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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 21
Fig. 7a N.A.C.A. Technical Note No. 612 Figure 7a.- Variation of normal-force coefficient Cg (body axes) with angle of attack; rec- tangular wing, roundecl 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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