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Planing-surface Tests at Large Froude Numbers - Airfoil Comparison (1938)
NASA Technical Reports Server (NTRS) · leaf 23
N.A.C.A. Technical Memorandum Ho. 848 Figs. 17,18,19,22 1A 4t Q5 * = 6 « x = 7,5 •• o = 9,5 » a =1Z <• = 16 » Figures 17,18,19.. Airfoil test Position 1.0 of lift 05 resultant(Ip/b) against aspect ratio(l/b). … Figure 22.- Experimental set-up with high-speed carriage.NASA Technical Reports Server (NTRS)
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