Chinese | English

Search in the results

IMECH-IR

Browse/Search Results:  1-10 of 14 Help

Filters        
Selected(0)Clear Items/Page:    Sort:
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  
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)
View  |  Adobe PDF(639Kb)  |  Favorite  |  View/Download：285/89  |  Submit date：2018/01/16
Aerodynamics  Air Engines  Aspect Ratio  Computational Fluid Dynamics  Drag  Engines  Hypersonic Aerodynamics  Lift  Lift Drag Ratio  Propulsion  Spacecraft  Vehicles  
Study on Compression Surface Deformation of Waveriders 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Xu YZ(徐应洲);  Cui K(崔凯);  Li GL(李广利);  Xiao Y(肖尧)
View  |  Adobe PDF(461Kb)  |  Favorite  |  View/Download：321/88  |  Submit date：2018/01/16
Aerodynamic Configurations  Aerodynamics  Computational Fluid Dynamics  Deformation  Evolutionary Algorithms  Fluid Dynamics  Hypersonic Aerodynamics  Optimization  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
Adobe PDF(872Kb)  |  Favorite  |  View/Download：364/156  |  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)
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  
双旁侧进气高超声速飞机气动布局与评估 会议论文
LHD2012夏季学术研讨会, 吉林延吉, 2012
Authors:  胡守超;  崔凯;  李广利;  屈志朋;  杨国伟
Adobe PDF(1737Kb)  |  Favorite  |  View/Download：516/134  |  Submit date：2014/01/23
高超声速  双旁侧进气  气动布局  计算流体动力学(Cfd)  
Aerothermal optimization of hypersonic vehicle leading edge based on genetic algorithm 会议论文
23rd International Congress of Theoretical and Applied Mechanics, 中国北京/Beijing, China, 2012-08-19
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)
View  |  Adobe PDF(199Kb)  |  Favorite  |  View/Download：480/75  |  Submit date：2014/04/02
Vehicle  Leading  0algorithm  Genetic  Hypersonic  Optimization  Aerothermal  Based  Method  Design  Attack  Novel  Around  Angle  Evaluated  Greatly  About  Fluid  Result  Differ  
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.
Adobe PDF(53Kb)  |  Favorite  |  View/Download：829/191  |  Submit date：2013/02/26
Hypersonic  Blunt Leading Edge  Aerothermodynamic  Inverse Design  Homotopy  
Optimization of the upper surface of hypersonic vehicle based on CFD analysis 会议论文
6th International Conference on Fluid Mechanics, Guangzhou, PEOPLES R CHINA, JUN 30-JUL 03, 2011
Authors:  Gao TY(高太元);  Cui K(崔凯);  Hu SC(胡守超);  Wang XP(王秀平);  Yang GW(杨国伟);  Gao, TY (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(305Kb)  |  Favorite  |  View/Download：732/199  |  Submit date：2013/02/26
Hypersonic  Shape Optimization  Sequential Quadratic Programming (Sqp)