Combustion modes of kerosene spray in a scramjet combustor with different injection schemes

Combustion modes of kerosene spray in a scramjet combustor condition with different injection schemes are experimentally investigated at Mach 2.52. The study is based on two single injectors with nozzle diameters of 0.79 and 1.14 mm and two dual injectors with nozzle diameters of 0.56 and 0.72 mm, r...

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Veröffentlicht in:	Physics of fluids (1994) 2024-09, Vol.36 (9)
Hauptverfasser:	Li, Fan, Zhang, Jincheng, Zhao, Guoyan, Sun, Mingbo, Li, Fei, Ma, Guangwei, Liu, Mingjiang
Format:	Artikel
Sprache:	eng
Schlagworte:	Combustion chambers Equivalence ratio Flame stability Injectors Kerosene Nozzles Supersonic combustion ramjet engines
Online-Zugang:	Volltext
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