Show simple item record

contributor authorFiquet, Anne-Lise
contributor authorOttavy, Xavier
contributor authorBrandstetter, Christoph
date accessioned2024-12-24T18:45:22Z
date available2024-12-24T18:45:22Z
date copyright3/18/2024 12:00:00 AM
date issued2024
identifier issn0889-504X
identifier otherturbo_146_7_071003.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4302687
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.
publisherThe American Society of Mechanical Engineers (ASME)
titleUHBR Open-Test Case Fan ECL5/CATANA: Non-Linear Analysis of Non-Synchronous Blade Vibration at Part-Speed Conditions
typeJournal Paper
journal volume146
journal issue7
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4064841
journal fristpage71003-1
journal lastpage71003-8
page8
treeJournal of Turbomachinery:;2024:;volume( 146 ):;issue: 007
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record