Author:
Wang Dini,Zeng Yi,Xiong Xiang,Li Guodong,Chen Zhaoke,Sun Wei,Wang Yalei
Funder
National Basic Research Program of China
Creative Research Group of National Natural Science Foundation of China
Subject
Materials Chemistry,Surfaces, Coatings and Films,Process Chemistry and Technology,Ceramics and Composites,Electronic, Optical and Magnetic Materials
Reference28 articles.
1. G. David, Ceramic matrix composite (CMC) thermal protection systems (TPS) and hot structures for hypersonic vehicles, in: 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, American Institute of Aeronautics and Astronautics, Dayton, OH, 2008.
2. The hypersonic environment: required operating conditions and design challenges;Wie;J. Mater. Sci.,2004
3. Microstructure and ablation behavior of carbon/carbon composites infiltrated with Zr–Ti;Zeng;Carbon,2013
4. Microstructure and ablation performances of dual-matrix carbon/carbon composites;Yin;Carbon,2006
5. Ablation behaviors of ultra-high temperature ceramic composites;Tang;Mater. Sci. Eng., A,2007
Cited by
31 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献