Experiment and Numerical Simulation of Aerodynamic Performance of Compressor with Damaged Blades

The present work attempted to lay a basis for evaluating the compressor aerodynamic performance in service environments. To achieve this goal, a low-speed compressor along with a transonic compressor rotor (NASA Rotor37) were studied. Different damaged blades were established, and three-dimensional...

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Bibliographic Details
Main Authors: H. Sun, Z. Wang, G. Luo
Format: Article
Language:English
Published: Isfahan University of Technology 2025-03-01
Series:Journal of Applied Fluid Mechanics
Subjects:
Online Access:https://www.jafmonline.net/article_2633_56b2ca6bdda9d139cf669eb33738bf6d.pdf
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