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Acta Aeronautica et Astronautica Sinica ›› 2023, Vol. 44 ›› Issue (15): 528875-528875.doi: 10.7527/S1000-6893.2023.28875

• Reviews • Previous Articles    

Research Progresses of rotating detonation combustion and its application

Weidong LIU, Haoyang PENG(), Shijie LIU, Hailong ZHANG, Xueqiang YUAN   

  1. College of Aerospace Science and Engineering,National University of Defense Technology,Changsha  410073,China
  • Received:2023-04-17 Revised:2023-04-27 Accepted:2023-05-20 Online:2023-08-15 Published:2023-05-31
  • Contact: Haoyang PENG E-mail:penghaoyang@nudt.edu.cn
  • Supported by:
    National Natural Science Foundation of China(12202491)

Abstract:

Detonation combustion is a combustion type that the shock wave is highly coupled with the reaction zone propagating at supersonic velocity. The detonation–based power propulsion system has the significant theory superiority, which is one of the vital development directions of the future aerospace technology. Continuous rotating detonation engine is one of the engineering applications of detonation combustion, with the obvious advantage over the high adaptation, short combustor length, and high thrust performance. It is expected to promote the significant development of aerospace power technology. This paper starts from the classical detonation theory, and then summarizes the related fundamental investigations of rotating detonation combustion. Subsequently, the recent progresses of engineering application on rotating detonation engine are introduced. And the development history of National University of Defense Technology on rotating detonation engine is reviewed and summarized. Last, the development and expectation of rotating detonation engine are proposed based on the current researches.

Key words: continuous rotating detonation, cycle analysis, combustion organization, combustion instability, detonation combustion

CLC Number: