Electric power transfer concept for improved performance of multi-spool turbofan jet engine
Twin spool high-bypass turbofan engines are the dominant sources of propulsion for most civil aircraft. The shaft speeds in these engines are thermodynamically coupled even with no mechanical link between them. This coupling effect results in inevitable limitations on the engine design and performan...
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| Format: | Thesis (University of Nottingham only) |
| Language: | English |
| Published: |
2020
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| Online Access: | https://eprints.nottingham.ac.uk/59843/ |