Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Mach Number Effect on Flowfield Over a Delta Wing in Supersonic Region


    Contributors:
    Oyama, Akira (author) / Ito, Masato (author) / Imai, Genta (author) / Tsutsumi, Seiji (author) / Amitani, Nobuo (author) / Fujii, Kozo (author)

    Conference:

    46th AIAA Aerospace Sciences Meeting and Exhibit



    Publication date :

    2008-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Mach Number Effect on Flowfield Over a Delta Wing in Supersonic Region

    Oyama, A. / Ito, M. / Imai, G. et al. | British Library Conference Proceedings | 2008


    Flowfield Study over a Bulbous Payload Shroud in Transonic and Low Supersonic Mach Number

    Mehta, R. / AIAA | British Library Conference Proceedings | 1997



    Vortex Interaction of a Delta-Wing Flowfield

    C. Shih / Z. Ding | AIAA | 2003