力学与实践 ›› 2011, Vol. 33 ›› Issue (1): 1-9.DOI: 10.6052/1000-0879-lxysj2010-524

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近空间高超声速飞行器防热隔热与热力耦合研究进展

蒋持平1,柴慧2,严鹏1   

  1. 1. 北京航空航天大学航空科学与工程学院
    2.
  • 收稿日期:2010-12-30 修回日期:2011-01-23 出版日期:2011-02-15 发布日期:2011-03-03
  • 通讯作者: 蒋持平

ADVANCES IN THERMAL PROTECTION OF NEAR SPACE HYPERSONIC FLYING VEHICLES AND RELATED RESEARCHES OF THERMO-MECHANICAL COUPLING

  • Received:2010-12-30 Revised:2011-01-23 Online:2011-02-15 Published:2011-03-03

摘要: 概述近空间的战略价值与世界主要国家在近空间高超声速飞行器研制方面的竞争, 高超声速飞行器热防护系统及其基础科学问题, 包括防热隔热技术原理与热力耦合问题的研究进展.

关键词:

热力耦合

Abstract: This paper briefly summarizes the strategic value of the near space and the fierce competition in developing hypersonic vehicles over the world, and focuses on the development of the thermal protection system of hypersonic vehicles as well as related fundamental scientific problems, including the thermal protection principle, technique and thermo-mechanical coupling analysis.

Key words:

thermo-mechanical coupling