Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Experimental and Numerical Investigation of Unsteady Shock Wave Interaction with a Thruster Cavity in Mach 7 Flow Over 30° Wedge


    Contributors:

    Conference:

    AIAA SciTech Forum and Exposition ; 2022 ; San Diego, Calif.; Online



    Publication date :

    2022


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Shock Wave Laminar Boundary Layer Interaction Over a Double Wedge in a High Mach Number Flow

    Badr, M.A. / Knight, D.D. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2014




    Unsteady Analysis of Shock-Wave/Boundary-Layer Interaction Experiments at Mach 4.2

    Combs, Christopher S. / Schmisseur, John D. / Bathel, Brett F. et al. | AIAA | 2019