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
Reference31 articles.
1. Fluctuating lift and moment coefficients for cascaded airfoils in a nonuniform compressible flow.
2. Further Developments in the Aerodynamic Analysis of Unsteady Supersonic Cascades—Part 1: The Unsteady Pressure Field
3. Unsteady Lifting Surface Theory for a Rotating Cascade of Swept Blades
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