Controllability and Maneuverability of Airplanes (1923)
NASA Technical Reports Server (NTRS) · leaf 8
he value of L when there is no rotation and with the ailerons at 13° is 9,000 foot-pounds.2 From this data we may approximately plot the variations in L with the variations in p. (Fig. 5.) It is evident that L falls off as p increases, although the form of the curve is not determined here with any… … Fig. 5—Effect on L' of changes in p, ailsrons at 13°, 80 M. P. H. FlG. 6. time required to reach the constant value is always the same under all conditions for a given airplane, so that the number of degrees turned in a unit time, that is, the area under the curve, will be proportional to the…
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