This study was conducted to obtain a detailed experimental description of the flow field created by the interaction of a single-expansion-ramp-nozzle flow with a hypersonic external stream. Data were obtained from a generic nozzle/afterbody model in the 3.5-Foot Hypersonic Wind Tunnel of the NASA Ames Research Center in a cooperative experimental program involving Ames and the McDonnell Douglas Research Laboratories. This paper presents experimental results consisting primarily of surveys obtained with a five-hole total-pressure/flow-direction probe and a total-temperature probe. These surveys were obtained in the flow field created by the interaction between the underexpanded jet plume and the external flow.


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    Titel :

    Hypersonic nozzle/afterbody CFD code validation. I - Experimental measurements


    Beteiligte:
    Spaid, Frank W. (Autor:in) / Keener, Earl R. (Autor:in)

    Kongress:

    AIAA, Aerospace Sciences Meeting and Exhibit ; 1993 ; Reno, NV, United States


    Erscheinungsdatum :

    1993-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Hypersonic Nozzle-Afterbody Experiment - Flowfield surveys

    Spaid, Frank W. / Keener, Earl R. | AIAA | 1996



    Experimental results for a hypersonic nozzle/afterbody flow field

    Spaid, Frank W. / Keener, Earl R. / Hui, Frank C. L. | NTRS | 1995