Experimental measurements of the effect of simulated glaze ice on a three-dimensional wing are presented. A semispan wing of effective aspect ratic five was mounted from a splitter plate in the OSU subsonic wind tunnel. The model has a straight, untwisted rectangular platform, and uses a NACA 0012 airfoil section. Surface pressures were measured at 5 semispan locations and a total-pressure wake-survey probe was used on the model centerline. The section lift and drag data from the model centerline compare well to earlier 2-D data. These data show a large drag and maximum lift penalty due to the simulated glaze ice. Three-dimensional span-load data compare well to computational results.


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    Titel :

    Effect of simulated glaze ice on a rectangular wing


    Weitere Titelangaben:

    Einfluss von simuliertem Eis auf die Stroemungsverhaeltnisse an einem rechteckigen Tragfluegel


    Beteiligte:
    Bragg, M.B. (Autor:in) / Khodadoust, A. (Autor:in)

    Erschienen in:

    AIAA-Papers ; Jan ; 1-9


    Erscheinungsdatum :

    1988


    Format / Umfang :

    9 Seiten, 19 Bilder, 12 Quellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Effect of simulated glaze ice on a rectangular wing

    BRAGG, M. / KHODADOUST, A. | AIAA | 1989



    LDV measurements on a rectangular wing with a simulated glaze ice accretion

    KHODADOUST, A. / BRAGG, M. / KERHO, M. | AIAA | 1992


    Finite wing aerodynamics with simulated glaze ice

    KHODADOUST, A. / BRAGG, M. / KERHO, M. et al. | AIAA | 1992


    The Effect of Glaze Icing on Wing Aerodynamics and Aircraft Lateral Stability

    Nair, G. G. / Chapleo, A. Q. | British Library Online Contents | 1994