Modular solvers: Reorganised directory structure of applications and tutorials

The new flexible and extensible modular solvers structure already provides most
of the simulation functionality needed for single phase, multiphase,
multicomponent etc. fluid flow problems as well as a very effective method of
combining these with solid heat transfer, solid stress, surface film to solve
complex multi-region, multi-physics problems and are now the primary mechanism
for the further development of OpenFOAM simulation capability in future.  To
emphasis this for both users and developers the applications/solvers directory
has been separated into applications/modules containing all the solver modules:

├── modules
│   ├── compressibleMultiphaseVoF
│   ├── compressibleVoF
│   ├── film
│   ├── fluid
│   ├── fluidSolver
│   ├── functions
│   ├── incompressibleDenseParticleFluid
│   ├── incompressibleDriftFlux
│   ├── incompressibleFluid
│   ├── incompressibleMultiphaseVoF
│   ├── incompressibleVoF
│   ├── isothermalFilm
│   ├── isothermalFluid
│   ├── movingMesh
│   ├── multicomponentFluid
│   ├── multiphaseEuler
│   ├── multiphaseVoFSolver
│   ├── shockFluid
│   ├── solid
│   ├── solidDisplacement
│   ├── twoPhaseSolver
│   ├── twoPhaseVoFSolver
│   ├── VoFSolver
│   └── XiFluid

applications/solvers containing the foamRun and foamMultiRun solver applications
which instantiate and execute the chosen solver modules and also standalone
solver applications for special initialisation and test activities:

├── solvers
│   ├── boundaryFoam
│   ├── chemFoam
│   ├── foamMultiRun
│   ├── foamRun
│   └── potentialFoam

and applications/legacy containing legacy solver applications which are not
currently being actively developed but the functionality of which will be merged
into the solver modules or form the basis of new solver modules as the need
arises:

├── legacy
│   ├── basic
│   │   ├── financialFoam
│   │   └── laplacianFoam
│   ├── combustion
│   │   └── PDRFoam
│   ├── compressible
│   │   └── rhoPorousSimpleFoam
│   ├── electromagnetics
│   │   ├── electrostaticFoam
│   │   ├── magneticFoam
│   │   └── mhdFoam
│   ├── incompressible
│   │   ├── adjointShapeOptimisationFoam
│   │   ├── dnsFoam
│   │   ├── icoFoam
│   │   ├── porousSimpleFoam
│   │   └── shallowWaterFoam
│   └── lagrangian
│       ├── dsmcFoam
│       ├── mdEquilibrationFoam
│       └── mdFoam

Correspondingly the tutorials directory structure has been reorganised with the
modular solver directories at the top level with names that make it easier for
users to find example cases relating to their particular requirements and a
legacy sub-directory containing cases corresponding to the legacy solver
applications listed above:

├── compressibleMultiphaseVoF
│   └── damBreak4phaseLaminar
├── compressibleVoF
│   ├── ballValve
│   ├── climbingRod
│   ├── damBreak
│   ├── depthCharge2D
│   ├── depthCharge3D
│   ├── sloshingTank2D
│   └── throttle
├── film
│   └── rivuletPanel
├── fluid
│   ├── aerofoilNACA0012
│   ├── aerofoilNACA0012Steady
│   ├── angledDuct
│   ├── angledDuctExplicitFixedCoeff
│   ├── angledDuctLTS
│   ├── annularThermalMixer
│   ├── BernardCells
│   ├── blockedChannel
│   ├── buoyantCavity
│   ├── cavity
│   ├── decompressionTank
│   ├── externalCoupledCavity
│   ├── forwardStep
│   ├── helmholtzResonance
│   ├── hotRadiationRoom
│   ├── hotRadiationRoomFvDOM
│   ├── hotRoom
│   ├── hotRoomBoussinesq
│   ├── hotRoomBoussinesqSteady
│   ├── hotRoomComfort
│   ├── iglooWithFridges
│   ├── mixerVessel2DMRF
│   ├── nacaAirfoil
│   ├── pitzDaily
│   ├── prism
│   ├── shockTube
│   ├── squareBend
│   ├── squareBendLiq
│   └── squareBendLiqSteady
├── incompressibleDenseParticleFluid
│   ├── column
│   ├── cyclone
│   ├── Goldschmidt
│   ├── GoldschmidtMPPIC
│   └── injectionChannel
├── incompressibleDriftFlux
│   ├── dahl
│   ├── mixerVessel2DMRF
│   └── tank3D
├── incompressibleFluid
│   ├── airFoil2D
│   ├── ballValve
│   ├── blockedChannel
│   ├── cavity
│   ├── cavityCoupledU
│   ├── channel395
│   ├── drivaerFastback
│   ├── ductSecondaryFlow
│   ├── elipsekkLOmega
│   ├── flowWithOpenBoundary
│   ├── hopperParticles
│   ├── impeller
│   ├── mixerSRF
│   ├── mixerVessel2D
│   ├── mixerVessel2DMRF
│   ├── mixerVesselHorizontal2DParticles
│   ├── motorBike
│   ├── motorBikeSteady
│   ├── movingCone
│   ├── offsetCylinder
│   ├── oscillatingInlet
│   ├── pipeCyclic
│   ├── pitzDaily
│   ├── pitzDailyLES
│   ├── pitzDailyLESDevelopedInlet
│   ├── pitzDailyLTS
│   ├── pitzDailyPulse
│   ├── pitzDailyScalarTransport
│   ├── pitzDailySteady
│   ├── pitzDailySteadyExperimentalInlet
│   ├── pitzDailySteadyMappedToPart
│   ├── pitzDailySteadyMappedToRefined
│   ├── planarContraction
│   ├── planarCouette
│   ├── planarPoiseuille
│   ├── porousBlockage
│   ├── propeller
│   ├── roomResidenceTime
│   ├── rotor2DRotating
│   ├── rotor2DSRF
│   ├── rotorDisk
│   ├── T3A
│   ├── TJunction
│   ├── TJunctionFan
│   ├── turbineSiting
│   ├── waveSubSurface
│   ├── windAroundBuildings
│   └── wingMotion
├── incompressibleMultiphaseVoF
│   ├── damBreak4phase
│   ├── damBreak4phaseFineLaminar
│   ├── damBreak4phaseLaminar
│   └── mixerVessel2DMRF
├── incompressibleVoF
│   ├── angledDuct
│   ├── capillaryRise
│   ├── cavitatingBullet
│   ├── climbingRod
│   ├── containerDischarge2D
│   ├── damBreak
│   ├── damBreakLaminar
│   ├── damBreakPorousBaffle
│   ├── damBreakWithObstacle
│   ├── DTCHull
│   ├── DTCHullMoving
│   ├── DTCHullWave
│   ├── floatingObject
│   ├── floatingObjectWaves
│   ├── forcedUpstreamWave
│   ├── mixerVessel
│   ├── mixerVessel2DMRF
│   ├── mixerVesselHorizontal2D
│   ├── nozzleFlow2D
│   ├── planingHullW3
│   ├── propeller
│   ├── sloshingCylinder
│   ├── sloshingTank2D
│   ├── sloshingTank2D3DoF
│   ├── sloshingTank3D
│   ├── sloshingTank3D3DoF
│   ├── sloshingTank3D6DoF
│   ├── testTubeMixer
│   ├── waterChannel
│   ├── wave
│   ├── wave3D
│   └── weirOverflow
├── isothermalFilm
│   └── rivuletPanel
├── isothermalFluid
│   ├── potentialFreeSurfaceMovingOscillatingBox
│   └── potentialFreeSurfaceOscillatingBox
├── legacy
│   ├── basic
│   │   ├── financialFoam
│   │   │   └── europeanCall
│   │   └── laplacianFoam
│   │       └── flange
│   ├── combustion
│   │   └── PDRFoam
│   │       └── flamePropagationWithObstacles
│   ├── compressible
│   │   └── rhoPorousSimpleFoam
│   │       ├── angledDuctExplicit
│   │       └── angledDuctImplicit
│   ├── electromagnetics
│   │   ├── electrostaticFoam
│   │   │   └── chargedWire
│   │   └── mhdFoam
│   │       └── hartmann
│   ├── incompressible
│   │   ├── adjointShapeOptimisationFoam
│   │   │   └── pitzDaily
│   │   ├── dnsFoam
│   │   │   └── boxTurb16
│   │   ├── icoFoam
│   │   │   ├── cavity
│   │   │   └── elbow
│   │   ├── porousSimpleFoam
│   │   │   ├── angledDuctExplicit
│   │   │   └── angledDuctImplicit
│   │   └── shallowWaterFoam
│   │       └── squareBump
│   ├── lagrangian
│   │   ├── dsmcFoam
│   │   │   ├── freeSpacePeriodic
│   │   │   ├── freeSpaceStream
│   │   │   ├── supersonicCorner
│   │   │   └── wedge15Ma5
│   │   ├── mdEquilibrationFoam
│   │   │   ├── periodicCubeArgon
│   │   │   └── periodicCubeWater
│   │   └── mdFoam
│   │       └── nanoNozzle
├── mesh
│   ├── blockMesh
│   │   ├── pipe
│   │   ├── sphere
│   │   ├── sphere7
│   │   └── sphere7ProjectedEdges
│   ├── refineMesh
│   │   └── refineFieldDirs
│   └── snappyHexMesh
│       ├── flange
│       └── pipe
├── movingMesh
│   └── SnakeRiverCanyon
├── multicomponentFluid
│   ├── aachenBomb
│   ├── counterFlowFlame2D
│   ├── counterFlowFlame2D_GRI
│   ├── counterFlowFlame2D_GRI_TDAC
│   ├── counterFlowFlame2DLTS
│   ├── counterFlowFlame2DLTS_GRI_TDAC
│   ├── DLR_A_LTS
│   ├── filter
│   ├── lockExchange
│   ├── membrane
│   ├── nc7h16
│   ├── parcelInBox
│   ├── SandiaD_LTS
│   ├── simplifiedSiwek
│   ├── smallPoolFire2D
│   ├── smallPoolFire3D
│   ├── verticalChannel
│   ├── verticalChannelLTS
│   └── verticalChannelSteady
├── multiphaseEuler
│   ├── bed
│   ├── bubbleColumn
│   ├── bubbleColumnEvaporating
│   ├── bubbleColumnEvaporatingDissolving
│   ├── bubbleColumnEvaporatingReacting
│   ├── bubbleColumnIATE
│   ├── bubbleColumnLaminar
│   ├── bubbleColumnLES
│   ├── bubblePipe
│   ├── damBreak4phase
│   ├── fluidisedBed
│   ├── fluidisedBedLaminar
│   ├── Grossetete
│   ├── hydrofoil
│   ├── injection
│   ├── LBend
│   ├── mixerVessel2D
│   ├── mixerVessel2DMRF
│   ├── pipeBend
│   ├── steamInjection
│   ├── titaniaSynthesis
│   ├── titaniaSynthesisSurface
│   ├── wallBoilingIATE
│   ├── wallBoilingPolydisperse
│   └── wallBoilingPolydisperseTwoGroups
├── multiRegion
│   ├── CHT
│   │   ├── circuitBoardCooling
│   │   ├── coolingCylinder2D
│   │   ├── coolingSphere
│   │   ├── heatedDuct
│   │   ├── heatExchanger
│   │   ├── multiphaseCoolingCylinder2D
│   │   ├── reverseBurner
│   │   ├── shellAndTubeHeatExchanger
│   │   ├── VoFcoolingCylinder2D
│   │   └── wallBoiling
│   └── film
│       ├── cylinder
│       ├── cylinderDripping
│       ├── cylinderVoF
│       ├── hotBoxes
│       ├── rivuletBox
│       ├── rivuletPanel
│       ├── splashPanel
│       └── VoFToFilm
├── potentialFoam
│   ├── cylinder
│   └── pitzDaily
├── resources
│   ├── blockMesh
│   ├── geometry
│   └── thermoData
├── shockFluid
│   ├── biconic25-55Run35
│   ├── forwardStep
│   ├── LadenburgJet60psi
│   ├── movingCone
│   ├── obliqueShock
│   ├── shockTube
│   └── wedge15Ma5
├── solidDisplacement
│   ├── beamEndLoad
│   └── plateHole
└── XiFluid
    ├── kivaTest
    └── moriyoshiHomogeneous
This commit is contained in:
Henry Weller
2023-05-25 18:14:41 +01:00
parent 20c181c5c0
commit e744fdb5f1
6180 changed files with 490 additions and 763 deletions

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/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
object T;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 1 0 0 0];
internalField uniform 300;
boundaryField
{
floor
{
type fixedValue;
value uniform 301;
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ceiling
{
type fixedValue;
value uniform 300;
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sideWalls
{
type zeroGradient;
}
#includeEtc "caseDicts/setConstraintTypes"
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
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object U;
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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wall
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type noSlip;
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#includeEtc "caseDicts/setConstraintTypes"
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -1 0 0 0 0];
internalField uniform 0;
boundaryField
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wall
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type compressible::alphatJayatillekeWallFunction;
Prt 0.85;
value $internalField;
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#includeEtc "caseDicts/setConstraintTypes"
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
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value $internalField;
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#includeEtc "caseDicts/setConstraintTypes"
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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#includeEtc "caseDicts/setConstraintTypes"
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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value $internalField;
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#includeEtc "caseDicts/setConstraintTypes"
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// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
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object p;
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -2 0 0 0 0];
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wall
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type calculated;
value $internalField;
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#includeEtc "caseDicts/setConstraintTypes"
}
// ************************************************************************* //

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@ -0,0 +1,31 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
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format ascii;
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -2 0 0 0 0];
internalField uniform 0;
boundaryField
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wall
{
type fixedFluxPressure;
value $internalField;
}
#includeEtc "caseDicts/setConstraintTypes"
}
// ************************************************************************* //

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@ -0,0 +1,21 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -2 0 0 0 0];
value (0 -9.81 0);
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
simulationType laminar;
RAS
{
model kEpsilon;
turbulence on;
printCoeffs on;
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// ************************************************************************* //

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@ -0,0 +1,53 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
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format ascii;
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location "constant";
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
thermoType
{
type heRhoThermo;
mixture pureMixture;
transport const;
thermo eConst;
equationOfState Boussinesq;
specie specie;
energy sensibleInternalEnergy;
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mixture
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specie
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transport
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mu 1e-03;
Pr 1;
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}
// ************************************************************************* //

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@ -0,0 +1,77 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
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object blockMeshDict;
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
convertToMeters 1;
vertices
(
(0 0 -1)
(9 0 -1)
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blocks
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hex (0 1 2 3 4 5 6 7) (90 10 1) simpleGrading (1 1 1)
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boundary
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faces
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faces
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faces
(
(0 3 2 1)
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);
// ************************************************************************* //

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@ -0,0 +1,55 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
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location "system";
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application foamRun;
solver fluid;
startFrom latestTime;
startTime 0;
stopAt endTime;
endTime 1000;
deltaT 1;
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functions
{
#includeFunc residuals(p_rgh)
#includeFunc streamlinesLine(name=streamlines, start=(0 0.5 0), end=(9 0.5 0), nPoints=24, U)
}
// ************************************************************************* //

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@ -0,0 +1,60 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
location "system";
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default Euler;
}
gradSchemes
{
default Gauss linear;
}
divSchemes
{
default none;
div(phi,U) Gauss linearUpwind grad(U);
div(phi,e) Gauss limitedLinear 1;
turbulence Gauss limitedLinear 1;
div(phi,k) $turbulence;
div(phi,epsilon) $turbulence;
div(phi,(p|rho)) Gauss limitedLinear 1;
div(phi,K) Gauss linear;
div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;
}
laplacianSchemes
{
default Gauss linear corrected;
}
interpolationSchemes
{
default linear;
}
snGradSchemes
{
default corrected;
}
// ************************************************************************* //

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@ -0,0 +1,73 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
location "system";
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
"rho.*"
{
solver diagonal;
}
p_rgh
{
solver GAMG;
smoother DIC;
tolerance 1e-8;
relTol 0.01;
}
p_rghFinal
{
$p_rgh;
relTol 0;
}
"(U|e|k|epsilon)"
{
solver PBiCGStab;
preconditioner DILU;
tolerance 1e-8;
relTol 0.01;
}
"(U|e|k|epsilon)Final"
{
$U;
relTol 0;
}
}
PIMPLE
{
momentumPredictor no;
nNonOrthogonalCorrectors 0;
nCorrectors 2;
pRefCell 0;
pRefValue 0;
}
relaxationFactors
{
equations
{
".*" 1.0;
}
}
// ************************************************************************* //

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@ -0,0 +1,39 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
object T;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Tinlet 298;
dimensions [0 0 0 1 0 0 0];
internalField uniform $Tinlet;
boundaryField
{
freestream
{
type inletOutlet;
inletValue uniform $Tinlet;
value $inletValue;
}
wall
{
type zeroGradient;
}
#includeEtc "caseDicts/setConstraintTypes"
}
// ************************************************************************* //

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@ -0,0 +1,38 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volVectorField;
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Uinlet (200 0 0);
dimensions [0 1 -1 0 0 0 0];
internalField uniform $Uinlet;
boundaryField
{
freestream
{
type freestreamVelocity;
freestreamValue uniform $Uinlet;
}
wall
{
type noSlip;
}
#includeEtc "caseDicts/setConstraintTypes"
}
// ************************************************************************* //

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@ -0,0 +1,37 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
object alphat;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
freestream
{
type calculated;
value uniform 0;
}
wall
{
type compressible::alphatWallFunction;
value uniform 0;
}
#includeEtc "caseDicts/setConstraintTypes"
}
// ************************************************************************* //

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@ -0,0 +1,40 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
object k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
kInlet 0.01;
dimensions [0 2 -2 0 0 0 0];
internalField uniform $kInlet;
boundaryField
{
freestream
{
type inletOutlet;
inletValue uniform $kInlet;
value uniform $kInlet;
}
wall
{
type kqRWallFunction;
value uniform $kInlet;
}
#includeEtc "caseDicts/setConstraintTypes"
}
// ************************************************************************* //

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@ -0,0 +1,38 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
object mut;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
freestream
{
type calculated;
value uniform 0;
}
wall
{
type nutkWallFunction;
type nutkWallFunction;
value uniform 0;
}
#includeEtc "caseDicts/setConstraintTypes"
}
// ************************************************************************* //

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@ -0,0 +1,40 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
object omega;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
omegaInlet 10;
dimensions [0 0 -1 0 0 0 0];
internalField uniform $omegaInlet;
boundaryField
{
freestream
{
type inletOutlet;
inletValue uniform $omegaInlet;
value uniform $omegaInlet;
}
wall
{
type omegaWallFunction;
value uniform $omegaInlet;
}
#includeEtc "caseDicts/setConstraintTypes"
}
// ************************************************************************* //

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@ -0,0 +1,48 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
object p;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
pOut 1e5;
dimensions [1 -1 -2 0 0 0 0];
internalField uniform $pOut;
boundaryField
{
outlet
{
type waveTransmissive;
field p;
gamma 1.4;
fieldInf $pOut;
lInf 5;
value uniform $pOut;
}
freestream
{
type freestreamPressure;
freestreamValue uniform $pOut;
}
wall
{
type zeroGradient;
}
#includeEtc "caseDicts/setConstraintTypes"
}
// ************************************************************************* //

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@ -0,0 +1,14 @@
#!/bin/sh
cd ${0%/*} || exit 1 # Run from this directory
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
# Remove surface
rm -f constant/geometry/NACA0012.obj.gz
cleanCase
rm -f constant/geometry/boundaryLayer.obj
#------------------------------------------------------------------------------

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@ -0,0 +1,18 @@
#!/bin/sh
cd ${0%/*} || exit 1 # Run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
# Copy aerofoil surface from resources directory
cp $FOAM_TUTORIALS/resources/geometry/NACA0012.obj.gz constant/geometry/
application="$(getApplication)"
runApplication blockMesh
runApplication transformPoints "scale=(1 0 1)"
runApplication extrudeMesh
runApplication $application
#------------------------------------------------------------------------------

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@ -0,0 +1,4 @@
Folder to house tri-surfaces
The Allrun script copies the surface from the $FOAM_TUTORIALS/resources/geometry
folder

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@ -0,0 +1,25 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
object momentumTransport;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
simulationType RAS;
RAS
{
model kOmegaSST;
turbulence on;
printCoeffs on;
}
// ************************************************************************* //

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@ -0,0 +1,46 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
location "constant";
object physicalProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
thermoType
{
type hePsiThermo;
mixture pureMixture;
transport const;
thermo hConst;
equationOfState perfectGas;
specie specie;
energy sensibleInternalEnergy;
}
mixture // air at room temperature (293 K)
{
specie
{
molWeight 28.9;
}
thermodynamics
{
Cp 1005;
Hf 0;
}
transport
{
mu 1.82e-05;
Pr 0.71;
}
}
// ************************************************************************* //

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@ -0,0 +1,224 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
object blockMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
domain
{
xMin -4;
xMax 4;
zMin -2;
zMax 2;
// Number of cells
zCells 80; // aerofoil to far field
xUCells 30; // upstream
xMCells 30; // middle
xDCells 40; // downstream
// Mesh grading
zGrading 40; // aerofoil to far field
xUGrading 5; // towards centre upstream
leadGrading 0.2; // towards leading edge
xDGrading 10; // downstream
}
aerofoil
{
xLead 0;
zLead 0;
xTrail 1;
zTrail 0;
xUpper 0.3;
zUpper 0.06;
xLower 0.3;
zLower -0.06;
}
geometry
{
aerofoil
{
type triSurfaceMesh;
file "NACA0012.obj";
}
cylinder
{
type searchableCylinder;
point1 ($!aerofoil/xUpper -1e3 0);
point2 ($!aerofoil/xUpper 1e3 0);
radius $!domain/zMax;
}
}
vertices
(
project ($aerofoil/xLower -0.1 $domain/zMin) (cylinder)
($aerofoil/xTrail -0.1 $domain/zMin)
($domain/xMax -0.1 $domain/zMin)
project ($domain/xMin -0.1 $aerofoil/zLead) (cylinder)
project ($aerofoil/xLead -0.1 $aerofoil/zLead) (aerofoil)
project ($aerofoil/xTrail -0.1 $aerofoil/zTrail) (aerofoil)
($domain/xMax -0.1 $aerofoil/zTrail)
project ($aerofoil/xLower -0.1 $aerofoil/zLower) (aerofoil)
project ($aerofoil/xUpper -0.1 $aerofoil/zUpper) (aerofoil)
project ($aerofoil/xUpper -0.1 $domain/zMax) (aerofoil)
project ($aerofoil/xTrail -0.1 $domain/zMax) (aerofoil)
($domain/xMax -0.1 $domain/zMax)
project ($aerofoil/xLower 0.1 $domain/zMin) (cylinder)
($aerofoil/xTrail 0.1 $domain/zMin)
($domain/xMax 0.1 $domain/zMin)
project ($domain/xMin 0.1 $aerofoil/zLead) (cylinder)
project ($aerofoil/xLead 0.1 $aerofoil/zLead) (aerofoil)
project ($aerofoil/xTrail 0.1 $aerofoil/zTrail) (aerofoil)
($domain/xMax 0.1 $aerofoil/zTrail)
project ($aerofoil/xLower 0.1 $aerofoil/zLower) (aerofoil)
project ($aerofoil/xUpper 0.1 $aerofoil/zUpper) (aerofoil)
project ($aerofoil/xUpper 0.1 $domain/zMax) (aerofoil)
project ($aerofoil/xTrail 0.1 $domain/zMax) (aerofoil)
($domain/xMax 0.1 $domain/zMax)
);
blocks
(
hex ( 7 4 16 19 0 3 15 12)
($!domain/xUCells 1 $!domain/zCells)
edgeGrading
(
$!domain/leadGrading $!domain/leadGrading $!domain/xUGrading $!domain/xUGrading
1 1 1 1
$!domain/zGrading $!domain/zGrading $!domain/zGrading $!domain/zGrading
)
hex ( 5 7 19 17 1 0 12 13)
($!domain/xMCells 1 $!domain/zCells)
simpleGrading (1 1 $!domain/zGrading)
hex ( 17 18 6 5 13 14 2 1)
($!domain/xDCells 1 $!domain/zCells)
simpleGrading ($!domain/xDGrading 1 $!domain/zGrading)
hex ( 20 16 4 8 21 15 3 9)
($!domain/xUCells 1 $!domain/zCells)
edgeGrading
(
$!domain/leadGrading $!domain/leadGrading $!domain/xUGrading $!domain/xUGrading
1 1 1 1
$!domain/zGrading $!domain/zGrading $!domain/zGrading $!domain/zGrading
)
hex ( 17 20 8 5 22 21 9 10)
($!domain/xMCells 1 $!domain/zCells)
simpleGrading (1 1 $!domain/zGrading)
hex ( 5 6 18 17 10 11 23 22)
($!domain/xDCells 1 $!domain/zCells)
simpleGrading ($!domain/xDGrading 1 $!domain/zGrading)
);
edges
(
project 4 7 (aerofoil)
project 7 5 (aerofoil)
project 4 8 (aerofoil)
project 8 5 (aerofoil)
project 16 19 (aerofoil)
project 19 17 (aerofoil)
project 16 20 (aerofoil)
project 20 17 (aerofoil)
project 3 0 (cylinder)
project 3 9 (cylinder)
project 15 12 (cylinder)
project 15 21 (cylinder)
);
boundary
(
aerofoil
{
type wall;
faces
(
(4 7 19 16)
(7 5 17 19)
(5 8 20 17)
(8 4 16 20)
);
}
inlet
{
type patch;
inGroups (freestream);
faces
(
(3 0 12 15)
(0 1 13 12)
(1 2 14 13)
(11 10 22 23)
(10 9 21 22)
(9 3 15 21)
);
}
outlet
{
type patch;
inGroups (freestream);
faces
(
(2 6 18 14)
(6 11 23 18)
);
}
back
{
type empty;
faces
(
(3 4 7 0)
(7 5 1 0)
(5 6 2 1)
(3 9 8 4)
(9 10 5 8)
(10 11 6 5)
);
}
front
{
type empty;
faces
(
(15 16 19 12)
(19 17 13 12)
(17 18 14 13)
(15 16 20 21)
(20 17 22 21)
(17 18 23 22)
);
}
);
// ************************************************************************* //

View File

@ -0,0 +1,54 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application foamRun;
solver fluid;
startFrom latestTime;
startTime 0;
stopAt endTime;
endTime 0.15;
deltaT 2e-5;
writeControl adjustableRunTime;
writeInterval 0.001;
purgeWrite 0;
writeFormat ascii;
writePrecision 8;
writeCompression off;
timeFormat general;
timePrecision 6;
runTimeModifiable true;
functions
{
#includeFunc MachNo
#includeFunc residuals
}
// ************************************************************************* //

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@ -0,0 +1,28 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
object extrudeMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
constructFrom patch;
sourceCase "$FOAM_CASE";
sourcePatches (back);
exposedPatchName front;
extrudeModel plane;
thickness 0.1;
flipNormals false;
mergeFaces false;
// ************************************************************************* //

View File

@ -0,0 +1,19 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
object fvConstraints;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
#includeConstraint limitPressure(minFactor=0.1, maxFactor=2)
#includeConstraint limitTemperature(min=101, max=1000)
//************************************************************************** //

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@ -0,0 +1,73 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default Euler;
}
gradSchemes
{
default Gauss linear;
limited cellLimited Gauss linear 1;
grad(U) $limited;
grad(k) $limited;
grad(omega) $limited;
}
divSchemes
{
default none;
div(phi,U) Gauss linearUpwind limited;
turbulence Gauss linearUpwind limited;
energy Gauss linearUpwind limited;
div(phi,k) $turbulence;
div(phi,omega) $turbulence;
div(phi,e) $energy;
div(phi,K) $energy;
div(phi,Ekp) $energy;
div(phi,(p|rho)) $energy;
div((phi|interpolate(rho)),p) Gauss upwind;
div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;
}
laplacianSchemes
{
default Gauss linear corrected;
}
interpolationSchemes
{
default linear;
}
snGradSchemes
{
default corrected;
}
wallDist
{
method meshWave;
}
// ************************************************************************* //

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@ -0,0 +1,74 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
p
{
solver GAMG;
smoother GaussSeidel;
tolerance 1e-6;
relTol 0.01;
}
pFinal
{
$p;
relTol 0;
}
"(rho|U|k|omega|e)"
{
solver PBiCGStab;
preconditioner DILU;
tolerance 1e-6;
relTol 0.1;
}
"(rho|U|k|omega|e)Final"
{
$U;
relTol 0;
}
}
SIMPLE
{
residualControl
{
p 1e-4;
U 1e-4;
"(k|omega|e)" 1e-4;
}
nNonOrthogonalCorrectors 0;
}
PIMPLE
{
nCorrectors 2;
nNonOrthogonalCorrectors 1;
nOuterCorrectors 1;
}
relaxationFactors
{
equations
{
".*" 1;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,19 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
-------------------------------------------------------------------------------
Description
For specified fields, writes out the initial residuals for the first
solution of each time step; for non-scalar fields (e.g. vectors), writes
the largest of the residuals for each component (e.g. x, y, z).
\*---------------------------------------------------------------------------*/
#includeEtc "caseDicts/postProcessing/numerical/residuals.cfg"
fields (p U e k omega);
// ************************************************************************* //

View File

@ -0,0 +1,39 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
object T;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Tinlet 298;
dimensions [0 0 0 1 0 0 0];
internalField uniform $Tinlet;
boundaryField
{
freestream
{
type inletOutlet;
inletValue uniform $Tinlet;
value $inletValue;
}
wall
{
type zeroGradient;
}
#includeEtc "caseDicts/setConstraintTypes"
}
// ************************************************************************* //

View File

@ -0,0 +1,59 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volVectorField;
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
speed 250;
angleOfAttack 0; // degs
angle #calc "degToRad($angleOfAttack)";
liftDir #codeStream
{
codeInclude #{ #include "vector.H" #};
code #{ os << vector(-::sin($angle), 0, ::cos($angle)); #};
};
dragDir #codeStream
{
codeInclude #{ #include "vector.H" #};
code #{ os << vector(::cos($angle), 0, ::sin($angle)); #};
};
Uinlet #codeStream
{
codeInclude #{ #include "vector.H" #};
code #{ os << $speed*vector(::cos($angle), 0, ::sin($angle)); #};
};
dimensions [0 1 -1 0 0 0 0];
internalField uniform $Uinlet;
boundaryField
{
freestream
{
type freestreamVelocity;
freestreamValue uniform $Uinlet;
value uniform $Uinlet;
}
wall
{
type noSlip;
}
#includeEtc "caseDicts/setConstraintTypes"
}
// ************************************************************************* //

View File

@ -0,0 +1,37 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
object alphat;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
freestream
{
type calculated;
value uniform 0;
}
wall
{
type compressible::alphatWallFunction;
value uniform 0;
}
#includeEtc "caseDicts/setConstraintTypes"
}
// ************************************************************************* //

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@ -0,0 +1,40 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
object k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
kInlet 1e-3;
dimensions [0 2 -2 0 0 0 0];
internalField uniform $kInlet;
boundaryField
{
freestream
{
type inletOutlet;
inletValue uniform $kInlet;
value uniform $kInlet;
}
wall
{
type kqRWallFunction;
value uniform $kInlet;
}
#includeEtc "caseDicts/setConstraintTypes"
}
// ************************************************************************* //

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@ -0,0 +1,37 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
object mut;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
freestream
{
type calculated;
value uniform 0;
}
wall
{
type nutkWallFunction;
value uniform 0;
}
#includeEtc "caseDicts/setConstraintTypes"
}
// ************************************************************************* //

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@ -0,0 +1,40 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
object omega;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
omegaInlet 1;
dimensions [0 0 -1 0 0 0 0];
internalField uniform $omegaInlet;
boundaryField
{
freestream
{
type inletOutlet;
inletValue uniform $omegaInlet;
value uniform $omegaInlet;
}
wall
{
type omegaWallFunction;
value uniform $omegaInlet;
}
#includeEtc "caseDicts/setConstraintTypes"
}
// ************************************************************************* //

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@ -0,0 +1,38 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
object p;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
pOut 1e5;
dimensions [1 -1 -2 0 0 0 0];
internalField uniform $pOut;
boundaryField
{
freestream
{
type freestreamPressure;
freestreamValue uniform $pOut;
}
wall
{
type zeroGradient;
}
#includeEtc "caseDicts/setConstraintTypes"
}
// ************************************************************************* //

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@ -0,0 +1,15 @@
#!/bin/sh
cd ${0%/*} || exit 1 # Run from this directory
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
# Remove surface
rm -f constant/geometry/NACA0012.obj.gz
cleanCase
rm -f 0/Ma
rm -f constant/geometry/boundaryLayer.obj
#------------------------------------------------------------------------------

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@ -0,0 +1,18 @@
#!/bin/sh
cd ${0%/*} || exit 1 # Run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
# Copy aerofoil surface from resources directory
cp $FOAM_TUTORIALS/resources/geometry/NACA0012.obj.gz constant/geometry/
application="$(getApplication)"
runApplication blockMesh
runApplication transformPoints "scale=(1 0 1)"
runApplication extrudeMesh
runApplication $application
#------------------------------------------------------------------------------

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@ -0,0 +1,4 @@
Folder to house tri-surfaces
The Allrun script copies the surface from the $FOAM_TUTORIALS/resources/geometry
folder

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@ -0,0 +1,25 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
object momentumTransport;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
simulationType RAS;
RAS
{
model kOmegaSST;
turbulence on;
printCoeffs on;
}
// ************************************************************************* //

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@ -0,0 +1,48 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
location "constant";
object physicalProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
thermoType
{
type hePsiThermo;
mixture pureMixture;
transport const;
thermo hConst;
equationOfState perfectGas;
specie specie;
energy sensibleEnthalpy;
}
mixture // air at room temperature (293 K)
{
specie
{
molWeight 28.9;
}
thermodynamics
{
Cp 1005;
Hf 0;
}
transport
{
mu 1.82e-05;
Pr 0.71;
}
}
// ************************************************************************* //

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@ -0,0 +1,226 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
object blockMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
domain
{
xMax 100;
zMax 50;
xMin #neg $xMax;
zMin #neg $zMax;
// Number of cells
zCells 60; // aerofoil to far field
xUCells 60; // upstream
xMCells 25; // middle
xDCells 50; // downstream
// Mesh grading
zGrading 30000; // aerofoil to far field
xUGrading 10; // towards centre upstream
leadGrading 0.005; // towards leading edge
xDGrading 400; // downstream
}
aerofoil
{
xLead 0;
zLead 0;
xTrail 1;
zTrail 0;
xUpper 0.3;
zUpper 0.06;
xLower $xUpper;
zLower #neg $zUpper;
}
geometry
{
aerofoil
{
type triSurfaceMesh;
file "NACA0012.obj";
}
cylinder
{
type searchableCylinder;
point1 ($!aerofoil/xUpper -1e3 0);
point2 ($!aerofoil/xUpper 1e3 0);
radius $!domain/zMax;
}
}
vertices
(
project ($aerofoil/xLower -0.1 $domain/zMin) (cylinder)
($aerofoil/xTrail -0.1 $domain/zMin)
($domain/xMax -0.1 $domain/zMin)
project ($domain/xMin -0.1 $aerofoil/zLead) (cylinder)
project ($aerofoil/xLead -0.1 $aerofoil/zLead) (aerofoil)
project ($aerofoil/xTrail -0.1 $aerofoil/zTrail) (aerofoil)
($domain/xMax -0.1 $aerofoil/zTrail)
project ($aerofoil/xLower -0.1 $aerofoil/zLower) (aerofoil)
project ($aerofoil/xUpper -0.1 $aerofoil/zUpper) (aerofoil)
project ($aerofoil/xUpper -0.1 $domain/zMax) (aerofoil)
project ($aerofoil/xTrail -0.1 $domain/zMax) (aerofoil)
($domain/xMax -0.1 $domain/zMax)
project ($aerofoil/xLower 0.1 $domain/zMin) (cylinder)
($aerofoil/xTrail 0.1 $domain/zMin)
($domain/xMax 0.1 $domain/zMin)
project ($domain/xMin 0.1 $aerofoil/zLead) (cylinder)
project ($aerofoil/xLead 0.1 $aerofoil/zLead) (aerofoil)
project ($aerofoil/xTrail 0.1 $aerofoil/zTrail) (aerofoil)
($domain/xMax 0.1 $aerofoil/zTrail)
project ($aerofoil/xLower 0.1 $aerofoil/zLower) (aerofoil)
project ($aerofoil/xUpper 0.1 $aerofoil/zUpper) (aerofoil)
project ($aerofoil/xUpper 0.1 $domain/zMax) (aerofoil)
project ($aerofoil/xTrail 0.1 $domain/zMax) (aerofoil)
($domain/xMax 0.1 $domain/zMax)
);
blocks
(
hex ( 7 4 16 19 0 3 15 12)
($!domain/xUCells 1 $!domain/zCells)
edgeGrading
(
$!domain/leadGrading $!domain/leadGrading $!domain/xUGrading $!domain/xUGrading
1 1 1 1
$!domain/zGrading $!domain/zGrading $!domain/zGrading $!domain/zGrading
)
hex ( 5 7 19 17 1 0 12 13)
($!domain/xMCells 1 $!domain/zCells)
simpleGrading (1 1 $!domain/zGrading)
hex ( 17 18 6 5 13 14 2 1)
($!domain/xDCells 1 $!domain/zCells)
simpleGrading ($!domain/xDGrading 1 $!domain/zGrading)
hex ( 20 16 4 8 21 15 3 9)
($!domain/xUCells 1 $!domain/zCells)
edgeGrading
(
$!domain/leadGrading $!domain/leadGrading $!domain/xUGrading $!domain/xUGrading
1 1 1 1
$!domain/zGrading $!domain/zGrading $!domain/zGrading $!domain/zGrading
)
hex ( 17 20 8 5 22 21 9 10)
($!domain/xMCells 1 $!domain/zCells)
simpleGrading (1 1 $!domain/zGrading)
hex ( 5 6 18 17 10 11 23 22)
($!domain/xDCells 1 $!domain/zCells)
simpleGrading ($!domain/xDGrading 1 $!domain/zGrading)
);
edges
(
project 4 7 (aerofoil)
project 7 5 (aerofoil)
project 4 8 (aerofoil)
project 8 5 (aerofoil)
project 16 19 (aerofoil)
project 19 17 (aerofoil)
project 16 20 (aerofoil)
project 20 17 (aerofoil)
project 3 0 (cylinder)
project 3 9 (cylinder)
project 15 12 (cylinder)
project 15 21 (cylinder)
);
boundary
(
aerofoil
{
type wall;
faces
(
(4 7 19 16)
(7 5 17 19)
(5 8 20 17)
(8 4 16 20)
);
}
inlet
{
type patch;
inGroups (freestream);
faces
(
(3 0 12 15)
(0 1 13 12)
(1 2 14 13)
(11 10 22 23)
(10 9 21 22)
(9 3 15 21)
);
}
outlet
{
type patch;
inGroups (freestream);
faces
(
(2 6 18 14)
(6 11 23 18)
);
}
back
{
type empty;
faces
(
(3 4 7 0)
(7 5 1 0)
(5 6 2 1)
(3 9 8 4)
(9 10 5 8)
(10 11 6 5)
);
}
front
{
type empty;
faces
(
(15 16 19 12)
(19 17 13 12)
(17 18 14 13)
(15 16 20 21)
(20 17 22 21)
(17 18 23 22)
);
}
);
// ************************************************************************* //

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@ -0,0 +1,55 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application foamRun;
solver fluid;
startFrom startTime;
startTime 0;
stopAt endTime;
endTime 5000;
deltaT 1;
writeControl timeStep;
writeInterval 50;
purgeWrite 0;
writeFormat ascii;
writePrecision 10;
writeCompression off;
timeFormat general;
timePrecision 6;
runTimeModifiable true;
functions
{
#includeFunc MachNo
#includeFunc residuals
#includeFunc forceCoeffsCompressible
}
// ************************************************************************* //

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@ -0,0 +1,28 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
object extrudeMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
constructFrom patch;
sourceCase "$FOAM_CASE";
sourcePatches (back);
exposedPatchName front;
extrudeModel plane;
thickness 1;
flipNormals false;
mergeFaces false;
// ************************************************************************* //

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@ -0,0 +1,29 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | Web: www.OpenFOAM.org
\\/ M anipulation |
-------------------------------------------------------------------------------
Description
Calculates lift, drag and moment coefficients by summing forces on
specified patches for a case where the solver is compressible (pressure is
in units M/(LT^2), e.g. Pa).
\*---------------------------------------------------------------------------*/
#include "$FOAM_CASE/0/U"
patches (aerofoil);
magUInf $speed;
lRef 1;
Aref 1; // span
rhoInf 1.2;
CofR (0.2 0 0);
pitchAxis (0 1 0);
#includeEtc "caseDicts/postProcessing/forces/forceCoeffs.cfg"
// ************************************************************************* //

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@ -0,0 +1,19 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
object fvConstraints;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
#includeConstraint limitPressure(minFactor=0.1, maxFactor=2)
#includeConstraint limitTemperature(min=101, max=1000)
// ************************************************************************* //

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@ -0,0 +1,68 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default steadyState;
}
gradSchemes
{
default Gauss linear;
limited cellLimited Gauss linear 1;
grad(U) $limited;
grad(k) $limited;
grad(omega) $limited;
}
divSchemes
{
default none;
div(phi,U) bounded Gauss linearUpwind limited;
energy bounded Gauss linearUpwind limited;
div(phi,h) $energy;
div(phi,K) $energy;
turbulence bounded Gauss upwind;
div(phi,k) $turbulence;
div(phi,omega) $turbulence;
div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;
}
laplacianSchemes
{
default Gauss linear corrected;
}
interpolationSchemes
{
default linear;
}
snGradSchemes
{
default corrected;
}
wallDist
{
method meshWave;
}
// ************************************************************************* //

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@ -0,0 +1,64 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
p
{
solver GAMG;
smoother DIC;
tolerance 1e-8;
relTol 0.01;
}
"(U|k|omega|h)"
{
solver PBiCGStab;
preconditioner DILU;
tolerance 1e-10;
relTol 0.1;
}
}
PIMPLE
{
residualControl
{
p 1e-6;
U 1e-5;
"(k|omega|h)" 1e-5;
}
nNonOrthogonalCorrectors 0;
}
relaxationFactors
{
fields
{
p 0.3;
rho 0.01;
}
equations
{
U 0.7;
h 0.7;
"(k|omega)" 0.7;
}
}
// ************************************************************************* //

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@ -0,0 +1,19 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
-------------------------------------------------------------------------------
Description
For specified fields, writes out the initial residuals for the first
solution of each time step; for non-scalar fields (e.g. vectors), writes
the largest of the residuals for each component (e.g. x, y, z).
\*---------------------------------------------------------------------------*/
#includeEtc "caseDicts/postProcessing/numerical/residuals.cfg"
fields (p U e k omega);
// ************************************************************************* //

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@ -0,0 +1,46 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
object T;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 1 0 0 0];
internalField uniform 293;
boundaryField
{
walls
{
type zeroGradient;
}
porosityWall
{
type zeroGradient;
}
inlet
{
type fixedValue;
value $internalField;
}
outlet
{
type inletOutlet;
value $internalField;
inletValue $internalField;
}
}
// ************************************************************************* //

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@ -0,0 +1,49 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volVectorField;
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
walls
{
type noSlip;
}
porosityWall
{
type slip;
value uniform (0 0 0);
}
inlet
{
type flowRateInletVelocity;
massFlowRate constant 0.1;
profile turbulentBL;
rhoInlet 1; // estimate for initial rho
}
outlet
{
type pressureInletOutletVelocity;
value uniform (0 0 0);
inletValue uniform (0 0 0);
}
}
// ************************************************************************* //

View File

@ -0,0 +1,49 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
location "0";
object alphat;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -1 0 0 0 0];
internalField uniform 1e-3;
boundaryField
{
walls
{
type compressible::alphatWallFunction;
value $internalField;
}
porosityWall
{
type compressible::alphatWallFunction;
value $internalField;
}
inlet
{
type calculated;
value $internalField;
}
outlet
{
type calculated;
value $internalField;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,51 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
location "0";
object epsilon;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -3 0 0 0 0];
internalField uniform 200;
boundaryField
{
walls
{
type epsilonWallFunction;
value uniform 200;
}
porosityWall
{
type epsilonWallFunction;
value uniform 200;
}
inlet
{
type turbulentMixingLengthDissipationRateInlet;
mixingLength 0.005;
value uniform 200;
}
outlet
{
type inletOutlet;
inletValue uniform 200;
value uniform 200;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,51 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
location "0";
object k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 1;
boundaryField
{
walls
{
type kqRWallFunction;
value uniform 1;
}
porosityWall
{
type kqRWallFunction;
value uniform 1;
}
inlet
{
type turbulentIntensityKineticEnergyInlet;
intensity 0.05;
value uniform 1;
}
outlet
{
type inletOutlet;
inletValue uniform 1;
value uniform 1;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,49 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
location "0";
object nut;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
walls
{
type nutkWallFunction;
value uniform 0;
}
porosityWall
{
type nutkWallFunction;
value uniform 0;
}
inlet
{
type calculated;
value uniform 0;
}
outlet
{
type calculated;
value uniform 0;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,44 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
object p;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -2 0 0 0 0];
internalField uniform 1e5;
boundaryField
{
walls
{
type zeroGradient;
}
porosityWall
{
type zeroGradient;
}
inlet
{
type zeroGradient;
}
outlet
{
type fixedValue;
value $internalField;
}
}
// ************************************************************************* //

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@ -0,0 +1,8 @@
#!/bin/sh
cd ${0%/*} || exit 1 # Run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
runApplication blockMesh -dict $FOAM_TUTORIALS/resources/blockMesh/angledDuct
runApplication $(getApplication)

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@ -0,0 +1,45 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
location "constant";
object fvModels;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
porosity1
{
type explicitPorositySource;
explicitPorositySourceCoeffs
{
cellZone porosity;
type DarcyForchheimer;
d (7e5 -1000 -1000);
f (0 0 0);
coordinateSystem
{
type cartesian;
origin (0 0 0);
coordinateRotation
{
type axesRotation;
e1 (0.70710678 0.70710678 0);
e3 (0 0 1);
}
}
}
}
//************************************************************************ //

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@ -0,0 +1,29 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
location "constant";
object momentumTransport;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
simulationType RAS;
RAS
{
model kEpsilon;
turbulence on;
printCoeffs on;
}
// ************************************************************************* //

View File

@ -0,0 +1,47 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
location "constant";
object physicalProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
thermoType
{
type hePsiThermo;
mixture pureMixture;
transport const;
thermo hConst;
equationOfState perfectGas;
specie specie;
energy sensibleInternalEnergy;
}
mixture
{
specie
{
molWeight 28.9;
}
thermodynamics
{
Cp 1005;
Hf 0;
}
transport
{
mu 1.82e-05;
Pr 0.71;
}
}
// ************************************************************************* //

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@ -0,0 +1,56 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
location "system";
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application foamRun;
solver fluid;
startFrom startTime;
startTime 0;
stopAt endTime;
endTime 10;
deltaT 1;
writeControl adjustableRunTime;
writeInterval 10;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
writeCompression off;
timeFormat general;
timePrecision 6;
runTimeModifiable true;
adjustTimeStep no;
maxCo 10;
maxDeltaT 1;
// ************************************************************************* //

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@ -0,0 +1,24 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
object fvConstraints;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
limitp
{
type limitPressure;
minFactor 0.9;
maxFactor 1.5;
}
// ************************************************************************* //

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@ -0,0 +1,64 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
location "system";
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default Euler;
}
gradSchemes
{
default Gauss linear;
}
divSchemes
{
default none;
div(phi,U) bounded Gauss upwind;
div(phid,p) bounded Gauss upwind;
div(phi,(p|rho)) bounded Gauss upwind;
div(phi,K) bounded Gauss linear;
div(phi,e) bounded Gauss upwind;
div(phi,k) bounded Gauss upwind;
div(phi,epsilon) bounded Gauss upwind;
div(phi,R) bounded Gauss upwind;
div(phi,omega) bounded Gauss upwind;
div((rho*R)) Gauss linear;
div(R) Gauss linear;
div(U) Gauss linear;
div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;
}
laplacianSchemes
{
default Gauss linear corrected;
}
interpolationSchemes
{
default linear;
}
snGradSchemes
{
default corrected;
}
// ************************************************************************* //

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@ -0,0 +1,86 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
location "system";
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
p
{
solver PCG;
preconditioner DIC;
tolerance 1e-07;
relTol 0.01;
}
pFinal
{
$p;
relTol 0;
}
"(rho|U|e|k|epsilon|omega)"
{
solver smoothSolver;
smoother symGaussSeidel;
tolerance 1e-06;
relTol 0.1;
}
"(rho|U|e|k|epsilon|omega)Final"
{
$U;
relTol 0;
}
}
PIMPLE
{
momentumPredictor yes;
transonic no;
nOuterCorrectors 50;
nCorrectors 1;
nNonOrthogonalCorrectors 0;
consistent yes;
simpleRho yes;
outerCorrectorResidualControl
{
"(U|k|epsilon)"
{
relTol 0;
tolerance 0.0001;
}
}
transportCorrectionFinal no;
}
relaxationFactors
{
fields
{
p 1;
rho 1;
}
equations
{
U 0.9;
e 0.7;
"(k|epsilon|omega)" 0.8;
}
}
// ************************************************************************* //

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@ -0,0 +1,46 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
object T;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 1 0 0 0];
internalField uniform 293;
boundaryField
{
walls
{
type zeroGradient;
}
porosityWall
{
type zeroGradient;
}
inlet
{
type fixedValue;
value $internalField;
}
outlet
{
type inletOutlet;
value $internalField;
inletValue $internalField;
}
}
// ************************************************************************* //

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@ -0,0 +1,49 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volVectorField;
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
walls
{
type noSlip;
}
porosityWall
{
type slip;
value uniform (0 0 0);
}
inlet
{
type flowRateInletVelocity;
massFlowRate constant 0.1;
profile turbulentBL;
value uniform (0 0 0);
}
outlet
{
type inletOutlet;
value uniform (0 0 0);
inletValue uniform (0 0 0);
}
}
// ************************************************************************* //

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@ -0,0 +1,49 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
location "0";
object alphat;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
walls
{
type compressible::alphatWallFunction;
value uniform 0;
}
porosityWall
{
type compressible::alphatWallFunction;
value uniform 0;
}
inlet
{
type calculated;
value uniform 0;
}
outlet
{
type calculated;
value uniform 0;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,51 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
location "0";
object epsilon;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -3 0 0 0 0];
internalField uniform 200;
boundaryField
{
walls
{
type epsilonWallFunction;
value uniform 200;
}
porosityWall
{
type epsilonWallFunction;
value uniform 200;
}
inlet
{
type turbulentMixingLengthDissipationRateInlet;
mixingLength 0.005;
value uniform 200;
}
outlet
{
type inletOutlet;
inletValue uniform 200;
value uniform 200;
}
}
// ************************************************************************* //

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@ -0,0 +1,51 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
location "0";
object k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 1;
boundaryField
{
walls
{
type kqRWallFunction;
value uniform 1;
}
porosityWall
{
type kqRWallFunction;
value uniform 1;
}
inlet
{
type turbulentIntensityKineticEnergyInlet;
intensity 0.05;
value uniform 1;
}
outlet
{
type inletOutlet;
inletValue uniform 1;
value uniform 1;
}
}
// ************************************************************************* //

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@ -0,0 +1,49 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
location "0";
object nut;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
walls
{
type nutkWallFunction;
value uniform 0;
}
porosityWall
{
type nutkWallFunction;
value uniform 0;
}
inlet
{
type calculated;
value uniform 0;
}
outlet
{
type calculated;
value uniform 0;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,44 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
object p;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -2 0 0 0 0];
internalField uniform 1.0e5;
boundaryField
{
walls
{
type zeroGradient;
}
porosityWall
{
type zeroGradient;
}
inlet
{
type zeroGradient;
}
outlet
{
type fixedValue;
value $internalField;
}
}
// ************************************************************************* //

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@ -0,0 +1,12 @@
#!/bin/sh
cd ${0%/*} || exit 1 # Run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
application=$(getApplication)
runApplication blockMesh -dict $FOAM_TUTORIALS/resources/blockMesh/angledDuct
runApplication $application
#------------------------------------------------------------------------------

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@ -0,0 +1,49 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
location "constant";
object fvModels;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
porosity
{
type explicitPorositySource;
explicitPorositySourceCoeffs
{
cellZone porosity;
type fixedCoeff;
fixedCoeffCoeffs
{
alpha (500 -1000 -1000);
beta (0 0 0);
rhoRef 1;
coordinateSystem
{
type cartesian;
origin (0 0 0);
coordinateRotation
{
type axesRotation;
e1 (0.70710678 0.70710678 0);
e2 (0 0 1);
}
}
}
}
}
// ************************************************************************* //

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@ -0,0 +1,29 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
location "constant";
object momentumTransport;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
simulationType RAS;
RAS
{
model kEpsilon;
turbulence on;
printCoeffs on;
}
// ************************************************************************* //

View File

@ -0,0 +1,47 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
location "constant";
object physicalProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
thermoType
{
type hePsiThermo;
mixture pureMixture;
transport const;
thermo hConst;
equationOfState perfectGas;
specie specie;
energy sensibleEnthalpy;
}
mixture
{
specie
{
molWeight 28.9;
}
thermodynamics
{
Cp 1005;
Hf 0;
}
transport
{
mu 1.82e-05;
Pr 0.71;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,52 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
location "system";
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application foamRun;
solver fluid;
startFrom startTime;
startTime 0;
stopAt endTime;
endTime 1000;
deltaT 1;
writeControl timeStep;
writeInterval 100;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
writeCompression off;
timeFormat general;
timePrecision 6;
graphFormat raw;
runTimeModifiable true;
// ************************************************************************* //

View File

@ -0,0 +1,50 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
location "system";
object fvConstraints;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
limitp
{
type limitPressure;
minFactor 0.4;
maxFactor 1.5;
}
fixedTemperature
{
type fixedTemperatureConstraint;
cellZone porosity;
mode uniform;
temperature 350;
}
porosityTurbulence
{
type fixedValueConstraint;
cellZone porosity;
fieldValues
{
k 1;
epsilon 150;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,58 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
location "system";
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default steadyState;
}
gradSchemes
{
default Gauss linear;
}
divSchemes
{
default none;
div(phi,U) bounded Gauss upwind;
div(phi,h) bounded Gauss upwind;
div(phi,K) bounded Gauss upwind;
div(phi,epsilon) bounded Gauss upwind;
div(phi,k) bounded Gauss upwind;
div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;
}
laplacianSchemes
{
default Gauss linear corrected;
}
interpolationSchemes
{
default linear;
}
snGradSchemes
{
default corrected;
}
// ************************************************************************* //

View File

@ -0,0 +1,85 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
location "system";
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
p
{
solver GAMG;
tolerance 1e-08;
relTol 0.05;
smoother GaussSeidel;
nCellsInCoarsestLevel 20;
}
U
{
solver smoothSolver;
smoother GaussSeidel;
tolerance 1e-6;
relTol 0.1;
}
h
{
solver smoothSolver;
smoother symGaussSeidel;
tolerance 1e-6;
relTol 0.1;
}
"(k|epsilon)"
{
$U;
tolerance 1e-07;
relTol 0.1;
}
}
PIMPLE
{
nNonOrthogonalCorrectors 0;
residualControl
{
p 1e-2;
U 1e-4;
e 1e-3;
"(k|epsilon)" 1e-3;
}
}
relaxationFactors
{
fields
{
p 0.3;
rho 0.01;
}
equations
{
U 0.7;
h 0.7;
"(k|epsilon)" 0.7;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,46 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
object T;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 1 0 0 0];
internalField uniform 293;
boundaryField
{
walls
{
type zeroGradient;
}
porosityWall
{
type zeroGradient;
}
inlet
{
type fixedValue;
value $internalField;
}
outlet
{
type inletOutlet;
value $internalField;
inletValue $internalField;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,49 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volVectorField;
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (47.8 0 0);
boundaryField
{
walls
{
type noSlip;
}
porosityWall
{
type slip;
value uniform (0 0 0);
}
inlet
{
type flowRateInletVelocity;
massFlowRate constant 0.1;
profile turbulentBL;
value uniform (0 0 0);
}
outlet
{
type fluxCorrectedVelocity; // inletOutlet;
value uniform (0 0 0);
inletValue uniform (0 0 0);
}
}
// ************************************************************************* //

View File

@ -0,0 +1,49 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
location "0";
object alphat;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
walls
{
type compressible::alphatWallFunction;
value uniform 0;
}
porosityWall
{
type compressible::alphatWallFunction;
value uniform 0;
}
inlet
{
type calculated;
value uniform 0;
}
outlet
{
type calculated;
value uniform 0;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,51 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
location "0";
object epsilon;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -3 0 0 0 0];
internalField uniform 200;
boundaryField
{
walls
{
type epsilonWallFunction;
value uniform 200;
}
porosityWall
{
type epsilonWallFunction;
value uniform 200;
}
inlet
{
type turbulentMixingLengthDissipationRateInlet;
mixingLength 0.005;
value uniform 200;
}
outlet
{
type inletOutlet;
inletValue uniform 200;
value uniform 200;
}
}
// ************************************************************************* //

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@ -0,0 +1,51 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
location "0";
object k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 1;
boundaryField
{
walls
{
type kqRWallFunction;
value uniform 1;
}
porosityWall
{
type kqRWallFunction;
value uniform 1;
}
inlet
{
type turbulentIntensityKineticEnergyInlet;
intensity 0.05;
value uniform 1;
}
outlet
{
type inletOutlet;
inletValue uniform 1;
value uniform 1;
}
}
// ************************************************************************* //

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@ -0,0 +1,49 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
location "0";
object nut;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
walls
{
type nutkWallFunction;
value uniform 0;
}
porosityWall
{
type nutkWallFunction;
value uniform 0;
}
inlet
{
type calculated;
value uniform 0;
}
outlet
{
type calculated;
value uniform 0;
}
}
// ************************************************************************* //

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@ -0,0 +1,44 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
object p;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -2 0 0 0 0];
internalField uniform 1e5;
boundaryField
{
walls
{
type zeroGradient;
}
porosityWall
{
type zeroGradient;
}
inlet
{
type zeroGradient;
}
outlet
{
type fixedValue;
value $internalField;
}
}
// ************************************************************************* //

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@ -0,0 +1,8 @@
#!/bin/sh
cd ${0%/*} || exit 1 # Run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
runApplication blockMesh -dict $FOAM_TUTORIALS/resources/blockMesh/angledDuct
runApplication $(getApplication)

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@ -0,0 +1,45 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
location "constant";
object fvModels;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
porosity1
{
type explicitPorositySource;
explicitPorositySourceCoeffs
{
cellZone porosity;
type DarcyForchheimer;
d (5e7 -1000 -1000);
f (0 0 0);
coordinateSystem
{
type cartesian;
origin (0 0 0);
coordinateRotation
{
type axesRotation;
e1 (0.70710678 0.70710678 0);
e2 (0 0 1);
}
}
}
}
// ************************************************************************* //

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@ -0,0 +1,29 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
location "constant";
object momentumTransport;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
simulationType RAS;
RAS
{
model kEpsilon;
turbulence on;
printCoeffs on;
}
// ************************************************************************* //

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@ -0,0 +1,47 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
location "constant";
object physicalProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
thermoType
{
type hePsiThermo;
mixture pureMixture;
transport const;
thermo hConst;
equationOfState perfectGas;
specie specie;
energy sensibleEnthalpy;
}
mixture
{
specie
{
molWeight 28.9;
}
thermodynamics
{
Cp 1005;
Hf 0;
}
transport
{
mu 1.82e-05;
Pr 0.71;
}
}
// ************************************************************************* //

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@ -0,0 +1,50 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
location "system";
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application foamRun;
solver fluid;
startFrom startTime;
startTime 0;
stopAt endTime;
endTime 500;
deltaT 1;
writeControl adjustableRunTime;
writeInterval 50;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
writeCompression off;
timeFormat general;
timePrecision 6;
runTimeModifiable true;
// ************************************************************************* //

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@ -0,0 +1,24 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
object fvConstraints;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
limitp
{
type limitPressure;
minFactor 0.9;
maxFactor 1.5;
}
// ************************************************************************* //

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@ -0,0 +1,60 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
location "system";
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default localEuler;
}
gradSchemes
{
default Gauss linear;
}
divSchemes
{
default none;
div(phi,U) Gauss upwind;
div(phid,p) Gauss upwind;
div(phi,K) Gauss linear;
div(phi,h) Gauss upwind;
div(phi,k) Gauss upwind;
div(phi,epsilon) Gauss upwind;
div(phi,R) Gauss upwind;
div(phi,omega) Gauss upwind;
div((rho*R)) Gauss linear;
div(R) Gauss linear;
div(U) Gauss linear;
div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;
}
laplacianSchemes
{
default Gauss linear corrected;
}
interpolationSchemes
{
default linear;
}
snGradSchemes
{
default corrected;
}
// ************************************************************************* //

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@ -0,0 +1,65 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
location "system";
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
p
{
solver PCG;
preconditioner DIC;
tolerance 1e-06;
relTol 0.1;
}
pFinal
{
$p;
tolerance 1e-06;
relTol 0.1;
}
"(rho|U|h|k|epsilon|omega)"
{
solver smoothSolver;
smoother symGaussSeidel;
tolerance 1e-05;
relTol 0.1;
}
"(rho|U|h|k|epsilon|omega)Final"
{
$U;
tolerance 1e-05;
relTol 0.1;
}
}
PIMPLE
{
momentumPredictor yes;
nOuterCorrectors 1;
nCorrectors 1;
nNonOrthogonalCorrectors 0;
maxCo 0.2;
rDeltaTSmoothingCoeff 0.1;
rDeltaTDampingCoeff 1;
maxDeltaT 1;
}
// ************************************************************************* //

View File

@ -0,0 +1,60 @@
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
location "0";
object T;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
#include "${FOAM_CASE}/constant/caseSettings"
dimensions [0 0 0 1 0 0 0];
internalField uniform $!outerInlet/T;
boundaryField
{
#includeEtc "caseDicts/setConstraintTypes"
innerInlet
{
type fixedValue;
value uniform $!innerInlet/T;
}
outerInlet
{
type fixedValue;
value uniform $!outerInlet/T;
}
outlet
{
$!outlet/T;
}
staticWalls
{
$!wall/T;
}
movingWalls
{
$staticWalls;
}
nonCouple
{
type zeroGradient;
}
}
// ************************************************************************* //

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