Abstract
This paper deals with the development of a procedure to model geometric variations of blades. Specifically, vibratory parameters of blades are extracted from CMM data on an integrally bladed rotor (IBR). The method is based on proper orthogonal decomposition (POD) of CMM data, solid modeling and finite element techniques. In addition to obtaining natural frequencies and mode shapes of each blade on an IBR, statistics of these modal parameters are also computed and characterized. Numerical results are validated by comparison with experimental results.
Original language | English (US) |
---|---|
Pages | 523-531 |
Number of pages | 9 |
DOIs | |
State | Published - 2005 |
Event | ASME Turbo Expo 2005 - Gas Turbie Technology: Focus for the Future - Reno-Tahoe, NV, United States Duration: Jun 6 2005 → Jun 9 2005 |
Other
Other | ASME Turbo Expo 2005 - Gas Turbie Technology: Focus for the Future |
---|---|
Country/Territory | United States |
City | Reno-Tahoe, NV |
Period | 6/6/05 → 6/9/05 |
All Science Journal Classification (ASJC) codes
- General Engineering