Active Flutter Control with a V-Stack Piezoelectric Flap Actuator
Author:
Affiliation:
1. Science Applications International Corporation, Albuquerque, New Mexico 87106
2. L-3 Communications Corporation, Pittsburgh, Pennsylvania 15238
3. Duke University, Durham, North Carolina 27708
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.12214
Reference23 articles.
1. Design of a high efficiency, large stroke, electromechanical actuator
2. Preliminary testing of a Mach-scaled active rotor blade with a trailing-edge servo flap
3. Actuation of Trailing Edge Flap in a Wing Model Using Piezostack Device
4. Analysis and Testing of Mach-Scaled Rotor with Trailing-Edge Flaps
5. ACTIVE WING FLUTTER SUPPRESSION USING A TRAILING EDGE FLAP
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