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 volVectorField;
object D;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 0 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
topSurface
{
type tractionDisplacement;
traction uniform (0 0 0);
pressure uniform 0;
value uniform (0 0 0);
}
bottomSurface
{
type tractionDisplacement;
traction uniform (0 0 0);
pressure uniform 0;
value uniform (0 0 0);
}
fixedEnd
{
type fixedValue;
value uniform (0 0 0);
}
tractionEnd
{
type tractionDisplacement;
traction uniform (0 10000 0);
pressure uniform 0;
value uniform (0 0 0);
}
defaultFaces
{
type empty;
}
}
// ************************************************************************* //

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@ -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 volScalarField;
object T;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 1 0 0 0];
internalField uniform 0;
boundaryField
{
topSurface
{
type calculated;
value uniform 0;
}
bottomSurface
{
type calculated;
value uniform 0;
}
fixedEnd
{
type calculated;
value uniform 0;
}
tractionEnd
{
type calculated;
value uniform 0;
}
defaultFaces
{
type empty;
}
}
// ************************************************************************* //

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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 "constant";
object physicalProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
rho
{
type uniform;
value 7854;
}
nu
{
type uniform;
value 0.0;
}
E
{
type uniform;
value 2e+11;
}
Cv
{
type uniform;
value 434;
}
kappa
{
type uniform;
value 60.5;
}
alphav
{
type uniform;
value 1.1e-05;
}
planeStress yes;
thermalStress no;
// ************************************************************************* //

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@ -0,0 +1,82 @@
/*--------------------------------*- 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;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
convertToMeters 1;
vertices
(
(0 0 0)
(30 0 0)
(30 1 0)
(0 1 0)
(0 0 1)
(30 0 1)
(30 1 1)
(0 1 1)
);
blocks
(
hex (0 1 2 3 4 5 6 7) (6 2 1) simpleGrading (1.0 1.0 1.0)
);
defaultPatch
{
type empty;
}
boundary
(
topSurface
{
type patch;
faces
(
(3 7 6 2)
);
}
bottomSurface
{
type patch;
faces
(
(4 0 1 5)
);
}
fixedEnd
{
type patch;
faces
(
(0 4 7 3)
);
}
tractionEnd
{
type patch;
faces
(
(1 2 6 5)
);
}
);
// ************************************************************************* //

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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 "system";
object controlDict.org;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application foamRun;
solver solidDisplacement;
startFrom startTime;
startTime 0;
stopAt endTime;
endTime 10000;
deltaT 1;
writeControl runTime;
writeInterval 1000;
purgeWrite 0;
writeFormat ascii;
writeCompression off;
timeFormat general;
timePrecision 6;
runTimeModifiable true;
// ************************************************************************* //

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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 "system";
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
d2dt2Schemes
{
default steadyState;
}
gradSchemes
{
default Gauss cubic;
}
divSchemes
{
default Gauss cubic;
}
laplacianSchemes
{
default Gauss linear uncorrected;
}
interpolationSchemes
{
default cubic;
}
snGradSchemes
{
default uncorrected;
}
// ************************************************************************* //

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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 dictionary;
location "system";
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
D
{
solver GAMG;
smoother GaussSeidel;
tolerance 1e-10;
relTol 0.99;
nCellsInCoarsestLevel 6;
}
}
PIMPLE
{
compactNormalStress no;
accelerationFactor 1.9; // Lower for higher Poisson ratio
}
// ************************************************************************* //

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@ -0,0 +1,57 @@
/*--------------------------------*- 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 D;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 0 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
left
{
type symmetryPlane;
}
right
{
type tractionDisplacement;
traction uniform (10000 0 0);
pressure uniform 0;
value uniform (0 0 0);
}
down
{
type symmetryPlane;
}
up
{
type tractionDisplacement;
traction uniform (0 0 0);
pressure uniform 0;
value uniform (0 0 0);
}
hole
{
type tractionDisplacement;
traction uniform (0 0 0);
pressure uniform 0;
value uniform (0 0 0);
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

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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;
object T;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 1 0 0 0];
internalField uniform 300;
boundaryField
{
left
{
type symmetryPlane;
}
right
{
type zeroGradient;
}
down
{
type symmetryPlane;
}
up
{
type zeroGradient;
}
hole
{
type fixedValue;
value uniform 400;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

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@ -0,0 +1,14 @@
#!/bin/sh
cd ${0%/*} || exit 1 # Run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
application=$(getApplication)
runApplication blockMesh
runApplication $application
runApplication -s sigma foamPostProcess -func "components(sigma)"
runApplication -s graphUniform foamPostProcess -func graphUniform
#------------------------------------------------------------------------------

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@ -0,0 +1,57 @@
/*--------------------------------*- 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;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
rho
{
type uniform;
value 7854;
}
nu
{
type uniform;
value 0.3;
}
E
{
type uniform;
value 2e+11;
}
Cv
{
type uniform;
value 434;
}
kappa
{
type uniform;
value 60.5;
}
alphav
{
type uniform;
value 1.1e-05;
}
planeStress yes;
thermalStress no;
// ************************************************************************* //

View File

@ -0,0 +1,132 @@
/*--------------------------------*- 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;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
convertToMeters 1;
vertices
(
(0.5 0 0)
(1 0 0)
(2 0 0)
(2 0.707107 0)
(0.707107 0.707107 0)
(0.353553 0.353553 0)
(2 2 0)
(0.707107 2 0)
(0 2 0)
(0 1 0)
(0 0.5 0)
(0.5 0 0.5)
(1 0 0.5)
(2 0 0.5)
(2 0.707107 0.5)
(0.707107 0.707107 0.5)
(0.353553 0.353553 0.5)
(2 2 0.5)
(0.707107 2 0.5)
(0 2 0.5)
(0 1 0.5)
(0 0.5 0.5)
);
blocks
(
hex (5 4 9 10 16 15 20 21) (10 10 1) simpleGrading (1 1 1)
hex (0 1 4 5 11 12 15 16) (10 10 1) simpleGrading (1 1 1)
hex (1 2 3 4 12 13 14 15) (20 10 1) simpleGrading (1 1 1)
hex (4 3 6 7 15 14 17 18) (20 20 1) simpleGrading (1 1 1)
hex (9 4 7 8 20 15 18 19) (10 20 1) simpleGrading (1 1 1)
);
edges
(
arc 0 5 (0.469846 0.17101 0)
arc 5 10 (0.17101 0.469846 0)
arc 1 4 (0.939693 0.34202 0)
arc 4 9 (0.34202 0.939693 0)
arc 11 16 (0.469846 0.17101 0.5)
arc 16 21 (0.17101 0.469846 0.5)
arc 12 15 (0.939693 0.34202 0.5)
arc 15 20 (0.34202 0.939693 0.5)
);
boundary
(
left
{
type symmetryPlane;
faces
(
(8 9 20 19)
(9 10 21 20)
);
}
right
{
type patch;
faces
(
(2 3 14 13)
(3 6 17 14)
);
}
down
{
type symmetryPlane;
faces
(
(0 1 12 11)
(1 2 13 12)
);
}
up
{
type patch;
faces
(
(7 8 19 18)
(6 7 18 17)
);
}
hole
{
type patch;
faces
(
(10 5 16 21)
(5 0 11 16)
);
}
frontAndBack
{
type empty;
faces
(
(10 9 4 5)
(5 4 1 0)
(1 4 3 2)
(4 7 6 3)
(4 9 8 7)
(21 16 15 20)
(16 11 12 15)
(12 13 14 15)
(15 14 17 18)
(15 18 19 20)
);
}
);
// ************************************************************************* //

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 solidDisplacement;
startFrom startTime;
startTime 0;
stopAt endTime;
endTime 100;
deltaT 1;
writeControl timeStep;
writeInterval 20;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
writeCompression off;
timeFormat general;
timePrecision 6;
graphFormat raw;
runTimeModifiable true;
// ************************************************************************* //

View File

@ -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
{
format ascii;
class dictionary;
location "system";
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
d2dt2Schemes
{
default steadyState;
}
ddtSchemes
{
default Euler;
}
gradSchemes
{
default leastSquares;
}
divSchemes
{
default none;
div(sigmaD) Gauss linear;
}
laplacianSchemes
{
default Gauss linear corrected;
}
interpolationSchemes
{
default linear;
}
snGradSchemes
{
default none;
}
// ************************************************************************* //

View File

@ -0,0 +1,35 @@
/*--------------------------------*- 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
{
"(D|e)"
{
solver GAMG;
tolerance 1e-06;
relTol 0.9;
smoother GaussSeidel;
nCellsInCoarsestLevel 20;
}
}
PIMPLE
{
compactNormalStress yes;
}
// ************************************************************************* //

View File

@ -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 |
-------------------------------------------------------------------------------
Description
Writes graph data for specified fields along a line, specified by start and
end points. A specified number of graph points are used, distributed
uniformly along the line.
\*---------------------------------------------------------------------------*/
start (0 0.5 0.25);
end (0 2 0.25);
nPoints 100;
fields (sigmaxx);
axis y;
#includeEtc "caseDicts/postProcessing/graphs/graphUniform.cfg"
// ************************************************************************* //