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Shock and Vibration
Volume 2016 (2016), Article ID 5090719, 17 pages
http://dx.doi.org/10.1155/2016/5090719
Research Article

Geometrically Nonlinear Aeroelastic Stability Analysis and Wind Tunnel Test Validation of a Very Flexible Wing

1School of Aeronautics Science and Engineering, Beihang University, Beijing, China
2Department of Aerospace Engineering, University of Bristol, Bristol, UK

Received 21 December 2015; Revised 22 March 2016; Accepted 3 April 2016

Academic Editor: Samuel da Silva

Copyright © 2016 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.

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