Use of low speed and high speed 2-dimensional cascade tunnels and low speed test blower, to determine experimental method of designing blades; important parameters involved in compressor blade design, turning angles or loading, design angle of attack, and qualitative critical speed evaluated.


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    Title :

    N.A.C.A. Cascade data for blade design of high-performance axial-flow compressors


    Additional title:

    J Aeronautical Sciences


    Contributors:


    Publication date :

    1948


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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