Investigation of the effect of Reynolds number on laminar separation bubbles on controlled-diffusion compressor blades in cascade
Approved for public release; distribution is unlimited === Detailed experimental investigation of second generation, controlled diffusion, compressor stator blades at an off-design inlet flow angle was performed in a low speed cascade wind tunnel using various experimental procedures. The objective...
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| Language: | en_US |
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Monterey, California. Naval Postgraduate School
2012
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| Online Access: | http://hdl.handle.net/10945/8578 |