Effect of tip shape and dihedral on lateral-stability characteristics (1937)
NASA Technical Reports Server (NTRS) · leaf 4
, cC, degrees FIOUBE 7.—Effect of wing Up plan foim on rate of change of rolUngmoment co- for three wings of the same elevation shape but having eflJcIeat viKb angle of yaw. Mnrlinnni oidinate points on mean lines in one different plan forms. The effect is pronoimced at an plane. angle of attack of… … remained practically constant. For dihedral angles Angle of attack, U ,clegrees normally used (5° or less), however, the effect is FiaoBi 8.—Sflect of wing tip plan foim on rata of obange of cross-wind forca and yawlng'moment coefflolents with angle of yaw. MaTlmnm ordinate polnts.on negligible. AH…
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