Reduction of Unsteady Rotor-Stator Interaction Using Trailing Edge Blowing
An aeroacoustic investigation was performed to assess the effects of adding mass flow at the trailing edges of four stators upstream of an aircraft engine simulator. By using trailing edge blowing to minimize the shed wakes of the stators, the flow into the rotor was made more uniform. In these expe...
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/30527 http://scholar.lib.vt.edu/theses/available/etd-4241161974360/ |