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Spinning characteristics of wings II : rectangular Clark Y biplane cellule: 25 percent stagger; 0 degree decalage; gap/chord 1.0 (1935)
NASA Technical Reports Server (NTRS) · leaf 28
rig. 7 H.A.C.A. Technical Note Mo. 526 Angle of attack, d , degrees 70 65 … Figure 7.- Variation of pitching-moment ooefficient 0m (body axes) with angle of attack.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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