Aerothermal optimization of hypersonic vehicle leading edge based on genetic algorithm
文献类型：会议论文
| 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)
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| 出版日期 | 2012 |
| 会议名称 | 23rd International Congress of Theoretical and Applied Mechanics |
| 会议日期 | 2012-08-19 |
| 会议地点 | 中国北京/Beijing, China |
| 关键词 | vehicle leading 0algorithm genetic hypersonic optimization aerothermal based method design attack novel around angle evaluated greatly about fluid result differ |
| 中文摘要 | 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- |
| 会议录 | Abstract Book of 23rd International Congress of Theoretical and Applied Mechanics
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| 语种 | 英语 |
| 源URL | [http://dspace.imech.ac.cn/handle/311007/48586]  |
| 专题 | 力学研究所_高温气体动力学国家重点实验室 |
| 推荐引用方式 GB/T 7714 | Cui K,Hu SC,Gao TY,et al. Aerothermal optimization of hypersonic vehicle leading edge based on genetic algorithm[C]. 见:23rd International Congress of Theoretical and Applied Mechanics. 中国北京/Beijing, China. 2012-08-19. |
入库方式： OAI收割
来源：力学研究所
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