Abstract
Nomenclature = b=S, aspect ratio b = span, mm CD = wing drag coefficient CL = wing lift coefficient c = chord, mm d = angle relative to wing chord plane, deg q = 1=2 1V 1, freestream dynamic pressure, kPa Re = 1V1c= 1, Reynolds number based on wing model chord S = reference area, mm V1 = freestream velocity, m=s x, y, z = aerodynamic axes = angle of attack, deg = strake leading-edge sweep angle, deg = absolute viscosity, N s=m = air density, kg=m
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