Abstract
A study of mode localization in mistuned bladed disks is performed using transfer matrices. The transfer matrix approach yields the free response of a general, mono-coupled, perfectly cyclic assembly in closed form. A mistuned structure is represented by random transfer matrices, and the expansion of these matrices in terms of the small mistuning parameter leads to the definition of a measure of sensitivity to mistuning. An approximation of the localization factor, the spatially averaged rate of exponential attenuation per blade-disk sector, is obtained through perturbation techniques in the limits of high and low sensitivity.
| Original language | English |
|---|---|
| Journal | American Society of Mechanical Engineers (Paper) |
| State | Published - 1993 |
| Event | International Gas Turbine and Aeroengine Congress and Exposition - Cincinnati, OH, USA Duration: 24 May 1993 → 27 May 1993 |
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