Flutter Suppression Using V-Stack Piezoelectric Actuator-Reference-Cited by-同舟云学术

Flutter Suppression Using V-Stack Piezoelectric Actuator

Published:2003-04-07 Issue: Volume: Page:
ISSN:
Container-title:44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
language:
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Author:

Ardelean Emil,McEver Mark,Cole D.,Clark Robert

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-1796

Reference9 articles.

1. Prechtl, E. F. and Hall, S. R. “An X-Frame Sctuator Servo-Flap Actuation System for Rotor Control,”Proceedings of SPIEVol.3329, pp309-320, San Diego, CA, March 1998.

2. Hall, S. R. andPrechtl, E. F. “Preliminary Testing of a Mach-Scaled Active Rotor Blade with a Trailing Edge Servo-Flap,” SPIE Smart Structures and Materials Symposium, NewportBeach, CA, March 1999.

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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