Provided is a nose for a supersonic flying object, which has a natural laminar flow nose shape capable of suppressing laminar-turbulent transition and drastically reducing a frictional drag. The nose for a supersonic flying object has a low resistive body shape symmetrical about a central axis as a base shape, wherein the base shape is approximately a cone shape having a linear, simple convex curve, or simple concave curve generatrix and a deformation element having a wavy shape is added to the base shape.


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    Titel :

    Nose for supersonic flying object


    Beteiligte:
    TOKUGAWA NAOKO (Autor:in) / KAWAI TARO (Autor:in) / TOZUKA AYAKO (Autor:in) / UEDA YOSHINE (Autor:in) / ISHIKAWA HIROAKI (Autor:in)

    Erscheinungsdatum :

    2016-08-30


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F42B EXPLOSIVE CHARGES, e.g. FOR BLASTING , Explosive Ladungen, z.B. für Sprengungen



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