Abstract
FMM is a reduced order model for efficiently calculating the forced response of a mistuned bladed disk. FMM ID is a companion program that determines the mistuning in a particular rotor. Together, these methods provide a way to acquire data on the mistuning in a population of bladed disks and then simulate the forced response of the fleet. This process is tested experimentally, and the simulated results are compared with laboratory measurements of a "fleet" of test rotors. The method is shown to work quite well. It is found that accuracy of the results depends on two factors: the quality of the statistical model used to characterize mistuning, and the sensitivity of the system to errors in the statistical modeling.
| Original language | English |
|---|---|
| Pages | 373-380 |
| Number of pages | 8 |
| DOIs | |
| State | Published - 2005 |
| Externally published | Yes |
| Event | ASME Turbo Expo 2005 - Gas Turbie Technology: Focus for the Future - Reno-Tahoe, NV, United States Duration: 6 Jun 2005 → 9 Jun 2005 |
Conference
| Conference | ASME Turbo Expo 2005 - Gas Turbie Technology: Focus for the Future |
|---|---|
| Country/Territory | United States |
| City | Reno-Tahoe, NV |
| Period | 6/06/05 → 9/06/05 |
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