Flow control via synthetic jet actuation
An experimental investigation was undertaken to determine the ability of Synthetic Jet Actuators to control the aerodynamic properties of a wing. The Synthetic Jet Actuator (SJA) was placed at two separate positions on a wing comprised of a NACA0015 airfoil. The first of the jet positions is located...
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Format: | Others |
Language: | en_US |
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Texas A&M University
2005
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Online Access: | http://hdl.handle.net/1969.1/1409 |