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Luftfahrzeug
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ANOPP2 Training Part 2 of 4: Aircraft System Noise Prediction
Turboelectric and Hybrid Electric Aircraft Drive Key Performance Parameters
NASA Power and Thermal Technology Overview
Analysis of a Stretched Derivative Aircraft with Open Rotor Propulsion
Revolutionary Vertical Lift Technology (RVLT)
Real-Time Hardware-in-the-Loop Evaluation of A Partially Turboelectric Propulsion Control Design
Electrified Aircraft Propulsion Flight Project Motor & Inverter Industry Day
System Noise Prediction of the DGEN 380 Turbofan Engine
Advances in Aircraft System Identification at NASA Langley Research Center
Overview of NASA GRC Electrified Aircraft Propulsion (EAP) Controls Research
Conceptual Exploration of Aircraft Configurations for the SUSAN Electrofan
System Noise Prediction of the DGEN 380 Turbofan Engine
Electrified Aircraft Propulsion Controls Hardware Testing
Initial Regulatory and Certification Approach for the SUSAN Electrofan Concept
Vision for H2 Aircraft Technology Development
Implementation Approach for an Electrified Aircraft Concept Vehicle in a Research Flight Simulator
NASA Meeting on Cryogenic Fuel Systems for Aircraft: Overview of Previous Workshops and Studies
Real-time Hardware-in-the-Loop Evaluation of a Partially Turboelectric Propulsion Control Design