Progress of continuously rotating detonation engines

被引:0
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作者
Zhou Rui [1 ]
Wu Dan [2 ]
Wang Jianping [3 ]
机构
[1] Center for Combustion and Propulsion, College of Engineering, Peking University
[2] Center for Applied Physics and Technology, Peking University
[3] State Key Laboratory for Turbulence & Complex Systems, Peking
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摘要
Continuously rotating detonation engine(CRDE) is a focus for concern in the field of aerospace propulsion. It has several advantages, including one-initiation, high thermal efficiency and simple structure. Due to these characteristics, it is expected to bring revolutionary advancements to aviation and aerospace propulsion systems and now has drawn much attention throughout the world. In this paper, an overview of the development of CRDE is given from several aspects:basic concepts, applications, experimental studies, numerical simulations, and so on. Representative results and outstanding contributions are summarized and the unresolved issues for further engineering applications of CRDE are provided.
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页数:15
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