旋转爆震燃烧及应用研究进展

doi:10.7527/S1000-6893.2023.28875

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旋转爆震燃烧及应用研究进展

刘卫东, 彭皓阳(), 刘世杰, 张海龙, 袁雪强

国防科技大学空天科学学院，长沙　410073

收稿日期:2023-04-17 修回日期:2023-04-27 接受日期:2023-05-20 出版日期:2023-08-15 发布日期:2023-05-31
通讯作者: 彭皓阳 E-mail:penghaoyang@nudt.edu.cn
基金资助:
国家自然科学基金(12202491)

Research Progresses of rotating detonation combustion and its application

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

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)

摘要/Abstract

摘要：

爆震燃烧是一种激波与反应面高度耦合并以超声速传播的燃烧方式，基于爆震燃烧构建的动力推进装置具有理论性能优势，是未来空天领域重要的发展方向。连续旋转爆震发动机是爆震燃烧的一种应用形式，具有自适应能力强、发动机长度短、推力性能高等优势，有望推动航空航天动力技术的跨越发展。以经典爆震理论为切入点，总结了旋转爆震发动机相关的基础研究问题及旋转爆震发动机工程应用的研究进展，回顾了国防科技大学在旋转爆震领域的发展历程，最后展望了旋转爆震发动机未来发展。

关键词: 连续旋转爆震, 循环分析, 燃烧组织, 不稳定燃烧, 爆震燃烧

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

中图分类号:

V231

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.

Weidong LIU, Haoyang PENG, Shijie LIU, Hailong ZHANG, Xueqiang YUAN. Research Progresses of rotating detonation combustion and its application[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(15): 528875-528875.

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[1]	田佳, 张靖周, 谭晓茗, 王元帅. 旋转爆震燃烧室梯度复合热防护结构热分析模型及验证[J]. 航空学报, 2022, 43(3): 125271-125271.
[2]	王超, 刘卫东, 刘世杰, 蒋露欣, 苏义. 吸气式连续旋转爆震与来流相互作用[J]. 航空学报, 2016, 37(5): 1411-1418.
[3]	邱华, 王玮, 范玮, 熊姹. U型方管中爆燃向爆震转变特性实验研究[J]. 航空学报, 2015, 36(6): 1788-1794.
[4]	左斌;胡云安;李静. 一种新的极值搜索算法及其在航空发动机燃烧主动控制中的应用[J]. 航空学报, 2009, 30(7): 1187-1196.
[5]	李建中;王家骅;唐豪;袁丽. 煤油/空气三管气动阀式脉冲爆震发动机[J]. 航空学报, 2009, 30(11): 2052-2058.

旋转爆震燃烧及应用研究进展

Research Progresses of rotating detonation combustion and its application

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