| 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)
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| 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. |
| Files in This Item: | Download All | |||||
| File Name/Size | DocType | Version | Access | License | ||
| IrCA542.pdf（199KB） | 开放获取 | -- | View Download | |||
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