Effect of an Oscillating Fence Actuator on a Stationary and Pitch Oscillating Wing-Reference-Cited by-同舟云学术

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Effect of an Oscillating Fence Actuator on a Stationary and Pitch Oscillating Wing

Published:2008-01-07 Issue: Volume: Page:
ISSN:
Container-title:46th AIAA Aerospace Sciences Meeting and Exhibit
language:
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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/10.2514/6.2008-280

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.

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Surface pressure and flow field behind an oscillating fence submerged in turbulent boundary layer;Experiments in Fluids;2010-09-24

2. 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

3. Surface Pressure and Flow Field Behind an Oscillating Fence Submerged in Turbulent Boundary Layer;4th Flow Control Conference;2008-06-15

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