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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    Titel :

    An Investigation of Viscous Losses in Radial Inflow Turbine Nozzles


    Beteiligte:
    I. Khalil (Autor:in) / W. Tabakoff (Autor:in) / A. Hamed (Autor:in)

    Erscheinungsdatum :

    1977


    Format / Umfang :

    87 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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