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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    Titel :

    Aerodynamic layout of drone aircraft


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

    Erscheinungsdatum :

    2015-09-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F41J TARGETS , Ziele / B64C AEROPLANES , Flugzeuge



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