FSD.C

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    Copyright (C) 2019 OpenCFD Ltd.
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#include "FSD.H"
#include "addToRunTimeSelectionTable.H"
#include "LESModel.H"
#include "fvcGrad.H"
#include "fvcDiv.H"
 
namespace Foam
{
namespace combustionModels
{
 
// * * * * * * * * * * * * * * * * Constructors  * * * * * * * * * * * * * * //
 
template<class ReactionThermo, class ThermoType>
FSD<ReactionThermo, ThermoType>::FSD
(
    const word& modelType,
    ReactionThermo& thermo,
    const compressibleTurbulenceModel& turb,
    const word& combustionProperties
)
:
    singleStepCombustion<ReactionThermo, ThermoType>
    (
        modelType,
        thermo,
        turb,
        combustionProperties
    ),
    reactionRateFlameArea_
    (
        reactionRateFlameArea::New
        (
            this->coeffs(),
            this->mesh(),
            *this
        )
    ),
    ft_
    (
        IOobject
        (
            this->thermo().phasePropertyName("ft"),
            this->mesh().time().timeName(),
            this->mesh(),
            IOobject::NO_READ,
            IOobject::AUTO_WRITE,
            IOobject::REGISTER
        ),
        this->mesh(),
        dimensionedScalar(dimless, Zero)
    ),
    YFuelFuelStream_(dimensionedScalar("YFuelStream", dimless, 1.0)),
    YO2OxiStream_(dimensionedScalar("YOxiStream", dimless, 0.23)),
    Cv_(this->coeffs().getScalar("Cv")),
    C_(5.0),
    ftMin_(0.0),
    ftMax_(1.0),
    ftDim_(300),
    ftVarMin_(this->coeffs().getScalar("ftVarMin"))
{}
 
 
// * * * * * * * * * * * * * * * * Destructor  * * * * * * * * * * * * * * * //
 
template<class ReactionThermo, class ThermoType>
FSD<ReactionThermo, ThermoType>::~FSD()
{}
 
 
// * * * * * * * * * * * * * * Member Functions  * * * * * * * * * * * * * * //
 
template<class ReactionThermo, class ThermoType>
void FSD<ReactionThermo, ThermoType>::calculateSourceNorm()
{
    this->singleMixturePtr_->fresCorrect();
 
    const label fuelI = this->singleMixturePtr_->fuelIndex();
 
    const volScalarField& YFuel = this->thermo().composition().Y()[fuelI];
 
    const volScalarField& YO2 = this->thermo().composition().Y("O2");
 
    const dimensionedScalar s = this->singleMixturePtr_->s();
 
    ft_ =
        (s*YFuel - (YO2 - YO2OxiStream_))/(s*YFuelFuelStream_ + YO2OxiStream_);
 
 
    volVectorField nft(fvc::grad(ft_));
 
    volScalarField mgft(mag(nft));
 
    surfaceVectorField SfHat(this->mesh().Sf()/this->mesh().magSf());
 
    volScalarField cAux(scalar(1) - ft_);
 
    dimensionedScalar dMgft = 1.0e-3*
        (ft_*cAux*mgft)().weightedAverage(this->mesh().V())
       /((ft_*cAux)().weightedAverage(this->mesh().V()) + SMALL)
      + dimensionedScalar("ddMgft", mgft.dimensions(), SMALL);
 
    mgft += dMgft;
 
    nft /= mgft;
 
    const volVectorField& U = YO2.db().lookupObject<volVectorField>("U");
 
    const volScalarField sigma
    (
        (nft & nft)*fvc::div(U) - (nft & fvc::grad(U) & nft)
    );
 
    reactionRateFlameArea_->correct(sigma);
 
    const volScalarField& omegaFuel = reactionRateFlameArea_->omega();
 
 
    const scalar ftStoich =
        YO2OxiStream_.value()
       /(
            s.value()*YFuelFuelStream_.value() + YO2OxiStream_.value()
        );
 
    auto tPc = volScalarField::New
    (
        this->thermo().phasePropertyName("Pc"),
        IOobject::NO_REGISTER,
        U.mesh(),
        dimensionedScalar(dimless, Zero)
    );
    auto& pc = tPc.ref();
 
    auto tomegaFuel = volScalarField::New
    (
        this->thermo().phasePropertyName("omegaFuelBar"),
        IOobject::NO_REGISTER,
        U.mesh(),
        dimensionedScalar(omegaFuel.dimensions(), Zero)
    );
    auto& omegaFuelBar = tomegaFuel.ref();
 
    // Calculation of the mixture fraction variance (ftVar)
    const compressible::LESModel& lesModel =
        YO2.db().lookupObject<compressible::LESModel>
        (
            turbulenceModel::propertiesName
        );
 
    const volScalarField& delta = lesModel.delta();
    const volScalarField ftVar(Cv_*sqr(delta)*sqr(mgft));
 
    // Thickened flame (average flame thickness for counterflow configuration
    // is 1.5 mm)
 
    volScalarField  deltaF
    (
        delta/dimensionedScalar("flame", dimLength, 1.5e-3)
    );
 
    // Linear correlation between delta and flame thickness
    volScalarField omegaF(max(deltaF*(4.0/3.0) + (2.0/3.0), scalar(1)));
 
    scalar deltaFt = 1.0/ftDim_;
 
    forAll(ft_, celli)
    {
        if (ft_[celli] > ftMin_ && ft_[celli] < ftMax_)
        {
            scalar ftCell = ft_[celli];
 
            if (ftVar[celli] > ftVarMin_) //sub-grid beta pdf of ft_
            {
                scalar ftVarc = ftVar[celli];
                scalar a =
                    max(ftCell*(ftCell*(1.0 - ftCell)/ftVarc - 1.0), 0.0);
                scalar b = max(a/ftCell - a, 0.0);
 
                for (int i=1; i<ftDim_; i++)
                {
                    scalar ft = i*deltaFt;
                    pc[celli] += pow(ft, a-1.0)*pow(1.0 - ft, b - 1.0)*deltaFt;
                }
 
                for (int i=1; i<ftDim_; i++)
                {
                    scalar ft = i*deltaFt;
                    omegaFuelBar[celli] +=
                        omegaFuel[celli]/omegaF[celli]
                       *exp
                        (
                           -sqr(ft - ftStoich)
                           /(2.0*sqr(0.01*omegaF[celli]))
                        )
                       *pow(ft, a - 1.0)
                       *pow(1.0 - ft, b - 1.0)
                       *deltaFt;
                }
                omegaFuelBar[celli] /= max(pc[celli], 1e-4);
            }
            else
            {
                omegaFuelBar[celli] =
                   omegaFuel[celli]/omegaF[celli]
                  *exp(-sqr(ftCell - ftStoich)/(2.0*sqr(0.01*omegaF[celli])));
            }
        }
        else
        {
            omegaFuelBar[celli] = 0.0;
        }
    }
 
 
    // Combustion progress variable, c
 
    List<label> productsIndex(2, label(-1));
    {
        label i = 0;
        forAll(this->singleMixturePtr_->specieProd(), specieI)
        {
            if (this->singleMixturePtr_->specieProd()[specieI] < 0)
            {
                productsIndex[i] = specieI;
                i++;
            }
        }
    }
 
 
    // Flamelet probability of the progress c based on IFC (reuse pc)
    scalar YprodTotal = 0;
    forAll(productsIndex, j)
    {
        YprodTotal += this->singleMixturePtr_->Yprod0()[productsIndex[j]];
    }
 
    forAll(ft_, celli)
    {
        if (ft_[celli] < ftStoich)
        {
            pc[celli] = ft_[celli]*(YprodTotal/ftStoich);
        }
        else
        {
            pc[celli] = (1.0 - ft_[celli])*(YprodTotal/(1.0 - ftStoich));
        }
    }
 
    auto tproducts = volScalarField::New
    (
        this->thermo().phasePropertyName("products"),
        IOobject::NO_REGISTER,
        U.mesh(),
        dimensionedScalar(dimless, Zero)
    );
    auto& products = tproducts.ref();
 
    forAll(productsIndex, j)
    {
        label specieI = productsIndex[j];
        const volScalarField& Yp = this->thermo().composition().Y()[specieI];
        products += Yp;
    }
 
    volScalarField c
    (
        max(scalar(1) - products/max(pc, scalar(1e-5)), scalar(0))
    );
 
    pc = min(C_*c, scalar(1));
 
    const volScalarField fres(this->singleMixturePtr_->fres(fuelI));
 
    this->wFuel_ == mgft*pc*omegaFuelBar;
}
 
 
template<class ReactionThermo, class ThermoType>
void FSD<ReactionThermo, ThermoType>::correct()
{
    this->wFuel_ == Zero;
 
    if (this->active())
    {
        calculateSourceNorm();
    }
}
 
 
template<class ReactionThermo, class ThermoType>
bool FSD<ReactionThermo, ThermoType>::read()
{
    if (singleStepCombustion<ReactionThermo, ThermoType>::read())
    {
        this->coeffs().readEntry("Cv", Cv_);
        this->coeffs().readEntry("ftVarMin", ftVarMin_);
        reactionRateFlameArea_->read(this->coeffs());
        return true;
    }
 
    return false;
}
 
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
 
} // End namespace combustionModels
} // End namespace Foam
 
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //