A Comparison Between the Theoretical and Measured Longitudinal Stability Characteristics of an Airplane (1934)
NASA Technical Reports Server (NTRS) · leaf 8
c clinometer, timer, control-position recorder, and angu- pressure, and components of weight parallel and per- lar-velocity recorder are given in references 3, 4, 5, 6, pendicular to the glide path, the effective drag coeffi- and 7, respectively. The angle-of-attack recorder is a cient being the… … Figure 2.—Side view of Doyle 0-2 airplane items, the average altitude, engine speed, and air airplane, mounted about a chord length ahead of the temperature were noted during each glide. wing at the outboard strut fitting. The motion of the Lift coefficients for the power-on condition were vane is…
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