An airfoil configured for low speed performance in an unmanned aerial vehicle includes an upper surface having an upper surface portion with a top local surface angle magnitude of less than 5 degrees at a subsection of a chord and a lower surface having a lower surface portion with a bottom local surface angle magnitude of less than 5 degrees at the subsection of the chord. The chord is defined by a line starting at a leading edge of the airfoil and extending to a trailing edge of the airfoil.


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    Title :

    Low speed airfoil design for aerodynamic improved performance of UAVs


    Contributors:

    Publication date :

    2018-01-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    LOW SPEED AIRFOIL DESIGN FOR AERODYNAMIC IMPROVED PERFORMANCE OF UAVS

    HOPPING BRADLEY M / GARRETT TIMOTHY M | European Patent Office | 2020

    Free access

    LOW SPEED AIRFOIL DESIGN FOR AERODYNAMIC IMPROVED PERFORMANCE OF UAVS

    HOPPING BRADLEY M / GARRETT TIMOTHY M | European Patent Office | 2020

    Free access

    Low Speed Airfoil Design for Aerodynamic Improved Performance of UAVs

    HOPPING BRADLEY M / GARRETT TIMOTHY M | European Patent Office | 2017

    Free access