Research is being conducted on the numerical simulation of transonic flow around a low noise short takeoff and landing (STOL) experimental aircraft, Asuka. The purposes of this research are to evaluate the high speed aerodynamic characteristics of the Asuka, to evaluate the aerodynamic interference between the elements and airframe according to the parametric study, and to construct a numeric data base.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Numerical Simulation of Transonic Flow Around Asuka


    Beteiligte:
    S. Takanashi (Autor:in)

    Erscheinungsdatum :

    1987


    Format / Umfang :

    2 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    QE2, Oriana, Asuka Call at Yokohama

    British Library Online Contents | 1998



    NUMERICAL SIMULATION OF SUBSONIC AND TRANSONIC FLOW AROUND THIN SHELLS

    A. A. Dyadkin / A. Yu. Lutsenko / D. K. Nazarova | DOAJ | 2016

    Freier Zugriff

    Construction of Ice Domes at Asuka Station

    Hannuki, T. / Ishizawa, K. / Kokawa, T. et al. | British Library Conference Proceedings | 1994