Design and implementation of an innovative airborne electric propulsion measure system of fixed-wing UAV

Zhao, A, Zhang, J, Li, K et al. (1 more author) (2021) Design and implementation of an innovative airborne electric propulsion measure system of fixed-wing UAV. Aerospace Science and Technology, 109. 106357. ISSN 1270-9638

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Authors/Creators:
Copyright, Publisher and Additional Information: © 2020 Elsevier Masson SAS. All rights reserved. This is an author produced version of an article published in Aerospace Science and Technology. Uploaded in accordance with the publisher's self-archiving policy.
Keywords: Airborne electric propulsion test system; Efficiency parameters; Flight test; Wind tunnel experiment; Fixed-wing unmanned aerial vehicle (UAV)
Dates:
  • Published: February 2021
  • Accepted: 8 November 2020
  • Published (online): 26 November 2020
Institution: The University of Leeds
Academic Units: The University of Leeds > Faculty of Engineering & Physical Sciences (Leeds) > School of Chemical & Process Engineering (Leeds)
Depositing User: Symplectic Publications
Date Deposited: 05 May 2021 10:35
Last Modified: 05 May 2021 10:35
Status: Published
Publisher: Elsevier
Identification Number: https://doi.org/10.1016/j.ast.2020.106357
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Licence: CC-BY-NC-ND 4.0

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