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Experimental investigation of relationship between deflagration and detonation in a rotating detonation engine

Siyuan HUANG Shijie LIU Yu CHEN Ping WANG Haoyang PENG

中国航空学报（英文版）2026，Vol.39Issue(8)：65-77,13.

中国航空学报（英文版）2026，Vol.39Issue(8)：65-77,13.DOI:10.1016/j.cja.2025.104054

Experimental investigation of relationship between deflagration and detonation in a rotating detonation engine

Siyuan HUANG ¹Shijie LIU ²Yu CHEN ¹Ping WANG ¹Haoyang PENG²

作者信息

1. Aviation University of Air Force,Changchun 130022,China
2. Hypersonic Technology Laboratory,National University of Defense Technology,Changsha 410073,China
折叠

摘要

关键词

Chemiluminescence imaging/Coupling effect/Deflagration/Hollow combustor/Propellant reactivity/Rotating detonation engine

Key words

Chemiluminescence imaging/Coupling effect/Deflagration/Hollow combustor/Propellant reactivity/Rotating detonation engine

引用本文复制引用

Siyuan HUANG,Shijie LIU,Yu CHEN,Ping WANG,Haoyang PENG..Experimental investigation of relationship between deflagration and detonation in a rotating detonation engine[J].中国航空学报（英文版）,2026,39(8):65-77,13.

基金项目

This work is supported by the National Natural Science Foun-dation of China(Nos.52506176 and 12202491). （Nos.52506176 and 12202491）

中国航空学报（英文版）

ISSN：1000-9361

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