A review of several simple, inviscid, high-altitude rocket plume models indicated the most accurate representation. Wind-tunnel plume measurements have been used to verify the Jarvinen-Hill model and to study the plume viscous mixing layers which simulated flight conditions by matching wind tunnel and flight plume Knudsen numbers. The HAPRAP data simulate typical ICBM sustainer flight in the 120 to 320 km altitude range. (Author)


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    Titel :

    Study of Wind Tunnel Simulation of High Altitude Rocket Plumes


    Beteiligte:
    J. S. Draper (Autor:in) / J. P. Moran (Autor:in)

    Erscheinungsdatum :

    1973


    Format / Umfang :

    162 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Wind-Tuimel Simulation of High-Altitude Rocket Plumes

    James Stark Draper / James P. Moran | AIAA | 1978


    High Altitude Rocket Plumes

    P. O. Jarvinen / J. A. F. Hill / J. S. Draper et al. | NTIS | 1966



    Intermediate altitude rocket exhaust plumes

    ANDERSON, E. W. | AIAA | 1971