Abstract
The literature on reduced-order modeling, simulation, and analysis of the vibration of bladed disks found in gas-turbine engines is reviewed. Applications to system identification and design are also considered. In selectively surveying the literature, an emphasis is placed on key developments in the last decade that have enabled better prediction and understanding of the forced response of mistuned bladed disks, especially with respect to assessing and mitigating the harmful impact of mistuning on blade vibration, stress increases, and attendant high cycle fatigue. Important developments and emerging directions in this research area are highlighted.
| Original language | English |
|---|---|
| Pages (from-to) | 384-396 |
| Number of pages | 13 |
| Journal | Journal of Propulsion and Power |
| Volume | 22 |
| Issue number | 2 |
| DOIs | |
| State | Published - 2006 |
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