ca89189ecd
executed with foamRun for single region simulations of foamMultiRun for
multi-region simulations. Replaces pimpleFoam, pisoFoam and simpleFoam and all
the corresponding tutorials have been updated and moved to
tutorials/modules/incompressibleFluid.
Class
Foam::solvers::incompressibleFluid
Description
Solver module for steady or transient turbulent flow of incompressible
isothermal fluids with optional mesh motion and change.
Uses the flexible PIMPLE (PISO-SIMPLE) solution for time-resolved and
pseudo-transient and steady simulations.
Optional fvModels and fvConstraints are provided to enhance the simulation
in many ways including adding various sources, constraining or limiting
the solution.
Reference:
\verbatim
Greenshields, C. J., & Weller, H. G. (2022).
Notes on Computational Fluid Dynamics: General Principles.
CFD Direct Ltd.: Reading, UK.
\endverbatim
SourceFiles
incompressibleFluid.C
See also
Foam::solvers::fluidSolver
Foam::solvers::isothermalFluid
105 lines
1.9 KiB
C++
105 lines
1.9 KiB
C++
/*--------------------------------*- C++ -*----------------------------------*\
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========= |
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\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
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\\ / O peration | Website: https://openfoam.org
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\\ / A nd | Version: dev
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\\/ M anipulation |
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\*---------------------------------------------------------------------------*/
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FoamFile
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{
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format ascii;
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class dictionary;
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object blockMeshDict;
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}
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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convertToMeters 0.0032;
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vertices
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(
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(-40 0 -1)
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( 0 0 -1)
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( 30 0 -1)
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(-40 1 -1)
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( 0 1 -1)
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( 30 1 -1)
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(-40 4 -1)
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( 0 4 -1)
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(-40 0 1)
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( 0 0 1)
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( 30 0 1)
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(-40 1 1)
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( 0 1 1)
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( 30 1 1)
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(-40 4 1)
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( 0 4 1)
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);
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blocks
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(
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hex (0 1 4 3 8 9 12 11) (40 12 1) simpleGrading (0.02 0.4 1)
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hex (1 2 5 4 9 10 13 12) (30 12 1) simpleGrading (50 0.4 1)
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hex (3 4 7 6 11 12 15 14) (40 24 1) simpleGrading (0.02 ((0.5 0.5 4.0) (0.5 0.5 0.25)) 1)
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);
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boundary
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(
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inlet
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{
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type patch;
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faces
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(
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(0 3 11 8)
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(3 6 14 11)
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);
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}
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walls
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{
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type wall;
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faces
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(
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(6 7 15 14)
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(7 4 12 15)
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(4 5 13 12)
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);
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}
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outlet
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{
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type patch;
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faces
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(
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(2 5 13 10)
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);
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}
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centreline
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{
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type symmetryPlane;
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faces
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(
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(0 1 9 8)
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(1 2 10 9)
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);
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}
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frontAndBack
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{
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type empty;
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faces
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(
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(0 1 4 3)
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(3 4 7 6)
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(1 2 5 4)
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(8 9 12 11)
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(11 12 15 14)
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(9 10 13 12)
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);
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}
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);
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// ************************************************************************* //
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