Article ID Journal Published Year Pages File Type
755642 Chinese Journal of Aeronautics 2006 4 Pages PDF
Abstract

An efficient multi-harmonic method is proposed for studying the effects of mistiming on resonant features of bladed disks with blade-to-blade dry friction damping. This method is able to predict accurately the forced response of bladed disks in frequency domain, which is validated by numerical integration method in time domain. The resonant features of both tuned and mistuned systems are investigated by using this method under various system coupling strengths, viscous dampings, and dry friction dampings, etc. The results demonstrate that the proposed multi-harmonic method is very efficient for studying the mistuning effects on the resonant response of bladed disks with blade-to-blade dry friction damping, especially considering the combined effects of various system parameters.

Related Topics
Physical Sciences and Engineering Engineering Aerospace Engineering