- 18 An airfoil active boundary layer control system. A housing includes an induction wall having a gas permeable surface, an exhaust wall having at least one exhaust port, and a chamber disposed between and at least partially defined by the induction and exhaust walls. At least one zero-net-mass-flux actuator are located in the chamber includes an actuator orifice in fluid communication with the gas permeable surface of the induction wall and the at least one exhaust port, the actuator orifice being aligned with the at least one exhaust port. 22" I- 24 Rotation 26" 10 FIG. ]A Wind 3 3842 28a 4444 40b FIG. 2 '"40a


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    Titel :

    Active Bleed For Airfoils


    Beteiligte:
    BARUZZINI DAN (Autor:in) / DOMEL NEAL DAVID (Autor:in) / HAKES JEFFREY G (Autor:in) / MILLER DANIEL N (Autor:in)

    Erscheinungsdatum :

    01.06.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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