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 32
H.A.C.A. Technical Note Mo. 536 *ig. 9 .16 … Angle of sideslip, P , degrees .25 ilb/37 figure 9.- Variation of rolling-moment ooeffioient C, (body axes) with angle of sideslip and with ilb/2V. 81gns for right spins.
NASA Technical Reports Server (NTRS)
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