High Efficiency Megawatt Motor Conceptual Design-Reference-Cited by-同舟云学术

High Efficiency Megawatt Motor Conceptual Design

Published:2018-07-08 Issue: Volume: Page:
ISSN:
Container-title:2018 Joint Propulsion Conference
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Author:

Jansen Ralph¹,De Jesus-Arce Yaritza¹,Kascak Peter¹,Dyson Rodger W.¹,Woodworth Andrew¹,Scheidler Justin J.¹,Edwards Ryan¹,Stalcup Erik J.¹,Wilhite Jarred¹,Duffy Kirsten P.²,Passe Paul³,McCormick Sean³

Affiliation:

1. NASA Glenn Research Center

2. University of Toledo

3. Vantage Partners, LLC

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2018-4699

Reference6 articles.

1. Conceptual Design of a Single-Aisle Turboelectric Commercial Transport with Fuselage Boundary Layer Ingestion

2. Turboelectric Aircraft Drive Key Performance Parameters and Functional Requirements

3. Partially Turboelectric Aircraft Drive Key Performance Parameters

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