Modeling and Analysis of Mistuned Bladed Disk Vibration: Current Status and Emerging Directions
Author:
Affiliation:
1. University of Michigan, Ann Arbor, Michigan 48109-2125
2. McGill University, Montreal, Quebec H3A 2K6, Canada
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/10.2514/1.16345
Reference148 articles.
1. Effect of Mistuning on the Vibration of Turbo-Machine Blades Induced by Wakes
2. Coupling of Turbomachine Blade Vibrations Through the Rotor
3. Vibration Amplitudes of Compressor Blades Resulting From Scatter in Blade Natural Frequencies
4. The effects of detuning upon the forced vibrations of bladed disks
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