192 lines
5.3 KiB
C
192 lines
5.3 KiB
C
/*---------------------------------------------------------------------------*\
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========= |
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\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
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\\ / O peration |
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\\ / A nd | Copyright (C) 2011-2012 OpenFOAM Foundation
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\\/ M anipulation |
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-------------------------------------------------------------------------------
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License
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This file is part of OpenFOAM.
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OpenFOAM is free software: you can redistribute it and/or modify it
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under the terms of the GNU General Public License as published by
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the Free Software Foundation, either version 3 of the License, or
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(at your option) any later version.
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OpenFOAM is distributed in the hope that it will be useful, but WITHOUT
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ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or
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FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License
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for more details.
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You should have received a copy of the GNU General Public License
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along with OpenFOAM. If not, see <http://www.gnu.org/licenses/>.
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\*---------------------------------------------------------------------------*/
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#include "forceCoeffs.H"
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#include "dictionary.H"
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#include "Time.H"
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#include "Pstream.H"
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#include "IOmanip.H"
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// * * * * * * * * * * * * * * Static Data Members * * * * * * * * * * * * * //
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defineTypeNameAndDebug(Foam::forceCoeffs, 0);
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// * * * * * * * * * * * * * * * * Constructors * * * * * * * * * * * * * * //
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Foam::forceCoeffs::forceCoeffs
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(
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const word& name,
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const objectRegistry& obr,
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const dictionary& dict,
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const bool loadFromFiles
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)
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:
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forces(name, obr, dict, loadFromFiles),
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liftDir_(vector::zero),
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dragDir_(vector::zero),
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pitchAxis_(vector::zero),
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magUInf_(0.0),
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lRef_(0.0),
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Aref_(0.0)
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{
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read(dict);
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}
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// * * * * * * * * * * * * * * * * Destructor * * * * * * * * * * * * * * * //
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Foam::forceCoeffs::~forceCoeffs()
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{}
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// * * * * * * * * * * * * * * * Member Functions * * * * * * * * * * * * * //
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void Foam::forceCoeffs::read(const dictionary& dict)
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{
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if (active_)
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{
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forces::read(dict);
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// Directions for lift and drag forces, and pitch moment
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dict.lookup("liftDir") >> liftDir_;
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dict.lookup("dragDir") >> dragDir_;
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dict.lookup("pitchAxis") >> pitchAxis_;
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// Free stream velocity magnitude
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dict.lookup("magUInf") >> magUInf_;
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// Reference length and area scales
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dict.lookup("lRef") >> lRef_;
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dict.lookup("Aref") >> Aref_;
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}
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}
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void Foam::forceCoeffs::writeFileHeader(const label i)
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{
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file()
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<< "# Time" << tab << "Cm" << tab << "Cd" << tab << "Cl" << tab
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<< "Cl(f)" << "Cl(r)" << endl;
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}
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void Foam::forceCoeffs::execute()
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{
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// Do nothing - only valid on write
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}
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void Foam::forceCoeffs::end()
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{
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// Do nothing - only valid on write
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}
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void Foam::forceCoeffs::write()
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{
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if (active_)
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{
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forces::calcForcesMoment();
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if (Pstream::master())
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{
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functionObjectFile::write();
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scalar pDyn = 0.5*rhoRef_*magUInf_*magUInf_;
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Field<vector> totForce(force_[0] + force_[1]);
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Field<vector> totMoment(moment_[0] + moment_[1]);
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List<Field<scalar> > coeffs(3);
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coeffs[0].setSize(nBin_);
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coeffs[1].setSize(nBin_);
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coeffs[2].setSize(nBin_);
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// lift, drag and moment
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coeffs[0] = (totForce & liftDir_)/(Aref_*pDyn);
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coeffs[1] = (totForce & dragDir_)/(Aref_*pDyn);
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coeffs[2] = (totMoment & pitchAxis_)/(Aref_*lRef_*pDyn);
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scalar Cl = sum(coeffs[0]);
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scalar Cd = sum(coeffs[1]);
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scalar Cm = sum(coeffs[2]);
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scalar Clf = Cl/2.0 - Cm;
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scalar Clr = Cl/2.0 + Cm;
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file()
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<< obr_.time().value() << tab
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<< Cm << tab << Cd << tab << Cl << tab << Clf << tab << Clr
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<< endl;
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if (log_)
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{
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Info<< type() << " output:" << nl
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<< " Cm = " << Cm << nl
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<< " Cd = " << Cd << nl
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<< " Cl = " << Cl << nl
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<< " Cl(f) = " << Clf << nl
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<< " Cl(r) = " << Clr << endl;
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}
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if (nBin_ > 1)
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{
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autoPtr<writer<scalar> >
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binWriterPtr(writer<scalar>::New(binFormat_));
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wordList fieldNames(IStringStream("(lift drag moment)")());
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coordSet axis
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(
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"forceCoeffs",
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"distance",
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binPoints_,
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mag(binPoints_)
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);
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fileName forcesDir =
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baseFileDir()/name_/obr_.time().timeName();
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mkDir(forcesDir);
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if (log_)
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{
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Info<< " Writing bins to " << forcesDir << endl;
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}
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OFstream osCoeffs(forcesDir/"forceCoeffs_bins");
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binWriterPtr->write(axis, fieldNames, coeffs, osCoeffs);
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}
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if (log_)
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{
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Info<< endl;
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}
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}
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}
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}
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// ************************************************************************* //
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