Structural Integrity Assessment on Cracked Composite Plate under Aeroelastic Loading by means of XFEM

Abdullah, N.A., Curiel-Sosa, J.L. orcid.org/0000-0003-4437-1439, Wirawan, N. et al. (1 more author) (Accepted: 2018) Structural Integrity Assessment on Cracked Composite Plate under Aeroelastic Loading by means of XFEM. In: Proceedings of the 6th International Conference on Integrity – Reliability -Failure. 6th International Conference on Integrity – Reliability -Failure, 22-26 Jul 2018, Lisbon, Portugal. , Lisbon, Portugal .

Abstract

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Authors/Creators:
Copyright, Publisher and Additional Information: © 2018 IRF
Keywords: flutter; composite; time-domain response; aerodynamic load; XFEM
Dates:
  • Accepted: 5 June 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 11:58
Last Modified: 14 Jun 2018 11:58
Status: Published
Refereed: Yes

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Filename: Ref 7207-STRUCTURAL INTEGRITY ASSESSMENT ON CRACKED COMPOSITE PLATE UNDER AEROELASTIC LOADING BY MEANS OF XFEM_nw.pdf

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