Investigation of the Effect of Vortex Generators on Flow Separation in a Supersonic Compressor Cascade
The interaction between a shock wave and a boundary layer promotes corner separation and prevents performance enhancement in a supersonic compressor cascade. Different vortex generator (VG) designs are presented to control corner separation in a supersonic compressor cascade, including endwall VGs (...
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| Glavni autori: | , , , |
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| Format: | Artigo |
| Jezik: | Inglês |
| Izdano: |
MDPI AG
2025-07-01
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| Serija: | Aerospace |
| Teme: | |
| Online pristup: | https://www.mdpi.com/2226-4310/12/8/692 |
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