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Effects of Shock Impingement on Aerothermal and Aerodynamic Performance for High-pressure Capturing Wings 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Li GL(李广利);  Cui K(崔凯);  Xiao Y(肖尧);  Xu YZ(徐应洲)
View  |  Adobe PDF(664Kb)  |  Favorite  |  View/Download：397/96  |  Submit date：2018/01/16
Aerodynamics  Angle Of Attack  Angle Of Attack Indicators  Boundary Layers  Drag  Drag Coefficient  High Pressure Effects  Hypersonic Aerodynamics  Hypersonic Flow  Spacecraft  
A conceptual design of next generation hypersonic air-breathing airplanes with dual waveriders forebody 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
Authors:  Cui K(崔凯);  Hu SC(胡守超);  Li GL;  Xiao Y(肖尧);  Situ M
View  |  Adobe PDF(872Kb)  |  Favorite  |  View/Download：363/156  |  Submit date：2017/05/05
Aero  Dynamic Performance  Aerodynamic Performance Predictions  Design Methodology  Flight Altitudes  Numerical Results  Propulsion System  Turbulent Models  Wing Body Aircraft  
Shape design to minimize the peak heat-flux of blunt leading-edge 会议论文
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013, Grapevine, TX, United states, JAN 07-10, 2013
Authors:  Cui K(崔凯);  Hu SC(胡守超);  Cui K(崔凯)
View  |  Adobe PDF(605Kb)  |  Favorite  |  View/Download：639/309  |  Submit date：2014/02/24
高压捕获翼气动布局研究 会议论文
中国力学大会——2013, 中国北京, 2013-08-19
Authors:  崔凯;  李广利;  胡守超;  屈志朋
Adobe PDF(1358Kb)  |  Favorite  |  View/Download：461/140  |  Submit date：2014/04/02
气动布局  高压  支撑机构  飞行器  乘波体  升阻比  三角翼  高升力  湍流  设计需求  阻性  计算结果  大容积  外形  进一步:0  
Leading edge aerothermal inverse design of hyersonic vehicle based on homotopy optimization method 会议论文
6th International Conference on Fluid Mechanics, Guangzhou, PEOPLES R CHINA, JUN 30-JUL 03, 2011
Authors:  Cui K(崔凯);  Hu SC(胡守超);  Gao TY(高太元);  Wang XP(王秀平);  Yang GW(杨国伟);  Cui, K (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
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Hypersonic  Blunt Leading Edge  Aerothermodynamic  Inverse Design  Homotopy  
Configuration optimization of hypersonic vehicles under transitional flow conditions 会议论文
16th AIAA/DLR/DGLR International Space Planes an Hypersonic Systems and Technologies Conference, Germany, Bremen, 2009-10
Authors:  Sun QH(孙泉华);  Fan J(樊菁);  Jiang JZ(蒋建政);  Cui K(崔凯);  Sun QH(孙泉华)
Adobe PDF(377Kb)  |  Favorite  |  View/Download：1228/407  |  Submit date：2009/12/28