An Approach for Utilizing Power Flow Modeling for Simulations of Hybrid Electric Propulsion Systems
Author:
Affiliation:
1. NASA Glenn Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-5018
Reference17 articles.
1. Overview of NASA Electrified Aircraft Propulsion (EAP) Research for Large Subsonic Transports
2. Aeropropulsive Interaction and Thermal System Integration within the ECO-150: A Turboelectric Distributed Propulsion Airliner with Conventional Electric Machines
3. Conceptual Design of a Single-Aisle Turboelectric Commercial Transport with Fuselage Boundary Layer Ingestion
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