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Flugtriebwerk
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Modeling and Control Design for a Turboelectric Single Aisle Aircraft Propulsion System
Turboelectric Distributed Propulsion in a Hybrid Wing Body Aircraft
Requirements for a Hydrogen Powered All-Electric Manned Helicopter
Determining the Pressure Gain of Pressure Gain Combustion
Propulsion Technologies for Future Commercial Aircraft
Assessment of Turbulence-Chemistry Interaction Models in the National Combustion Code (NCC) - Part I
LEAPTech/HEIST Experiment Test and Evaluation Summary