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Comparative study on aerodynamic heating under perfect and nonequilibrium hypersonic flows 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2016, 卷号: 59, 期号: 2, 页码: 624701
作者:  Wang Q(汪球);  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林);  Li, JP (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(763Kb)  |  收藏  |  浏览/下载：539/228  |  提交时间：2016/03/21
Aerodynamic Heating  Hypersonic  Shock Tunnel  Stanton Number  Sharp Cone  
Development of the detonation-driven expansion tube for orbital speed experiments 期刊论文
Science China-Technological Sciences, 2015, 卷号: 58, 期号: 4, 页码: 695-700
作者:  Jiang ZL(姜宗林);  Wu B(吴波);  Gao YL;  Zhao W(赵伟);  Hu ZM(胡宗民);  Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(532Kb)  |  收藏  |  浏览/下载：642/156  |  提交时间：2015/04/28
Detonation Driver  Shock-expansion Tube  High-enthalpy Flow  Test Flow  
A novel oblique detonation structure and its stability 期刊论文
Chinese Physics Letters, 2007, 卷号: 24, 期号: 7, 页码: 1985-1988
作者:  Teng HH(滕宏辉);  Zhao W(赵伟);  Jiang ZL(姜宗林);  Hong-Hui, T (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100080, Peoples R China.
Adobe PDF(319Kb)  |  收藏  |  浏览/下载：735/207  |  提交时间：2009/08/03
Waves