rhoPimpleFoam: Improved support for compressible liquids

See tutorials/compressible/rhoPimpleFoam/RAS/squareBendLiq for exapmle

pimpleControl: Added SIMPLErho option for running in SIMPLE mode

with large time-step/Courant number and relaxation.  With this option the
density is updated from thermodynamics rather than continuity after the pressure
equation which is better behaved if pressure is relaxed and/or solved to a
loose relative tolerance.  The need for this option is demonstrated in the
tutorials/compressible/rhoPimpleFoam/RAS/angledDuct tutorial which is unstable
without the option.
This commit is contained in:
Henry Weller
2017-05-17 17:05:43 +01:00
parent 8462549695
commit 79ff91350e
44 changed files with 1188 additions and 550 deletions

View File

@ -52,27 +52,7 @@ volScalarField& p = thermo.p();
#include "compressibleCreatePhi.H"
dimensionedScalar rhoMax
(
dimensionedScalar::lookupOrDefault
(
"rhoMax",
pimple.dict(),
dimDensity,
GREAT
)
);
dimensionedScalar rhoMin
(
dimensionedScalar::lookupOrDefault
(
"rhoMin",
pimple.dict(),
dimDensity,
0
)
);
pressureControl pressureControl(p, rho, pimple.dict(), false);
mesh.setFluxRequired(p.name());

View File

@ -1,7 +1,4 @@
rho = thermo.rho();
rho = max(rho, rhoMin);
rho = min(rho, rhoMax);
rho.relax();
volScalarField rAU(1.0/UEqn.A());
surfaceScalarField rhorAUf("rhorAUf", fvc::interpolate(rho*rAU));
@ -87,19 +84,17 @@ else
// Explicitly relax pressure for momentum corrector
p.relax();
// Recalculate density from the relaxed pressure
rho = thermo.rho();
rho = max(rho, rhoMin);
rho = min(rho, rhoMax);
rho.relax();
Info<< "rho max/min : " << max(rho).value()
<< " " << min(rho).value() << endl;
U = HbyA - rAU*fvc::grad(p);
U.correctBoundaryConditions();
fvOptions.correct(U);
K = 0.5*magSqr(U);
if (pressureControl.limit(p))
{
p.correctBoundaryConditions();
rho = thermo.rho();
}
if (thermo.dpdt())
{
dpdt = fvc::ddt(p);

View File

@ -1,7 +1,4 @@
rho = thermo.rho();
rho = max(rho, rhoMin);
rho = min(rho, rhoMax);
rho.relax();
volScalarField rAU(1.0/UEqn.A());
volScalarField rAtU(1.0/(1.0/rAU - UEqn.H1()));
@ -109,19 +106,13 @@ U.correctBoundaryConditions();
fvOptions.correct(U);
K = 0.5*magSqr(U);
if (pressureControl.limit(p))
{
p.correctBoundaryConditions();
rho = thermo.rho();
}
if (thermo.dpdt())
{
dpdt = fvc::ddt(p);
}
// Recalculate density from the relaxed pressure
rho = thermo.rho();
rho = max(rho, rhoMin);
rho = min(rho, rhoMax);
if (!pimple.transonic())
{
rho.relax();
}
Info<< "rho max/min : " << max(rho).value() << " " << min(rho).value() << endl;

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | Copyright (C) 2011-2016 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2017 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -34,6 +34,7 @@ Description
#include "psiCombustionModel.H"
#include "multivariateScheme.H"
#include "pimpleControl.H"
#include "pressureControl.H"
#include "fvOptions.H"
#include "localEulerDdtScheme.H"
#include "fvcSmooth.H"
@ -111,6 +112,8 @@ int main(int argc, char *argv[])
}
}
rho = thermo.rho();
runTime.write();
Info<< "ExecutionTime = " << runTime.elapsedCpuTime() << " s"

View File

@ -1,76 +1,74 @@
rho = thermo.rho();
// Thermodynamic density needs to be updated by psi*d(p) after the
// pressure solution
const volScalarField psip0(psi*p);
volScalarField rAU(1.0/UEqn.A());
surfaceScalarField rhorAUf("rhorAUf", fvc::interpolate(rho*rAU));
volVectorField HbyA(constrainHbyA(rAU*UEqn.H(), U, p));
surfaceScalarField phig(-rhorAUf*ghf*fvc::snGrad(rho)*mesh.magSf());
surfaceScalarField phiHbyA
(
"phiHbyA",
(
fvc::flux(rho*HbyA)
+ rhorAUf*fvc::ddtCorr(rho, U, phi)
)
+ phig
);
MRF.makeRelative(fvc::interpolate(rho), phiHbyA);
// Update the pressure BCs to ensure flux consistency
constrainPressure(p_rgh, rho, U, phiHbyA, rhorAUf, MRF);
fvScalarMatrix p_rghDDtEqn
(
fvc::ddt(rho) + psi*correction(fvm::ddt(p_rgh))
+ fvc::div(phiHbyA)
==
fvOptions(psi, p_rgh, rho.name())
);
while (pimple.correctNonOrthogonal())
{
rho = thermo.rho();
// Thermodynamic density needs to be updated by psi*d(p) after the
// pressure solution - done in 2 parts. Part 1:
thermo.rho() -= psi*p;
volScalarField rAU(1.0/UEqn.A());
surfaceScalarField rhorAUf("rhorAUf", fvc::interpolate(rho*rAU));
volVectorField HbyA(constrainHbyA(rAU*UEqn.H(), U, p));
surfaceScalarField phig(-rhorAUf*ghf*fvc::snGrad(rho)*mesh.magSf());
surfaceScalarField phiHbyA
fvScalarMatrix p_rghEqn
(
"phiHbyA",
(
fvc::flux(rho*HbyA)
+ rhorAUf*fvc::ddtCorr(rho, U, phi)
)
+ phig
p_rghDDtEqn
- fvm::laplacian(rhorAUf, p_rgh)
);
MRF.makeRelative(fvc::interpolate(rho), phiHbyA);
p_rghEqn.solve(mesh.solver(p_rgh.select(pimple.finalInnerIter())));
// Update the pressure BCs to ensure flux consistency
constrainPressure(p_rgh, rho, U, phiHbyA, rhorAUf, MRF);
fvScalarMatrix p_rghDDtEqn
(
fvc::ddt(rho) + psi*correction(fvm::ddt(p_rgh))
+ fvc::div(phiHbyA)
==
fvOptions(psi, p_rgh, rho.name())
);
while (pimple.correctNonOrthogonal())
if (pimple.finalNonOrthogonalIter())
{
fvScalarMatrix p_rghEqn
(
p_rghDDtEqn
- fvm::laplacian(rhorAUf, p_rgh)
);
// Calculate the conservative fluxes
phi = phiHbyA + p_rghEqn.flux();
p_rghEqn.solve(mesh.solver(p_rgh.select(pimple.finalInnerIter())));
// Explicitly relax pressure for momentum corrector
p_rgh.relax();
if (pimple.finalNonOrthogonalIter())
{
// Calculate the conservative fluxes
phi = phiHbyA + p_rghEqn.flux();
// Explicitly relax pressure for momentum corrector
p_rgh.relax();
// Correct the momentum source with the pressure gradient flux
// calculated from the relaxed pressure
U = HbyA + rAU*fvc::reconstruct((phig + p_rghEqn.flux())/rhorAUf);
U.correctBoundaryConditions();
fvOptions.correct(U);
K = 0.5*magSqr(U);
}
// Correct the momentum source with the pressure gradient flux
// calculated from the relaxed pressure
U = HbyA + rAU*fvc::reconstruct((phig + p_rghEqn.flux())/rhorAUf);
U.correctBoundaryConditions();
fvOptions.correct(U);
K = 0.5*magSqr(U);
}
p = p_rgh + rho*gh;
// Second part of thermodynamic density update
thermo.rho() += psi*p;
if (thermo.dpdt())
{
dpdt = fvc::ddt(p);
}
#include "rhoEqn.H"
#include "compressibleContinuityErrs.H"
}
p = p_rgh + rho*gh;
// Thermodynamic density update
thermo.correctRho(psi*p - psip0);
if (thermo.dpdt())
{
dpdt = fvc::ddt(p);
}
#include "rhoEqn.H"
#include "compressibleContinuityErrs.H"

View File

@ -52,6 +52,8 @@ volScalarField& p = thermo.p();
#include "compressibleCreatePhi.H"
pressureControl pressureControl(p, rho, pimple.dict(), false);
mesh.setFluxRequired(p.name());

View File

@ -1,109 +0,0 @@
{
rho = thermo.rho();
// Thermodynamic density needs to be updated by psi*d(p) after the
// pressure solution - done in 2 parts. Part 1:
thermo.rho() -= psi*p;
volScalarField rAU(1.0/UEqn.A());
surfaceScalarField rhorAUf("rhorAUf", fvc::interpolate(rho*rAU));
volVectorField HbyA(constrainHbyA(rAU*UEqn.H(), U, p));
if (pimple.transonic())
{
surfaceScalarField phiHbyA
(
"phiHbyA",
(
fvc::flux(HbyA)
+ rhorAUf*fvc::ddtCorr(rho, U, phi)/fvc::interpolate(rho)
)
);
MRF.makeRelative(phiHbyA);
surfaceScalarField phid("phid", fvc::interpolate(thermo.psi())*phiHbyA);
phiHbyA *= fvc::interpolate(rho);
fvScalarMatrix pDDtEqn
(
fvc::ddt(rho) + fvc::div(phiHbyA)
+ correction(psi*fvm::ddt(p) + fvm::div(phid, p))
);
while (pimple.correctNonOrthogonal())
{
fvScalarMatrix pEqn
(
pDDtEqn
- fvm::laplacian(rhorAUf, p)
==
fvOptions(psi, p, rho.name())
);
pEqn.solve(mesh.solver(p.select(pimple.finalInnerIter())));
if (pimple.finalNonOrthogonalIter())
{
phi = phiHbyA + pEqn.flux();
}
}
}
else
{
surfaceScalarField phiHbyA
(
"phiHbyA",
(
fvc::flux(rho*HbyA)
+ rhorAUf*fvc::ddtCorr(rho, U, phi)
)
);
MRF.makeRelative(fvc::interpolate(rho), phiHbyA);
// Update the pressure BCs to ensure flux consistency
constrainPressure(p, rho, U, phiHbyA, rhorAUf, MRF);
fvScalarMatrix pDDtEqn
(
fvc::ddt(rho) + psi*correction(fvm::ddt(p))
+ fvc::div(phiHbyA)
==
fvOptions(psi, p, rho.name())
);
while (pimple.correctNonOrthogonal())
{
fvScalarMatrix pEqn
(
pDDtEqn
- fvm::laplacian(rhorAUf, p)
);
pEqn.solve(mesh.solver(p.select(pimple.finalInnerIter())));
if (pimple.finalNonOrthogonalIter())
{
phi = phiHbyA + pEqn.flux();
}
}
}
// Second part of thermodynamic density update
thermo.rho() += psi*p;
#include "rhoEqn.H"
#include "compressibleContinuityErrs.H"
U = HbyA - rAU*fvc::grad(p);
U.correctBoundaryConditions();
fvOptions.correct(U);
K = 0.5*magSqr(U);
if (thermo.dpdt())
{
dpdt = fvc::ddt(p);
}
}

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | Copyright (C) 2011-2016 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2017 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -35,6 +35,7 @@ Description
#include "turbulentFluidThermoModel.H"
#include "multivariateScheme.H"
#include "pimpleControl.H"
#include "pressureControl.H"
#include "fvOptions.H"
#include "localEulerDdtScheme.H"
#include "fvcSmooth.H"
@ -97,7 +98,14 @@ int main(int argc, char *argv[])
// --- Pressure corrector loop
while (pimple.correct())
{
#include "pEqn.H"
if (pimple.consistent())
{
#include "../../../compressible/rhoPimpleFoam/pcEqn.H"
}
else
{
#include "../../../compressible/rhoPimpleFoam/pEqn.H"
}
}
if (pimple.turbCorr())

View File

@ -42,6 +42,8 @@ volVectorField U
pressureControl pressureControl(p, rho, pimple.dict(), false);
mesh.setFluxRequired(p.name());
Info<< "Creating turbulence model\n" << endl;
autoPtr<compressible::turbulenceModel> turbulence
(
@ -54,8 +56,6 @@ autoPtr<compressible::turbulenceModel> turbulence
)
);
mesh.setFluxRequired(p.name());
Info<< "Creating field dpdt\n" << endl;
volScalarField dpdt
(

View File

@ -1,4 +1,11 @@
rho = thermo.rho();
if (!pimple.SIMPLErho())
{
rho = thermo.rho();
}
// Thermodynamic density needs to be updated by psi*d(p) after the
// pressure solution
const volScalarField psip0(psi*p);
volScalarField rAU(1.0/UEqn.A());
surfaceScalarField rhorAUf("rhorAUf", fvc::interpolate(rho*rAU));
@ -31,17 +38,17 @@ if (pimple.transonic())
phiHbyA -= fvc::interpolate(psi*p)*phiHbyA/fvc::interpolate(rho);
fvScalarMatrix pDDtEqn
(
fvc::ddt(rho) + psi*correction(fvm::ddt(p))
+ fvc::div(phiHbyA) + fvm::div(phid, p)
==
fvOptions(psi, p, rho.name())
);
while (pimple.correctNonOrthogonal())
{
fvScalarMatrix pEqn
(
fvm::ddt(psi, p)
+ fvc::div(phiHbyA)
+ fvm::div(phid, p)
- fvm::laplacian(rhorAUf, p)
==
fvOptions(psi, p, rho.name())
);
fvScalarMatrix pEqn(pDDtEqn - fvm::laplacian(rhorAUf, p));
// Relax the pressure equation to ensure diagonal-dominance
pEqn.relax();
@ -56,16 +63,17 @@ if (pimple.transonic())
}
else
{
fvScalarMatrix pDDtEqn
(
fvc::ddt(rho) + psi*correction(fvm::ddt(p))
+ fvc::div(phiHbyA)
==
fvOptions(psi, p, rho.name())
);
while (pimple.correctNonOrthogonal())
{
fvScalarMatrix pEqn
(
fvm::ddt(psi, p)
+ fvc::div(phiHbyA)
- fvm::laplacian(rhorAUf, p)
==
fvOptions(psi, p, rho.name())
);
fvScalarMatrix pEqn(pDDtEqn - fvm::laplacian(rhorAUf, p));
pEqn.solve(mesh.solver(p.select(pimple.finalInnerIter())));
@ -76,6 +84,9 @@ else
}
}
// Thermodynamic density update
thermo.correctRho(psi*p - psip0);
#include "rhoEqn.H"
#include "compressibleContinuityErrs.H"
@ -92,10 +103,9 @@ if (pressureControl.limit(p))
p.correctBoundaryConditions();
rho = thermo.rho();
}
if (!pimple.transonic())
else if (pimple.SIMPLErho())
{
rho.relax();
rho = thermo.rho();
}
if (thermo.dpdt())

View File

@ -1,4 +1,11 @@
rho = thermo.rho();
if (!pimple.SIMPLErho())
{
rho = thermo.rho();
}
// Thermodynamic density needs to be updated by psi*d(p) after the
// pressure solution
const volScalarField psip0(psi*p);
volScalarField rAU(1.0/UEqn.A());
volScalarField rAtU(1.0/(1.0/rAU - UEqn.H1()));
@ -39,17 +46,17 @@ if (pimple.transonic())
HbyA -= (rAU - rAtU)*fvc::grad(p);
fvScalarMatrix pDDtEqn
(
fvc::ddt(rho) + psi*correction(fvm::ddt(p))
+ fvc::div(phiHbyA) + fvm::div(phid, p)
==
fvOptions(psi, p, rho.name())
);
while (pimple.correctNonOrthogonal())
{
fvScalarMatrix pEqn
(
fvm::ddt(psi, p)
+ fvc::div(phiHbyA)
+ fvm::div(phid, p)
- fvm::laplacian(rhorAtU, p)
==
fvOptions(psi, p, rho.name())
);
fvScalarMatrix pEqn(pDDtEqn - fvm::laplacian(rhorAtU, p));
// Relax the pressure equation to ensure diagonal-dominance
pEqn.relax();
@ -67,16 +74,17 @@ else
phiHbyA += fvc::interpolate(rho*(rAtU - rAU))*fvc::snGrad(p)*mesh.magSf();
HbyA -= (rAU - rAtU)*fvc::grad(p);
fvScalarMatrix pDDtEqn
(
fvc::ddt(rho) + psi*correction(fvm::ddt(p))
+ fvc::div(phiHbyA)
==
fvOptions(psi, p, rho.name())
);
while (pimple.correctNonOrthogonal())
{
fvScalarMatrix pEqn
(
fvm::ddt(psi, p)
+ fvc::div(phiHbyA)
- fvm::laplacian(rhorAtU, p)
==
fvOptions(psi, p, rho.name())
);
fvScalarMatrix pEqn(pDDtEqn - fvm::laplacian(rhorAtU, p));
pEqn.solve(mesh.solver(p.select(pimple.finalInnerIter())));
@ -87,6 +95,9 @@ else
}
}
// Thermodynamic density update
thermo.correctRho(psi*p - psip0);
#include "rhoEqn.H"
#include "compressibleContinuityErrs.H"
@ -103,10 +114,9 @@ if (pressureControl.limit(p))
p.correctBoundaryConditions();
rho = thermo.rho();
}
if (!pimple.transonic())
else if (pimple.SIMPLErho())
{
rho.relax();
rho = thermo.rho();
}
if (thermo.dpdt())

View File

@ -36,7 +36,7 @@ if (pimple.transonic())
{
fvScalarMatrix pEqn
(
fvm::ddt(psi, p)
fvc::ddt(rho) + psi*correction(fvm::ddt(p))
+ fvc::div(phiHbyA)
+ fvm::div(phid, p)
- fvm::laplacian(rhorAUf, p)
@ -62,7 +62,7 @@ else
// Pressure corrector
fvScalarMatrix pEqn
(
fvm::ddt(psi, p)
fvc::ddt(rho) + psi*correction(fvm::ddt(p))
+ fvc::div(phiHbyA)
- fvm::laplacian(rhorAUf, p)
==
@ -95,11 +95,6 @@ if (pressureControl.limit(p))
rho = thermo.rho();
}
if (!pimple.transonic())
{
rho.relax();
}
{
rhoUf = fvc::interpolate(rho*U);
surfaceVectorField n(mesh.Sf()/mesh.magSf());

View File

@ -119,6 +119,8 @@ int main(int argc, char *argv[])
}
}
rho = thermo.rho();
runTime.write();
Info<< "ExecutionTime = " << runTime.elapsedCpuTime() << " s"

View File

@ -1,76 +1,74 @@
rho = thermo.rho();
// Thermodynamic density needs to be updated by psi*d(p) after the
// pressure solution
const volScalarField psip0(psi*p);
volScalarField rAU(1.0/UEqn.A());
surfaceScalarField rhorAUf("rhorAUf", fvc::interpolate(rho*rAU));
volVectorField HbyA(constrainHbyA(rAU*UEqn.H(), U, p_rgh));
surfaceScalarField phig(-rhorAUf*ghf*fvc::snGrad(rho)*mesh.magSf());
surfaceScalarField phiHbyA
(
"phiHbyA",
(
fvc::flux(rho*HbyA)
+ rhorAUf*fvc::ddtCorr(rho, U, phi)
)
+ phig
);
MRF.makeRelative(fvc::interpolate(rho), phiHbyA);
// Update the pressure BCs to ensure flux consistency
constrainPressure(p_rgh, rho, U, phiHbyA, rhorAUf, MRF);
fvScalarMatrix p_rghDDtEqn
(
fvc::ddt(rho) + psi*correction(fvm::ddt(p_rgh))
+ fvc::div(phiHbyA)
==
fvOptions(psi, p_rgh, rho.name())
);
while (pimple.correctNonOrthogonal())
{
rho = thermo.rho();
// Thermodynamic density needs to be updated by psi*d(p) after the
// pressure solution - done in 2 parts. Part 1:
thermo.rho() -= psi*p_rgh;
volScalarField rAU(1.0/UEqn.A());
surfaceScalarField rhorAUf("rhorAUf", fvc::interpolate(rho*rAU));
volVectorField HbyA(constrainHbyA(rAU*UEqn.H(), U, p_rgh));
surfaceScalarField phig(-rhorAUf*ghf*fvc::snGrad(rho)*mesh.magSf());
surfaceScalarField phiHbyA
fvScalarMatrix p_rghEqn
(
"phiHbyA",
(
fvc::flux(rho*HbyA)
+ rhorAUf*fvc::ddtCorr(rho, U, phi)
)
+ phig
p_rghDDtEqn
- fvm::laplacian(rhorAUf, p_rgh)
);
MRF.makeRelative(fvc::interpolate(rho), phiHbyA);
p_rghEqn.solve(mesh.solver(p_rgh.select(pimple.finalInnerIter())));
// Update the pressure BCs to ensure flux consistency
constrainPressure(p_rgh, rho, U, phiHbyA, rhorAUf, MRF);
fvScalarMatrix p_rghDDtEqn
(
fvc::ddt(rho) + psi*correction(fvm::ddt(p_rgh))
+ fvc::div(phiHbyA)
==
fvOptions(psi, p_rgh, rho.name())
);
while (pimple.correctNonOrthogonal())
if (pimple.finalNonOrthogonalIter())
{
fvScalarMatrix p_rghEqn
(
p_rghDDtEqn
- fvm::laplacian(rhorAUf, p_rgh)
);
// Calculate the conservative fluxes
phi = phiHbyA + p_rghEqn.flux();
p_rghEqn.solve(mesh.solver(p_rgh.select(pimple.finalInnerIter())));
// Explicitly relax pressure for momentum corrector
p_rgh.relax();
if (pimple.finalNonOrthogonalIter())
{
// Calculate the conservative fluxes
phi = phiHbyA + p_rghEqn.flux();
// Explicitly relax pressure for momentum corrector
p_rgh.relax();
// Correct the momentum source with the pressure gradient flux
// calculated from the relaxed pressure
U = HbyA + rAU*fvc::reconstruct((phig + p_rghEqn.flux())/rhorAUf);
U.correctBoundaryConditions();
fvOptions.correct(U);
K = 0.5*magSqr(U);
}
// Correct the momentum source with the pressure gradient flux
// calculated from the relaxed pressure
U = HbyA + rAU*fvc::reconstruct((phig + p_rghEqn.flux())/rhorAUf);
U.correctBoundaryConditions();
fvOptions.correct(U);
K = 0.5*magSqr(U);
}
p = p_rgh + rho*gh;
// Second part of thermodynamic density update
thermo.rho() += psi*p_rgh;
if (thermo.dpdt())
{
dpdt = fvc::ddt(p);
}
#include "rhoEqn.H"
#include "compressibleContinuityErrs.H"
}
p = p_rgh + rho*gh;
// Thermodynamic density update
thermo.correctRho(psi*p - psip0);
if (thermo.dpdt())
{
dpdt = fvc::ddt(p);
}
#include "rhoEqn.H"
#include "compressibleContinuityErrs.H"

View File

@ -1,101 +1,99 @@
{
bool closedVolume = p_rgh.needReference();
dimensionedScalar compressibility = fvc::domainIntegrate(psi);
bool compressible = (compressibility.value() > SMALL);
bool closedVolume = p_rgh.needReference();
dimensionedScalar compressibility = fvc::domainIntegrate(psi);
bool compressible = (compressibility.value() > SMALL);
rho = thermo.rho();
rho = thermo.rho();
volScalarField rAU("rAU", 1.0/UEqn.A());
surfaceScalarField rhorAUf("rhorAUf", fvc::interpolate(rho*rAU));
volVectorField HbyA(constrainHbyA(rAU*UEqn.H(), U, p_rgh));
volScalarField rAU("rAU", 1.0/UEqn.A());
surfaceScalarField rhorAUf("rhorAUf", fvc::interpolate(rho*rAU));
volVectorField HbyA(constrainHbyA(rAU*UEqn.H(), U, p_rgh));
surfaceScalarField phig(-rhorAUf*ghf*fvc::snGrad(rho)*mesh.magSf());
surfaceScalarField phig(-rhorAUf*ghf*fvc::snGrad(rho)*mesh.magSf());
surfaceScalarField phiHbyA
surfaceScalarField phiHbyA
(
"phiHbyA",
(
"phiHbyA",
(
fvc::flux(rho*HbyA)
+ rhorAUf*fvc::ddtCorr(rho, U, phi)
)
+ phig
fvc::flux(rho*HbyA)
+ rhorAUf*fvc::ddtCorr(rho, U, phi)
)
+ phig
);
MRF.makeRelative(fvc::interpolate(rho), phiHbyA);
// Update the pressure BCs to ensure flux consistency
constrainPressure(p_rgh, rho, U, phiHbyA, rhorAUf, MRF);
{
fvScalarMatrix p_rghDDtEqn
(
fvc::ddt(rho) + psi*correction(fvm::ddt(p_rgh))
+ fvc::div(phiHbyA)
);
MRF.makeRelative(fvc::interpolate(rho), phiHbyA);
// Update the pressure BCs to ensure flux consistency
constrainPressure(p_rgh, rho, U, phiHbyA, rhorAUf, MRF);
// Thermodynamic density needs to be updated by psi*d(p) after the
// pressure solution
const volScalarField psip0(psi*p);
for (int nonOrth=0; nonOrth<=nNonOrthCorr; nonOrth++)
{
fvScalarMatrix p_rghDDtEqn
fvScalarMatrix p_rghEqn
(
fvc::ddt(rho) + psi*correction(fvm::ddt(p_rgh))
+ fvc::div(phiHbyA)
p_rghDDtEqn
- fvm::laplacian(rhorAUf, p_rgh)
);
// Thermodynamic density needs to be updated by psi*d(p) after the
// pressure solution - done in 2 parts. Part 1:
thermo.rho() -= psi*p_rgh;
for (int nonOrth=0; nonOrth<=nNonOrthCorr; nonOrth++)
{
fvScalarMatrix p_rghEqn
solvPerfp_rgh = p_rghEqn.solve
(
mesh.solver
(
p_rghDDtEqn
- fvm::laplacian(rhorAUf, p_rgh)
);
solvPerfp_rgh = p_rghEqn.solve
(
mesh.solver
p_rgh.select
(
p_rgh.select
(
(
oCorr == nOuterCorr-1
&& corr == nCorr-1
&& nonOrth == nNonOrthCorr
)
oCorr == nOuterCorr-1
&& corr == nCorr-1
&& nonOrth == nNonOrthCorr
)
)
);
)
);
if (nonOrth == nNonOrthCorr)
{
phi = phiHbyA + p_rghEqn.flux();
U = HbyA
+ rAU*fvc::reconstruct((phig + p_rghEqn.flux())/rhorAUf);
U.correctBoundaryConditions();
fvOptions.correct(U);
K = 0.5*magSqr(U);
}
if (nonOrth == nNonOrthCorr)
{
phi = phiHbyA + p_rghEqn.flux();
U = HbyA
+ rAU*fvc::reconstruct((phig + p_rghEqn.flux())/rhorAUf);
U.correctBoundaryConditions();
fvOptions.correct(U);
K = 0.5*magSqr(U);
}
// Second part of thermodynamic density update
thermo.rho() += psi*p_rgh;
}
p = p_rgh + rho*gh;
// Update pressure time derivative if needed
if (thermo.dpdt())
{
dpdt = fvc::ddt(p);
}
// Solve continuity
#include "rhoEqn.H"
// Update continuity errors
#include "compressibleContinuityErrors.H"
// For closed-volume cases adjust the pressure and density levels
// to obey overall mass continuity
if (closedVolume && compressible)
{
p += (initialMass - fvc::domainIntegrate(thermo.rho()))
/compressibility;
rho = thermo.rho();
p_rgh = p - rho*gh;
}
// Thermodynamic density update
thermo.correctRho(psi*p - psip0);
}
p = p_rgh + rho*gh;
// Update pressure time derivative if needed
if (thermo.dpdt())
{
dpdt = fvc::ddt(p);
}
// Solve continuity
#include "rhoEqn.H"
// Update continuity errors
#include "compressibleContinuityErrors.H"
// For closed-volume cases adjust the pressure and density levels
// to obey overall mass continuity
if (closedVolume && compressible)
{
p += (initialMass - fvc::domainIntegrate(thermo.rho()))
/compressibility;
rho = thermo.rho();
p_rgh = p - rho*gh;
}

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | Copyright (C) 2011-2016 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2017 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -39,6 +39,7 @@ Description
#include "radiationModel.H"
#include "SLGThermo.H"
#include "pimpleControl.H"
#include "pressureControl.H"
#include "localEulerDdtScheme.H"
#include "fvcSmooth.H"

View File

@ -1,73 +1,71 @@
rho = thermo.rho();
// Thermodynamic density needs to be updated by psi*d(p) after the
// pressure solution
const volScalarField psip0(psi*p);
volScalarField rAU(1.0/UEqn.A());
surfaceScalarField rhorAUf("rhorAUf", fvc::interpolate(rho*rAU));
volVectorField HbyA(constrainHbyA(rAU*UEqn.H(), U, p));
surfaceScalarField phiHbyA
(
"phiHbyA",
(
fvc::flux(rho*HbyA)
+ rhorAUf*fvc::ddtCorr(rho, U, phi)
)
);
MRF.makeRelative(fvc::interpolate(rho), phiHbyA);
// Update the pressure BCs to ensure flux consistency
constrainPressure(p, rho, U, phiHbyA, rhorAUf, MRF);
fvScalarMatrix pDDtEqn
(
fvc::ddt(rho) + psi*correction(fvm::ddt(p))
+ fvc::div(phiHbyA)
==
parcels.Srho()
+ fvOptions(psi, p, rho.name())
);
while (pimple.correctNonOrthogonal())
{
rho = thermo.rho();
// Thermodynamic density needs to be updated by psi*d(p) after the
// pressure solution - done in 2 parts. Part 1:
thermo.rho() -= psi*p;
volScalarField rAU(1.0/UEqn.A());
surfaceScalarField rhorAUf("rhorAUf", fvc::interpolate(rho*rAU));
volVectorField HbyA(constrainHbyA(rAU*UEqn.H(), U, p));
surfaceScalarField phiHbyA
fvScalarMatrix pEqn
(
"phiHbyA",
(
fvc::flux(rho*HbyA)
+ rhorAUf*fvc::ddtCorr(rho, U, phi)
)
pDDtEqn
- fvm::laplacian(rhorAUf, p)
);
MRF.makeRelative(fvc::interpolate(rho), phiHbyA);
pEqn.solve(mesh.solver(p.select(pimple.finalInnerIter())));
// Update the pressure BCs to ensure flux consistency
constrainPressure(p, rho, U, phiHbyA, rhorAUf, MRF);
fvScalarMatrix pDDtEqn
(
fvc::ddt(rho) + psi*correction(fvm::ddt(p))
+ fvc::div(phiHbyA)
==
parcels.Srho()
+ fvOptions(psi, p, rho.name())
);
while (pimple.correctNonOrthogonal())
if (pimple.finalNonOrthogonalIter())
{
fvScalarMatrix pEqn
(
pDDtEqn
- fvm::laplacian(rhorAUf, p)
);
pEqn.solve(mesh.solver(p.select(pimple.finalInnerIter())));
if (pimple.finalNonOrthogonalIter())
{
phi = phiHbyA + pEqn.flux();
}
phi = phiHbyA + pEqn.flux();
}
p.relax();
// Second part of thermodynamic density update
thermo.rho() += psi*p;
#include "rhoEqn.H" // NOTE: flux and time scales now inconsistent
#include "compressibleContinuityErrs.H"
U = HbyA - rAU*fvc::grad(p);
U.correctBoundaryConditions();
fvOptions.correct(U);
K = 0.5*magSqr(U);
if (thermo.dpdt())
{
dpdt = fvc::ddt(p);
}
rho = thermo.rho();
rho = max(rho, rhoMin);
rho = min(rho, rhoMax);
Info<< "p min/max = " << min(p).value() << ", " << max(p).value() << endl;
}
p.relax();
// Thermodynamic density update
thermo.correctRho(psi*p - psip0);
#include "rhoEqn.H" // NOTE: flux and time scales now inconsistent
#include "compressibleContinuityErrs.H"
U = HbyA - rAU*fvc::grad(p);
U.correctBoundaryConditions();
fvOptions.correct(U);
K = 0.5*magSqr(U);
if (thermo.dpdt())
{
dpdt = fvc::ddt(p);
}
rho = thermo.rho();
rho = max(rho, rhoMin);
rho = min(rho, rhoMax);
Info<< "p min/max = " << min(p).value() << ", " << max(p).value() << endl;

View File

@ -1,57 +1,55 @@
{
// Thermodynamic density needs to be updated by psi*d(p) after the
// pressure solution - done in 2 parts. Part 1:
thermo.rho() -= psi*p;
// Thermodynamic density needs to be updated by psi*d(p) after the
// pressure solution
const volScalarField psip0(psi*p);
volScalarField rAU(1.0/UEqn.A());
surfaceScalarField rhorAUf("rhorAUf", fvc::interpolate(rho*rAU));
volVectorField HbyA(constrainHbyA(rAU*UEqn.H(), U, p));
tUEqn.clear();
surfaceScalarField phiHbyA
volScalarField rAU(1.0/UEqn.A());
surfaceScalarField rhorAUf("rhorAUf", fvc::interpolate(rho*rAU));
volVectorField HbyA(constrainHbyA(rAU*UEqn.H(), U, p));
tUEqn.clear();
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);
while (simple.correctNonOrthogonal())
{
fvScalarMatrix pEqn
(
"phiHbyA",
fvc::interpolate(rho)*fvc::flux(HbyA)
fvc::div(phiHbyA)
- fvm::laplacian(rhorAUf, p)
==
parcels.Srho()
+ fvOptions(psi, p, rho.name())
);
MRF.makeRelative(fvc::interpolate(rho), phiHbyA);
pEqn.solve();
// Update the pressure BCs to ensure flux consistency
constrainPressure(p, rho, U, phiHbyA, rhorAUf, MRF);
while (simple.correctNonOrthogonal())
if (simple.finalNonOrthogonalIter())
{
fvScalarMatrix pEqn
(
fvc::div(phiHbyA)
- fvm::laplacian(rhorAUf, p)
==
parcels.Srho()
+ fvOptions(psi, p, rho.name())
);
pEqn.solve();
if (simple.finalNonOrthogonalIter())
{
phi = phiHbyA + pEqn.flux();
}
phi = phiHbyA + pEqn.flux();
}
p.relax();
// Second part of thermodynamic density update
thermo.rho() += psi*p;
#include "compressibleContinuityErrs.H"
U = HbyA - rAU*fvc::grad(p);
U.correctBoundaryConditions();
fvOptions.correct(U);
rho = thermo.rho();
rho = max(rho, rhoMin);
rho = min(rho, rhoMax);
rho.relax();
Info<< "p min/max = " << min(p).value() << ", " << max(p).value() << endl;
}
p.relax();
// Thermodynamic density update
thermo.correctRho(psi*p - psip0);
#include "compressibleContinuityErrs.H"
U = HbyA - rAU*fvc::grad(p);
U.correctBoundaryConditions();
fvOptions.correct(U);
rho = thermo.rho();
rho = max(rho, rhoMin);
rho = min(rho, rhoMax);
rho.relax();
Info<< "p min/max = " << min(p).value() << ", " << max(p).value() << endl;

View File

@ -113,8 +113,8 @@
}
// Update densities from change in p_rgh
rho1 += psi1*(p_rgh - p_rgh_0);
rho2 += psi2*(p_rgh - p_rgh_0);
mixture.thermo1().correctRho(psi1*(p_rgh - p_rgh_0));
mixture.thermo2().correctRho(psi2*(p_rgh - p_rgh_0));
rho = alpha1*rho1 + alpha2*rho2;

View File

@ -38,8 +38,8 @@ volScalarField& alpha2(mixture.alpha2());
Info<< "Reading thermophysical properties\n" << endl;
volScalarField& rho1 = mixture.thermo1().rho();
volScalarField& rho2 = mixture.thermo2().rho();
const volScalarField& rho1 = mixture.thermo1().rho();
const volScalarField& rho2 = mixture.thermo2().rho();
volScalarField rho
(

View File

@ -104,8 +104,8 @@
}
// Update densities from change in p_rgh
rho1 += psi1*(p_rgh - p_rgh_0);
rho2 += psi2*(p_rgh - p_rgh_0);
mixture.thermo1().correctRho(psi1*(p_rgh - p_rgh_0));
mixture.thermo2().correctRho(psi2*(p_rgh - p_rgh_0));
rho = alpha1*rho1 + alpha2*rho2;

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | Copyright (C) 2011-2016 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2017 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -45,6 +45,7 @@ void Foam::pimpleControl::read()
solveFlow_ = pimpleDict.lookupOrDefault<Switch>("solveFlow", true);
nCorrPIMPLE_ = pimpleDict.lookupOrDefault<label>("nOuterCorrectors", 1);
nCorrPISO_ = pimpleDict.lookupOrDefault<label>("nCorrectors", 1);
SIMPLErho_ = pimpleDict.lookupOrDefault<Switch>("SIMPLErho", false);
turbOnFinalIterOnly_ =
pimpleDict.lookupOrDefault<Switch>("turbOnFinalIterOnly", true);
}
@ -128,6 +129,7 @@ Foam::pimpleControl::pimpleControl(fvMesh& mesh, const word& dictName)
nCorrPIMPLE_(0),
nCorrPISO_(0),
corrPISO_(0),
SIMPLErho_(false),
turbOnFinalIterOnly_(true),
converged_(false)
{

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | Copyright (C) 2011-2016 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2017 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -81,6 +81,10 @@ protected:
//- Current PISO corrector
label corrPISO_;
//- Flag to indicate whether to update density in SIMPLE
// rather than PISO mode
bool SIMPLErho_;
//- Flag to indicate whether to only solve turbulence on final iter
bool turbOnFinalIterOnly_;
@ -128,6 +132,10 @@ public:
//- Current PISO corrector index
inline label corrPISO() const;
//- Flag to indicate whether to update density in SIMPLE
// rather than PISO mode
inline bool SIMPLErho() const;
// Solution control

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | Copyright (C) 2011-2016 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2017 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -43,6 +43,12 @@ inline Foam::label Foam::pimpleControl::corrPISO() const
}
inline bool Foam::pimpleControl::SIMPLErho() const
{
return SIMPLErho_;
}
inline bool Foam::pimpleControl::correct()
{
corrPISO_++;

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | Copyright (C) 2012-2015 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2012-2017 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -103,6 +103,10 @@ public:
// Access to thermodynamic state variables
//- Add the given density correction to the density field.
// Used to update the density field following pressure solution
virtual void correctRho(const volScalarField& deltaRho) = 0;
//- Compressibility [s^2/m^2]
virtual const volScalarField& psi() const = 0;

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | Copyright (C) 2011-2015 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2017 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -102,6 +102,10 @@ Foam::tmp<Foam::scalarField> Foam::psiThermo::rho(const label patchi) const
}
void Foam::psiThermo::correctRho(const Foam::volScalarField& deltaRho)
{}
const Foam::volScalarField& Foam::psiThermo::psi() const
{
return psi_;

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | Copyright (C) 2011-2015 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2017 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -112,6 +112,11 @@ public:
// Fields derived from thermodynamic state variables
//- Add the given density correction to the density field.
// Used to update the density field following pressure solution.
// For psiThermo does nothing.
virtual void correctRho(const volScalarField& deltaRho);
//- Density [kg/m^3] - uses current value of pressure
virtual tmp<volScalarField> rho() const;

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | Copyright (C) 2011-2015 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2017 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -173,6 +173,12 @@ Foam::volScalarField& Foam::rhoThermo::rho()
}
void Foam::rhoThermo::correctRho(const Foam::volScalarField& deltaRho)
{
rho_ += deltaRho;
}
const Foam::volScalarField& Foam::rhoThermo::psi() const
{
return psi_;

View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | Copyright (C) 2011-2015 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2017 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -133,6 +133,10 @@ public:
//- Return non-const access to the local density field [kg/m^3]
virtual volScalarField& rho();
//- Add the given density correction to the density field.
// Used to update the density field following pressure solution
virtual void correctRho(const volScalarField& deltaRho);
//- Compressibility [s^2/m^2]
virtual const volScalarField& psi() const;

View File

@ -54,6 +54,7 @@ PIMPLE
nCorrectors 1;
nNonOrthogonalCorrectors 0;
consistent yes;
SIMPLErho yes;
pMaxFactor 1.5;
pMinFactor 0.9;

View File

@ -0,0 +1,42 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object T;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 1 0 0 0];
internalField uniform 300;
boundaryField
{
Default_Boundary_Region
{
type fixedValue;
value uniform 350;
}
inlet
{
type fixedValue;
value $internalField;
}
outlet
{
type inletOutlet;
inletValue $internalField;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,43 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volVectorField;
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
Default_Boundary_Region
{
type noSlip;
}
inlet
{
type flowRateInletVelocity;
massFlowRate constant 5;
rhoInlet 1000; // Guess for rho
}
outlet
{
type pressureInletOutletVelocity;
value $internalField;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,45 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ 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
{
Default_Boundary_Region
{
type compressible::alphatWallFunction;
Prt 0.85;
value uniform 0;
}
inlet
{
type calculated;
value uniform 0;
}
outlet
{
type calculated;
value uniform 0;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,49 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object epsilon;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -3 0 0 0 0];
internalField uniform 200;
boundaryField
{
Default_Boundary_Region
{
type epsilonWallFunction;
Cmu 0.09;
kappa 0.41;
E 9.8;
value uniform 200;
}
inlet
{
type turbulentMixingLengthDissipationRateInlet;
mixingLength 0.005;
value uniform 200;
}
outlet
{
type inletOutlet;
inletValue uniform 200;
value uniform 200;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,46 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 1;
boundaryField
{
Default_Boundary_Region
{
type kqRWallFunction;
value uniform 1;
}
inlet
{
type turbulentIntensityKineticEnergyInlet;
intensity 0.05;
value uniform 1;
}
outlet
{
type inletOutlet;
inletValue uniform 1;
value uniform 1;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,47 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object nut;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
Default_Boundary_Region
{
type nutkWallFunction;
Cmu 0.09;
kappa 0.41;
E 9.8;
value uniform 0;
}
inlet
{
type calculated;
value uniform 0;
}
outlet
{
type calculated;
value uniform 0;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,41 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object p;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -2 0 0 0 0];
internalField uniform 1e5;
boundaryField
{
Default_Boundary_Region
{
type zeroGradient;
}
inlet
{
type zeroGradient;
}
outlet
{
type fixedValue;
value $internalField;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,31 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object thermophysicalProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
thermoType
{
type heRhoThermo;
mixture pureMixture;
properties liquid;
energy sensibleInternalEnergy;
}
mixture
{
H2O;
}
// ************************************************************************* //

View File

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

View File

@ -0,0 +1,127 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object blockMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
convertToMeters 0.001;
vertices
(
// front-plane: z = +25mm
// inlet region
( -50 25 25) // pt 0
( 0 25 25) // pt 1
( -50 75 25) // pt 2
( 0 75 25) // pt 3
// outlet region
( -500 -75 25) // pt 4
( 0 -75 25) // pt 5
( -500 -25 25) // pt 6
( 0 -25 25) // pt 7
// bend mid-points
( 25 0 25) // pt 8
( 75 0 25) // pt 9
// back-plane: z = -25mm
// inlet region
( -50 25 -25) // pt 0 + 10
( 0 25 -25) // pt 1 + 10
( -50 75 -25) // pt 2 + 10
( 0 75 -25) // pt 3 + 10
// outlet region
( -500 -75 -25) // pt 4 + 10
( 0 -75 -25) // pt 5 + 10
( -500 -25 -25) // pt 7 + 10
( 0 -25 -25) // pt 8 + 10
// bend mid-points
( 25 0 -25) // pt 8 + 10
( 75 0 -25) // pt 9 + 10
);
blocks
(
hex (0 1 11 10 2 3 13 12) inlet ( 20 20 20) simpleGrading (1 1 1)
hex (4 5 15 14 6 7 17 16) outlet (200 20 20) simpleGrading (1 1 1)
hex (1 8 18 11 3 9 19 13) bend1 ( 30 20 20) simpleGrading (1 1 1)
hex (5 9 19 15 7 8 18 17) bend2 ( 30 20 20) simpleGrading (1 1 1)
);
edges
(
// block 2
arc 1 8 ( 17.678 17.678 25)
arc 11 18 ( 17.678 17.678 -25)
arc 3 9 ( 53.033 53.033 25)
arc 13 19 ( 53.033 53.033 -25)
// block 3
arc 7 8 ( 17.678 -17.678 25)
arc 17 18 ( 17.678 -17.678 -25)
arc 5 9 ( 53.033 -53.033 25)
arc 15 19 ( 53.033 -53.033 -25)
);
boundary
(
// is there no way of defining all my 'defaultFaces' to be 'wall'?
Default_Boundary_Region
{
type wall;
faces
(
// block0
( 0 1 3 2 )
( 11 10 12 13 )
( 0 10 11 1 )
( 2 3 13 12 )
// block1
( 4 5 7 6 )
( 15 14 16 17 )
( 4 14 15 5 )
( 6 7 17 16 )
// block2
( 1 8 9 3 )
( 18 11 13 19 )
( 3 9 19 13 )
( 1 11 18 8 )
// block3
( 5 9 8 7 )
( 19 15 17 18 )
( 5 15 19 9 )
( 7 8 18 17 )
);
}
inlet
{
type patch;
faces
(
(0 2 12 10)
);
}
outlet
{
type patch;
faces
(
(4 6 16 14)
);
}
);
mergePatchPairs
(
);
// ************************************************************************* //

View File

@ -0,0 +1,51 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application rhoPimpleFoam;
startFrom startTime;
startTime 0;
stopAt endTime;
endTime 0.5;
deltaT 2e-3;
writeControl timeStep;
writeInterval 10;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
writeCompression off;
timeFormat general;
timePrecision 6;
graphFormat raw;
runTimeModifiable true;
// ************************************************************************* //

View File

@ -0,0 +1,45 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object decomposeParDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
numberOfSubdomains 8;
method hierarchical;
simpleCoeffs
{
n (8 1 1);
delta 0.001;
}
hierarchicalCoeffs
{
n (4 2 1);
delta 0.001;
order xyz;
}
manualCoeffs
{
dataFile "";
}
distributed no;
roots ( );
// ************************************************************************* //

View File

@ -0,0 +1,60 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default Euler;
}
gradSchemes
{
default Gauss linear;
limited cellLimited Gauss linear 1;
}
divSchemes
{
default none;
div(phi,U) Gauss linearUpwind limited;
div(phi,e) Gauss linearUpwind limited;
div(phi,epsilon) Gauss linearUpwind limited;
div(phi,k) Gauss linearUpwind limited;
div(phi,K) Gauss linearUpwind limited;
div(phiv,p) Gauss linearUpwind limited;
div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;
}
laplacianSchemes
{
default Gauss linear corrected;
}
interpolationSchemes
{
default linear;
}
snGradSchemes
{
default corrected;
}
// ************************************************************************* //

View File

@ -0,0 +1,63 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
"rho.*"
{
solver nthn;
}
"p.*"
{
solver GAMG;
smoother GaussSeidel;
tolerance 1e-7;
relTol 0;
}
"(U|e|k|epsilon).*"
{
solver PBiCGStab;
preconditioner DILU;
tolerance 1e-7;
relTol 0;
}
}
PIMPLE
{
nCorrectors 3;
nNonOrthogonalCorrectors 0;
pMinFactor 0.1;
pMaxFactor 1.5;
transonic no;
consistent no;
}
relaxationFactors
{
equations
{
".*" 1;
}
}
// ************************************************************************* //