The invention discloses an embedded control surface applied to flying wing configuration course control. The backward sweep range of the embedded control surface is 40-70 degrees. When the control surface is operated, the magnitudes of lateral force and resistance on the control surface are equivalent, so yawing moment with equivalent magnitude and same direction can be produced, and course control of the flying wing configuration can be realized. Compared with the conventional embedded surface, the embedded control surface has the advantage that the resistance magnitude of the full machine is dramatically reduced during course control.


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    Titel :

    Embedded control surface for flying wing configuration course control


    Beteiligte:
    HUANG YONG (Autor:in) / MA XIAOYONG (Autor:in) / WANG YIQING (Autor:in) / SHAN JIXIANG (Autor:in) / ZHONG SHIDONG (Autor:in) / SU JICHUAN (Autor:in) / LI YONGHONG (Autor:in) / PENG XIN (Autor:in)

    Erscheinungsdatum :

    2015-06-10


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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