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    Title :

    Modeling of Highly Instrumented Honeywell Turbofan Engine Tested with Ice Crystal Ingestion in the NASA Propulsion System Laboratory (AIAA 2016-3895)


    Contributors:

    Conference:

    AIAA atmospheric and space environments (Conference)



    Publication date :

    2016-01-01


    Size :

    21 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English