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Flugtriebwerk
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Turboelectric and Hybrid Electric Aircraft Drive Key Performance Parameters
Design of a High Power Density, High Efficiency, Low THD 250kW Converter for Electric Aircraft
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
Power Cable Mass Estimation for Electric Aircraft Propulsion
Health Monitoring and Prognostics for More Electric Aircrafts
Turboelectric and Hybrid Electric Aircraft Drive Key Performance Parameters
Adaptive Processes for the Aircraft Engines of Tomorrow. What is AdaM doing at the ILA?