A method for active flow control of a fluid flow that flows along a flow surface includes generating a first local velocity field in the fluid flow by introducing a first vortex structure into the fluid flow by means of a first flow control actuator coupled to a first actuation site of the flow surface, and introducing a second vortex structure into the first local velocity field by means of a second flow control actuator coupled to a second actuation site of the flow surface located downstream of the first actuation site, when a head vortex of the first vortex structure has propagated with the fluid flow downstream the second actuation site.


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    Title :

    METHOD FOR ACTIVE FLOW CONTROL, FLOW BODY, AND AIRCRAFT


    Additional title:

    VERFAHREN ZUR AKTIVEN STRÖMUNGSSTEUERUNG, STRÖMUNGSKÖRPER SOWIE FLUGZEUG
    PROCÉDÉ DE RÉGULATION ACTIVE DE FLUX, CORPS DE FLUX ET AÉRONEF


    Contributors:

    Publication date :

    2023-07-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F15D FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS , Strömungsdynamik, d.h. Verfahren oder Vorrichtungen zum Beeinflussen der Strömung von Gasen oder Flüssigkeiten / B64C AEROPLANES , Flugzeuge



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