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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    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


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1960


    Size :

    31 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English