Abstract
Nomenclature Cp = surface pressure coefficients, p p1 = 0:5 U 1 L = wing root chord length p1 = freestream static pressure Re = Reynolds number based on the wing root chord, UL= U1 = freestream velocity = angle of attack x = local nondimensional coordinates based on the characteristic length which is the sectional circumference for the sections S1–S8 and the curve length of the sectional upper surface for the sections S9–S19
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