Vortex reduction apparatus for use with airfoils are disclosed. An example vortex reduction apparatus includes a housing to couple to a tip of an airfoil. The housing defines a volute fluid flow passageway between an inlet and an outlet. The volute fluid flow passageway is structured to induce a rotational fluid flow in a first rotational direction opposite a second rotational direction of a shed vortex induced at the tip of the airfoil during flight.


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    Titel :

    Vortex reduction apparatus for use with airfoils


    Beteiligte:

    Erscheinungsdatum :

    2022-07-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    VORTEX REDUCTION APPARATUS FOR USE WITH AIRFOILS

    WALLISER ERIC W | Europäisches Patentamt | 2020

    Freier Zugriff

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    Vortex Shedding from Airfoils in Reverse Flow

    Lind, Andrew H | Online Contents | 2015


    Vortex noise from nonrotating cylinders and airfoils

    SCHLINKER, R. / AMIET, R. | AIAA | 1976