Background - A joint program (FAA): Honeywell-U.S. Air Force- NASA to develop highly-loaded LPT stages Objective of current work - Application and evaluation of a High-Fidelity numerical simulation for flow field in a highly loaded LPT stage. 1. loss generation mechanism. 2. Reynolds number effects on stage performance


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    Title :

    Aerodynamic Loss Generation in a Low-Pressure Turbine Stage with High Lift Blading


    Contributors:
    C. Hah (author) / J. Loellbach (author)

    Publication date :

    2022


    Size :

    31 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






    Gas-turbine blading

    Colwell, A.T. / Cummings, R.E. | Engineering Index Backfile | 1948