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Reduction of wing lift by the drag (1932)
NASA Technical Reports Server (NTRS) · leaf 7
Figs. 5,6 U.A.C.A. Technical Memorandum No. 681 … '(^-14.3 16.5 _lb 8 -L9.7 Jig. 5 plotted against for Joulcowsky airfoil f/t = 0.05, d/t 0T25 d/t = 0.05 ^c. " = 0.15 +■ - " = 0.25 0 -1 .1 .2 .3 0 Pig. 5 Symmetrical wing sections (f/t = 0) liNASA Technical Reports Server (NTRS)
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