The production-model 333-A-23 turbojet-engine compressor with a 17-blade impeller was operated at ambient and 0 F inlet temperatures and at inlet pressures of 14 and 5 inches mercury absolute for equivalent impeller speeds from 6000 to 12,750 rpm. The results of this investigation are compared with those of the 533-A-21 compressor. At the design equivalent speed of 11,750 rpm the maximum pressure ratio was 4.39. This occurred at the surge point at which the equivalent weight flow was 80.8 pounds per second, ana the adiabatic temperature-rise efficiency was 0.757. The maximum flow at the design equivalent speed was 88.0 pounds per second. The maximum adiabatic temperature-rise efficiency of 0.799 was obtained at an equivalent speed of 10,000 rpm, and equivalent weight flow of 62.9 pounds per second, and a pressure ratio of 3.20. At the maximum equivalent speed investigated (12,750 rpm), a peak pressure ratio of 4.90 was attained at an equivalent weight flow of 85.4 pounds per second and an efficiency of 0.680.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Performance of J33-A-23 Turbojet-Engine Compressor


    Beteiligte:
    Beede, William L. (Autor:in) / Kottas, Harry (Autor:in)

    Erscheinungsdatum :

    20.07.1948


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Performance of J33-A-27 Turbojet-Engine Compressor

    Kovach, Karl / Osborn, Walter M. | NTRS | 1949


    Performance of J33-A-27 Turbojet-Engine Compressor

    Beede, William L. / Ginsburg, Ambrose | NTRS | 1950


    Performance of J33-A-27 Turbojet-Engine Compressor

    Withee, Joseph R., Jr. / Beede, William L. / Ginsburg, Ambrose | NTRS | 1950


    Performance of Allison Model 400-C6 Turbojet-Engine Compressor

    Kovach, Karl / Withee, Joseph R., Jr. | NTRS | 1948


    Performance of Compressor of XJ-41-V Turbojet Engine

    Creagh, John W. R. / Ginsburg, Ambrose | NTRS | 1947