Effectiveness of a Serpentine Inlet Duct Flow Control Scheme at Design and Off-Design Simulated Flight Conditions
An experimental investigation was conducted in a static ground test facility to determine the flow quality of a serpentine inlet duct incorporating active flow control for several simulated flight conditions. The total pressure distortion at the aerodynamic interface plane (AIP) was then used to pr...
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/28653 http://scholar.lib.vt.edu/theses/available/etd-08142003-225036/ |