Impact of Identical Volume Notch Damage at Different Locations of Rotor Blades on the Aerodynamic Performance of Transonic Compressors
This study aims to provide data and theoretical support for evaluating the aerodynamic performance of compressors with blade notch damage under operational conditions. Taking the NASA Rotor37 transonic axial compressor rotor blade as the research object, it incorporates the characteristics of damage...
Kaydedildi:
| Asıl Yazarlar: | , , , , , |
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| Materyal Türü: | Artigo |
| Dil: | Inglês |
| Baskı/Yayın Bilgisi: |
Isfahan University of Technology
2026-04-01
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| Seri Bilgileri: | Journal of Applied Fluid Mechanics |
| Konular: | |
| Online Erişim: | https://www.jafmonline.net/article_2907_c7558e9d1f956b016d1fdba7ea132378.pdf |
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