Full-scale Force and Pressure-distribution Tests on a Tapered U.S.A. 45 Airfoil (1935)
NASA Technical Reports Server (NTRS) · leaf 13
Figure 4.- Characteristics of the tapered U.S.A.45 airfoil as determined by force tests. Velocity: 112.3 ft./sec Av. Reynolds lumber:5,030,000. 8i£e; 7.38'(mean chord) by 45.75' . Results corrected for tunnel effects. F.8.W.T.
NASA Technical Reports Server (NTRS)
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