IMECH-IR  > 高温气体动力学国家重点实验室
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 PublicationAbstract Book of 23rd International Congress of Theoretical and Applied Mechanics
2012
Conference Name23rd International Congress of Theoretical and Applied Mechanics
Conference Date2012-08-19
Conference Place中国北京/Beijing, China
AbstractThis 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-
KeywordVehicle Leading 0algorithm Genetic Hypersonic Optimization Aerothermal Based Method Design Attack Novel Around Angle Evaluated Greatly About Fluid Result Differ
DepartmentLHD气动布局优化与计算方法
Language英语
Document Type会议论文
Identifierhttp://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
Related Services
Recommend this item
Bookmark
Usage statistics
Export to Endnote
Google Scholar
Similar articles in Google Scholar
[崔凯]'s Articles
[胡守超]'s Articles
[高太元]'s Articles
Baidu academic
Similar articles in Baidu academic
[崔凯]'s Articles
[胡守超]'s Articles
[高太元]'s Articles
Bing Scholar
Similar articles in Bing Scholar
[崔凯]'s Articles
[胡守超]'s Articles
[高太元]'s Articles
Terms of Use
No data!
Social Bookmark/Share
File name: IrCA542.pdf
Format: Adobe PDF
 

Items in the repository are protected by copyright, with all rights reserved, unless otherwise indicated.