宽速域飞行器发展及研究现状综述  

Overview of development and research status of wide speed range aircraft

作　　者：谢赞 周灿灿 赵振涛 黄伟[1] Xie Zan;Zhou Cancan;Zhao Zhentao;Huang Wei(College of Aerospace Science and Engineering,National University of Defense Technology,Changsha 410073,China)

机构地区：[1]国防科技大学空天科学学院,长沙410073

出　　处：《空天技术》2022年第4期28-39,86,共13页Aerospace Technology

基　　金：湖南省杰出青年基金(2021JJ10045)。

摘　　要：水平起降、可重复使用的高超声速宽速域飞行器具有宽速域、大空域飞行全包线的适用性,具有飞行轨迹自由、能低成本快速入轨等优势。对水平起降、可重复使用的高超声速宽速域飞行器的研究进展进行综述,主要介绍了国外宽速域飞行器项目的研究进展和现状,阐述了国内宽速域飞行器的研究情况,得出了涡波效应-乘波构型、机翼-乘波构型和变形/组合构型三大类布局是发展水平起降宽速域飞行器主要思路的结论。介绍了未来水平起降、可重复使用的高超声速宽速域飞行器在升阻特性匹配、稳定性、减阻降热、推进技术和一体化设计方面的技术研究难点,提出了宽速域飞行器的后续研究发展方向,以期对宽速域飞行器的研究有一定的参考作用。The horizontal take-off and landing, reusable hypersonic wide speed range vehicle has the applicability of the full envelope of wide speed and large airspace flight. At the same time, it also owns the advantages of freedom of flight trajectory and entry into orbit fast with low cost. The research progress of the horizontal take-off and landing, reusable hypersonic wide speed range vehicle are summarized. The research progress and status of foreign wide speed range vehicles’ projects and expounded the current domestic research situation of wide speed range vehicles are mainly analyzed. It is naturally put forward that the three layouts of vortex effect-waverider configuration, wing-waverider configuration and deformation/combination configuration are the main ideas for the development of this kind of vehicle. Nevertheless, there are still many problems to be solved in the engineering application of hypersonic wide speed range vehicle. Therefore, it mainly introduces the technical research difficulties of the future horizontal take-off and landing, reusable hypersonic wide speed range vehicle in terms of lift-drag characteristic matching, stability, drag and heat reduction, propulsion technology and integrated design. Then, the follow-up research and development direction of this kind of vehicle is proposed. It is hoped that it will be a certain reference for the research of the wide speed range vehicle.

关 键 词：宽速域 水平起降 高超声速 气动布局 乘波构型 

分 类 号：V411[航空宇航科学与技术—航空宇航推进理论与工程]