标题
Performance of Transpiration-Cooled Heat Shields for Reentry Vehicles
作者
关键词
-
出版物
AIAA JOURNAL
Volume 58, Issue 2, Pages 830-841
出版商
American Institute of Aeronautics and Astronautics (AIAA)
发表日期
2019-12-18
DOI
10.2514/1.j058515
参考文献
相关参考文献
注意:仅列出部分参考文献,下载原文获取全部文献信息。- Influence of shock waves on supersonic transpiration cooling
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- Transpiration Cooling Using Liquid Water
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- (2008) Nobuaki ISHII et al. TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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