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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)
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Vehicle  Leading  0algorithm  Genetic  Hypersonic  Optimization  Aerothermal  Based  Method  Design  Attack  Novel  Around  Angle  Evaluated  Greatly  About  Fluid  Result  Differ  
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
Authors:  Cui K(崔凯);  Wang XP;  Hu SC;  Gao TY;  Yang GW(杨国伟)
Adobe PDF(797Kb)  |  Favorite  |  View/Download:1008/257  |  Submit date:2012/09/26
High Speed Train  Head Shape  Optimization  Rbf  Genetic Algorithm  Computational Fluid Dynamics  
基于CFD分析的高超声速飞行器上表面优化 会议论文
LHD2011夏季学术研讨会, 内蒙赤峰, 2011
Authors:  高太元;  崔凯;  胡守超;  王秀平;  杨国伟
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高超声速  B-样条参数化  Sqp  Cfd  
高速列车头型优化评估 会议论文
LHD2011夏季学术研讨会, 内蒙赤峰, 2011
Authors:  王秀平;  崔凯;  高太元;  胡守超
Adobe PDF(406Kb)  |  Favorite  |  View/Download:310/104  |  Submit date:2014/01/23
高速列车  头型  计算流体力学  优化设计  
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  
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
Authors:  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.
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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
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.
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Hypersonic  Shape Optimization  Sequential Quadratic Programming (Sqp)  
双发动机高超声速乘波飞行器性能分析 会议论文
LHD2011夏季学术研讨会, 内蒙赤峰, 2011
Authors:  崔凯;  高太元;  胡守超;  王秀平;  杨国伟
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高超声速  乘波体  升阻比  计算流体力学  
后体/尾喷管一体化设计构型对高超声速飞行器冷热态力矩差的影响 会议论文
LHD2011夏季学术研讨会, 内蒙赤峰, 2011
Authors:  胡守超;  崔凯;  高太元;  王秀平
Adobe PDF(691Kb)  |  Favorite  |  View/Download:355/90  |  Submit date:2014/01/23
高超声速  后体/尾喷管  一体化设计  冷热态力矩差  
吸气式高超声速飞行器上壁面多约束/多目标优化设计和分析 会议论文
第四届高超声速科技学术会议, 中国海南三亚, 2011
Authors:  崔凯;  高太元;  胡守超;  王秀平
Adobe PDF(65Kb)  |  Favorite  |  View/Download:493/138  |  Submit date:2012/04/01
高超声速  遗传算法  多目标优化  升阻比  容积