Effect of Variation of Chord and Span of Ailerons on Rolling and Yawing Moments at Several Angles of Pitch (1931)
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lute rolling and yawing moment coefficients for one aileron. As before, simultaneous measurements of the tension L and are respectively rolling and yawing mo- in the roll and yaw balance wires were made at speeds ments in pounds-feet. of 40, 58.7, and 80 feet per second (respectively, 27.3, g =… … direct summation of the values for corresponding Figure 4.—Photograph of model set at 12° pitch in tunnel aileron settings and are for the condition of right characteristics of the curves. The ailerons were set to aileron up and left aileron down. The reference axes the desired angle by the use of…
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