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213 lines
5.7 KiB
C
213 lines
5.7 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) 1991-2010 OpenCFD Ltd.
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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 "pressureGradientExplicitSource.H"
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#include "volFields.H"
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#include "IFstream.H"
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// * * * * * * * * * * * * * Private Member Functions * * * * * * * * * * * //
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void Foam::pressureGradientExplicitSource::writeGradP() const
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{
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// Only write on output time
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if (mesh_.time().outputTime())
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{
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IOdictionary propsDict
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(
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IOobject
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(
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sourceName_ + "Properties",
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mesh_.time().timeName(),
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"uniform",
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mesh_,
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IOobject::NO_READ,
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IOobject::NO_WRITE
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)
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);
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propsDict.add("gradient", gradP_);
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propsDict.regIOobject::write();
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}
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}
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// * * * * * * * * * * * * * * * * Constructors * * * * * * * * * * * * * * //
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Foam::pressureGradientExplicitSource::pressureGradientExplicitSource
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(
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const word& sourceName,
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volVectorField& U
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)
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:
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sourceName_(sourceName),
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mesh_(U.mesh()),
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U_(U),
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dict_
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(
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IOobject
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(
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sourceName + "Properties",
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mesh_.time().constant(),
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mesh_,
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IOobject::MUST_READ_IF_MODIFIED,
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IOobject::NO_WRITE
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)
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),
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Ubar_(dict_.lookup("Ubar")),
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gradPini_(dict_.lookup("gradPini")),
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gradP_(gradPini_),
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flowDir_(Ubar_/mag(Ubar_)),
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cellSource_(dict_.lookup("cellSource")),
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cellSelector_
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(
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topoSetSource::New
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(
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cellSource_,
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mesh_,
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dict_.subDict(cellSource_ + "Coeffs")
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)
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),
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selectedCellSet_
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(
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mesh_,
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sourceName_ + "CellSet",
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mesh_.nCells()/10 + 1 // Reasonable size estimate.
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)
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{
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// Create the cell set
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cellSelector_->applyToSet
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(
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topoSetSource::NEW,
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selectedCellSet_
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);
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// Give some feedback
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Info<< " Selected "
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<< returnReduce(selectedCellSet_.size(), sumOp<label>())
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<< " cells" << endl;
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// Read the initial pressure gradient from file if it exists
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IFstream propsFile
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(
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mesh_.time().timeName()/"uniform"/(sourceName_ + "Properties")
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);
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if (propsFile.good())
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{
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Info<< " Reading pressure gradient from file" << endl;
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dictionary propsDict(dictionary::null, propsFile);
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propsDict.lookup("gradient") >> gradP_;
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}
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Info<< " Initial pressure gradient = " << gradP_ << nl << endl;
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}
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// * * * * * * * * * * * * * * * Member Functions * * * * * * * * * * * * * //
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Foam::tmp<Foam::DimensionedField<Foam::vector, Foam::volMesh> >
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Foam::pressureGradientExplicitSource::Su() const
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{
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tmp<DimensionedField<vector, volMesh> > tSource
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(
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new DimensionedField<vector, volMesh>
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(
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IOobject
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(
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sourceName_,
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mesh_.time().timeName(),
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mesh_,
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IOobject::NO_READ,
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IOobject::NO_WRITE
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),
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mesh_,
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dimensionedVector("zero", gradP_.dimensions(), vector::zero)
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)
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);
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DimensionedField<vector, volMesh>& sourceField = tSource();
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forAllConstIter(cellSet, selectedCellSet_, iter)
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{
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label cellI = iter.key();
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sourceField[cellI] = flowDir_*gradP_.value();
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}
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return tSource;
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}
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void Foam::pressureGradientExplicitSource::update()
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{
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const volScalarField& rAU =
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mesh_.lookupObject<volScalarField>("(1|A(" + U_.name() + "))");
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// Integrate flow variables over cell set
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scalar volTot = 0.0;
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scalar magUbarAve = 0.0;
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scalar rAUave = 0.0;
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forAllConstIter(cellSet, selectedCellSet_, iter)
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{
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label cellI = iter.key();
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scalar volCell = mesh_.V()[cellI];
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volTot += volCell;
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magUbarAve += (flowDir_ & U_[cellI])*volCell;
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rAUave += rAU[cellI]*volCell;
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}
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// Collect across all processors
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reduce(volTot, sumOp<scalar>());
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reduce(magUbarAve, sumOp<scalar>());
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reduce(rAUave, sumOp<scalar>());
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// Volume averages
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magUbarAve /= volTot;
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rAUave /= volTot;
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// Calculate the pressure gradient increment needed to adjust the average
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// flow-rate to the desired value
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scalar gradPplus = (mag(Ubar_) - magUbarAve)/rAUave;
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// Apply correction to velocity field
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forAllConstIter(cellSet, selectedCellSet_, iter)
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{
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label cellI = iter.key();
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U_[cellI] += flowDir_*rAU[cellI]*gradPplus;
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}
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// Update pressure gradient
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gradP_.value() += gradPplus;
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Info<< "Uncorrected Ubar = " << magUbarAve << tab
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<< "Pressure gradient = " << gradP_.value() << endl;
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writeGradP();
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}
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// ************************************************************************* //
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