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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| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Isfahan University of Technology
2025-03-01
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| Series: | Journal of Applied Fluid Mechanics |
| Subjects: | |
| Online Access: | https://www.jafmonline.net/article_2633_56b2ca6bdda9d139cf669eb33738bf6d.pdf |
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