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turbulence intensity of 9% just after the trailing edge. Maximum turbulence intensity after x/c = 0 is observed in the vortex core which decays with downstream distance. Five-hole probe mean velocity measurements revealed jet like and wake like axial velocity profiles depending on wing angle of attack, with values of 1.33U∞ and 0.83U∞ being measured for 10° and 5°. Axial vorticity is also observed to increase gradually with downstream distance. A full Reynolds stress turbulence model with a second order upwind differencing scheme is used to compute the vortex in the near-field. Vortex structure and trajectory correlate well with experiment. It is thought that the dissipative nature of the second order convection scheme led to discrepancies between numerical and experimental results.