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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    Title :

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


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1943


    Size :

    19 pages


    Remarks:

    Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English




    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