Investigation of combustion mode conversion driven by fuel flow variation in a cavity-based scramjet

This work aimed to investigate combustion mode conversions by rapid variation of the fuel flow rate in a cavity-based scramjet combustor. The experiments were carried out on a direct-connected facility with an inflow condition of Mach number 2.52, a total pressure of 1.35 MPa, and a total temperatur...

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Veröffentlicht in:	Physics of fluids (1994) 2024-10, Vol.36 (10)
Hauptverfasser:	Li, Le, Wan, Minggang, Sun, Mingbo, Tian, Yifu, Zhu, Jiajian
Format:	Artikel
Sprache:	eng
Schlagworte:	Combustion chambers Conversion Equivalence ratio Flame propagation Flow velocity Fuel flow Fuel injection Imaging techniques Mach number Propagation modes Shear layers Supersonic combustion ramjet engines Upstream
Online-Zugang:	Volltext
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