Aeroelastic assessment of cracked composite plate by means of fully coupled finite element and Doublet Lattice Method

Abdullah, N.A., Curiel-Sosa, J.L. orcid.org/0000-0003-4437-1439 and Akbar, M. (2018) Aeroelastic assessment of cracked composite plate by means of fully coupled finite element and Doublet Lattice Method. Composite Structures. ISSN 0263-8223

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Copyright, Publisher and Additional Information: © 2018 Elsevier. 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: Flutter; Crack; Composite; Mori-Tanaka; Doublet Lattice Method; FEM
Dates:
  • Published (online): 9 January 2018
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: 25 Jan 2018 15:00
Last Modified: 09 Jan 2019 01:38
Published Version: https://doi.org/10.1016/j.compstruct.2018.01.015
Status: Published online
Publisher: Elsevier
Refereed: Yes
Identification Number: https://doi.org/10.1016/j.compstruct.2018.01.015

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