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dc.contributor.authorFiquet, Anne-Lise
dc.contributor.authorOttavy, Xavier
dc.contributor.authorBrandstetter, Christoph
dc.date.accessioned2024-12-24T18:45:22Z
dc.date.available2024-12-24T18:45:22Z
dc.date.copyright3/18/2024 12:00:00 AM
dc.date.issued2024
dc.identifier.issn0889-504X
dc.identifier.otherturbo_146_7_071003.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4302687
dc.description.abstractThe onset of non-synchronous vibrations has been predicted for a composite open-test-case UHBR fan geometry by time-linearized simulations at part-speed conditions. In the current study, time-accurate simulations with harmonic blade oscillations have been conducted to investigate the non-linear behavior. Results for different operating conditions show the evolution of aeroelastic stability. The lock-in of convected aerodynamic disturbances with structural vibration is analyzed for different vibration amplitudes and frequencies. The simulations show the development of multiple wave numbers, mode scattering, and a non-linear dependency on vibration amplitude. The results indicate the possibility of limit-cycle prediction and the necessity of strongly coupled methods for the assessment of non-synchronous vibration.
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titleUHBR Open-Test Case Fan ECL5/CATANA: Non-Linear Analysis of Non-Synchronous Blade Vibration at Part-Speed Conditions
dc.typeJournal Paper
dc.journal.volume146
dc.journal.issue7
dc.journal.titleJournal of Turbomachinery
dc.identifier.doi10.1115/1.4064841
dc.journal.fristpage71003-1
dc.journal.lastpage71003-8
dc.page8
dc.treeJournal of Turbomachinery:;2024:;volume( 146 ):;issue: 007
dc.contenttypeFulltext


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