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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：305/81  |  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  
Highly expanded flashing liquid jets in vacuum environment 会议论文
64th International Astronautical Congress 2013, IAC 2013, Beijing, China, September 23, 2013 - September 27, 2013
作者:  Du WF(杜王芳);  Zhao JF(赵建福)
Adobe PDF(36Kb)  |  收藏  |  浏览/下载：236/35  |  提交时间：2018/11/08
Environmental management  Evaporation  Fighter aircraft  Jets  Nozzles  Shock waves  Solenoid valves  Solenoids  Syringes  Testing  Environmental control system  Environmental pressures  Flashing liquid jets  Initial temperatures  Injection temperature  Low pressure environment  Pressurized liquids  Saturation pressure