Merge branch 'master' into splitCyclic

Conflicts:
	src/OpenFOAM/meshes/polyMesh/polyPatches/basic/coupled/coupledPolyPatch.C
	src/OpenFOAM/meshes/polyMesh/polyPatches/constraint/cyclic/cyclicPolyPatch.C
	src/OpenFOAM/meshes/polyMesh/polyPatches/constraint/cyclic/cyclicPolyPatch.H
	src/dynamicMesh/polyTopoChange/polyTopoChange/addPatchCellLayer.C
	src/mesh/autoMesh/autoHexMesh/autoHexMeshDriver/autoLayerDriver.C
	src/parallel/decompose/scotchDecomp/scotchDecomp.C
	src/parallel/parMetisDecomp/parMetisDecomp.C
	src/sampling/sampledSurface/isoSurface/isoSurfaceCell.C
This commit is contained in:
mattijs
2010-03-25 13:54:12 +00:00
538 changed files with 15929 additions and 5466 deletions

View File

@ -1,35 +1,4 @@
#!/bin/sh
#------------------------------------------------------------------------------
# ========= |
# \\ / F ield | OpenFOAM: The Open Source CFD Toolbox
# \\ / O peration |
# \\ / A nd | Copyright (C) 1991-2009 OpenCFD Ltd.
# \\/ M anipulation |
#------------------------------------------------------------------------------
# License
# This file is part of OpenFOAM.
#
# OpenFOAM is free software; you can redistribute it and/or modify it
# under the terms of the GNU General Public License as published by the
# Free Software Foundation; either version 2 of the License, or (at your
# option) any later version.
#
# OpenFOAM is distributed in the hope that it will be useful, but WITHOUT
# ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or
# FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License
# for more details.
#
# You should have received a copy of the GNU General Public License
# along with OpenFOAM; if not, write to the Free Software Foundation,
# Inc., 51 Franklin St, Fifth Floor, Boston, MA 02110-1301 USA
#
# Script
# Allclean
#
# Description
#
#------------------------------------------------------------------------------
cd ${0%/*} || exit 1 # run from this directory
echo "--------"
@ -43,4 +12,5 @@ rm logs testLoopReport > /dev/null 2>&1
foamCleanTutorials cases
echo "--------"
# ----------------------------------------------------------------- end-of-file

View File

@ -3,7 +3,7 @@
# ========= |
# \\ / F ield | OpenFOAM: The Open Source CFD Toolbox
# \\ / O peration |
# \\ / A nd | Copyright (C) 1991-2009 OpenCFD Ltd.
# \\ / A nd | Copyright (C) 1991-2010 OpenCFD Ltd.
# \\/ M anipulation |
#------------------------------------------------------------------------------
# License
@ -29,7 +29,6 @@
# Description
#
#------------------------------------------------------------------------------
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
@ -37,10 +36,11 @@ cd ${0%/*} || exit 1 # run from this directory
# logReport <logfile>
# Extracts useful info from log file.
logReport () {
case=`dirname $1 | sed s/"\(.*\)\.\/"/""/g`
logReport()
{
caseName=`dirname $1 | sed s/"\(.*\)\.\/"/""/g`
app=`echo $1 | sed s/"\(.*\)\."/""/g`
appAndCase="Application $app - case $case"
appAndCase="Application $app - case $caseName"
fatalError=`grep "FOAM FATAL" $1`
UxSS=`grep -E "Ux[:| ]*solution singularity" $1`
@ -51,11 +51,9 @@ logReport () {
if [ "$fatalError" ]
then
echo "$appAndCase: ** FOAM FATAL ERROR **"
return
elif [ "$UxSS" -a "$UySS" -a "$UzSS" ]
then
echo "$appAndCase: ** Solution singularity **"
return
elif [ "$completed" ]
then
completionTime=`tail -10 $log | grep Execution | cut -d= -f2 | sed 's/^[ \t]*//'`
@ -64,7 +62,6 @@ logReport () {
completionTime="in $completionTime"
fi
echo "$appAndCase: completed $completionTime"
return
else
echo "$appAndCase: unconfirmed completion"
fi
@ -78,18 +75,18 @@ foamRunTutorials cases
# Analyse all log files
rm testLoopReport > /dev/null 2>&1 &
touch testLoopReport
for application in *
for appDir in *
do
if [ -d $application ]
then
cd $application
for log in `find . -name "log.*" | xargs ls -rt`
do
logReport $log >> ../testLoopReport
done
echo "" >> ../testLoopReport
cd ..
fi
(
[ -d $appDir ] && cd $appDir || exit
for log in `find . -name "log.*" | xargs ls -rt`
do
logReport $log >> ../testLoopReport
done
echo "" >> ../testLoopReport
)
done
find . -name "log.*" -exec cat {} \; >> logs

View File

@ -3,7 +3,7 @@
# ========= |
# \\ / F ield | OpenFOAM: The Open Source CFD Toolbox
# \\ / O peration |
# \\ / A nd | Copyright (C) 1991-2009 OpenCFD Ltd.
# \\ / A nd | Copyright (C) 1991-2010 OpenCFD Ltd.
# \\/ M anipulation |
#------------------------------------------------------------------------------
# License
@ -30,10 +30,10 @@
# quickly tests the tutorials and writes out the scheme/solver information
#
#------------------------------------------------------------------------------
cd ${0%/*} || exit 1 # run from this directory
usage() {
usage()
{
while [ "$#" -ge 1 ]; do echo "$1"; shift; done
cat<<USAGE
@ -50,7 +50,8 @@ USAGE
}
setDefaultFvSchemes() {
setDefaultFvSchemes()
{
cat<<EOF
gradSchemes { default Gauss linear; }
divSchemes
@ -127,8 +128,12 @@ eval set -- "$OPTS"
while [ $1 != -- ]
do
case $1 in
-d) DEFAULT_SCHEMES=1;;
-h) usage;;
-d)
DEFAULT_SCHEMES=1
;;
-h)
usage
;;
esac
shift
done
@ -225,5 +230,4 @@ do
echo "" >> $SOLVERS_FILE
done
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,5 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
@ -6,3 +7,5 @@
cleanCase
rm -rf 0
cp -r 0.org 0
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,6 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
@ -9,3 +11,5 @@ runApplication blockMesh
runApplication boxTurb
runApplication $application
runApplication enstrophy
# ----------------------------------------------------------------- end-of-file

View File

@ -1,8 +1,10 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
cleanCase
rm -rf Fieldview > /dev/null 2>&1
rm -rf EnSight > /dev/null 2>&1
rm -rf EnSight Ensight Fieldview > /dev/null 2>&1
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,6 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
@ -20,3 +22,5 @@ runAnsysToFoam flange.ans 0.001
runApplication $application
runApplication foamToFieldview9
runApplication foamToEnsight
# ----------------------------------------------------------------- end-of-file

View File

@ -1,18 +1,25 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
cd cylinder
(
cd cylinder || exit
cleanCase
rm -rf 0 > /dev/null 2>&1
cp -r 0.org 0
wclean analyticalCylinder
cd ..
)
(
cd pitzDaily || exit
cd pitzDaily
cleanCase
rm -rf 0 > /dev/null 2>&1
cp -r 0.org 0
cd ..
)
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,6 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
@ -9,3 +11,5 @@ runApplication $application
compileApplication analyticalCylinder
runApplication analyticalCylinder
runApplication streamFunction
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,6 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
@ -7,3 +9,5 @@ application=`getApplication`
runApplication blockMesh
runApplication $application
runApplication streamFunction
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,5 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
@ -6,12 +7,18 @@
keepCases="moriyoshiHomogeneous"
loseCases="moriyoshiHomogeneousPart2"
for case in $keepCases
for caseName in $keepCases
do
(cd $case && foamCleanTutorials)
(
cd $caseName || exit
foamCleanTutorials
)
done
for case in $loseCases
for caseName in $loseCases
do
removeCase $case
removeCase $caseName
done
# ----------------------------------------------------------------- end-of-file

View File

@ -1,12 +1,16 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
# Set application name
application="XiFoam"
setControlDict () {
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 \
@ -15,15 +19,20 @@ setControlDict () {
mv temp.$$ $controlDict
}
# Do moriyoshiHomogeneous
(cd moriyoshiHomogeneous && foamRunTutorials)
( cd moriyoshiHomogeneous && foamRunTutorials )
# Clone case
cloneCase moriyoshiHomogeneous moriyoshiHomogeneousPart2
# Modify and execute
cd moriyoshiHomogeneousPart2
(
cd moriyoshiHomogeneousPart2 || exit
cp -r ../moriyoshiHomogeneous/0.005 .
setControlDict
runApplication $application
cd ..
)
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,5 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
@ -8,3 +9,5 @@ rm -rf 0
cp system/controlDict.1st system/controlDict
cleanCase
mv temp180 ./-180
# ----------------------------------------------------------------- end-of-file

View File

@ -1,32 +1,42 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
# Get application name
application=`getApplication`
runKivaToFoam ()
runKivaToFoam()
{
if [ -f $1/log.kivaToFoam ] ; then
echo "kivaToFoam already run on $1: remove log file to run"
if [ -f log.kivaToFoam ]
then
echo "kivaToFoam already run: remove log file to run"
else
echo "kivaToFoam: converting kiva file"
kivaToFoam -case $1 -file $2 > $1/log.kivaToFoam 2>&1
kivaToFoam -file $1 > log.kivaToFoam 2>&1
fi
}
restartApplication ()
restartApplication()
{
if [ -f $2/log-2.$1 ] ; then
echo "$1 already run on $2: remove log file to run"
if [ -f log-2.$1 ]
then
echo "$1 already run: remove log file to run"
else
echo "Running $1 on $2"
$1 -case $2 > $2/log-2.$1 2>&1
echo "Running $1"
$1 > log-2.$1 2>&1
fi
}
runKivaToFoam . otape17
runKivaToFoam otape17
cp system/controlDict.1st system/controlDict
runApplication $application
cp system/controlDict.2nd system/controlDict
restartApplication $application .
restartApplication $application
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,6 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
@ -10,4 +12,4 @@ runApplication createPatch -overwrite
# Run
runApplication fireFoam
# -----------------------------------------------------------------------------
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,5 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
@ -12,19 +13,25 @@ LadenburgJet60psi \
biconic25-55Run35 \
"
for case in $cases
for caseName in $cases
do
if [ "$case" = "shockTube" ]
(
cd $caseName || exit
if [ "$caseName" = shockTube ]
then
rm -rf $case/0
cp -r $case/0.org $case/0
rm -rf 0
cp -r 0.org 0
fi
(cd $case && foamCleanTutorials && cleanSamples)
foamCleanTutorials && cleanSamples
if [ "$case" = "biconic25-55Run35" ]
if [ "$caseName" = "biconic25-55Run35" ]
then
rm -rf $case/constant/polyMesh/boundary
wclean $case/datToFoam
rm -rf constant/polyMesh/boundary
wclean datToFoam
fi
)
done
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,6 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
@ -14,26 +16,30 @@ LadenburgJet60psi \
biconic25-55Run35 \
"
moveTimeMeshToConstant ()
moveTimeMeshToConstant()
{
DT=`foamInfoExec -times | tail -1`
if [ "$DT" != 0 ] ; then
if [ "$DT" != 0 ]
then
mv ${DT}/polyMesh/* constant/polyMesh
rm -rf ${DT}
fi
}
for case in $cases
do
(cd $case && runApplication blockMesh)
#
if [ "$case" = "shockTube" ] ; then
(cd $case && runApplication setFields)
fi
#
if [ "$case" = "biconic25-55Run35" ] ; then
cd $case
for caseName in $cases
do
(
cd $caseName || exit
runApplication blockMesh
case "$caseName" in
shockTube)
runApplication setFields
;;
biconic25-55Run35)
wmake datToFoam
runApplication datToFoam grid256.dat
@ -46,9 +52,11 @@ do
mv $CONST/polyMesh/boundary $CONST/polyMesh/boundary.bak
sed -f $CONST/wedgeScr $CONST/polyMesh/boundary.bak > $CONST/polyMesh/boundary
rm $CONST/polyMesh/boundary.bak
;;
esac
cd ..
fi
#
(cd $case && runApplication $application)
runApplication $application
)
done
# ----------------------------------------------------------------- end-of-file

View File

@ -1,43 +1,54 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
#
# FUNCTIONS
#
printUsage () {
cat <<EOF
Usage: $0 [options]
Runs a set of samples across the cone face and concatenates output files
usage()
{
while [ "$#" -ge 1 ]; do echo "$1"; shift; done
Options are:
-l -latestTime option for sample
-h help
EOF
cat<<USAGE
Usage: ${0##*/} [OPTION]
options:
-l -latestTime option for sample
-h help
Runs a set of samples across the cone face and concatenates output files
USAGE
exit 1
}
LATEST_TIME=""
unset timeOpt
OPTS=`getopt hl $*`
if [ $? -ne 0 ] ; then
echo "Aborting due to invalid option"
printUsage
exit 1
fi
[ $? -eq 0 ] || usage "Aborting due to invalid option"
eval set -- "$OPTS"
while [ $1 != -- ]; do
while [ $1 != -- ]
do
case $1 in
-l) LATEST_TIME="-latestTime";;
-h) printUsage; exit 1;;
-l)
timeOpt="-latestTime"
;;
-h)
usage
;;
esac
shift
done
shift
sample ${LATEST_TIME}
sample $timeOpt
SDIR="sets"
LSDIR=`ls $SDIR | head -1`
EXAMPLE_FILE=`ls -1 $SDIR/${LSDIR}/* | head -1`
FS=`basename $EXAMPLE_FILE | cut -d_ -f2-`
for d in $SDIR/*
do
cat ${d}/cone25_${FS} ${d}/cone55_${FS} ${d}/base_${FS} > ${d}/biconic_${FS}
cat ${d}/cone25_${FS} ${d}/cone55_${FS} ${d}/base_${FS} > ${d}/biconic_${FS}
done
# ----------------------------------------------------------------- end-of-file

View File

@ -0,0 +1,44 @@
/*--------------------------------*- 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 T;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 1 0 0 0];
internalField uniform 293;
boundaryField
{
rotor
{
type zeroGradient;
}
stator
{
type zeroGradient;
}
front
{
type empty;
}
back
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,46 @@
/*--------------------------------*- 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
{
rotor
{
type fixedValue;
value uniform (0 0 0);
}
stator
{
type fixedValue;
value uniform (0 0 0);
}
front
{
type empty;
}
back
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,47 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6.x |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object alphat;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
rotor
{
type alphatWallFunction;
Prt 0.85;
value uniform 0;
}
stator
{
type alphatWallFunction;
Prt 0.85;
value uniform 0;
}
front
{
type empty;
}
back
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,48 @@
/*--------------------------------*- 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 volScalarField;
location "0";
object epsilon;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [ 0 2 -3 0 0 0 0 ];
internalField uniform 20;
boundaryField
{
rotor
{
type compressible::epsilonWallFunction;
value uniform 20;
}
stator
{
type compressible::epsilonWallFunction;
value uniform 20;
}
front
{
type empty;
}
back
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,48 @@
/*--------------------------------*- 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 volScalarField;
location "0";
object k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [ 0 2 -2 0 0 0 0 ];
internalField uniform 1;
boundaryField
{
rotor
{
type compressible::kqRWallFunction;
value uniform 0;
}
stator
{
type compressible::kqRWallFunction;
value uniform 0;
}
front
{
type empty;
}
back
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,48 @@
/*--------------------------------*- 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 volScalarField;
location "0";
object mut;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
rotor
{
type mutkWallFunction;
value uniform 0;
}
stator
{
type mutkWallFunction;
value uniform 0;
}
front
{
type empty;
}
back
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,44 @@
/*--------------------------------*- 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 [1 -1 -2 0 0 0 0];
internalField uniform 1e5;
boundaryField
{
rotor
{
type zeroGradient;
}
stator
{
type zeroGradient;
}
front
{
type empty;
}
back
{
type empty;
}
}
// ************************************************************************* //

View File

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

View File

@ -0,0 +1,31 @@
/*--------------------------------*- 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;
location "constant";
object MRFZones;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
1
(
rotor
{
// Fixed patches (by default they 'move' with the MRF zone)
nonRotatingPatches ();
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] 1047.2;
}
)
// ************************************************************************* //

View File

@ -0,0 +1,25 @@
/*--------------------------------*- 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 RASProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
RASModel kEpsilon;
turbulence on;
printCoeffs on;
// ************************************************************************* //

View File

@ -0,0 +1,42 @@
/*--------------------------------*- 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 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

@ -0,0 +1,834 @@
/*--------------------------------*- 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;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// General macros to create 2D/extruded-2D meshes
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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)
stator
(12 4 1)
simpleGrading (1 1 1)
// block1
hex (21 22 30 29 69 70 78 77)
stator
(12 4 1)
simpleGrading (1 1 1)
// block2
hex (22 23 31 30 70 71 79 78)
stator
(12 4 1)
simpleGrading (1 1 1)
// block3
hex (23 24 32 31 71 72 80 79)
stator
(12 4 1)
simpleGrading (1 1 1)
// block4
hex (24 25 33 32 72 73 81 80)
stator
(12 4 1)
simpleGrading (1 1 1)
// block5
hex (25 26 34 33 73 74 82 81)
stator
(12 4 1)
simpleGrading (1 1 1)
// block6
hex (26 27 35 34 74 75 83 82)
stator
(12 4 1)
simpleGrading (1 1 1)
// block7
hex (27 20 28 35 75 68 76 83)
stator
(12 4 1)
simpleGrading (1 1 1)
// block0
hex (28 29 38 36 76 77 86 84)
stator
(12 12 1)
simpleGrading (1 1 1)
// block1
hex (29 30 39 37 77 78 87 85)
stator
(12 12 1)
simpleGrading (1 1 1)
// block2
hex (30 31 41 39 78 79 89 87)
stator
(12 12 1)
simpleGrading (1 1 1)
// block3
hex (31 32 42 40 79 80 90 88)
stator
(12 12 1)
simpleGrading (1 1 1)
// block4
hex (32 33 44 42 80 81 92 90)
stator
(12 12 1)
simpleGrading (1 1 1)
// block5
hex (33 34 45 43 81 82 93 91)
stator
(12 12 1)
simpleGrading (1 1 1)
// block6
hex (34 35 47 45 82 83 95 93)
stator
(12 12 1)
simpleGrading (1 1 1)
// block7
hex (35 28 36 46 83 76 84 94)
stator
(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

@ -0,0 +1,834 @@
/*--------------------------------*- 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;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// 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)
stator
(Na Ni Nz)
simpleGrading (1 1 1)
// block1
hex2D(ri1, ri2, Rb2, Rb1)
stator
(Na Ni Nz)
simpleGrading (1 1 1)
// block2
hex2D(ri2, ri3, Rb3, Rb2)
stator
(Na Ni Nz)
simpleGrading (1 1 1)
// block3
hex2D(ri3, ri4, Rb4, Rb3)
stator
(Na Ni Nz)
simpleGrading (1 1 1)
// block4
hex2D(ri4, ri5, Rb5, Rb4)
stator
(Na Ni Nz)
simpleGrading (1 1 1)
// block5
hex2D(ri5, ri6, Rb6, Rb5)
stator
(Na Ni Nz)
simpleGrading (1 1 1)
// block6
hex2D(ri6, ri7, Rb7, Rb6)
stator
(Na Ni Nz)
simpleGrading (1 1 1)
// block7
hex2D(ri7, ri0, Rb0, Rb7)
stator
(Na Ni Nz)
simpleGrading (1 1 1)
// block0
hex2D(Rb0, Rb1, R1s, R0)
stator
(Na NR Nz)
simpleGrading (1 1 1)
// block1
hex2D(Rb1, Rb2, R2, R1)
stator
(Na NR Nz)
simpleGrading (1 1 1)
// block2
hex2D(Rb2, Rb3, R3s, R2)
stator
(Na NR Nz)
simpleGrading (1 1 1)
// block3
hex2D(Rb3, Rb4, R4, R3)
stator
(Na NR Nz)
simpleGrading (1 1 1)
// block4
hex2D(Rb4, Rb5, R5s, R4)
stator
(Na NR Nz)
simpleGrading (1 1 1)
// block5
hex2D(Rb5, Rb6, R6, R5)
stator
(Na NR Nz)
simpleGrading (1 1 1)
// block6
hex2D(Rb6, Rb7, R7s, R6)
stator
(Na NR Nz)
simpleGrading (1 1 1)
// block7
hex2D(Rb7, Rb0, R0, R7)
stator
(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

@ -0,0 +1,46 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class polyBoundaryMesh;
location "constant/polyMesh";
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

@ -0,0 +1,36 @@
/*--------------------------------*- 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;
location "constant";
object porousZones;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
1
(
stator
{
coordinateSystem
{
e1 (1 0 0);
e2 (0 1 0);
}
Darcy
{
d d [0 -2 0 0 0 0 0] (1e5 -1000 -1000);
f f [0 -1 0 0 0 0 0] (0 0 0);
}
}
)
// ************************************************************************* //

View File

@ -0,0 +1,23 @@
/*--------------------------------*- 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 thermophysicalProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
thermoType hPsiThermo<pureMixture<sutherlandTransport<specieThermo<hConstThermo<perfectGas>>>>>;
mixture air 1 28.9 1007 0 1.4792e-06 116;
// ************************************************************************* //

View File

@ -0,0 +1,39 @@
/*--------------------------------*- 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;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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

@ -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 turbulenceProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
simulationType RASModel;
// ************************************************************************* //

View File

@ -0,0 +1,5 @@
#!/bin/sh
set -x
m4 < constant/polyMesh/blockMeshDict.m4 > constant/polyMesh/blockMeshDict
blockMesh >& log.blockMesh

View File

@ -0,0 +1,52 @@
/*--------------------------------*- 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 rhoPorousMRFPimpleFoam;
startFrom startTime;
startTime 0;
stopAt endTime;
endTime 0.1;
deltaT 1e-5;
writeControl adjustableRunTime;
writeInterval 1e-2;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
writeCompression uncompressed;
timeFormat general;
timePrecision 6;
runTimeModifiable yes;
adjustTimeStep yes;
maxCo 1;
// ************************************************************************* //

View File

@ -0,0 +1,25 @@
/*--------------------------------*- 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 faceSetDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
name rotor;
action delete;
topoSetSources ( boundaryToFace { } );
// ************************************************************************* //

View File

@ -0,0 +1,25 @@
/*--------------------------------*- 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 faceSetDict_noBoundaryFaces;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
name rotor;
action delete;
topoSetSources ( boundaryToFace { } );
// ************************************************************************* //

View File

@ -11,7 +11,7 @@ FoamFile
format ascii;
class dictionary;
location "system";
object cellSetDict;
object faceSetDict_rotorFaces;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
@ -19,7 +19,7 @@ name rotor;
action new;
topoSetSources ( zoneToCell { name rotor ; } );
topoSetSources ( cellToFace { set rotor ; option all ; } );
// ************************************************************************* //

View File

@ -0,0 +1,67 @@
/*--------------------------------*- 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;
}
divSchemes
{
default none;
div(phi,U) Gauss limitedLinearV 1;
div(phi,h) Gauss limitedLinear 1;
div(phi,k) Gauss limitedLinear 1;
div(phi,epsilon) Gauss limitedLinear 1;
div((muEff*dev2(grad(U).T()))) Gauss linear;
div(phiU,p) Gauss linear;
}
laplacianSchemes
{
default none;
laplacian(muEff,U) Gauss linear corrected;
laplacian((rho*(1|A(U))),p) Gauss linear corrected;
laplacian(alphaEff,h) 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

@ -0,0 +1,121 @@
/*--------------------------------*- 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
{
rho
{
solver PCG;
preconditioner DIC;
tolerance 1e-5;
relTol 0;
}
U
{
solver PBiCG;
preconditioner DILU;
tolerance 1e-5;
relTol 0.1;
}
UFinal
{
solver PBiCG;
preconditioner DILU;
tolerance 1e-5;
relTol 0;
}
p
{
solver GAMG;
tolerance 1e-6;
relTol 0.05;
smoother GaussSeidel;
cacheAgglomeration true;
nCellsInCoarsestLevel 20;
agglomerator faceAreaPair;
mergeLevels 1;
}
pFinal
{
solver GAMG;
tolerance 1e-6;
relTol 0;
smoother GaussSeidel;
cacheAgglomeration true;
nCellsInCoarsestLevel 20;
agglomerator faceAreaPair;
mergeLevels 1;
}
h
{
solver PBiCG;
preconditioner DILU;
tolerance 1e-5;
relTol 0.1;
}
hFinal
{
solver PBiCG;
preconditioner DILU;
tolerance 1e-5;
relTol 0;
}
k
{
solver PBiCG;
preconditioner DILU;
tolerance 1e-5;
relTol 0;
}
epsilon
{
solver PBiCG;
preconditioner DILU;
tolerance 1e-5;
relTol 0;
}
}
PIMPLE
{
nOuterCorrectors 1;
nCorrectors 2;
nNonOrthogonalCorrectors 0;
momentumPredictor yes;
pMin pMin [ 1 -1 -2 0 0 0 0 ] 1000;
pRefCell 0;
pRefValue 1e5;
}
relaxationFactors
{
U 1;
h 1;
k 1;
epsilon 1;
}
// ************************************************************************* //

View File

@ -1,4 +1,6 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
@ -9,3 +11,5 @@ application=`getApplication`
runApplication blockMesh
runApplication setFields
runApplication $application
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,5 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
@ -6,3 +7,5 @@
rm -rf 0
cp -r 0.org 0
cleanCase
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,6 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
@ -7,3 +9,5 @@ application=`getApplication`
runApplication blockMesh
runApplication setFields
runApplication $application
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,5 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
@ -7,3 +8,5 @@ cleanCase
rm -rf 0
cp -r 0.org 0
cleanSamples
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,6 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
@ -9,3 +11,5 @@ runApplication setFields
runApplication $application
runApplication foamCalc mag U
runApplication sample
# ----------------------------------------------------------------- end-of-file

View File

@ -1,11 +1,13 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
# Get application name
application=`getApplication`
runStarToFoam ()
runStarToFoam()
{
if [ -f log.star3ToFoam -o -f log.starToFoam ]
then
@ -24,3 +26,5 @@ rm temp
runApplication $application
# end-of-file
# ----------------------------------------------------------------- end-of-file

View File

@ -1,7 +1,10 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
removeCase decompressionTankFine
foamCleanTutorials cases
# ----------------------------------------------------------------- end-of-file

View File

@ -1,14 +1,17 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
# Set application name
application="sonicLiquidFoam"
setDecompressionTankFine ()
setDecompressionTankFine()
{
blockMeshDict="$1/constant/polyMesh/blockMeshDict"
controlDict="$1/system/controlDict"
blockMeshDict="constant/polyMesh/blockMeshDict"
controlDict="system/controlDict"
sed \
-e s/"30 20"/"120 80"/g \
-e s/"30 5"/"120 20"/g \
@ -16,6 +19,7 @@ setDecompressionTankFine ()
-e s/"30 95"/"120 380"/g \
$blockMeshDict > temp.$$
mv temp.$$ $blockMeshDict
sed \
-e s/"\(deltaT[ \t]*\) 5e-07;"/"\1 1e-07;"/g \
-e s/"\(endTime[ \t]*\) 0.00025;"/"\1 0.00015;"/g \
@ -23,16 +27,22 @@ setDecompressionTankFine ()
mv temp.$$ $controlDict
}
# Do decompressionTank
(cd decompressionTank && foamRunTutorials)
( cd decompressionTank && foamRunTutorials )
# Clone case
cloneCase decompressionTank decompressionTankFine
cd decompressionTankFine
(
cd decompressionTankFine || exit
# Modify case
setDecompressionTankFine .
setDecompressionTankFine
# And execute
runApplication blockMesh
runApplication $application
cd ..
)
# ----------------------------------------------------------------- end-of-file

View File

@ -1,7 +1,10 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
cleanCase
rm -rf 0/lagrangian 0/dsmcSigmaTcRMax
# ----------------------------------------------------------------- end-of-file

View File

@ -1,7 +1,11 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
runApplication blockMesh
runApplication dsmcInitialise
runApplication dsmcFoam
# ----------------------------------------------------------------- end-of-file

View File

@ -1,7 +1,10 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
cleanCase
rm -rf 0/lagrangian 0/dsmcSigmaTcRMax
# ----------------------------------------------------------------- end-of-file

View File

@ -1,7 +1,11 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
runApplication blockMesh
runApplication dsmcInitialise
runApplication dsmcFoam
# ----------------------------------------------------------------- end-of-file

View File

@ -1,7 +1,10 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
cleanCase
rm -rf 0/lagrangian 0/dsmcSigmaTcRMax
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,6 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
@ -8,3 +10,5 @@ runParallel dsmcInitialise 4
runParallel dsmcFoam 4
runApplication reconstructPar -noLagrangian
# ----------------------------------------------------------------- end-of-file

View File

@ -1,7 +1,10 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
cleanCase
rm -rf 0/lagrangian 0/dsmcSigmaTcRMax
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,6 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
@ -8,3 +10,5 @@ runParallel dsmcInitialise 4
runParallel dsmcFoam 4
runApplication reconstructPar -noLagrangian
# ----------------------------------------------------------------- end-of-file

View File

@ -1,22 +1,30 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
cd periodicCubeArgon
(
cd periodicCubeArgon || exit
rm -rf 0/*
rm -f Ar-Ar
rm -f electrostatic
rm -f constant/idList
rm -rf constant/polyMesh/sets
cleanCase
cd ..
)
(
cd periodicCubeWater || exit
cd periodicCubeWater
rm -rf 0/*
rm -f O-O
rm -f electrostatic
rm -f constant/idList
rm -rf constant/polyMesh/sets
cleanCase
cd ..
)
# ----------------------------------------------------------------- end-of-file

View File

@ -1,18 +1,20 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
application="mdEquilibrationFoam"
cd periodicCubeArgon
runApplication blockMesh
runApplication mdInitialise
runApplication $application
cd ..
for caseName in periodicCubeArgon periodicCubeWater
do
(
cd $caseName || exit
cd periodicCubeWater
runApplication blockMesh
runApplication mdInitialise
runApplication $application
cd ..
)
done
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,5 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
@ -6,3 +7,5 @@
rm -rf constant/polyMesh/sets
rm -rf processor[0-9]
cleanCase
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,6 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
@ -13,3 +15,5 @@ runParallel mdInitialise 4
runParallel $application 4
runApplication reconstructPar
# ----------------------------------------------------------------- end-of-file

View File

@ -1,7 +1,14 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
(cd hartmann && cleanCase)
(cd hartmann && cleanSamples)
(
cd hartmann || exit
cleanCase
cleanSamples
)
# ----------------------------------------------------------------- end-of-file

View File

@ -1,11 +1,19 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
# Set application name
application="mhdFoam"
(cd hartmann && runApplication blockMesh)
(cd hartmann && runApplication $application)
(cd hartmann && runApplication foamCalc components U)
(cd hartmann && runApplication sample)
(
cd hartmann || exit
runApplication blockMesh
runApplication $application
runApplication foamCalc components U
runApplication sample
)
# ----------------------------------------------------------------- end-of-file

View File

@ -1,7 +1,10 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
cleanCase
cp 0/T.org 0/T
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,6 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
@ -8,3 +10,5 @@ compileApplication ../../buoyantPisoFoam/hotRoom/setHotRoom
runApplication blockMesh
runApplication setHotRoom
runApplication $application
# ----------------------------------------------------------------- end-of-file

View File

@ -1,7 +1,10 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
cleanCase
cp 0/T.org 0/T
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,6 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
@ -8,3 +10,5 @@ compileApplication ../../buoyantPisoFoam/hotRoom/setHotRoom
runApplication blockMesh
runApplication setHotRoom
runApplication $application
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,6 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
@ -6,3 +8,4 @@ runApplication blockMesh
runApplication snappyHexMesh -overwrite
runApplication buoyantBoussinesqSimpleFoam
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,5 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
@ -6,3 +7,5 @@
cleanCase
cp 0/T.org 0/T
wclean setHotRoom
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,6 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
@ -9,3 +11,5 @@ compileApplication setHotRoom
runApplication blockMesh
runApplication setHotRoom
runApplication $application
# ----------------------------------------------------------------- end-of-file

View File

@ -1,7 +1,11 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
cleanCase
rm -rf sets
(cd validation && rm -f *.eps)
rm -f validation/*.eps
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,6 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
@ -8,4 +10,7 @@ application="buoyantSimpleFoam"
runApplication blockMesh
runApplication $application
runApplication sample -latestTime
(cd validation && ./createGraphs)
( cd validation && ./createGraphs )
# ----------------------------------------------------------------- end-of-file

View File

@ -32,7 +32,8 @@
#
#------------------------------------------------------------------------------
createEpsT() {
createEpsT()
{
index=$1
OF=$2
EXPT=$3
@ -54,7 +55,8 @@ EOF
}
createEpsU() {
createEpsU()
{
index=$1
OF=$2
EXPT=$3
@ -78,7 +80,8 @@ EOF
# test if gnuplot exists on the system
type -P gnuplot &>/dev/null || {
echo "gnuplot not found - skipping graph creation" >&2; exit 1;
echo "gnuplot not found - skipping graph creation" >&2
exit 1
}
# paths to data
@ -89,7 +92,8 @@ EXPTDATAROOT=./exptData
# generate temperature profiles
TSets="1 3 4 5 6 7 9"
for i in $TSets; do
for i in $TSets
do
echo " processing temperature profile at y/yMax of 0.$i"
OF="$OFDATAROOT/y0.${i}_T.xy"
@ -101,7 +105,8 @@ done
# generate velocity profiles
USets="1 3 4 5 6 7 9"
for i in $USets; do
for i in $USets
do
echo " processing velocity profile at y/yMax of 0.$i"
OF="$OFDATAROOT/y0.${i}_U.xy"
@ -110,6 +115,6 @@ for i in $USets; do
createEpsU $i $OF $EXPT
done
echo "done"
echo Done
#------------------------------------------------------------------------------

View File

@ -1,7 +1,10 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
cleanCase
cp 0/T.org 0/T
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,6 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
@ -8,3 +10,5 @@ compileApplication ../../buoyantPisoFoam/hotRoom/setHotRoom
runApplication blockMesh
runApplication setHotRoom
runApplication $application
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,5 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
@ -18,4 +19,4 @@ rm -rf constant/heater/polyMesh
rm -rf constant/leftSolid/polyMesh
rm -rf constant/rightSolid/polyMesh
# -----------------------------------------------------------------------------
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,6 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
@ -58,4 +60,4 @@ do
paraFoam -touch -region $i
done
# -----------------------------------------------------------------------------
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,5 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
@ -18,4 +19,4 @@ rm -rf constant/heater/polyMesh
rm -rf constant/leftSolid/polyMesh
rm -rf constant/rightSolid/polyMesh
# -----------------------------------------------------------------------------
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,6 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
@ -55,4 +57,4 @@ do
paraFoam -touch -region $i
done
# -----------------------------------------------------------------------------
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,6 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
@ -7,3 +9,5 @@ application=`getApplication`
./makeMesh
runApplication $application
# ----------------------------------------------------------------- end-of-file

View File

@ -3,11 +3,3 @@ set -x
m4 < constant/polyMesh/blockMeshDict.m4 > constant/polyMesh/blockMeshDict
blockMesh >& log.blockMesh
cellSet >& log.cellSet
#- MRF determines its own faceZone if not supplied
#cp system/faceSetDict_rotorFaces system/faceSetDict
#faceSet
#cp system/faceSetDict_noBoundaryFaces system/faceSetDict
#faceSet
setsToZones -noFlipMap >& log.setsToZones

View File

@ -0,0 +1,54 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volVectorField;
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
inlet
{
type fixedValue;
value uniform (10 0 0);
}
outlet
{
//type zeroGradient;
type inletOutlet;
inletValue 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

@ -0,0 +1,56 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volVectorField;
object Ua;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
inlet
{
type fixedValue;
value uniform (-1 0 0);
}
outlet
{
//type zeroGradient;
//type inletOutlet;
//inletValue uniform (0 0 0);
type adjointOutletVelocity;
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

@ -0,0 +1,56 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object epsilon;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -3 0 0 0 0];
internalField uniform 14.855;
boundaryField
{
inlet
{
type fixedValue;
value uniform 14.855;
}
outlet
{
type zeroGradient;
}
upperWall
{
type epsilonWallFunction;
Cmu 0.09;
kappa 0.41;
E 9.8;
value uniform 14.855;
}
lowerWall
{
type epsilonWallFunction;
Cmu 0.09;
kappa 0.41;
E 9.8;
value uniform 14.855;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,50 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 0.375;
boundaryField
{
inlet
{
type fixedValue;
value uniform 0.375;
}
outlet
{
type zeroGradient;
}
upperWall
{
type kqRWallFunction;
value uniform 0.375;
}
lowerWall
{
type kqRWallFunction;
value uniform 0.375;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,57 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object nut;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
inlet
{
type calculated;
value uniform 0;
}
outlet
{
type calculated;
value uniform 0;
}
upperWall
{
type nutkWallFunction;
Cmu 0.09;
kappa 0.41;
E 9.8;
value uniform 0;
}
lowerWall
{
type nutkWallFunction;
Cmu 0.09;
kappa 0.41;
E 9.8;
value uniform 0;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

View File

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

View File

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

View File

@ -0,0 +1,24 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object RASProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
RASModel kEpsilon;
turbulence on;
printCoeffs on;
// ************************************************************************* //

View File

@ -0,0 +1,153 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class 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

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

View File

@ -0,0 +1,25 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object transportProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
transportModel Newtonian;
nu nu [0 2 -1 0 0 0 0] 1e-5;
lambda lambda [0 -2 1 0 0 0 0] 1e5;
alphaMax alphaMax [0 0 -1 0 0 0 0] 200.0;
// ************************************************************************* //

View File

@ -0,0 +1,48 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application adjointShapeOptimizationFoam;
startFrom startTime;
startTime 0;
stopAt endTime;
endTime 1000;
deltaT 1;
writeControl timeStep;
writeInterval 100;
purgeWrite 0;
writeFormat ascii;
writePrecision 12;
writeCompression uncompressed;
timeFormat general;
timePrecision 12;
runTimeModifiable yes;
// ************************************************************************* //

View File

@ -0,0 +1,76 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default steadyState;
}
gradSchemes
{
default Gauss linear;
grad(p) Gauss linear;
grad(U) Gauss linear;
}
divSchemes
{
default none;
div(phi,U) Gauss upwind;
div(phi,k) Gauss upwind;
div(phi,epsilon) Gauss upwind;
div((nuEff*dev(grad(U).T()))) Gauss linear;
div(-phi,Ua) Gauss upwind;
div((nuEff*dev(grad(Ua).T()))) Gauss linear;
}
laplacianSchemes
{
default Gauss linear corrected;
laplacian(nuEff,U) Gauss linear corrected;
laplacian(1,p) Gauss linear corrected;
laplacian(1|A(U),p) Gauss linear corrected;
laplacian(DkEff,k) Gauss linear corrected;
laplacian(DepsilonEff,epsilon) Gauss linear corrected;
laplacian(nuEff,Ua) Gauss linear corrected;
laplacian(1|A(Ua),pa) Gauss linear corrected;
}
interpolationSchemes
{
default linear;
interpolate(U) linear;
}
snGradSchemes
{
default corrected;
}
fluxRequired
{
default no;
p;
pa;
}
// ************************************************************************* //

View File

@ -0,0 +1,60 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
"(p|pa)"
{
solver GAMG;
tolerance 1e-08;
relTol 0.01;
smoother GaussSeidel;
nPreSweeps 0;
nPostSweeps 2;
cacheAgglomeration true;
nCellsInCoarsestLevel 10;
agglomerator faceAreaPair;
mergeLevels 1;
}
"(U|Ua|k|epsilon)"
{
solver smoothSolver;
smoother GaussSeidel;
nSweeps 2;
tolerance 1e-08;
relTol 0.1;
}
}
SIMPLE
{
nNonOrthogonalCorrectors 0;
pRefCell 0;
pRefValue 0;
}
relaxationFactors
{
"(p|pa)" 0.3;
"(U|Ua)" 0.7;
"(k|epsilon)" 0.7;
alpha 0.1;
}
// ************************************************************************* //

View File

@ -1,4 +1,5 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
@ -7,3 +8,5 @@ cleanCase
rm -rf logs
rm -f *.eps yPlus_vs_uPlus
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,5 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
@ -9,7 +10,8 @@ exponents="2 3 4 5 6 7 8"
echo "# yPlus vs uPlus" > yPlus_vs_uPlus
for e in $exponents; do
for e in $exponents
do
echo " Setting nu to 1e-$e"
sed "s/XXX/$e/g" constant/transportProperties.template \
@ -25,7 +27,8 @@ for e in $exponents; do
mv log.foamLog log.foamLog_$e
if [ -e logs/yPlus_0 ]; then
if [ -e logs/yPlus_0 ]
then
yPlus=`awk < logs/yPlus_0 'END{print $2}'`
uPlus=`awk < logs/uPlus_0 'END{print $2}'`
@ -39,7 +42,8 @@ done
# create validation plot
# test if gnuplot exists on the system
type -P gnuplot &>/dev/null || {
echo "gnuplot not found - skipping graph creation" >&2; exit 1;
echo "gnuplot not found - skipping graph creation" >&2
exit 1
}
graphName="OF_vs_ANAYTICAL.eps"
@ -65,5 +69,6 @@ gnuplot<<EOF
"yPlus_vs_uPlus" title "OpenFOAM" with points lt 1 pt 6
EOF
echo Done
echo "done"
# ----------------------------------------------------------------- end-of-file

View File

@ -1,4 +1,6 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
@ -8,3 +10,5 @@ application=`getApplication`
runApplication blockMesh
runApplication $application
runApplication postChannel
# ----------------------------------------------------------------- end-of-file

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