Continuation of studies initiated in 1944 regarding potential improvements of turbojet propulsion systems for supersonic flight; comparison of some aspects of axial compressor design for accommodating high rate of mass flow.


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    Title :

    Simplified design comparisons of axial compressors


    Additional title:

    J. Aeronautical Sciences


    Contributors:


    Publication date :

    1951


    Size :

    13 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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