Noise Reduction in an Axisymmetric Supersonic Aircraft Inlet using Trailing Edge Blowing
Acoustic experiments were conducted in an anechoic chamber with a 1/14th scale model of a supersonic aircraft engine inlet using Trailing Edge Blowing (TEB) to reduce the engine fan noise from a turbofan propulsion simulator (TPS). The TPS is 4.1 in. (10.4 cm) in diameter and is powered by compress...
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/31385 http://scholar.lib.vt.edu/theses/available/etd-02898-16741/ |