void Foam::combustionModels::PaSR<Type>::correct()
{
if (this->active())
{
laminar<Type>::correct();
if (turbulentReaction_)
{
tmp<volScalarField> tepsilon(this->turbulence().epsilon());
const volScalarField& epsilon = tepsilon();
tmp<volScalarField> tmuEff(this->turbulence().muEff());
const volScalarField& muEff = tmuEff();
tmp<volScalarField> ttc(this->tc());
const volScalarField& tc = ttc();
tmp<volScalarField> trho(this->rho());
const volScalarField& rho = trho();
forAll(epsilon, i)
{
scalar tk =
Cmix_*sqrt(max(muEff[i]/rho[i]/(epsilon[i] + SMALL), 0));
if (tk > SMALL)
{
kappa_[i] = tc[i]/(tc[i] + tk);
}
else
{
kappa_[i] = 1.0;
}
}
}
void Foam::combustionModels::EDC<ReactionThermo>::correct()
{
tmp<volScalarField> tepsilon(this->turbulence().epsilon());
const volScalarField& epsilon = tepsilon();
tmp<volScalarField> tmu(this->turbulence().mu());
const volScalarField& mu = tmu();
tmp<volScalarField> tk(this->turbulence().k());
const volScalarField& k = tk();
tmp<volScalarField> trho(this->rho());
const volScalarField& rho = trho();
scalarField tauStar(epsilon.size(), 0);
if (version_ == EDCversions::v2016)
{
tmp<volScalarField> ttc(this->chemistryPtr_->tc());
const volScalarField& tc = ttc();
forAll(tauStar, i)
{
const scalar nu = mu[i]/(rho[i] + small);
const scalar Da =
max(min(sqrt(nu/(epsilon[i] + small))/tc[i], 10), 1e-10);
const scalar ReT = sqr(k[i])/(nu*epsilon[i] + small);
const scalar CtauI = min(C1_/(Da*sqrt(ReT + 1)), 2.1377);
const scalar CgammaI =
max(min(C2_*sqrt(Da*(ReT + 1)), 5), 0.4082);
const scalar gammaL =
CgammaI*pow025(nu*epsilon[i]/(sqr(k[i]) + small));
tauStar[i] = CtauI*sqrt(nu/(epsilon[i] + small));
if (gammaL >= 1)
{
kappa_[i] = 1;
}
else
{
kappa_[i] =
max
(
min
(
pow(gammaL, exp1_)/(1 - pow(gammaL, exp2_)),
1
),
0
);
}
}
}
void Foam::combustionModels::PaSR<Type>::correct()
{
if (this->active())
{
const scalar t = this->mesh().time().value();
const scalar dt = this->mesh().time().deltaTValue();
if (!useReactionRate_)
{
this->chemistryPtr_->solve(t - dt, dt);
}
else
{
this->chemistryPtr_->calculate();
}
if (turbulentReaction_)
{
tmp<volScalarField> trho(this->rho());
const volScalarField& rho = trho();
tmp<volScalarField> tepsilon(this->turbulence().epsilon());
const volScalarField& epsilon = tepsilon();
tmp<volScalarField> tmuEff(this->turbulence().muEff());
const volScalarField& muEff = tmuEff();
tmp<volScalarField> ttc(tc());
const volScalarField& tc = ttc();
forAll(epsilon, i)
{
if (epsilon[i] > 0)
{
scalar tk =
Cmix_*Foam::sqrt(muEff[i]/rho[i]/(epsilon[i] + SMALL));
// Chalmers PaSR model
if (!useReactionRate_)
{
kappa_[i] = (dt + tc[i])/(dt + tc[i] + tk);
}
else
{
kappa_[i] = tc[i]/(tc[i] + tk);
}
}
else
{
// Return to laminar combustion
kappa_[i] = 1.0;
}
}
}
else
{
kappa_ = 1.0;
}
}
void Foam::DispersionRASModel<CloudType>::cacheFields(const bool store)
{
if (store)
{
tmp<volScalarField> tk = this->kModel();
if (tk.isTmp())
{
kPtr_ = tk.ptr();
ownK_ = true;
}
else
{
kPtr_ = &tk();
ownK_ = false;
}
tmp<volScalarField> tepsilon = this->epsilonModel();
if (tepsilon.isTmp())
{
epsilonPtr_ = tepsilon.ptr();
ownEpsilon_ = true;
}
else
{
epsilonPtr_ = &tepsilon();
ownEpsilon_ = false;
}
}
else
{
if (ownK_ && kPtr_)
{
deleteDemandDrivenData(kPtr_);
ownK_ = false;
}
if (ownEpsilon_ && epsilonPtr_)
{
deleteDemandDrivenData(epsilonPtr_);
ownEpsilon_ = false;
}
}
}
int main(int argc, char *argv[])
{
argList::addNote
(
"apply a simplified boundary-layer model to the velocity and\n"
"turbulence fields based on the 1/7th power-law."
);
argList::addOption
(
"ybl",
"scalar",
"specify the boundary-layer thickness"
);
argList::addOption
(
"Cbl",
"scalar",
"boundary-layer thickness as Cbl * mean distance to wall"
);
argList::addBoolOption
(
"writenut",
"write nut field"
);
#include "setRootCase.H"
if (!args.optionFound("ybl") && !args.optionFound("Cbl"))
{
FatalErrorIn(args.executable())
<< "Neither option 'ybl' or 'Cbl' have been provided to calculate "
<< "the boundary-layer thickness.\n"
<< "Please choose either 'ybl' OR 'Cbl'."
<< exit(FatalError);
}
else if (args.optionFound("ybl") && args.optionFound("Cbl"))
{
FatalErrorIn(args.executable())
<< "Both 'ybl' and 'Cbl' have been provided to calculate "
<< "the boundary-layer thickness.\n"
<< "Please choose either 'ybl' OR 'Cbl'."
<< exit(FatalError);
}
#include "createTime.H"
#include "createMesh.H"
#include "createFields.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// Modify velocity by applying a 1/7th power law boundary-layer
// u/U0 = (y/ybl)^(1/7)
// assumes U0 is the same as the current cell velocity
Info<< "Setting boundary layer velocity" << nl << endl;
scalar yblv = ybl.value();
forAll(U, cellI)
{
if (y[cellI] <= yblv)
{
mask[cellI] = 1;
U[cellI] *= ::pow(y[cellI]/yblv, (1.0/7.0));
}
}
mask.correctBoundaryConditions();
Info<< "Writing U\n" << endl;
U.write();
// Update/re-write phi
#include "createPhi.H"
phi.write();
singlePhaseTransportModel laminarTransport(U, phi);
autoPtr<incompressible::turbulenceModel> turbulence
(
incompressible::turbulenceModel::New(U, phi, laminarTransport)
);
if (isA<incompressible::RASModel>(turbulence()))
{
// Calculate nut - reference nut is calculated by the turbulence model
// on its construction
tmp<volScalarField> tnut = turbulence->nut();
volScalarField& nut = tnut();
volScalarField S(mag(dev(symm(fvc::grad(U)))));
nut = (1 - mask)*nut + mask*sqr(kappa*min(y, ybl))*::sqrt(2)*S;
// do not correct BC - wall functions will 'undo' manipulation above
// by using nut from turbulence model
if (args.optionFound("writenut"))
{
Info<< "Writing nut" << endl;
nut.write();
}
//--- Read and modify turbulence fields
// Turbulence k
tmp<volScalarField> tk = turbulence->k();
volScalarField& k = tk();
scalar ck0 = pow025(Cmu)*kappa;
k = (1 - mask)*k + mask*sqr(nut/(ck0*min(y, ybl)));
// do not correct BC - operation may use inconsistent fields wrt these
// local manipulations
// k.correctBoundaryConditions();
Info<< "Writing k\n" << endl;
k.write();
// Turbulence epsilon
tmp<volScalarField> tepsilon = turbulence->epsilon();
volScalarField& epsilon = tepsilon();
scalar ce0 = ::pow(Cmu, 0.75)/kappa;
epsilon = (1 - mask)*epsilon + mask*ce0*k*sqrt(k)/min(y, ybl);
// do not correct BC - wall functions will use non-updated k from
// turbulence model
// epsilon.correctBoundaryConditions();
Info<< "Writing epsilon\n" << endl;
epsilon.write();
// Turbulence omega
IOobject omegaHeader
(
"omega",
runTime.timeName(),
mesh,
IOobject::MUST_READ,
IOobject::NO_WRITE,
false
);
if (omegaHeader.headerOk())
{
volScalarField omega(omegaHeader, mesh);
dimensionedScalar k0("VSMALL", k.dimensions(), VSMALL);
omega = (1 - mask)*omega + mask*epsilon/(Cmu*k + k0);
// do not correct BC - wall functions will use non-updated k from
// turbulence model
// omega.correctBoundaryConditions();
Info<< "Writing omega\n" << endl;
omega.write();
}
// Turbulence nuTilda
IOobject nuTildaHeader
(
"nuTilda",
runTime.timeName(),
mesh,
IOobject::MUST_READ,
IOobject::NO_WRITE,
false
);
if (nuTildaHeader.headerOk())
{
volScalarField nuTilda(nuTildaHeader, mesh);
nuTilda = nut;
// do not correct BC
// nuTilda.correctBoundaryConditions();
Info<< "Writing nuTilda\n" << endl;
nuTilda.write();
}
}
Info<< nl << "ExecutionTime = " << runTime.elapsedCpuTime() << " s"
<< " ClockTime = " << runTime.elapsedClockTime() << " s"
<< nl << endl;
Info<< "End\n" << endl;
return 0;
}