Flameholding characteristics and flame behaviors of a scramjet model combustor with two-stage fuel injection for low flight Mach numbers

In this study, two types of fuel injection methods were applied to a scramjet model combustor equipped with a dual-cavity flameholder and a burned-gas injection to achieve operation at a low flight speed corresponding to a flight Mach number of approximately 3. The first method was single-stage fuel...

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Những tác giả chính:	Kei NORIMATSU, Noriko KATSUMURA, Satoshi NISHIURA, Taku KUDO, Akihiro HAYAKAWA
Định dạng:	Artigo
Ngôn ngữ:	Inglês
Được phát hành:	The Japan Society of Mechanical Engineers 2026-02-01
Loạt:	Journal of Thermal Science and Technology
Những chủ đề:	scramjet combustor two-stage fuel injection dual-cavity flameholder flameholding characteristics supersonic combustion low flight mach number
Truy cập trực tuyến:	https://www.jstage.jst.go.jp/article/jtst/21/2/21_25-00382/_pdf/-char/en
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