Wind Tunnel Simulation of Flow Control With Pulsed Impinging Air Jets

Dunne, Reeve

The technology of natural laminar flow airfoils presents an opportunity to vastly increase the efficiency of aircraft by decreasing the friction drag on the wing during flight. These airfoils however are much more susceptible to flow separation and stall conditions resulting in increased drag and loss of lift on the airfoil. Flow control represents a possibility to prevent separation on these airf... read more

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Undergraduate honors theses
Department of Mechanical Engineering
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