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.
Hypersonic vehicles represent furore trends of military equipments and play an important role in future war. Thermal protection materials and structures, which relate to the safety of hypersonic vehicles, are one of the most key techniques in design and manufacture of hypersonic vehicles. Among these materials and structures, such as metallic temperature protection structure, the a-high temperature ceramics and carbon/carbon composites are usually adopted in design. The recent progresses of research and application of ultra-high temperature materials in preparation, oxidation resistance, mechanical and physical characterization were summarized.
出处
《应用数学和力学》
CSCD
北大核心
2008年第1期47-56,共10页
Applied Mathematics and Mechanics
关键词
高超声速飞行器
高温
热防护
hypersonic vehicle
high-temperature
thermal protection
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）．
