The disclosure relates to a wing 2 with at least two winglets 8,9,10 having a relative dihedral angle between them, and to an airplane 1 having such wings. An upstream winglet 8 broadens a region of inclined airflow, and a more downstream winglet 9 produces a thrust contribution therein.


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    Title :

    AIRPLANE WING


    Additional title:

    FLUGZEUGFLÜGEL
    AILE D'AVION


    Contributors:

    Publication date :

    2021-12-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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