QQ客服 官方微博 反馈留言

	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.; Mathematics, Interdisciplinary Applications; Mechanics; Physics, Fluids & Plasmas; EI; CPCI-S(ISTP); 1
语种	英语
内容类型	会议论文
源URL	[http://ir.pku.edu.cn/handle/20.500.11897/316479]
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:.

个性服务

查看访问统计

相关权益政策

暂无数据

收藏/分享

除非特别说明，本系统中所有内容都受版权保护，并保留所有权利。