The invention relates to a wing (2, 3) with two winglets (9-12) and a respective airplane. An upstream winglet broadens a region of inclined airflow and a downstream winglet produces a thrust contribution therein.


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    Title :

    КОНСОЛЬ КРЫЛА САМОЛЕТА


    Publication date :

    2020-08-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Russian


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge