Comparison of aerodynamic characteristics of three wings having similar plan forms and root- and tip-chord thickness ratios with aspect ratio of 10, taper ratio 2.5; results show effects of airfoil section on characteristics of tapered wings for Reynolds number range of 2.0 × 106 to 5.0 × 106.
Experimental and calculated characteristics of several high-aspect-ratio tapered wings incorporating NACA 44-series, 230-series, and low-drag 64-series airfoil sections
Nat Advisory Committee Aeronautics -- Tech Note
1948
37 pages
Aufsatz (Zeitschrift)
Englisch
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