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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：337/94  |  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  
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.
View  |  Adobe PDF(8891Kb)  |  Favorite  |  View/Download：415/121  |  Submit date：2015/03/17