Modeling, Manufacturing, and Experimental Validation of an Electric Machine for Aircraft Propulsion
The work presented in this thesis is part of an effort at MIT to develop a 1-MW electric machine which achieves the specific power necessary for hybrid-electric aviation: 13 kW/kg [1]. The models for torque and core loss used in the design of the 1-MW machine are revised and expanded based on experi...
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| Format: | Thesis |
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Massachusetts Institute of Technology
2024
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| Online Access: | https://hdl.handle.net/1721.1/153873 |