The effect of lateral controls in producing motion of an airplane as computed from wind-tunnel data (1937)
NASA Technical Reports Server (NTRS) · leaf 5
470 REPORT NO. 570 NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS … Time, second (a) (b) Ci-OOi C-0 (o) (d) Ci=0 C.-0.01 Fioukb 6 (a, b, c d).—Computed rolling and yawing motions of average airplane. V d ' 0.35 ■ • • 1.0 ■ IS / / Bank due to control yawing moment Bank due to control rolling moment Sideslip due to control Sideslip due to control yawing moment…
NASA Technical Reports Server (NTRS)
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