The dangerous sideslip of a stalled airplane and its prevention (1931)
NASA Technical Reports Server (NTRS) · leaf 20
Pigs. 10,11,12 N.A.C.A. Technical Memorandum No. 638 … 2 v Pig. 11 Coefficient F30°35° of wing ^^0 moment about the normal axis against a = 15?20° ^i , and 2 v a as parameter. Fig. 12 Increase in angles of "bank and yaw following a passing asynmetric disturbance. M,0 = +0.1 (l/s) .2 .4 .6 t(s)
NASA Technical Reports Server (NTRS)
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