The present disclosure directed to an aircraft comprising one or more propulsion devices, a flexible wing, at least two tail booms having a proximal end and a distal end, the tail booms being secured to said flexible wing at the proximal end, wherein the tail booms comprise of a tail section connected at the distal end of said tail boom and wherein the tail section comprises of at least one control surface.


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    Title :

    Wing-Twist Controlled Aircraft


    Contributors:
    UHLIG DANIEL (author) / KAYS CORY (author) / ULECK KEVIN (author) / CROUSE GIL (author)

    Publication date :

    2019-03-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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