Statistical analysis of the forced response of mistuned cyclic assemblies
Author:
Affiliation:
1. Aerostructures, Inc., Arlington, Virginia
2. University of Michigan, Ann Arbor, Michigan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.25131
Reference14 articles.
1. Vibrations of Bladed-Disk Assemblies—A Selected Survey (Survey Paper)
2. Fatigue life estimates of mistuned blades via a stochastic approach
3. Model Development and Statistical Investigation of Turbine Blade Mistuning
4. Vibration of Some Structures with Periodic Random Parameters
5. Calculating the statistics of forced response of a mistuned bladed disk assembly
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