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¢)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    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