The effect of area aspect ratio on the yawing moments of rudders at large angles of pitch on three fuselages (1933)
NASA Technical Reports Server (NTRS) · leaf 2
symmetry of the model, i. e., about a steel pivot which engaged a socket in a brass plate "body" axis. No motion in roll was permitted, but fastened to the rudder. The gap between the rudder the angle of pitch could be varied and the model and fin was sealed with a thin layer of petroleum jelly.… … Fiqtjee 5.—Dimensions and arrangement of tail surfaces plates. These settings were made with respect to wire running from a point on the fuselage near the the fixed surface, which had been aligned with the tail to a balance of the pendulum type. A counter- axis of the model. The axis of the model…
NASA Technical Reports Server (NTRS)
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