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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)
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Aerodynamic Coefficients  Two Stage to Orbit  Aerodynamic Performance  Hypersonic Flight  Hypersonic Wind Tunnels  Solenoid Valves  Oblique Shock  Pneumatic Actuator  Hypersonic Flows  Computer Aided Engineering  
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.
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Micro-shock waves generated inside a fluid jet impinging on plane wall 期刊论文
AIAA Journal, 2001, 卷号: 39, 期号: 3, 页码: 424-430
Authors:  Jagadeesh G;  Onodera O;  Ogawa T;  Takayama K;  Jiang ZL(姜宗林);  Jagadeesh, G (reprint author), Tohoku Univ, Shock Wave Res Ctr, Inst Fluid Sci, Sendai, Miyagi 9808577, Japan.
Adobe PDF(1027Kb)  |  Favorite  |  View/Download：806/291  |  Submit date：2007/06/15