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DYNAMIC STALL OF A RAPIDLY PITCHING NACA AIRFOIL
Philip Morgan and Miguel Visbal
Air Force Research Laboratory, Wright-Patterson Air Force Base, Ohio, U.S.A.

This video shows computations of flow separation over a three-dimensional wing.

Reference: P. Morgan and M. Visbal, "Simulation of unsteady three-dimensional separation on a pitching wing," 31st AIAA Fluid Dynamics Conference & Exhibit, Anaheim, CA, June 11-14, 2001.
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