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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
作者:  Cui K(崔凯);  Hu SC(胡守超);  Li GL;  Xiao Y(肖尧);  Situ M
浏览  |  Adobe PDF(872Kb)  |  收藏  |  浏览/下载：351/152  |  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  
Conceptual design and aerodynamic evaluation of hypersonic airplane with double flanking air inlets 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2013, 卷号: 56, 期号: 8, 页码: 1980-1988
作者:  Cui K(崔凯);  Hu SC(胡守超);  Li GL(李广利);  Qu ZP(屈志朋);  Situ M;  Cui, K (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(1426Kb)  |  收藏  |  浏览/下载：865/295  |  提交时间：2013/09/27
Hypersonic  Flanking Air Inlet  Waverider  Computational Fluid Dynamics(Cfd)  
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
作者:  Cui K(崔凯);  Hu SC(胡守超);  Cui K(崔凯)
浏览  |  Adobe PDF(605Kb)  |  收藏  |  浏览/下载：628/306  |  提交时间：2014/02/24
Shape Optimization of High-Speed Train with the Speed of 500kph 会议论文
The 1st International Workshop on High-Speed and Intercity Railways, Beijing, 2012
作者:  Cui K(崔凯);  Wang XP;  Hu SC;  Gao TY;  Yang GW(杨国伟)
Adobe PDF(797Kb)  |  收藏  |  浏览/下载：1212/353  |  提交时间：2012/09/26
High Speed Train  Head Shape  Optimization  Rbf  Genetic Algorithm  Computational Fluid Dynamics  
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
作者:  Cui K(崔凯);  Hu SC(胡守超);  Gao TY(高太元);  Wang XP(王秀平);  Yang GW(杨国伟)
浏览  |  Adobe PDF(199Kb)  |  收藏  |  浏览/下载：472/73  |  提交时间：2014/04/02
Vehicle  Leading  0algorithm  Genetic  Hypersonic  Optimization  Aerothermal  Based  Method  Design  Attack  Novel  Around  Angle  Evaluated  Greatly  About  Fluid  Result  Differ  
Aerodynamic optimization and evaluation for the three-dimensional afterbody/nozzle integrated configuration of hypersonic vehicles 期刊论文
Chinese Science Bulletin, 2012, 卷号: 57, 期号: 8, 页码: 849-857
作者:  Gao TY(高太元);  Cui K(崔凯);  Wang XP(王秀平);  Hu SC(胡守超);  Yang GW(杨国伟);  Ren L;  kcui@imech.ac.cn
Adobe PDF(985Kb)  |  收藏  |  浏览/下载：1127/307  |  提交时间：2012/09/26
Hypersonic Afterbody/Nozzle Integrated Configuration Single Expanding Ramp Nozzle Optimization Computational Fluid Dynamics  
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
作者:  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)  |  收藏  |  浏览/下载：784/188  |  提交时间：2013/02/26
Hypersonic  Blunt Leading Edge  Aerothermodynamic  Inverse Design  Homotopy  
Primary study of aerodynamic performance evaluation and optimization of the high-speed train 会议论文
6th International Conference on Fluid Mechanics, Guangzhou, PEOPLES R CHINA, JUN 30-JUL 03, 2011
作者:  Wang XP(王秀平);  Cui K(崔凯);  Hu SC(胡守超);  Gao TY(高太元);  Yang GW(杨国伟);  Wang, XP (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
Adobe PDF(349Kb)  |  收藏  |  浏览/下载：606/142  |  提交时间：2013/02/26
China Railways High-speed (Crh)  Nose Shape  Computational Fluid Mechanics  Optimization  
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
作者:  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)  |  收藏  |  浏览/下载：719/195  |  提交时间：2013/02/26
Hypersonic  Shape Optimization  Sequential Quadratic Programming (Sqp)