Experimental investigation of vortex shedding in high Reynolds number flow over compressor blades in cascade
Approved for public release, distribution unlimited === An investigation of vortex shedding downstream of a cascade of compressor stator blades, at off-design inlet-flow angles of 35, 33 and 31 degrees and Reynolds numbers, based on chord length, of 625,000, 750,000 and 800,000 is reported. The obj...
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| Format: | Others |
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Monterey, California. Naval Postgraduate School
2012
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| Online Access: | http://hdl.handle.net/10945/1087 |