The first shock reflection within truncated plug nozzle propulsive jets is investigated experimentally using a free jet blow-down facility. The locations and sizes of these reflections in axisymmetric plug nozzles, with cylindrical shrouds and conical truncated plugs, are presented. Data are presented for a range of ambient to nozzle total pressure ratios. The effects of Mach disk location and size resulting from changing plug length and from varying amounts of base bleed are documented.


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    Titel :

    The Mach disc in truncated plug nozzle flows


    Beteiligte:
    Giel, T. V., Jr. (Autor:in) / Mueller, T. J. (Autor:in)

    Kongress:

    American Institute of Aeronautics and Astronautics, Fluid and Plasma Dynamics Conference ; 1975 ; Hartford, CT


    Erscheinungsdatum :

    01.06.1975


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    The Mach disc in truncated plug nozzle flows

    GIEL, JR., T. / MUELLER, T. | AIAA | 1975


    Mach Disk In Truncated Plug Nozzle Flows

    Thomas V. Giel Thomas J. Mueller | AIAA | 1976


    Cylindrical diffuser performance using a truncated plug nozzle

    GALANGA, F. L. / MUELLER, T. J. | AIAA | 1976