A Tool for Modeling and Analysis of Electrified Aircraft Power Systems-Reference-Cited by-同舟云学术

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A Tool for Modeling and Analysis of Electrified Aircraft Power Systems

Published:2019-08-16 Issue: Volume: Page:
ISSN:
Container-title:AIAA Propulsion and Energy 2019 Forum
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Author:

Hanlon Patrick¹,Thomas George L.¹,Csank Jeffrey¹,Sadey David J.¹

Affiliation:

1. NASA Glenn Research Center

Publisher

American Institute of Aeronautics and Astronautics

Reference11 articles.

1. Bradley, M. K. and Droney, C. K. "Subsonic Ultra Green Aircraft Research Phase II: Hybrid Electric Design Exploration," Contractor Report NASA/CR-2015-218704/Volume II, NASA Langley Research Center, Hampton, VA, April 2015.

2. A Review of Distributed Electric Propulsion Concepts for Air Vehicle Technology

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2. A Modelling Design Framework for Integrated Electrical Power and Non-Electrical Systems Design on Electrical Propulsion Aircraft;2022 IEEE Transportation Electrification Conference & Expo (ITEC);2022-06-15

3. High-Level Integration Sizing Tool for Electrical Architectures (HighLITE);2022 IEEE Transportation Electrification Conference & Expo (ITEC);2022-06-15

4. NASA concept vehicles and the engineering of advanced air mobility aircraft;The Aeronautical Journal;2021-10-13

5. A Modelling Framework for Efficient Design of Electrical Power Systems for Electrical Propulsion Aircraft;AIAA Propulsion and Energy 2021 Forum;2021-07-28

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