This is a repository copy of Numerical inspection based on quasi-static analysis using Rousselier damage model for aluminium wingbox aircraft structure . White Rose Research Online URL for this paper: http://eprints.whiterose.ac.uk/140811/ Version: Published Version Proceedings Paper: Ahmad, M.I.M., Curiel-Sosa, J.L., Akbar, M. et al. (1 more author) (2018) Numerical inspection based on quasi-static analysis using Rousselier damage model for aluminium wingbox aircraft structure. In: Journal of Physics: Conference Series. Modern Practice in Stress and Vibration Analysis (MPSVA) 2018, 02-04 Jul 2018, Cambridge, United Kingdom. IOP Publishing . https://doi.org/10.1088/1742-6596/1106/1/012013 [email protected] https://eprints.whiterose.ac.uk/ Reuse This article is distributed under the terms of the Creative Commons Attribution (CC BY) licence. This licence allows you to distribute, remix, tweak, and build upon the work, even commercially, as long as you credit the authors for the original work. More information and the full terms of the licence here: https://creativecommons.org/licenses/ Takedown If you consider content in White Rose Research Online to be in breach of UK law, please notify us by emailing [email protected] including the URL of the record and the reason for the withdrawal request.
Numerical inspection based on quasi-static analysis using Rousselier damage model for aluminium wingbox aircraft structure
Jun 16, 2023
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