Thermal design of linear induction and synchronous motor for electromagnetic launch of civil aircraft
The engine size of modern passenger transport aircraft is principally determined by take-off conditions, since initial acceleration requires maximum engine power. An elec¬tromagnetic launch (EML) system could provide some or all of the energy required at takeoff so that the aircraft engine power req...
| Main Authors: | , , , , |
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| Format: | Article |
| Published: |
Institute of Electrical and Electronics Engineers
2017
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| Subjects: | |
| Online Access: | https://eprints.nottingham.ac.uk/44031/ |