摘要
简述了美国高超音速飞行器计划的研制背景,介绍了乘波者飞行器的构型特点与热应力松弛设计考虑,初步探讨了高超音速验证飞行器的典型代表X-51A和HTV-2验证飞行失败的原因与遇到的技术困难。
In this paper, we simply mentioned the background of us hypersonic vehicles project and introduced a configuration characteristics and thermal stress relaxation considerations of wave-rider vehicle, preliminarily discussed a reason of failure of X-51A and HTV-2 vehicles and wave-rider confronting difficult.
出处
《强度与环境》
2012年第5期55-64,共10页
Structure & Environment Engineering