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Research on the control of airplanes (1928)
NASA Technical Reports Server (NTRS) · leaf 26
FigB.S & 6 N.A.O.A. Teclinical Memoranduim No.485 Seconds 0 2 4 6 8 10 12 14 … ^8 -20 S 10 03 0 f-< -10 -i8f Fig.5 Failure of ailerons to check a rolling turn. o Seconds (D 2 0 4 6 8 10 12 14 16 18 1— —1— —r- u 20 I- ft 10 - CQ 0 CD <D -10 Yaw U Roll ba -20 Pitch -30 Angular velocities 40 Rudder 0 -40 l- 0, 10^ Ailerons 03 0 S-10 Elevators ^ 20t -10 F Fig.6 Effect of rudder…NASA Technical Reports Server (NTRS)
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