A vortex generator may include a depression in an aerodynamic surface, and a vortex generator leading edge located in the depression. The vortex generator leading edge may include a leading edge upper surface. The leading edge upper surface may be positioned at or below a tangent line defined at a location along the aerodynamic surface upstream of the depression relative to an oncoming local flow.


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    Titel :

    SUBMERGED VORTEX GENERATOR


    Beteiligte:
    HARRISON NEAL A (Autor:in) / DEHAAN MARK (Autor:in) / VASSBERG JOHN C (Autor:in) / SCLAFANI ANTHONY J (Autor:in)

    Erscheinungsdatum :

    2016-02-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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