Development and Validation of a Numerical Tool for the Aeromechanical Design of Turbomachinery
In aeromechanical design one of the major rules is to operate under High Cyclic Fatigue (HCF) margins and away from flutter. The level of dynamic excitations and risk of HCF can be estimated by performing forced response analyses from blade row interaction forces or Low Engine Order (LEO) excitation...
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| Format: | Others |
| Language: | English |
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KTH, Kraft- och värmeteknologi
2010
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-11992 http://nbn-resolving.de/urn:isbn:978-91-7415-561-7 |