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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
Adaptive Processes for the Aircraft Engines of Tomorrow. What is AdaM doing at the ILA?
A Cryogenically-Cooled MW Inverter for Electric Aircraft Propulsion
Liquid-Hydrogen-Cooled 450-hp Electric Motor Test Stand Being Developed
Electric Motors for Non-Cryogenic Hybrid Electric and Turboelectric Propulsion
A Study on the Use of Solid-Oxide Fuel Cells for Increased Power Generation on Small Aircraft
Electric Motor Considerations for Non-Cryogenic Hybrid Electric and Turboelectric Propulsion
Design and Performance of a Hybrid-Electric Fuel Cell Flight Demonstration Concept