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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    Title :

    Effect of simulated glaze ice on a rectangular wing


    Additional title:

    Einfluss von simuliertem Eis auf die Stroemungsverhaeltnisse an einem rechteckigen Tragfluegel


    Contributors:

    Published in:

    AIAA-Papers ; Jan ; 1-9


    Publication date :

    1988


    Size :

    9 Seiten, 19 Bilder, 12 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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