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Aerodynamics of the rotary leading edge aircraft wing was experimented by the help of modified NACA-0010 airfoil. CFD simulation was done by converting the 2-D NACA-0010 airfoil to a 3-D aircraft wing. A cylinder was mounted at the leading edge of the modified aircraft wing and then it was allowed to rotate in anti-clockwise direction at a certain rpm. The simulation showed that there was a significant...