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	Experimental Investigation of Shock-Wave-Streamwise-Vortex Interaction 期刊论文 OAI收割 AIAA JOURNAL, 2025, 卷号: 63, 期号: 8, 页码: 3079-3106 作者: Wang, Ziao; Yao, Kai; Chang, Juntao; Yue LJ(岳连捷); Chen, Hao \| 收藏 \| 浏览/下载：1/0 \| 提交时间：2025/09/15 Shock Wave Interaction Vortex Structure Strong Oblique Shock Waves Aerodynamics Fluid Mechanics Aircraft Wing Design Supersonic Wind Tunnels Aircraft Engines Aircraft Components and Structure Flow Conditions
	A conceptual design of next generation hypersonic air-breathing airplanes with dual waveriders forebody 会议论文 OAI收割 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015 作者: Cui K(崔凯); Hu SC(胡守超); Li GL; Xiao Y(肖尧); Situ M 收藏 \| 浏览/下载：46/0 \| 提交时间：2017/05/05 Aero dynamic performance Aerodynamic performance predictions Design Methodology Flight altitudes Numerical results Propulsion system Turbulent models Wing body aircraft
	Longitudinal control law design and simulation of fixed-wing UAV (EI CONFERENCE) 会议论文 OAI收割 2012 International Conference on Measurement, Instrumentation and Automation, ICMIA 2012, September 15, 2012 - September 16, 2012, Guangzhou, China 作者: Duan Z. 收藏 \| 浏览/下载：36/0 \| 提交时间：2013/03/25 Taken some fixed-wing UAV as the study object the aircraft movement was broken down into the longitudinal movement and lateral movement according to the linearized small perturbation principle the longitudinal control law design method was discussed using root locus which belonged to classical control theory. The six degrees of freedom nonlinear model simulation result shows that: the control parameters designed are reasonable the simulation profile is fully consistent with the setting profile the control effect of pitch angle loop and altitude loop meets with the indices requirements the method is mature and reliable easy to realize in engineering. (2013) Trans Tech Publications Switzerland.