Rolling Moments Due to Rolling and Yaw for Four Wing Models in Rotation (1932)
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moments due to wind direction in these tests. (See Table XXVI1 for lolling and yaw will first be made, using as a basis the standard equivalents.) N. A. C. A. 84 monoplane wing, for which not only The characteristic curves of rolling-moment co- aiitorotation but also pressure-distribution data are… … FiGURE 6.—Torque balance installation In (he tests the axis of yaw was in a plane parallel monu^ter, are shown in Figure 0. Tlie dashed por- to the wind direction and normal to the plane of tlie tions of the curves represent estimated failings where wing chords. This is not the conventional axis of…
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