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    UHBR Open-Test Case Fan ECL5/CATANA: Non-Linear Analysis of Non-Synchronous Blade Vibration at Part-Speed Conditions

    Source: Journal of Turbomachinery:;2024:;volume( 146 ):;issue: 007::page 71003-1
    Author:
    Fiquet, Anne-Lise
    ,
    Ottavy, Xavier
    ,
    Brandstetter, Christoph
    DOI: 10.1115/1.4064841
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The 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.
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      UHBR Open-Test Case Fan ECL5/CATANA: Non-Linear Analysis of Non-Synchronous Blade Vibration at Part-Speed Conditions

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4302687
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    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
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