The self-sustaining mechanisms of shock oscillations in transonic airfoil buffet are studied by wall-resolved large-eddy simulation (LES) and resolvent analysis. The LES successfully reproduces the large-scale shock oscillations over a transonic OAT15A airfoil, and the resolvent analysis using the high-fidelity LES data reveals the input–output relations in the self-sustained shock oscillations. Based on the input–output relations revealed by the resolvent analysis, this study identifies two mechanisms of the self-sustained shock oscillations. The first mechanism is closely tied to the periodic variations of the shock-induced separation height, whereas the second mechanism is related to the pressure dynamics around the shock wave. The mechanisms of the self-sustained shock oscillations identified by the input–output relations are examined in detail along with the high-fidelity LES data to aid the understanding of the feedback formulations in transonic airfoil buffet.


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    Titel :

    Identifying the Self-Sustaining Mechanisms of Transonic Airfoil Buffet with Resolvent Analysis


    Beteiligte:
    Iwatani, Yuta (Autor:in) / Asada, Hiroyuki (Autor:in) / Yeh, Chi-An (Autor:in) / Taira, Kunihiko (Autor:in) / Kawai, Soshi (Autor:in)

    Erschienen in:

    AIAA Journal ; 61 , 6 ; 2400-2411


    Erscheinungsdatum :

    01.06.2023




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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