Investigation of the combined effects of intentional and random mistuning on the forced response of bladed disks
Author:
Affiliation:
1. Michigan, Univ., Ann Arbor
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-3720
Reference17 articles.
1. Effect of Mistuning on the Vibration of Turbo-Machine Blades Induced by Wakes
2. Vibration Amplitudes of Compressor Blades Resulting From Scatter in Blade Natural Frequencies
3. The Maximum Factor by Which Forced Vibration of Blades Can Increase Due to Mistuning
4. The effects of detuning upon the forced vibrations of bladed disks
5. Maximum Resonant Response of Mistuned Bladed Disks
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2. The Performance of Friction Dampers on the Intentionally Mistuned Bladed Disk Assembly Subjected to Narrow Band Random Excitation;Transactions of the Korean Society for Noise and Vibration Engineering;2023-06-20
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4. Nonlinear stochastic dynamics of detuned bladed-disks with uncertain mistuning and detuning optimization using a probabilistic machine learning tool;International Journal of Non-Linear Mechanics;2022-07
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