STYLE: remove trailing space, tabs
This commit is contained in:
Mark Olesen
parent
7bef18a274
commit
2b1061420c
@ -113,7 +113,7 @@ void Foam::checkPatch
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labelList() // null value
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);
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label labelTyp = TopoType::MANIFOLD;
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forAll(meshEdges, edgei)
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{
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@ -57,7 +57,7 @@ Description
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-combineZones '((zoneA "zoneB.*")(none otherZone))
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This can be combined with e.g. 'cellZones' or 'cellZonesOnly'. The
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addZones option supplies the destination region name as first element in
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the list. The combineZones option synthesises the region name e.g.
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the list. The combineZones option synthesises the region name e.g.
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zoneA_zoneB0_zoneB1
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- cellZonesOnly does not do a walk and uses the cellZones only. Use
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@ -1830,7 +1830,7 @@ int main(int argc, char *argv[])
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{
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label ownCluster = clusterID[mesh.faceOwner()[facei]];
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label neiCluster = clusterID[mesh.faceNeighbour()[facei]];
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if (ownCluster != neiCluster)
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{
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blockedFace[facei] = true;
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@ -39,27 +39,28 @@ Description
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and the distance between face centres.
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The input from viewFactorsDict are:
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\verbatim
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GaussQuadTol 0.1; // GaussQuad error
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distTol 8; // R/Average(rm)
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alpha 0.22; // Use for common edges for 2LI
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\endverbatim
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For debugging purposes, the following entries can be set in viewFactorsDict:
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\verbatim
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writeViewFactorMatrix true;
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writeFacesAgglomeration false;
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dumpRays false;
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dumpRays false;
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writeViewFactorMatrix writes the sum of the VF on each face.
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writeFacesAgglomeration writes the agglomeration
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dumpRays dumps rays
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\endverbatim
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The participating patches in the VF calculation have to be in the
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'viewFactorWall' patch group (in the polyMesh/boundary file), e.g.
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\verbatim
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floor
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{
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type wall;
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@ -67,6 +68,7 @@ Description
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nFaces 100;
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startFace 3100;
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}
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\endverbatim
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Compile with -DNO_CGAL only if no CGAL present - CGAL AABB tree performs
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better than the built-in octree.
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@ -216,7 +216,7 @@ void Foam::dynamicRefineFvMesh::mapFields(const mapPolyMesh& mpm)
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const label oldCelli = cellMap[celli];
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if (oldCelli >= 0 && reverseCellMap[oldCelli] >= 0)
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{
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// Found master cell.
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// Found master cell.
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nSubCells[oldCelli]++;
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}
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}
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@ -36,7 +36,7 @@ Description
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The computation of the sensitivity derivatives follows the (E-)SI
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formulation of
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Kavvadias, I. S., Papoutsis-Kiachagias, E. M.,
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Kavvadias, I. S., Papoutsis-Kiachagias, E. M.,
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Giannakoglou, K. C. (2015).
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On the proper treatment of grid sensitivities in continuous adjoint
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methods for shape optimization.
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@ -45,7 +45,7 @@ Description
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whereas their smoothing based on the computation of the 'Sobolev
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gradient' is derived from
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Vassberg J. C., Jameson A. (2006).
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Aerodynamic Shape Optimization Part I: Theoretical Background.
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VKI Lecture Series, Introduction to Optimization and
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@ -119,7 +119,7 @@ protected:
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//- Write geometric info for use by external programs
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bool writeGeometricInfo_;
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//- Smooth sensitivity derivatives based on the computation of the
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//- Smooth sensitivity derivatives based on the computation of the
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//- 'Sobolev gradient'
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bool smoothSensitivities_;
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@ -142,7 +142,7 @@ protected:
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//- Set suffix name for sensitivity fields
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void setSuffixName();
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//- Smooth sensitivity derivatives based on the computation of the
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//- Smooth sensitivity derivatives based on the computation of the
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//- 'Sobolev gradient'
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void smoothSensitivities();
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@ -185,7 +185,7 @@ Foam::meltingEvaporationModels::diffusionGasEvaporation<Thermo, OtherThermo>
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)
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);
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const volScalarField Ygm(max(from*YvSat + to*Yv, Zero));
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const volScalarField Ygm(max(from*YvSat + to*Yv, Zero));
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const multiphaseInterSystem& fluid = this->fluid();
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@ -54,7 +54,7 @@ Description
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Extension to porous media flows:
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\verbatim
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Missios, K., Jacobsen, N. G., Moeller, K., & Roenby, J.
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Using the isoAdvector Geometric VOF Method for Interfacial Flows
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Using the isoAdvector Geometric VOF Method for Interfacial Flows
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Through Porous Media. MARINE 2021.
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\endverbatim
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@ -20,7 +20,7 @@ runParallel $(getApplication)
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foamDictionary -entry solvers.p.processorAgglomerator -set 'masterCoarsest' system/fvSolution
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runParallel -s masterCoarsest $(getApplication)
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#- Run with processorAgglomerator - multiple masters
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#- Run with processorAgglomerator - multiple masters
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foamDictionary -entry solvers.p.nMasters -set '2' system/fvSolution
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runParallel -s masterCoarsest2 $(getApplication)
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@ -35,7 +35,7 @@ solvers
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tolerance 1e-9;
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relTol 0.01;
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};
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"U|Ua|nuTilda|nuaTilda|yWall|da|k|ka|omega|wa"
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"U|Ua|nuTilda|nuaTilda|yWall|da|k|ka|omega|wa"
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{
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solver PBiCGStab;
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preconditioner DILU;
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@ -20,7 +20,7 @@ internalField uniform (0 0 0);
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boundaryField
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{
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innerWall
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innerWall
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{
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type noSlip;
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}
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@ -20,7 +20,7 @@ internalField uniform 0;
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boundaryField
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{
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"innerWall|outerWall"
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"innerWall|outerWall"
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{
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type zeroGradient;
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}
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@ -25,7 +25,7 @@ geom
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ntheta 40;
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g 10;
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mr0 #eval{ - $r0 };
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mr1 #eval{ - $r1 };
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invG #eval{ 1./$g };
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@ -1,57 +1,57 @@
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/*--------------------------------*- C++ -*----------------------------------*\
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| ========= | |
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| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
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| \\ / O peration | Version: v2212 |
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| \\ / A nd | Website: www.openfoam.com |
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| \\/ M anipulation | |
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\*---------------------------------------------------------------------------*/
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FoamFile
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{
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version 2.0;
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format ascii;
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class volScalarField;
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object epsilon;
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}
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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dimensions [0 2 -3 0 0 0 0];
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internalField uniform 6.9e-5;
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boundaryField
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{
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#includeEtc "caseDicts/setConstraintTypes"
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inlet
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{
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type fixedValue;
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value $internalField;
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}
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"(atmosphere|outlet)"
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{
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type inletOutlet;
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inletValue $internalField;
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value $internalField;
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}
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"(HULL*.*)"
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{
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type epsilonWallFunction;
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value $internalField;
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}
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"(BLADES|HUB_DISK|HUB)"
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{
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type epsilonWallFunction;
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value $internalField;
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}
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"(overset-1|oversetPatch)"
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{
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type overset;
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}
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}
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// ************************************************************************* //
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/*--------------------------------*- C++ -*----------------------------------*\
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| ========= | |
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| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
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| \\ / O peration | Version: v2212 |
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| \\ / A nd | Website: www.openfoam.com |
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| \\/ M anipulation | |
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\*---------------------------------------------------------------------------*/
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FoamFile
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{
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version 2.0;
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format ascii;
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class volScalarField;
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object epsilon;
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}
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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dimensions [0 2 -3 0 0 0 0];
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internalField uniform 6.9e-5;
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boundaryField
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{
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#includeEtc "caseDicts/setConstraintTypes"
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inlet
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{
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type fixedValue;
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value $internalField;
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}
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"(atmosphere|outlet)"
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{
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type inletOutlet;
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inletValue $internalField;
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value $internalField;
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}
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"(HULL*.*)"
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{
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type epsilonWallFunction;
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value $internalField;
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}
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"(BLADES|HUB_DISK|HUB)"
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{
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type epsilonWallFunction;
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value $internalField;
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}
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"(overset-1|oversetPatch)"
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{
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type overset;
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}
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}
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// ************************************************************************* //
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@ -31,7 +31,7 @@ boundaryField
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{
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type overset;
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value uniform 0;
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fluxCorrection false;
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fluxCorrection false;
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}
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top
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@ -47,7 +47,7 @@ runTimeModifiable true;
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adjustTimeStep yes;
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maxCo 1.0;
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maxAlphaCo 2.0;
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maxAlphaCo 2.0;
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functions
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{
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