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Spinning Characteristics of Wings IV : Changes in Stagger of Rectangular Clark Y Cellules (1937)
NASA Technical Reports Server (NTRS) · leaf 26
C.A. Technical Hot© Ho. 635 Fig. 13 … v 2 - k z -0.0C20(cC - 20°) p. - 5 2 nr 1.0 Figure 13.- Effect of pitching-moment inertia parameter upon yawing-mcaenw coefficient that must be supplied by parts other than the wing for equilibrium in a spin.NASA Technical Reports Server (NTRS)
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