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

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


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    Titel :

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

    Beteiligte:
    Nguyen, Nhan T. (Autor:in) / Cramer, Nick B. (Autor:in) / Hashemi, Kelley E. (Autor:in) / Drew, Michael C. (Autor:in) / Xiong, Juntao (Autor:in) / Mundt, Tyler (Autor:in) / Mor, Marat (Autor:in) / Livne, Eli (Autor:in)
    Kongress:

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

    Erschienen in:

    Structural dynamics ; Volume 1 of 2

    Erscheinungsdatum :

    2020

    Medientyp :

    Aufsatz (Konferenz)

    Format :

    Print

    Sprache :

    Englisch

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