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Merge branch '2770-wall-functions' into 'develop'

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ENH: wall functions: swap the order of switch statements and for loops

See merge request Development/openfoam!635
This commit is contained in:
Andrew Heather 2023-12-08 11:21:04 +00:00
commit 863dbc68cb
5 changed files with 447 additions and 269 deletions
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193
src/TurbulenceModels/turbulenceModels/derivedFvPatchFields/wallFunctions/epsilonWallFunctions/epsilonWallFunction/epsilonWallFunctionFvPatchScalarField.C
View File

@ -6,7 +6,7 @@
\\/ M anipulation |
-------------------------------------------------------------------------------
Copyright (C) 2011-2019 OpenFOAM Foundation
Copyright (C) 2017-2022 OpenCFD Ltd.
Copyright (C) 2017-2023 OpenCFD Ltd.
-------------------------------------------------------------------------------
License
This file is part of OpenFOAM.
@ -189,105 +189,150 @@ void Foam::epsilonWallFunctionFvPatchScalarField::calculate
{
const label patchi = patch.index();
const tmp<scalarField> tnutw = turbModel.nut(patchi);
const scalarField& nutw = tnutw();
const scalar Cmu25 = pow025(wallCoeffs_.Cmu());
const scalar Cmu75 = pow(wallCoeffs_.Cmu(), 0.75);
const scalar kappa = wallCoeffs_.kappa();
const scalar yPlusLam = wallCoeffs_.yPlusLam();
const scalarField& y = turbModel.y()[patchi];
const labelUList& faceCells = patch.faceCells();
const tmp<scalarField> tnuw = turbModel.nu(patchi);
const scalarField& nuw = tnuw();
const tmp<volScalarField> tk = turbModel.k();
const volScalarField& k = tk();
const fvPatchVectorField& Uw = turbModel.U().boundaryField()[patchi];
const scalarField magGradUw(mag(Uw.snGrad()));
const scalar Cmu25 = pow025(wallCoeffs_.Cmu());
const scalar Cmu75 = pow(wallCoeffs_.Cmu(), 0.75);
const scalar kappa = wallCoeffs_.kappa();
const scalar yPlusLam = wallCoeffs_.yPlusLam();
// Set epsilon and G
forAll(nutw, facei)
// Calculate y-plus
const auto yPlus = [&](const label facei) -> scalar
{
const label celli = patch.faceCells()[facei];
return
(
Cmu25*y[facei]*sqrt(k[faceCells[facei]])/nuw[facei]
);
};
const scalar yPlus = Cmu25*y[facei]*sqrt(k[celli])/nuw[facei];
// Contribution from the viscous sublayer
const auto epsilonVis = [&](const label facei) -> scalar
{
return
(
cornerWeights[facei]*2.0*k[faceCells[facei]]*nuw[facei]
/ sqr(y[facei])
);
};
const scalar w = cornerWeights[facei];
// Contribution from the inertial sublayer
const auto epsilonLog = [&](const label facei) -> scalar
{
return
(
cornerWeights[facei]*Cmu75*pow(k[faceCells[facei]], 1.5)
/ (kappa*y[facei])
);
};
// Contribution from the viscous sublayer
const scalar epsilonVis = w*2.0*k[celli]*nuw[facei]/sqr(y[facei]);
// Contribution from the inertial sublayer
const scalar epsilonLog = w*Cmu75*pow(k[celli], 1.5)/(kappa*y[facei]);
switch (blender_)
switch (blender_)
{
case blenderType::STEPWISE:
{
case blenderType::STEPWISE:
forAll(faceCells, facei)
{
if (lowReCorrection_ && yPlus < yPlusLam)
if (lowReCorrection_ && yPlus(facei) < yPlusLam)
{
epsilon0[celli] += epsilonVis;
epsilon0[faceCells[facei]] += epsilonVis(facei);
}
else
{
epsilon0[celli] += epsilonLog;
epsilon0[faceCells[facei]] += epsilonLog(facei);
}
break;
}
case blenderType::BINOMIAL:
{
// (ME:Eqs. 15-16)
epsilon0[celli] +=
pow
(
pow(epsilonVis, n_) + pow(epsilonLog, n_),
scalar(1)/n_
);
break;
}
case blenderType::MAX:
{
// (PH:Eq. 27)
epsilon0[celli] += max(epsilonVis, epsilonLog);
break;
}
case blenderType::EXPONENTIAL:
{
// (PH:p. 193)
const scalar Gamma = 0.001*pow4(yPlus)/(scalar(1) + yPlus);
const scalar invGamma = scalar(1)/(Gamma + ROOTVSMALL);
epsilon0[celli] +=
epsilonVis*exp(-Gamma) + epsilonLog*exp(-invGamma);
break;
}
case blenderType::TANH:
{
// (KAS:Eqs. 33-34)
const scalar phiTanh = tanh(pow4(0.1*yPlus));
const scalar b1 = epsilonVis + epsilonLog;
const scalar b2 =
pow(pow(epsilonVis, 1.2) + pow(epsilonLog, 1.2), 1.0/1.2);
epsilon0[celli] += phiTanh*b1 + (1 - phiTanh)*b2;
break;
}
break;
}
if (!lowReCorrection_ || (yPlus > yPlusLam))
case blenderType::BINOMIAL:
{
G0[celli] +=
w
forAll(faceCells, facei)
{
// (ME:Eqs. 15-16)
epsilon0[faceCells[facei]] +=
pow
(
pow(epsilonVis(facei), n_) + pow(epsilonLog(facei), n_),
scalar(1)/n_
);
}
break;
}
case blenderType::MAX:
{
forAll(faceCells, facei)
{
// (PH:Eq. 27)
epsilon0[faceCells[facei]] +=
max(epsilonVis(facei), epsilonLog(facei));
}
break;
}
case blenderType::EXPONENTIAL:
{
forAll(faceCells, facei)
{
// (PH:p. 193)
const scalar yPlusFace = yPlus(facei);
const scalar Gamma =
0.001*pow4(yPlusFace)/(scalar(1) + yPlusFace);
const scalar invGamma = scalar(1)/(Gamma + ROOTVSMALL);
epsilon0[faceCells[facei]] +=
(
epsilonVis(facei)*exp(-Gamma)
+ epsilonLog(facei)*exp(-invGamma)
);
}
break;
}
case blenderType::TANH:
{
forAll(faceCells, facei)
{
// (KAS:Eqs. 33-34)
const scalar epsilonVisFace = epsilonVis(facei);
const scalar epsilonLogFace = epsilonLog(facei);
const scalar b1 = epsilonVisFace + epsilonLogFace;
const scalar b2 =
pow
(
pow(epsilonVisFace, 1.2) + pow(epsilonLogFace, 1.2),
1.0/1.2
);
const scalar phiTanh = tanh(pow4(0.1*yPlus(facei)));
epsilon0[faceCells[facei]] += phiTanh*b1 + (1 - phiTanh)*b2;
}
break;
}
}
const fvPatchVectorField& Uw = turbModel.U().boundaryField()[patchi];
const scalarField magGradUw(mag(Uw.snGrad()));
const tmp<scalarField> tnutw = turbModel.nut(patchi);
const scalarField& nutw = tnutw();
forAll(faceCells, facei)
{
if (!lowReCorrection_ || (yPlus(facei) > yPlusLam))
{
G0[faceCells[facei]] +=
cornerWeights[facei]
*(nutw[facei] + nuw[facei])
*magGradUw[facei]
*Cmu25*sqrt(k[celli])
*Cmu25*sqrt(k[faceCells[facei]])
/(kappa*y[facei]);
}
}

96
src/TurbulenceModels/turbulenceModels/derivedFvPatchFields/wallFunctions/nutWallFunctions/nutUWallFunction/nutUWallFunctionFvPatchScalarField.C
View File

@ -6,7 +6,7 @@
\\/ M anipulation |
-------------------------------------------------------------------------------
Copyright (C) 2011-2016 OpenFOAM Foundation
Copyright (C) 2019-2021 OpenCFD Ltd.
Copyright (C) 2019-2023 OpenCFD Ltd.
-------------------------------------------------------------------------------
License
This file is part of OpenFOAM.
@ -32,7 +32,6 @@ License
#include "volFields.H"
#include "addToRunTimeSelectionTable.H"
// * * * * * * * * * * * * Protected Member Functions * * * * * * * * * * * //
Foam::tmp<Foam::scalarField>
@ -40,6 +39,10 @@ Foam::nutUWallFunctionFvPatchScalarField::calcNut() const
{
const label patchi = patch().index();
const scalar kappa = wallCoeffs_.kappa();
const scalar E = wallCoeffs_.E();
const scalar yPlusLam = wallCoeffs_.yPlusLam();
const auto& turbModel = db().lookupObject<turbulenceModel>
(
IOobject::groupName
@ -52,88 +55,107 @@ Foam::nutUWallFunctionFvPatchScalarField::calcNut() const
const fvPatchVectorField& Uw = U(turbModel).boundaryField()[patchi];
const scalarField magUp(mag(Uw.patchInternalField() - Uw));
const tmp<scalarField> tnuw = turbModel.nu(patchi);
const scalarField& nuw = tnuw();
const scalar kappa = wallCoeffs_.kappa();
const scalar E = wallCoeffs_.E();
const scalar yPlusLam = wallCoeffs_.yPlusLam();
tmp<scalarField> tyPlus = calcYPlus(magUp);
const scalarField& yPlus = tyPlus();
// Viscous sublayer contribution
const tmp<scalarField> tnutVis = turbModel.nu(patchi);
const scalarField& nutVis = tnutVis();
// Inertial sublayer contribution
const auto nutLog = [&](const label facei) -> scalar
{
const scalar yPlusFace = yPlus[facei];
return
(
nutVis[facei]*yPlusFace*kappa/log(max(E*yPlusFace, 1 + 1e-4))
);
};
auto tnutw = tmp<scalarField>::New(patch().size(), Zero);
auto& nutw = tnutw.ref();
forAll(yPlus, facei)
switch (blender_)
{
// Viscous sublayer contribution
const scalar nutVis = 0;
// Inertial sublayer contribution
const scalar nutLog =
nuw[facei]
*(yPlus[facei]*kappa/log(max(E*yPlus[facei], 1 + 1e-4)) - 1.0);
switch (blender_)
case blenderType::STEPWISE:
{
case blenderType::STEPWISE:
forAll(nutw, facei)
{
if (yPlus[facei] > yPlusLam)
{
nutw[facei] = nutLog;
nutw[facei] = nutLog(facei);
}
else
{
nutw[facei] = nutVis;
nutw[facei] = nutVis[facei];
}
break;
}
break;
}
case blenderType::MAX:
case blenderType::MAX:
{
forAll(nutw, facei)
{
// (PH:Eq. 27)
nutw[facei] = max(nutVis, nutLog);
break;
nutw[facei] = max(nutVis[facei], nutLog(facei));
}
break;
}
case blenderType::BINOMIAL:
case blenderType::BINOMIAL:
{
forAll(nutw, facei)
{
// (ME:Eqs. 15-16)
nutw[facei] =
pow
(
pow(nutVis, n_) + pow(nutLog, n_),
pow(nutVis[facei], n_) + pow(nutLog(facei), n_),
scalar(1)/n_
);
break;
}
break;
}
case blenderType::EXPONENTIAL:
case blenderType::EXPONENTIAL:
{
forAll(nutw, facei)
{
// (PH:Eq. 31)
const scalar Gamma =
0.01*pow4(yPlus[facei])/(1 + 5*yPlus[facei]);
const scalar invGamma = scalar(1)/(Gamma + ROOTVSMALL);
nutw[facei] = nutVis*exp(-Gamma) + nutLog*exp(-invGamma);
break;
nutw[facei] =
nutVis[facei]*exp(-Gamma) + nutLog(facei)*exp(-invGamma);
}
break;
}
case blenderType::TANH:
case blenderType::TANH:
{
forAll(nutw, facei)
{
// (KAS:Eqs. 33-34)
const scalar phiTanh = tanh(pow4(0.1*yPlus[facei]));
const scalar b1 = nutVis + nutLog;
const scalar nutLogFace = nutLog(facei);
const scalar b1 = nutVis[facei] + nutLogFace;
const scalar b2 =
pow(pow(nutVis, 1.2) + pow(nutLog, 1.2), 1.0/1.2);
pow
(
pow(nutVis[facei], 1.2) + pow(nutLogFace, 1.2),
1.0/1.2
);
const scalar phiTanh = tanh(pow4(0.1*yPlus[facei]));
nutw[facei] = phiTanh*b1 + (1 - phiTanh)*b2;
break;
}
break;
}
}
nutw -= nutVis;
return tnutw;
}

118
src/TurbulenceModels/turbulenceModels/derivedFvPatchFields/wallFunctions/nutWallFunctions/nutkWallFunction/nutkWallFunctionFvPatchScalarField.C
View File

@ -6,7 +6,7 @@
\\/ M anipulation |
-------------------------------------------------------------------------------
Copyright (C) 2011-2016, 2019 OpenFOAM Foundation
Copyright (C) 2019-2022 OpenCFD Ltd.
Copyright (C) 2019-2023 OpenCFD Ltd.
-------------------------------------------------------------------------------
License
This file is part of OpenFOAM.
@ -40,6 +40,11 @@ calcNut() const
{
const label patchi = patch().index();
const scalar Cmu25 = pow025(wallCoeffs_.Cmu());
const scalar kappa = wallCoeffs_.kappa();
const scalar E = wallCoeffs_.E();
const scalar yPlusLam = wallCoeffs_.yPlusLam();
const auto& turbModel = db().lookupObject<turbulenceModel>
(
IOobject::groupName
@ -49,93 +54,118 @@ calcNut() const
)
);
const labelUList& faceCells = patch().faceCells();
const scalarField& y = turbModel.y()[patchi];
const tmp<volScalarField> tk = turbModel.k();
const volScalarField& k = tk();
const tmp<scalarField> tnuw = turbModel.nu(patchi);
const scalarField& nuw = tnuw();
// Viscous sublayer contribution
const tmp<scalarField> tnutVis = turbModel.nu(patchi);
const scalarField& nutVis = tnutVis();
const scalar Cmu25 = pow025(wallCoeffs_.Cmu());
const scalar kappa = wallCoeffs_.kappa();
const scalar E = wallCoeffs_.E();
const scalar yPlusLam = wallCoeffs_.yPlusLam();
// Calculate y-plus
const auto yPlus = [&](const label facei) -> scalar
{
return (Cmu25*y[facei]*sqrt(k[faceCells[facei]])/nutVis[facei]);
};
// Inertial sublayer contribution
const auto nutLog = [&](const label facei) -> scalar
{
const scalar yPlusFace = yPlus(facei);
return
(
nutVis[facei]*yPlusFace*kappa
/ log(max(E*yPlusFace, 1 + 1e-4))
);
};
auto tnutw = tmp<scalarField>::New(patch().size(), Zero);
auto& nutw = tnutw.ref();
forAll(nutw, facei)
switch (blender_)
{
const label celli = patch().faceCells()[facei];
const scalar yPlus = Cmu25*y[facei]*sqrt(k[celli])/nuw[facei];
// Viscous sublayer contribution
const scalar nutVis = 0;
// Inertial sublayer contribution
const scalar nutLog =
nuw[facei]*(yPlus*kappa/log(max(E*yPlus, 1 + 1e-4)) - 1.0);
switch (blender_)
case blenderType::STEPWISE:
{
case blenderType::STEPWISE:
forAll(nutw, facei)
{
if (yPlus > yPlusLam)
if (yPlus(facei) > yPlusLam)
{
nutw[facei] = nutLog;
nutw[facei] = nutLog(facei);
}
else
{
nutw[facei] = nutVis;
nutw[facei] = nutVis[facei];
}
break;
}
break;
}
case blenderType::MAX:
case blenderType::MAX:
{
forAll(nutw, facei)
{
// (PH:Eq. 27)
nutw[facei] = max(nutVis, nutLog);
break;
nutw[facei] = max(nutVis[facei], nutLog(facei));
}
break;
}
case blenderType::BINOMIAL:
case blenderType::BINOMIAL:
{
forAll(nutw, facei)
{
// (ME:Eqs. 15-16)
nutw[facei] =
pow
(
pow(nutVis, n_) + pow(nutLog, n_),
pow(nutVis[facei], n_) + pow(nutLog(facei), n_),
scalar(1)/n_
);
break;
}
break;
}
case blenderType::EXPONENTIAL:
case blenderType::EXPONENTIAL:
{
forAll(nutw, facei)
{
// (PH:Eq. 31)
const scalar Gamma = 0.01*pow4(yPlus)/(1 + 5*yPlus);
const scalar yPlusFace = yPlus(facei);
const scalar Gamma = 0.01*pow4(yPlusFace)/(1 + 5*yPlusFace);
const scalar invGamma = scalar(1)/(Gamma + ROOTVSMALL);
nutw[facei] = nutVis*exp(-Gamma) + nutLog*exp(-invGamma);
break;
nutw[facei] =
nutVis[facei]*exp(-Gamma) + nutLog(facei)*exp(-invGamma);
}
break;
}
case blenderType::TANH:
case blenderType::TANH:
{
forAll(nutw, facei)
{
// (KAS:Eqs. 33-34)
const scalar phiTanh = tanh(pow4(0.1*yPlus));
const scalar b1 = nutVis + nutLog;
const scalar nutLogFace = nutLog(facei);
const scalar b1 = nutVis[facei] + nutLogFace;
const scalar b2 =
pow(pow(nutVis, 1.2) + pow(nutLog, 1.2), 1.0/1.2);
pow
(
pow(nutVis[facei], 1.2) + pow(nutLogFace, 1.2),
1.0/1.2
);
const scalar phiTanh = tanh(pow4(0.1*yPlus(facei)));
nutw[facei] = phiTanh*b1 + (1 - phiTanh)*b2;
break;
}
break;
}
}
nutw -= nutVis;
return tnutw;
}
@ -231,8 +261,8 @@ yPlus() const
tmp<scalarField> tkwc = k.boundaryField()[patchi].patchInternalField();
const scalarField& kwc = tkwc();
tmp<scalarField> tnuw = turbModel.nu(patchi);
const scalarField& nuw = tnuw();
tmp<scalarField> tnutVis = turbModel.nu(patchi);
const scalarField& nutVis = tnutVis();
tmp<scalarField> tnuEff = turbModel.nuEff(patchi);
const scalarField& nuEff = tnuEff();
@ -249,13 +279,13 @@ yPlus() const
forAll(yPlus, facei)
{
// inertial sublayer
yPlus[facei] = Cmu25*y[facei]*sqrt(kwc[facei])/nuw[facei];
yPlus[facei] = Cmu25*y[facei]*sqrt(kwc[facei])/nutVis[facei];
if (yPlusLam > yPlus[facei])
{
// viscous sublayer
yPlus[facei] =
y[facei]*sqrt(nuEff[facei]*magGradUw[facei])/nuw[facei];
y[facei]*sqrt(nuEff[facei]*magGradUw[facei])/nutVis[facei];
}
}

186
src/TurbulenceModels/turbulenceModels/derivedFvPatchFields/wallFunctions/omegaWallFunctions/omegaWallFunction/omegaWallFunctionFvPatchScalarField.C
View File

@ -6,7 +6,7 @@
\\/ M anipulation |
-------------------------------------------------------------------------------
Copyright (C) 2011-2016, 2019 OpenFOAM Foundation
Copyright (C) 2017-2022 OpenCFD Ltd.
Copyright (C) 2017-2023 OpenCFD Ltd.
-------------------------------------------------------------------------------
License
This file is part of OpenFOAM.
@ -188,102 +188,146 @@ void Foam::omegaWallFunctionFvPatchScalarField::calculate
{
const label patchi = patch.index();
const tmp<scalarField> tnutw = turbModel.nut(patchi);
const scalarField& nutw = tnutw();
const scalar Cmu25 = pow025(wallCoeffs_.Cmu());
const scalar kappa = wallCoeffs_.kappa();
const scalar yPlusLam = wallCoeffs_.yPlusLam();
const scalarField& y = turbModel.y()[patchi];
const labelUList& faceCells = patch.faceCells();
const tmp<scalarField> tnutw = turbModel.nut(patchi);
const scalarField& nutw = tnutw();
const tmp<scalarField> tnuw = turbModel.nu(patchi);
const scalarField& nuw = tnuw();
const tmp<volScalarField> tk = turbModel.k();
const volScalarField& k = tk();
const fvPatchVectorField& Uw = turbModel.U().boundaryField()[patchi];
const scalarField magGradUw(mag(Uw.snGrad()));
const scalar Cmu25 = pow025(wallCoeffs_.Cmu());
const scalar kappa = wallCoeffs_.kappa();
const scalar yPlusLam = wallCoeffs_.yPlusLam();
// Set omega and G
forAll(nutw, facei)
// Calculate y-plus
const auto yPlus = [&](const label facei) -> scalar
{
const label celli = patch.faceCells()[facei];
const scalar yPlus = Cmu25*y[facei]*sqrt(k[celli])/nuw[facei];
const scalar w = cornerWeights[facei];
return
(
Cmu25*y[facei]*sqrt(k[faceCells[facei]])/nuw[facei]
);
};
// Contribution from the viscous sublayer
const scalar omegaVis = 6.0*nuw[facei]/(beta1_*sqr(y[facei]));
// Contribution from the viscous sublayer
const auto omegaVis = [&](const label facei) -> scalar
{
return
(
cornerWeights[facei]*6.0*nuw[facei]/(beta1_*sqr(y[facei]))
);
};
// Contribution from the inertial sublayer
const scalar omegaLog = sqrt(k[celli])/(Cmu25*kappa*y[facei]);
// Contribution from the inertial sublayer
const auto omegaLog = [&](const label facei) -> scalar
{
return
(
cornerWeights[facei]*sqrt(k[faceCells[facei]])
/ (Cmu25*kappa*y[facei])
);
};
switch (blender_)
switch (blender_)
{
case blenderType::STEPWISE:
{
case blenderType::STEPWISE:
forAll(faceCells, facei)
{
if (yPlus > yPlusLam)
if (yPlus(facei) > yPlusLam)
{
omega0[celli] += w*omegaLog;
omega0[faceCells[facei]] += omegaLog(facei);
}
else
{
omega0[celli] += w*omegaVis;
omega0[faceCells[facei]] += omegaVis(facei);
}
break;
}
case blenderType::BINOMIAL:
{
omega0[celli] +=
w*pow
(
pow(omegaVis, n_) + pow(omegaLog, n_),
scalar(1)/n_
);
break;
}
case blenderType::MAX:
{
// (PH:Eq. 27)
omega0[celli] += max(omegaVis, omegaLog);
break;
}
case blenderType::EXPONENTIAL:
{
// (PH:Eq. 31)
const scalar Gamma = 0.01*pow4(yPlus)/(1 + 5*yPlus);
const scalar invGamma = scalar(1)/(Gamma + ROOTVSMALL);
omega0[celli] +=
w*(omegaVis*exp(-Gamma) + omegaLog*exp(-invGamma));
break;
}
case blenderType::TANH:
{
// (KAS:Eqs. 33-34)
const scalar phiTanh = tanh(pow4(0.1*yPlus));
const scalar b1 = omegaVis + omegaLog;
const scalar b2 =
pow(pow(omegaVis, 1.2) + pow(omegaLog, 1.2), 1.0/1.2);
omega0[celli] += phiTanh*b1 + (1 - phiTanh)*b2;
break;
}
break;
}
if (!(blender_ == blenderType::STEPWISE) || yPlus > yPlusLam)
case blenderType::BINOMIAL:
{
G0[celli] +=
w
forAll(faceCells, facei)
{
omega0[faceCells[facei]] +=
pow
(
pow(omegaVis(facei), n_) + pow(omegaLog(facei), n_),
scalar(1)/n_
);
}
break;
}
case blenderType::MAX:
{
forAll(faceCells, facei)
{
// (PH:Eq. 27)
omega0[faceCells[facei]] +=
max(omegaVis(facei), omegaLog(facei));
}
break;
}
case blenderType::EXPONENTIAL:
{
forAll(faceCells, facei)
{
// (PH:Eq. 31)
const scalar yPlusFace = yPlus(facei);
const scalar Gamma = 0.01*pow4(yPlusFace)/(1 + 5*yPlusFace);
const scalar invGamma = scalar(1)/(Gamma + ROOTVSMALL);
omega0[faceCells[facei]] +=
(
omegaVis(facei)*exp(-Gamma)
+ omegaLog(facei)*exp(-invGamma)
);
}
break;
}
case blenderType::TANH:
{
forAll(faceCells, facei)
{
// (KAS:Eqs. 33-34)
const scalar omegaVisFace = omegaVis(facei);
const scalar omegaLogFace = omegaLog(facei);
const scalar b1 = omegaVisFace + omegaLogFace;
const scalar b2 =
pow
(
pow(omegaVisFace, 1.2) + pow(omegaLogFace, 1.2),
1.0/1.2
);
const scalar phiTanh = tanh(pow4(0.1*yPlus(facei)));
omega0[faceCells[facei]] += phiTanh*b1 + (1 - phiTanh)*b2;
}
break;
}
}
const fvPatchVectorField& Uw = turbModel.U().boundaryField()[patchi];
const scalarField magGradUw(mag(Uw.snGrad()));
forAll(faceCells, facei)
{
if (!(blender_ == blenderType::STEPWISE) || yPlus(facei) > yPlusLam)
{
G0[faceCells[facei]] +=
cornerWeights[facei]
*(nutw[facei] + nuw[facei])
*magGradUw[facei]
*Cmu25*sqrt(k[celli])
*Cmu25*sqrt(k[faceCells[facei]])
/(kappa*y[facei]);
}
}

123
src/thermoTools/derivedFvPatchFields/wallFunctions/sorptionWallFunction/sorptionWallFunctionFvPatchScalarField.C
View File

@ -5,7 +5,7 @@
\\ / A nd | www.openfoam.com
\\/ M anipulation |
-------------------------------------------------------------------------------
Copyright (C) 2022 OpenCFD Ltd.
Copyright (C) 2022-2023 OpenCFD Ltd.
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License
This file is part of OpenFOAM.
@ -64,9 +64,16 @@ static scalar calcYStarLam
tmp<scalarField> sorptionWallFunctionFvPatchScalarField::yPlus() const
{
// Calculate fields of interest
const label patchi = patch().index();
// Calculate the empirical constant given by (Jayatilleke, 1966) (FDC:Eq. 6)
const scalar Pc =
9.24*(pow(Sc_/Sct_, 0.75) - 1)*(1 + 0.28*exp(-0.007*Sc_/Sct_));
const scalar Cmu25 = pow025(wallCoeffs_.Cmu());
const scalar kappa = wallCoeffs_.kappa();
const scalar E = wallCoeffs_.E();
// Calculate fields of interest
const auto& k = db().lookupObject<volScalarField>(kName_);
tmp<scalarField> tkwc = k.boundaryField()[patchi].patchInternalField();
const scalarField& kwc = tkwc.cref();
@ -79,86 +86,116 @@ tmp<scalarField> sorptionWallFunctionFvPatchScalarField::yPlus() const
tmp<scalarField> tywc = y.boundaryField()[patchi].patchInternalField();
const scalarField& ywc = tywc.cref();
// (FDC:Eq. 3)
const auto yStar = [&](const label facei) -> scalar
{
return
(
Cmu25*sqrt(kwc[facei])*ywc[facei]/nuwc[facei]
);
};
// Calculate the empirical constant given by (Jayatilleke, 1966) (FDC:Eq. 6)
const scalar Pc =
9.24*(pow(Sc_/Sct_, 0.75) - 1)*(1 + 0.28*exp(-0.007*Sc_/Sct_));
const scalar Cmu25 = pow025(wallCoeffs_.Cmu());
const scalar kappa = wallCoeffs_.kappa();
const scalar E = wallCoeffs_.E();
// (FDC:Eq. 4)
const auto yPlusVis = [&](const label facei) -> scalar
{
return (Sc_*yStar(facei));
};
auto tyPlus = tmp<scalarField>::New(patch().size(), Zero);
// (FDC:Eq. 5)
const auto yPlusLog = [&](const label facei) -> scalar
{
return
(
Sct_*(log(max(E*yStar(facei), 1 + 1e-4))/kappa + Pc)
);
};
auto tyPlus = tmp<scalarField>::New(patch().size());
auto& yPlus = tyPlus.ref();
forAll(yPlus, facei)
switch (blender_)
{
// (FDC:Eq. 3)
const scalar yStar = Cmu25*sqrt(kwc[facei])*ywc[facei]/nuwc[facei];
// (FDC:Eq. 4)
const scalar yPlusVis = Sc_*yStar;
// (FDC:Eq. 5)
const scalar yPlusLog = Sct_*(log(max(E*yStar, 1 + 1e-4))/kappa + Pc);
switch (blender_)
case blenderType::EXPONENTIAL:
{
case blenderType::EXPONENTIAL:
forAll(yPlus, facei)
{
// (FDC:Eq. 2)
const scalar yStarFace = yStar(facei);
const scalar Gamma =
0.01*pow4(Sc_*yStar)/(1 + 5*pow3(Sc_)*yStar);
0.01*pow4(Sc_*yStarFace)/(1 + 5*pow3(Sc_)*yStarFace);
const scalar invGamma = scalar(1)/max(Gamma, ROOTVSMALL);
// (FDC:Eq. 1)
yPlus[facei] = yPlusVis*exp(-Gamma) + yPlusLog*exp(-invGamma);
break;
yPlus[facei] =
(
yPlusVis(facei)*exp(-Gamma)
+ yPlusLog(facei)*exp(-invGamma)
);
}
break;
}
case blenderType::STEPWISE:
case blenderType::STEPWISE:
{
static const scalar yStarLam =
calcYStarLam(kappa, E, Sc_, Sct_, Pc);
forAll(yPlus, facei)
{
static const scalar yStarLam =
calcYStarLam(kappa, E, Sc_, Sct_, Pc);
// (F:Eq. 5.3)
if (yStar < yStarLam)
if (yStar(facei) < yStarLam)
{
yPlus[facei] = yPlusVis;
yPlus[facei] = yPlusVis(facei);
}
else
{
yPlus[facei] = yPlusLog;
yPlus[facei] = yPlusLog(facei);
}
break;
}
break;
}
case blenderType::BINOMIAL:
case blenderType::BINOMIAL:
{
forAll(yPlus, facei)
{
yPlus[facei] =
pow
(
pow(yPlusVis, n_) + pow(yPlusLog, n_),
pow(yPlusVis(facei), n_) + pow(yPlusLog(facei), n_),
scalar(1)/n_
);
break;
}
break;
}
case blenderType::MAX:
case blenderType::MAX:
{
forAll(yPlus, facei)
{
yPlus[facei] = max(yPlusVis, yPlusLog);
break;
yPlus[facei] = max(yPlusVis(facei), yPlusLog(facei));
}
break;
}
case blenderType::TANH:
case blenderType::TANH:
{
forAll(yPlus, facei)
{
const scalar phiTanh = tanh(pow4(0.1*yStar));
const scalar b1 = yPlusVis + yPlusLog;
const scalar yPlusVisFace = yPlusVis(facei);
const scalar yPlusLogFace = yPlusLog(facei);
const scalar b1 = yPlusVisFace + yPlusLogFace;
const scalar b2 =
pow(pow(yPlusVis, 1.2) + pow(yPlusLog, 1.2), 1.0/1.2);
pow
(
pow(yPlusVisFace, 1.2) + pow(yPlusLogFace, 1.2),
1.0/1.2
);
const scalar phiTanh = tanh(pow4(0.1*yStar(facei)));
yPlus[facei] = phiTanh*b1 + (1 - phiTanh)*b2;
break;
}
break;
}
}