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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    Title :

    SUBMERGED VORTEX GENERATOR


    Contributors:

    Publication date :

    2016-02-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    SUBMERGED VORTEX GENERATOR

    HARRISON NEAL A / DEHAAN MARK / VASSBERG JOHN C et al. | European Patent Office | 2017

    Free access

    Submerged vortex generator

    HARRISON NEAL A / DEHAAN MARK / VASSBERG JOHN C et al. | European Patent Office | 2016

    Free access

    SUBMERGED VORTEX GENERATOR

    HARRISON NEAL A / DEHAAN MARK / VASSBERG JOHN CHARLES et al. | European Patent Office | 2018

    Free access