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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 30
rig. 8 N.A.C.A. Technical Note No. 536 … Angle of attack, ct , degrees Figure 8.- Variation of yawing-moment coefficient 0n (body axes) with angle of attack. Signs for right spins.NASA Technical Reports Server (NTRS)
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