Potential increases in ideal stage pressure ratio theoretically possible in axial compressors; paper shows various configurations of flow diagram, for four individual cases, which result in considerable increases in ideal stage pressure ratio; considerations limited to ideal adiabatic flow through curved lattice types of blading.


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    Title :

    High-speed flow through cambered rotating grids


    Additional title:

    J Aeronautical Sciences


    Contributors:


    Publication date :

    1948


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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