In one embodiment, an airfoil includes a first end and a second end opposite the first end. The airfoil also includes a first side and a second side opposite the first side. The airfoil includes a continuous panel coupled to the first side of the airfoil. The continuous panel includes a first edge having a first uneven edge pattern. The first edge has at least four vertices disposed thereon. The continuous panel extends from the first end of the airfoil to a second end of the airfoil.


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    Titel :

    Panels comprising uneven edge patterns for reducing boundary layer separation


    Beteiligte:
    DOMEL NEAL DAVID (Autor:in) / BARUZZINI DAN (Autor:in) / BENNER KENT W (Autor:in) / ELY II RICHARD SCOTT (Autor:in) / MILLER DANIEL N (Autor:in)

    Erscheinungsdatum :

    2019-09-24


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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