Drag reduction systems and methods for an aircraft include a first vortex generator position on a portion of the aircraft, and a second vortex generator positioned on the portion of the aircraft. The first vortex generator is associated with the second vortex generator. The first vortex generator is asymmetrical to the second vortex generator in relation to a coupling axis in order to offset the longitudinal contribution of the vortex generator to vehicle cross-sectional area.


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    Titel :

    Drag reduction systems for aircraft


    Beteiligte:
    TILLOTSON BRIAN (Autor:in) / PFLUG WILLIAM (Autor:in)

    Erscheinungsdatum :

    2021-04-20


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    DRAG REDUCTION SYSTEMS FOR AIRCRAFT

    TILLOTSON BRIAN / PFLUG WILLIAM | Europäisches Patentamt | 2020

    Freier Zugriff

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    Aircraft Drag Reduction Technology

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