A recent consideration in aircraft design is the use of folding wingtips, with the aim of enabling higher-aspect-ratio aircraft with less induced drag but also meeting airport gate limitations. This study investigates the impact of floating folding wingtips on the aircraft flight dynamics. It is found that a floating wingtip aircraft has similar handling qualities with respect to an aircraft with no wing extension.


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    Titel :

    Aeroelastics Flight Dynamics Coupling Effects of the Semi-Aeroelastic Hinge Device


    Beteiligte:
    Castrichini, A. (Autor:in) / Wilson, T. (Autor:in) / Saltari, F. (Autor:in) / Mastroddi, F. (Autor:in) / Viceconti, N. (Autor:in) / Cooper, J. E. (Autor:in)

    Erschienen in:

    Journal of Aircraft ; 57 , 2 ; 333-341


    Erscheinungsdatum :

    2019-11-27


    Format / Umfang :

    9 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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