Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    The flowfield structure of the 3-D shock wave - Boundary layer interaction generated by a 20 deg sharp fin at Mach 3


    Contributors:
    KNIGHT, D. (author) / HORSTMAN, C. (author) / BOGDONOFF, S. (author)

    Conference:

    24th Aerospace Sciences Meeting ; 1986 ; Reno , NV , U.S.A.



    Publication date :

    1986-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English