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Experimental investigation of the effect of bleed on the aerodynamics of a low-pressure compressor stage in a turbofan engine [GT2023-102260]
The compression system in modern turbofan engines is split into several stages linked by s-shaped transition ducts. Downstream of the low-pressure system, a handling bleed is often required for off-design performance and/or to extract ice/water and foreign debris prior to the air entering the high-p...
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| Main Authors: | , , , |
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| Format: | Default Conference proceeding |
| Published: |
2023
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| Subjects: | |
| Online Access: | https://hdl.handle.net/2134/24065724.v1 |
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