Flutter of turbofan rotors with mistuned blades
Author:
Affiliation:
1. NASA Lewis Research Center, Cleveland, Ohio
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.8827
Reference9 articles.
1. 3Kielb, R. E. "Aeroelastic Characteristics of a Mistuned Bladed-Disc Assembly," Ph.D. Dissertation,The Ohio State University, Columbus, Ohio, 1981.
2. Coupled bending-bending-torsion flutter of a mistuned cascade with nonuniform blades
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