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5d9e278e92
- for some special cases we wish to mark command-line arguments as
being optional, in order to do our own treatment. For example,
when an arbitrary number of arguments should be allowed.
Now tag this situation with argList::noMandatoryArgs().
The argList::argsMandatory() query can then be used in any further
logic, including the standard default argument checking.
- with the new default check, can consolidate the special-purpose
"setRootCaseNonMandatoryArgs.H"
into the regular
"setRootCase.H"
- revert to a simple "setRootCase.H" and move all the listing related
bits to a "setRootCaseLists.H" file. This leaves the information
available for solvers, or whoever else wishes, without being
introduced everywhere.
- add include guards and scoping to the listing files and rename to
something less generic.
listOptions.H -> setRootCaseListOptions.H
listOutput.H -> setRootCaseListOutput.H
123 lines
3.3 KiB
C
123 lines
3.3 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) 2011-2017 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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coldEngineFoam
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Group
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grpCombustionSolvers grpMovingMeshSolvers
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Description
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Solver for cold-flow in internal combustion engines.
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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 "psiThermo.H"
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#include "turbulentFluidThermoModel.H"
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#include "OFstream.H"
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#include "fvOptions.H"
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#include "pimpleControl.H"
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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int main(int argc, char *argv[])
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{
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argList::addNote
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(
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"Solver for cold-flow in internal combustion engines."
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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 "setRootCaseLists.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 "createFields.H"
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#include "createFieldRefs.H"
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#include "createRhoUf.H"
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#include "initContinuityErrs.H"
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#include "readEngineTimeControls.H"
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#include "compressibleCourantNo.H"
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#include "setInitialDeltaT.H"
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#include "startSummary.H"
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turbulence->validate();
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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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<< "Engine time = " << runTime.theta() << runTime.unit()
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<< endl;
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mesh.move();
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#include "rhoEqn.H"
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// --- Pressure-velocity PIMPLE corrector loop
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while (pimple.loop())
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{
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#include "UEqn.H"
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// --- Pressure corrector loop
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while (pimple.correct())
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{
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#include "EEqn.H"
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#include "pEqn.H"
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}
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if (pimple.turbCorr())
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{
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turbulence->correct();
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}
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}
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runTime.write();
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#include "logSummary.H"
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runTime.printExecutionTime(Info);
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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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