Proposed is an airfoil wing-shaped aircraft including a body having a wing-shaped longitudinal cross-section and having an upper surface on which a shape of a concave curvature-surface portion is formed along a center axis in a streamwise direction, a fluid inlet being formed in each of the opposite lateral sides of a leading portion of the body, and a fluid output being formed in each of the opposite lateral sides of a tail portion of the body, wherein a duct connects the fluid inlet and the fluid outlet to each other.


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    Titel :

    Airfoil wing-shaped aircraft


    Beteiligte:
    CHO HYUNG HEE (Autor:in) / CHOI SEUNGYEONG (Autor:in) / KIM JIHYUK (Autor:in) / NAM JUYEONG (Autor:in) / YUN MAROOSOL (Autor:in) / YOON TAEDOO (Autor:in) / BANG MINHO (Autor:in) / LIM JOON-SOO (Autor:in)

    Erscheinungsdatum :

    23.07.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64U



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