Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    A study of incipient separation limits for shock-induced boundary layer separation for Mach 6 high Reynolds flow


    Contributors:
    FREW, D. (author) / GALASSI, L. (author) / STAVA, D. (author) / AZEVEDO, D. (author)

    Conference:

    29th Joint Propulsion Conference and Exhibit ; 1993 ; Monterey , CA , U.S.A.



    Publication date :

    1993-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




    Incipient Separation of a Supersonic Turbulent Boundary Layer at High Reynolds Numbers

    Gary S. Settles / Seymour M. Bogdonoff / Irwin E. Vas | AIAA | 1976


    Incipient Separation in Laminar Ramp-Induced Shock-Wave/Boundary-Layer Interactions

    Grisham, James R. / Dennis, Brian H. / Lu, Frank K. | AIAA | 2018




    Reynolds Number and Mach Number Effects on the Shock-Induced Separation

    Zuo, Feng-Yuan / Shen, Yu / Wei, Jia-Rui et al. | AIAA | 2024