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Simulations of High Reynolds Number Air Flow Over the NACA 0012 Airfoil Using the Immersed Boundary Method
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The immersedboundary method is coupled to an incompressibleflow Reynoldsaveraged Navier Stokes solver, based on a twoequation turbulence model, to perform unsteady numerical simulations of airflow past the NACA0012 airfoil ...