Structural Damping Identification for Mistuned Bladed Disks and Blisks
Author:
Affiliation:
1. Department of Mechanical Engineering, University of Michigan, Ann Arbor, MI 48109
2. Aeromechanics Technology, GE Aviation, Cincinnati, OH 45245 e-mail:
Abstract
Publisher
ASME International
Subject
General Engineering
Link
http://asmedigitalcollection.asme.org/vibrationacoustics/article-pdf/doi/10.1115/1.4005009/5739333/024504_1.pdf
Reference28 articles.
1. Estimation of Mass, Stiffness and Damping Matrices From Frequency Response Functions;Chen;J. Vib. Acoust.
2. Experimental Identification of Generalized Propotional Viscous Damping Matrix;Adhikari;J. Vib. Acoust.
3. A System Matrices Reduction Method for Damped Systems;Chen;JSME Int. J. Ser. C
4. Structural Parameters Identification Using Improved Normal Frequency Response Function Method;Kim;Mech. Syst. Signal Process.
5. Expressions for Damping Matrices in Linear Vibration Problems;Lancaster;J. Aerosp. Sci.
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1. An Optimization Method for Stiffness and Damping Mistuning Identification From Blade Tip Timing Data;Journal of Engineering for Gas Turbines and Power;2024-08-23
2. A Complex Mode Superposition Method Based on Hysteretic Damping Model for Mode Static Correction;International Journal of Applied Mechanics;2023-08-30
3. Application of Improved Dynamic Substructure Finite Element Model-Based State-Space Techniques in Mistuned Blisks;International Journal of Aerospace Engineering;2020-12-16
4. A structural damping identification technique for coatings on blisks based on improved component mode mistuning model;Thin-Walled Structures;2020-06
5. Bibliography;Structural Dynamic Analysis with Generalized Damping Models;2014-01-24
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