Results of analysis applied to design of inlet guide vanes of axial flow compressor.


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    Title :

    Compressibility correction for turning angles of axial-flow inlet guide vanes


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1950


    Size :

    31 pages


    Remarks:

    Diagrams, Graphs


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English