Study of under-expanded jet was made using modified "hot-shot" wind-tunnel facility; Mach disk location was insensitive to ratio of specific heats, condensation, nozzle lip geometry, and absolute pressure level; for overall pressure ratios to about 300, 000 Mach disk location was found to vary as square root of overall pressure ratio; expression for Mach number distribution along jet axis is given to good approximation as function of specific heat ratio.


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    Titel :

    Study of highly underexpanded sonic jet


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Crist, S. (Autor:in) / Sherman, P.M. (Autor:in) / Glass, D.R. (Autor:in)

    Erschienen in:

    AIAA Journal ; 4 , n 1


    Erscheinungsdatum :

    1966


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Study of the highly underexpanded sonic jet.

    CRIST, S. / GLASS, D. R. | AIAA | 1966


    Flat plate in a highly-underexpanded sonic jet

    Seivwright, Douglas / Shreeve, Raymond | AIAA | 1997


    Flat Plate in a Highly-Underexpanded Sonic Jet

    Seivwright, D. L. / Shreeve, R. P. / AIAA | British Library Conference Proceedings | 1997


    Numerical Simulation of Underexpanded Sonic Jet

    Dharavath, Malsur | Online Contents | 2012


    Scaling parameters for underexpanded sonic jets

    Yuceil, K. / Otugen, M. | AIAA | 2001