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Flugtriebwerk
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A Cryogenically-Cooled MW Inverter for Electric Aircraft Propulsion
An advanced pitch change mechanism incorporating a hybrid traction drive
An End-To-End Test of A Simulated Nuclear Electric Propulsion System
A Study on the Use of Solid-Oxide Fuel Cells for Increased Power Generation on Small Aircraft
Certification of lightning protection for a full-authority digital engine control
Certification of Lightning Protection for a Full-Authority Digital Engine Control
Classifier performance measures in multi-fault diagnosis for aircraft engines
Conceptual design of an optic based engine control system
Considerations of the all electric (accessory) engine concept
Demonstrating the more electric engine: a step towards the power optimised aircraft
Design and Performance of a Hybrid-Electric Fuel Cell Flight Demonstration Concept
Design of a High Power Density, High Efficiency, Low THD 250kW Converter for Electric Aircraft
Development of the S-76B/PT6B-36B engine acceleration schedule
Development Plan for Nj-18A Power Package Flight Test Program, 1963--1967
Electric Motor Considerations for Non-Cryogenic Hybrid Electric and Turboelectric Propulsion
Electric Motor Noise for Small Quadcopters: Part I - Acoustic Measurements
Electric Motors for Non-Cryogenic Hybrid Electric and Turboelectric Propulsion
External Requirements for Electrified Commuter Aircraft
Factoring a priori classifier performance into decision fusion
Fault Signal Analysis for Aircraft Generator Rectifier
Feasibility of a Solid Oxide Fuel Cell System Applied to Hybrid-Electric Regional Aircraft
Flight Evaluation of an Advanced Engine Display and Monitoring System
Flight test validation of the dynamic model of a fuel cell system for ultra-light aircraft
Fuel cell-based powertrain system modeling and simulation for small aircraft propulsion applications
Future Concepts for Modular, Intelligent Aerospace Power Systems
Generation of desired signals from acoustic drivers
Health Monitoring and Prognostics for More Electric Aircrafts
HTS motors in aircraft propulsion: design considerations