Performance and stalling behavior of an axial-flow compressor subjected to three circumferential inlet distortion levels
<p>The performance and stalling behavior of an axial-flow compressor subjected to several different inlet distortion patterns was investigated. The effect of inlet distortion on overall compressor performance was determined through the measurement of compressor characteristics for each inlet f...
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/43934 http://scholar.lib.vt.edu/theses/available/etd-07282010-020119/ |