Preliminary investigation was made of first stage of 2-stage turbine; this stage was matched to centrifugal compressor and operated in conjunction with combustors, engine accessories, and three sizes of jet nozzle.


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    Title :

    Investigation of first stage of two-stage turbine designed for free-vortex flow


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Englert, G.W. (author) / Ross, A.O. (author)


    Publication date :

    1950


    Size :

    30 pages


    Remarks:

    Diagrs, Charts, Tables


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English







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