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T HE present experiment investigates the interaction of canard and wing vortices and their effect on the lifting wing's flowfield turbulence and Reynolds stresses. Spanwise wing blowing was used to enhance the leading edge vortex and alter the vortex trajectory in an effort to keep it locked to the wing's leading edge for lift enhancement. The turbulence intensity and Reynolds stress values, obtained by using hot film anemometers, illustrate the vortex structure.