Piezoelectric energy harvester composite under dynamic bending with implementation to aircraft wingbox structure

Akbar, M. orcid.org/0000-0001-7998-0846 and Curiel-Sosa, J.L. (2016) Piezoelectric energy harvester composite under dynamic bending with implementation to aircraft wingbox structure. Composite Structures, 153. pp. 193-203. ISSN 0263-8223

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Authors/Creators:
Copyright, Publisher and Additional Information: © 2016 Elsevier Ltd. This is an author produced version of a paper subsequently published in Composite Structures. Uploaded in accordance with the publisher's self-archiving policy. Article available under the terms of the CC-BY-NC-ND licence (https://creativecommons.org/licenses/by-nc-nd/4.0/)
Keywords: Piezoelectric; Energy harvester; Dynamic bending; Aircraft wingbox
Dates:
  • Published: 1 October 2016
  • Accepted: 3 June 2016
  • Published (online): 4 June 2016
Institution: The University of Sheffield
Academic Units: The University of Sheffield > Faculty of Engineering (Sheffield) > Department of Mechanical Engineering (Sheffield)
Depositing User: Symplectic Sheffield
Date Deposited: 13 Sep 2016 15:36
Last Modified: 02 Jul 2017 09:45
Published Version: http://dx.doi.org/10.1016/j.compstruct.2016.06.010
Status: Published
Publisher: Elsevier
Refereed: Yes
Identification Number: https://doi.org/10.1016/j.compstruct.2016.06.010

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