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...

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Autors principals:	X. Chen, Z. Li, Y. Cong, W. Wu, M. Wang, Z. Wang
Format:	Artigo
Idioma:	Inglês
Publicat:	Isfahan University of Technology 2026-04-01
Col·lecció:	Journal of Applied Fluid Mechanics
Matèries:	transonic compressor aerodynamic performance blade notch damage leakage vortex flow loss shock wave
Accés en línia:	https://www.jafmonline.net/article_2907_c7558e9d1f956b016d1fdba7ea132378.pdf
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