Development and Validation of a Numerical Tool for the Aeromechanical Design of Turbomachinery

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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Bibliographic Details
Main Author: Mayorca, María Angélica
Format: Others
Language:English
Published: KTH, Kraft- och värmeteknologi 2010
Subjects:
aeromechanical design
turbomachinery
numerical tool
reduced order modeling
mistuning
ROM
aero-structure coupling
CFD
FEM
methods
Mechanical energy engineering
Mekanisk energiteknik
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

Internet

http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-11992
http://nbn-resolving.de/urn:isbn:978-91-7415-561-7

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