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高超声速飞行器热防护材料与结构的研究进展

杨亚政 杨嘉陵 方岱宁

杨亚政, 杨嘉陵, 方岱宁. 高超声速飞行器热防护材料与结构的研究进展[J]. 应用数学和力学, 2008, 29(1): 47-56.
引用本文: 杨亚政, 杨嘉陵, 方岱宁. 高超声速飞行器热防护材料与结构的研究进展[J]. 应用数学和力学, 2008, 29(1): 47-56.
YANG Ya-zheng, YANG Jia-ling, FANG Dai-ning. Research Progress on the Thermal Protection Materials and Structures in Hypersonic Vehicles[J]. Applied Mathematics and Mechanics, 2008, 29(1): 47-56.
Citation: YANG Ya-zheng, YANG Jia-ling, FANG Dai-ning. Research Progress on the Thermal Protection Materials and Structures in Hypersonic Vehicles[J]. Applied Mathematics and Mechanics, 2008, 29(1): 47-56.

高超声速飞行器热防护材料与结构的研究进展

详细信息
    作者简介:

    杨亚政(1968- ),男,黑龙江北安人,副编审,硕士(联系人.Tel:+86-10-62559209;Fax:+86-10-62559588;E-mail:yzyang@cstam.org.cn).

  • 中图分类号: V250.1

Research Progress on the Thermal Protection Materials and Structures in Hypersonic Vehicles

  • 摘要: 高超声速飞行器是航空航天的一个重要发展方向,在未来国防安全中起着重要作用.高超声速飞行器热防护材料与结构是高超声速飞行器设计与制造的关键技术之一,它关系到飞行器的安全.高超声速飞行器热防护材料与结构主要有金属TPS热防护系统、超高温陶瓷、C/C复合材料等.从材料制备、抗氧化、力学与物理性能表征等方面综述了热防护材料与结构的研究与应用现状,评述了其发展趋势.
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出版历程
  • 收稿日期:  2007-10-07
  • 修回日期:  2007-10-29
  • 刊出日期:  2008-01-15

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