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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    Title :

    Spin Resistant Aircraft Configuration


    Contributors:
    KARKOW JON (author) / GIONTA MATTHEW (author) / LEDNICER DAVID (author) / KOEHLER DIETER (author) / RONCZ JOHN (author)

    Publication date :

    2018-04-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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