A Comparison Between the Theoretical and Measured Longitudinal Stability Characteristics of an Airplane (1934)
NASA Technical Reports Server (NTRS) · leaf 7
se of the relatively greater velocity over the tail for the power-on condition. Weight 1,290-1,340 lb. Attempts were made to evaluate the derivatives Moment of inertia about Y axis (B) 673 slug ft.2 Wing dimensions: mM) mw, and mq for the power-on condition on the Span 30.0 ft. basis of assumed… … Figure 1.—Front view of Doyle 0-2 airpl so many arbitrary assumptions had to be made in Ccnter-of-gravity position: Below chord 23.4 in., 36.0 per cent their evaluation that it is not considered worth while chord. to include either the methods used to compute the Rear of L. E 22.4 in., 34.0 per…
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