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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
作者:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(2434Kb)  |  收藏  |  浏览/下载:324/86  |  提交时间: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  
Numerical and Experimental Study on Vertical Takeoff and Separation of the Compound Aircraft 期刊论文
IEEE ACCESS, 2022, 卷号: 10, 页码: 47597-47617
作者:  Wang D;  Hong QZ(洪启臻);  Huang X(黄鑫);  Pei XB;  Wang J
Adobe PDF(4750Kb)  |  收藏  |  浏览/下载:163/24  |  提交时间:2022/07/18
Aircraft  Aircraft propulsion  Compounds  Aerodynamics  Engines  Automotive components  Tail  Compound aircraft  CFD  vertical take-off  dynamical separation of two aircraft