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Shock and Vibration
Volume 2016, Article ID 5096128, 14 pages
http://dx.doi.org/10.1155/2016/5096128
Research Article

Stall Flutter Control of a Smart Blade Section Undergoing Asymmetric Limit Oscillations

1School of Hydraulic, Energy and Power Engineering, Yangzhou University, Yangzhou, Jiangsu 225127, China
2Aerospace Engineering Department, Embry-Riddle Aeronautical University, Daytona Beach, FL 32114-3900, USA
3Wind Energy Center, University of Wyoming, Laramie, WY 82072, USA

Received 14 November 2015; Revised 10 February 2016; Accepted 23 February 2016

Academic Editor: Gianluca Gatti

Copyright © 2016 Nailu Li 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

Nailu Li, Mark J. Balas, Pourya Nikoueeyan, Hua Yang, and Jonathan W. Naughton, “Stall Flutter Control of a Smart Blade Section Undergoing Asymmetric Limit Oscillations,” Shock and Vibration, vol. 2016, Article ID 5096128, 14 pages, 2016. https://doi.org/10.1155/2016/5096128.