OpenFOAM-dev / data /applications /utilities /postProcessing /miscellaneous /engineCompRatio /engineCompRatio.C
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| /*---------------------------------------------------------------------------*\ | |
| ========= | | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | |
| \\ / O peration | Website: https://openfoam.org | |
| \\ / A nd | Copyright (C) 2011-2026 OpenFOAM Foundation | |
| \\/ M anipulation | | |
| ------------------------------------------------------------------------------- | |
| 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 | |
| engineCompRatio | |
| Description | |
| Calculate the compression ratio of the engine combustion chamber | |
| If the combustion chamber is not the entire mesh a \c cellSet or | |
| \c cellZone name of the cells in the combustion chamber can be provided. | |
| Usage | |
| \b engineCompRatio [OPTION] | |
| - \par -cellSet \<name\> | |
| Specify the cellSet name of the combustion chamber | |
| - \par -cellZone zoneName | |
| Specify the cellZone name of the combustion chamber | |
| \*---------------------------------------------------------------------------*/ | |
| using namespace Foam; | |
| // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // | |
| int main(int argc, char *argv[]) | |
| { | |
| argList::addOption | |
| ( | |
| "cellSet", | |
| "name", | |
| "Calculate the volume of the specified cellSet" | |
| ); | |
| argList::addOption | |
| ( | |
| "cellZone", | |
| "name", | |
| "Calculate the volume of the specified cellZone" | |
| ); | |
| // Cell labels of the cells in the combustion chamber | |
| // Defaults to all cells | |
| labelList ccCells(identityMap(mesh.nCells())); | |
| word cellSetName; | |
| word cellZoneName; | |
| if (args.optionReadIfPresent("cellSet", cellSetName)) | |
| { | |
| // Read the cellSet for the combustion chamber | |
| const cellSet ccCellSet(mesh, cellSetName); | |
| ccCells = ccCellSet.toc(); | |
| } | |
| else if (args.optionReadIfPresent("cellZone", cellZoneName)) | |
| { | |
| const cellZone& ccCellZone = mesh.cellZones()[cellZoneName]; | |
| ccCells = ccCellZone; | |
| } | |
| // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // | |
| const scalar eps = 1.0e-10; | |
| // Search for the CA >= the current CA which is divisible by 180 | |
| int ca0 = -360; | |
| while (runTime.userTimeValue() > ca0) | |
| { | |
| ca0 += 180; | |
| } | |
| int ca1 = ca0 + 180; | |
| if (mag(runTime.userTimeValue() - ca0) > eps) | |
| { | |
| const scalar t0 = runTime.userTimeToTime(ca0 - runTime.userTimeValue()); | |
| runTime.setDeltaT(t0); | |
| runTime++; | |
| Info<< "Moving to CA = " << runTime.userTimeValue() << endl; | |
| mesh.move(); | |
| } | |
| const scalar V0 = gSum(scalarField(mesh.V(), ccCells)); | |
| Info << "Volume at " << runTime.userTimeValue() << "CA = " << V0 << endl; | |
| if (mag(runTime.userTimeValue()-ca1) > eps) | |
| { | |
| const scalar t1 = runTime.userTimeToTime(ca1 - runTime.userTimeValue()); | |
| runTime.setDeltaT(t1); | |
| runTime++; | |
| Info<< "Moving to CA = " << runTime.userTimeValue() << endl; | |
| mesh.move(); | |
| } | |
| const scalar V1 = gSum(scalarField(mesh.V(), ccCells)); | |
| Info << "Volume at " << runTime.userTimeValue() << "CA = " << V1 << endl; | |
| const scalar Vmin(min(V0, V1)); | |
| const scalar Vmax(max(V0, V1)); | |
| Info<< "\nCompression ratio = " << Vmax/Vmin << endl; | |
| Info<< "\nEnd\n" << endl; | |
| return 0; | |
| } | |
| // ************************************************************************* // | |