@
 #!/bin/sh
 . $WM_PROJECT_DIR/bin/tools/RunFunctions
 
-cp -rf 0.orig 0
 runApplication blockMesh
 
 #runApplication setSet -batch wallFilmRegion.setSet
@@ -11,3 +10,5 @@ runApplication extrudeToRegionMesh -overwrite
 
 paraFoam -touch
 paraFoam -touch -region wallFilmRegion
+
+#------------------------------------------------------------------------------