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AERODYNAMIC DRAG MEASUREMENT IN A HIGH-ENTHALPY SHOCK TUNNEL 会议论文
ASME Fluids Engineering Division Summer Meeting (FEDSM2018), Montreal, CANADA, JUL 15-20, 2018
Authors:  Wang YP(汪运鹏);  Jiang ZL(姜宗林);  Teng HH(滕宏辉)
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Starting Process in a Large-Scale Shock Tunnel 会议论文
22nd AIAA Computational Fluid Dynamics Conference, Dallas, TX, JUN 22-26, 2015
Authors:  Wang YP;  Hu ZM(胡宗民);  Liu YF(刘云峰);  Jiang ZL(姜宗林);  Wang, YP (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
View  |  Adobe PDF(764Kb)  |  Favorite  |  View/Download:366/103  |  Submit date:2016/06/28
Concept of non-ablative thermal protection system for hypersonic vehicles 会议论文
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, CA, APR 11-14, 2011
Authors:  Liu YF(刘云峰);  Jiang ZL(姜宗林);  Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temperature Gas Dynam, Beijing 100190, Peoples R China.
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Research progress on high-enthalpy and hypersonic flows 会议论文
5th International Conference on Fluid Mechanics, Shanghai, PEOPLES R CHINA, AUG 15-19, 2007
Authors:  Jiang ZL(姜宗林);  Yu HR(俞鸿儒);  Lin ZB(林贞彬);  Jiang Z
Adobe PDF(690Kb)  |  Favorite  |  View/Download:894/246  |  Submit date:2009/07/23
Hypersonic Flows  Detonation Driver  Shock-reflected Tunnels  Shock-expanded Tube  Heat Transfer