Assessment of the Impact of an Advanced Power System on a Turboelectric Single-Aisle Concept Aircraft
Author:
Affiliation:
1. NASA Glenn Research Center
2. NASA Ames Research Center
3. NASA Armstrong Flight Research Center
4. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Reference17 articles.
1. VTOL Urban Air Mobility Concept Vehicles for Technology Development
2. Conceptual Design of a Single-Aisle Turboelectric Commercial Transport with Fuselage Boundary Layer Ingestion
3. Turboelectric Aircraft Drive Key Performance Parameters and Functional Requirements
4. Parallel Hybrid Gas-Electric Geared Turbofan Engine Conceptual Design and Benefits Analysis
5. High Efficiency Megawatt Motor Conceptual Design
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