Initial Results of an Experimental Study of Oscillating Fence Actuators on a Stationary and Pitch Oscillating Wing-Reference-Cited by-同舟云学术

Initial Results of an Experimental Study of Oscillating Fence Actuators on a Stationary and Pitch Oscillating Wing

Published:2007-01-08 Issue: Volume: Page:
ISSN:
Container-title:45th AIAA Aerospace Sciences Meeting and Exhibit
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Author:

Saini Manjinder¹,Lindberg William¹,Naughton Jonathan¹

Affiliation:

1. University of Wyoming

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-881

Reference24 articles.

1. 1Sandford, M. C., Abel, I., and Gray, D. L. “Developement and Demonstration of a Flutter-Suppression System using Active Controls,” Tech. Rep. TR-R450, NASA TR-R450, 1975.

2. Flutter suppression for the active flexible wing - A classical design

3. 3Waszak, M. R. and Srinathkumar, S. “Design and Experimental Validation of a Flutter Suppression Controller for the Active Flexible Wing,” Tech. Rep. TM-4381, NASA, 1992.

4. Review of Smart-Materials Actuation Solutions for Aeroelastic and Vibration Control

5. 5Heeg, J. “Analytical and Experimental Investigation of Flutter Suppression by Piezoelectric Actuation,” Tech. Rep. Technical Paper No. 3241, NASA, 1993.

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1. Frequency Effect on Flow Field Behind an Oscillating Fence Submerged in Turbulent Boundary Layer;48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition;2010-01-04

2. Effect of an Oscillating Fence Actuator on a Stationary and Pitch Oscillating Wing;46th AIAA Aerospace Sciences Meeting and Exhibit;2008-01-07