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Tutorial fix elasticThermalSolidFoam

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This commit is contained in:
Hrvoje Jasak 2014-04-10 20:54:24 +01:00
parent 45576c2dea
commit e732980a53
8 changed files with 181 additions and 190 deletions
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57
applications/solvers/solidMechanics/elasticThermalSolidFoam/createFields.H
View file

@ -12,21 +12,20 @@
mesh
);
// volTensorField gradU = fvc::grad(U);
volTensorField gradU
(
IOobject
(
"grad(U)",
runTime.timeName(),
mesh,
IOobject::NO_READ,
IOobject::NO_WRITE
),
"grad(U)",
runTime.timeName(),
mesh,
IOobject::NO_READ,
IOobject::NO_WRITE
),
mesh,
dimensionedTensor("zero", dimless, tensor::zero)
);
//surfaceVectorField snGradU = fvc::snGrad(U);
);
surfaceVectorField snGradU
(
IOobject
@ -38,7 +37,7 @@
IOobject::NO_WRITE
),
mesh,
dimensionedVector("zero", dimless, vector::zero)
dimensionedVector("zero", dimless, vector::zero)
);
volSymmTensorField epsilon
@ -115,31 +114,33 @@
thermalModel thermal(T);
volScalarField C = thermal.C();
volScalarField k = thermal.k();
volScalarField k
(
"DT",
thermal.k()
);
volScalarField threeKalpha = rheology.threeK()*rho*thermal.alpha();
surfaceScalarField threeKalphaf = fvc::interpolate(threeKalpha, "threeKalpha");
surfaceScalarField threeKalphaf =
fvc::interpolate(threeKalpha, "threeKalpha");
volScalarField T0 = thermal.T0();
volScalarField rhoC = rho*C;
// for aitken relaxation
volVectorField aitkenDelta
(
// for aitken relaxation
volVectorField aitkenDelta
(
IOobject
(
"aitkenDelta",
runTime.timeName(),
mesh,
IOobject::NO_READ,
IOobject::NO_WRITE
),
"aitkenDelta",
runTime.timeName(),
mesh,
IOobject::NO_READ,
IOobject::NO_WRITE
),
mesh,
dimensionedVector("zero", dimLength, vector::zero)
);
// aitken relaxation factor
scalar aitkenInitialRes = 1.0;
scalar aitkenTheta = 0.01;
// if(mesh.relax(U.name()))
// {
// aitkenTheta = mesh.relaxationFactor(U.name());
// }
// aitken relaxation factor
scalar aitkenInitialRes = 1.0;
scalar aitkenTheta = 0.01;

171
applications/solvers/solidMechanics/elasticThermalSolidFoam/elasticThermalSolidFoam.C
View file

@ -46,100 +46,99 @@ Author
int main(int argc, char *argv[])
{
# include "setRootCase.H"
# include "createTime.H"
# include "createMesh.H"
# include "createFields.H"
# include "readDivSigmaExpMethod.H"
# include "setRootCase.H"
# include "createTime.H"
# include "createMesh.H"
# include "createFields.H"
# include "readDivSigmaExpMethod.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Info<< "\nStarting time loop\n" << endl;
Info<< "\nStarting time loop\n" << endl;
while(runTime.loop())
while(runTime.loop())
{
Info<< "Time: " << runTime.timeName() << nl << endl;
Info<< "Time: " << runTime.timeName() << nl << endl;
# include "readSolidMechanicsControls.H"
# include "readSolidMechanicsControls.H"
int iCorr = 0;
scalar initialResidual = 1.0;
scalar relResT = 1.0;
scalar relResU = 1.0;
lduMatrix::solverPerformance solverPerfU;
lduMatrix::solverPerformance solverPerfT;
lduMatrix::debug = 0;
int iCorr = 0;
scalar initialResidual = 1.0;
scalar relResT = 1.0;
scalar relResU = 1.0;
lduMatrix::solverPerformance solverPerfU;
lduMatrix::solverPerformance solverPerfT;
lduMatrix::debug = 0;
// solve energy equation for temperature
// the loop is for non-orthogonal corrections
Info<< "Solving for " << T.name() << nl;
do
{
T.storePrevIter();
// solve energy equation for temperature
// the loop is for non-orthogonal corrections
Info<< "Solving for " << T.name() << nl;
do
{
T.storePrevIter();
fvScalarMatrix TEqn
(
rhoC*fvm::ddt(T) == fvm::laplacian(k, T, "laplacian(k,T)")
);
fvScalarMatrix TEqn
(
rhoC*fvm::ddt(T) == fvm::laplacian(k, T, "laplacian(k,T)")
);
solverPerfT = TEqn.solve();
solverPerfT = TEqn.solve();
T.relax();
T.relax();
# include "calculateRelResT.H"
# include "calculateRelResT.H"
if (iCorr % infoFrequency == 0)
{
Info<< "\tCorrector " << iCorr
<< ", residual = " << solverPerfT.initialResidual()
<< ", relative res = " << relResT
<< ", inner iters = " << solverPerfT.nIterations() << endl;
}
}
while
(
relResT > convergenceToleranceT
&&
++iCorr < nCorr
);
if (iCorr % infoFrequency == 0)
{
Info<< "\tCorrector " << iCorr
<< ", residual = " << solverPerfT.initialResidual()
<< ", relative res = " << relResT
<< ", inner iters = " << solverPerfT.nIterations() << endl;
}
}
while
(
relResT > convergenceToleranceT
&& ++iCorr < nCorr
);
Info<< "Solved for " << T.name()
<< " using " << solverPerfT.solverName()
<< " in " << iCorr << " iterations"
<< ", residual = " << solverPerfT.initialResidual()
<< ", relative res = " << relResT << nl
<< "ExecutionTime = " << runTime.elapsedCpuTime() << " s"
<< ", ClockTime = " << runTime.elapsedClockTime() << " s"
<< endl;
Info<< "Solved for " << T.name()
<< " using " << solverPerfT.solverName()
<< " in " << iCorr << " iterations"
<< ", residual = " << solverPerfT.initialResidual()
<< ", relative res = " << relResT << nl
<< "ExecutionTime = " << runTime.elapsedCpuTime() << " s"
<< ", ClockTime = " << runTime.elapsedClockTime() << " s"
<< endl;
// solve momentum equation for displacement
iCorr = 0;
volVectorField gradThreeKalphaDeltaT =
fvc::grad(threeKalpha*(T-T0), "grad(threeKalphaDeltaT)");
surfaceVectorField threeKalphaDeltaTf =
mesh.Sf()*threeKalphaf*fvc::interpolate(T-T0, "deltaT");
// Solve momentum equation for displacement
iCorr = 0;
volVectorField gradThreeKalphaDeltaT =
fvc::grad(threeKalpha*(T-T0), "grad(threeKalphaDeltaT)");
surfaceVectorField threeKalphaDeltaTf =
mesh.Sf()*threeKalphaf*fvc::interpolate(T-T0, "deltaT");
Info<< "Solving for " << U.name() << nl;
do
Info<< "Solving for " << U.name() << nl;
do
{
U.storePrevIter();
# include "calculateDivSigmaExp.H"
# include "calculateDivSigmaExp.H"
// Linear momentum equaiton
fvVectorMatrix UEqn
(
rho*fvm::d2dt2(U)
==
fvm::laplacian(2*muf + lambdaf, U, "laplacian(DU,U)")
+ divSigmaExp
);
(
rho*fvm::d2dt2(U)
==
fvm::laplacian(2*muf + lambdaf, U, "laplacian(DU,U)")
+ divSigmaExp
);
solverPerfU = UEqn.solve();
if (aitkenRelax)
{
# include "aitkenRelaxation.H"
# include "aitkenRelaxation.H"
}
else
{
@ -148,7 +147,7 @@ int main(int argc, char *argv[])
gradU = fvc::grad(U);
# include "calculateRelResU.H"
# include "calculateRelResU.H"
if (iCorr == 0)
{
@ -160,6 +159,7 @@ int main(int argc, char *argv[])
Info<< "\tCorrector " << iCorr
<< ", residual = " << solverPerfU.initialResidual()
<< ", relative res = " << relResU;
if (aitkenRelax)
{
Info << ", aitken = " << aitkenTheta;
@ -167,25 +167,24 @@ int main(int argc, char *argv[])
Info<< ", inner iters = " << solverPerfU.nIterations() << endl;
}
}
while
(
iCorr++ == 0
||
(//solverPerfU.initialResidual() > convergenceTolerance
relResU > convergenceToleranceU
&&
iCorr < nCorr)
);
while
(
iCorr++ == 0
|| (
relResU > convergenceToleranceU
&& iCorr < nCorr
)
);
Info<< "Solved for " << U.name()
<< " using " << solverPerfU.solverName()
<< " in " << iCorr << " iterations"
<< ", initial res = " << initialResidual
<< ", final res = " << solverPerfU.initialResidual()
<< ", final rel res = " << relResU << nl
<< "ExecutionTime = " << runTime.elapsedCpuTime() << " s"
<< ", ClockTime = " << runTime.elapsedClockTime() << " s"
<< endl;
Info<< "Solved for " << U.name()
<< " using " << solverPerfU.solverName()
<< " in " << iCorr << " iterations"
<< ", initial res = " << initialResidual
<< ", final res = " << solverPerfU.initialResidual()
<< ", final rel res = " << relResU << nl
<< "ExecutionTime = " << runTime.elapsedCpuTime() << " s"
<< ", ClockTime = " << runTime.elapsedClockTime() << " s"
<< endl;
# include "calculateEpsilonSigma.H"
# include "writeFields.H"

18
tutorials/solidMechanics/elasticThermalSolidFoam/hotCylinder/0/T
View file

@ -32,27 +32,23 @@ boundaryField
inside
{
type fixedValue;
value uniform 100;
type fixedValue;
value uniform 100;
}
outside
{
type fixedValue;
value uniform 100;
type fixedValue;
value uniform 100;
}
front
{
type empty;
//type symmetryPlane;
type empty;
}
back
{
type empty;
//type symmetryPlane;
type empty;
}
}
// ************************************************************************* //

19
tutorials/solidMechanics/elasticThermalSolidFoam/hotCylinder/0/U
View file

@ -29,32 +29,31 @@ boundaryField
{
type symmetryPlane;
}
inside
{
type solidTraction;
traction uniform ( 0 0 0 );
pressure uniform 50e6;
value uniform (0 0 0);
type solidTraction;
traction uniform ( 0 0 0 );
pressure uniform 50e6;
DT k;
value uniform (0 0 0);
}
outside
{
type solidTraction;
traction uniform ( 0 0 0 );
pressure uniform 0.1e6;
DT k;
value uniform (0 0 0);
}
front
{
type empty;
type empty;
}
back
{
type empty;
type empty;
}
}
// ************************************************************************* //

2
tutorials/solidMechanics/elasticThermalSolidFoam/hotCylinder/Allrun
View file

@ -9,4 +9,4 @@ runApplication blockMesh
runApplication $application
(cd analyticalHotCylinder && runApplication wmake)
runApplication analyticalHotCylinder
runApplication analyticalHotCylinder

59
tutorials/solidMechanics/elasticThermalSolidFoam/hotCylinder/constant/polyMesh/blockMeshDict
View file

@ -19,15 +19,14 @@ convertToMeters 1;
vertices
(
(0 0.5 0)
(0.5 0 0)
(0.7 0 0)
(0 0.7 0)
(0 0.5 0.1)
(0.5 0 0.1)
(0.7 0 0.1)
(0 0.7 0.1)
(0 0.5 0)
(0.5 0 0)
(0.7 0 0)
(0 0.7 0)
(0 0.5 0.1)
(0.5 0 0.1)
(0.7 0 0.1)
(0 0.7 0.1)
);
blocks
@ -45,34 +44,30 @@ edges
patches
(
symmetryPlane left
(
(4 7 3 0)
)
symmetryPlane bottom
(
(1 2 6 5)
)
patch inside
(
(0 1 5 4)
)
patch outside
(
(7 6 2 3)
)
empty back
(
(3 2 1 0)
(3 2 1 0)
)
empty front
(
(4 5 6 7)
)
symmetryPlane left
(
(4 7 3 0)
)
symmetryPlane bottom
(
(1 2 6 5)
)
patch inside
(
(0 1 5 4)
)
patch outside
(
(7 6 2 3)
)
(4 5 6 7)
)
);
mergePatchPairs

34
tutorials/solidMechanics/elasticThermalSolidFoam/hotCylinder/constant/polyMesh/boundary
View file

@ -1,7 +1,7 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | foam-extend: Open Source CFD |
| \\ / O peration | Version: 3.0 |
| \\ / O peration | Version: 3.0 |
| \\ / A nd | Web: http://www.extend-project.de |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
@ -17,41 +17,41 @@ FoamFile
6
(
back
{
type empty;
nFaces 600;
startFace 1130;
}
front
{
type empty;
nFaces 600;
startFace 1730;
}
left
{
type symmetryPlane;
nFaces 10;
startFace 2330;
startFace 1130;
}
bottom
{
type symmetryPlane;
nFaces 10;
startFace 2340;
startFace 1140;
}
inside
{
type patch;
nFaces 60;
startFace 2350;
startFace 1150;
}
outside
{
type patch;
nFaces 60;
startFace 2410;
startFace 1210;
}
back
{
type empty;
nFaces 600;
startFace 1270;
}
front
{
type empty;
nFaces 600;
startFace 1870;
}
)

11
tutorials/solidMechanics/elasticThermalSolidFoam/hotCylinder/constant/thermalProperties
View file

@ -16,11 +16,12 @@ FoamFile
thermal
{
type constant;
C C [0 2 -2 -1 0 0 0] 434;
k k [1 1 -3 -1 0 0 0] 250;
alpha alpha [0 0 0 -1 0 0 0] 2.3e-05;
T0 T0 [0 0 0 1 0 0 0] 0;
type constant;
C C [0 2 -2 -1 0 0 0] 434;
k k [1 1 -3 -1 0 0 0] 250;
alpha alpha [0 0 0 -1 0 0 0] 2.3e-05;
T0 T0 [0 0 0 1 0 0 0] 0;
}
// ************************************************************************* //