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Commit 031de9c4 authored by mattijs's avatar mattijs
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ENH: XiDyMFoam: new solver and tutorials

XiDyMFoam               : compressible version of XiFoam
oscillatingCylinder     : 2D case with cylinder moving up and down
annularCombustorTurbine : part of 3D combuster using cyclicPeriodicAMI
parent 4ef54948
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with 895 additions and 8 deletions
XiDyMFoam.C
EXE = $(FOAM_APPBIN)/XiDyMFoam
EXE_INC = \
-I.. \
-I$(LIB_SRC)/finiteVolume/lnInclude \
-I$(LIB_SRC)/fvOptions/lnInclude \
-I$(LIB_SRC)/dynamicFvMesh/lnInclude \
-I$(LIB_SRC)/dynamicMesh/lnInclude \
-I$(LIB_SRC)/meshTools/lnInclude \
-I$(LIB_SRC)/sampling/lnInclude \
-I$(LIB_SRC)/engine/lnInclude \
-I$(LIB_SRC)/thermophysicalModels/specie/lnInclude \
-I$(LIB_SRC)/transportModels/compressible/lnInclude \
-I$(LIB_SRC)/thermophysicalModels/basic/lnInclude \
-I$(LIB_SRC)/thermophysicalModels/reactionThermo/lnInclude \
-I$(LIB_SRC)/TurbulenceModels/turbulenceModels/lnInclude \
-I$(LIB_SRC)/TurbulenceModels/compressible/lnInclude \
-I$(LIB_SRC)/thermophysicalModels/laminarFlameSpeed/lnInclude
EXE_LIBS = \
-lfiniteVolume \
-lfvOptions \
-ldynamicFvMesh \
-ltopoChangerFvMesh \
-ldynamicMesh \
-lmeshTools \
-lsampling \
-lengine \
-lturbulenceModels \
-lcompressibleTurbulenceModels \
-lcompressibleTransportModels \
-lfluidThermophysicalModels \
-lreactionThermophysicalModels \
-lspecie \
-llaminarFlameSpeedModels
/*---------------------------------------------------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | Copyright (C) 2011-2015 OpenFOAM Foundation
\\/ M anipulation | Copyright (C) 2015 OpenCFD Ltd.
-------------------------------------------------------------------------------
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 3 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, see <http://www.gnu.org/licenses/>.
Application
XiFoam
Description
Solver for compressible premixed/partially-premixed combustion with
turbulence modelling.
Combusting RANS code using the b-Xi two-equation model.
Xi may be obtained by either the solution of the Xi transport
equation or from an algebraic exression. Both approaches are
based on Gulder's flame speed correlation which has been shown
to be appropriate by comparison with the results from the
spectral model.
Strain effects are encorporated directly into the Xi equation
but not in the algebraic approximation. Further work need to be
done on this issue, particularly regarding the enhanced removal rate
caused by flame compression. Analysis using results of the spectral
model will be required.
For cases involving very lean Propane flames or other flames which are
very strain-sensitive, a transport equation for the laminar flame
speed is present. This equation is derived using heuristic arguments
involving the strain time scale and the strain-rate at extinction.
the transport velocity is the same as that for the Xi equation.
\*---------------------------------------------------------------------------*/
#include "fvCFD.H"
#include "dynamicFvMesh.H"
#include "psiuReactionThermo.H"
#include "turbulentFluidThermoModel.H"
#include "laminarFlameSpeed.H"
#include "ignition.H"
#include "Switch.H"
#include "pimpleControl.H"
#include "CorrectPhi.H"
#include "fvIOoptionList.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
int main(int argc, char *argv[])
{
#include "setRootCase.H"
#include "createTime.H"
#include "createDynamicFvMesh.H"
#include "initContinuityErrs.H"
pimpleControl pimple(mesh);
#include "readCombustionProperties.H"
#include "readGravitationalAcceleration.H"
#include "createFields.H"
#include "createMRF.H"
#include "createFvOptions.H"
#include "createRhoUf.H"
#include "createControls.H"
#include "initContinuityErrs.H"
#include "compressibleCourantNo.H"
#include "setInitialDeltaT.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Info<< "\nStarting time loop\n" << endl;
while (runTime.run())
{
#include "createTimeControls.H"
{
// Store divrhoU from the previous mesh so that it can be mapped
// and used in correctPhi to ensure the corrected phi has the
// same divergence
volScalarField divrhoU
(
"divrhoU",
fvc::div(fvc::absolute(phi, rho, U))
);
#include "compressibleCourantNo.H"
#include "setDeltaT.H"
runTime++;
Info<< "Time = " << runTime.timeName() << nl << endl;
// Store momentum to set rhoUf for introduced faces.
volVectorField rhoU("rhoU", rho*U);
// Do any mesh changes
mesh.update();
if (mesh.changing() && correctPhi)
{
// Calculate absolute flux from the mapped surface velocity
phi = mesh.Sf() & rhoUf;
#include "correctPhi.H"
// Make the fluxes relative to the mesh-motion
fvc::makeRelative(phi, rho, U);
}
}
if (mesh.changing() && checkMeshCourantNo)
{
#include "meshCourantNo.H"
}
#include "rhoEqn.H"
Info<< "rhoEqn max/min : " << max(rho).value()
<< " " << min(rho).value() << endl;
// --- Pressure-velocity PIMPLE corrector loop
while (pimple.loop())
{
#include "UEqn.H"
#include "ftEqn.H"
#include "bEqn.H"
#include "EauEqn.H"
#include "EaEqn.H"
if (!ign.ignited())
{
thermo.heu() == thermo.he();
}
// --- Pressure corrector loop
while (pimple.correct())
{
#include "pEqn.H"
}
if (pimple.turbCorr())
{
turbulence->correct();
}
}
rho = thermo.rho();
runTime.write();
Info<< "ExecutionTime = " << runTime.elapsedCpuTime() << " s"
<< " ClockTime = " << runTime.elapsedClockTime() << " s"
<< nl << endl;
}
Info<< "End\n" << endl;
return 0;
}
// ************************************************************************* //
CorrectPhi
(
U,
phi,
p,
rho,
psi,
dimensionedScalar("rAUf", dimTime, 1),
divrhoU,
pimple
);
#include "createTimeControls.H"
bool correctPhi
(
pimple.dict().lookupOrDefault<Switch>("correctPhi", true)
);
bool checkMeshCourantNo
(
pimple.dict().lookupOrDefault<Switch>("checkMeshCourantNo", false)
);
rho = thermo.rho();
volScalarField rAU(1.0/UEqn.A());
surfaceScalarField rhorAUf("rhorAUf", fvc::interpolate(rho*rAU));
volVectorField HbyA("HbyA", U);
HbyA = rAU*UEqn.H();
if (pimple.transonic())
{
surfaceScalarField phid
(
"phid",
fvc::interpolate(psi)
*(
(fvc::interpolate(HbyA) & mesh.Sf())
+ rhorAUf*fvc::ddtCorr(rho, U, phi)/fvc::interpolate(rho)
)
);
fvc::makeRelative(phid, psi, U);
MRF.makeRelative(fvc::interpolate(psi), phid);
while (pimple.correctNonOrthogonal())
{
fvScalarMatrix pEqn
(
fvm::ddt(psi, p)
+ fvm::div(phid, p)
- fvm::laplacian(rhorAUf, p)
==
fvOptions(psi, p, rho.name())
);
pEqn.solve(mesh.solver(p.select(pimple.finalInnerIter())));
if (pimple.finalNonOrthogonalIter())
{
phi == pEqn.flux();
}
}
}
else
{
surfaceScalarField phiHbyA
(
"phiHbyA",
(
(fvc::interpolate(rho*HbyA) & mesh.Sf())
+ rhorAUf*fvc::ddtCorr(rho, U, rhoUf)
)
);
fvc::makeRelative(phiHbyA, rho, U);
MRF.makeRelative(phiHbyA);
while (pimple.correctNonOrthogonal())
{
fvScalarMatrix pEqn
(
fvm::ddt(psi, p)
+ fvc::div(phiHbyA)
- fvm::laplacian(rhorAUf, p)
==
fvOptions(psi, p, rho.name())
);
pEqn.solve(mesh.solver(p.select(pimple.finalInnerIter())));
if (pimple.finalNonOrthogonalIter())
{
phi = phiHbyA + pEqn.flux();
}
}
}
#include "rhoEqn.H"
#include "compressibleContinuityErrs.H"
U = HbyA - rAU*fvc::grad(p);
U.correctBoundaryConditions();
fvOptions.correct(U);
K = 0.5*magSqr(U);
{
rhoUf = fvc::interpolate(rho*U);
surfaceVectorField n(mesh.Sf()/mesh.magSf());
rhoUf += n*(fvc::absolute(phi, rho, U)/mesh.magSf() - (n & rhoUf));
}
if (thermo.dpdt())
{
dpdt = fvc::ddt(p);
if (mesh.moving())
{
dpdt -= fvc::div(fvc::meshPhi(rho, U), p);
}
}
#include "readTimeControls.H"
bool correctPhi =
pimple.dict().lookupOrDefault<Switch>("correctPhi", true);
bool checkMeshCourantNo =
pimple.dict().lookupOrDefault<Switch>("checkMeshCourantNo", false);
......@@ -3,7 +3,7 @@
# \\ / F ield | OpenFOAM: The Open Source CFD Toolbox
# \\ / O peration |
# \\ / A nd | Copyright (C) 2011-2015 OpenFOAM Foundation
# \\/ M anipulation |
# \\/ M anipulation | Copyright (C) 2015 OpenCFD Ltd.
#------------------------------------------------------------------------------
# License
# This file is part of OpenFOAM.
......@@ -40,28 +40,46 @@ getApplication()
runApplication()
{
APP_LOGFILE=''
if [ "$1" = "-l" ]
then
APP_LOGFILE=$2
shift 2
fi
APP_RUN=$1
APP_NAME=${1##*/}
shift
if [ -f log.$APP_NAME ]
APP_LOGFILE=${APP_LOGFILE:="log.$APP_NAME"}
if [ -f $APP_LOGFILE ]
then
echo "$APP_NAME already run on $PWD: remove log file to re-run"
echo "$APP_NAME already run on $PWD: remove log file $APP_LOGFILE to re-run"
else
echo "Running $APP_RUN on $PWD"
$APP_RUN "$@" > log.$APP_NAME 2>&1
$APP_RUN "$@" > $APP_LOGFILE 2>&1
fi
}
runParallel()
{
APP_LOGFILE=''
if [ "$1" = "-l" ]
then
APP_LOGFILE=$2
shift 2
fi
APP_RUN=$1
APP_NAME=${1##*/}
shift
if [ -f log.$APP_NAME ]
APP_LOGFILE=${APP_LOGFILE:="log.$APP_NAME"}
if [ -f $APP_LOGFILE ]
then
echo "$APP_NAME already run on $PWD: remove log file to re-run"
echo "$APP_NAME already run on $PWD: remove log file $APP_LOGFILE to re-run"
else
nProcs=$1
shift
......@@ -70,9 +88,9 @@ runParallel()
#if [ "$WM_SCHEDULER" ]
#then
# echo "$PWD: $WM_SCHEDULER -np $nProcs" 1>&2
# $WM_SCHEDULER -np $nProcs "( mpirun -np $nProcs $APP_RUN -parallel "$@" < /dev/null > log.$APP_NAME 2>&1 )"
# $WM_SCHEDULER -np $nProcs "( mpirun -np $nProcs $APP_RUN -parallel "$@" < /dev/null > $APP_LOGFILE 2>&1 )"
#else
( mpirun -np $nProcs $APP_RUN -parallel "$@" < /dev/null > log.$APP_NAME 2>&1 )
( mpirun -np $nProcs $APP_RUN -parallel "$@" < /dev/null > $APP_LOGFILE 2>&1 )
#fi
fi
}
......
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object Su;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform 0.135;
boundaryField
{
#include "${WM_PROJECT_DIR}/etc/caseDicts/setConstraintTypes"
inlet
{
type fixedValue;
value $internalField;
}
outlet
{
type inletOutlet;
inletValue $internalField;
value $internalField;
}
wall
{
type zeroGradient;
}
}
// ************************************************************************* //
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object T;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 1 0 0 0];
inletField uniform 573;
internalField uniform 2400;
boundaryField
{
#include "${WM_PROJECT_DIR}/etc/caseDicts/setConstraintTypes"
inlet
{
type fixedValue;
value $inletField;
}
outlet
{
type inletOutlet;
inletValue $internalField;
value $internalField;
}
wall
{
type zeroGradient;
}
}
// ************************************************************************* //
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object Tu;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 1 0 0 0];
internalField uniform 573;
boundaryField
{
#include "${WM_PROJECT_DIR}/etc/caseDicts/setConstraintTypes"
inlet
{
type fixedValue;
value $internalField;
}
outlet
{
type inletOutlet;
inletValue $internalField;
value $internalField;
}
wall
{
type zeroGradient;
}
}
// ************************************************************************* //
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volVectorField;
location "0";
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (4 0 0);
boundaryField
{
#include "${WM_PROJECT_DIR}/etc/caseDicts/setConstraintTypes"
inlet
{
type cylindricalInletVelocity;
centre (-0.64 0.5 0);
axis (1 0 0);
axialVelocity 40;
radialVelocity 20;
rpm 12732; // ut=40,r=3e-2,omega=ut/r,rpm=omega*60/(2*pi)
value uniform (0 0 0);
}
outlet
{
type pressureInletOutletVelocity;
inletValue (0 0 0);
value $internalField;
}
wall
{
type movingWallVelocity;
value uniform (0 0 0);
}
}
// ************************************************************************* //
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object Xi;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 1;
boundaryField
{
#include "${WM_PROJECT_DIR}/etc/caseDicts/setConstraintTypes"
inlet
{
type fixedValue;
value $internalField;
}
outlet
{
type inletOutlet;
inletValue $internalField;
value $internalField;
}
wall
{
type zeroGradient;
}
}
// ************************************************************************* //
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object alphat;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
#include "${WM_PROJECT_DIR}/etc/caseDicts/setConstraintTypes"
inlet
{
type calculated;
}
outlet
{
type calculated;
}
wall
{
//type compressible::alphatWallFunction;
//mut mut;
//value $internalField;
type calculated;
}
}
// ************************************************************************* //
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object b;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0;
boundaryField
{
#include "${WM_PROJECT_DIR}/etc/caseDicts/setConstraintTypes"
inlet
{
type fixedValue;
value uniform 1;
}
outlet
{
type inletOutlet;
inletValue $internalField;
value $internalField;
}
wall
{
type zeroGradient;
}
}
// ************************************************************************* //
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object ft;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0.0834168596800118;
boundaryField
{
#include "${WM_PROJECT_DIR}/etc/caseDicts/setConstraintTypes"
inlet
{
type fixedValue;
value $internalField;
}
outlet
{
type inletOutlet;
inletValue $internalField;
value $internalField;
}
wall
{
type zeroGradient;
}
}
// ************************************************************************* //
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [ 0 2 -2 0 0 0 0 ];
internalField uniform 6;
boundaryField
{
#include "${WM_PROJECT_DIR}/etc/caseDicts/setConstraintTypes"
inlet
{
type turbulentIntensityKineticEnergyInlet;
intensity 0.05;
value $internalField;
}
outlet
{
type inletOutlet;
inletValue $internalField;
value $internalField;
}
wall
{
type zeroGradient;
}
}
// ************************************************************************* //
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object nut;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [ 0 2 -1 0 0 0 0 ];
internalField uniform 0;
boundaryField
{
#include "${WM_PROJECT_DIR}/etc/caseDicts/setConstraintTypes"
inlet
{
type calculated;
}
outlet
{
type calculated;
}
wall
{
//type nutUSpaldingWallFunction;
//value $internalField;
type calculated;
}
}
// ************************************************************************* //
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object p;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -2 0 0 0 0];
internalField uniform 10e5;
boundaryField
{
#include "${WM_PROJECT_DIR}/etc/caseDicts/setConstraintTypes"
inlet
{
type zeroGradient;
}
outlet
{
type waveTransmissive;
gamma 1.28;
fieldInf 10e5;
lInf 0.2;
value $internalField;
}
wall
{
type zeroGradient;
}
}
// ************************************************************************* //
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object pPotential;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 0;
boundaryField
{
#include "${WM_PROJECT_DIR}/etc/caseDicts/setConstraintTypes"
inlet
{
type zeroGradient;
}
outlet
{
type fixedValue;
value $internalField;
}
wall
{
type zeroGradient;
}
}
// ************************************************************************* //
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