d cw N.A.C.A. Rep. 431 (Sharp rectangular wing) x Wind axis measurement; A.= 6 + Computed from cS|_ and cw a Wind axis measurement; A= 3 a Computed from and cw Figure 1,- Lateral forces on a yawed wing. r. Outflow direcfi Hound iMity o mS bum, i-i o ARC RM 1059 (Tropez) 1-6 — NACA Rep. 519*Army… … 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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