/*---------------------------------------------------------------------------*\ ========= | \\ / 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 . Description Calculates the total forces on a patch: total force vector total normal force total force in each direction (x, y and z) Author philip.cardiff@ucd.ie \*---------------------------------------------------------------------------*/ #include "fvCFD.H" // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // int main(int argc, char *argv[]) { argList::validArgs.append("patch name"); argList::validOptions.insert("noMeshUpdate", ""); argList::validOptions.insert("nonLinear", ""); # include "addTimeOptions.H" # include "setRootCase.H" # include "createTime.H" // Get times list instantList Times = runTime.times(); // set startTime and endTime depending on -time and -latestTime options # include "checkTimeOptions.H" runTime.setTime(Times[startTime], startTime); # include "createMesh.H" bool noMeshUpdate = args.optionFound("noMeshUpdate"); bool nonLinear = args.optionFound("nonLinear"); word patchName(args.additionalArgs()[0]); label patchID = mesh.boundaryMesh().findPatchID(patchName); if (patchID == -1) { FatalError << "Cannot find patch " << patchName << exit(FatalError); } for (label i=startTime; iboundaryField()[patchID]; const scalarField J = det(F); const tensorField Finv = hinv(F); // current deformed patch area vectors are given by // Nanson's formula const vectorField deformedSf = J * Finv & Sf; const vectorField deformedN = deformedSf/mag(deformedSf); const symmTensorField& sigmaCauchyPatch = sigmaCauchyPtr->boundaryField()[patchID]; // reference areas and 2nd Piola-Kirchhoff stress totalForce = Sf & (sigmaPatch & F); totalNormalForce = sum(deformedN & (totalForce)); totalShearForce = sum((I -sqr(deformedN)) & (totalForce)); // deformed normals and Cauchy stress totalForceCauchy = deformedSf & (sigmaCauchyPatch); totalNormalForceCauchy = sum(deformedN & (totalForceCauchy)); totalShearForceCauchy = sum((I -sqr(deformedN)) & (totalForceCauchy)); //netForceCauchy += sum(totalForceCauchy); } else { // small strain totalForce = Sf & sigmaPatch; totalNormalForce = sum(n & (totalForce)); totalShearForce = sum((I -sqr(n)) & (totalForce)); } //netForce += sum(totalForce); // scalar totalNormalForce = sum(n & (totalForce)); // vector totalShearForce = sum((I -sqr(n)) & (totalForce)); //maxPatchForce = max(maxPatchForce, mag(sum(totalForce))); Info<< "Patch: " << mesh.boundary()[patchID].name() << nl << "\tTotal Force:\t\t" << sum(totalForce) << " N\n" << "\tTotal Normal Force:\t" << totalNormalForce << " N\n" << "\tTotal Shear Force:\t" << totalShearForce << " N\n"; if (nonLinear) { Info<< "\tForces calculated with Cauchy stress\n" << "\tTotal Force:\t\t" << sum(totalForceCauchy) << " N\n" << "\tTotal Normal Force:\t" << totalNormalForceCauchy << " N\n" << "\tTotal Shear Force:\t" << totalShearForceCauchy << " N\n"; } Info<< endl; } // scalar percentNetForce = 100.0*mag(netForce)/maxPatchForce; // scalar percentNetForceCauchy = // 100.0*mag(netForceCauchy)/maxPatchForce; // Info<< nl << "Net force on model is " // << netForce << " N\twhich is " // << percentNetForce << "% of maximum patch force"; Info<< endl; } } Info<< nl << "End" << endl; return 0; } // ************************************************************************* //