Abstract
b = local semispan Cl = rolling moment coefficient Cp = pressure coefficient Cr = root chord d = diameter of artificial nose perturbation Re = Reynolds number by root chord V∞ = speed of freestream X = axial location of artificial nose perturbation x = axial body-fixed coordinate y = spanwise body-fixed coordinate z = normal body-fixed coordinate and normal position of the leading-edge vortex α = angle of attack θ = circumferential location of artificial nose perturbation ω = maximum vorticity of leading-edge vortex
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