收稿日期:2023-11-15
修回日期:2023-11-20
接受日期:2023-11-24
出版日期:2024-03-15
发布日期:2023-12-13
通讯作者:
刘小勇
E-mail:31suoban@sina.com
基金资助:
Xiaoyong LIU(
), Mingfu WANG, Jianwen LIU, Xin REN, Xuan ZHANG
Received:2023-11-15
Revised:2023-11-20
Accepted:2023-11-24
Online:2024-03-15
Published:2023-12-13
Contact:
Xiaoyong LIU
E-mail:31suoban@sina.com
Supported by:摘要:
自20世纪50年代以来,航空航天领域把超燃冲压发动机作为高超声速推进系统的一种追求目标,在理论和技术方面矢志不渝地开展了大量研究工作。21世纪初,美国取得了一系列接近实际应用的技术突破,将超燃冲压发动机技术的研究和应用推动至新阶段。简述了超燃冲压发动机工作原理,论述了双模态工作过程、高超声速压缩流动、超声速燃烧、超高温结构与热防护、地面试验与数值模拟等关键技术的难点和新进展,并针对超燃冲压发动机宽速域、可重复和更高马赫数等当前重点技术发展方向,阐述了认识和建议。
中图分类号:
刘小勇, 王明福, 刘建文, 任鑫, 张轩. 超燃冲压发动机研究回顾与展望[J]. 航空学报, 2024, 45(5): 529878.
Xiaoyong LIU, Mingfu WANG, Jianwen LIU, Xin REN, Xuan ZHANG. Review and prospect of research on scramjet[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(5): 529878.
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