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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    Titel :

    Aerodynamic Effects Of Deicing And Anti-Icing Fluids


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1994-02-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



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    Aerodynamic effects of deicing and anti-icing fluids

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    Aerodynamic effects of deicing and anti-icing fluids

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