Theses and Dissertations
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Computational investigations of a NACA 0012 airfoil in low Reynolds number flows
(Monterey, California. Naval Postgraduate School, 1992-09)
A steady flow analysis is conducted for a NACA 0012 airfoil in low Reynolds number flows ranging from 540,000 to 1,000,000. Emphasis is placed on prediction and location of the separation bubble. Computational methods ...