Low-speed aerodynamic characteristics of a 16-percent-thick variable-geometry airfoil designed for general aviation applications

Low-speed aerodynamic characteristics of a 16-percent-thick variable-geometry airfoil designed for general aviation applications - - Washington, D.C. National Aeronautics & Space Administration 1978 - 74 p. - NASA TP 1324 : 1978 .





Low-speed airfoil section, Reynolds number effects, Experimental-theoretical, General aviation aircraft, GA (PC)-l airfoil

LNASA TP 1324 : 1978

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