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	Investigation of winglet on the transonic flutter characteristics for a wind tunnel test model CHNT-1
	Binbin Lv; Zhiliang Lu; Tongqing Guo; Di Tang; Li Yu; Hongtao Guo
刊名	Aerospace Science and Technology
	2019
关键词	Winglet effect Transonic flutter Wind tunnel test Critical dynamic pressure Linear fitting
ISSN号	1270-9638
URL标识	查看原文
公开日期	[db:dc_date_available]
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/4605546
专题	湖南大学
作者单位	1.c High Speed Aerodynamic Institute, China Aerodynamics Research and Development Center, Mianyang 621000, China 2.College of Mechanical Engineering, Zhejiang University of Technology, Hangzhou 310014, China a College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
推荐引用方式 GB/T 7714	Binbin Lv,Zhiliang Lu,Tongqing Guo,et al. Investigation of winglet on the transonic flutter characteristics for a wind tunnel test model CHNT-1[J]. Aerospace Science and Technology,2019.
APA	Binbin Lv,Zhiliang Lu,Tongqing Guo,Di Tang,Li Yu,&Hongtao Guo.(2019).Investigation of winglet on the transonic flutter characteristics for a wind tunnel test model CHNT-1.Aerospace Science and Technology.
MLA	Binbin Lv,et al."Investigation of winglet on the transonic flutter characteristics for a wind tunnel test model CHNT-1".Aerospace Science and Technology (2019).

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