Merge branch 'master' into splitCyclic

Conflicts:
	applications/utilities/mesh/advanced/modifyMesh/cellSplitter.C
	applications/utilities/mesh/conversion/fluent3DMeshToFoam/fluent3DMeshToFoam.L
	applications/utilities/mesh/generation/blockMesh/blockMesh.C
	applications/utilities/mesh/generation/blockMesh/createTopology.C
	applications/utilities/mesh/generation/snappyHexMesh/Make/options
	src/OpenFOAM/containers/Lists/ListOps/ListOps.H
	src/OpenFOAM/containers/Lists/ListOps/ListOpsTemplates.C
	src/OpenFOAM/containers/Lists/UList/UList.H
	src/OpenFOAM/containers/Lists/UList/UListI.H
	src/OpenFOAM/fields/pointPatchFields/constraint/processor/processorPointPatchField.C
	src/OpenFOAM/meshes/polyMesh/polyMeshFromShapeMesh.C
	src/OpenFOAM/meshes/polyMesh/polyPatches/basic/coupled/coupledPolyPatch.C
	src/OpenFOAM/meshes/polyMesh/polyPatches/basic/coupled/coupledPolyPatch.H
	src/OpenFOAM/meshes/polyMesh/polyPatches/constraint/cyclic/cyclicPolyPatch.C
	src/OpenFOAM/meshes/polyMesh/polyPatches/constraint/cyclic/cyclicPolyPatch.H
	src/OpenFOAM/meshes/polyMesh/polyPatches/constraint/processor/processorPolyPatch.C
	src/OpenFOAM/meshes/polyMesh/syncTools/syncTools.C
	src/OpenFOAM/meshes/polyMesh/syncTools/syncTools.H
	src/OpenFOAM/meshes/polyMesh/syncTools/syncToolsTemplates.C
	src/autoMesh/autoHexMesh/autoHexMeshDriver/autoLayerDriver.C
	src/autoMesh/autoHexMesh/meshRefinement/meshRefinementBaffles.C
	src/decompositionAgglomeration/Allwmake
	src/decompositionAgglomeration/decompositionMethods/Make/files
	src/decompositionAgglomeration/decompositionMethods/Make/options
	src/dynamicMesh/attachDetach/attachInterface.C
	src/dynamicMesh/polyTopoChange/polyTopoChange/addPatchCellLayer.C
	src/dynamicMesh/polyTopoChange/polyTopoChange/addPatchCellLayer.H
	src/dynamicMesh/polyTopoChange/polyTopoChange/hexRef8.C
	src/dynamicMesh/polyTopoChange/polyTopoChange/polyTopoChange.C
	src/dynamicMesh/polyTopoChange/polyTopoChange/polyTopoChange.H
	src/dynamicMesh/polyTopoChange/polyTopoChange/removePoints.H
	src/dynamicMesh/slidingInterface/coupleSlidingInterface.C
	src/finiteVolume/Make/files
	tutorials/channelOodles/channel395/constant/polyMesh/blockMeshDict
	tutorials/icoFoam/cavity/constant/polyMesh/blockMeshDict
	wmake/rules/linux64Gcc/c++Opt
This commit is contained in:
mattijs
2009-08-07 08:19:53 +01:00
9335 changed files with 762380 additions and 594169 deletions

View File

@ -3,7 +3,7 @@
# ========= |
# \\ / F ield | OpenFOAM: The Open Source CFD Toolbox
# \\ / O peration |
# \\ / A nd | Copyright (C) 1991-2008 OpenCFD Ltd.
# \\ / A nd | Copyright (C) 1991-2009 OpenCFD Ltd.
# \\/ M anipulation |
#------------------------------------------------------------------------------
# License
@ -36,7 +36,7 @@ echo "--------"
echo "Cleaning tutorials ..."
echo "Removing backup files"
find . -type f \( -name "*~" -o -name "*.bak" \) -exec rm {} \;
find . \( -name 'core' -o -name 'core.[1-9]*' \) -exec rm {} \;
find . \( -name core -o -name 'core.[1-9]*' \) -exec rm {} \;
find . \( -name '*.pvs' -o -name '*.OpenFOAM' \) -exec rm {} \;
rm logs testLoopReport > /dev/null 2>&1

View File

@ -3,7 +3,7 @@
# ========= |
# \\ / F ield | OpenFOAM: The Open Source CFD Toolbox
# \\ / O peration |
# \\ / A nd | Copyright (C) 1991-2008 OpenCFD Ltd.
# \\ / A nd | Copyright (C) 1991-2009 OpenCFD Ltd.
# \\/ M anipulation |
#------------------------------------------------------------------------------
# License
@ -48,15 +48,19 @@ logReport () {
UzSS=`grep -E "Uz[:| ]*solution singularity" $1`
completed=`grep -E "^[\t ]*[eE]nd" $1`
if [ "$fatalError" ] ; then
if [ "$fatalError" ]
then
echo "$appAndCase: ** FOAM FATAL ERROR **"
return
elif [ "$UxSS" -a "$UySS" -a "$UzSS" ] ; then
elif [ "$UxSS" -a "$UySS" -a "$UzSS" ]
then
echo "$appAndCase: ** Solution singularity **"
return
elif [ "$completed" ] ; then
elif [ "$completed" ]
then
completionTime=`tail -10 $log | grep Execution | cut -d= -f2 | sed 's/^[ \t]*//'`
if [ "$completionTime" ] ; then
if [ "$completionTime" ]
then
completionTime="in $completionTime"
fi
echo "$appAndCase: completed $completionTime"
@ -90,5 +94,4 @@ done
find . -name "log.*" -exec cat {} \; >> logs
# ----------------------------------------------------------------- end-of-file

View File

@ -3,7 +3,7 @@
# ========= |
# \\ / F ield | OpenFOAM: The Open Source CFD Toolbox
# \\ / O peration |
# \\ / A nd | Copyright (C) 1991-2008 OpenCFD Ltd.
# \\ / A nd | Copyright (C) 1991-2009 OpenCFD Ltd.
# \\/ M anipulation |
#------------------------------------------------------------------------------
# License
@ -27,25 +27,30 @@
# Alltest
#
# Description
# quickly tests the tutorials and writes out the scheme/solver information
#
#------------------------------------------------------------------------------
cd ${0%/*} || exit 1 # run from this directory
# FUNCTIONS
#
printUsage () {
cat <<EOF
Usage: $0
Quickly tests the tutorials and writes out the scheme/solver information
usage() {
while [ "$#" -ge 1 ]; do echo "$1"; shift; done
cat<<USAGE
Options are:
-d sets up a default scheme on all schemes
-h help
EOF
usage: $0 [OPTION]
options:
-d sets up a default scheme on all schemes
-h this usage
* quickly tests the tutorials and writes out the scheme/solver information
USAGE
exit 1
}
setDefaultFvSchemes () {
setDefaultFvSchemes() {
cat<<EOF
gradSchemes { default Gauss linear; }
divSchemes
@ -72,23 +77,27 @@ snGradSchemes { default corrected; }
fluxRequired { default yes; }
EOF
}
#
# VARIABLE
#
MAIN_CONTROL_DICT=
unset MAIN_CONTROL_DICT
for i in \
$HOME/.$WM_PROJECT-$WM_PROJECT_VERSION \
$HOME/.$WM_PROJECT/$WM_PROJECT_VERSION \
$HOME/.$WM_PROJECT \
$WM_PROJECT_DIR/etc \
;
$HOME/.$WM_PROJECT/$WM_PROJECT_VERSION \
$HOME/.$WM_PROJECT \
$WM_PROJECT_DIR/etc \
;
do
if [ -f "$i/controlDict" ]; then
MAIN_CONTROL_DICT="$i/controlDict"
break
fi
if [ -f "$i/controlDict" ]
then
MAIN_CONTROL_DICT="$i/controlDict"
break
fi
done
[ -f "$MAIN_CONTROL_DICT" ] || usage "main controlDict not found"
TUTORIALS_DIR=.
TEST_RUN_DIR=../tutorialsTest
FV_SCHEMES=\
@ -110,16 +119,16 @@ DEFAULT_SCHEMES=0
# OPTIONS
#
OPTS=`getopt hd $*`
if [ $? -ne 0 ] ; then
echo "Aborting due to invalid option"
printUsage
exit 1
if [ $? -ne 0 ]
then
usage "Aborting due to invalid option"
fi
eval set -- "$OPTS"
while [ $1 != -- ]; do
while [ $1 != -- ]
do
case $1 in
-d) DEFAULT_SCHEMES=1;;
-h) printUsage; exit 1;;
-h) usage;;
esac
shift
done
@ -129,14 +138,15 @@ shift
# MAIN
#
if [ -d "$TEST_RUN_DIR" ] ; then
if [ -d "$TEST_RUN_DIR" ]
then
rm -rf $TEST_RUN_DIR
fi
echo "Modifying ${MAIN_CONTROL_DICT}"
if [ -e ${MAIN_CONTROL_DICT}.org ]
then
echo "File " ${MAIN_CONTROL_DICT}.org " already exists"
echo "File ${MAIN_CONTROL_DICT}.org already exists"
echo "Did Alltest fail in some way and then run again?"
exit 1
fi
@ -155,20 +165,21 @@ echo "Copying the tutorials"
cp -a ${TUTORIALS_DIR} ${TEST_RUN_DIR}
echo "Modifying the controlDicts to run only one time step"
cd ${TEST_RUN_DIR}
cd ${TEST_RUN_DIR} || exit 1
for CD in `find . -name "controlDict*"`
do
mv ${CD} ${CD}.org
sed \
-e s/"\(startFrom[ \t]*\)\([a-zA-Z]*\);"/"\1 latestTime;"/g \
-e s/"\(startFrom[ \t]*\)\([a-zA-Z]*\);"/"\1 latestTime;"/g \
-e s/"\(stopAt[ \t]*\)\([a-zA-Z]*\);"/"\1 nextWrite;"/g \
-e s/"\(writeControl[ \t]*\)\([a-zA-Z]*\);"/"\1 timeStep;"/g \
-e s/"\(writeInterval[ \t]*\)\([0-9a-zA-Z.-]*\);"/"\1 1;"/g \
${CD}.org > ${CD}
done
if [ $DEFAULT_SCHEMES = 1 ] ; then
if [ $DEFAULT_SCHEMES = 1 ]
then
echo "Modifying the fvSchemes to contain only default schemes"
for FV_SC in `find . -name fvSchemes`
do
@ -205,7 +216,8 @@ do
done
echo `grep solver ${LOG} | cut -d" " -f4` >> $SOLVERS_TEMP
done
if [ -f $SCHEMES_TEMP ] ; then
if [ -f $SCHEMES_TEMP ]
then
cat $SCHEMES_TEMP | sort -u >> $SCHEMES_FILE
fi
done

View File

@ -0,0 +1,37 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 |
| \\ / 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 (0 0 0);
boundaryField
{
patch0
{
type cyclic;
}
patch1
{
type cyclic;
}
patch2
{
type cyclic;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,40 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object enstrophy;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 -2 0 0 0 0];
internalField uniform 0;
boundaryField
{
patch0
{
type cyclic;
value uniform 0;
}
patch1
{
type cyclic;
value uniform 0;
}
patch2
{
type cyclic;
value uniform 0;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,39 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 |
| \\ / 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
{
patch0
{
type cyclic;
}
patch1
{
type cyclic;
}
patch2
{
type cyclic;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,37 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 |
| \\ / 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 (0 0 0);
boundaryField
{
patch0
{
type cyclic;
}
patch1
{
type cyclic;
}
patch2
{
type cyclic;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,40 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object enstrophy;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 -2 0 0 0 0];
internalField uniform 0;
boundaryField
{
patch0
{
type cyclic;
value uniform 0;
}
patch1
{
type cyclic;
value uniform 0;
}
patch2
{
type cyclic;
value uniform 0;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,39 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 |
| \\ / 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
{
patch0
{
type cyclic;
}
patch1
{
type cyclic;
}
patch2
{
type cyclic;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,11 @@
#!/bin/sh
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
# Get application name
application=`getApplication`
runApplication blockMesh
runApplication boxTurb
runApplication $application
runApplication enstrophy

View File

@ -1,8 +1,8 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\ / O peration | Version: 1.6 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
@ -10,6 +10,7 @@ FoamFile
version 2.0;
format ascii;
class dictionary;
location "constant";
object boxTurbDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
@ -18,4 +19,5 @@ Ea 10;
k0 5;
// ************************************************************************* //

View File

@ -0,0 +1,63 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object blockMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
convertToMeters 1;
vertices
(
(0 0 0)
(1 0 0)
(1 1 0)
(0 1 0)
(0 0 1)
(1 0 1)
(1 1 1)
(0 1 1)
);
blocks
(
hex (0 1 2 3 4 5 6 7) (16 16 16) simpleGrading (1 1 1)
);
edges
(
);
patches
(
cyclic patch0
(
(0 3 2 1)
(4 5 6 7)
)
cyclic patch1
(
(0 4 7 3)
(2 6 5 1)
)
cyclic patch2
(
(3 7 6 2)
(1 5 4 0)
)
);
mergePatchPairs
(
);
// ************************************************************************* //

View File

@ -0,0 +1,43 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class polyBoundaryMesh;
location "constant/polyMesh";
object boundary;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
3
(
patch0
{
type cyclic;
nFaces 512;
startFace 11520;
featureCos 0.9;
}
patch1
{
type cyclic;
nFaces 512;
startFace 12032;
featureCos 0.9;
}
patch2
{
type cyclic;
nFaces 512;
startFace 12544;
featureCos 0.9;
}
)
// ************************************************************************* //

View File

@ -0,0 +1,21 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object transportProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
nu nu [ 0 2 -1 0 0 0 0 ] 0.025;
// ************************************************************************* //

View File

@ -0,0 +1,27 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object turbulenceProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
UOsigma 0.090295;
UOalpha 0.81532;
UOKupper 10;
UOKlower 7;
// ************************************************************************* //

View File

@ -0,0 +1,51 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application dnsFoam;
startFrom startTime;
startTime 0;
stopAt endTime;
endTime 10;
deltaT 0.025;
writeControl runTime;
writeInterval 0.25;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
writeCompression uncompressed;
timeFormat general;
timePrecision 6;
runTimeModifiable yes;
graphFormat raw;
// ************************************************************************* //

View File

@ -0,0 +1,61 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default Euler;
}
gradSchemes
{
default Gauss linear;
grad(p) Gauss linear;
grad(U) Gauss linear;
}
divSchemes
{
default none;
div(phi,U) Gauss cubic;
}
laplacianSchemes
{
default none;
laplacian(nu,U) Gauss linear corrected;
laplacian((1|A(U)),p) Gauss linear corrected;
}
interpolationSchemes
{
default linear;
interpolate(U) linear;
}
snGradSchemes
{
default corrected;
}
fluxRequired
{
default no;
p ;
}
// ************************************************************************* //

View File

@ -0,0 +1,44 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
p
{
solver PCG;
preconditioner DIC;
tolerance 1e-06;
relTol 0;
}
U
{
solver PBiCG;
preconditioner DILU;
tolerance 1e-05;
relTol 0;
}
}
PISO
{
nCorrectors 2;
nNonOrthogonalCorrectors 0;
}
// ************************************************************************* //

View File

@ -1,9 +0,0 @@
EXE_INC = \
-I$(LIB_SRC)/finiteVolume/lnInclude \
-I$(LIB_SRC)/turbulenceModels/RAS \
-I$(LIB_SRC)/transportModels
EXE_LIBS = \
-lincompressibleRASModels \
-lincompressibleTransportModels \
-lfiniteVolume

View File

@ -1,46 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / 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 (0 0 0);
boundaryField
{
rotor
{
type fixedValue;
value uniform (0 0 0);
}
stator
{
type fixedValue;
value uniform (0 0 0);
}
front
{
type empty;
}
back
{
type empty;
}
}
// ************************************************************************* //

View File

@ -1,44 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object epsilon;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -3 0 0 0 0];
internalField uniform 20;
boundaryField
{
rotor
{
type zeroGradient;
}
stator
{
type zeroGradient;
}
front
{
type empty;
}
back
{
type empty;
}
}
// ************************************************************************* //

View File

@ -1,44 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 1;
boundaryField
{
rotor
{
type zeroGradient;
}
stator
{
type zeroGradient;
}
front
{
type empty;
}
back
{
type empty;
}
}
// ************************************************************************* //

View File

@ -1,44 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / 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
{
rotor
{
type zeroGradient;
}
stator
{
type zeroGradient;
}
front
{
type empty;
}
back
{
type empty;
}
}
// ************************************************************************* //

View File

@ -1,9 +0,0 @@
#!/bin/sh
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
application="MRFSimpleFoam"
./makeMesh
runApplication $application

View File

@ -1,28 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object MRFZones;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
1
(
rotor
{
patches (rotor);
origin origin [0 1 0 0 0 0 0] (0 0 0);
axis axis [0 0 0 0 0 0 0] (0 0 1);
omega omega [0 0 -1 0 0 0 0] 104.72;
}
)
// ************************************************************************* //

View File

@ -1,191 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object RASProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
RASModel kEpsilon;
turbulence on;
printCoeffs 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;
}
kOmegaSSTCoeffs
{
alphaK1 0.85034;
alphaK2 1.0;
alphaOmega1 0.5;
alphaOmega2 0.85616;
gamma1 0.5532;
gamma2 0.4403;
beta1 0.0750;
beta2 0.0828;
betaStar 0.09;
a1 0.31;
c1 10;
Cmu 0.09;
}
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;
Cv2 5.0;
}
wallFunctionCoeffs
{
kappa 0.4187;
E 9;
}
// ************************************************************************* //

View File

@ -1,39 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object dynamicMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dynamicFvMeshLib "libtopoChangerFvMesh.so";
dynamicFvMesh mixerFvMesh;
mixerFvMeshCoeffs
{
coordinateSystem
{
type cylindrical;
origin (0 0 0);
axis (0 0 1);
direction (1 0 0);
}
rpm 10;
slider
{
inside insideSlider;
outside outsideSlider;
}
}
// ************************************************************************* //

View File

@ -1,559 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object blockMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// General macros to create 2D/extruded-2D meshes
//define(calc, [esyscmd(echo $1 | bc | tr -d \\n)])
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
convertToMeters 0.1;
// Hub radius
// Impeller-tip radius
// Baffle-tip radius
// Tank radius
// MRF region radius
// Thickness of 2D slab
// Base z
// Top z
// Number of cells radially between hub and impeller tip
// Number of cells radially in each of the two regions between
// impeller and baffle tips
// Number of cells radially between baffle tip and tank
// Number of cells azimuthally in each of the 8 blocks
// Number of cells in the thickness of the slab
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
vertices
(
(0.2 0 0) // Vertex r0b = 0
(0.2 0 0) // Vertex r0sb = 1
(0.141421356364228 -0.141421356110391 0) // Vertex r1b = 2
(3.58979347393082e-10 -0.2 0) // Vertex r2b = 3
(3.58979347393082e-10 -0.2 0) // Vertex r2sb = 4
(-0.141421355856554 -0.141421356618065 0) // Vertex r3b = 5
(-0.2 7.17958694786164e-10 0) // Vertex r4b = 6
(-0.2 7.17958694786164e-10 0) // Vertex r4sb = 7
(-0.141421355856554 0.141421356618065 0) // Vertex r5b = 8
(3.58979347393082e-10 0.2 0) // Vertex r6b = 9
(3.58979347393082e-10 0.2 0) // Vertex r6sb = 10
(0.141421356364228 0.141421356110391 0) // Vertex r7b = 11
(0.5 0 0) // Vertex rb0b = 12
(0.353553390910569 -0.353553390275978 0) // Vertex rb1b = 13
(8.97448368482705e-10 -0.5 0) // Vertex rb2b = 14
(-0.353553389641386 -0.353553391545162 0) // Vertex rb3b = 15
(-0.5 1.79489673696541e-09 0) // Vertex rb4b = 16
(-0.353553389641386 0.353553391545162 0) // Vertex rb5b = 17
(8.97448368482705e-10 0.5 0) // Vertex rb6b = 18
(0.353553390910569 0.353553390275978 0) // Vertex rb7b = 19
(0.6 0 0) // Vertex ri0b = 20
(0.424264069092683 -0.424264068331174 0) // Vertex ri1b = 21
(1.07693804217925e-09 -0.6 0) // Vertex ri2b = 22
(-0.424264067569663 -0.424264069854194 0) // Vertex ri3b = 23
(-0.6 2.15387608435849e-09 0) // Vertex ri4b = 24
(-0.424264067569663 0.424264069854194 0) // Vertex ri5b = 25
(1.07693804217925e-09 0.6 0) // Vertex ri6b = 26
(0.424264069092683 0.424264068331174 0) // Vertex ri7b = 27
(0.7 0 0) // Vertex Rb0b = 28
(0.494974747274797 -0.494974746386369 0) // Vertex Rb1b = 29
(1.25642771587579e-09 -0.7 0) // Vertex Rb2b = 30
(-0.49497474549794 -0.494974748163226 0) // Vertex Rb3b = 31
(-0.7 2.51285543175157e-09 0) // Vertex Rb4b = 32
(-0.49497474549794 0.494974748163226 0) // Vertex Rb5b = 33
(1.25642771587579e-09 0.7 0) // Vertex Rb6b = 34
(0.494974747274797 0.494974746386369 0) // Vertex Rb7b = 35
(1 0 0) // Vertex R0b = 36
(0.707106781821139 -0.707106780551956 0) // Vertex R1b = 37
(0.707106781821139 -0.707106780551956 0) // Vertex R1sb = 38
(1.79489673696541e-09 -1 0) // Vertex R2b = 39
(-0.707106779282772 -0.707106783090323 0) // Vertex R3b = 40
(-0.707106779282772 -0.707106783090323 0) // Vertex R3sb = 41
(-1 3.58979347393082e-09 0) // Vertex R4b = 42
(-0.707106779282772 0.707106783090323 0) // Vertex R5b = 43
(-0.707106779282772 0.707106783090323 0) // Vertex R5sb = 44
(1.79489673696541e-09 1 0) // Vertex R6b = 45
(0.707106781821139 0.707106780551956 0) // Vertex R7b = 46
(0.707106781821139 0.707106780551956 0) // Vertex R7sb = 47
(0.2 0 0.1) // Vertex r0t = 48
(0.2 0 0.1) // Vertex r0st = 49
(0.141421356364228 -0.141421356110391 0.1) // Vertex r1t = 50
(3.58979347393082e-10 -0.2 0.1) // Vertex r2t = 51
(3.58979347393082e-10 -0.2 0.1) // Vertex r2st = 52
(-0.141421355856554 -0.141421356618065 0.1) // Vertex r3t = 53
(-0.2 7.17958694786164e-10 0.1) // Vertex r4t = 54
(-0.2 7.17958694786164e-10 0.1) // Vertex r4st = 55
(-0.141421355856554 0.141421356618065 0.1) // Vertex r5t = 56
(3.58979347393082e-10 0.2 0.1) // Vertex r6t = 57
(3.58979347393082e-10 0.2 0.1) // Vertex r6st = 58
(0.141421356364228 0.141421356110391 0.1) // Vertex r7t = 59
(0.5 0 0.1) // Vertex rb0t = 60
(0.353553390910569 -0.353553390275978 0.1) // Vertex rb1t = 61
(8.97448368482705e-10 -0.5 0.1) // Vertex rb2t = 62
(-0.353553389641386 -0.353553391545162 0.1) // Vertex rb3t = 63
(-0.5 1.79489673696541e-09 0.1) // Vertex rb4t = 64
(-0.353553389641386 0.353553391545162 0.1) // Vertex rb5t = 65
(8.97448368482705e-10 0.5 0.1) // Vertex rb6t = 66
(0.353553390910569 0.353553390275978 0.1) // Vertex rb7t = 67
(0.6 0 0.1) // Vertex ri0t = 68
(0.424264069092683 -0.424264068331174 0.1) // Vertex ri1t = 69
(1.07693804217925e-09 -0.6 0.1) // Vertex ri2t = 70
(-0.424264067569663 -0.424264069854194 0.1) // Vertex ri3t = 71
(-0.6 2.15387608435849e-09 0.1) // Vertex ri4t = 72
(-0.424264067569663 0.424264069854194 0.1) // Vertex ri5t = 73
(1.07693804217925e-09 0.6 0.1) // Vertex ri6t = 74
(0.424264069092683 0.424264068331174 0.1) // Vertex ri7t = 75
(0.7 0 0.1) // Vertex Rb0t = 76
(0.494974747274797 -0.494974746386369 0.1) // Vertex Rb1t = 77
(1.25642771587579e-09 -0.7 0.1) // Vertex Rb2t = 78
(-0.49497474549794 -0.494974748163226 0.1) // Vertex Rb3t = 79
(-0.7 2.51285543175157e-09 0.1) // Vertex Rb4t = 80
(-0.49497474549794 0.494974748163226 0.1) // Vertex Rb5t = 81
(1.25642771587579e-09 0.7 0.1) // Vertex Rb6t = 82
(0.494974747274797 0.494974746386369 0.1) // Vertex Rb7t = 83
(1 0 0.1) // Vertex R0t = 84
(0.707106781821139 -0.707106780551956 0.1) // Vertex R1t = 85
(0.707106781821139 -0.707106780551956 0.1) // Vertex R1st = 86
(1.79489673696541e-09 -1 0.1) // Vertex R2t = 87
(-0.707106779282772 -0.707106783090323 0.1) // Vertex R3t = 88
(-0.707106779282772 -0.707106783090323 0.1) // Vertex R3st = 89
(-1 3.58979347393082e-09 0.1) // Vertex R4t = 90
(-0.707106779282772 0.707106783090323 0.1) // Vertex R5t = 91
(-0.707106779282772 0.707106783090323 0.1) // Vertex R5st = 92
(1.79489673696541e-09 1 0.1) // Vertex R6t = 93
(0.707106781821139 0.707106780551956 0.1) // Vertex R7t = 94
(0.707106781821139 0.707106780551956 0.1) // Vertex R7st = 95
);
blocks
(
// block0
hex (0 2 13 12 48 50 61 60)
rotor
(12 12 1)
simpleGrading (1 1 1)
// block1
hex (2 4 14 13 50 52 62 61)
rotor
(12 12 1)
simpleGrading (1 1 1)
// block2
hex (3 5 15 14 51 53 63 62)
rotor
(12 12 1)
simpleGrading (1 1 1)
// block3
hex (5 7 16 15 53 55 64 63)
rotor
(12 12 1)
simpleGrading (1 1 1)
// block4
hex (6 8 17 16 54 56 65 64)
rotor
(12 12 1)
simpleGrading (1 1 1)
// block5
hex (8 10 18 17 56 58 66 65)
rotor
(12 12 1)
simpleGrading (1 1 1)
// block6
hex (9 11 19 18 57 59 67 66)
rotor
(12 12 1)
simpleGrading (1 1 1)
// block7
hex (11 1 12 19 59 49 60 67)
rotor
(12 12 1)
simpleGrading (1 1 1)
// block0
hex (12 13 21 20 60 61 69 68)
rotor
(12 4 1)
simpleGrading (1 1 1)
// block1
hex (13 14 22 21 61 62 70 69)
rotor
(12 4 1)
simpleGrading (1 1 1)
// block2
hex (14 15 23 22 62 63 71 70)
rotor
(12 4 1)
simpleGrading (1 1 1)
// block3
hex (15 16 24 23 63 64 72 71)
rotor
(12 4 1)
simpleGrading (1 1 1)
// block4
hex (16 17 25 24 64 65 73 72)
rotor
(12 4 1)
simpleGrading (1 1 1)
// block5
hex (17 18 26 25 65 66 74 73)
rotor
(12 4 1)
simpleGrading (1 1 1)
// block6
hex (18 19 27 26 66 67 75 74)
rotor
(12 4 1)
simpleGrading (1 1 1)
// block7
hex (19 12 20 27 67 60 68 75)
rotor
(12 4 1)
simpleGrading (1 1 1)
// block0
hex (20 21 29 28 68 69 77 76)
(12 4 1)
simpleGrading (1 1 1)
// block1
hex (21 22 30 29 69 70 78 77)
(12 4 1)
simpleGrading (1 1 1)
// block2
hex (22 23 31 30 70 71 79 78)
(12 4 1)
simpleGrading (1 1 1)
// block3
hex (23 24 32 31 71 72 80 79)
(12 4 1)
simpleGrading (1 1 1)
// block4
hex (24 25 33 32 72 73 81 80)
(12 4 1)
simpleGrading (1 1 1)
// block5
hex (25 26 34 33 73 74 82 81)
(12 4 1)
simpleGrading (1 1 1)
// block6
hex (26 27 35 34 74 75 83 82)
(12 4 1)
simpleGrading (1 1 1)
// block7
hex (27 20 28 35 75 68 76 83)
(12 4 1)
simpleGrading (1 1 1)
// block0
hex (28 29 38 36 76 77 86 84)
(12 12 1)
simpleGrading (1 1 1)
// block1
hex (29 30 39 37 77 78 87 85)
(12 12 1)
simpleGrading (1 1 1)
// block2
hex (30 31 41 39 78 79 89 87)
(12 12 1)
simpleGrading (1 1 1)
// block3
hex (31 32 42 40 79 80 90 88)
(12 12 1)
simpleGrading (1 1 1)
// block4
hex (32 33 44 42 80 81 92 90)
(12 12 1)
simpleGrading (1 1 1)
// block5
hex (33 34 45 43 81 82 93 91)
(12 12 1)
simpleGrading (1 1 1)
// block6
hex (34 35 47 45 82 83 95 93)
(12 12 1)
simpleGrading (1 1 1)
// block7
hex (35 28 36 46 83 76 84 94)
(12 12 1)
simpleGrading (1 1 1)
);
edges
(
arc 0 2 (0.184775906536601 -0.0765366863901046 0)
arc 2 4 (0.0765366867217582 -0.184775906399226 0)
arc 3 5 (-0.0765366860584508 -0.184775906673977 0)
arc 5 7 (-0.18477590626185 -0.0765366870534118 0)
arc 6 8 (-0.18477590626185 0.0765366870534118 0)
arc 8 10 (-0.0765366860584508 0.184775906673977 0)
arc 9 11 (0.0765366867217582 0.184775906399226 0)
arc 11 1 (0.184775906536601 0.0765366863901046 0)
arc 12 13 (0.461939766341503 -0.191341715975262 0)
arc 13 14 (0.191341716804395 -0.461939765998065 0)
arc 14 15 (-0.191341715146127 -0.461939766684942 0)
arc 15 16 (-0.461939765654626 -0.19134171763353 0)
arc 16 17 (-0.461939765654626 0.19134171763353 0)
arc 17 18 (-0.191341715146127 0.461939766684942 0)
arc 18 19 (0.191341716804395 0.461939765998065 0)
arc 19 12 (0.461939766341503 0.191341715975262 0)
arc 20 21 (0.554327719609804 -0.229610059170314 0)
arc 21 22 (0.229610060165275 -0.554327719197677 0)
arc 22 23 (-0.229610058175352 -0.55432772002193 0)
arc 23 24 (-0.554327718785551 -0.229610061160235 0)
arc 24 25 (-0.554327718785551 0.229610061160235 0)
arc 25 26 (-0.229610058175352 0.55432772002193 0)
arc 26 27 (0.229610060165275 0.554327719197677 0)
arc 27 20 (0.554327719609804 0.229610059170314 0)
arc 28 29 (0.646715672878104 -0.267878402365366 0)
arc 29 30 (0.267878403526154 -0.64671567239729 0)
arc 30 31 (-0.267878401204578 -0.646715673358918 0)
arc 31 32 (-0.646715671916476 -0.267878404686941 0)
arc 32 33 (-0.646715671916476 0.267878404686941 0)
arc 33 34 (-0.267878401204578 0.646715673358918 0)
arc 34 35 (0.267878403526154 0.64671567239729 0)
arc 35 28 (0.646715672878104 0.267878402365366 0)
arc 36 38 (0.923879532683006 -0.382683431950523 0)
arc 37 39 (0.382683433608791 -0.923879531996129 0)
arc 39 41 (-0.382683430292254 -0.923879533369883 0)
arc 40 42 (-0.923879531309252 -0.382683435267059 0)
arc 42 44 (-0.923879531309252 0.382683435267059 0)
arc 43 45 (-0.382683430292254 0.923879533369883 0)
arc 45 47 (0.382683433608791 0.923879531996129 0)
arc 46 36 (0.923879532683006 0.382683431950523 0)
arc 48 50 (0.184775906536601 -0.0765366863901046 0.1)
arc 50 52 (0.0765366867217582 -0.184775906399226 0.1)
arc 51 53 (-0.0765366860584508 -0.184775906673977 0.1)
arc 53 55 (-0.18477590626185 -0.0765366870534118 0.1)
arc 54 56 (-0.18477590626185 0.0765366870534118 0.1)
arc 56 58 (-0.0765366860584508 0.184775906673977 0.1)
arc 57 59 (0.0765366867217582 0.184775906399226 0.1)
arc 59 49 (0.184775906536601 0.0765366863901046 0.1)
arc 60 61 (0.461939766341503 -0.191341715975262 0.1)
arc 61 62 (0.191341716804395 -0.461939765998065 0.1)
arc 62 63 (-0.191341715146127 -0.461939766684942 0.1)
arc 63 64 (-0.461939765654626 -0.19134171763353 0.1)
arc 64 65 (-0.461939765654626 0.19134171763353 0.1)
arc 65 66 (-0.191341715146127 0.461939766684942 0.1)
arc 66 67 (0.191341716804395 0.461939765998065 0.1)
arc 67 60 (0.461939766341503 0.191341715975262 0.1)
arc 68 69 (0.554327719609804 -0.229610059170314 0.1)
arc 69 70 (0.229610060165275 -0.554327719197677 0.1)
arc 70 71 (-0.229610058175352 -0.55432772002193 0.1)
arc 71 72 (-0.554327718785551 -0.229610061160235 0.1)
arc 72 73 (-0.554327718785551 0.229610061160235 0.1)
arc 73 74 (-0.229610058175352 0.55432772002193 0.1)
arc 74 75 (0.229610060165275 0.554327719197677 0.1)
arc 75 68 (0.554327719609804 0.229610059170314 0.1)
arc 76 77 (0.646715672878104 -0.267878402365366 0.1)
arc 77 78 (0.267878403526154 -0.64671567239729 0.1)
arc 78 79 (-0.267878401204578 -0.646715673358918 0.1)
arc 79 80 (-0.646715671916476 -0.267878404686941 0.1)
arc 80 81 (-0.646715671916476 0.267878404686941 0.1)
arc 81 82 (-0.267878401204578 0.646715673358918 0.1)
arc 82 83 (0.267878403526154 0.64671567239729 0.1)
arc 83 76 (0.646715672878104 0.267878402365366 0.1)
arc 84 86 (0.923879532683006 -0.382683431950523 0.1)
arc 85 87 (0.382683433608791 -0.923879531996129 0.1)
arc 87 89 (-0.382683430292254 -0.923879533369883 0.1)
arc 88 90 (-0.923879531309252 -0.382683435267059 0.1)
arc 90 92 (-0.923879531309252 0.382683435267059 0.1)
arc 91 93 (-0.382683430292254 0.923879533369883 0.1)
arc 93 95 (0.382683433608791 0.923879531996129 0.1)
arc 94 84 (0.923879532683006 0.382683431950523 0.1)
);
patches
(
wall rotor
(
(0 2 50 48)
(2 4 52 50)
(3 5 53 51)
(5 7 55 53)
(6 8 56 54)
(8 10 58 56)
(9 11 59 57)
(11 1 49 59)
(0 12 60 48)
(1 12 60 49)
(3 14 62 51)
(4 14 62 52)
(6 16 64 54)
(7 16 64 55)
(9 18 66 57)
(10 18 66 58)
)
wall stator
(
(36 38 86 84)
(37 39 87 85)
(39 41 89 87)
(40 42 90 88)
(42 44 92 90)
(43 45 93 91)
(45 47 95 93)
(46 36 84 94)
(37 29 77 85)
(38 29 77 86)
(40 31 79 88)
(41 31 79 89)
(43 33 81 91)
(44 33 81 92)
(46 35 83 94)
(47 35 83 95)
)
empty front
(
(48 50 61 60)
(50 52 62 61)
(51 53 63 62)
(53 55 64 63)
(54 56 65 64)
(56 58 66 65)
(57 59 67 66)
(59 49 60 67)
(60 61 69 68)
(61 62 70 69)
(62 63 71 70)
(63 64 72 71)
(64 65 73 72)
(65 66 74 73)
(66 67 75 74)
(67 60 68 75)
(68 69 77 76)
(69 70 78 77)
(70 71 79 78)
(71 72 80 79)
(72 73 81 80)
(73 74 82 81)
(74 75 83 82)
(75 68 76 83)
(76 77 86 84)
(77 78 87 85)
(78 79 89 87)
(79 80 90 88)
(80 81 92 90)
(81 82 93 91)
(82 83 95 93)
(83 76 84 94)
)
empty back
(
(0 12 13 2)
(2 13 14 4)
(3 14 15 5)
(5 15 16 7)
(6 16 17 8)
(8 17 18 10)
(9 18 19 11)
(11 19 12 1)
(12 20 21 13)
(13 21 22 14)
(14 22 23 15)
(15 23 24 16)
(16 24 25 17)
(17 25 26 18)
(18 26 27 19)
(19 27 20 12)
(20 28 29 21)
(21 29 30 22)
(22 30 31 23)
(23 31 32 24)
(24 32 33 25)
(25 33 34 26)
(26 34 35 27)
(27 35 28 20)
(28 36 38 29)
(29 37 39 30)
(30 39 41 31)
(31 40 42 32)
(32 42 44 33)
(33 43 45 34)
(34 45 47 35)
(35 46 36 28)
)
);
// ************************************************************************* //

View File

@ -1,818 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
`format' ascii;
class dictionary;
object blockMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// General macros to create 2D/extruded-2D meshes
changecom(//)changequote([,])
define(calc, [esyscmd(perl -e 'print ($1)')])
define(VCOUNT, 0)
define(vlabel, [[// ]Vertex $1 = VCOUNT define($1, VCOUNT)define([VCOUNT], incr(VCOUNT))])
define(pi, 3.14159265)
define(hex2D, hex ($1b $2b $3b $4b $1t $2t $3t $4t))
define(quad2D, ($1b $2b $2t $1t))
define(frontQuad, ($1t $2t $3t $4t))
define(backQuad, ($1b $4b $3b $2b))
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
convertToMeters 0.1;
// Hub radius
define(r, 0.2)
// Impeller-tip radius
define(rb, 0.5)
// Baffle-tip radius
define(Rb, 0.7)
// Tank radius
define(R, 1)
// MRF region radius
define(ri, calc(0.5*(rb + Rb)))
// Thickness of 2D slab
define(z, 0.1)
// Base z
define(Zb, 0)
// Top z
define(Zt, calc(Zb + z))
// Number of cells radially between hub and impeller tip
define(Nr, 12)
// Number of cells radially in each of the two regions between
// impeller and baffle tips
define(Ni, 4)
// Number of cells radially between baffle tip and tank
define(NR, 12)
// Number of cells azimuthally in each of the 8 blocks
define(Na, 12)
// Number of cells in the thickness of the slab
define(Nz, 1)
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
define(vert, (x$1$2 y$1$2 $3))
define(evert, (ex$1$2 ey$1$2 $3))
define(a0, 0)
define(a1, -45)
define(a2, -90)
define(a3, -135)
define(a4, 180)
define(a5, 135)
define(a6, 90)
define(a7, 45)
define(ea0, -22.5)
define(ea1, -67.5)
define(ea2, -112.5)
define(ea3, -157.5)
define(ea4, 157.5)
define(ea5, 112.5)
define(ea6, 67.5)
define(ea7, 22.5)
define(ca0, calc(cos((pi/180)*a0)))
define(ca1, calc(cos((pi/180)*a1)))
define(ca2, calc(cos((pi/180)*a2)))
define(ca3, calc(cos((pi/180)*a3)))
define(ca4, calc(cos((pi/180)*a4)))
define(ca5, calc(cos((pi/180)*a5)))
define(ca6, calc(cos((pi/180)*a6)))
define(ca7, calc(cos((pi/180)*a7)))
define(sa0, calc(sin((pi/180)*a0)))
define(sa1, calc(sin((pi/180)*a1)))
define(sa2, calc(sin((pi/180)*a2)))
define(sa3, calc(sin((pi/180)*a3)))
define(sa4, calc(sin((pi/180)*a4)))
define(sa5, calc(sin((pi/180)*a5)))
define(sa6, calc(sin((pi/180)*a6)))
define(sa7, calc(sin((pi/180)*a7)))
define(cea0, calc(cos((pi/180)*ea0)))
define(cea1, calc(cos((pi/180)*ea1)))
define(cea2, calc(cos((pi/180)*ea2)))
define(cea3, calc(cos((pi/180)*ea3)))
define(cea4, calc(cos((pi/180)*ea4)))
define(cea5, calc(cos((pi/180)*ea5)))
define(cea6, calc(cos((pi/180)*ea6)))
define(cea7, calc(cos((pi/180)*ea7)))
define(sea0, calc(sin((pi/180)*ea0)))
define(sea1, calc(sin((pi/180)*ea1)))
define(sea2, calc(sin((pi/180)*ea2)))
define(sea3, calc(sin((pi/180)*ea3)))
define(sea4, calc(sin((pi/180)*ea4)))
define(sea5, calc(sin((pi/180)*ea5)))
define(sea6, calc(sin((pi/180)*ea6)))
define(sea7, calc(sin((pi/180)*ea7)))
define(x00, calc(r*ca0))
define(x01, calc(r*ca1))
define(x02, calc(r*ca2))
define(x03, calc(r*ca3))
define(x04, calc(r*ca4))
define(x05, calc(r*ca5))
define(x06, calc(r*ca6))
define(x07, calc(r*ca7))
define(x10, calc(rb*ca0))
define(x11, calc(rb*ca1))
define(x12, calc(rb*ca2))
define(x13, calc(rb*ca3))
define(x14, calc(rb*ca4))
define(x15, calc(rb*ca5))
define(x16, calc(rb*ca6))
define(x17, calc(rb*ca7))
define(x20, calc(ri*ca0))
define(x21, calc(ri*ca1))
define(x22, calc(ri*ca2))
define(x23, calc(ri*ca3))
define(x24, calc(ri*ca4))
define(x25, calc(ri*ca5))
define(x26, calc(ri*ca6))
define(x27, calc(ri*ca7))
define(x30, calc(Rb*ca0))
define(x31, calc(Rb*ca1))
define(x32, calc(Rb*ca2))
define(x33, calc(Rb*ca3))
define(x34, calc(Rb*ca4))
define(x35, calc(Rb*ca5))
define(x36, calc(Rb*ca6))
define(x37, calc(Rb*ca7))
define(x40, calc(R*ca0))
define(x41, calc(R*ca1))
define(x42, calc(R*ca2))
define(x43, calc(R*ca3))
define(x44, calc(R*ca4))
define(x45, calc(R*ca5))
define(x46, calc(R*ca6))
define(x47, calc(R*ca7))
define(y00, calc(r*sa0))
define(y01, calc(r*sa1))
define(y02, calc(r*sa2))
define(y03, calc(r*sa3))
define(y04, calc(r*sa4))
define(y05, calc(r*sa5))
define(y06, calc(r*sa6))
define(y07, calc(r*sa7))
define(y10, calc(rb*sa0))
define(y11, calc(rb*sa1))
define(y12, calc(rb*sa2))
define(y13, calc(rb*sa3))
define(y14, calc(rb*sa4))
define(y15, calc(rb*sa5))
define(y16, calc(rb*sa6))
define(y17, calc(rb*sa7))
define(y20, calc(ri*sa0))
define(y21, calc(ri*sa1))
define(y22, calc(ri*sa2))
define(y23, calc(ri*sa3))
define(y24, calc(ri*sa4))
define(y25, calc(ri*sa5))
define(y26, calc(ri*sa6))
define(y27, calc(ri*sa7))
define(y30, calc(Rb*sa0))
define(y31, calc(Rb*sa1))
define(y32, calc(Rb*sa2))
define(y33, calc(Rb*sa3))
define(y34, calc(Rb*sa4))
define(y35, calc(Rb*sa5))
define(y36, calc(Rb*sa6))
define(y37, calc(Rb*sa7))
define(y40, calc(R*sa0))
define(y41, calc(R*sa1))
define(y42, calc(R*sa2))
define(y43, calc(R*sa3))
define(y44, calc(R*sa4))
define(y45, calc(R*sa5))
define(y46, calc(R*sa6))
define(y47, calc(R*sa7))
define(ex00, calc(r*cea0))
define(ex01, calc(r*cea1))
define(ex02, calc(r*cea2))
define(ex03, calc(r*cea3))
define(ex04, calc(r*cea4))
define(ex05, calc(r*cea5))
define(ex06, calc(r*cea6))
define(ex07, calc(r*cea7))
define(ex10, calc(rb*cea0))
define(ex11, calc(rb*cea1))
define(ex12, calc(rb*cea2))
define(ex13, calc(rb*cea3))
define(ex14, calc(rb*cea4))
define(ex15, calc(rb*cea5))
define(ex16, calc(rb*cea6))
define(ex17, calc(rb*cea7))
define(ex20, calc(ri*cea0))
define(ex21, calc(ri*cea1))
define(ex22, calc(ri*cea2))
define(ex23, calc(ri*cea3))
define(ex24, calc(ri*cea4))
define(ex25, calc(ri*cea5))
define(ex26, calc(ri*cea6))
define(ex27, calc(ri*cea7))
define(ex30, calc(Rb*cea0))
define(ex31, calc(Rb*cea1))
define(ex32, calc(Rb*cea2))
define(ex33, calc(Rb*cea3))
define(ex34, calc(Rb*cea4))
define(ex35, calc(Rb*cea5))
define(ex36, calc(Rb*cea6))
define(ex37, calc(Rb*cea7))
define(ex40, calc(R*cea0))
define(ex41, calc(R*cea1))
define(ex42, calc(R*cea2))
define(ex43, calc(R*cea3))
define(ex44, calc(R*cea4))
define(ex45, calc(R*cea5))
define(ex46, calc(R*cea6))
define(ex47, calc(R*cea7))
define(ey00, calc(r*sea0))
define(ey01, calc(r*sea1))
define(ey02, calc(r*sea2))
define(ey03, calc(r*sea3))
define(ey04, calc(r*sea4))
define(ey05, calc(r*sea5))
define(ey06, calc(r*sea6))
define(ey07, calc(r*sea7))
define(ey10, calc(rb*sea0))
define(ey11, calc(rb*sea1))
define(ey12, calc(rb*sea2))
define(ey13, calc(rb*sea3))
define(ey14, calc(rb*sea4))
define(ey15, calc(rb*sea5))
define(ey16, calc(rb*sea6))
define(ey17, calc(rb*sea7))
define(ey20, calc(ri*sea0))
define(ey21, calc(ri*sea1))
define(ey22, calc(ri*sea2))
define(ey23, calc(ri*sea3))
define(ey24, calc(ri*sea4))
define(ey25, calc(ri*sea5))
define(ey26, calc(ri*sea6))
define(ey27, calc(ri*sea7))
define(ey30, calc(Rb*sea0))
define(ey31, calc(Rb*sea1))
define(ey32, calc(Rb*sea2))
define(ey33, calc(Rb*sea3))
define(ey34, calc(Rb*sea4))
define(ey35, calc(Rb*sea5))
define(ey36, calc(Rb*sea6))
define(ey37, calc(Rb*sea7))
define(ey40, calc(R*sea0))
define(ey41, calc(R*sea1))
define(ey42, calc(R*sea2))
define(ey43, calc(R*sea3))
define(ey44, calc(R*sea4))
define(ey45, calc(R*sea5))
define(ey46, calc(R*sea6))
define(ey47, calc(R*sea7))
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
vertices
(
vert(0, 0, Zb) vlabel(r0b)
vert(0, 0, Zb) vlabel(r0sb)
vert(0, 1, Zb) vlabel(r1b)
vert(0, 2, Zb) vlabel(r2b)
vert(0, 2, Zb) vlabel(r2sb)
vert(0, 3, Zb) vlabel(r3b)
vert(0, 4, Zb) vlabel(r4b)
vert(0, 4, Zb) vlabel(r4sb)
vert(0, 5, Zb) vlabel(r5b)
vert(0, 6, Zb) vlabel(r6b)
vert(0, 6, Zb) vlabel(r6sb)
vert(0, 7, Zb) vlabel(r7b)
vert(1, 0, Zb) vlabel(rb0b)
vert(1, 1, Zb) vlabel(rb1b)
vert(1, 2, Zb) vlabel(rb2b)
vert(1, 3, Zb) vlabel(rb3b)
vert(1, 4, Zb) vlabel(rb4b)
vert(1, 5, Zb) vlabel(rb5b)
vert(1, 6, Zb) vlabel(rb6b)
vert(1, 7, Zb) vlabel(rb7b)
vert(2, 0, Zb) vlabel(ri0b)
vert(2, 1, Zb) vlabel(ri1b)
vert(2, 2, Zb) vlabel(ri2b)
vert(2, 3, Zb) vlabel(ri3b)
vert(2, 4, Zb) vlabel(ri4b)
vert(2, 5, Zb) vlabel(ri5b)
vert(2, 6, Zb) vlabel(ri6b)
vert(2, 7, Zb) vlabel(ri7b)
vert(3, 0, Zb) vlabel(Rb0b)
vert(3, 1, Zb) vlabel(Rb1b)
vert(3, 2, Zb) vlabel(Rb2b)
vert(3, 3, Zb) vlabel(Rb3b)
vert(3, 4, Zb) vlabel(Rb4b)
vert(3, 5, Zb) vlabel(Rb5b)
vert(3, 6, Zb) vlabel(Rb6b)
vert(3, 7, Zb) vlabel(Rb7b)
vert(4, 0, Zb) vlabel(R0b)
vert(4, 1, Zb) vlabel(R1b)
vert(4, 1, Zb) vlabel(R1sb)
vert(4, 2, Zb) vlabel(R2b)
vert(4, 3, Zb) vlabel(R3b)
vert(4, 3, Zb) vlabel(R3sb)
vert(4, 4, Zb) vlabel(R4b)
vert(4, 5, Zb) vlabel(R5b)
vert(4, 5, Zb) vlabel(R5sb)
vert(4, 6, Zb) vlabel(R6b)
vert(4, 7, Zb) vlabel(R7b)
vert(4, 7, Zb) vlabel(R7sb)
vert(0, 0, Zt) vlabel(r0t)
vert(0, 0, Zt) vlabel(r0st)
vert(0, 1, Zt) vlabel(r1t)
vert(0, 2, Zt) vlabel(r2t)
vert(0, 2, Zt) vlabel(r2st)
vert(0, 3, Zt) vlabel(r3t)
vert(0, 4, Zt) vlabel(r4t)
vert(0, 4, Zt) vlabel(r4st)
vert(0, 5, Zt) vlabel(r5t)
vert(0, 6, Zt) vlabel(r6t)
vert(0, 6, Zt) vlabel(r6st)
vert(0, 7, Zt) vlabel(r7t)
vert(1, 0, Zt) vlabel(rb0t)
vert(1, 1, Zt) vlabel(rb1t)
vert(1, 2, Zt) vlabel(rb2t)
vert(1, 3, Zt) vlabel(rb3t)
vert(1, 4, Zt) vlabel(rb4t)
vert(1, 5, Zt) vlabel(rb5t)
vert(1, 6, Zt) vlabel(rb6t)
vert(1, 7, Zt) vlabel(rb7t)
vert(2, 0, Zt) vlabel(ri0t)
vert(2, 1, Zt) vlabel(ri1t)
vert(2, 2, Zt) vlabel(ri2t)
vert(2, 3, Zt) vlabel(ri3t)
vert(2, 4, Zt) vlabel(ri4t)
vert(2, 5, Zt) vlabel(ri5t)
vert(2, 6, Zt) vlabel(ri6t)
vert(2, 7, Zt) vlabel(ri7t)
vert(3, 0, Zt) vlabel(Rb0t)
vert(3, 1, Zt) vlabel(Rb1t)
vert(3, 2, Zt) vlabel(Rb2t)
vert(3, 3, Zt) vlabel(Rb3t)
vert(3, 4, Zt) vlabel(Rb4t)
vert(3, 5, Zt) vlabel(Rb5t)
vert(3, 6, Zt) vlabel(Rb6t)
vert(3, 7, Zt) vlabel(Rb7t)
vert(4, 0, Zt) vlabel(R0t)
vert(4, 1, Zt) vlabel(R1t)
vert(4, 1, Zt) vlabel(R1st)
vert(4, 2, Zt) vlabel(R2t)
vert(4, 3, Zt) vlabel(R3t)
vert(4, 3, Zt) vlabel(R3st)
vert(4, 4, Zt) vlabel(R4t)
vert(4, 5, Zt) vlabel(R5t)
vert(4, 5, Zt) vlabel(R5st)
vert(4, 6, Zt) vlabel(R6t)
vert(4, 7, Zt) vlabel(R7t)
vert(4, 7, Zt) vlabel(R7st)
);
blocks
(
// block0
hex2D(r0, r1, rb1, rb0)
rotor
(Na Nr Nz)
simpleGrading (1 1 1)
// block1
hex2D(r1, r2s, rb2, rb1)
rotor
(Na Nr Nz)
simpleGrading (1 1 1)
// block2
hex2D(r2, r3, rb3, rb2)
rotor
(Na Nr Nz)
simpleGrading (1 1 1)
// block3
hex2D(r3, r4s, rb4, rb3)
rotor
(Na Nr Nz)
simpleGrading (1 1 1)
// block4
hex2D(r4, r5, rb5, rb4)
rotor
(Na Nr Nz)
simpleGrading (1 1 1)
// block5
hex2D(r5, r6s, rb6, rb5)
rotor
(Na Nr Nz)
simpleGrading (1 1 1)
// block6
hex2D(r6, r7, rb7, rb6)
rotor
(Na Nr Nz)
simpleGrading (1 1 1)
// block7
hex2D(r7, r0s, rb0, rb7)
rotor
(Na Nr Nz)
simpleGrading (1 1 1)
// block0
hex2D(rb0, rb1, ri1, ri0)
rotor
(Na Ni Nz)
simpleGrading (1 1 1)
// block1
hex2D(rb1, rb2, ri2, ri1)
rotor
(Na Ni Nz)
simpleGrading (1 1 1)
// block2
hex2D(rb2, rb3, ri3, ri2)
rotor
(Na Ni Nz)
simpleGrading (1 1 1)
// block3
hex2D(rb3, rb4, ri4, ri3)
rotor
(Na Ni Nz)
simpleGrading (1 1 1)
// block4
hex2D(rb4, rb5, ri5, ri4)
rotor
(Na Ni Nz)
simpleGrading (1 1 1)
// block5
hex2D(rb5, rb6, ri6, ri5)
rotor
(Na Ni Nz)
simpleGrading (1 1 1)
// block6
hex2D(rb6, rb7, ri7, ri6)
rotor
(Na Ni Nz)
simpleGrading (1 1 1)
// block7
hex2D(rb7, rb0, ri0, ri7)
rotor
(Na Ni Nz)
simpleGrading (1 1 1)
// block0
hex2D(ri0, ri1, Rb1, Rb0)
(Na Ni Nz)
simpleGrading (1 1 1)
// block1
hex2D(ri1, ri2, Rb2, Rb1)
(Na Ni Nz)
simpleGrading (1 1 1)
// block2
hex2D(ri2, ri3, Rb3, Rb2)
(Na Ni Nz)
simpleGrading (1 1 1)
// block3
hex2D(ri3, ri4, Rb4, Rb3)
(Na Ni Nz)
simpleGrading (1 1 1)
// block4
hex2D(ri4, ri5, Rb5, Rb4)
(Na Ni Nz)
simpleGrading (1 1 1)
// block5
hex2D(ri5, ri6, Rb6, Rb5)
(Na Ni Nz)
simpleGrading (1 1 1)
// block6
hex2D(ri6, ri7, Rb7, Rb6)
(Na Ni Nz)
simpleGrading (1 1 1)
// block7
hex2D(ri7, ri0, Rb0, Rb7)
(Na Ni Nz)
simpleGrading (1 1 1)
// block0
hex2D(Rb0, Rb1, R1s, R0)
(Na NR Nz)
simpleGrading (1 1 1)
// block1
hex2D(Rb1, Rb2, R2, R1)
(Na NR Nz)
simpleGrading (1 1 1)
// block2
hex2D(Rb2, Rb3, R3s, R2)
(Na NR Nz)
simpleGrading (1 1 1)
// block3
hex2D(Rb3, Rb4, R4, R3)
(Na NR Nz)
simpleGrading (1 1 1)
// block4
hex2D(Rb4, Rb5, R5s, R4)
(Na NR Nz)
simpleGrading (1 1 1)
// block5
hex2D(Rb5, Rb6, R6, R5)
(Na NR Nz)
simpleGrading (1 1 1)
// block6
hex2D(Rb6, Rb7, R7s, R6)
(Na NR Nz)
simpleGrading (1 1 1)
// block7
hex2D(Rb7, Rb0, R0, R7)
(Na NR Nz)
simpleGrading (1 1 1)
);
edges
(
arc r0b r1b evert(0, 0, Zb)
arc r1b r2sb evert(0, 1, Zb)
arc r2b r3b evert(0, 2, Zb)
arc r3b r4sb evert(0, 3, Zb)
arc r4b r5b evert(0, 4, Zb)
arc r5b r6sb evert(0, 5, Zb)
arc r6b r7b evert(0, 6, Zb)
arc r7b r0sb evert(0, 7, Zb)
arc rb0b rb1b evert(1, 0, Zb)
arc rb1b rb2b evert(1, 1, Zb)
arc rb2b rb3b evert(1, 2, Zb)
arc rb3b rb4b evert(1, 3, Zb)
arc rb4b rb5b evert(1, 4, Zb)
arc rb5b rb6b evert(1, 5, Zb)
arc rb6b rb7b evert(1, 6, Zb)
arc rb7b rb0b evert(1, 7, Zb)
arc ri0b ri1b evert(2, 0, Zb)
arc ri1b ri2b evert(2, 1, Zb)
arc ri2b ri3b evert(2, 2, Zb)
arc ri3b ri4b evert(2, 3, Zb)
arc ri4b ri5b evert(2, 4, Zb)
arc ri5b ri6b evert(2, 5, Zb)
arc ri6b ri7b evert(2, 6, Zb)
arc ri7b ri0b evert(2, 7, Zb)
arc Rb0b Rb1b evert(3, 0, Zb)
arc Rb1b Rb2b evert(3, 1, Zb)
arc Rb2b Rb3b evert(3, 2, Zb)
arc Rb3b Rb4b evert(3, 3, Zb)
arc Rb4b Rb5b evert(3, 4, Zb)
arc Rb5b Rb6b evert(3, 5, Zb)
arc Rb6b Rb7b evert(3, 6, Zb)
arc Rb7b Rb0b evert(3, 7, Zb)
arc R0b R1sb evert(4, 0, Zb)
arc R1b R2b evert(4, 1, Zb)
arc R2b R3sb evert(4, 2, Zb)
arc R3b R4b evert(4, 3, Zb)
arc R4b R5sb evert(4, 4, Zb)
arc R5b R6b evert(4, 5, Zb)
arc R6b R7sb evert(4, 6, Zb)
arc R7b R0b evert(4, 7, Zb)
arc r0t r1t evert(0, 0, Zt)
arc r1t r2st evert(0, 1, Zt)
arc r2t r3t evert(0, 2, Zt)
arc r3t r4st evert(0, 3, Zt)
arc r4t r5t evert(0, 4, Zt)
arc r5t r6st evert(0, 5, Zt)
arc r6t r7t evert(0, 6, Zt)
arc r7t r0st evert(0, 7, Zt)
arc rb0t rb1t evert(1, 0, Zt)
arc rb1t rb2t evert(1, 1, Zt)
arc rb2t rb3t evert(1, 2, Zt)
arc rb3t rb4t evert(1, 3, Zt)
arc rb4t rb5t evert(1, 4, Zt)
arc rb5t rb6t evert(1, 5, Zt)
arc rb6t rb7t evert(1, 6, Zt)
arc rb7t rb0t evert(1, 7, Zt)
arc ri0t ri1t evert(2, 0, Zt)
arc ri1t ri2t evert(2, 1, Zt)
arc ri2t ri3t evert(2, 2, Zt)
arc ri3t ri4t evert(2, 3, Zt)
arc ri4t ri5t evert(2, 4, Zt)
arc ri5t ri6t evert(2, 5, Zt)
arc ri6t ri7t evert(2, 6, Zt)
arc ri7t ri0t evert(2, 7, Zt)
arc Rb0t Rb1t evert(3, 0, Zt)
arc Rb1t Rb2t evert(3, 1, Zt)
arc Rb2t Rb3t evert(3, 2, Zt)
arc Rb3t Rb4t evert(3, 3, Zt)
arc Rb4t Rb5t evert(3, 4, Zt)
arc Rb5t Rb6t evert(3, 5, Zt)
arc Rb6t Rb7t evert(3, 6, Zt)
arc Rb7t Rb0t evert(3, 7, Zt)
arc R0t R1st evert(4, 0, Zt)
arc R1t R2t evert(4, 1, Zt)
arc R2t R3st evert(4, 2, Zt)
arc R3t R4t evert(4, 3, Zt)
arc R4t R5st evert(4, 4, Zt)
arc R5t R6t evert(4, 5, Zt)
arc R6t R7st evert(4, 6, Zt)
arc R7t R0t evert(4, 7, Zt)
);
patches
(
wall rotor
(
quad2D(r0, r1)
quad2D(r1, r2s)
quad2D(r2, r3)
quad2D(r3, r4s)
quad2D(r4, r5)
quad2D(r5, r6s)
quad2D(r6, r7)
quad2D(r7, r0s)
quad2D(r0, rb0)
quad2D(r0s, rb0)
quad2D(r2, rb2)
quad2D(r2s, rb2)
quad2D(r4, rb4)
quad2D(r4s, rb4)
quad2D(r6, rb6)
quad2D(r6s, rb6)
)
wall stator
(
quad2D(R0, R1s)
quad2D(R1, R2)
quad2D(R2, R3s)
quad2D(R3, R4)
quad2D(R4, R5s)
quad2D(R5, R6)
quad2D(R6, R7s)
quad2D(R7, R0)
quad2D(R1, Rb1)
quad2D(R1s, Rb1)
quad2D(R3, Rb3)
quad2D(R3s, Rb3)
quad2D(R5, Rb5)
quad2D(R5s, Rb5)
quad2D(R7, Rb7)
quad2D(R7s, Rb7)
)
empty front
(
frontQuad(r0, r1, rb1, rb0)
frontQuad(r1, r2s, rb2, rb1)
frontQuad(r2, r3, rb3, rb2)
frontQuad(r3, r4s, rb4, rb3)
frontQuad(r4, r5, rb5, rb4)
frontQuad(r5, r6s, rb6, rb5)
frontQuad(r6, r7, rb7, rb6)
frontQuad(r7, r0s, rb0, rb7)
frontQuad(rb0, rb1, ri1, ri0)
frontQuad(rb1, rb2, ri2, ri1)
frontQuad(rb2, rb3, ri3, ri2)
frontQuad(rb3, rb4, ri4, ri3)
frontQuad(rb4, rb5, ri5, ri4)
frontQuad(rb5, rb6, ri6, ri5)
frontQuad(rb6, rb7, ri7, ri6)
frontQuad(rb7, rb0, ri0, ri7)
frontQuad(ri0, ri1, Rb1, Rb0)
frontQuad(ri1, ri2, Rb2, Rb1)
frontQuad(ri2, ri3, Rb3, Rb2)
frontQuad(ri3, ri4, Rb4, Rb3)
frontQuad(ri4, ri5, Rb5, Rb4)
frontQuad(ri5, ri6, Rb6, Rb5)
frontQuad(ri6, ri7, Rb7, Rb6)
frontQuad(ri7, ri0, Rb0, Rb7)
frontQuad(Rb0, Rb1, R1s, R0)
frontQuad(Rb1, Rb2, R2, R1)
frontQuad(Rb2, Rb3, R3s, R2)
frontQuad(Rb3, Rb4, R4, R3)
frontQuad(Rb4, Rb5, R5s, R4)
frontQuad(Rb5, Rb6, R6, R5)
frontQuad(Rb6, Rb7, R7s, R6)
frontQuad(Rb7, Rb0, R0, R7)
)
empty back
(
backQuad(r0, r1, rb1, rb0)
backQuad(r1, r2s, rb2, rb1)
backQuad(r2, r3, rb3, rb2)
backQuad(r3, r4s, rb4, rb3)
backQuad(r4, r5, rb5, rb4)
backQuad(r5, r6s, rb6, rb5)
backQuad(r6, r7, rb7, rb6)
backQuad(r7, r0s, rb0, rb7)
backQuad(rb0, rb1, ri1, ri0)
backQuad(rb1, rb2, ri2, ri1)
backQuad(rb2, rb3, ri3, ri2)
backQuad(rb3, rb4, ri4, ri3)
backQuad(rb4, rb5, ri5, ri4)
backQuad(rb5, rb6, ri6, ri5)
backQuad(rb6, rb7, ri7, ri6)
backQuad(rb7, rb0, ri0, ri7)
backQuad(ri0, ri1, Rb1, Rb0)
backQuad(ri1, ri2, Rb2, Rb1)
backQuad(ri2, ri3, Rb3, Rb2)
backQuad(ri3, ri4, Rb4, Rb3)
backQuad(ri4, ri5, Rb5, Rb4)
backQuad(ri5, ri6, Rb6, Rb5)
backQuad(ri6, ri7, Rb7, Rb6)
backQuad(ri7, ri0, Rb0, Rb7)
backQuad(Rb0, Rb1, R1s, R0)
backQuad(Rb1, Rb2, R2, R1)
backQuad(Rb2, Rb3, R3s, R2)
backQuad(Rb3, Rb4, R4, R3)
backQuad(Rb4, Rb5, R5s, R4)
backQuad(Rb5, Rb6, R6, R5)
backQuad(Rb6, Rb7, R7s, R6)
backQuad(Rb7, Rb0, R0, R7)
)
);
// ************************************************************************* //

View File

@ -1,48 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class polyBoundaryMesh;
object boundary;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
4
(
rotor
{
type wall;
nFaces 192;
startFace 5952;
}
stator
{
type wall;
nFaces 192;
startFace 6144;
}
front
{
type empty;
nFaces 3072;
startFace 6336;
}
back
{
type empty;
nFaces 3072;
startFace 9408;
}
)
// ************************************************************************* //

View File

@ -1,37 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object transportProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
transportModel Newtonian;
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;
}
// ************************************************************************* //

View File

@ -1,10 +0,0 @@
#!/bin/sh
m4 < constant/polyMesh/blockMeshDict.m4 > constant/polyMesh/blockMeshDict
blockMesh
cellSet
cp system/faceSetDict_rotorFaces system/faceSetDict
faceSet
cp system/faceSetDict_noBoundaryFaces system/faceSetDict
faceSet
setsToZones -noFlipMap

View File

@ -1,36 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object cellSetDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// Name of set to operate on
name rotor;
// One of clear/new/invert/add/delete|subset/list
action new;
// Actions to apply to cellSet. These are all the topoSetSource's ending
// in ..ToCell (see the meshTools library).
topoSetSources
(
// Cells in cell zone
zoneToCell
{
name rotor; // name of cellZone
}
);
// ************************************************************************* //

View File

@ -1,47 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application simpleFoam;
startFrom startTime;
startTime 0;
stopAt endTime;
endTime 500;
deltaT 1;
writeControl timeStep;
writeInterval 50;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
writeCompression uncompressed;
timeFormat general;
timePrecision 6;
runTimeModifiable yes;
// ************************************************************************* //

View File

@ -1,33 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object faceSetDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// Name of set to operate on
name rotor;
// One of clear/new/invert/add/delete|subset/list
action delete;
// Actions to apply to pointSet. These are all the topoSetSource's ending
// in ..ToFace (see the meshTools library).
topoSetSources
(
// Select boundary faces
boundaryToFace
{
}
);
// ************************************************************************* //

View File

@ -1,33 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object faceSetDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// Name of set to operate on
name rotor;
// One of clear/new/invert/add/delete|subset/list
action delete;
// Actions to apply to pointSet. These are all the topoSetSource's ending
// in ..ToFace (see the meshTools library).
topoSetSources
(
// Select boundary faces
boundaryToFace
{
}
);
// ************************************************************************* //

View File

@ -1,35 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object faceSetDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// Name of set to operate on
name rotor;
// One of clear/new/invert/add/delete|subset/list
action new;
// Actions to apply to pointSet. These are all the topoSetSource's ending
// in ..ToFace (see the meshTools library).
topoSetSources
(
// Select based on cellSet
cellToFace
{
set rotor;
option all; // All faces of cells
}
);
// ************************************************************************* //

View File

@ -1,64 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default steadyState;
}
gradSchemes
{
default Gauss linear;
grad(p) Gauss linear;
grad(U) Gauss linear;
}
divSchemes
{
default none;
div(phi,U) Gauss limitedLinearV 1;
div(phi,k) Gauss limitedLinear 1;
div(phi,epsilon) Gauss limitedLinear 1;
div((nuEff*dev(grad(U).T()))) Gauss linear;
}
laplacianSchemes
{
default none;
laplacian(nuEff,U) Gauss linear corrected;
laplacian((1|A(U)),p) Gauss linear corrected;
laplacian(DkEff,k) Gauss linear corrected;
laplacian(DepsilonEff,epsilon) Gauss linear corrected;
}
interpolationSchemes
{
default linear;
interpolate(U) linear;
}
snGradSchemes
{
default corrected;
}
fluxRequired
{
default no;
p;
}
// ************************************************************************* //

View File

@ -1,73 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
p GAMG
{
tolerance 1e-8;
relTol 0.05;
smoother GaussSeidel;
cacheAgglomeration true;
nCellsInCoarsestLevel 20;
agglomerator faceAreaPair;
mergeLevels 1;
};
U smoothSolver
{
smoother GaussSeidel;
nSweeps 2;
tolerance 1e-7;
relTol 0.1;
};
k smoothSolver
{
smoother GaussSeidel;
nSweeps 2;
tolerance 1e-7;
relTol 0.1;
};
epsilon smoothSolver
{
smoother GaussSeidel;
nSweeps 2;
tolerance 1e-7;
relTol 0.1;
};
}
SIMPLE
{
nNonOrthogonalCorrectors 0;
pRefCell 0;
pRefValue 0;
}
relaxationFactors
{
p 0.3;
U 0.5;
k 0.5;
epsilon 0.5;
}
// ************************************************************************* //

View File

@ -1,28 +0,0 @@
#!/bin/sh
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
# Get application name from directory
application=`basename $PWD`
setControlDict () {
controlDict="system/controlDict"
sed \
-e s/"\(deltaT[ \t]*\) 5e-06;"/"\1 1e-05;"/g \
-e s/"\(endTime[ \t]*\) 0.005;"/"\1 0.015;"/g \
-e s/"\(writeInterval[ \t]*\) 10;"/"\1 50;"/g \
$controlDict > temp.$$
mv temp.$$ $controlDict
}
# Do moriyoshiHomogeneous
(cd moriyoshiHomogeneous && foamRunTutorials)
# Clone case
cloneCase moriyoshiHomogeneous moriyoshiHomogeneousPart2
# Modify and execute
cd moriyoshiHomogeneousPart2
cp -r ../moriyoshiHomogeneous/0.005 .
setControlDict
runApplication $application
cd ..

View File

@ -1,49 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object Su;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform 0.434;
boundaryField
{
left
{
type symmetryPlane;
}
right
{
type symmetryPlane;
}
top
{
type symmetryPlane;
}
bottom
{
type symmetryPlane;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

View File

@ -1,49 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://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 300;
boundaryField
{
left
{
type symmetryPlane;
}
right
{
type symmetryPlane;
}
top
{
type symmetryPlane;
}
bottom
{
type symmetryPlane;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

View File

@ -1,49 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object Tu;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 1 0 0 0];
internalField uniform 300;
boundaryField
{
left
{
type symmetryPlane;
}
right
{
type symmetryPlane;
}
top
{
type symmetryPlane;
}
bottom
{
type symmetryPlane;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

View File

@ -1,49 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / 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 (0 0 0);
boundaryField
{
left
{
type symmetryPlane;
}
right
{
type symmetryPlane;
}
top
{
type symmetryPlane;
}
bottom
{
type symmetryPlane;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

View File

@ -1,49 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object Xi;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 1;
boundaryField
{
left
{
type symmetryPlane;
}
right
{
type symmetryPlane;
}
top
{
type symmetryPlane;
}
bottom
{
type symmetryPlane;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

View File

@ -1,49 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object b;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 1;
boundaryField
{
left
{
type symmetryPlane;
}
right
{
type symmetryPlane;
}
top
{
type symmetryPlane;
}
bottom
{
type symmetryPlane;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

View File

@ -1,49 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object epsilon;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -3 0 0 0 0];
internalField uniform 375;
boundaryField
{
left
{
type symmetryPlane;
}
right
{
type symmetryPlane;
}
top
{
type symmetryPlane;
}
bottom
{
type symmetryPlane;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

View File

@ -1,49 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object ft;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0.06;
boundaryField
{
left
{
type symmetryPlane;
}
right
{
type symmetryPlane;
}
top
{
type symmetryPlane;
}
bottom
{
type symmetryPlane;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

View File

@ -1,49 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object fu;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0;
boundaryField
{
left
{
type symmetryPlane;
}
right
{
type symmetryPlane;
}
top
{
type symmetryPlane;
}
bottom
{
type symmetryPlane;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

View File

@ -1,49 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 1.5;
boundaryField
{
left
{
type symmetryPlane;
}
right
{
type symmetryPlane;
}
top
{
type symmetryPlane;
}
bottom
{
type symmetryPlane;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

View File

@ -1,49 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://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 118000;
boundaryField
{
left
{
type symmetryPlane;
}
right
{
type symmetryPlane;
}
top
{
type symmetryPlane;
}
bottom
{
type symmetryPlane;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

View File

@ -1,98 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object RASProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
RASModel LaunderSharmaKE;
turbulence on;
printCoeffs on;
laminarCoeffs
{
}
kEpsilonCoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
C3 0;
alphah 1.111;
alphak 1;
alphaEps 0.76923;
}
RNGkEpsilonCoeffs
{
Cmu 0.0845;
C1 1.42;
C2 1.68;
C3 0;
alphah 1.111;
alphak 1.39;
alphaEps 1.39;
eta0 4.38;
beta 0.012;
}
LaunderSharmaKECoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
C3 0;
alphah 1.111;
alphak 1;
alphaEps 0.76923;
}
LRRCoeffs
{
Cmu 0.09;
Clrr1 1.8;
Clrr2 0.6;
C1 1.44;
C2 1.92;
Cs 0.25;
Ceps 0.15;
alphah 1;
alphaEps 0.76923;
alphaR 1.22;
}
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;
alphah 1;
alphaEps 0.76923;
alphaR 1.22;
}
wallFunctionCoeffs
{
kappa 0.4187;
E 9;
}
// ************************************************************************* //

View File

@ -1,90 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object combustionProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
laminarFlameSpeedCorrelation Gulders;
fuel Propane;
Su Su [0 1 -1 0 0 0 0] 0.434;
SuModel unstrained;
equivalenceRatio equivalenceRatio [0 0 0 0 0 0 0] 1;
sigmaExt sigmaExt [0 0 -1 0 0 0 0] 100000;
XiModel transport;
XiCoef XiCoef [0 0 0 0 0 0 0] 0.62;
XiShapeCoef XiShapeCoef [0 0 0 0 0 0 0] 1;
uPrimeCoef uPrimeCoef [0 0 0 0 0 0 0] 1;
GuldersCoeffs
{
Methane
{
W 0.422;
eta 0.15;
xi 5.18;
alpha 2;
beta -0.5;
f 2.3;
}
Propane
{
W 0.446;
eta 0.12;
xi 4.95;
alpha 1.77;
beta -0.2;
f 2.3;
}
IsoOctane
{
W 0.4658;
eta -0.326;
xi 4.48;
alpha 1.56;
beta -0.22;
f 2.3;
}
}
ignite yes;
ignitionSites
(
{
location (0 0 0.0005);
diameter 0.003;
start 0;
duration 0.001;
strength 1;
}
);
ignitionSphereFraction 1;
ignitionThickness ignitionThickness [0 1 0 0 0 0 0] 0.001;
ignitionCircleFraction 0.5;
ignitionKernelArea ignitionKernelArea [0 2 0 0 0 0 0] 0.001;
// ************************************************************************* //

View File

@ -1,19 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object environmentalProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
g g [0 1 -2 0 0 0 0] (0 0 0);
// ************************************************************************* //

View File

@ -1,69 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object blockMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
convertToMeters 0.001;
vertices
(
(0 0 0)
(0 35 0)
(70 0 0)
(70 35 0)
(0 0 1)
(0 35 1)
(70 0 1)
(70 35 1)
);
blocks
(
hex (0 2 3 1 4 6 7 5) (70 35 1) simpleGrading (1 1 1)
);
edges
(
);
patches
(
symmetryPlane left
(
(0 4 5 1)
)
symmetryPlane right
(
(2 3 7 6)
)
symmetryPlane top
(
(1 5 7 3)
)
symmetryPlane bottom
(
(0 2 6 4)
)
empty frontAndBack
(
(4 5 7 6)
(0 1 3 2)
)
);
mergePatchPairs
(
);
// ************************************************************************* //

View File

@ -1,51 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class polyBoundaryMesh;
object boundary;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
5
(
left
{
type symmetryPlane;
nFaces 35;
startFace 4795;
}
right
{
type symmetryPlane;
nFaces 35;
startFace 4830;
}
top
{
type symmetryPlane;
nFaces 70;
startFace 4865;
}
bottom
{
type symmetryPlane;
nFaces 70;
startFace 4935;
}
frontAndBack
{
type empty;
nFaces 4900;
startFace 5005;
}
)
// ************************************************************************* //

View File

@ -1,31 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object thermophysicalProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
thermoType hhuMixtureThermo<homogeneousMixture<sutherlandTransport<specieThermo<janafThermo<perfectGas>>>>>;
stoichiometricAirFuelMassRatio stoichiometricAirFuelMassRatio [0 0 0 0 0 0 0] 15.675;
fuel fuel 1 44.0962 200 5000 1000 7.53414 0.0188722 -6.27185e-06 9.14756e-10 -4.78381e-14 -16467.5 -17.8923 0.933554 0.0264246 6.10597e-06 -2.19775e-08 9.51493e-12 -13958.5 19.2017 1.67212e-06 170.672;
oxidant oxidant 1 28.8504 200 6000 1000 3.10205 0.00123963 -4.17512e-07 6.60292e-11 -3.87448e-15 -985.517 5.35187 3.58378 -0.0007269 1.66985e-06 -1.08452e-10 -4.31951e-13 -1050.53 3.11223 1.67212e-06 170.672;
reactants reactants 24.8095 29.4649 200 5000 1000 3.28069 0.00195035 -6.53483e-07 1.00239e-10 -5.64653e-15 -1609.55 4.41496 3.47696 0.000367499 1.84866e-06 -9.8993e-10 -3.10214e-14 -1570.81 3.76075 1.67212e-06 170.672;
products products 1 28.3233 200 5000 1000 3.106 0.00179682 -5.94382e-07 9.04998e-11 -5.08033e-15 -11003.7 5.11872 3.49612 0.000650364 -2.08029e-07 1.2291e-09 -7.73697e-13 -11080.3 3.18978 1.67212e-06 170.672;
burntProducts burntProducts 25.8095 28.3233 200 6000 1000 3.106 0.00179682 -5.94382e-07 9.04998e-11 -5.08033e-15 -11003.7 5.11872 3.49612 0.000650364 -2.08029e-07 1.2291e-09 -7.73697e-13 -11080.3 3.18978 1.67212e-06 170.672;
// ************************************************************************* //

View File

@ -1,53 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application XiFoam;
startFrom latestTime;
startTime 0;
stopAt endTime;
endTime 0.005;
deltaT 5e-06;
writeControl timeStep;
writeInterval 20;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
writeCompression uncompressed;
timeFormat general;
timePrecision 6;
runTimeModifiable yes;
adjustTimeStep no;
maxCo 0.2;
maxDeltaT 1;
// ************************************************************************* //

View File

@ -1,85 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default Euler;
}
gradSchemes
{
default Gauss linear;
grad(p) Gauss linear;
}
divSchemes
{
default none;
div(phi,U) Gauss limitedLinearV 1;
div(phid,p) Gauss limitedLinear 1;
div(phiU,p) Gauss linear;
div(phi,k) Gauss limitedLinear 1;
div(phi,epsilon) Gauss limitedLinear 1;
div(phi,R) Gauss limitedLinear 1;
div(R) Gauss linear;
div(phiXi,Xi) Gauss limitedLinear 1;
div(phiXi,Su) Gauss limitedLinear 1;
div(phiSt,b) Gauss limitedLinear01 1;
div(phi,ft_b_h_hu) Gauss multivariateSelection
{
fu limitedLinear01 1;
ft limitedLinear01 1;
b limitedLinear01 1;
h limitedLinear 1;
hu limitedLinear 1;
};
div(U) Gauss linear;
div((Su*grad(b))) Gauss linear;
div((U+((Su*Xi)*grad(b)))) Gauss linear;
div((muEff*dev2(grad(U).T()))) Gauss linear;
}
laplacianSchemes
{
default none;
laplacian(muEff,U) Gauss linear corrected;
laplacian(DkEff,k) Gauss linear corrected;
laplacian(DepsilonEff,epsilon) Gauss linear corrected;
laplacian(DREff,R) Gauss linear corrected;
laplacian((rho*(1|A(U))),p) Gauss linear corrected;
laplacian(muEff,b) Gauss linear corrected;
laplacian(muEff,ft) Gauss linear corrected;
laplacian(alphaEff,h) Gauss linear corrected;
laplacian(alphaEff,hu) Gauss linear corrected;
}
interpolationSchemes
{
default linear;
}
snGradSchemes
{
default corrected;
}
fluxRequired
{
default no;
p;
}
// ************************************************************************* //

View File

@ -1,106 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
rho PCG
{
preconditioner DIC;
tolerance 1e-05;
relTol 0;
};
U PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0;
};
p PCG
{
preconditioner DIC;
tolerance 1e-06;
relTol 0;
};
ft PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0;
};
fu PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0;
};
b PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0;
};
Xi PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0;
};
Su PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0;
};
h PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0;
};
hu PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0;
};
R PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0;
};
k PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0;
};
epsilon PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0;
};
}
PISO
{
nCorrectors 2;
nNonOrthogonalCorrectors 0;
momentumPredictor yes;
}
// ************************************************************************* //

View File

@ -1,50 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volTensorField;
object B;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -2 0 0 0 0];
internalField uniform (0 0 0 0 0 0 0 0 0);
boundaryField
{
inlet
{
type fixedValue;
value uniform (0 0 0 0 0 0 0 0 0);
}
outlet
{
type zeroGradient;
}
upperWall
{
type zeroGradient;
}
lowerWall
{
type zeroGradient;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

View File

@ -1,52 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object Su;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform 0.135;
boundaryField
{
inlet
{
type fixedValue;
value uniform 0.135;
}
outlet
{
type inletOutlet;
inletValue uniform 0.135;
value uniform 0.135;
}
upperWall
{
type zeroGradient;
}
lowerWall
{
type zeroGradient;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

View File

@ -1,54 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://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 293;
boundaryField
{
inlet
{
type fixedValue;
value uniform 293;
}
outlet
{
type inletOutlet;
inletValue uniform 293;
value uniform 293;
}
upperWall
{
type fixedValue;
value uniform 293;
}
lowerWall
{
type fixedValue;
value uniform 293;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

View File

@ -1,54 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object Tu;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 1 0 0 0];
internalField uniform 293;
boundaryField
{
inlet
{
type fixedValue;
value uniform 293;
}
outlet
{
type inletOutlet;
inletValue uniform 293;
value uniform 293;
}
upperWall
{
type fixedValue;
value uniform 293;
}
lowerWall
{
type fixedValue;
value uniform 293;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

View File

@ -1,55 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / 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 (0 0 0);
boundaryField
{
inlet
{
type turbulentInlet;
referenceField uniform (13.3 0 0);
fluctuationScale (0.04 0.02 0.02);
}
outlet
{
type inletOutlet;
inletValue uniform (0 0 0);
value uniform (0 0 0);
}
upperWall
{
type fixedValue;
value uniform (0 0 0);
}
lowerWall
{
type fixedValue;
value uniform (0 0 0);
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

View File

@ -1,52 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object Xi;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 1;
boundaryField
{
inlet
{
type fixedValue;
value uniform 1;
}
outlet
{
type inletOutlet;
inletValue uniform 1;
value uniform 1;
}
upperWall
{
type zeroGradient;
}
lowerWall
{
type zeroGradient;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

View File

@ -1,52 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object b;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 1;
boundaryField
{
inlet
{
type fixedValue;
value uniform 1;
}
outlet
{
type inletOutlet;
inletValue uniform 1;
value uniform 1;
}
upperWall
{
type zeroGradient;
}
lowerWall
{
type zeroGradient;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

View File

@ -1,52 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object ft;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0;
boundaryField
{
inlet
{
type fixedValue;
value uniform 0;
}
outlet
{
type inletOutlet;
inletValue uniform 0;
value uniform 0;
}
upperWall
{
type zeroGradient;
}
lowerWall
{
type zeroGradient;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

View File

@ -1,54 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 2e-05;
boundaryField
{
inlet
{
type fixedValue;
value uniform 2e-05;
}
outlet
{
type inletOutlet;
inletValue uniform 2e-05;
value uniform 2e-05;
}
upperWall
{
type fixedValue;
value uniform 1e-8;
}
lowerWall
{
type fixedValue;
value uniform 1e-8;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

View File

@ -1,49 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object muSgs;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
inlet
{
type zeroGradient;
}
outlet
{
type zeroGradient;
}
upperWall
{
type zeroGradient;
}
lowerWall
{
type zeroGradient;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

View File

@ -1,50 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://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 100000;
boundaryField
{
inlet
{
type zeroGradient;
}
outlet
{
type fixedValue;
value uniform 100000;
}
upperWall
{
type zeroGradient;
}
lowerWall
{
type zeroGradient;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

View File

@ -1,120 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object LESProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
LESModel oneEqEddy;
delta cubeRootVol;
printCoeffs on;
laminarCoeffs
{
}
oneEqEddyCoeffs
{
ce 1.048;
ck 0.094;
}
dynOneEqEddyCoeffs
{
ce 1.05;
filter simple;
}
lowReOneEqEddyCoeffs
{
ck 0.07;
ce 1.05;
beta 0.01;
}
SmagorinskyCoeffs
{
ck 0.02;
ce 0.202;
}
DeardorffDiffStressCoeffs
{
ce 1.048;
ck 0.094;
cm 4.13;
}
cubeRootVolCoeffs
{
deltaCoeff 1;
}
PrandtlCoeffs
{
delta cubeRootVol;
cubeRootVolCoeffs
{
deltaCoeff 1;
}
smoothCoeffs
{
delta cubeRootVol;
cubeRootVolCoeffs
{
deltaCoeff 1;
}
maxDeltaRatio 1.1;
}
Cdelta 0.158;
}
vanDriestCoeffs
{
delta cubeRootVol;
cubeRootVolCoeffs
{
deltaCoeff 1;
}
smoothCoeffs
{
delta cubeRootVol;
cubeRootVolCoeffs
{
deltaCoeff 1;
}
maxDeltaRatio 1.1;
}
Aplus 26;
Cdelta 0.158;
}
smoothCoeffs
{
delta cubeRootVol;
cubeRootVolCoeffs
{
deltaCoeff 1;
}
maxDeltaRatio 1.1;
}
kappa 0.4187;
wallFunctionCoeffs
{
E 9;
}
// ************************************************************************* //

View File

@ -1,82 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object combustionProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
laminarFlameSpeedCorrelation constant;
fuel Propane;
Su Su [0 1 -1 0 0 0 0] 0.135;
SuModel transport;
equivalenceRatio equivalenceRatio [0 0 0 0 0 0 0] 0.6;
sigmaExt sigmaExt [0 0 -1 0 0 0 0] 338;
XiModel transport;
XiCoef XiCoef [0 0 0 0 0 0 0] 0.62;
XiShapeCoef XiShapeCoef [0 0 0 0 0 0 0] 1;
uPrimeCoef uPrimeCoef [0 0 0 0 0 0 0] 1;
GuldersCoeffs
{
Methane
{
W 0.422;
eta 0.15;
xi 5.18;
alpha 2;
beta -0.5;
f 2.3;
}
Propane
{
W 0.446;
eta 0.12;
xi 4.95;
alpha 1.77;
beta -0.2;
f 2.3;
}
IsoOctane
{
W 0.4658;
eta -0.326;
xi 4.48;
alpha 1.56;
beta -0.22;
f 2.3;
}
}
ignite no;
ignitionSites
(
);
ignitionSphereFraction 0;
ignitionThickness ignitionThickness [0 1 0 0 0 0 0] 0;
ignitionCircleFraction 0;
ignitionKernelArea ignitionKernelArea [0 2 0 0 0 0 0] 0;
// ************************************************************************* //

View File

@ -1,19 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object environmentalProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
g g [0 1 -2 0 0 0 0] (0 -9.81 0);
// ************************************************************************* //

View File

@ -1,153 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object blockMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
convertToMeters 0.001;
vertices
(
(-20.6 0 -0.5)
(-20.6 3 -0.5)
(-20.6 12.7 -0.5)
(-20.6 25.4 -0.5)
(0 -25.4 -0.5)
(0 -5 -0.5)
(0 0 -0.5)
(0 3 -0.5)
(0 12.7 -0.5)
(0 25.4 -0.5)
(206 -25.4 -0.5)
(206 -8.5 -0.5)
(206 0 -0.5)
(206 6.5 -0.5)
(206 17 -0.5)
(206 25.4 -0.5)
(290 -16.6 -0.5)
(290 -6.3 -0.5)
(290 0 -0.5)
(290 4.5 -0.5)
(290 11 -0.5)
(290 16.6 -0.5)
(-20.6 0 0.5)
(-20.6 3 0.5)
(-20.6 12.7 0.5)
(-20.6 25.4 0.5)
(0 -25.4 0.5)
(0 -5 0.5)
(0 0 0.5)
(0 3 0.5)
(0 12.7 0.5)
(0 25.4 0.5)
(206 -25.4 0.5)
(206 -8.5 0.5)
(206 0 0.5)
(206 6.5 0.5)
(206 17 0.5)
(206 25.4 0.5)
(290 -16.6 0.5)
(290 -6.3 0.5)
(290 0 0.5)
(290 4.5 0.5)
(290 11 0.5)
(290 16.6 0.5)
);
blocks
(
hex (0 6 7 1 22 28 29 23) (18 7 1) simpleGrading (0.5 1.8 1)
hex (1 7 8 2 23 29 30 24) (18 10 1) simpleGrading (0.5 4 1)
hex (2 8 9 3 24 30 31 25) (18 13 1) simpleGrading (0.5 0.25 1)
hex (4 10 11 5 26 32 33 27) (180 18 1) simpleGrading (4 1 1)
hex (5 11 12 6 27 33 34 28) (180 9 1) edgeGrading (4 4 4 4 0.5 1 1 0.5 1 1 1 1)
hex (6 12 13 7 28 34 35 29) (180 7 1) edgeGrading (4 4 4 4 1.8 1 1 1.8 1 1 1 1)
hex (7 13 14 8 29 35 36 30) (180 10 1) edgeGrading (4 4 4 4 4 1 1 4 1 1 1 1)
hex (8 14 15 9 30 36 37 31) (180 13 1) simpleGrading (4 0.25 1)
hex (10 16 17 11 32 38 39 33) (25 18 1) simpleGrading (2.5 1 1)
hex (11 17 18 12 33 39 40 34) (25 9 1) simpleGrading (2.5 1 1)
hex (12 18 19 13 34 40 41 35) (25 7 1) simpleGrading (2.5 1 1)
hex (13 19 20 14 35 41 42 36) (25 10 1) simpleGrading (2.5 1 1)
hex (14 20 21 15 36 42 43 37) (25 13 1) simpleGrading (2.5 0.25 1)
);
edges
(
);
patches
(
patch inlet
(
(0 22 23 1)
(1 23 24 2)
(2 24 25 3)
)
patch outlet
(
(16 17 39 38)
(17 18 40 39)
(18 19 41 40)
(19 20 42 41)
(20 21 43 42)
)
wall upperWall
(
(3 25 31 9)
(9 31 37 15)
(15 37 43 21)
)
wall lowerWall
(
(0 6 28 22)
(6 5 27 28)
(5 4 26 27)
(4 10 32 26)
(10 16 38 32)
)
empty frontAndBack
(
(22 28 29 23)
(23 29 30 24)
(24 30 31 25)
(26 32 33 27)
(27 33 34 28)
(28 34 35 29)
(29 35 36 30)
(30 36 37 31)
(32 38 39 33)
(33 39 40 34)
(34 40 41 35)
(35 41 42 36)
(36 42 43 37)
(0 1 7 6)
(1 2 8 7)
(2 3 9 8)
(4 5 11 10)
(5 6 12 11)
(6 7 13 12)
(7 8 14 13)
(8 9 15 14)
(10 11 17 16)
(11 12 18 17)
(12 13 19 18)
(13 14 20 19)
(14 15 21 20)
)
);
mergePatchPairs
(
);
// ************************************************************************* //

View File

@ -1,55 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class polyBoundaryMesh;
object boundary;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
5
(
inlet
{
type patch;
nFaces 30;
startFace 24170;
}
outlet
{
type patch;
nFaces 57;
startFace 24200;
}
upperWall
{
type wall;
nFaces 223;
startFace 24257;
}
lowerWall
{
type wall;
nFaces 250;
startFace 24480;
}
frontAndBack
{
type empty;
nFaces 24450;
startFace 24730;
}
)
// ************************************************************************* //

View File

@ -1,41 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object thermophysicalProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
thermoType hhuMixtureThermo<homogeneousMixture<sutherlandTransport<specieThermo<janafThermo<perfectGas>>>>>;
stoichiometricAirFuelMassRatio stoichiometricAirFuelMassRatio [0 0 0 0 0 0 0] 15.675;
fuel fuel 1 44.0962 200 5000 1000 7.53414 0.0188722 -6.27185e-06 9.14756e-10 -4.78381e-14 -16467.5 -17.8923 0.933554 0.0264246 6.10597e-06 -2.19775e-08 9.51493e-12 -13958.5 19.2017 1.67212e-06 170.672;
oxidant oxidant 1 28.8504 200 6000 1000 3.10205 0.00123963 -4.17512e-07 6.60292e-11 -3.87448e-15 -985.517 5.35187 3.58378 -0.0007269 1.66985e-06 -1.08452e-10 -4.31951e-13 -1050.53 3.11223 1.67212e-06 170.672;
reactants reactants 24.8095 29.4649 200 5000 1000 3.28069 0.00195035 -6.53483e-07 1.00239e-10 -5.64653e-15 -1609.55 4.41496 3.47696 0.000367499 1.84866e-06 -9.8993e-10 -3.10214e-14 -1570.81 3.76075 1.67212e-06 170.672;
products products 1 28.3233 200 5000 1000 3.106 0.00179682 -5.94382e-07 9.04998e-11 -5.08033e-15 -11003.7 5.11872 3.49612 0.000650364 -2.08029e-07 1.2291e-09 -7.73697e-13 -11080.3 3.18978 1.67212e-06 170.672;
burntProducts burntProducts 25.8095 28.3233 200 6000 1000 3.106 0.00179682 -5.94382e-07 9.04998e-11 -5.08033e-15 -11003.7 5.11872 3.49612 0.000650364 -2.08029e-07 1.2291e-09 -7.73697e-13 -11080.3 3.18978 1.67212e-06 170.672;
/*
thermoType hhuMixtureThermo<homogeneousMixture<constTransport<specieThermo<hConstThermo<perfectGas>>>>>;
stoichiometricAirFuelMassRatio stoichiometricAirFuelMassRatio [0 0 0 0 0 0 0] 9.286;
reactants reactants 1 28 1330.9 2.133e+06 1.798e-05 0.7;
products products 1 28 1579.9 0 5.016e-05 0.7;
*/
// ************************************************************************* //

View File

@ -1,80 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application Xoodles;
startFrom startTime;
startTime 0;
stopAt endTime;
endTime 10;
deltaT 5e-06;
writeControl runTime;
writeInterval 0.1;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
writeCompression uncompressed;
timeFormat general;
timePrecision 6;
runTimeModifiable yes;
functions
(
fieldAverage1
{
// Type of functionObject
type fieldAverage;
// Where to load it from (if not already in solver)
functionObjectLibs ("libfieldAverage.so");
enabled true;
outputControl outputTime;
// Fields to be averaged - runTime modifiable
fields
(
U
{
mean on;
prime2Mean on;
base time;
}
p
{
mean on;
prime2Mean on;
base time;
}
);
}
);
// ************************************************************************* //

View File

@ -1,83 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default Euler;
}
gradSchemes
{
default Gauss linear;
grad(p) Gauss linear;
}
divSchemes
{
default none;
div(phi,U) Gauss limitedLinearV 1;
div(phid,p) Gauss linear;
div(phiU,p) Gauss linear;
div(phi,k) Gauss limitedLinear 1;
div(phi,B) Gauss limitedLinear 1;
div(B) Gauss linear;
div(phiXi,Xi) Gauss limitedLinear 1;
div(phiXi,Su) Gauss limitedLinear 1;
div(phiSt,b) Gauss limitedLinear01 1;
div(phi,ft_b_h_hu) Gauss multivariateSelection
{
fu limitedLinear01 1;
ft limitedLinear01 1;
b limitedLinear01 1;
h limitedLinear 1;
hu limitedLinear 1;
};
div(U) Gauss linear;
div((Su*grad(b))) Gauss linear;
div((U+((Su*Xi)*grad(b)))) Gauss linear;
div((muEff*dev2(grad(U).T()))) Gauss linear;
}
laplacianSchemes
{
default none;
laplacian(muEff,U) Gauss linear corrected;
laplacian(DkEff,k) Gauss linear corrected;
laplacian(DBEff,B) Gauss linear corrected;
laplacian((rho*(1|A(U))),p) Gauss linear corrected;
laplacian(muEff,b) Gauss linear corrected;
laplacian(muEff,ft) Gauss linear corrected;
laplacian(alphaEff,h) Gauss linear corrected;
laplacian(alphaEff,hu) Gauss linear corrected;
}
interpolationSchemes
{
default linear;
}
snGradSchemes
{
default corrected;
}
fluxRequired
{
default no;
p;
}
// ************************************************************************* //

View File

@ -1,105 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
rho PCG
{
preconditioner DIC;
tolerance 1e-05;
relTol 0;
};
U PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0;
};
p PCG
{
preconditioner DIC;
tolerance 1e-06;
relTol 0;
};
ft PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0;
};
fu PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0;
};
b PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0;
};
Xi PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0;
};
Su PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0;
};
h PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0;
};
hu PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0;
};
R PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0;
};
k PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0;
};
epsilon PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0;
};
}
PISO
{
nCorrectors 2;
nNonOrthogonalCorrectors 0;
}
// ************************************************************************* //

View File

@ -1,50 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volTensorField;
object B;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -2 0 0 0 0];
internalField uniform (0 0 0 0 0 0 0 0 0);
boundaryField
{
inlet
{
type fixedValue;
value uniform (0 0 0 0 0 0 0 0 0);
}
outlet
{
type zeroGradient;
}
upperWall
{
type zeroGradient;
}
lowerWall
{
type zeroGradient;
}
frontAndBack
{
type cyclic;
}
}
// ************************************************************************* //

View File

@ -1,52 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object Su;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform 0.135;
boundaryField
{
inlet
{
type fixedValue;
value uniform 0.135;
}
outlet
{
type inletOutlet;
inletValue uniform 0.135;
value uniform 0.135;
}
upperWall
{
type zeroGradient;
}
lowerWall
{
type zeroGradient;
}
frontAndBack
{
type cyclic;
}
}
// ************************************************************************* //

View File

@ -1,54 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://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 293;
boundaryField
{
inlet
{
type fixedValue;
value uniform 293;
}
outlet
{
type inletOutlet;
inletValue uniform 293;
value uniform 293;
}
upperWall
{
type fixedValue;
value uniform 293;
}
lowerWall
{
type fixedValue;
value uniform 293;
}
frontAndBack
{
type cyclic;
}
}
// ************************************************************************* //

View File

@ -1,54 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object Tu;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 1 0 0 0];
internalField uniform 293;
boundaryField
{
inlet
{
type fixedValue;
value uniform 293;
}
outlet
{
type inletOutlet;
inletValue uniform 293;
value uniform 293;
}
upperWall
{
type fixedValue;
value uniform 293;
}
lowerWall
{
type fixedValue;
value uniform 293;
}
frontAndBack
{
type cyclic;
}
}
// ************************************************************************* //

View File

@ -1,55 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / 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 (0 0 0);
boundaryField
{
inlet
{
type turbulentInlet;
referenceField uniform (13.3 0 0);
fluctuationScale (0.04 0.02 0.02);
}
outlet
{
type inletOutlet;
inletValue uniform (0 0 0);
value uniform (0 0 0);
}
upperWall
{
type fixedValue;
value uniform (0 0 0);
}
lowerWall
{
type fixedValue;
value uniform (0 0 0);
}
frontAndBack
{
type cyclic;
}
}
// ************************************************************************* //

View File

@ -1,52 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object Xi;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 1;
boundaryField
{
inlet
{
type fixedValue;
value uniform 1;
}
outlet
{
type inletOutlet;
inletValue uniform 1;
value uniform 1;
}
upperWall
{
type zeroGradient;
}
lowerWall
{
type zeroGradient;
}
frontAndBack
{
type cyclic;
}
}
// ************************************************************************* //

View File

@ -1,52 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object b;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 1;
boundaryField
{
inlet
{
type fixedValue;
value uniform 1;
}
outlet
{
type inletOutlet;
inletValue uniform 1;
value uniform 1;
}
upperWall
{
type zeroGradient;
}
lowerWall
{
type zeroGradient;
}
frontAndBack
{
type cyclic;
}
}
// ************************************************************************* //

View File

@ -1,52 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object ft;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0;
boundaryField
{
inlet
{
type fixedValue;
value uniform 0;
}
outlet
{
type inletOutlet;
inletValue uniform 0;
value uniform 0;
}
upperWall
{
type zeroGradient;
}
lowerWall
{
type zeroGradient;
}
frontAndBack
{
type cyclic;
}
}
// ************************************************************************* //

View File

@ -1,54 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 2e-05;
boundaryField
{
inlet
{
type fixedValue;
value uniform 2e-05;
}
outlet
{
type inletOutlet;
inletValue uniform 2e-05;
value uniform 2e-05;
}
upperWall
{
type fixedValue;
value uniform 1e-8;
}
lowerWall
{
type fixedValue;
value uniform 1e-8;
}
frontAndBack
{
type cyclic;
}
}
// ************************************************************************* //

View File

@ -1,49 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object muSgs;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
inlet
{
type zeroGradient;
}
outlet
{
type zeroGradient;
}
upperWall
{
type zeroGradient;
}
lowerWall
{
type zeroGradient;
}
frontAndBack
{
type cyclic;
}
}
// ************************************************************************* //

View File

@ -1,50 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://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 100000;
boundaryField
{
inlet
{
type zeroGradient;
}
outlet
{
type fixedValue;
value uniform 100000;
}
upperWall
{
type zeroGradient;
}
lowerWall
{
type zeroGradient;
}
frontAndBack
{
type cyclic;
}
}
// ************************************************************************* //

View File

@ -1,120 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object LESProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
LESModel oneEqEddy;
delta cubeRootVol;
printCoeffs on;
laminarCoeffs
{
}
oneEqEddyCoeffs
{
ce 1.048;
ck 0.094;
}
dynOneEqEddyCoeffs
{
ce 1.05;
filter simple;
}
lowReOneEqEddyCoeffs
{
ck 0.07;
ce 1.05;
beta 0.01;
}
SmagorinskyCoeffs
{
ck 0.02;
ce 0.202;
}
DeardorffDiffStressCoeffs
{
ce 1.048;
ck 0.094;
cm 4.13;
}
cubeRootVolCoeffs
{
deltaCoeff 1;
}
PrandtlCoeffs
{
delta cubeRootVol;
cubeRootVolCoeffs
{
deltaCoeff 1;
}
smoothCoeffs
{
delta cubeRootVol;
cubeRootVolCoeffs
{
deltaCoeff 1;
}
maxDeltaRatio 1.1;
}
Cdelta 0.158;
}
vanDriestCoeffs
{
delta cubeRootVol;
cubeRootVolCoeffs
{
deltaCoeff 1;
}
smoothCoeffs
{
delta cubeRootVol;
cubeRootVolCoeffs
{
deltaCoeff 1;
}
maxDeltaRatio 1.1;
}
Aplus 26;
Cdelta 0.158;
}
smoothCoeffs
{
delta cubeRootVol;
cubeRootVolCoeffs
{
deltaCoeff 1;
}
maxDeltaRatio 1.1;
}
kappa 0.4187;
wallFunctionCoeffs
{
E 9;
}
// ************************************************************************* //

View File

@ -1,90 +0,0 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object combustionProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
laminarFlameSpeedCorrelation Gulders;
fuel Propane;
Su Su [0 1 -1 0 0 0 0] 0.135;
SuModel transport;
equivalenceRatio equivalenceRatio [0 0 0 0 0 0 0] 0.6;
sigmaExt sigmaExt [0 0 -1 0 0 0 0] 338;
XiModel transport;
XiCoef XiCoef [0 0 0 0 0 0 0] 0.62;
XiShapeCoef XiShapeCoef [0 0 0 0 0 0 0] 1;
uPrimeCoef uPrimeCoef [0 0 0 0 0 0 0] 1;
GuldersCoeffs
{
Methane
{
W 0.422;
eta 0.15;
xi 5.18;
alpha 2;
beta -0.5;
f 2.3;
}
Propane
{
W 0.446;
eta 0.12;
xi 4.95;
alpha 1.77;
beta -0.2;
f 2.3;
}
IsoOctane
{
W 0.4658;
eta -0.326;
xi 4.48;
alpha 1.56;
beta -0.22;
f 2.3;
}
}
ignite yes;
ignitionSites
(
{
location (0 0 0);
diameter 0.003;
start 0;
duration 0.001;
strength 2;
}
);
ignitionSphereFraction 1;
ignitionThickness ignitionThickness [0 1 0 0 0 0 0] 0;
ignitionCircleFraction 0;
ignitionKernelArea ignitionKernelArea [0 2 0 0 0 0 0] 0;
// ************************************************************************* //

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