Analysis on cracked commuter aircraft wing under dynamic cruise load by means of XFEM

Wirawan, N., Abdullah, N.A., Akbar, M. et al. (1 more author) (2018) Analysis on cracked commuter aircraft wing under dynamic cruise load by means of XFEM. In: Journal of Physics: Conference Series. Modern Practice in Stress and Vibration Analysis (MPSVA) 2018, 02-04 Jul 2018, Cambridge, UK. IOP Publishing .

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Copyright, Publisher and Additional Information: © 2018 IOP Publishing. Content from this work may be used under the terms of the Creative Commons Attribution 3.0 licence (https://creativecommons.org/licenses/by/3.0/). Any further distribution of this work must maintain attribution to the author(s) and the title of the work, journal citation and DOI.
Dates:
  • Accepted: 25 May 2018
  • Published (online): 5 November 2018
  • Published: 5 November 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: 14 Jun 2018 11:06
Last Modified: 13 Dec 2018 12:25
Published Version: https://doi.org/10.1088/1742-6596/1106/1/012014
Status: Published
Publisher: IOP Publishing
Refereed: Yes
Identification Number: https://doi.org/10.1088/1742-6596/1106/1/012014

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