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Effects of Shrouded Stator Cavity Flows on Multistage Axial Compressor Aerodynamic Performance by National Aeronautics and Space Adm Nasa

Effects of Shrouded Stator Cavity Flows on Multistage Axial Compressor Aerodynamic Performance

National Aeronautics and Space Adm Nasa

142 pages missing pub info (view editions)

nonfiction science informative slow-paced
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Experiments were performed on a low-speed multistage axial-flow compressor to assess the effects of shrouded stator cavity flows on aerodynamic performance. Five configurations, which involved changes in seal-tooth leakage rates and/or elimination...

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