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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...

詳細記述

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書誌詳細
主要な著者: Kei NORIMATSU, Noriko KATSUMURA, Satoshi NISHIURA, Taku KUDO, Akihiro HAYAKAWA
フォーマット: Artigo
言語:Inglês
出版事項: The Japan Society of Mechanical Engineers 2026-02-01
シリーズ:Journal of Thermal Science and Technology
主題:
オンライン・アクセス:https://www.jstage.jst.go.jp/article/jtst/21/2/21_25-00382/_pdf/-char/en
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