摘要
总结了空空导弹气动设计特点,简要回顾了导弹空气动力学发展,介绍了不同时期典型空空导弹气动外形设计的独到之处,并结合在型号研制中遇到的工程实际问题和未来空战对空空导弹气动需求,提出了空空导弹气动设计面临的技术困难。
The characteristics of aerodynamic design for air-to-air missile are summarized. After a brief review of the development of missile aerodynamics, the originalities in aerodynamic configuration design for typical air-to-air missile in different periods are introduced. Then, considering both the practical engineering problems and the aerodynamics demand in future air combat, the technology difficulties for aerodynamic design of air-to-air missiles are proposed.
作者
李斌
刘仙名
Li Bin;Liu Xianming(China Airborne Missile Academy,Luoyang 471009,China;Aviation Key Laboratory of Science and Technology on Airborne Guided Weapons,Luoyang 471009,China)
出处
《航空兵器》
CSCD
北大核心
2019年第2期1-14,共14页
Aero Weaponry
关键词
空空导弹
气动外形
关键技术
air-to-air missile
aerodynamic configuration
key technology
