The effect of lateral controls in producing motion of an airplane as computed from wind-tunnel data (1937)
NASA Technical Reports Server (NTRS) · leaf 9
in- assumed independence of small longitudinal and lateral tended. motions, which is supported by both experience and Stability derivatives above stalling angles.—The reason for the ordinary-flight range, cannot be said to reasons for the apparently contradictory results of the hold under these new… … O 4 8 12 16 20 24 28 cc, degrees different from that used in the cases of ordinary flight. Figure 11.—Coefficients, of rolling moment due to rolling and sideslip at various The wind-tunnel measurements were studied to find the angles of attack. Eectangular Clark Y monoplane; data from tests In the…
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