Durability Characterization of Active Fiber Composite Actuators for Helicopter Rotor Blade Applications
Author:
Affiliation:
1. Institute for Aerospace Research, National Research Council Canada, Ottawa, Ontario, Canada, K1G 0R6
2. Continuum Photonics, Inc., Billerica, Massachusetts 01821
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.988
Reference23 articles.
1. Closed-loop vibration control experiments on a rotor with blade mounted actuation
2. Development of a piezoelectric actuator for trailing edge flap control of full scale rotor blades
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