Stall flutter prediction techniques for fan and compressor blades
Author:
Affiliation:
1. University of California, Davis, Davis, California 95616
2. Pratt and Whitney, United Technologies, West Palm Beach, Florida 33477
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.24104
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1. Fluctuating lift and moment coefficients for cascaded airfoils in a nonuniform compressible flow.
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