The injectors near-field region of LRE combustion chambers is numerically investigated by means of both multi and single-injector combustor simulations. An efficient and validated uRANS numerical framework based on non-adiabatic flamelets is used to describe methane-oxygen turbulent nonpremixed combustion. Two paradigmatic configurations, representing the flame-wall and flame-flame interactions occurring on an injection plate are used to develop a 2D axy-symetric dataset. On both configurations, the confinement length of the injector is parametrically varied in order to isolate its effect on the heat flux insisting on the injector face-plate. Finally the results are compared to a fully 3D case, consisting in 37 injectors characterized by the same operating conditions and parameters as the 2D cases.

Characterization of the injectors near-field region of LRE combustion chambers / Lapenna, P. E.; Remiddi, A.; Indelicato, G.; Valorani, M.; Pizzarelli, M.; Creta, F.. - (2022). (Intervento presentato al convegno 9ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) tenutosi a Lille, France) [10.13009/EUCASS2022-4851].

Characterization of the injectors near-field region of LRE combustion chambers

P. E. Lapenna
;
A. Remiddi;G. Indelicato;M. Valorani;M. Pizzarelli;F. Creta
2022

Abstract

The injectors near-field region of LRE combustion chambers is numerically investigated by means of both multi and single-injector combustor simulations. An efficient and validated uRANS numerical framework based on non-adiabatic flamelets is used to describe methane-oxygen turbulent nonpremixed combustion. Two paradigmatic configurations, representing the flame-wall and flame-flame interactions occurring on an injection plate are used to develop a 2D axy-symetric dataset. On both configurations, the confinement length of the injector is parametrically varied in order to isolate its effect on the heat flux insisting on the injector face-plate. Finally the results are compared to a fully 3D case, consisting in 37 injectors characterized by the same operating conditions and parameters as the 2D cases.
2022
9ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
liquid rocket engines; combustion chambers; computational fluid dynamics; parametric analysis
04 Pubblicazione in atti di convegno::04b Atto di convegno in volume
Characterization of the injectors near-field region of LRE combustion chambers / Lapenna, P. E.; Remiddi, A.; Indelicato, G.; Valorani, M.; Pizzarelli, M.; Creta, F.. - (2022). (Intervento presentato al convegno 9ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) tenutosi a Lille, France) [10.13009/EUCASS2022-4851].
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11573/1666674
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