Performance of a Dual-Mode Combustor with Multistaged Fuel Injection

A scramjet combustor, which has a constant cross-sectional area combustor (designated as combustor 1), and a diverging combustor (designated as combustor 2), was examined with both single and two-stage fuel injection to determine whether it could be operated in the ramjet mode. The combustor was dir...

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Veröffentlicht in:	Journal of propulsion and power 2006-05, Vol.22 (3), p.518-526
Hauptverfasser:	Kobayashi, Kan, Tomioka, Sadatake, Kato, Kanenori, Murakami, Atsuo, Kudo, Kenji
Format:	Artikel
Sprache:	eng
Schlagworte:	Combustion chambers Fuel injection
Online-Zugang:	Volltext
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