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    Title :

    High-temperature high-frequency turbine exit flow field measurements in a military engine with a cooled unsteady total pressure probe




    Publication date :

    2011



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    52.50 Energietechnik: Allgemeines / 52.30 Strömungskraftmaschinen, Turbomaschinen / 52.30 / 52.50
    Local classification TIB:    275/5345/5365/5500





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