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Normal acceleration reduce guidanceand control for sub-orbit vehicle re-entry 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Li WH(李文皓);  Xiao XX(肖歆昕);  Zhang H(张珩);  Xiao XX(肖歆昕)
Adobe PDF(1066Kb)  |  Favorite  |  View/Download：436/94  |  Submit date：2018/01/16
Aerodynamics  Air Navigation  Angle Of Attack  Control Surfaces  Control Theory  Degrees Of Freedom (Mechanics)  Dynamic Models  Flight Control Systems  Flight Simulators  Monte Carlo Methods  Reentry  Spacecraft  Surface Reactions  Uncertainty Analysis  Vehicles  
Preliminary Study of Aerodynamic Performance for Waverider-based Hypersonic Vehicles with Dorsal Mounted Engines 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Xiao Y(肖尧);  Cui K(崔凯);  Li GL(李广利);  Xu YZ(徐应洲)
Adobe PDF(639Kb)  |  Favorite  |  View/Download：298/96  |  Submit date：2018/01/16
Aerodynamics  Air Engines  Aspect Ratio  Computational Fluid Dynamics  Drag  Engines  Hypersonic Aerodynamics  Lift  Lift Drag Ratio  Propulsion  Spacecraft  Vehicles