Pneumatic deicer boots for helicopter rotor blades were tested. The tests were conducted in the 6 by 9 ft icing research tunnel on a stationary section of a UH-IH helicopter main rotor blade. The boots were effective in removing ice and in reducing aerodynamic drag due to ice.


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    Titel :

    Pneumatic boot for helicopter rotor deicing


    Beteiligte:
    Blaha, B. J. (Autor:in) / Evanich, P. L. (Autor:in)


    Erscheinungsdatum :

    01.03.1981


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch





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