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Shock and Vibration
Volume 18 (2011), Issue 5, Pages 727-745
http://dx.doi.org/10.3233/SAV-2010-0594

Identification of Flap Motion Parameters for Vibration Reduction in Helicopter Rotors with Multiple Active Trailing Edge Flaps

Uğbreve;ur Dalli1 and Şcedilefaatdin Yüksel2

1ASELSAN Inc., MGEO Division, 06511 Akyurt, Ankara, Turkey
2Department of Mechanical Engineering, Faculty of Engineering and Architecture, Gazi University, 06570 Maltepe, Ankara, Turkey

Received 1 October 2009; Revised 21 April 2010

Copyright © 2011 Hindawi Publishing Corporation. 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

Uğbreve;ur Dalli and Şcedilefaatdin Yüksel, “Identification of Flap Motion Parameters for Vibration Reduction in Helicopter Rotors with Multiple Active Trailing Edge Flaps,” Shock and Vibration, vol. 18, no. 5, pp. 727-745, 2011. doi:10.3233/SAV-2010-0594