143 lines
4.2 KiB
C
143 lines
4.2 KiB
C
/*---------------------------------------------------------------------------*\
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========= |
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\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
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\\ / O peration |
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\\ / A nd | Copyright (C) 2011-2016 OpenFOAM Foundation
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\\/ M anipulation |
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-------------------------------------------------------------------------------
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License
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This file is part of OpenFOAM.
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OpenFOAM is free software: you can redistribute it and/or modify it
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under the terms of the GNU General Public License as published by
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the Free Software Foundation, either version 3 of the License, or
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(at your option) any later version.
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OpenFOAM is distributed in the hope that it will be useful, but WITHOUT
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ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or
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FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License
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for more details.
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You should have received a copy of the GNU General Public License
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along with OpenFOAM. If not, see <http://www.gnu.org/licenses/>.
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Application
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sprayEngineFoam
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Description
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Transient solver for compressible, turbulent engine flow with a spray
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particle cloud.
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\*---------------------------------------------------------------------------*/
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#include "fvCFD.H"
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#include "engineTime.H"
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#include "engineMesh.H"
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#include "turbulentFluidThermoModel.H"
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#include "basicSprayCloud.H"
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#include "psiChemistryModel.H"
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#include "radiationModel.H"
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#include "SLGThermo.H"
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#include "pisoControl.H"
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#include "fvOptions.H"
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#include "IFstream.H"//karam file in
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#include "OFstream.H"//karam file out
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#include "Math.H" //karam, math function (AMC, gammaln, TDMA)
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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int main(int argc, char *argv[])
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{
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#define CREATE_TIME createEngineTime.H
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#define CREATE_MESH createEngineMesh.H
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#include "postProcess.H"
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#include "setRootCase.H"
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#include "createEngineTime.H"
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#include "createEngineMesh.H"
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#include "createControl.H"
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#include "readEngineTimeControls.H"
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#include "createFields.H"
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#include "createFieldRefs.H"
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#include "createFvOptions.H"
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#include "createRhoUf.H"
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#include "compressibleCourantNo.H"
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#include "setInitialDeltaT.H"
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#include "initContinuityErrs.H"
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#include "startSummary.H"
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turbulence->validate();
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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#include "readCMCProperties.H" //karam, read and set fields for CMC calculation
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#include "setInitializationTime.H" //karam, set re-initialization time
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Info<< "\nStarting time loop\n" << endl;
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while (runTime.run())
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{
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#include "readEngineTimeControls.H"
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#include "compressibleCourantNo.H"
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#include "setDeltaT.H"
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runTime++;
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Info<< "Crank angle = " << runTime.theta() << " CA-deg" << endl;
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mesh.move();
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parcels.evolve();
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#include "rhoEqn.H"
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#include "UEqn.H"
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if(runTime.value() >= parcels.injectors()[0].timeStart())
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{
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CMC_on = true;
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if(init_start_CMC == true)
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{
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#include "QiCMC_init.H"
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#include "QhCMC_init.H"
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#include "CMCwrite.H"
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init_start_CMC = false;
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}
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#include "CMCequation.H"
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}
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#include "YEqn.H"
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#include "CMCintegration.H" //karam, conditional field integration and get reaction rate
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#include "EEqn.H"
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// --- Pressure corrector loop
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while (piso.correct())
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{
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#include "pEqn.H"
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}
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turbulence->correct();
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rho = thermo.rho();
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Pin_old = Pin; //karam, save old time value of pressure
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Pin = p.weightedAverage(mesh.V()).value(); //karam, get average pressure
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#include "logSummary.H" //karam, print log data
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if (runTime.write())
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{
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if(CMC_on == true)
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{
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#include "CMCwrite.H"
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}
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}
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Info<< "ExecutionTime = " << runTime.elapsedCpuTime() << " s"
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<< " ClockTime = " << runTime.elapsedClockTime() << " s"
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<< nl << endl;
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}
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Info<< "End\n" << endl;
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return 0;
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}
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// ************************************************************************* //
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