Aerodynamic forces induced by controlled transitory flow on a body of revolution
The aerodynamic forces and moments on an axisymmetric body of revolution are controlled in a low-speed wind tunnel by induced local flow attachment. Control is effected by an array of aft-facing synthetic jets emanating from narrow, azimuthally segmented slots embedded within an axisymmetric backwar...
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Georgia Institute of Technology
2012
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| Online Access: | http://hdl.handle.net/1853/42830 |