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Investigation of dual ignition for a detonation-driven shock tunnel in forward driving mode 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 5, 页码: 1468-1475
Authors:  Wang Q(汪球);  Luo K(罗凯);  Li JW(栗继伟);  Li JP(李进平);  Zhao W(赵伟)
Adobe PDF(2057Kb)  |  Favorite  |  View/Download：264/82  |  Submit date：2020/08/26
Shock tunnel  Detonation driver  Diaphragm  Dual ignition  High-enthalpy flow  
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
Authors:  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.
View  |  Adobe PDF(763Kb)  |  Favorite  |  View/Download：544/230  |  Submit date：2016/03/21
Aerodynamic Heating  Hypersonic  Shock Tunnel  Stanton Number  Sharp Cone