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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:300/80  |  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  
Chemical kinetics and self-ignition in a model supersonic hydrogen-air combustor 期刊论文
AIAA Journal, 1999, 卷号: 37, 期号: 2, 页码: 208-214
作者:  Sung CJ;  Li JG(李建国);  Yu G(俞刚);  Sung, CJ (reprint author), Princeton Univ, Dept Mech & Aerosp Engn, Princeton, NJ 08544 USA.
Adobe PDF(267Kb)  |  收藏  |  浏览/下载:572/213  |  提交时间:2007/06/15