Performance Enhancement of a Transonic Axial Flow Compressor with Circumferential Casing Grooves to Improve the Stall Margin
The stability range of the gas turbine engine compressors is being challenged in the modern days due to the intention of increasing per stage maximum loading. Casing treatment has been widely adopted as a realistic passive flow control means to improve the stall margin with a slight decrease of effi...
Main Authors: | , , , , |
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Format: | Article |
Language: | English |
Published: |
Isfahan University of Technology
2020-01-01
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Series: | Journal of Applied Fluid Mechanics |
Subjects: | |
Online Access: | http://jafmonline.net/JournalArchive/download?file_ID=50602&issue_ID=1004 |