In one embodiment, a wing includes a low pressure side, a high pressure side opposite the low pressure side, and a drag reducing apparatus coupled to the low pressure using an adhesive. The drag reducing apparatus includes a first side coupled to the low pressure side of the wing, and a second side opposite the first side, the second side comprising a plurality of vortex generators arranged in an array configuration, the array configuration of vortex generators operable to weaken a wingtip vortex generated by the wing by generating one or more vane vortices near an end of the low pressure side of the wing.


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    Titel :

    ADHESIVE PANELS OF MICROVANE ARRAYS FOR REDUCING EFFECTS OF WINGTIP VORTICES


    Weitere Titelangaben:

    KLEBEPLATTEN AUS MIKROSCHAUFELGRUPPEN ZUR VERMINDERUNG DER EFFEKTE VON FLÜGELSPITZENWIRBELN
    PANNEAUX ADHÉSIFS DE RÉSEAUX DE MICROVANNE DESTINÉS À RÉDUIRE LES EFFETS DES TOURBILLONS DE BOUT D'AILE


    Beteiligte:

    Erscheinungsdatum :

    2024-03-27


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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