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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
Health Monitoring and Prognostics for More Electric Aircrafts
X-57 Maxwell Battery from Cell Level to System Level Design and Testing
Turboelectric and Hybrid Electric Aircraft Drive Key Performance Parameters
Power Cable Mass Estimation for Electric Aircraft Propulsion
Design of a High Power Density, High Efficiency, Low THD 250kW Converter for Electric Aircraft
Overview of NASA GRC Research on Damping of Jet Engine Blades
A Cryogenically-Cooled MW Inverter for Electric Aircraft Propulsion
The science, technology, and implementation of TiAl alloys in commercial aircraft engines
Aeroegine [i.e. aeroengine] noise : December 2 - 4, 2014
Liquid-Hydrogen-Cooled 450-hp Electric Motor Test Stand Being Developed
Electrodynamic Tether as a Thruster for MXER Studies
Electric Motors for Non-Cryogenic Hybrid Electric and Turboelectric Propulsion
Electric Motor Considerations for Non-Cryogenic Hybrid Electric and Turboelectric Propulsion
Design and Performance of a Hybrid-Electric Fuel Cell Flight Demonstration Concept
9x15 Low Speed Wind Tunnel Improvements Update
Impedance Measurements of Motor Drives and Supplies in NASA NEAT Facility
Impedance Measurements of Motor Drives and Supplies in NASA NEAT Facility
Concerning flow about ring shaped cowlings -- 8-further measurements on annular profiles
A Study on the Use of Solid-Oxide Fuel Cells for Increased Power Generation on Small Aircraft
Future Concepts for Modular, Intelligent Aerospace Power Systems
An End-To-End Test of A Simulated Nuclear Electric Propulsion System
New Franklin engine offers increased performance
Attenuation characteristics of four specially designed mufflers tested on practical engine setup
Concerning flow about ring shaped cowlings -- 6-further measurements on inlet devices
A unified analytical approach for the acoustic conceptual design of fans of modern aero-engines
A unified analytical approach for the acoustic conceptual design of fans of modern aero-engines
Electric Motor Noise for Small Quadcopters: Part I - Acoustic Measurements
Generation of desired signals from acoustic drivers
Altitude Performance of J35-A-17 Turbojet Engine in an Altitude Chamber
Assessment of High Temperature Superconducting (HTS) electric motors for rotorcraft propulsion
Impedance Measurements of Motor Drives and Supplies in NASA NEAT Facility
Aeroelastic dynamics of mistuned blade assemblies with closely spaced blade modes
Certification of lightning protection for a full-authority digital engine control
Analytical and experimental validation of the Oblique Detonation Wave Engine concept
The all-electric aircraft - A systems view and proposed NASA research Programs