Numerical Investigation of Aerodynamic Blade Excitation Mechanisms in Transonic Turbine Stages
With the present drive in turbomachine engine developmenttowards thinner and lighter bladings, closer spaced blade rowsand higher aerodynamic loads per blade row and blade, advanceddesign criteria and accurate prediction methods for vibrationalproblems such as forced response become increasingly imp...
| Main Author: | |
|---|---|
| Format: | Doctoral Thesis |
| Language: | English |
| Published: |
KTH, Energiteknik
2002
|
| Subjects: | |
| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-3417 http://nbn-resolving.de/urn:isbn:91-7283-354-8 |