openfoam/tutorials/basic/potentialFoam/cylinder/analyticalCylinder/analyticalCylinder.C
2010-07-27 15:45:43 +01:00

70 lines
2.2 KiB
C

/*---------------------------------------------------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | Copyright (C) 1991-2010 OpenCFD Ltd.
\\/ 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
analyticalCylinder
Description
Generates an analytical solution for potential flow around a cylinder.
Can be compared with the solution from the potentialFlow/cylinder example.
\*---------------------------------------------------------------------------*/
#include "fvCFD.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
int main(int argc, char *argv[])
{
# include "setRootCase.H"
# include "createTime.H"
# include "createMesh.H"
# include "createFields.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Info<< "\nEvaluating analytical solution" << endl;
volVectorField centres = UA.mesh().C();
volScalarField magCentres = mag(centres);
volScalarField theta = acos((centres & vector(1,0,0))/magCentres);
volVectorField cs2theta =
cos(2*theta)*vector(1,0,0)
+ sin(2*theta)*vector(0,1,0);
UA = uInfX*(dimensionedVector(vector(1,0,0))
- pow((radius/magCentres),2)*cs2theta);
runTime.write();
Info<< "end" << endl;
return 0;
}
// ************************************************************************* //