Vibration Reduction of Mistuned Bladed Disks by Passive Piezoelectric Shunt Damping Techniques
Author:
Affiliation:
1. Laboratoire de Tribologie et Dynamique des System, École Centrale de Lyon, 69134 Écully, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052202
Reference29 articles.
1. Flutter and Resonant Vibration Characteristics of Engine Blades
2. Modeling and Analysis of Mistuned Bladed Disk Vibration: Current Status and Emerging Directions
3. Using Intentional Mistuning in the Design of Turbomachinery Rotors
4. Minimizing Blade Dynamic Response in a Bladed Disk Through Design Optimization
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