An icing test program was carried out during the 1986-87 and 1987-88 icing seasons at the Fluidyne Icing Tunnel. The testing consisted of evaluating the icing characteristics and aerodynamic performance characteristics of two thin, two-dimensional airfoil sections. The two airfoils were a NACA Series 16-203 and a Hamilton Standard PF1-304, 3 and 4 percent thickness-to-chord ratio airfoils, respectively. These airfoils are representative of the thin airfoils currently being evaluated for Prop-Fan propulsion systems. The tests were conducted over a wide range of icing conditions, angles-of-attack, and Mach numbers (0.3 to 0.8).


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    Titel :

    Prop-fan airfoil icing characteristics


    Beteiligte:
    Pike, J. A. (Autor:in) / Wainauski, H. S. (Autor:in) / Boyd, L. S. (Autor:in)

    Erscheinungsdatum :

    1989-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Prop-fan airfoil icing characteristics

    PIKE, J. / WAINAUSKI, H. / BOYD, L. | AIAA | 1989


    Prop-fan airfoil icing characteristics

    Pike, J.A. / Wainauski, H.S. / Boyd, L.S. | Tema Archiv | 1988


    An experimental study of airfoil icing characteristics

    SHAW, R. / SOTOS, R. / SOLANO, F. | AIAA | 1982