A vertical-tailless aircraft (10) includes: a body (20) extending in a direction along an aircraft axis; a main wing (30) provided on a side surface (55) of the body (20); and a negative pressure generating portion (40) configured to generate negative pressure on the side surface (55) of a rear portion of the body (20) when the vertical-tailless aircraft (10) sideslips.


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    Title :

    AIRCRAFT WITH NO VERTICAL TAIL


    Additional title:

    FLUGZEUG OHNE VERTIKALES LEITWERK
    AÉRONEF SANS EMPANNAGE VERTICAL


    Contributors:

    Publication date :

    2023-07-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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