A vertical-tailless aircraft includes a body, a main wing, and a negative pressure generating portion. The body extends in a direction along an aircraft axis and includes a front body and a rear body. The main wing is provided on a side surface of the body. The negative pressure generating portion is provided at the rear body and is configured to generate negative pressure on the side surface of the rear body in a case that the vertical-tailless aircraft sideslips.


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    Titel :

    VERTICAL-TAILLESS AIRCRAFT


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

    Erscheinungsdatum :

    25.02.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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