跨流域高速飞行器气动设计研究现状及思考  

Research Status and Consideration on Aerodynamic Design of Hypersonic Flight Vehicle Covering Various Flow Regimes

作　　者：朱广生[1] 段毅 姚世勇 刘元春 李昊歌 ZHU Guangsheng;DUAN Yi;YAO Shiyong;LIU Yuanchun;LI Haoge(China Academy of Launch Vehicle Technology,Beijing 100076,China;Science and Technology on Space Physics Laboratory,Beijing 100076,China)

机构地区：[1]中国运载火箭技术研究院,北京100076 [2]空间物理重点实验室,北京100076

出　　处：《宇航学报》2023年第3期358-367,共10页Journal of Astronautics

基　　金：国家自然科学基金(U21B6003,12172058)。

摘　　要：针对跨流域空气动力学理论的不完善、多物理非平衡效应耦合的跨流域流场高精度预示模型缺乏、大空域和宽速域流动控制难度大等问题,本文从气动布局、气动预示和气动优化三个方面对跨流域高速飞行器气动设计的研究现状进行了回顾,对气动设计中涉及到的难点和关键问题进行了思考,并提出了相关发展建议。Aiming at the problems such as the imperfection of trans-regimes aerodynamic theory,the lack of high-precision prediction model of trans-regimes flow field coupled by multi-physical non-equilibrium effects,and the difficulty of flow control in large airspace and wide velocity domain,the aerodynamic design of hypersonic vehicles covering various flow regimes is summarized.Then,the research status of aerodynamic configuration,aerodynamic prediction and aerodynamic optimization of trans-regimes high-speed vehicles is described.Finally,some difficulties and key problems involved in aerodynamic design are proposed.

关 键 词：高速飞行器 跨流域 气动设计 气动布局 气动优化 

分 类 号：V19[航空宇航科学与技术—人机与环境工程]