The present work focuses on the numerical modeling through Large Eddy Simulations (LES) of a low-swirl partially premixed lean flame operated with gaseous fuel using a hybrid Thickened Flame (TF)-Flamelet Generated Manifolds (FGM) combustion model. This approach aims to overcome the challenges of modeling the flame lift-off in this burner and the stabilization of the reaction zone at a remarkable distance from the nozzle outlet section, for which the reproduction of finite rate effects on combustion physics is crucial. The underlying strategy consists of applying the artificial thickening to the scalar equations required for the query of the look-up table computed a priori. The mentioned combustion model has been implemented in a general-purpose commercial CFD solver and Non-Adiabatic Flamelets have been employed for the look-up table computation. The goal is to include a detailed chemistry description while maintaining a cost-effective approach and improving the reproduction of the turbulence-chemistry interaction. Results are validated with experimental data in terms of temperature and chemical species concentration maps, showing the potential of the coupled TF-FGM approach for describing this type of flame.

ASSESSMENT OF THICKENED FLAME MODEL COUPLED WITH FLAMELET GENERATED MANIFOLD ON A LOW-SWIRL PARTIALLY PREMIXED GASEOUS LIFTED FLAME / Langone L.; Amerighi M.; Mazzei L.; Andreini A.; Orsino S.; Ansari N.; Yadav R.. - ELETTRONICO. - 3-B:(2022), pp. 1-14. (Intervento presentato al convegno ASME Turbo Expo 2022: Turbomachinery Technical Conference and Exposition, GT 2022 nel 2022) [10.1115/GT2022-82122].

ASSESSMENT OF THICKENED FLAME MODEL COUPLED WITH FLAMELET GENERATED MANIFOLD ON A LOW-SWIRL PARTIALLY PREMIXED GASEOUS LIFTED FLAME

Langone L.;Amerighi M.;Mazzei L.;Andreini A.;
2022

Abstract

The present work focuses on the numerical modeling through Large Eddy Simulations (LES) of a low-swirl partially premixed lean flame operated with gaseous fuel using a hybrid Thickened Flame (TF)-Flamelet Generated Manifolds (FGM) combustion model. This approach aims to overcome the challenges of modeling the flame lift-off in this burner and the stabilization of the reaction zone at a remarkable distance from the nozzle outlet section, for which the reproduction of finite rate effects on combustion physics is crucial. The underlying strategy consists of applying the artificial thickening to the scalar equations required for the query of the look-up table computed a priori. The mentioned combustion model has been implemented in a general-purpose commercial CFD solver and Non-Adiabatic Flamelets have been employed for the look-up table computation. The goal is to include a detailed chemistry description while maintaining a cost-effective approach and improving the reproduction of the turbulence-chemistry interaction. Results are validated with experimental data in terms of temperature and chemical species concentration maps, showing the potential of the coupled TF-FGM approach for describing this type of flame.
2022
ASME Turbo Expo 2022
ASME Turbo Expo 2022: Turbomachinery Technical Conference and Exposition, GT 2022
2022
Langone L.; Amerighi M.; Mazzei L.; Andreini A.; Orsino S.; Ansari N.; Yadav R.
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Utilizza questo identificatore per citare o creare un link a questa risorsa: https://hdl.handle.net/2158/1294925
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