Comparative Analysis of Serrated Trailing Edge Designs on Idealized Aircraft Engine Fan Blades for Noise Reduction
The effects of serrated trailing edge designs, designed for noise reduction, on the flow-field downstream of an idealized aircraft engine fan blade row were investigated in detail. The measurements were performed in the Virginia Tech low speed linear cascade tunnel on one set of baseline GE-Rotor-B...
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Virginia Tech
2014
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Online Access: | http://hdl.handle.net/10919/40542 http://scholar.lib.vt.edu/theses/available/etd-01102005-202530/ |