The static program has shown to date that very large noise reductions can be achieved by the sonic inlet concept with realistic inlet length and good aerodynamic performance. It is also shown that different inlet concepts produce substantially different results.


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    Titel :

    Sonic inlet development for turbofan engines


    Beteiligte:
    Klujber, F. (Autor:in)


    Erscheinungsdatum :

    01.01.1972


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Turbofan noise reduction using a near sonic inlet

    KOCH, R. / CISKOWSKI, T. / GARZON, J. | AIAA | 1974



    Active Control of Radiated Inlet Noise from Turbofan Engines

    Fuller, Chris R. / Burdisso, Ricardo A. / Thomas, Russell H. et al. | SAE Technical Papers | 1993


    Active control of radiated inlet noise from turbofan engines

    Burdisso,R.A. / Thomas,R.H. / Fuller,C.R. et al. | Kraftfahrwesen | 1993