The effect of lateral controls in producing motion of an airplane as computed from wind-tunnel data (1937)
NASA Technical Reports Server (NTRS) · leaf 17
deducted from the yawing- reaching a maximum of 30° at -k seconds. This formula moment curves. These computations showed that the determined the angular velocities and accelerations by maximum yawing moment necessary at the lowest the principles already demonstrated. Inasmuch as the speed was 10… … 0 1 2 3 4 5 6 1. The agreement of the computations with the Time, seconds results of flight tests verifies the usefulness of the (a) Low speed, flaps down, Cl—1.8. (b) Gliding speed, <7l=1.0. method utilizing stability derivatives for the study of Fiotoe20—Budder control-moment coefficients during…
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