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The document presents a study on the aerodynamic performance of a NACA 0012 airfoil with a focus on the effects of a rotating disk mounted on its upper surface. It analyzes three configurations: a clean airfoil, an airfoil with a non-rotating disk, and an airfoil with a rotating disk, with findings indicating that the rotating disk significantly enhances lift due to the Magnus effect. The study employs numerical simulations to evaluate lift and drag coefficients and emphasizes the potential of using rotatin

Author

SUBRAT SWAMY

Language

EN