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International Journal of Aerospace Engineering
Volume 2015, Article ID 485964, 10 pages
http://dx.doi.org/10.1155/2015/485964
Research Article

Helicopter Vibratory Loads Alleviation through Combined Action of Trailing-Edge Flap and Variable-Stiffness Devices

Department of Engineering, Roma Tre University, Via della Vasca Navale 79, 00146 Rome, Italy

Received 12 March 2015; Accepted 21 May 2015

Academic Editor: R. Ganguli

Copyright © 2015 Massimo Gennaretti 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

Massimo Gennaretti, Giovanni Bernardini, Jacopo Serafini, and Marco Molica Colella, “Helicopter Vibratory Loads Alleviation through Combined Action of Trailing-Edge Flap and Variable-Stiffness Devices,” International Journal of Aerospace Engineering, vol. 2015, Article ID 485964, 10 pages, 2015. https://doi.org/10.1155/2015/485964.