Stability Enhancement of a Single-Stage Transonic Axial Compressor Using Inclined Oblique Slots
A casing treatment using inclined oblique slots (INOS) is proposed to improve the stability of the single-stage transonic axial compressor, NASA Stage 37, during operation. The slots are installed on the casing of the rotor blades. The aerodynamic performance was estimated using three-dimensional st...
Main Authors: | , |
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Format: | Article |
Language: | English |
Published: |
MDPI AG
2021-04-01
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Series: | Energies |
Subjects: | |
Online Access: | https://www.mdpi.com/1996-1073/14/9/2346 |