Development of a geometric model for the study of propagating stall inception based on flow visualization in a linear cascade
Flow visualization movies of flow through a cascade of compressor blades showed propagating stall at stagger angles of 36.5 and 45 degrees for angles of attack of 20 degrees and higher. At a stagger angle of 25 degrees, the development of a steady, separated boundary layer occurred with no propagati...
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Format: | Others |
Language: | en_US |
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Virginia Polytechnic Institute and State University
2017
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Online Access: | http://hdl.handle.net/10919/76198 |