Thermal design of linear induction and synchronous motor for electromagnetic launch of civil aircraft

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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...

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Bibliographic Details
Main Authors:	Bertola, Luca, Cox, Tom, Wheeler, Patrick, Garvey, Seamus D., Morvan, Herve
Format:	Article
Published:	Institute of Electrical and Electronics Engineers 2017
Subjects:	Civil aircraft Electromagnetic launch (EML)/ EMLs Electromagneticcatapult Linear inductionmotor Linear synchronous motor Thermal analysis
Online Access:	https://eprints.nottingham.ac.uk/44031/

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