engineCompRatio: Added support for specifying the combustion chamber cellSet/Zone
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
This commit is contained in:
@ -2,7 +2,7 @@
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========= |
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\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
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\\ / O peration | Website: https://openfoam.org
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\\ / A nd | Copyright (C) 2011-2022 OpenFOAM Foundation
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\\ / A nd | Copyright (C) 2011-2023 OpenFOAM Foundation
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\\/ M anipulation |
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-------------------------------------------------------------------------------
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License
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@ -25,15 +25,25 @@ Application
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engineCompRatio
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Description
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Calculate the geometric compression ratio.
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Calculate the compression ratio of the engine combustion chamber
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Note that if you have valves and/or extra volumes it will not work,
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since it calculates the volume at BDC and TDC.
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If the combustion chamber is not the entire mesh a \c cellSet or
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\c cellZone name of the cells in the combustion chamber can be provided.
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Usage
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\b engineCompRatio [OPTION]
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- \par -cellSet \<name\>
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Specify the cellSet name of the combustion chamber
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- \par -cellZone zoneName
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Specify the cellZone name of the combustion chamber
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\*---------------------------------------------------------------------------*/
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#include "argList.H"
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#include "volMesh.H"
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#include "cellSet.H"
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using namespace Foam;
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@ -41,49 +51,83 @@ using namespace Foam;
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int main(int argc, char *argv[])
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{
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argList::addOption
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(
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"cellSet",
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"name",
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"Calculate the volume of the specified cellSet"
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);
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argList::addOption
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(
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"cellZone",
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"name",
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"Calculate the volume of the specified cellZone"
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);
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#include "setRootCase.H"
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#include "createTime.H"
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#include "createMesh.H"
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// Cell labels of the cells in the combustion chamber
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// Defaults to all cells
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labelList ccCells(identityMap(mesh.nCells()));
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word cellSetName;
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word cellZoneName;
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if (args.optionReadIfPresent("cellSet", cellSetName))
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{
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// Read the cellSet for the combustion chamber
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const cellSet ccCellSet(mesh, cellSetName);
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ccCells = ccCellSet.toc();
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}
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else if (args.optionReadIfPresent("cellZone", cellZoneName))
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{
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const cellZone& ccCellZone = mesh.cellZones()[cellZoneName];
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ccCells = ccCellZone;
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}
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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scalar eps = 1.0e-10;
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scalar fullCycle = 360.0;
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scalar ca0 = -180.0;
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scalar ca1 = 0.0;
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const scalar eps = 1.0e-10;
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// Search for the CA >= the current CA which is divisible by 180
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int ca0 = -360;
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while (runTime.userTimeValue() > ca0)
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{
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ca0 += fullCycle;
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ca1 += fullCycle;
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ca0 += 180;
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}
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int ca1 = ca0 + 180;
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while (mag(runTime.userTimeValue() - ca0) > eps)
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if (mag(runTime.userTimeValue() - ca0) > eps)
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{
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scalar t0 = runTime.userTimeToTime(ca0 - runTime.userTimeValue());
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const scalar t0 = runTime.userTimeToTime(ca0 - runTime.userTimeValue());
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runTime.setDeltaT(t0);
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runTime++;
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Info<< "CA = " << runTime.userTimeValue() << endl;
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Info<< "Moving to CA = " << runTime.userTimeValue() << endl;
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mesh.move();
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}
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scalar Vmax = sum(mesh.V().field());
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const scalar V0 = gSum(scalarField(mesh.V(), ccCells));
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Info << "Volume at " << runTime.userTimeValue() << "CA = " << V0 << endl;
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while (mag(runTime.userTimeValue()-ca1) > eps)
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if (mag(runTime.userTimeValue()-ca1) > eps)
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{
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scalar t1 = runTime.userTimeToTime(ca1 - runTime.userTimeValue());
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const scalar t1 = runTime.userTimeToTime(ca1 - runTime.userTimeValue());
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runTime.setDeltaT(t1);
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runTime++;
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Info<< "CA = " << runTime.userTimeValue() << endl;
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Info<< "Moving to CA = " << runTime.userTimeValue() << endl;
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mesh.move();
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}
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scalar Vmin = sum(mesh.V().field());
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const scalar V1 = gSum(scalarField(mesh.V(), ccCells));
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Info << "Volume at " << runTime.userTimeValue() << "CA = " << V1 << endl;
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const scalar Vmin(min(V0, V1));
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const scalar Vmax(max(V0, V1));
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Info<< "\nCompression ratio = " << Vmax/Vmin << endl;
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Info<< "\nVmax = " << Vmax;
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Info<< ", Vmin = " << Vmin << endl;
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Info<< "Compression ratio Vmax/Vmin = " << Vmax/Vmin << endl;
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Info<< "\nEnd\n" << endl;
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return 0;
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