The invention provides an aerodynamic layout of a drone aircraft and belongs to the field of aerodynamic layout design technology of air vehicles. The aerodynamic layout is provided with a front edge strip used for high-attack angle flying and two steering-free air inlets, an aircraft body for optimizing the aerodynamic characteristics, a low-aspect ratio wing with a thin win and a cambered face, horizontal tail ands and a vertical tail. Thus, maneuvering characteristics and high angle of attack flying ability of the drone aircraft are greatly improved.


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    Title :

    Aerodynamic layout of drone aircraft


    Contributors:
    ZHANG HONG (author) / YANG BO (author) / YU YUHUA (author) / LI TAIAN (author) / FU SONGHAI (author) / YANG XIUMAO (author) / JIANG YA NAN (author) / LU SEN (author) / HE MINGQING (author) / XIN RONGTI (author)

    Publication date :

    2015-09-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F41J TARGETS , Ziele / B64C AEROPLANES , Flugzeuge



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