Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Rapid expansion of a supersonic boundary layer and its application to the near wake.


    Author / Creator :

    WEINBAUM, S. /GENERAL ELECTRIC CO., MISSILE AND SPACE DIV., SPACE SCIENCES LAB., THEORETICAL FLUID P


    Contributors:

    Published in:

    AIAA Journal ; 4 , 2 ; 217-226


    Publication date :

    1966




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



    Boundary layer and wake investigation in supersonic flow

    Lukasiewicz, Julius / Royle, J. K. / Aeronautical Research Council | TIBKAT | 1952


    Boundary-Layer Instabilities in Supersonic Expansion Corner Flows

    Chuvakhov, Pavel V. / Egorov, Ivan V. / Ilyukhin, Ivan M. et al. | AIAA | 2021



    Laminar boundary-layer separation and near-wake flow for smooth blunt body at supersonic and hypersonic speeds

    Grange, J.M. / Klinenberg, J.M. / Lees, L. | Engineering Index Backfile | 1967


    Mass transfer in a supersonic near wake

    DIEP, G. B. / MAGRE, P. | AIAA | 1977