Active Flow Control Using Synthetic Jet Actuation
The influence of periodic excitation from synthetic jet actuators, SJA, on boundary layer separation and reattachment over a NACA 0025 airfoil at a low Reynolds number is studied. All experiments reported are performed in a low-turbulence recirculating wind tunnel at a Reynolds number of 100000 and...
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| Language: | en_ca |
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2010
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| Online Access: | http://hdl.handle.net/1807/25715 |