Investigation of flow field set up by transverse gas jet issuing into supersonic stream, such as occurring in applications to jet-flaps and to thrust vector control for rocket motors; results of wall and impact pressure measurements throughout core of interaction field, and flow visualization tests, are reported for 11 tests differing by injected mass rate, injection station Mach number, and primary to secondary stagnation pressure ratio; measurements are used to reconstruct true structure of flow and suggest characteristic features which are outlined.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Interaction of supersonic stream and transverse supersonic jet


    Additional title:

    AIAA J


    Contributors:
    Charwat, A.F. (author) / Allegre, J. (author)

    Published in:

    AIAA Journal ; 2 , n 11


    Publication date :

    1964


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Interaction of a supersonic stream and a transverse supersonic jet

    ALLEGRE, J. / CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE / LABORATOIRE D'AEROTHERMIQUE et al. | AIAA | 1964


    Supersonic transverse injection into a supersonic stream.

    MAHAFFEY, R. E. / SCHETZ, J. A. | AIAA | 1968


    Transverse Supersonic Controlled Swirling Jet in a Supersonic Cross Stream

    Shanmugam Murugappan / Ephraim Gutmark / Campbell Carter et al. | AIAA | 2006


    CONTROL OF A TRANSVERSE SUPERSONIC JET INJECTION INTO A SUPERSONIC CROSS-STREAM

    Murugappan, S. / Gutmark, E. / Carter, C. et al. | British Library Conference Proceedings | 2004