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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    Titel :

    AIRCRAFT WITH NO VERTICAL TAIL


    Weitere Titelangaben:

    FLUGZEUG OHNE VERTIKALES LEITWERK
    AÉRONEF SANS EMPANNAGE VERTICAL


    Beteiligte:
    FURUMOTO TAKUYA (Autor:in) / SONODA SEIICHI (Autor:in) / SHIBATA YOSHIYUKI (Autor:in) / ASANO HIROYOSHI (Autor:in)

    Erscheinungsdatum :

    19.07.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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