Results indicate that performance of combinations was little affected by sonic or supersonic base bleed; efficiency of terminal-fairing model, designed to improve performance of fixed geometry nozzle at transonic speeds, was only about 3 to 5% less than those of convergent divergent nozzles.


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    Titel :

    Effect of base bleed and terminal fairings on performance of exhaust-nozzle-afterbody combinations at mach numbers of 1.93, 2.55, and 3.05


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:


    Erscheinungsdatum :

    1960


    Format / Umfang :

    31 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch