Pigs. 1,3,4,5 N.A.C.A. Technical Memorandum No. 906 Figure 3..- Circulation Luftf. Forschg, 1929 S.27 about A= 5; Sharp edges, straight wing in yaw. o Wing axis measurement a Computed from cSp and cw TJ.A.C.A. Hep. 548; ^- 6 D Wind axis measurement • Computed from csi and cw N.A.C.A. Rep. 431… … Figure 5.- Rolling moments due W -20° 30' W.° P* to yaw£ii& against Angle of sideslip aspect ratio; apolicable to Figure 4,~ Rolling moments due to T=0 to 25°. yawing of straight wings (zero dihedral).
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