This paper presents a numerical study of the Benchmark Supercritical Wing at flutter condition, which was performed as a part of the AIAA Aeroelastic Prediction Workshop II. The primary purpose is the evaluation of the time-synchronization effect on the convergence of the coupled computational fluid dynamics/computational structural mechanics process. The proposed methodology was then used to predict the flutter boundary for the range of Mach numbers.


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    Titel :

    Computational Fluid Dynamics Study of Benchmark Supercritical Wing at Flutter Condition


    Beteiligte:
    Jirásek, Adam (Autor:in) / Dalenbring, Mats (Autor:in) / Navrátil, Jan (Autor:in)

    Erschienen in:

    AIAA Journal ; 55 , 1 ; 153-160


    Erscheinungsdatum :

    2016-08-30


    Format / Umfang :

    8 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch






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