Boundary Layer Control and Wall-Pressure Fluctuations in a Serpentine Inlet
In this thesis, the benefits of boundary layer control (BLC) in improving aerodynamic performance and engine stability were examined in a compact, serpentine inlet exhibiting flow separation. A 1/14-scale turbofan engine simulator provided the flow through the inlet. The inletâ s mass flow was me...
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/32841 http://scholar.lib.vt.edu/theses/available/etd-05162000-11450016/ |