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Spinning Characteristics of Wings III : a Rectangular and Tapered Clark Y Monoplane Wing with Rounded Tips (1937)
NASA Technical Reports Server (NTRS) · leaf 19
N.A.C.A. Technical Note No. 612 Fig. 5b 30 40 50 60 70 Angle of attack, cC ,deg. Figure 5b.- Variation of longitudinal-force coefficient Cx" (earth axes) with angle of attack; 5:2 tapered wing, rounded tips.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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