Improved supersonic laminar flow wing structure, on a supersonic aircraft, having strake extending forwardly of the wing inboard extent, and reversed fillet at strake junction with the wing leading edge. Plain and split flap structures may also be provided at each laminar flow wing.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Highly efficient supersonic laminar flow wing structure


    Beteiligte:
    CHASE JAMES D (Autor:in) / HENDERSON MICHAEL (Autor:in) / PETER STURDZA (Autor:in)

    Erscheinungsdatum :

    2016-01-12


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge




    Natural laminar flow wing concept for supersonic transports

    Gibson, Berry T. / Gerhardt, Heinz A. | AIAA | 1995



    Stability Characteristics of Supersonic Natural Laminar Flow Wing Design Concept

    Ide, Y. / Yoshida, K. / Ueda, Y. et al. | British Library Conference Proceedings | 2012


    LAMINAR FLOW WING OPTIMIZED FOR TRANSONIC AND SUPERSONIC CRUISE AIRCRAFT

    TRACY RICHARD R / CHASE JAMES D | Europäisches Patentamt | 2021

    Freier Zugriff