Noise-source separation techniques, using three engine-internal sensors, are applied to existing static-engine test data to determine the turbine transfer function for the currently subdominant combustion noise. The results are used to assess the combustion-noise prediction capability of the Aircraft Noise Prediction Program (ANOPP) and an improvement to the combustion-noise module GECOR is suggested. The work was carried out in response to the NASA Fundamental Aeronautics Subsonic Fixed Wing Program s Reduced-Perceived-Noise Technical Challenge.


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    Titel :

    Full-Scale Turbofan-Engine Turbine-Transfer Function Determination Using Three Internal Sensors


    Beteiligte:

    Kongress:

    17th Aeroacoustics Conference ; 2011 ; Portland, OR, United States


    Erscheinungsdatum :

    01.02.2012


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :