Response Surface Technique for Static Aeroelastic Optimization on a High-Aspect-Ratio Wing

	Response Surface Technique for Static Aeroelastic Optimization on a High-Aspect-Ratio Wing
	Yang GW(杨国伟); Chen DW(陈大伟); Cui K(崔凯); Yang GW
发表期刊	Journal of Aircraft
	2009
卷号	46 期号:4 页码:1444-1450
ISSN	0021-8669
关键词	Navier-stokes Solver Aircraft
DOI	10.2514/1.42370
收录类别	SCI
语种	英语
WOS记录号	WOS:000268906100038
关键词[WOS]	NAVIER-STOKES SOLVER ; AIRCRAFT
WOS研究方向	Engineering
WOS类目	Engineering, Aerospace
引用统计	被引频次：8[WOS] [WOS记录] [WOS相关记录]
文献类型	期刊论文
条目标识符	http://dspace.imech.ac.cn/handle/311007/33545
专题	高温气体动力学国家重点实验室
通讯作者	Yang GW
推荐引用方式 GB/T 7714	Yang GW,Chen DW,Cui K,et al. Response Surface Technique for Static Aeroelastic Optimization on a High-Aspect-Ratio Wing[J]. Journal of Aircraft,2009,46,4,:1444-1450.
APA	杨国伟,陈大伟,崔凯,&Yang GW.(2009).Response Surface Technique for Static Aeroelastic Optimization on a High-Aspect-Ratio Wing.Journal of Aircraft,46(4),1444-1450.
MLA	杨国伟,et al."Response Surface Technique for Static Aeroelastic Optimization on a High-Aspect-Ratio Wing".Journal of Aircraft 46.4(2009):1444-1450.