Airfoil trailing-edge noise up to a Reynolds number based on chord of 2.96 x 10 to the 6th power was studied. Comparisons are made with current theory, particularly with regard to the nature of the pressure field in the vicinity of the trailing-edge and its influence on the radiated noise.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    An experimental investigation of trailing-edge noise


    Beteiligte:
    Brooks, T. F. (Autor:in) / Hodgson, T. H. (Autor:in)

    Erscheinungsdatum :

    01.06.1979


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Experimental Investigation Into Trailing Edge Noise Sources

    Garcia-Sagrado, Ana / Hynes, Tom / Hodson, Howard | AIAA | 2006





    Trailing Edge Noise

    Strahle, Warren C. / Nagamatsu, Henry T. / Schwartz, Ira R. | AIAA | 1976