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The dangerous sideslip of a stalled airplane and its prevention (1931)
NASA Technical Reports Server (NTRS) · leaf 23
1J.A.C;A. Technical Memcranduh No. 633 Figs. 18,19 … Fig. 18, Increase in angle of hank following a passing asymmetric disturbance fi0 = +0.1 (l/s). Bantam 40° "biplane Low-wing 30° monoplane Junkers A35 20° Staggered "biplane Bristol-fighter 10° ,2 .4 . .6 .8 1.0 t(s) Fig.. 19, Increase in angle of hank following a massing asymetric disturbance fL =…NASA Technical Reports Server (NTRS)
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