Rotating detonation engine injection velocity limit and nozzle effects on its propulsion performance

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	Rotating detonation engine injection velocity limit and nozzle effects on its propulsion performance
	Wang, Jian-Ping ; Shao, Ye-Tao
	2011
DOI	10.1007/978-3-642-17884-9-100
英文摘要	Three-dimensional numerical simulation of a rotating detonation engine (RDE) is carried out in coaxial tube chamber to reveal its physical characteristics. Multi-cycle process of RDE is numerically obtained, and it qualitatively agrees with former experimental results. Some key problems about RDE achievements such as fuel injection, pre-combustion, detonation structure are discussed. At last, we made a propulsion performance analysis about RDE by several different numerical cases. ? 2011 Springer-Verlag Berlin Heidelberg.; EI; 789-795
会议录	6th International Conference on Computational Fluid Dynamics, ICCFD 2010
语种	英语
内容类型	会议论文
源URL	[http://ir.pku.edu.cn/handle/20.500.11897/461730]
专题	工学院
推荐引用方式 GB/T 7714	Wang, Jian-Ping,Shao, Ye-Tao. Rotating detonation engine injection velocity limit and nozzle effects on its propulsion performance[C]. 见:.