A study of the two-control operation of an airplane (1938)
NASA Technical Reports Server (NTRS) · leaf 10
eration). described in the discussion of the stability of this mo- shows the control-moment coefficients necessary to tion. The damping of these oscillations is slight and is constrain the rolling and yawing motions to the speci- most apparent at the lowest lift coefficient, (7i=0.35. fied maneuver… … the two-control airplane with the most perfect possible Time, seconds coordination of the motions that might be obtained Figubje 9—Angle of bank and rates oi rolling and yawing specified for 30° bant two- control torn maneuvers. with three-control operation. Obviously, it will be necessary to…
NASA Technical Reports Server (NTRS)
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