F100 fan stall flutter problem review and solution
Author:
Affiliation:
1. Pratt & Whitney Division, United Aircraft Corporation, West Palm Beach, Fla.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.44454
Reference6 articles.
1. 2Woods, L. C. "Aerodynamic Forces on an Oscillating Aerofoil Fitted With a Spoiler," Royal Society Proceedings,New South Wales University of Technology, Ser. A, Vol.239, 1957, pp.328-337.
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