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Experimental Study of Longitudinal Stage Separation of Two-Body Configuration in Shock Tunnel 期刊论文
AIAA Journal, 2022, 卷号: 60, 期号: 12, 页码: 6940-6946
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(2434Kb)  |  Favorite  |  View/Download：351/102  |  Submit date：2022/08/23
Aerodynamic Coefficients  Two Stage to Orbit  Aerodynamic Performance  Hypersonic Flight  Hypersonic Wind Tunnels  Solenoid Valves  Oblique Shock  Pneumatic Actuator  Hypersonic Flows  Computer Aided Engineering  
Starting Process in a Large-Scale Shock Tunnel 期刊论文
AIAA Journal, 2016, 卷号: 54, 期号: 5, 页码: 1240-1249
Authors:  Wang YP(汪运鹏);  Hu ZM(胡宗民);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
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Forward-Running Detonation Drivers for High-Enthalpy Shock Tunnels 期刊论文
AIAA Journal, 2002, 卷号: 40, 期号: 10, 页码: 2009-2016
Authors:  Jiang ZL(姜宗林);  Zhao W(赵伟);  Wang C(王超);  Takayama K;  Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gasdynam, Beijing 100080, Peoples R China.
View  |  Adobe PDF(288Kb)  |  Favorite  |  View/Download：1151/307  |  Submit date：2007/06/15