Reduced-Order Modeling for Nonlinear Analysis of Cracked Mistuned Multistage Bladed-Disk Systems
Author:
Affiliation:
1. University of Michigan, Ann Arbor, Michigan 48109-2125
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J051021
Reference27 articles.
1. Song, S. H. "Vibration Analysis and System Identification of Mistuned Multistage Turbine Engine Rotors," Ph.D. Thesis,The University of Michigan, Ann Arbor, MI, 2007.
2. Modeling and Analysis of Mistuned Bladed Disk Vibration: Current Status and Emerging Directions
3. Effects of Multistage Coupling and Disk Flexibility on Mistuned Bladed Disk Dynamics
4. Multi-Stage Modeling of Turbine Engine Rotor Vibration
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