Non-Intrusive Sensing and Feedback Control of Serpentine Inlet Flow Distortion
A technique to infer circumferential total pressure distortion intensity found in serpentine inlet airflow was established using wall-pressure fluctuation measurements. This sensing technique was experimentally developed for aircraft with serpentine inlets in a symmetric, level flight condition. T...
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/27120 http://scholar.lib.vt.edu/theses/available/etd-04222003-144211/ |