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[WIP] Turbulent kinetic energy based on inlet condition for supersonic inlet #2430

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[WIP] Turbulent kinetic energy based on inlet condition for supersonic inlet #2430

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91c3bc1
computing tke based on inlet values
Cristopher-Morales Jan 14, 2025
08384b8
Merge branch 'develop' into feature_tke_supersonic
Cristopher-Morales Jan 23, 2025
f837bd5
small fix
Cristopher-Morales Jan 23, 2025
441ddf7
Merge branch 'develop' into feature_tke_supersonic
Cristopher-Morales Jan 25, 2025
572aba9
Merge branch 'develop' into feature_tke_supersonic
Cristopher-Morales Jan 27, 2025
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7 changes: 6 additions & 1 deletion SU2_CFD/src/solvers/CEulerSolver.cpp
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Expand Up @@ -7356,7 +7356,12 @@ void CEulerSolver::BC_Supersonic_Inlet(CGeometry *geometry, CSolver **solver_con

const su2double Velocity2 = GeometryToolbox::SquaredNorm(int(MAXNDIM), Velocity);
su2double Energy = Pressure / (Density * Gamma_Minus_One) + 0.5 * Velocity2;
if (tkeNeeded) Energy += GetTke_Inf();
if (tkeNeeded) {
const su2double* Turb_Properties = config->GetInlet_TurbVal(Marker_Tag);
const su2double Intensity = Turb_Properties[0];
const su2double Tke = 3.0 / 2.0 * (Velocity2* pow(Intensity, 2));
Energy += Tke;
}

/*--- Primitive variables, using the derived quantities. ---*/

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