Blade-end treatment to improve the performance of axial compressors: An overview
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Mechanical Engineering,Mechanics of Materials,Aerospace Engineering
Reference72 articles.
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2. Loss reduction in axial-flow compressors through low-speed model testing;Wisler;ASME J. Eng. Gas. Turbines Power,1985
3. Highly loaded axial flow compressors: history and current developments;Wennerstrom;ASME J. Turbomach.,1990
4. Numerical investigation of end wall boundary layer removal on highly loaded axial compressor blade rows;Gümmer;ASME J. Turbomach.,2008
5. Effect of tip clearance flow on compressor stability and engine performance;Freeman;VKI Lect. Ser.,1985
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