Structural design and experimental verification of a novel split aileron wing

Zhao, A, He, D and Wen, D orcid.org/0000-0003-3492-7982 (2020) Structural design and experimental verification of a novel split aileron wing. Aerospace Science and Technology, 98. 105635. ISSN 1270-9638

Abstract

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Authors/Creators:
Copyright, Publisher and Additional Information: © 2019 Elsevier Masson SAS. This is an author produced version of a paper published in Aerospace Science and Technology. Uploaded in accordance with the publisher's self-archiving policy.
Keywords: Split aileron; Aerodynamic performance; Structural weight; Function prototype; Flight test
Dates:
  • Published: March 2020
  • Accepted: 9 December 2019
  • Published (online): 18 December 2019
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: 23 Jan 2020 14:43
Last Modified: 18 Dec 2020 01:38
Status: Published
Publisher: Elsevier BV
Identification Number: https://doi.org/10.1016/j.ast.2019.105635

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