Abstract
A = coefficient for span-loading series CD = drag coefficient CL = lift coefficient CM = pitching-moment coefficient ACM = CM contributed by the nonelliptical portion of the span loading N = number of terms in the span-loading series S = reference area for coefficients a = aspect ratio b = span c = chord ci = section lift coefficient Cm = section pitching-moment coefficient m = mean aerodynamic chord x, y = longitudinal and lateral coordinates A = quarter-chord sweep angle 0 = transformed lateral coordinate, cos0 — —2y/b = taper ratio
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