旋转爆震燃烧及应用研究进展
收稿日期: 2023-04-17
修回日期: 2023-04-27
录用日期: 2023-05-20
网络出版日期: 2023-05-31
基金资助
国家自然科学基金(12202491)
Research Progresses of rotating detonation combustion and its application
Received date: 2023-04-17
Revised date: 2023-04-27
Accepted date: 2023-05-20
Online published: 2023-05-31
Supported by
National Natural Science Foundation of China(12202491)
刘卫东 , 彭皓阳 , 刘世杰 , 张海龙 , 袁雪强 . 旋转爆震燃烧及应用研究进展[J]. 航空学报, 2023 , 44(15) : 528875 -528875 . DOI: 10.7527/S1000-6893.2023.28875
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.
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