Validation of Geometric Mistuning Reduced-Order Models for Single and Dual Flow-Path Integrally Bladed Rotors
Author:
Affiliation:
1. Air Force Research Laboratory
2. Universal Technology Corporation
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-1373
Reference49 articles.
1. Dynamics of rotationally periodic structures
2. The Maximum Factor by Which Forced Vibration of Blades Can Increase Due to Mistuning
3. Analysis of the Worst Mistuning Patterns in Bladed Disk Assemblies
4. Mode localization and eigenvalue loci veering phenomena in disordered structures
5. Localization phenomena in structural dynamics
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