This repository has been archived on 2023-11-20. You can view files and clone it, but cannot push or open issues or pull requests.
foam-extend4.1-coherent-io/tutorials/basic/potentialFoam/cylinder/analyticalCylinder/analyticalCylinder.C

70 lines
2.3 KiB
C
Raw Normal View History

/*---------------------------------------------------------------------------*\
========= |
2013-12-11 16:09:41 +00:00
\\ / F ield | foam-extend: Open Source CFD
\\ / O peration | Version: 3.2
\\ / A nd | Web: http://www.foam-extend.org
\\/ M anipulation | For copyright notice see file Copyright
-------------------------------------------------------------------------------
License
2013-12-11 16:09:41 +00:00
This file is part of foam-extend.
2013-12-11 16:09:41 +00:00
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
2013-12-11 16:09:41 +00:00
Free Software Foundation, either version 3 of the License, or (at your
option) any later version.
2013-12-11 16:09:41 +00:00
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
2013-12-11 16:09:41 +00:00
along with foam-extend. 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;
2010-10-01 09:29:30 +00:00
return 0;
}
// ************************************************************************* //