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
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- 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
Low-speed airfoil section, Reynolds number effects, Experimental-theoretical, General aviation aircraft, GA (PC)-l airfoil
LNASA TP 1324 : 1978