Flutter suppression for the active flexible wing - A classical design-Reference-Cited by-同舟云学术

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Flutter suppression for the active flexible wing - A classical design

Published:1995-01 Issue:1 Volume:32 Page:61-67
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Waszak M. R.¹,Srinathkumar S.²

Affiliation:

1. NASA Langley Research Center, Hampton, Virginia 23665

2. National Aeronautical Laboratory, Bangalore 560017, India

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.46684

Reference28 articles.

1. 'Miller, G. D. "Active Flexible Wing (AFW) Technology,11Air Force Wright Aeronautical Labs., AFWAL-TR-87-3096, Feb. 1988.

2. 2Perry, B., Cole, S. R., and Miller, G. D. "A Summary of the Active Flexible Wing Program,'1AIAA Paper 92-2080, April 1992.

3. Triplett, W. E., Kappus, H. F., and Landy, R. J. "Active Flutter Control,11AIAA Paper 73-194, Jan. 1973.

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