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Shock and Vibration
Volume 2017, Article ID 2564314, 16 pages
https://doi.org/10.1155/2017/2564314
Research Article

Aeroelastic Optimization Design for High-Aspect-Ratio Wings with Large Deformation

1School of Aeronautic Science and Engineering, Beihang University, Beijing, China
2Chengdu Aircraft Design & Research Institute, Chengdu, China

Correspondence should be addressed to Yang Meng; nc.ude.aaub@ymmus

Received 17 May 2017; Revised 11 September 2017; Accepted 17 September 2017; Published 23 October 2017

Academic Editor: Enrico Zappino

Copyright © 2017 Changchuan Xie 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.

How to Cite this Article

Changchuan Xie, Yang Meng, Fei Wang, and Zhiqiang Wan, “Aeroelastic Optimization Design for High-Aspect-Ratio Wings with Large Deformation,” Shock and Vibration, vol. 2017, Article ID 2564314, 16 pages, 2017. https://doi.org/10.1155/2017/2564314.