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foam-extend4.1-coherent-io/applications/solvers/solidMechanics/elasticOrthoNonLinULSolidFoam/elasticOrthoNonLinULSolidFoam.C

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C++

/*---------------------------------------------------------------------------*\
========= |
\\ / F ield | foam-extend: Open Source CFD
\\ / O peration | Version: 4.1
\\ / A nd | Web: http://www.foam-extend.org
\\/ M anipulation | For copyright notice see file Copyright
-------------------------------------------------------------------------------
License
This file is part of foam-extend.
foam-extend 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.
foam-extend 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 foam-extend. If not, see <http://www.gnu.org/licenses/>.
Application
elasticOrthoGenDirULSolidFoam
Description
Transient/steady-state segregated finite-volume solver for large strain
elastic orthotropic solid bodies allowing for general principal material
directions.
Displacement increment field DU is solved for using an updated Lagrangian
approach,
also generating the Almansi strain tensor field epsilon and Cauchy stress
tensor field sigma.
At the end of each time-step, the mesh is moved and sigma, epsilon and C
are rotated to the new configuration.
Please cite:
Cardiff P, Karac A & Ivankovic A, A Large Strain Finite Volume Method for
Orthotropic Bodies with General Material Orientations, Computer Methods
in Applied Mechanics & Engineering, Sep 2013,
http://dx.doi.org/10.1016/j.cma.2013.09.008
Author
Philip Cardiff UCD
\*---------------------------------------------------------------------------*/
#include "fvCFD.H"
#include "constitutiveModel.H"
#include "transformField.H"
#include "transformGeometricField.H"
#include "pointPatchInterpolation.H"
#include "primitivePatchInterpolation.H"
#include "pointFields.H"
#include "twoDPointCorrector.H"
#include "leastSquaresVolPointInterpolation.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
int main(int argc, char *argv[])
{
# include "setRootCase.H"
# include "createTime.H"
# include "createMesh.H"
# include "createFields.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Info<< "\nStarting time loop\n" << endl;
while(runTime.loop())
{
Info<< "Time = " << runTime.timeName() << nl << endl;
# include "readSolidMechanicsControls.H"
int iCorr = 0;
lduSolverPerformance solverPerf;
scalar initialResidual = 1.0;
lduMatrix::debug = 0;
//- div(sigmaOld) should be zero but I will include
//- it to make sure errors don't accumulate
volVectorField* oldErrorPtr = nullptr;
if (ensureTotalEquilibrium)
{
oldErrorPtr = new volVectorField
(
fvc::d2dt2(rho.oldTime(), U.oldTime())
- fvc::div(sigma)
);
}
do
{
DU.storePrevIter();
//- Updated lagrangian momentum equation
fvVectorMatrix DUEqn
(
fvm::d2dt2(rho, DU)
+ fvc::d2dt2(rho, U)
==
fvm::laplacian(K, DU, "laplacian(K,DU)")
+ fvc::div
(
DSigma
- (K & gradDU)
+ ( (sigma + DSigma) & gradDU ),
"div(sigma)"
)
//- fvc::laplacian(K, DU)
);
if (ensureTotalEquilibrium)
{
//- to stop accumulation of errors
DUEqn += *oldErrorPtr;
}
solverPerf = DUEqn.solve();
if (iCorr == 0)
{
initialResidual = solverPerf.initialResidual();
}
DU.relax();
gradDU = fvc::grad(DU);
//- for 2-D plane stress simulations, the zz component of gradDU
//- ensures sigma.zz() is zero
//- it is assumed that z is the empty direction
//# include "checkPlaneStress.H"
//- sigma needs to be calculated inside the momentum loop as
//- it is used in the momentum equation
DEpsilon = symm(gradDU) + 0.5*symm(gradDU & gradDU.T());
DSigma = C && DEpsilon;
if (iCorr % infoFrequency == 0)
{
Info<< "\tTime " << runTime.value()
<< ", Corr " << iCorr
<< ", Solving for " << DU.name()
<< " using " << solverPerf.solverName()
<< ", res = " << solverPerf.initialResidual()
//<< ", rel res = " << relativeResidual
<< ", inner iters " << solverPerf.nIterations() << endl;
}
}
while
(
solverPerf.initialResidual() > convergenceTolerance
&& ++iCorr < nCorr
);
Info<< nl << "Time " << runTime.value() << ", Solving for " << DU.name()
<< ", Initial residual = " << initialResidual
<< ", Final residual = " << solverPerf.initialResidual()
<< ", No outer iterations " << iCorr
<< nl << "ExecutionTime = " << runTime.elapsedCpuTime() << " s"
<< " ClockTime = " << runTime.elapsedClockTime() << " s"
<< endl;
# include "moveMeshLeastSquares.H"
# include "rotateFields.H"
# include "writeFields.H"
Info<< "ExecutionTime = " << runTime.elapsedCpuTime() << " s"
<< " ClockTime = " << runTime.elapsedClockTime() << " s\n\n"
<< endl;
}
Info<< "End\n" << endl;
return(0);
}
// ************************************************************************* //