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    Title :

    PROGRESS ON GUST LOAD ALLEVIATION WIND TUNNEL EXPERIMENT AND AEROSERVOELASTIC MODEL VALIDATION FOR A FLEXIBLE WING WITH VARIABLE CAMBER CONTINUOUS TRAILING EDGE FLAP SYSTEM


    Contributors:

    Conference:

    AIAA SciTech Forum and Exposition ; 2020 ; Orlando, Fla.



    Publication date :

    2020


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English