Experimental investigation on vortex shedding in flow over second-generation, controlled-diffusion, compressor blades in cascade
Approved for public release, distribution unlimited === An investigation of vortex shedding downstream of a cascade of second-generation, controlled-diffusion, compressor stator blades, at off-design inlet-flow angles of 31, 33 and 35 degrees and Reynolds numbers, based on chord length, of 280,000,...
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Monterey, California. Naval Postgraduate School
2012
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| Online Access: | http://hdl.handle.net/10945/6092 |