A full scale general aviation wing with a NACA 63 sub 2 A415 airfoil section was tested to determine icing characteristics for representative rime and glaze icing conditions. Measurements were made of ice accretion shapes and resultant wing section drag coefficient levels. It was found that the NACA 63 sub 2 A415 wing section was less sensitive to rime and glaze icing encounters for climb conditions.


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    Title :

    An Experimental Study of Airfoil Icing Characteristics


    Contributors:
    Shaw, R. J. (author) / Sotos, R. G. (author) / Solano, F. R. (author)

    Conference:

    Twentieth Aerospace Sci. Conf. ; 1982 ; Orlando, FL, United States


    Publication date :

    1982-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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