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
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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:. |
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