The influence of fan root flow on the aerodynamics of a low-pressure compressor transition duct
To reduce fuel-burn and CO2 emissions from aero gas turbines there is a drive towards very-high bypass ratio and smaller ultra-high-pressure ratio core engine technologies. However, this makes the design of the ducts connecting various compressor spools more challenging as the higher required radius...
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| Main Authors: | , , , , |
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| Format: | Default Conference proceeding |
| Published: |
2019
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| Subjects: | |
| Online Access: | https://hdl.handle.net/2134/37468 |
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