Aeroelastic Model for Macrofiber Composite Actuators on Micro Air Vehicles-Reference-Cited by-同舟云学术

Aeroelastic Model for Macrofiber Composite Actuators on Micro Air Vehicles

Published:2017-01 Issue:1 Volume:54 Page:199-208
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

LaCroix Bradley W.¹,Ifju Peter G.¹

Affiliation:

1. University of Florida, Gainesville, Florida 32611

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C032919

Reference17 articles.

1. HighJ.WilkieW. “Method of Fabricating NASA-Standard Macro-Fiber Composite Piezoelectric Actuators, ” NASA TM-2003-212427, 2003.

2. Investigating potential substrates to maximize out-of-plane deflection of piezoelectric macro-fiber composite actuators

3. Closed-loop vibration control experiments on a rotor with blade mounted actuation

4. Material characterization of active fiber composites for integral twist-actuated rotor blade application

5. WilkieW.BelvinW.ParkK. “Aeroelastic Analysis of Helicopter Rotor Blades Incorporating Anisotropic Piezoelectric Twist Actuation,” Proceedings of the ASME 1996 World Congress and Exposition, Adaptive Structures Symposium, Proceedings, Aerospace Division, NASA Technical Reports Server (NTRS), 1996.

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