The Effects of Free Stream Turbulence on the Flow Field through a Compressor Cascade
The flow through a compressor cascade with tip leakage has been studied experimentally. The cascade of GE rotor B section blades had an inlet angle of 65.1º, a stagger angle of 56.9º, and a solidity of 1.08. The final turning angle of the cascade was 11.8º. This compressor configuration was re...
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/28753 http://scholar.lib.vt.edu/theses/available/etd-08222002-194441/ |