A theoretical model is developed to predict losses in radial inflow turbine nozzles. The analysis is presented in two parts. The first one evaluates the losses which occur across the vaned region of the nozzle, while the second part deals with the losses which take place in the vaneless field. It is concluded that the losses in a radial nozzle would not be greatly affected by the addition of a large vaneless space.


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    Title :

    An Investigation of Viscous Losses in Radial Inflow Turbine Nozzles


    Contributors:
    I. Khalil (author) / W. Tabakoff (author) / A. Hamed (author)

    Publication date :

    1977


    Size :

    87 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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