Statistical Analysis of the Nonlinear Response of Bladed Disks with Mistuning and Cracks
Author:
Affiliation:
1. The Ohio State University, Columbus, Ohio 43210
Funder
Division of Civil, Mechanical and Manufacturing Innovation
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.J058190
Reference35 articles.
1. Compact, Generalized Component Mode Mistuning Representation for Modeling Bladed Disk Vibration
2. Vibration Amplitudes of Compressor Blades Resulting From Scatter in Blade Natural Frequencies
3. The effects of detuning upon the forced vibrations of bladed disks
4. Model Development and Statistical Investigation of Turbine Blade Mistuning
5. Localization Phenomena in Mistuned Assemblies with Cyclic Symmetry Part I: Free Vibrations
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