Aerothermal optimization of hypersonic vehicle leading edge based on genetic algorithm | |
Cui K(崔凯); Hu SC(胡守超); Gao TY(高太元); Wang XP(王秀平); Yang GW(杨国伟) | |
Source Publication | Abstract Book of 23rd International Congress of Theoretical and Applied Mechanics |
2012 | |
Conference Name | 23rd International Congress of Theoretical and Applied Mechanics |
Conference Date | 2012-08-19 |
Conference Place | 中国北京/Beijing, China |
Abstract | This work is concerned with the design of a leading edge for hypersonic vehicles used to minimize the peak heat flux of the leading edge.The leading edge is parameterized by using B-spline curve method.The hypersonic flow field and the heat flux dis- |
Keyword | Vehicle Leading 0algorithm Genetic Hypersonic Optimization Aerothermal Based Method Design Attack Novel Around Angle Evaluated Greatly About Fluid Result Differ |
Department | LHD气动布局优化与计算方法 |
Language | 英语 |
Document Type | 会议论文 |
Identifier | http://dspace.imech.ac.cn/handle/311007/48586 |
Collection | 高温气体动力学国家重点实验室 |
Recommended Citation GB/T 7714 | Cui K,Hu SC,Gao TY,et al. Aerothermal optimization of hypersonic vehicle leading edge based on genetic algorithm[C]Abstract Book of 23rd International Congress of Theoretical and Applied Mechanics,2012. |
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