System Weight Comparison of Electric Machine Topologies for Electric Aircraft Propulsion-Reference-Cited by-同舟云学术

System Weight Comparison of Electric Machine Topologies for Electric Aircraft Propulsion

Published:2018-07-08 Issue: Volume: Page:
ISSN:
Container-title:2018 AIAA/IEEE Electric Aircraft Technologies Symposium
language:
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Author:

Anderson Aaron D.¹,Renner Nathaniel J.¹,Wang Yuyao¹,Lee Dongsu¹,Agrawal Shivang¹,Sirimanna Samith¹,Haran Kiruba¹,Banerjee Arijit¹,Starr Matthew J.²,Felder James L.³

Affiliation:

1. University of Illinois, Urbana-Champaign

2. Rolls-Royce Group plc

3. NASA Glenn Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2018-4983

Reference26 articles.

1. Overview of NASA Electrified Aircraft Propulsion (EAP) Research for Large Subsonic Transports

2. Turboelectric Aircraft Drive Key Performance Parameters and Functional Requirements

3. Overview of Electric Motor Technologies Used for More Electric Aircraft (MEA)

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