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About Computational prediction of airfoil dynamic stall
Abstract—The term dynamic stall refers to unsteady flow separation occurring on aerodynamic bodies, such as . Dynamic stall events on a NACA-0012 airfoil at low free-stream Mach number [from Ref. (10)] and Reding or to use Theodorsen's flat plate theory, as applied by Tyler and Leish- man.
Detailed Information
| Author: | Unknown |
|---|---|
| Publication Year: | 1997 |
| Pages: | 89 |
| Language: | English |
| File Size: | 4.68 |
| Format: | |
| Price: | FREE |
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