Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Supersonic turbulent flow past a swept compression corner at Mach 3.II


    Contributors:

    Conference:

    26th Aerospace Sciences Meeting ; 1988 ; Reno , NV , U.S.A.



    Publication date :

    1988-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Supersonic turbulent flow past a 3-D swept compression corner at Mach 3

    KNIGHT, DOYLE / HORSTMAN, C. / RUDERICH, R. et al. | AIAA | 1987


    Structure of supersonic turbulent flow past a swept compression corner

    KNIGHT, DOYLE D. / HORSTMAN, C. C. / BOGDONOFF, SEYMOUR | AIAA | 1992


    Structure of supersonic turbulent flow past a swept compression corner

    Knight, Doyle D. / Horstman, C. C. / Bogdonoff, Seymour | NTRS | 1992