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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  
Local Piston Theory with Viscous Correction and Its Application 期刊论文
AIAA Journal, 2017, 卷号: 55, 期号: 3, 页码: 942-954
作者:  Liu W(刘文);  Zhang CA(张陈安);  Han HQ;  Wang FM(王发民);  Zhang, CA (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1329Kb)  |  收藏  |  浏览/下载:573/114  |  提交时间:2017/03/28
Hypersonic  Unsteady Aerodynamics  Piston Theory  Aeroelasticity