Abstract
The method of polynomial chaos has been used to analytically compute the statistics of forced response of a mistuned bladed disk assembly. The model of the bladed disk assembly considers only one mode of vibration of each blade. Mistuning phenomenon has been simulated by treating the modal stiffness of each blade as a random variable. The validity of the polynomial chaos method has been corroborated by comparison with the results from numerical simulations.
Original language | English (US) |
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Pages | 287-297 |
Number of pages | 11 |
DOIs | |
State | Published - 2003 |
Event | 2003 ASME Turbo Expo - Atlanta, GA, United States Duration: Jun 16 2003 → Jun 19 2003 |
Other
Other | 2003 ASME Turbo Expo |
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Country/Territory | United States |
City | Atlanta, GA |
Period | 6/16/03 → 6/19/03 |
All Science Journal Classification (ASJC) codes
- Engineering(all)