Tests of NACA 0009, 0012, and 0018 Airfoils in the Full-Scale Tunnel (1939)
NASA Technical Reports Server (NTRS) · leaf 8
5 AIRFOILS IN THE FULL-SCALE TUNNEL TESTS OF N. A. C. A. 0009, 0012, AND 0018 … Angle of attack, ct ,deg. Angle of attack, ot ,deg. Figure 9.—Characteristics of the N. A. C. A. 0018 airfoil of aspect ratio 6. Figure 7.—Characteristics of the N\ A. C. A. 0009 airfoil of aspect ratio 6. 20 40 60 80 /OO Percent of chord 32 28 8., 24 14 20 24 20 40 20 P c * Hi 16 0 <\/6 4: /e c>…
NASA Technical Reports Server (NTRS)
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