A study of the two-control operation of an airplane (1938)
NASA Technical Reports Server (NTRS) · leaf 11
tions, it appeared that In the calculations illustrated in figure 11 the banking a certain amount of favorable secondary aileron yawing motion was assumed to be forced to follow the ideal moment might be desirable to overcome the adverse bank by means of a rolling control and the resultant yaw… … Time, seconds Fiouek 13.—The effect of secondary yawing moments on yawing motions during 30° bank maneuver performed with rolling control; Qi°U C«-± O.SlCi, FlQOBE 10.—Control-moment coefficients necessary to produce specified manuaver («-±0J«. with ten sideslip. turn. The effects of secondary…
NASA Technical Reports Server (NTRS)
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