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	Modal parameter identification of finishing assembly interface of vertical tail section of large aircraft based on optimized STD method
	Zhao, Xiong; Fan, Wei; Zheng, Lianyu; Liu, Xinyu; An, Zewu; Yang, Sen
刊名	Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
	2019
卷号	40
ISSN号	10006893
DOI	10.7527/S1000-6893.2019.22950
URL标识	查看原文
收录类别	EI
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/5914645
专题	北京航空航天大学
推荐引用方式 GB/T 7714	Zhao, Xiong,Fan, Wei,Zheng, Lianyu,et al. Modal parameter identification of finishing assembly interface of vertical tail section of large aircraft based on optimized STD method[J]. Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,2019,40.
APA	Zhao, Xiong,Fan, Wei,Zheng, Lianyu,Liu, Xinyu,An, Zewu,&Yang, Sen.(2019).Modal parameter identification of finishing assembly interface of vertical tail section of large aircraft based on optimized STD method.Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,40.
MLA	Zhao, Xiong,et al."Modal parameter identification of finishing assembly interface of vertical tail section of large aircraft based on optimized STD method".Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica 40(2019).

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