zhyang-dev/openfoam
1
0
Fork 0
mirror of https://develop.openfoam.com/Development/openfoam.git synced 2025-11-28 03:28:01 +00:00
Code Issues Actions Packages Projects Releases Wiki Activity

Adding overPotentialFoam and overRhoSimpleFoam and tutorials

Browse Source
This commit is contained in:
sergio
2017-12-19 11:33:43 -08:00
parent a6d88f2fe7
commit 985a18df75
74 changed files with 3737 additions and 0 deletions
Download Patch File Download Diff File Expand all files Collapse all files

3
applications/solvers/basic/potentialFoam/overPotentialFoam/Make/files Normal file
View File

@ -0,0 +1,3 @@
potentialFoam.C
EXE = $(FOAM_APPBIN)/overPotentialFoam

12
applications/solvers/basic/potentialFoam/overPotentialFoam/Make/options Normal file
View File

@ -0,0 +1,12 @@
EXE_INC = \
-I$(LIB_SRC)/finiteVolume/lnInclude \
-I$(LIB_SRC)/dynamicFvMesh/lnInclude \
-I$(LIB_SRC)/overset/lnInclude \
-I$(LIB_SRC)/meshTools/lnInclude \
-I$(LIB_SRC)/sampling/lnInclude
EXE_LIBS = \
-lfiniteVolume \
-lmeshTools \
-lsampling \
-loverset

9
applications/solvers/basic/potentialFoam/overPotentialFoam/createControls.H Normal file
View File

@ -0,0 +1,9 @@
const dictionary& potentialFlow
(
mesh.solutionDict().subDict("potentialFlow")
);
const int nNonOrthCorr
(
potentialFlow.lookupOrDefault<int>("nNonOrthogonalCorrectors", 0)
);

146
applications/solvers/basic/potentialFoam/overPotentialFoam/createFields.H Normal file
View File

@ -0,0 +1,146 @@
Info<< "Reading velocity field U\n" << endl;
volVectorField U
(
IOobject
(
"U",
runTime.timeName(),
mesh,
IOobject::MUST_READ,
IOobject::AUTO_WRITE
),
mesh
);
// Initialise the velocity internal field to zero
U = dimensionedVector("0", U.dimensions(), Zero);
surfaceScalarField phi
(
IOobject
(
"phi",
runTime.timeName(),
mesh,
IOobject::NO_READ,
IOobject::AUTO_WRITE
),
fvc::flux(U)
);
if (args.optionFound("initialiseUBCs"))
{
U.correctBoundaryConditions();
phi = fvc::flux(U);
}
// Construct a pressure field
// If it is available read it otherwise construct from the velocity BCs
// converting fixed-value BCs to zero-gradient and vice versa.
word pName("p");
// Update name of the pressure field from the command-line option
args.optionReadIfPresent("pName", pName);
// Infer the pressure BCs from the velocity
wordList pBCTypes
(
U.boundaryField().size(),
fixedValueFvPatchScalarField::typeName
);
forAll(U.boundaryField(), patchi)
{
if (U.boundaryField()[patchi].fixesValue())
{
pBCTypes[patchi] = zeroGradientFvPatchScalarField::typeName;
}
}
// Note that registerObject is false for the pressure field. The pressure
// field in this solver doesn't have a physical value during the solution.
// It shouldn't be looked up and used by sub models or boundary conditions.
Info<< "Constructing pressure field " << pName << nl << endl;
volScalarField p
(
IOobject
(
pName,
runTime.timeName(),
mesh,
IOobject::READ_IF_PRESENT,
IOobject::NO_WRITE,
false
),
mesh,
dimensionedScalar(pName, sqr(dimVelocity), 0),
pBCTypes
);
// Infer the velocity potential BCs from the pressure
wordList PhiBCTypes
(
p.boundaryField().size(),
zeroGradientFvPatchScalarField::typeName
);
forAll(p.boundaryField(), patchi)
{
if (p.boundaryField()[patchi].fixesValue())
{
PhiBCTypes[patchi] = fixedValueFvPatchScalarField::typeName;
}
}
Info<< "Constructing velocity potential field Phi\n" << endl;
volScalarField Phi
(
IOobject
(
"Phi",
runTime.timeName(),
mesh,
IOobject::READ_IF_PRESENT,
IOobject::NO_WRITE
),
mesh,
dimensionedScalar("Phi", dimLength*dimVelocity, 0),
PhiBCTypes
);
label PhiRefCell = 0;
scalar PhiRefValue = 0;
setRefCell
(
Phi,
potentialFlow.dict(),
PhiRefCell,
PhiRefValue
);
mesh.setFluxRequired(Phi.name());
#include "createMRF.H"
// Add overset specific interpolations
{
dictionary oversetDict;
oversetDict.add("Phi", true);
oversetDict.add("U", true);
const_cast<dictionary&>
(
mesh.schemesDict()
).add
(
"oversetInterpolationRequired",
oversetDict,
true
);
}
// Mask field for zeroing out contributions on hole cells
#include "createCellMask.H"
// Create bool field with interpolated cells
#include "createInterpolatedCells.H"

260
applications/solvers/basic/potentialFoam/overPotentialFoam/potentialFoam.C Normal file
View File

@ -0,0 +1,260 @@
/*---------------------------------------------------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | Copyright (C) 2017 OpenCFD Ltd
\\/ M anipulation |
-------------------------------------------------------------------------------
License
This file is part of OpenFOAM.
OpenFOAM is free software: you can redistribute it and/or modify it
under the terms of the GNU General Public License as published by
the Free Software Foundation, either version 3 of the License, or
(at your option) any later version.
OpenFOAM is distributed in the hope that it will be useful, but WITHOUT
ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or
FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License
for more details.
You should have received a copy of the GNU General Public License
along with OpenFOAM. If not, see <http://www.gnu.org/licenses/>.
Application
potentialFoam
Group
grpBasicSolvers
Description
Potential flow solver which solves for the velocity potential, to
calculate the flux-field, from which the velocity field is obtained by
reconstructing the flux.
\heading Solver details
The potential flow solution is typically employed to generate initial fields
for full Navier-Stokes codes. The flow is evolved using the equation:
\f[
\laplacian \Phi = \div(\vec{U})
\f]
Where:
\vartable
\Phi | Velocity potential [m2/s]
\vec{U} | Velocity [m/s]
\endvartable
The corresponding pressure field could be calculated from the divergence
of the Euler equation:
\f[
\laplacian p + \div(\div(\vec{U}\otimes\vec{U})) = 0
\f]
but this generates excessive pressure variation in regions of large
velocity gradient normal to the flow direction. A better option is to
calculate the pressure field corresponding to velocity variation along the
stream-lines:
\f[
\laplacian p + \div(\vec{F}\cdot\div(\vec{U}\otimes\vec{U})) = 0
\f]
where the flow direction tensor \f$\vec{F}\f$ is obtained from
\f[
\vec{F} = \hat{\vec{U}}\otimes\hat{\vec{U}}
\f]
\heading Required fields
\plaintable
U | Velocity [m/s]
\endplaintable
\heading Optional fields
\plaintable
p | Kinematic pressure [m2/s2]
Phi | Velocity potential [m2/s]
| Generated from p (if present) or U if not present
\endplaintable
\heading Options
\plaintable
-writep | write the Euler pressure
-writePhi | Write the final velocity potential
-initialiseUBCs | Update the velocity boundaries before solving for Phi
\endplaintable
\*---------------------------------------------------------------------------*/
#include "fvCFD.H"
#include "pisoControl.H"
#include "dynamicFvMesh.H"
#include "cellCellStencilObject.H"
#include "localMin.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
int main(int argc, char *argv[])
{
argList::addOption
(
"pName",
"pName",
"Name of the pressure field"
);
argList::addBoolOption
(
"initialiseUBCs",
"Initialise U boundary conditions"
);
argList::addBoolOption
(
"writePhi",
"Write the final velocity potential field"
);
argList::addBoolOption
(
"writep",
"Calculate and write the Euler pressure field"
);
argList::addBoolOption
(
"withFunctionObjects",
"execute functionObjects"
);
#include "setRootCase.H"
#include "createTime.H"
#include "createNamedDynamicFvMesh.H"
pisoControl potentialFlow(mesh, "potentialFlow");
#include "createFields.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Info<< nl << "Calculating potential flow" << endl;
mesh.update();
surfaceScalarField faceMask(localMin<scalar>(mesh).interpolate(cellMask));
// Since solver contains no time loop it would never execute
// function objects so do it ourselves
runTime.functionObjects().start();
MRF.makeRelative(phi);
adjustPhi(phi, U, p);
// Non-orthogonal velocity potential corrector loop
while (potentialFlow.correct())
{
phi = fvc::flux(U);
while (potentialFlow.correctNonOrthogonal())
{
fvScalarMatrix PhiEqn
(
fvm::laplacian(faceMask, Phi)
==
fvc::div(phi)
);
PhiEqn.setReference(PhiRefCell, PhiRefValue);
PhiEqn.solve();
if (potentialFlow.finalNonOrthogonalIter())
{
phi -= PhiEqn.flux();
}
}
MRF.makeAbsolute(phi);
Info<< "Continuity error = "
<< mag(fvc::div(phi))().weightedAverage(mesh.V()).value()
<< endl;
U = fvc::reconstruct(phi);
U.correctBoundaryConditions();
Info<< "Interpolated velocity error = "
<< (sqrt(sum(sqr(fvc::flux(U) - phi)))/sum(mesh.magSf())).value()
<< endl;
}
// Write U and phi
U.write();
phi.write();
// Optionally write Phi
if (args.optionFound("writePhi"))
{
Phi.write();
}
// Calculate the pressure field from the Euler equation
if (args.optionFound("writep"))
{
Info<< nl << "Calculating approximate pressure field" << endl;
label pRefCell = 0;
scalar pRefValue = 0.0;
setRefCell
(
p,
potentialFlow.dict(),
pRefCell,
pRefValue
);
// Calculate the flow-direction filter tensor
volScalarField magSqrU(magSqr(U));
volSymmTensorField F(sqr(U)/(magSqrU + SMALL*average(magSqrU)));
// Calculate the divergence of the flow-direction filtered div(U*U)
// Filtering with the flow-direction generates a more reasonable
// pressure distribution in regions of high velocity gradient in the
// direction of the flow
volScalarField divDivUU
(
fvc::div
(
F & fvc::div(phi, U),
"div(div(phi,U))"
)
);
// Solve a Poisson equation for the approximate pressure
while (potentialFlow.correctNonOrthogonal())
{
fvScalarMatrix pEqn
(
fvm::laplacian(p) + divDivUU
);
pEqn.setReference(pRefCell, pRefValue);
pEqn.solve();
}
p.write();
}
runTime.functionObjects().end();
Info<< "ExecutionTime = " << runTime.elapsedCpuTime() << " s"
<< " ClockTime = " << runTime.elapsedClockTime() << " s"
<< nl << endl;
Info<< "End\n" << endl;
return 0;
}
// ************************************************************************* //

3
applications/solvers/compressible/rhoSimpleFoam/overRhoSimpleFoam/Make/files Normal file
View File

@ -0,0 +1,3 @@
rhoSimpleFoam.C
EXE = $(FOAM_APPBIN)/overRhoSimpleFoam

27
applications/solvers/compressible/rhoSimpleFoam/overRhoSimpleFoam/Make/options Normal file
View File

@ -0,0 +1,27 @@
EXE_INC = \
-I.. \
-I$(LIB_SRC)/transportModels/compressible/lnInclude \
-I$(LIB_SRC)/thermophysicalModels/basic/lnInclude \
-I$(LIB_SRC)/TurbulenceModels/turbulenceModels/lnInclude \
-I$(LIB_SRC)/TurbulenceModels/compressible/lnInclude \
-I$(LIB_SRC)/finiteVolume/cfdTools \
-I$(LIB_SRC)/finiteVolume/lnInclude \
-I$(LIB_SRC)/sampling/lnInclude \
-I$(LIB_SRC)/dynamicFvMesh/lnInclude \
-I$(LIB_SRC)/dynamicMesh/lnInclude \
-I$(LIB_SRC)/meshTools/lnInclude \
-I$(LIB_SRC)/overset/lnInclude
EXE_LIBS = \
-lcompressibleTransportModels \
-lfluidThermophysicalModels \
-lspecie \
-lturbulenceModels \
-lcompressibleTurbulenceModels \
-lfiniteVolume \
-lsampling \
-lmeshTools \
-lfvOptions \
-loverset \
-ldynamicFvMesh \
-ltopoChangerFvMesh

23
applications/solvers/compressible/rhoSimpleFoam/overRhoSimpleFoam/UEqn.H Normal file
View File

@ -0,0 +1,23 @@
// Solve the Momentum equation
MRF.correctBoundaryVelocity(U);
tmp<fvVectorMatrix> tUEqn
(
fvm::div(phi, U)
+ MRF.DDt(rho, U)
+ turbulence->divDevRhoReff(U)
==
fvOptions(rho, U)
);
fvVectorMatrix& UEqn = tUEqn.ref();
UEqn.relax();
fvOptions.constrain(UEqn);
if (simple.momentumPredictor())
{
solve(UEqn == -cellMask*fvc::grad(p));
}
fvOptions.correct(U);

1
applications/solvers/compressible/rhoSimpleFoam/overRhoSimpleFoam/createFieldRefs.H Normal file
View File

@ -0,0 +1 @@
const volScalarField& psi = thermo.psi();

91
applications/solvers/compressible/rhoSimpleFoam/overRhoSimpleFoam/createFields.H Normal file
View File

@ -0,0 +1,91 @@
Info<< "Reading thermophysical properties\n" << endl;
autoPtr<fluidThermo> pThermo
(
fluidThermo::New(mesh)
);
fluidThermo& thermo = pThermo();
thermo.validate(args.executable(), "h", "e");
volScalarField& p = thermo.p();
volScalarField rho
(
IOobject
(
"rho",
runTime.timeName(),
mesh,
IOobject::READ_IF_PRESENT,
IOobject::AUTO_WRITE
),
thermo.rho()
);
Info<< "Reading field U\n" << endl;
volVectorField U
(
IOobject
(
"U",
runTime.timeName(),
mesh,
IOobject::MUST_READ,
IOobject::AUTO_WRITE
),
mesh
);
#include "compressibleCreatePhi.H"
pressureControl pressureControl(p, rho, simple.dict());
mesh.setFluxRequired(p.name());
Info<< "Creating turbulence model\n" << endl;
autoPtr<compressible::turbulenceModel> turbulence
(
compressible::turbulenceModel::New
(
rho,
U,
phi,
thermo
)
);
dimensionedScalar initialMass = fvc::domainIntegrate(rho);
#include "createMRF.H"
//- Overset specific
// Add solver-specific interpolations
{
dictionary oversetDict;
oversetDict.add("U", true);
oversetDict.add("p", true);
oversetDict.add("HbyA", true);
oversetDict.add("grad(p)", true);
oversetDict.add("rho", true);
const_cast<dictionary&>
(
mesh.schemesDict()
).add
(
"oversetInterpolationRequired",
oversetDict,
true
);
}
// Mask field for zeroing out contributions on hole cells
#include "createCellMask.H"
#include "createInterpolatedCells.H"
bool adjustFringe
(
simple.dict().lookupOrDefault("oversetAdjustPhi", false)
);

22
applications/solvers/compressible/rhoSimpleFoam/overRhoSimpleFoam/createUpdatedDynamicFvMesh.H Normal file
View File

@ -0,0 +1,22 @@
Info<< "Create dynamic mesh for time = "
<< runTime.timeName() << nl << endl;
autoPtr<dynamicFvMesh> meshPtr
(
dynamicFvMesh::New
(
IOobject
(
dynamicFvMesh::defaultRegion,
runTime.timeName(),
runTime,
IOobject::MUST_READ
)
)
);
dynamicFvMesh& mesh = meshPtr();
// Calculate initial mesh-to-mesh mapping. Note that this should be
// done under the hood, e.g. as a MeshObject
mesh.update();

123
applications/solvers/compressible/rhoSimpleFoam/overRhoSimpleFoam/pEqn.H Normal file
View File

@ -0,0 +1,123 @@
{
surfaceScalarField faceMask(localMin<scalar>(mesh).interpolate(cellMask));
volScalarField rAU(1.0/UEqn.A());
surfaceScalarField rhorAUf("rhorAUf", faceMask*fvc::interpolate(rho*rAU));
volVectorField HbyA("HbyA", U);
HbyA = constrainHbyA(cellMask*rAU*UEqn.H(), U, p);
tUEqn.clear();
bool closedVolume = false;
surfaceScalarField phiHbyA("phiHbyA", fvc::interpolate(rho)*fvc::flux(HbyA));
MRF.makeRelative(fvc::interpolate(rho), phiHbyA);
// Update the pressure BCs to ensure flux consistency
constrainPressure(p, rho, U, phiHbyA, rhorAUf, MRF);
if (simple.transonic())
{
surfaceScalarField phid
(
"phid",
(fvc::interpolate(psi)/fvc::interpolate(rho))*phiHbyA
);
phiHbyA -= fvc::interpolate(psi*p)*phiHbyA/fvc::interpolate(rho);
while (simple.correctNonOrthogonal())
{
fvScalarMatrix pEqn
(
fvc::div(phiHbyA)
+ fvm::div(phid, p)
- fvm::laplacian(rhorAUf, p)
==
fvOptions(psi, p, rho.name())
);
// Relax the pressure equation to ensure diagonal-dominance
pEqn.relax();
pEqn.setReference
(
pressureControl.refCell(),
pressureControl.refValue()
);
pEqn.solve();
if (simple.finalNonOrthogonalIter())
{
phi = phiHbyA + pEqn.flux();
}
}
}
else
{
closedVolume = adjustPhi(phiHbyA, U, p);
if (adjustFringe)
{
oversetAdjustPhi(phiHbyA, U);
}
while (simple.correctNonOrthogonal())
{
fvScalarMatrix pEqn
(
fvc::div(phiHbyA)
- fvm::laplacian(rhorAUf, p)
==
fvOptions(psi, p, rho.name())
);
pEqn.setReference
(
pressureControl.refCell(),
pressureControl.refValue()
);
pEqn.solve();
if (simple.finalNonOrthogonalIter())
{
phi = phiHbyA + pEqn.flux();
}
}
}
#include "incompressible/continuityErrs.H"
// Explicitly relax pressure for momentum corrector
p.relax();
volVectorField gradP(fvc::grad(p));
U = HbyA - rAU*cellMask*gradP;
U.correctBoundaryConditions();
fvOptions.correct(U);
bool pLimited = pressureControl.limit(p);
// For closed-volume cases adjust the pressure and density levels
// to obey overall mass continuity
if (closedVolume)
{
p += (initialMass - fvc::domainIntegrate(psi*p))
/fvc::domainIntegrate(psi);
}
if (pLimited || closedVolume)
{
p.correctBoundaryConditions();
}
rho = thermo.rho();
if (!simple.transonic())
{
rho.relax();
}
}

92
applications/solvers/compressible/rhoSimpleFoam/overRhoSimpleFoam/rhoSimpleFoam.C Normal file
View File

@ -0,0 +1,92 @@
/*---------------------------------------------------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | Copyright (C) 2017 OpenCFD Ltd
\\/ M anipulation |
-------------------------------------------------------------------------------
License
This file is part of OpenFOAM.
OpenFOAM is free software: you can redistribute it and/or modify it
under the terms of the GNU General Public License as published by
the Free Software Foundation, either version 3 of the License, or
(at your option) any later version.
OpenFOAM is distributed in the hope that it will be useful, but WITHOUT
ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or
FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License
for more details.
You should have received a copy of the GNU General Public License
along with OpenFOAM. If not, see <http://www.gnu.org/licenses/>.
Application
overRhoSimpleFoam
Group
grpCompressibleSolvers
Description
Overset steady-state solver for turbulent flow of compressible fluids.
\*---------------------------------------------------------------------------*/
#include "fvCFD.H"
#include "dynamicFvMesh.H"
#include "fluidThermo.H"
#include "turbulentFluidThermoModel.H"
#include "simpleControl.H"
#include "pressureControl.H"
#include "fvOptions.H"
#include "cellCellStencilObject.H"
#include "localMin.H"
#include "oversetAdjustPhi.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
int main(int argc, char *argv[])
{
#define CREATE_MESH createUpdatedDynamicFvMesh.H
#include "postProcess.H"
#include "setRootCase.H"
#include "createTime.H"
#include "createUpdatedDynamicFvMesh.H"
#include "createControl.H"
#include "createFields.H"
#include "createFieldRefs.H"
#include "createFvOptions.H"
#include "initContinuityErrs.H"
turbulence->validate();
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Info<< "\nStarting time loop\n" << endl;
while (simple.loop())
{
Info<< "Time = " << runTime.timeName() << nl << endl;
// Pressure-velocity SIMPLE corrector
#include "UEqn.H"
#include "EEqn.H"
#include "pEqn.H"
turbulence->correct();
runTime.write();
Info<< "ExecutionTime = " << runTime.elapsedCpuTime() << " s"
<< " ClockTime = " << runTime.elapsedClockTime() << " s"
<< nl << endl;
}
Info<< "End\n" << endl;
return 0;
}
// ************************************************************************* //

11
tutorials/basic/overPotentialFoam/cylinder/Allclean Executable file
View File

@ -0,0 +1,11 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
# Extrude mesh around cylinder
(cd cylinderAndBackground && ./Allclean)
# Add background mesh
(cd cylinderMesh && foamCleanTutorials)
# ----------------------------------------------------------------- end-of-file

8
tutorials/basic/overPotentialFoam/cylinder/Allrun Executable file
View File

@ -0,0 +1,8 @@
#!/bin/sh
. $WM_PROJECT_DIR/bin/tools/RunFunctions
# Extrude mesh around cylinder
(cd cylinderMesh && ./Allrun.pre)
# Add background mesh
(cd cylinderAndBackground && ./Allrun)

8
tutorials/basic/overPotentialFoam/cylinder/Allrun.pre Executable file
View File

@ -0,0 +1,8 @@
#!/bin/sh
. $WM_PROJECT_DIR/bin/tools/RunFunctions
# Extrude mesh around cylinder
(cd cylinderMesh && ./Allrun.pre)
# Add background mesh
(cd cylinderAndBackground && ./Allrun.pre)

57
tutorials/basic/overPotentialFoam/cylinder/cylinderAndBackground/0.orig/U Normal file
View File

@ -0,0 +1,57 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volVectorField;
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
#include "include/initialConditions"
dimensions [0 1 -1 0 0 0 0];
internalField uniform $flowVelocity;
boundaryField
{
#includeEtc "caseDicts/setConstraintTypes"
overset
{
type overset;
}
walls
{
type movingWallVelocity;
value uniform (0 0 0);
}
inlet
{
type fixedValue;
value $internalField;
}
outlet
{
type inletOutlet;
inletValue uniform (0 0 0);
value $internalField;
}
topAndBottom
{
type zeroGradient;
}
}
// ************************************************************************* //

15
tutorials/basic/overPotentialFoam/cylinder/cylinderAndBackground/0.orig/include/fixedInlet Normal file
View File

@ -0,0 +1,15 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
inlet
{
type fixedValue;
value $internalField;
}
// ************************************************************************* //

13
tutorials/basic/overPotentialFoam/cylinder/cylinderAndBackground/0.orig/include/initialConditions Normal file
View File

@ -0,0 +1,13 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
flowVelocity (1 0 0);
pressure 0;
#inputMode merge
// ************************************************************************* //

54
tutorials/basic/overPotentialFoam/cylinder/cylinderAndBackground/0.orig/p Normal file
View File

@ -0,0 +1,54 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object p;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
#include "include/initialConditions"
dimensions [0 2 -2 0 0 0 0];
internalField uniform $pressure;
boundaryField
{
#includeEtc "caseDicts/setConstraintTypes"
overset
{
type overset;
}
wall
{
type zeroGradient;
}
inlet
{
type zeroGradient;
}
outlet
{
type fixedValue; //calculated;
value $internalField;
}
".*"
{
type zeroGradient;
}
}
// ************************************************************************* //

42
tutorials/basic/overPotentialFoam/cylinder/cylinderAndBackground/0.orig/pointDisplacement Normal file
View File

@ -0,0 +1,42 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class pointVectorField;
object pointDisplacement;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 0 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
overset
{
patchType overset;
type zeroGradient;
}
walls
{
type uniformFixedValue;
uniformValue (0 0 0);
}
".*"
{
type uniformFixedValue;
uniformValue (0 0 0);
}
}
// ************************************************************************* //

36
tutorials/basic/overPotentialFoam/cylinder/cylinderAndBackground/0.orig/zoneID Normal file
View File

@ -0,0 +1,36 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object zoneID;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0;
boundaryField
{
#includeEtc "caseDicts/setConstraintTypes"
overset
{
type overset;
}
".*"
{
type zeroGradient;
}
}
// ************************************************************************* //

12
tutorials/basic/overPotentialFoam/cylinder/cylinderAndBackground/Allclean Executable file
View File

@ -0,0 +1,12 @@
#!/bin/sh
cd ${0%/*} || exit 1 # Run from this directory
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
cleanCase
rm -f constant/polyMesh/boundary
rm -f constant/polyMesh/zoneID
rm -f constant/cellInterpolationWeight
rm -rf 0
#------------------------------------------------------------------------------

10
tutorials/basic/overPotentialFoam/cylinder/cylinderAndBackground/Allrun Executable file
View File

@ -0,0 +1,10 @@
#!/bin/sh
cd ${0%/*} || exit 1 # Run from this directory
. $WM_PROJECT_DIR/bin/tools/RunFunctions
./Allrun.pre
# Run it for a bit
runApplication $(getApplication)
#------------------------------------------------------------------------------

22
tutorials/basic/overPotentialFoam/cylinder/cylinderAndBackground/Allrun.pre Executable file
View File

@ -0,0 +1,22 @@
#!/bin/sh
cd ${0%/*} || exit 1 # Run from this directory
. $WM_PROJECT_DIR/bin/tools/RunFunctions
# Create background mesh
runApplication blockMesh
# Add the cylinder mesh
runApplication mergeMeshes . ../cylinderMesh -overwrite
## Make it a bit smaller to keep it laminar
#runApplication transformPoints -scale '(0.001 0.001 0.001)'
# Select cellSets for the different zones
runApplication topoSet
restore0Dir
# Use cellSets to write zoneID
runApplication setFields
#------------------------------------------------------------------------------

33
tutorials/basic/overPotentialFoam/cylinder/cylinderAndBackground/constant/dynamicMeshDict Normal file
View File

@ -0,0 +1,33 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object dynamicMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
motionSolverLibs ( "libfvMotionSolvers.so" );
solver displacementLaplacian;
displacementLaplacianCoeffs
{
diffusivity uniform 1;
}
dynamicFvMesh dynamicOversetFvMesh;
dynamicOversetFvMeshCoeffs
{
// layerRelax 0.3;
}
// ************************************************************************* //

83
tutorials/basic/overPotentialFoam/cylinder/cylinderAndBackground/system/blockMeshDict Normal file
View File

@ -0,0 +1,83 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object blockMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
convertToMeters 1;
vertices
(
(-2 -0.05 -2.0)
( 2 -0.05 -2.0)
( 2 0.05 -2.0)
(-2 0.05 -2.0)
(-2 -0.05 2.0)
( 2 -0.05 2.0)
( 2 0.05 2.0)
(-2 0.05 2.0)
);
blocks
(
hex (0 1 2 3 4 5 6 7) (80 1 60) simpleGrading (1 1 1)
);
edges
(
);
boundary
(
topAndBottom
{
type patch;
faces
(
(4 5 6 7)
(0 3 2 1)
);
}
inlet
{
type patch;
faces
(
(0 4 7 3)
);
}
outlet
{
type patch;
faces
(
(2 6 5 1)
);
}
frontAndBack
{
type empty;
faces
(
(3 7 6 2)
(1 5 4 0)
);
}
);
// ************************************************************************* //

51
tutorials/basic/overPotentialFoam/cylinder/cylinderAndBackground/system/controlDict Normal file
View File

@ -0,0 +1,51 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// Make sure all preprocessing tools know about the 'overset' bc
libs ("liboverset.so");
application overPotentialFoam;
startFrom startTime;
startTime 0;
stopAt nextWrite;
endTime 2;
deltaT 1;
writeControl timeStep;
writeInterval 2;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
writeCompression off;
timeFormat general;
timePrecision 6;
runTimeModifiable true;
// ************************************************************************* //

57
tutorials/basic/overPotentialFoam/cylinder/cylinderAndBackground/system/fvSchemes Normal file
View File

@ -0,0 +1,57 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default steadyState;
}
gradSchemes
{
default leastSquares;
}
divSchemes
{
default none;
div(phi,U) bounded Gauss linear;
div(div(phi,U)) Gauss linear;
}
laplacianSchemes
{
default Gauss linear corrected;
}
interpolationSchemes
{
default linear;
}
snGradSchemes
{
default corrected;
}
oversetInterpolation
{
method leastSquares;//inverseDistanc;
}
// ************************************************************************* //

54
tutorials/basic/overPotentialFoam/cylinder/cylinderAndBackground/system/fvSolution Normal file
View File

@ -0,0 +1,54 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
cellDisplacement
{
solver PCG;
preconditioner DIC;
tolerance 1e-06;
relTol 0;
maxIter 100;
}
Phi
{
solver PBiCGStab;
preconditioner DILU;
tolerance 1e-6;
relTol 0.01;
}
p
{
$Phi;
}
}
potentialFlow
{
nNonOrthogonalCorrectors 3;
nCorrectors 3;
}
// ************************************************************************* //

48
tutorials/basic/overPotentialFoam/cylinder/cylinderAndBackground/system/setFieldsDict Normal file
View File

@ -0,0 +1,48 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object setFieldsDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
defaultFieldValues
(
volScalarFieldValue zoneID 123
);
regions
(
// Set cell values
// (does zerogradient on boundaries)
cellToCell
{
set c0;
fieldValues
(
volScalarFieldValue zoneID 0
);
}
cellToCell
{
set c1;
fieldValues
(
volScalarFieldValue zoneID 1
);
}
);
// ************************************************************************* //

48
tutorials/basic/overPotentialFoam/cylinder/cylinderAndBackground/system/topoSetDict Normal file
View File

@ -0,0 +1,48 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object topoSetDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
actions
(
{
name c0;
type cellSet;
action new;
source regionToCell;
sourceInfo
{
insidePoints ((-1.999 0 -1.999));
}
}
{
name c1;
type cellSet;
action new;
source cellToCell;
sourceInfo
{
set c0;
}
}
{
name c1;
type cellSet;
action invert;
}
);
// ************************************************************************* //

8
tutorials/basic/overPotentialFoam/cylinder/cylinderMesh/Allrun.pre Executable file
View File

@ -0,0 +1,8 @@
#!/bin/sh
. $WM_PROJECT_DIR/bin/tools/RunFunctions
# Generate mesh from surface (in constant/triSurface)
runApplication extrudeMesh
# Make front and back type empty
runApplication createPatch -overwrite

221
tutorials/basic/overPotentialFoam/cylinder/cylinderMesh/constant/triSurface/cylinder.vtk Normal file
View File

@ -0,0 +1,221 @@
# vtk DataFile Version 4.0
vtk output
ASCII
DATASET POLYDATA
POINTS 150 float
0.5 0.05 0 0.5 -0.05 0 0.498246 0.05 -0.0418389
0.498246 -0.05 -0.0418389 0.492998 0.05 -0.0833844 0.492998 -0.05 -0.0833844
0.484292 0.05 -0.124345 0.484292 -0.05 -0.124345 0.472188 0.05 -0.164433
0.472188 -0.05 -0.164433 0.456773 0.05 -0.203368 0.456773 -0.05 -0.203368
0.438153 0.05 -0.240877 0.438153 -0.05 -0.240877 0.416461 0.05 -0.276696
0.416461 -0.05 -0.276696 0.391847 0.05 -0.310574 0.391847 -0.05 -0.310574
0.364484 0.05 -0.342274 0.364484 -0.05 -0.342274 0.334565 0.05 -0.371572
0.334565 -0.05 -0.371572 0.3023 0.05 -0.398265 0.3023 -0.05 -0.398265
0.267913 0.05 -0.422164 0.267913 -0.05 -0.422164 0.231648 0.05 -0.443102
0.231648 -0.05 -0.443102 0.193758 0.05 -0.460932 0.193758 -0.05 -0.460932
0.154509 0.05 -0.475528 0.154509 -0.05 -0.475528 0.114175 0.05 -0.486789
0.114175 -0.05 -0.486789 0.0730415 0.05 -0.494636 0.0730415 -0.05 -0.494636
0.0313953 0.05 -0.499013 0.0313953 -0.05 -0.499013 -0.0104712 0.05 -0.49989
-0.0104712 -0.05 -0.49989 -0.0522642 0.05 -0.497261 -0.0522642 -0.05 -0.497261
-0.0936907 0.05 -0.491144 -0.0936907 -0.05 -0.491144 -0.13446 0.05 -0.481581
-0.13446 -0.05 -0.481581 -0.174286 0.05 -0.468641 -0.174286 -0.05 -0.468641
-0.21289 0.05 -0.452414 -0.21289 -0.05 -0.452414 -0.25 0.05 -0.433013
-0.25 -0.05 -0.433013 -0.285357 0.05 -0.410575 -0.285357 -0.05 -0.410575
-0.318712 0.05 -0.385257 -0.318712 -0.05 -0.385257 -0.349832 0.05 -0.357236
-0.349832 -0.05 -0.357236 -0.378498 0.05 -0.32671 -0.378498 -0.05 -0.32671
-0.404509 0.05 -0.293893 -0.404509 -0.05 -0.293893 -0.427682 0.05 -0.259014
-0.427682 -0.05 -0.259014 -0.447856 0.05 -0.222318 -0.447856 -0.05 -0.222318
-0.464888 0.05 -0.184062 -0.464888 -0.05 -0.184062 -0.47866 0.05 -0.144516
-0.47866 -0.05 -0.144516 -0.489074 0.05 -0.103956 -0.489074 -0.05 -0.103956
-0.496057 0.05 -0.0626666 -0.496057 -0.05 -0.0626666 -0.499561 0.05 -0.0209378
-0.499561 -0.05 -0.0209378 -0.499561 0.05 0.0209378 -0.499561 -0.05 0.0209378
-0.496057 0.05 0.0626666 -0.496057 -0.05 0.0626666 -0.489074 0.05 0.103956
-0.489074 -0.05 0.103956 -0.47866 0.05 0.144516 -0.47866 -0.05 0.144516
-0.464888 0.05 0.184062 -0.464888 -0.05 0.184062 -0.447856 0.05 0.222318
-0.447856 -0.05 0.222318 -0.427682 0.05 0.259014 -0.427682 -0.05 0.259014
-0.404509 0.05 0.293893 -0.404509 -0.05 0.293893 -0.378498 0.05 0.32671
-0.378498 -0.05 0.32671 -0.349832 0.05 0.357236 -0.349832 -0.05 0.357236
-0.318712 0.05 0.385257 -0.318712 -0.05 0.385257 -0.285357 0.05 0.410575
-0.285357 -0.05 0.410575 -0.25 0.05 0.433013 -0.25 -0.05 0.433013
-0.21289 0.05 0.452414 -0.21289 -0.05 0.452414 -0.174286 0.05 0.468641
-0.174286 -0.05 0.468641 -0.13446 0.05 0.481581 -0.13446 -0.05 0.481581
-0.0936907 0.05 0.491144 -0.0936907 -0.05 0.491144 -0.0522642 0.05 0.497261
-0.0522642 -0.05 0.497261 -0.0104712 0.05 0.49989 -0.0104712 -0.05 0.49989
0.0313953 0.05 0.499013 0.0313953 -0.05 0.499013 0.0730415 0.05 0.494636
0.0730415 -0.05 0.494636 0.114175 0.05 0.486789 0.114175 -0.05 0.486789
0.154509 0.05 0.475528 0.154509 -0.05 0.475528 0.193758 0.05 0.460932
0.193758 -0.05 0.460932 0.231648 0.05 0.443102 0.231648 -0.05 0.443102
0.267913 0.05 0.422164 0.267913 -0.05 0.422164 0.3023 0.05 0.398265
0.3023 -0.05 0.398265 0.334565 0.05 0.371572 0.334565 -0.05 0.371572
0.364484 0.05 0.342274 0.364484 -0.05 0.342274 0.391847 0.05 0.310574
0.391847 -0.05 0.310574 0.416461 0.05 0.276696 0.416461 -0.05 0.276696
0.438153 0.05 0.240877 0.438153 -0.05 0.240877 0.456773 0.05 0.203368
0.456773 -0.05 0.203368 0.472188 0.05 0.164433 0.472188 -0.05 0.164433
0.484292 0.05 0.124345 0.484292 -0.05 0.124345 0.492998 0.05 0.0833844
0.492998 -0.05 0.0833844 0.498246 0.05 0.0418389 0.498246 -0.05 0.0418389
POLYGONS 75 375
4 0 1 3 2
4 2 3 5 4
4 4 5 7 6
4 6 7 9 8
4 8 9 11 10
4 10 11 13 12
4 12 13 15 14
4 14 15 17 16
4 16 17 19 18
4 18 19 21 20
4 20 21 23 22
4 22 23 25 24
4 24 25 27 26
4 26 27 29 28
4 28 29 31 30
4 30 31 33 32
4 32 33 35 34
4 34 35 37 36
4 36 37 39 38
4 38 39 41 40
4 40 41 43 42
4 42 43 45 44
4 44 45 47 46
4 46 47 49 48
4 48 49 51 50
4 50 51 53 52
4 52 53 55 54
4 54 55 57 56
4 56 57 59 58
4 58 59 61 60
4 60 61 63 62
4 62 63 65 64
4 64 65 67 66
4 66 67 69 68
4 68 69 71 70
4 70 71 73 72
4 72 73 75 74
4 74 75 77 76
4 76 77 79 78
4 78 79 81 80
4 80 81 83 82
4 82 83 85 84
4 84 85 87 86
4 86 87 89 88
4 88 89 91 90
4 90 91 93 92
4 92 93 95 94
4 94 95 97 96
4 96 97 99 98
4 98 99 101 100
4 100 101 103 102
4 102 103 105 104
4 104 105 107 106
4 106 107 109 108
4 108 109 111 110
4 110 111 113 112
4 112 113 115 114
4 114 115 117 116
4 116 117 119 118
4 118 119 121 120
4 120 121 123 122
4 122 123 125 124
4 124 125 127 126
4 126 127 129 128
4 128 129 131 130
4 130 131 133 132
4 132 133 135 134
4 134 135 137 136
4 136 137 139 138
4 138 139 141 140
4 140 141 143 142
4 142 143 145 144
4 144 145 147 146
4 146 147 149 148
4 148 149 1 0
POINT_DATA 150
NORMALS Normals float
1 0 -0 1 0 -0 0.996493 0 -0.0836778
0.996493 0 -0.0836778 0.985996 0 -0.166769 0.985996 0 -0.166769
0.968583 0 -0.24869 0.968583 0 -0.24869 0.944376 0 -0.328867
0.944376 0 -0.328867 0.913545 0 -0.406737 0.913545 0 -0.406737
0.876307 0 -0.481754 0.876307 0 -0.481754 0.832921 0 -0.553392
0.832921 0 -0.553392 0.783693 0 -0.621148 0.783693 0 -0.621148
0.728969 0 -0.684547 0.728969 0 -0.684547 0.669131 0 -0.743145
0.669131 0 -0.743145 0.604599 0 -0.79653 0.604599 0 -0.79653
0.535827 0 -0.844328 0.535827 0 -0.844328 0.463296 0 -0.886204
0.463296 0 -0.886204 0.387516 0 -0.921863 0.387516 0 -0.921863
0.309017 0 -0.951057 0.309017 0 -0.951057 0.228351 0 -0.973579
0.228351 0 -0.973579 0.146083 0 -0.989272 0.146083 0 -0.989272
0.0627905 0 -0.998027 0.0627905 0 -0.998027 -0.0209424 0 -0.999781
-0.0209424 0 -0.999781 -0.104528 0 -0.994522 -0.104528 0 -0.994522
-0.187381 0 -0.982287 -0.187381 0 -0.982287 -0.26892 0 -0.963163
-0.26892 0 -0.963163 -0.348572 0 -0.937282 -0.348572 0 -0.937282
-0.425779 0 -0.904827 -0.425779 0 -0.904827 -0.5 0 -0.866025
-0.5 0 -0.866025 -0.570714 0 -0.821149 -0.570714 0 -0.821149
-0.637424 0 -0.770513 -0.637424 0 -0.770513 -0.699663 0 -0.714473
-0.699663 0 -0.714473 -0.756995 0 -0.653421 -0.756995 0 -0.653421
-0.809017 0 -0.587785 -0.809017 0 -0.587785 -0.855364 0 -0.518027
-0.855364 0 -0.518027 -0.895712 0 -0.444635 -0.895712 0 -0.444635
-0.929776 0 -0.368125 -0.929776 0 -0.368125 -0.957319 0 -0.289032
-0.957319 0 -0.289032 -0.978148 0 -0.207912 -0.978148 0 -0.207912
-0.992115 0 -0.125333 -0.992115 0 -0.125333 -0.999123 0 -0.0418757
-0.999123 0 -0.0418757 -0.999123 0 0.0418757 -0.999123 0 0.0418757
-0.992115 0 0.125333 -0.992115 0 0.125333 -0.978148 0 0.207912
-0.978148 0 0.207912 -0.957319 0 0.289032 -0.957319 0 0.289032
-0.929776 0 0.368125 -0.929776 0 0.368125 -0.895712 0 0.444635
-0.895712 0 0.444635 -0.855364 0 0.518027 -0.855364 0 0.518027
-0.809017 0 0.587785 -0.809017 0 0.587785 -0.756995 0 0.653421
-0.756995 0 0.653421 -0.699663 0 0.714473 -0.699663 0 0.714473
-0.637424 0 0.770513 -0.637424 0 0.770513 -0.570714 0 0.821149
-0.570714 0 0.821149 -0.5 0 0.866025 -0.5 0 0.866025
-0.425779 0 0.904827 -0.425779 0 0.904827 -0.348572 0 0.937282
-0.348572 0 0.937282 -0.26892 0 0.963163 -0.26892 0 0.963163
-0.187381 0 0.982287 -0.187381 0 0.982287 -0.104528 0 0.994522
-0.104528 0 0.994522 -0.0209424 0 0.999781 -0.0209424 0 0.999781
0.0627905 0 0.998027 0.0627905 0 0.998027 0.146083 0 0.989272
0.146083 0 0.989272 0.228351 0 0.973579 0.228351 0 0.973579
0.309017 0 0.951057 0.309017 0 0.951057 0.387516 0 0.921863
0.387516 0 0.921863 0.463296 0 0.886204 0.463296 0 0.886204
0.535827 0 0.844328 0.535827 0 0.844328 0.604599 0 0.79653
0.604599 0 0.79653 0.669131 0 0.743145 0.669131 0 0.743145
0.728969 0 0.684547 0.728969 0 0.684547 0.783693 0 0.621148
0.783693 0 0.621148 0.832921 0 0.553392 0.832921 0 0.553392
0.876307 0 0.481754 0.876307 0 0.481754 0.913545 0 0.406737
0.913545 0 0.406737 0.944376 0 0.328867 0.944376 0 0.328867
0.968583 0 0.24869 0.968583 0 0.24869 0.985996 0 0.166769
0.985996 0 0.166769 0.996493 0 0.0836778 0.996493 0 0.0836778
TEXTURE_COORDINATES TCoords 2 float
1 0 1 1 0.973333 0 0.973333 1 0.946667
0 0.946667 1 0.92 0 0.92 1 0.893333 0
0.893333 1 0.866667 0 0.866667 1 0.84 0 0.84
1 0.813333 0 0.813333 1 0.786667 0 0.786667 1
0.76 0 0.76 1 0.733333 0 0.733333 1 0.706667
0 0.706667 1 0.68 0 0.68 1 0.653333 0
0.653333 1 0.626667 0 0.626667 1 0.6 0 0.6
1 0.573333 0 0.573333 1 0.546667 0 0.546667 1
0.52 0 0.52 1 0.493333 0 0.493333 1 0.466667
0 0.466667 1 0.44 0 0.44 1 0.413333 0
0.413333 1 0.386667 0 0.386667 1 0.36 0 0.36
1 0.333333 0 0.333333 1 0.306667 0 0.306667 1
0.28 0 0.28 1 0.253333 0 0.253333 1 0.226667
0 0.226667 1 0.2 0 0.2 1 0.173333 0
0.173333 1 0.146667 0 0.146667 1 0.12 0 0.12
1 0.0933333 0 0.0933333 1 0.0666667 0 0.0666667 1
0.04 0 0.04 1 0.0133333 0 0.0133333 1 0.0133333
0 0.0133333 1 0.04 0 0.04 1 0.0666667 0
0.0666667 1 0.0933333 0 0.0933333 1 0.12 0 0.12
1 0.146667 0 0.146667 1 0.173333 0 0.173333 1
0.2 0 0.2 1 0.226667 0 0.226667 1 0.253333
0 0.253333 1 0.28 0 0.28 1 0.306667 0
0.306667 1 0.333333 0 0.333333 1 0.36 0 0.36
1 0.386667 0 0.386667 1 0.413333 0 0.413333 1
0.44 0 0.44 1 0.466667 0 0.466667 1 0.493333
0 0.493333 1 0.52 0 0.52 1 0.546667 0
0.546667 1 0.573333 0 0.573333 1 0.6 0 0.6
1 0.626667 0 0.626667 1 0.653333 0 0.653333 1
0.68 0 0.68 1 0.706667 0 0.706667 1 0.733333
0 0.733333 1 0.76 0 0.76 1 0.786667 0
0.786667 1 0.813333 0 0.813333 1 0.84 0 0.84
1 0.866667 0 0.866667 1 0.893333 0 0.893333 1
0.92 0 0.92 1 0.946667 0 0.946667 1 0.973333
0 0.973333 1

50
tutorials/basic/overPotentialFoam/cylinder/cylinderMesh/system/controlDict Normal file
View File

@ -0,0 +1,50 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application snappyHexMesh;
startFrom latestTime;
startTime 0;
stopAt endTime;
endTime 100;
deltaT 1;
writeControl runTime;
writeInterval 1;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
writeCompression off;
timeFormat general;
timePrecision 6;
runTimeModifiable true;
}
// ************************************************************************* //

84
tutorials/basic/overPotentialFoam/cylinder/cylinderMesh/system/createPatchDict Normal file
View File

@ -0,0 +1,84 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object createPatchDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
pointSync false;
// Patches to create.
patches
(
{
// Name of new patch
name oversetPatch;
// Dictionary to construct new patch from
patchInfo
{
type overset;
}
// How to construct: either from 'patches' or 'set'
constructFrom patches;
// If constructFrom = patches : names of patches. Wildcards allowed.
patches (otherSide);
// If constructFrom = set : name of faceSet
set f0;
}
{
// Name of new patch
name walls;
// Dictionary to construct new patch from
patchInfo
{
type wall;
}
// How to construct: either from 'patches' or 'set'
constructFrom patches;
// If constructFrom = patches : names of patches. Wildcards allowed.
patches (originalPatch);
// If constructFrom = set : name of faceSet
set f0;
}
{
// Name of new patch
name frontAndBack;
// Dictionary to construct new patch from
patchInfo
{
type empty;
}
// How to construct: either from 'patches' or 'set'
constructFrom patches;
// If constructFrom = patches : names of patches. Wildcards allowed.
patches (sides);
// If constructFrom = set : name of faceSet
set f0;
}
);
// ************************************************************************* //

136
tutorials/basic/overPotentialFoam/cylinder/cylinderMesh/system/extrudeMeshDict Normal file
View File

@ -0,0 +1,136 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object extrudeMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// What to extrude:
// patch : from patch of another case ('sourceCase')
// mesh : as above but with original case included
// surface : from externally read surface
//constructFrom mesh;
//constructFrom patch;
constructFrom surface;
// If construct from patch/mesh:
sourceCase "../cavity";
sourcePatches (movingWall);
// If construct from patch: patch to use for back (can be same as sourcePatch)
exposedPatchName movingWall;
// If construct from surface:
surface "constant/triSurface/cylinder.vtk";
// Flip surface normals before usage. Valid only for extrude from surface or
// patch.
flipNormals false;
//- Linear extrusion in point-normal direction
extrudeModel linearNormal;
//- Single layer linear extrusion in point-normal direction
// with empty patches on front and back
//extrudeModel plane;
//- Linear extrusion in specified direction
//extrudeModel linearDirection;
//- Sector extrusion
//extrudeModel sector;
//- Wedge extrusion of a single layer
// with wedge patches on front and back
//extrudeModel wedge;
//- Extrudes into sphere around (0 0 0)
//extrudeModel linearRadial;
//- Extrudes into sphere around (0 0 0) with specified radii
//extrudeModel radial;
//- Extrudes into sphere with grading according to pressure (atmospherics)
//extrudeModel sigmaRadial;
//- Extrudes by interpolating along path inbetween two (topologically identical)
// surfaces (e.g. one is an offsetted version of the other)
//extrudeModel offsetSurface;
nLayers 10;
expansionRatio 1.02;
sectorCoeffs
{
axisPt (0 0.1 -0.05);
axis (-1 0 0);
angle 360; // For nLayers=1 assume symmetry so angle/2 on each side
}
linearNormalCoeffs
{
thickness 0.7;
}
planeCoeffs
{
// thickness 0.1;
nLayers 4;
}
linearDirectionCoeffs
{
direction (0 1 0);
thickness 0.5;
}
linearRadialCoeffs
{
R 0.1;
// Optional inner radius
Rsurface 0.01;
}
radialCoeffs
{
// Radii specified through interpolation table
R table ((0 0.01)(3 0.03)(10 0.1));
}
sigmaRadialCoeffs
{
RTbyg 1;
pRef 1;
pStrat 1;
}
offsetSurfaceCoeffs
{
// Surface that mesh has been meshed to
baseSurface "$FOAM_CASE/constant/triSurface/DTC-scaled-inflated.obj";
// Surface to fill in to
offsetSurface "$FOAM_CASE/constant/triSurface/DTC-scaled.obj";
}
// Do front and back need to be merged? Usually only makes sense for 360
// degree wedges.
mergeFaces false;
// Merge small edges. Fraction of bounding box.
mergeTol 0;
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

58
tutorials/basic/overPotentialFoam/cylinder/cylinderMesh/system/fvSchemes Normal file
View File

@ -0,0 +1,58 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default Euler;
}
gradSchemes
{
default Gauss linear;
}
divSchemes
{
default none;
div(phi,U) Gauss limitedLinearV 1;
div(phi,k) Gauss upwind;
div(phi,epsilon) Gauss upwind;
div(phi,R) Gauss upwind;
div(R) Gauss linear;
div(phid,p) Gauss limitedLinear 1;
div(phi,K) Gauss limitedLinear 1;
div(phi,e) Gauss limitedLinear 1;
div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;
}
laplacianSchemes
{
default Gauss linear limited corrected 0.5;
}
interpolationSchemes
{
default linear;
}
snGradSchemes
{
default corrected;
}
// ************************************************************************* //

51
tutorials/basic/overPotentialFoam/cylinder/cylinderMesh/system/fvSolution Normal file
View File

@ -0,0 +1,51 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
p
{
solver smoothSolver;
smoother symGaussSeidel;
tolerance 1e-12;
relTol 0;
}
rho
{
solver PCG;
preconditioner DIC;
tolerance 1e-08;
relTol 0;
}
"(U|e|k|epsilon|R)"
{
$p;
tolerance 1e-08;
relTol 0;
}
}
PISO
{
nCorrectors 2;
nNonOrthogonalCorrectors 2;
}
// ************************************************************************* //

10
tutorials/compressible/overRhoSimpleFoam/hotCylinder/Allclean Executable file
View File

@ -0,0 +1,10 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Extrude mesh around cylinder
(cd cylinderAndBackground && ./Allclean)
# Add background mesh
(cd cylinderMesh && foamCleanTutorials)
# ----------------------------------------------------------------- end-of-file

8
tutorials/compressible/overRhoSimpleFoam/hotCylinder/Allrun Executable file
View File

@ -0,0 +1,8 @@
#!/bin/sh
. $WM_PROJECT_DIR/bin/tools/RunFunctions
# Extrude mesh around cylinder
(cd cylinderMesh && ./Allrun.pre)
# Add background mesh
(cd cylinderAndBackground && ./Allrun)

8
tutorials/compressible/overRhoSimpleFoam/hotCylinder/Allrun.pre Executable file
View File

@ -0,0 +1,8 @@
#!/bin/sh
. $WM_PROJECT_DIR/bin/tools/RunFunctions
# Extrude mesh around cylinder
(cd cylinderMesh && ./Allrun.pre)
# Add background mesh
(cd cylinderAndBackground && ./Allrun.pre)

53
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderAndBackground/0.orig/T Normal file
View File

@ -0,0 +1,53 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object T;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
#include "include/initialConditions"
dimensions [0 0 0 1 0 0 0];
internalField uniform $temperature;
boundaryField
{
#includeEtc "caseDicts/setConstraintTypes"
wall
{
type fixedValue;
value uniform 450;
}
inlet
{
type fixedValue;
value uniform $temperature;
}
outlet
{
type inletOutlet;
value $internalField;
inletValue $internalField;
}
".*"
{
type zeroGradient;
}
}
// ************************************************************************* //

54
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderAndBackground/0.orig/U Normal file
View File

@ -0,0 +1,54 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volVectorField;
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
#include "include/initialConditions"
dimensions [0 1 -1 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
#includeEtc "caseDicts/setConstraintTypes"
walls
{
type movingWallVelocity;
value uniform (0 0 0);
}
inlet
{
type fixedValue;
value uniform $flowVelocity;
}
outlet
{
type inletOutlet;
inletValue uniform (0 0 0);
value $internalField;
}
topAndBottom
{
type inletOutlet;
inletValue uniform (0 0 0);
value $internalField;
}
}
// ************************************************************************* //

40
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderAndBackground/0.orig/alphat Normal file
View File

@ -0,0 +1,40 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object alphat;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
#includeEtc "caseDicts/setConstraintTypes"
walls
{
type compressible::alphatWallFunction;
Prt 0.85;
value uniform 0;
}
".*"
{
type calculated;
value uniform 0;
}
}
// ************************************************************************* //

54
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderAndBackground/0.orig/epsilon Normal file
View File

@ -0,0 +1,54 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object epsilon;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
#include "include/initialConditions"
dimensions [0 2 -3 0 0 0 0];
internalField uniform $turbulentEpsilon;
boundaryField
{
#includeEtc "caseDicts/setConstraintTypes"
walls
{
type epsilonWallFunction;
value $internalField;
}
inlet
{
type fixedValue;
value $internalField;
}
outlet
{
type inletOutlet;
inletValue $internalField;
value $internalField;
}
topAndBottom
{
type inletOutlet;
inletValue $internalField
value $internalField;
}
}
// ************************************************************************* //

15
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderAndBackground/0.orig/include/fixedInlet Normal file
View File

@ -0,0 +1,15 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
inlet
{
type fixedValue;
value $internalField;
}
// ************************************************************************* //

16
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderAndBackground/0.orig/include/initialConditions Normal file
View File

@ -0,0 +1,16 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
flowVelocity (1 0 0);
pressure 1e5;
temperature 300;
turbulentEpsilon 10;
turbulentKE 1;
#inputMode merge
// ************************************************************************* //

48
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderAndBackground/0.orig/k Normal file
View File

@ -0,0 +1,48 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
#include "include/initialConditions"
dimensions [ 0 2 -2 0 0 0 0 ];
internalField uniform $turbulentKE;
boundaryField
{
#includeEtc "caseDicts/setConstraintTypes"
wall
{
type kqRWallFunction;
value uniform 0;
}
inlet
{
type turbulentIntensityKineticEnergyInlet;
intensity 0.05; // 5% turbulent intensity
value $internalField;
}
"outlet|topAndBottom"
{
type inletOutlet;
inletValue $internalField;
value $internalField;
}
}
// ************************************************************************* //

38
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderAndBackground/0.orig/nut Normal file
View File

@ -0,0 +1,38 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object nut;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [ 0 2 -1 0 0 0 0 ];
internalField uniform 0;
boundaryField
{
#includeEtc "caseDicts/setConstraintTypes"
walls
{
type nutkWallFunction;
value uniform 0;
}
".*"
{
type calculated;
value uniform 0;
}
}
// ************************************************************************* //

46
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderAndBackground/0.orig/p Normal file
View File

@ -0,0 +1,46 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object p;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
#include "include/initialConditions"
dimensions [1 -1 -2 0 0 0 0];
internalField uniform $pressure;
boundaryField
{
#includeEtc "caseDicts/setConstraintTypes"
wall
{
type zeroGradient;
}
inlet
{
type zeroGradient;
}
outlet
{
type fixedValue;
value $internalField;
}
topAndBottom
{
type zeroGradient;
}
}
// ************************************************************************* //

42
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderAndBackground/0.orig/pointDisplacement Normal file
View File

@ -0,0 +1,42 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class pointVectorField;
object pointDisplacement;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 0 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
overset
{
patchType overset;
type zeroGradient;
}
walls
{
type uniformFixedValue;
uniformValue (0 0 0);
}
".*"
{
type uniformFixedValue;
uniformValue (0 0 0);
}
}
// ************************************************************************* //

37
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderAndBackground/0.orig/zoneID Normal file
View File

@ -0,0 +1,37 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object zoneID;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0;
boundaryField
{
#includeEtc "caseDicts/setConstraintTypes"
oversetPatch
{
type overset;
value uniform 0;
}
".*"
{
type zeroGradient;
}
}
// ************************************************************************* //

12
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderAndBackground/Allclean Executable file
View File

@ -0,0 +1,12 @@
#!/bin/sh
cd ${0%/*} || exit 1 # Run from this directory
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
cleanCase
rm -f constant/polyMesh/boundary
rm -f constant/polyMesh/zoneID
rm -f constant/cellInterpolationWeight
rm -rf 0
#------------------------------------------------------------------------------

10
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderAndBackground/Allrun Executable file
View File

@ -0,0 +1,10 @@
#!/bin/sh
cd ${0%/*} || exit 1 # Run from this directory
. $WM_PROJECT_DIR/bin/tools/RunFunctions
./Allrun.pre
# Run it for a bit
runApplication $(getApplication)
#------------------------------------------------------------------------------

22
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderAndBackground/Allrun.pre Executable file
View File

@ -0,0 +1,22 @@
#!/bin/sh
cd ${0%/*} || exit 1 # Run from this directory
. $WM_PROJECT_DIR/bin/tools/RunFunctions
# Create background mesh
runApplication blockMesh
# Add the cylinder mesh
runApplication mergeMeshes . ../cylinderMesh -overwrite
## Make it a bit smaller to keep it laminar
#runApplication transformPoints -scale '(0.001 0.001 0.001)'
# Select cellSets for the different zones
runApplication topoSet
restore0Dir
# Use cellSets to write zoneID
runApplication setFields
#------------------------------------------------------------------------------

33
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderAndBackground/constant/dynamicMeshDict Normal file
View File

@ -0,0 +1,33 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object dynamicMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
motionSolverLibs ( "libfvMotionSolvers.so" );
solver displacementLaplacian;
displacementLaplacianCoeffs
{
diffusivity uniform 1;
}
dynamicFvMesh dynamicOversetFvMesh;
dynamicOversetFvMeshCoeffs
{
// layerRelax 0.3;
}
// ************************************************************************* //

48
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderAndBackground/constant/thermophysicalProperties Normal file
View File

@ -0,0 +1,48 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object thermophysicalProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
thermoType
{
type heRhoThermo;
mixture pureMixture;
transport sutherland;
thermo hConst;
equationOfState perfectGas;
specie specie;
energy sensibleEnthalpy;
}
mixture
{
specie
{
molWeight 28.9;
}
thermodynamics
{
Cp 1007;
Hf 0;
}
transport
{
As 1.4792e-06;
Ts 116;
}
}
// ************************************************************************* //

39
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderAndBackground/constant/transportProperties Normal file
View File

@ -0,0 +1,39 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object transportProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
DT DT [ 0 2 -1 0 0 0 0 ] 1; //4e-05;
transportModel Newtonian;
nu nu [ 0 2 -1 0 0 0 0 ] 1e-03;
CrossPowerLawCoeffs
{
nu0 nu0 [ 0 2 -1 0 0 0 0 ] 1e-06;
nuInf nuInf [ 0 2 -1 0 0 0 0 ] 1e-06;
m m [ 0 0 1 0 0 0 0 ] 1;
n n [ 0 0 0 0 0 0 0 ] 1;
}
BirdCarreauCoeffs
{
nu0 nu0 [ 0 2 -1 0 0 0 0 ] 1e-06;
nuInf nuInf [ 0 2 -1 0 0 0 0 ] 1e-06;
k k [ 0 0 1 0 0 0 0 ] 0;
n n [ 0 0 0 0 0 0 0 ] 1;
}
// ************************************************************************* //

30
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderAndBackground/constant/turbulenceProperties Normal file
View File

@ -0,0 +1,30 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object turbulenceProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
simulationType RAS;
RAS
{
RASModel kEpsilon;
turbulence on;
printCoeffs on;
}
// ************************************************************************* //

83
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderAndBackground/system/blockMeshDict Normal file
View File

@ -0,0 +1,83 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object blockMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
convertToMeters 1;
vertices
(
(-2 -0.05 -2.0)
( 4 -0.05 -2.0)
( 4 0.05 -2.0)
(-2 0.05 -2.0)
(-2 -0.05 2.0)
( 4 -0.05 2.0)
( 4 0.05 2.0)
(-2 0.05 2.0)
);
blocks
(
hex (0 1 2 3 4 5 6 7) (120 1 60) simpleGrading (1 1 1)
);
edges
(
);
boundary
(
topAndBottom
{
type patch;
faces
(
(4 5 6 7)
(0 3 2 1)
);
}
inlet
{
type patch;
faces
(
(0 4 7 3)
);
}
outlet
{
type patch;
faces
(
(2 6 5 1)
);
}
frontAndBack
{
type empty;
faces
(
(3 7 6 2)
(1 5 4 0)
);
}
);
// ************************************************************************* //

51
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderAndBackground/system/controlDict Normal file
View File

@ -0,0 +1,51 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// Make sure all preprocessing tools know about the 'overset' bc
libs ("liboverset.so");
application overRhoSimpleFoam;
startFrom startTime;
startTime 0;
stopAt endTime;
endTime 1000;
deltaT 1;
writeControl timeStep;
writeInterval 100;
purgeWrite 0;
writeFormat ascii;
writePrecision 12;
writeCompression off;
timeFormat general;
timePrecision 6;
runTimeModifiable true;
// ************************************************************************* //

30
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderAndBackground/system/decomposeParDict Normal file
View File

@ -0,0 +1,30 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
note "mesh decomposition control dictionary";
object decomposeParDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
numberOfSubdomains 4;
method hierarchical;
hierarchicalCoeffs
{
n (2 2 1);
delta 0.001;
order xyz;
}
// ************************************************************************* //

71
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderAndBackground/system/fvSchemes Normal file
View File

@ -0,0 +1,71 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
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(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;
div((nuEff*dev2(T(grad(U))))) Gauss linear;
div(phi,h) bounded Gauss upwind;
div(phi,epsilon) bounded Gauss upwind;
div(phi,k) bounded Gauss upwind;
div(phi,Ekp) bounded Gauss upwind;
div(phi,K) bounded Gauss upwind;
}
laplacianSchemes
{
default Gauss linear corrected;
}
interpolationSchemes
{
default linear;
}
snGradSchemes
{
default corrected;
}
oversetInterpolation
{
method inverseDistance;
}
oversetInterpolationRequired
{
epsilon;
k;
nut;
}
// ************************************************************************* //

80
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderAndBackground/system/fvSolution Normal file
View File

@ -0,0 +1,80 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
cellDisplacement
{
solver PCG;
preconditioner DIC;
tolerance 1e-06;
relTol 0;
maxIter 100;
}
"(U|e|h|k|epsilon)"
{
solver PBiCGStab;
preconditioner DILU;
tolerance 1e-6;
relTol 0.01;
}
p
{
$U;
}
}
SIMPLE
{
momentumPredictor true;
nNonOrthogonalCorrectors 1;
pMinFactor 0.1;
pMaxFactor 2;
residualControl
{
p 1e-3;
U 1e-4;
e 1e-3;
// possibly check turbulence fields
"(k|epsilon|omega)" 1e-3;
}
}
relaxationFactors
{
fields
{
p 0.7;
rho 1;
}
equations
{
U 0.3;
h 0.8;
k 0.4;
epsilon 0.4;
}
}
// ************************************************************************* //

48
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderAndBackground/system/setFieldsDict Normal file
View File

@ -0,0 +1,48 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object setFieldsDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
defaultFieldValues
(
volScalarFieldValue zoneID 123
);
regions
(
// Set cell values
// (does zerogradient on boundaries)
cellToCell
{
set c0;
fieldValues
(
volScalarFieldValue zoneID 0
);
}
cellToCell
{
set c1;
fieldValues
(
volScalarFieldValue zoneID 1
);
}
);
// ************************************************************************* //

48
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderAndBackground/system/topoSetDict Normal file
View File

@ -0,0 +1,48 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object topoSetDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
actions
(
{
name c0;
type cellSet;
action new;
source regionToCell;
sourceInfo
{
insidePoints ((-1.999 0 -1.999));
}
}
{
name c1;
type cellSet;
action new;
source cellToCell;
sourceInfo
{
set c0;
}
}
{
name c1;
type cellSet;
action invert;
}
);
// ************************************************************************* //

8
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderMesh/Allrun.pre Executable file
View File

@ -0,0 +1,8 @@
#!/bin/sh
. $WM_PROJECT_DIR/bin/tools/RunFunctions
# Generate mesh from surface (in constant/triSurface)
runApplication extrudeMesh
# Make front and back type empty
runApplication createPatch -overwrite

221
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderMesh/constant/triSurface/cylinder.vtk Normal file
View File

@ -0,0 +1,221 @@
# vtk DataFile Version 4.0
vtk output
ASCII
DATASET POLYDATA
POINTS 150 float
0.5 0.05 0 0.5 -0.05 0 0.498246 0.05 -0.0418389
0.498246 -0.05 -0.0418389 0.492998 0.05 -0.0833844 0.492998 -0.05 -0.0833844
0.484292 0.05 -0.124345 0.484292 -0.05 -0.124345 0.472188 0.05 -0.164433
0.472188 -0.05 -0.164433 0.456773 0.05 -0.203368 0.456773 -0.05 -0.203368
0.438153 0.05 -0.240877 0.438153 -0.05 -0.240877 0.416461 0.05 -0.276696
0.416461 -0.05 -0.276696 0.391847 0.05 -0.310574 0.391847 -0.05 -0.310574
0.364484 0.05 -0.342274 0.364484 -0.05 -0.342274 0.334565 0.05 -0.371572
0.334565 -0.05 -0.371572 0.3023 0.05 -0.398265 0.3023 -0.05 -0.398265
0.267913 0.05 -0.422164 0.267913 -0.05 -0.422164 0.231648 0.05 -0.443102
0.231648 -0.05 -0.443102 0.193758 0.05 -0.460932 0.193758 -0.05 -0.460932
0.154509 0.05 -0.475528 0.154509 -0.05 -0.475528 0.114175 0.05 -0.486789
0.114175 -0.05 -0.486789 0.0730415 0.05 -0.494636 0.0730415 -0.05 -0.494636
0.0313953 0.05 -0.499013 0.0313953 -0.05 -0.499013 -0.0104712 0.05 -0.49989
-0.0104712 -0.05 -0.49989 -0.0522642 0.05 -0.497261 -0.0522642 -0.05 -0.497261
-0.0936907 0.05 -0.491144 -0.0936907 -0.05 -0.491144 -0.13446 0.05 -0.481581
-0.13446 -0.05 -0.481581 -0.174286 0.05 -0.468641 -0.174286 -0.05 -0.468641
-0.21289 0.05 -0.452414 -0.21289 -0.05 -0.452414 -0.25 0.05 -0.433013
-0.25 -0.05 -0.433013 -0.285357 0.05 -0.410575 -0.285357 -0.05 -0.410575
-0.318712 0.05 -0.385257 -0.318712 -0.05 -0.385257 -0.349832 0.05 -0.357236
-0.349832 -0.05 -0.357236 -0.378498 0.05 -0.32671 -0.378498 -0.05 -0.32671
-0.404509 0.05 -0.293893 -0.404509 -0.05 -0.293893 -0.427682 0.05 -0.259014
-0.427682 -0.05 -0.259014 -0.447856 0.05 -0.222318 -0.447856 -0.05 -0.222318
-0.464888 0.05 -0.184062 -0.464888 -0.05 -0.184062 -0.47866 0.05 -0.144516
-0.47866 -0.05 -0.144516 -0.489074 0.05 -0.103956 -0.489074 -0.05 -0.103956
-0.496057 0.05 -0.0626666 -0.496057 -0.05 -0.0626666 -0.499561 0.05 -0.0209378
-0.499561 -0.05 -0.0209378 -0.499561 0.05 0.0209378 -0.499561 -0.05 0.0209378
-0.496057 0.05 0.0626666 -0.496057 -0.05 0.0626666 -0.489074 0.05 0.103956
-0.489074 -0.05 0.103956 -0.47866 0.05 0.144516 -0.47866 -0.05 0.144516
-0.464888 0.05 0.184062 -0.464888 -0.05 0.184062 -0.447856 0.05 0.222318
-0.447856 -0.05 0.222318 -0.427682 0.05 0.259014 -0.427682 -0.05 0.259014
-0.404509 0.05 0.293893 -0.404509 -0.05 0.293893 -0.378498 0.05 0.32671
-0.378498 -0.05 0.32671 -0.349832 0.05 0.357236 -0.349832 -0.05 0.357236
-0.318712 0.05 0.385257 -0.318712 -0.05 0.385257 -0.285357 0.05 0.410575
-0.285357 -0.05 0.410575 -0.25 0.05 0.433013 -0.25 -0.05 0.433013
-0.21289 0.05 0.452414 -0.21289 -0.05 0.452414 -0.174286 0.05 0.468641
-0.174286 -0.05 0.468641 -0.13446 0.05 0.481581 -0.13446 -0.05 0.481581
-0.0936907 0.05 0.491144 -0.0936907 -0.05 0.491144 -0.0522642 0.05 0.497261
-0.0522642 -0.05 0.497261 -0.0104712 0.05 0.49989 -0.0104712 -0.05 0.49989
0.0313953 0.05 0.499013 0.0313953 -0.05 0.499013 0.0730415 0.05 0.494636
0.0730415 -0.05 0.494636 0.114175 0.05 0.486789 0.114175 -0.05 0.486789
0.154509 0.05 0.475528 0.154509 -0.05 0.475528 0.193758 0.05 0.460932
0.193758 -0.05 0.460932 0.231648 0.05 0.443102 0.231648 -0.05 0.443102
0.267913 0.05 0.422164 0.267913 -0.05 0.422164 0.3023 0.05 0.398265
0.3023 -0.05 0.398265 0.334565 0.05 0.371572 0.334565 -0.05 0.371572
0.364484 0.05 0.342274 0.364484 -0.05 0.342274 0.391847 0.05 0.310574
0.391847 -0.05 0.310574 0.416461 0.05 0.276696 0.416461 -0.05 0.276696
0.438153 0.05 0.240877 0.438153 -0.05 0.240877 0.456773 0.05 0.203368
0.456773 -0.05 0.203368 0.472188 0.05 0.164433 0.472188 -0.05 0.164433
0.484292 0.05 0.124345 0.484292 -0.05 0.124345 0.492998 0.05 0.0833844
0.492998 -0.05 0.0833844 0.498246 0.05 0.0418389 0.498246 -0.05 0.0418389
POLYGONS 75 375
4 0 1 3 2
4 2 3 5 4
4 4 5 7 6
4 6 7 9 8
4 8 9 11 10
4 10 11 13 12
4 12 13 15 14
4 14 15 17 16
4 16 17 19 18
4 18 19 21 20
4 20 21 23 22
4 22 23 25 24
4 24 25 27 26
4 26 27 29 28
4 28 29 31 30
4 30 31 33 32
4 32 33 35 34
4 34 35 37 36
4 36 37 39 38
4 38 39 41 40
4 40 41 43 42
4 42 43 45 44
4 44 45 47 46
4 46 47 49 48
4 48 49 51 50
4 50 51 53 52
4 52 53 55 54
4 54 55 57 56
4 56 57 59 58
4 58 59 61 60
4 60 61 63 62
4 62 63 65 64
4 64 65 67 66
4 66 67 69 68
4 68 69 71 70
4 70 71 73 72
4 72 73 75 74
4 74 75 77 76
4 76 77 79 78
4 78 79 81 80
4 80 81 83 82
4 82 83 85 84
4 84 85 87 86
4 86 87 89 88
4 88 89 91 90
4 90 91 93 92
4 92 93 95 94
4 94 95 97 96
4 96 97 99 98
4 98 99 101 100
4 100 101 103 102
4 102 103 105 104
4 104 105 107 106
4 106 107 109 108
4 108 109 111 110
4 110 111 113 112
4 112 113 115 114
4 114 115 117 116
4 116 117 119 118
4 118 119 121 120
4 120 121 123 122
4 122 123 125 124
4 124 125 127 126
4 126 127 129 128
4 128 129 131 130
4 130 131 133 132
4 132 133 135 134
4 134 135 137 136
4 136 137 139 138
4 138 139 141 140
4 140 141 143 142
4 142 143 145 144
4 144 145 147 146
4 146 147 149 148
4 148 149 1 0
POINT_DATA 150
NORMALS Normals float
1 0 -0 1 0 -0 0.996493 0 -0.0836778
0.996493 0 -0.0836778 0.985996 0 -0.166769 0.985996 0 -0.166769
0.968583 0 -0.24869 0.968583 0 -0.24869 0.944376 0 -0.328867
0.944376 0 -0.328867 0.913545 0 -0.406737 0.913545 0 -0.406737
0.876307 0 -0.481754 0.876307 0 -0.481754 0.832921 0 -0.553392
0.832921 0 -0.553392 0.783693 0 -0.621148 0.783693 0 -0.621148
0.728969 0 -0.684547 0.728969 0 -0.684547 0.669131 0 -0.743145
0.669131 0 -0.743145 0.604599 0 -0.79653 0.604599 0 -0.79653
0.535827 0 -0.844328 0.535827 0 -0.844328 0.463296 0 -0.886204
0.463296 0 -0.886204 0.387516 0 -0.921863 0.387516 0 -0.921863
0.309017 0 -0.951057 0.309017 0 -0.951057 0.228351 0 -0.973579
0.228351 0 -0.973579 0.146083 0 -0.989272 0.146083 0 -0.989272
0.0627905 0 -0.998027 0.0627905 0 -0.998027 -0.0209424 0 -0.999781
-0.0209424 0 -0.999781 -0.104528 0 -0.994522 -0.104528 0 -0.994522
-0.187381 0 -0.982287 -0.187381 0 -0.982287 -0.26892 0 -0.963163
-0.26892 0 -0.963163 -0.348572 0 -0.937282 -0.348572 0 -0.937282
-0.425779 0 -0.904827 -0.425779 0 -0.904827 -0.5 0 -0.866025
-0.5 0 -0.866025 -0.570714 0 -0.821149 -0.570714 0 -0.821149
-0.637424 0 -0.770513 -0.637424 0 -0.770513 -0.699663 0 -0.714473
-0.699663 0 -0.714473 -0.756995 0 -0.653421 -0.756995 0 -0.653421
-0.809017 0 -0.587785 -0.809017 0 -0.587785 -0.855364 0 -0.518027
-0.855364 0 -0.518027 -0.895712 0 -0.444635 -0.895712 0 -0.444635
-0.929776 0 -0.368125 -0.929776 0 -0.368125 -0.957319 0 -0.289032
-0.957319 0 -0.289032 -0.978148 0 -0.207912 -0.978148 0 -0.207912
-0.992115 0 -0.125333 -0.992115 0 -0.125333 -0.999123 0 -0.0418757
-0.999123 0 -0.0418757 -0.999123 0 0.0418757 -0.999123 0 0.0418757
-0.992115 0 0.125333 -0.992115 0 0.125333 -0.978148 0 0.207912
-0.978148 0 0.207912 -0.957319 0 0.289032 -0.957319 0 0.289032
-0.929776 0 0.368125 -0.929776 0 0.368125 -0.895712 0 0.444635
-0.895712 0 0.444635 -0.855364 0 0.518027 -0.855364 0 0.518027
-0.809017 0 0.587785 -0.809017 0 0.587785 -0.756995 0 0.653421
-0.756995 0 0.653421 -0.699663 0 0.714473 -0.699663 0 0.714473
-0.637424 0 0.770513 -0.637424 0 0.770513 -0.570714 0 0.821149
-0.570714 0 0.821149 -0.5 0 0.866025 -0.5 0 0.866025
-0.425779 0 0.904827 -0.425779 0 0.904827 -0.348572 0 0.937282
-0.348572 0 0.937282 -0.26892 0 0.963163 -0.26892 0 0.963163
-0.187381 0 0.982287 -0.187381 0 0.982287 -0.104528 0 0.994522
-0.104528 0 0.994522 -0.0209424 0 0.999781 -0.0209424 0 0.999781
0.0627905 0 0.998027 0.0627905 0 0.998027 0.146083 0 0.989272
0.146083 0 0.989272 0.228351 0 0.973579 0.228351 0 0.973579
0.309017 0 0.951057 0.309017 0 0.951057 0.387516 0 0.921863
0.387516 0 0.921863 0.463296 0 0.886204 0.463296 0 0.886204
0.535827 0 0.844328 0.535827 0 0.844328 0.604599 0 0.79653
0.604599 0 0.79653 0.669131 0 0.743145 0.669131 0 0.743145
0.728969 0 0.684547 0.728969 0 0.684547 0.783693 0 0.621148
0.783693 0 0.621148 0.832921 0 0.553392 0.832921 0 0.553392
0.876307 0 0.481754 0.876307 0 0.481754 0.913545 0 0.406737
0.913545 0 0.406737 0.944376 0 0.328867 0.944376 0 0.328867
0.968583 0 0.24869 0.968583 0 0.24869 0.985996 0 0.166769
0.985996 0 0.166769 0.996493 0 0.0836778 0.996493 0 0.0836778
TEXTURE_COORDINATES TCoords 2 float
1 0 1 1 0.973333 0 0.973333 1 0.946667
0 0.946667 1 0.92 0 0.92 1 0.893333 0
0.893333 1 0.866667 0 0.866667 1 0.84 0 0.84
1 0.813333 0 0.813333 1 0.786667 0 0.786667 1
0.76 0 0.76 1 0.733333 0 0.733333 1 0.706667
0 0.706667 1 0.68 0 0.68 1 0.653333 0
0.653333 1 0.626667 0 0.626667 1 0.6 0 0.6
1 0.573333 0 0.573333 1 0.546667 0 0.546667 1
0.52 0 0.52 1 0.493333 0 0.493333 1 0.466667
0 0.466667 1 0.44 0 0.44 1 0.413333 0
0.413333 1 0.386667 0 0.386667 1 0.36 0 0.36
1 0.333333 0 0.333333 1 0.306667 0 0.306667 1
0.28 0 0.28 1 0.253333 0 0.253333 1 0.226667
0 0.226667 1 0.2 0 0.2 1 0.173333 0
0.173333 1 0.146667 0 0.146667 1 0.12 0 0.12
1 0.0933333 0 0.0933333 1 0.0666667 0 0.0666667 1
0.04 0 0.04 1 0.0133333 0 0.0133333 1 0.0133333
0 0.0133333 1 0.04 0 0.04 1 0.0666667 0
0.0666667 1 0.0933333 0 0.0933333 1 0.12 0 0.12
1 0.146667 0 0.146667 1 0.173333 0 0.173333 1
0.2 0 0.2 1 0.226667 0 0.226667 1 0.253333
0 0.253333 1 0.28 0 0.28 1 0.306667 0
0.306667 1 0.333333 0 0.333333 1 0.36 0 0.36
1 0.386667 0 0.386667 1 0.413333 0 0.413333 1
0.44 0 0.44 1 0.466667 0 0.466667 1 0.493333
0 0.493333 1 0.52 0 0.52 1 0.546667 0
0.546667 1 0.573333 0 0.573333 1 0.6 0 0.6
1 0.626667 0 0.626667 1 0.653333 0 0.653333 1
0.68 0 0.68 1 0.706667 0 0.706667 1 0.733333
0 0.733333 1 0.76 0 0.76 1 0.786667 0
0.786667 1 0.813333 0 0.813333 1 0.84 0 0.84
1 0.866667 0 0.866667 1 0.893333 0 0.893333 1
0.92 0 0.92 1 0.946667 0 0.946667 1 0.973333
0 0.973333 1

50
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderMesh/system/controlDict Normal file
View File

@ -0,0 +1,50 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application snappyHexMesh;
startFrom latestTime;
startTime 0;
stopAt endTime;
endTime 100;
deltaT 1;
writeControl runTime;
writeInterval 1;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
writeCompression off;
timeFormat general;
timePrecision 6;
runTimeModifiable true;
}
// ************************************************************************* //

84
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderMesh/system/createPatchDict Normal file
View File

@ -0,0 +1,84 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object createPatchDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
pointSync false;
// Patches to create.
patches
(
{
// Name of new patch
name oversetPatch;
// Dictionary to construct new patch from
patchInfo
{
type overset;
}
// How to construct: either from 'patches' or 'set'
constructFrom patches;
// If constructFrom = patches : names of patches. Wildcards allowed.
patches (otherSide);
// If constructFrom = set : name of faceSet
set f0;
}
{
// Name of new patch
name walls;
// Dictionary to construct new patch from
patchInfo
{
type wall;
}
// How to construct: either from 'patches' or 'set'
constructFrom patches;
// If constructFrom = patches : names of patches. Wildcards allowed.
patches (originalPatch);
// If constructFrom = set : name of faceSet
set f0;
}
{
// Name of new patch
name frontAndBack;
// Dictionary to construct new patch from
patchInfo
{
type empty;
}
// How to construct: either from 'patches' or 'set'
constructFrom patches;
// If constructFrom = patches : names of patches. Wildcards allowed.
patches (sides);
// If constructFrom = set : name of faceSet
set f0;
}
);
// ************************************************************************* //

109
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderMesh/system/extrudeMeshDict Normal file
View File

@ -0,0 +1,109 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object extrudeMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// What to extrude:
// patch : from patch of another case ('sourceCase')
// mesh : as above but with original case included
// surface : from externally read surface
//constructFrom mesh;
//constructFrom patch;
constructFrom surface;
// If construct from patch/mesh:
sourceCase "../cavity";
sourcePatches (movingWall);
// If construct from patch: patch to use for back (can be same as sourcePatch)
exposedPatchName movingWall;
// If construct from surface:
surface "constant/triSurface/cylinder.vtk";
// Flip surface normals before usage. Valid only for extrude from surface or
// patch.
flipNormals false;
//- Linear extrusion in point-normal direction
extrudeModel linearNormal;
nLayers 10;
expansionRatio 1.02;
sectorCoeffs
{
axisPt (0 0.1 -0.05);
axis (-1 0 0);
angle 360; // For nLayers=1 assume symmetry so angle/2 on each side
}
linearNormalCoeffs
{
thickness 0.7;
}
planeCoeffs
{
// thickness 0.1;
nLayers 4;
}
linearDirectionCoeffs
{
direction (0 1 0);
thickness 0.5;
}
linearRadialCoeffs
{
R 0.1;
// Optional inner radius
Rsurface 0.01;
}
radialCoeffs
{
// Radii specified through interpolation table
R table ((0 0.01)(3 0.03)(10 0.1));
}
sigmaRadialCoeffs
{
RTbyg 1;
pRef 1;
pStrat 1;
}
offsetSurfaceCoeffs
{
// Surface that mesh has been meshed to
baseSurface "$FOAM_CASE/constant/triSurface/DTC-scaled-inflated.obj";
// Surface to fill in to
offsetSurface "$FOAM_CASE/constant/triSurface/DTC-scaled.obj";
}
// Do front and back need to be merged? Usually only makes sense for 360
// degree wedges.
mergeFaces false;
// Merge small edges. Fraction of bounding box.
mergeTol 0;
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

58
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderMesh/system/fvSchemes Normal file
View File

@ -0,0 +1,58 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default Euler;
}
gradSchemes
{
default Gauss linear;
}
divSchemes
{
default none;
div(phi,U) Gauss limitedLinearV 1;
div(phi,k) Gauss upwind;
div(phi,epsilon) Gauss upwind;
div(phi,R) Gauss upwind;
div(R) Gauss linear;
div(phid,p) Gauss limitedLinear 1;
div(phi,K) Gauss limitedLinear 1;
div(phi,e) Gauss limitedLinear 1;
div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;
}
laplacianSchemes
{
default Gauss linear limited corrected 0.5;
}
interpolationSchemes
{
default linear;
}
snGradSchemes
{
default corrected;
}
// ************************************************************************* //

51
tutorials/compressible/overRhoSimpleFoam/hotCylinder/cylinderMesh/system/fvSolution Normal file
View File

@ -0,0 +1,51 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: plus |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
p
{
solver smoothSolver;
smoother symGaussSeidel;
tolerance 1e-12;
relTol 0;
}
rho
{
solver PCG;
preconditioner DIC;
tolerance 1e-08;
relTol 0;
}
"(U|e|k|epsilon|R)"
{
$p;
tolerance 1e-08;
relTol 0;
}
}
PISO
{
nCorrectors 2;
nNonOrthogonalCorrectors 2;
}
// ************************************************************************* //