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Flugtriebwerk
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Turboelectric and Hybrid Electric Aircraft Drive Key Performance Parameters
Continued Exploration of the Electrified Aircraft Propulsion Design Space
Electrified Aircraft Propulsion Controls Hardware Testing
NASA’s Quiet Electric ENgines (QUEEN): Summary of the QUEEN V2 Test
Electrical Propulsive Fuselage Concept for Transonic Transport Aircraft
Considering Turbofan Operability in Hybrid Electric Aircraft Propulsion System Design
Design of a High Power Density, High Efficiency, Low THD 250kW Converter for Electric Aircraft
Additive Manufacture of Refractory Metal Green Propulsion Thrusters
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
Cruise Propulsion System Thermal Analysis for NASA’s X-57 “Maxwell” Mod II Configuration
Design of a Magnetic Gear for NASA's Vertical Lift Quadrotor Concept Vehicle
Feasibility of a Solid Oxide Fuel Cell System Applied to Hybrid-Electric Regional Aircraft
Propulsion System Optimization for a Turboelectric Tiltwing Urban Air Mobility Aircraft
Resonance and Tones in Dual-Stream Nozzle Flows
Modeling Turboshaft Engines for the Revolutionary Vertical Lift Technology Project