Active Control and Closed-Loop Identification of Flutter Instability in Typical Section Airfoil-Reference-Cited by-同舟云学术

Active Control and Closed-Loop Identification of Flutter Instability in Typical Section Airfoil

Published:2007-05 Issue:3 Volume:30 Page:733-740
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

McEver Mark A.¹,Ardelean Emil V.²,Cole Daniel G.³,Clark Robert L.⁴

Affiliation:

1. L-3 Communications Corporation, Pittsburgh, Pennsylvania 15238

2. Science Applications International Corporation, Albuquerque, New Mexico 87106

3. University of Pittsburgh, Pittsburgh, Pennsylvania 15237

4. Duke University, Durham, North Carolina 27708

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.26335

Reference18 articles.

1. Noll, T. E., Structural Dynamics and Aeroelasticity, Vol.5, Flight-Vehicle Materials,Structures, and Dynamics-Assessment and Future Directions, ASME,New York, 1993, pp.179-212.

2. Summary of an Active Flexible Wing program

3. Experimental Active Control of a Typical Section Using a Trailing-Edge Flap

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