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:

    Conference:

    25th International Society of Air-breathing Engines (ISABE) Conference ; 2022 ; Ottawa, Ontario, CA


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English






    Gas-turbine blading

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