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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    Title :

    Computational Fluid Dynamics Study of Benchmark Supercritical Wing at Flutter Condition


    Contributors:

    Published in:

    AIAA Journal ; 55 , 1 ; 153-160


    Publication date :

    2016-08-30


    Size :

    8 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English






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