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    Title :

    AIAA-2019-3591: Study on Wing Rock Phenomenon of a Fighter Aircraft Using Free-To-Roll Wind Tunnel Test and Dynamic CFD Method


    Contributors:

    Conference:

    Applied aerodynamics ; 2019 ; Dallas, TX



    Publication date :

    2019-01-01


    Size :

    13 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Nr. 3591

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