Abstract
This paper deals with the development of an accurate reduced-order model of a bladed disk with geometric mistuning. The method is based on vibratory modes of various tuned systems and proper orthogonal decomposition of coordinate measurement machine data on blade geometries. Results for an academic rotor are presented to establish the validity of the technique.
| Original language | English (US) |
|---|---|
| Article number | 031007 |
| Journal | Journal of Turbomachinery |
| Volume | 131 |
| Issue number | 3 |
| DOIs | |
| State | Published - Jul 2009 |
All Science Journal Classification (ASJC) codes
- Mechanical Engineering