In one embodiment, a horizontal stabilizer (200) comprises an airfoil structure (210) configured to be mounted to an aircraft (100) at a horizontal orientation. The airfoil structure (210) comprises a leading edge (202), a trailing edge (204), a top surface (212), and a bottom surface (213). Moreover, the airfoil structure (210) is cambered (211), wherein a camber (211) of the airfoil structure (210) forms a concave slope on the top surface (212) and a convex slope on the bottom surface (213).


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    Title :

    AIRCRAFT HORIZONTAL STABILIZER DESIGN


    Additional title:

    KONSTRUKTION HORIZONTALER FLUGZEUGSTABILISATOREN
    CONCEPTION DE STABILISATEUR HORIZONTAL D'AÉRONEF


    Contributors:

    Publication date :

    2019-06-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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