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Title: Dynamic stall of rapidly pitching NACA airfoil

Description: Computations were performed by Dr. Philip Morgan and Dr. Miguel Visbal, Computational Sciences Branch, U.S. Air Force Research Laboratory, Wright-Patterson Air Force Base, Ohio.

Credits:

References: 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

Web Page:

Contributed By: Dr. Miguel Visbal, Air Force Research Laboratory, Wright-Patterson Air Force Base, Ohio, U.S.A.

 
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