This is an overview of the technical challenges, objectives, and approaches to enable compact, high overall pressure ratio gas turbine engine in support of NASA N+3 goals.


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    Title :

    Compact Gas Turbine Sub-Project - TC 4.2 Compact, High Overall Pressure Ratio (OPR 50+) Gas Generator


    Contributors:

    Conference:

    Icing Hazards Workshop ; 2015 ; Cleveland, OH, United States


    Publication date :

    2015-01-28


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English





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