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高超声速飞行器一体化防热与热控设计方法

王浚 王佩广

王浚, 王佩广. 高超声速飞行器一体化防热与热控设计方法[J]. 北京航空航天大学学报, 2006, 32(10): 1129-1134.
引用本文: 王浚, 王佩广. 高超声速飞行器一体化防热与热控设计方法[J]. 北京航空航天大学学报, 2006, 32(10): 1129-1134.
Wang Jun, Wang Peiguang. Integrated thermal protection and control system design methodology for hypersonic vehicles[J]. Journal of Beijing University of Aeronautics and Astronautics, 2006, 32(10): 1129-1134. (in Chinese)
Citation: Wang Jun, Wang Peiguang. Integrated thermal protection and control system design methodology for hypersonic vehicles[J]. Journal of Beijing University of Aeronautics and Astronautics, 2006, 32(10): 1129-1134. (in Chinese)

高超声速飞行器一体化防热与热控设计方法

详细信息
  • 中图分类号: V 245

Integrated thermal protection and control system design methodology for hypersonic vehicles

  • 摘要: 围绕高超声速飞行器所遭遇的"热障"问题,阐述了防热与热控系统一体化设计的思想,指出将机身结构、防热与热控系统、推进系统耦合在一起进行一体化设计是解决"热障"问题的有效途径,并提出了不同任务需求的高超声速飞行器防热与热控系统方案思路.介绍了部分防热材料的性能,指出了在设计中选择防热材料的原则.对防热与热控系统的优化方法进行了探讨,指出了防热与热控系统一体化设计中涉及的关键技术,举例说明了防热与热控一体化设计的基本流程.

     

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出版历程
  • 收稿日期:  2006-05-30
  • 网络出版日期:  2006-10-31

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