Full-scale Force and Pressure-distribution Tests on a Tapered U.S.A. 45 Airfoil (1935)
NASA Technical Reports Server (NTRS) · leaf 11
N.A.C.A. Technical Mete Ho.521 figs* 1,6 H 0 V E DOB A-«—Orifice ribs (* 25 percent stations B inohes Figure 1.- Tapered U.8.A.45 airfoil. Plan form and orifice location. … Figure 6.- Variation of effective-profile-drag coefficient with lift coefficient of the tapered U.S.A.45 airfoil. 8ize. 7.38'(mean chord) by 45.75'. Results corrected for tunnel effects. F.8.W.T.
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