A configuration for an aircraft so as to be spin resistant, said aircraft comprising a fuselage and a wing wherein the wing includes a first region adjacent to the fuselage and a second region adjacent to a wing tip, the first region being contiguous with the second region, and wherein at high angles of attack a stall cell is constrained to remain within the first region so as to remain apart from flight controls within the second region.


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    Titel :

    Spin Resistant Aircraft Configuration


    Beteiligte:
    KARKOW JON (Autor:in) / GIONTA MATTHEW (Autor:in) / LEDNICER DAVID (Autor:in) / KOEHLER DIETER (Autor:in) / RONCZ JOHN (Autor:in)

    Erscheinungsdatum :

    05.04.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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