Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    EXPERIMENTAL INVESTIGATION OF TRANSVERSE INJECTION FLOWFIELD AT MACH 5 AND THE INFLUENCE OF IMPINGING SHOCK WAVE



    Conference:

    18th, AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference ; 2012 ; Tours, France



    Publication date :

    2012-01-01


    Size :

    22 pages


    Remarks:

    Includes bibliographical references and index



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English






    Experimental Study of a Mach 3 Bump-Compression Flowfield

    Tillotson, Benjamin J. / Loth, Eric / Dutton, J. Craig et al. | AIAA | 2009


    Experimental Study of a Mach 3 Bump Compression Flowfield

    Tillotson, Benjamin / Loth, Eric / Dutton, J | AIAA | 2006