Effect of tip shape and dihedral on lateral-stability characteristics (1937)
NASA Technical Reports Server (NTRS) · leaf 8
angle the new wing chord along the wind direction FiauBE 21,—Effect of dibedral of 93 percent semispan of lectangular wing on rate of change of cross-wind force and yswlng-moment coefficients with an(^ of yaw. IS c'=- cos 4/ The increments ^(^p^ aJid A^^^^ lend them- and the spanwise displacement… … Dihedral angle, T , degrees FtaoBE 22.—Effect of dihedral on rates of change of rolling-moment, yawlne-moment, and cross-wind fbrcecoeffidents with angle of yaw. Consequentiy, the valuesof^ A(^^)^and^ a(^)^ Then, owing to the dihedral angle, the trailing edge of the new chord of the rearward wing…
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