There is disclosed a blended wing body aircraft including a center body having a lower side and an upper side opposed to the lower side. The center body has a central chord extending from a leading edge to a trailing edge of the center body. The lower side has a lowest point located between a first location forward of a pivot point about which the aircraft rotates during take-off and a second location aft of the pivot point. The first location is at a first distance corresponding to about 10% of a length of the central chord forward of the pivot point.


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    Title :

    BLENDED WING BODY AIRCRAFT


    Additional title:

    FUSELAGE INTEGRE D`AERONEF


    Contributors:
    CHITTICK IAN (author) / RAKOWITZ MARK (author) / REIST THOMAS (author)

    Publication date :

    2019-12-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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