Report presents results of wind-tunnel tests of aerodynamic effects of deicing and anti-icing fluids on airplane wings. Tests conducted on three-dimensional half-model airplane and two-dimensional airfoil model at temperatures ranging from -29 to +10 degrees C. Fluids used included three commercial fluids available for use during 1987-1988 winter season, one discontinued commercial fluid, and eight newer fluids experimental at time of test.


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    Title :

    Aerodynamic Effects Of Deicing And Anti-Icing Fluids


    Contributors:

    Published in:

    Publication date :

    1994-02-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English





    Aerodynamic Effects of Deicing and Anti-Icing Fluids

    Reinmann, J.J. | Online Contents | 1993


    Aerodynamic effects of deicing and anti-icing fluids

    Reinmann, John J. / Adams, Dick | NTRS | 1993


    Aerodynamic effects of deicing and anti-icing fluids

    REINMANN, JOHN J. / ADAMS, DICK | AIAA | 1993