The DGEN 380 is a small, separate-flow, geared turbofan being promoted for a small twinjet application in the emerging personal light jet market. Smaller, and producing less thrust than other entries in the industry, the engine could be applied to a four to five place twinjet designed to compete in an area currently dominated by propeller-driven airplanes. This paper documents the procedures used to project static noise measurements collected from the engine to flight conditions and the prediction of certification noise of a notional airplane powered by twin DGEN engines. A novel noise model calibration technique and a Monte Carlo uncertainty experiment are emphasized.


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    Titel :

    System Noise Prediction of the DGEN 380 Turbofan Engine


    Beteiligte:

    Erschienen in:

    Journal of Aircraft ; 53 , 6 ; 1779-1786


    Erscheinungsdatum :

    2016-05-25


    Format / Umfang :

    8 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch