A flow control system includes a movable wing attachable to a wing of an aircraft, and a plasma actuator mountable on a surface of the movable wing. The flow control system is configured to control air flow around the wing by having the changing of the steering angle of the movable wing work in conjunction with the operation of the plasma actuator.


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    Titel :

    FLOW CONTROL SYSTEM, FLOW CONTROL METHOD, AND AIRCRAFT


    Beteiligte:
    KIKUCHI MAKI (Autor:in) / KATO HIROKI (Autor:in) / KONO MITSURU (Autor:in) / YOSHIDA KENTARO (Autor:in) / NAKAZATO NOBUYUKI (Autor:in)

    Erscheinungsdatum :

    2019-10-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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