Performance determined for speeds from 5000 to 14,000 rpm with varying air flow at each speed; determination was in accordance with Committee's recommended procedure for testing superchargers; conclusion was that multistage compressor of high efficiency can be designed by application of airfoil theory. (released 1948) (20¢)


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    Titel :

    Performance of NACA eight-stage axial-flow compressor designed on basis of airfoil theory


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Report


    Beteiligte:
    Sinnette, Jr., J.T. (Autor:in) / Schey, O.W. (Autor:in) / King, J.A. (Autor:in)


    Erscheinungsdatum :

    1943


    Format / Umfang :

    19 pages


    Anmerkungen:

    Bibliography


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Performance of NACA eight-stage axial-flow compressor designed on basis of airfoil theory

    Sinnette, Jr., J.T. / Schey, O.W. / King, J.A. | Engineering Index Backfile | 1943



    Performance of NACA eight-stage axial-flow compressor designed on the basis of airfoil theory

    Sinnette, John T. / Schey, Oscar W. / King, J. Austin | TIBKAT | 1944


    Performance of NACA eight-stage axial-flow compressor at simulated altitudes

    King, J.A. / Regan, O.W. | Engineering Index Backfile | 1944