Aerothermal optimization of hypersonic vehicle leading edge based on genetic algorithm

	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)
会议录名称	Abstract Book of 23rd International Congress of Theoretical and Applied Mechanics
	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
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-
关键词	Vehicle Leading 0algorithm Genetic Hypersonic Optimization Aerothermal Based Method Design Attack Novel Around Angle Evaluated Greatly About Fluid Result Differ
课题组名称	LHD气动布局优化与计算方法
语种	英语
文献类型	会议论文
条目标识符	http://dspace.imech.ac.cn/handle/311007/48586
专题	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]Abstract Book of 23rd International Congress of Theoretical and Applied Mechanics,2012.