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Flugtriebwerk
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Turboelectric and Hybrid Electric Aircraft Drive Key Performance Parameters
Power Quality Analysis for a High Voltage Power System for Urban Air Mobility Application
Investigation of Rectifier Diode Failures in the NEXT-C Power Processing Unit
Feasibility of a Solid Oxide Fuel Cell System Applied to Hybrid-Electric Regional Aircraft
X-57 Maxwell Battery from Cell Level to System Level Design and Testing
Turboelectric and Hybrid Electric Aircraft Drive Key Performance Parameters
Health Monitoring and Prognostics for More Electric Aircrafts
Power Cable Mass Estimation for Electric Aircraft Propulsion
Design of a High Power Density, High Efficiency, Low THD 250kW Converter for Electric Aircraft
Time-Varying Operating Condition–Based Prediction of the Remaining Useful Life for Aeroengine