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	A design method of the static aeroelastic aircraft model based on stereolithgraphy for wind tunnel test
	Wang, Chao; Zhang, Zhengyu; Yin, Guofu; Sun, Yan; Zhu, Weijun
刊名	Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
	2014
卷号	35期号:[db:dc_citation_issue]页码:1193-1199
关键词	Aeroelastic modeling Model design Stereolithgraphy Stiffness distributions Wind tunnel tests
ISSN号	1000-6893
DOI	[db:dc_identifier_doi]
URL标识	查看原文
WOS记录号	[DB:DC_IDENTIFIER_WOSID]
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/3300640
专题	西安交通大学
推荐引用方式 GB/T 7714	Wang, Chao,Zhang, Zhengyu,Yin, Guofu,et al. A design method of the static aeroelastic aircraft model based on stereolithgraphy for wind tunnel test[J]. Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,2014,35([db:dc_citation_issue]):1193-1199.
APA	Wang, Chao,Zhang, Zhengyu,Yin, Guofu,Sun, Yan,&Zhu, Weijun.(2014).A design method of the static aeroelastic aircraft model based on stereolithgraphy for wind tunnel test.Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,35([db:dc_citation_issue]),1193-1199.
MLA	Wang, Chao,et al."A design method of the static aeroelastic aircraft model based on stereolithgraphy for wind tunnel test".Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica 35.[db:dc_citation_issue](2014):1193-1199.

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