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International Journal of Aerospace Engineering
Volume 2017 (2017), Article ID 1592527, 12 pages
https://doi.org/10.1155/2017/1592527
Research Article

Efficient Method for Aeroelastic Tailoring of Composite Wing to Minimize Gust Response

1School of Mechatronical Engineering, Beijing Institute of Technology, Beijing 100081, China
2Aerospace Engineering, Cranfield University, Cranfield MK43 0BL, UK

Correspondence should be addressed to Yang Yu; moc.liamg@2102tib.uygnay

Received 14 November 2016; Accepted 28 December 2016; Published 26 January 2017

Academic Editor: Marine Mikilyan

Copyright © 2017 Yang Yu et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

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