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Systematic investigation of Joukowsky wing sections (1927)
NASA Technical Reports Server (NTRS) · leaf 14
H.A.C.A. Technical Memorandum No.422 + d/z = 0.05 o u _ 0.10 • it =i 0.15 0.20 X II = 0.25 © II = … 0.30 0.05 0.10 0.15 0.20 0.10 0.20 0 f/z Fig.8 Minimum section drag plotted against f/z and d/l. o d/Z =0.05 x - =0.10 + «•■ =0.15 © <• =0.20 • " =0.25 0 Fig.12 cP plotted amax o against wing- O H section camber 601- 0.3 0.4 0.2 0.1 0 f/lNASA Technical Reports Server (NTRS)
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