Force tests on rubber de-icer models of several different profiles, at approximately one-third full scale, been carried out in the NACA 8-foot high speed wind tunnel. The conventional de-icer installation, deflated, added about 15 percent to the smooth-wing drag and, inflated, added about 100 percent. An improved installation with flash attaching strips added about 10 percent, deflated. The bulging, or ballooning, of de-icers from the wing surface is described and some remedies are discussed.


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    Titel :

    The drag of inflatable rubber de-icers


    Beteiligte:

    Erscheinungsdatum :

    01.10.1938


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch



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    Robinson, R.G. | Engineering Index Backfile | 1938


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