| 高超音速技术发展概述 |
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| 引用本文： | 李清源,史俊红.高超音速技术发展概述[J].强度与环境,2012(5):55-64. |
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| 作者姓名： | 李清源 史俊红 |
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| 作者单位： | 北京强度环境研究所,北京 100076 |
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| 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。
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| 关 键 词： | X-51A HTV-2 高超音速技术 乘波者 |
Recent developments of hypersonic technology |
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| LI Qingyuan,SHI Junhong.Recent developments of hypersonic technology[J].Structure & Environment Engineering,2012(5):55-64. |
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| Authors: | LI Qingyuan SHI Junhong |
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| Institution: | (Beijing Institute of Structure and Environment Engineering, Beijing 100076, China) |
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| Abstract: | 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. |
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| Keywords: | X-51A HTV-2 hypersonic technology wave-rider |
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