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).
Prop-fan airfoil icing characteristics
1989-01-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Prop-fan airfoil icing characteristics
AIAA | 1989
|Prop-fan airfoil icing characteristics
Tema Archiv | 1988
|An experimental study of airfoil icing characteristics
AIAA | 1982
|Effect of geometry on airfoil icing characteristics
AIAA | 1984
|Effect of geometry on airfoil icing characteristics
NTRS | 1984
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