The effect of area aspect ratio on the yawing moments of rudders at large angles of pitch on three fuselages (1933)
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700 COMMITTEE FOR AERONAUTICS REPORT NATIONAL ADVISORY TABLE n tematic deviation, especially in the case of rudder 1 of aspect ratio 0.77, but on the whole, the fit is considered EMPIRICAL EQUATIONS REPRESENTING OBSERVED DATA ON TAWING MOMENTS DUE TO RUDDER satisfactory. The method of deriving the… … Area ratio,Sr/S* Figube 82.—Effect of area ratio (aspect ratio 1.66-L88) on yawing moment cooffl- From these equations, the value of—r-. dents of readers on cabin fuselage at 0° pitch. (Angles marked on curves aro 5 {A^r-0.0075) mdder angles) at certain values of aspect ratio and angle of pitch are…
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