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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  
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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Accurate Measurement of Nonlinear Liquid Sloshing 期刊论文
AIAA Journal, 2015, 卷号: 53, 期号: 3, 页码: 771-779
Authors:  Yang Y;  Liu ZW;  Shi WX;  Huang XF(黄先富);  Liu, ZW (reprint author), Beijing Inst Technol, Sch Aerosp Engn, Dept Mech, Beijing 100081, Peoples R China.
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Control Of Vortex Shedding From A Square Cylinder 期刊论文
AIAA Journal, 2008, 页码: 397-407
Authors:  Shao CP(邵传平);  Wei QD;  Shao, CP (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100080, Peoples R China.
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Spatially Developing Flows  
Shock-Tube Operation with Laser-Beam-Induced Diaphragm Rupture 期刊论文
AIAA Journal, 2006, 卷号: 44, 期号: 5, 页码: 1110-1112
Authors:  Sasoh A;  Takahashi T;  Watanabe K;  Torikai H;  Yang QS(杨乾锁)
Adobe PDF(228Kb)  |  Favorite  |  View/Download：697/217  |  Submit date：2007/06/15