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	Design and test of a practical aircraft model for wind tunnel testing with adjustable control surfaces based on 3D printing
	Zhu, Weijun; Li, Dichen; Ren, Ke; Zhang, Zhengyu
刊名	Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
	2014
卷号	35期号:[db:dc_citation_issue]页码:400-407
关键词	3-D printing Aircraft development Computational structure dynamics Low-speed wind tunnel Metal hybrid structures Testing conditions Wind tunnel modeling Wind-tunnel testing
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/3298819
专题	西安交通大学
推荐引用方式 GB/T 7714	Zhu, Weijun,Li, Dichen,Ren, Ke,et al. Design and test of a practical aircraft model for wind tunnel testing with adjustable control surfaces based on 3D printing[J]. Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,2014,35([db:dc_citation_issue]):400-407.
APA	Zhu, Weijun,Li, Dichen,Ren, Ke,&Zhang, Zhengyu.(2014).Design and test of a practical aircraft model for wind tunnel testing with adjustable control surfaces based on 3D printing.Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,35([db:dc_citation_issue]),400-407.
MLA	Zhu, Weijun,et al."Design and test of a practical aircraft model for wind tunnel testing with adjustable control surfaces based on 3D printing".Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica 35.[db:dc_citation_issue](2014):400-407.

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