Dorman, M.; Toparli, M. B.; Smyth, N.; Cini, A.; Fitzpatrick, M. E. and Irving, P. E.
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|DOI (Digital Object Identifier) Link:||http://doi.org/10.1016/j.msea.2012.04.002|
|Google Scholar:||Look up in Google Scholar|
Laser peening at a range of power densities has been applied to 2-mm-thick sheets of 2024 T351 aluminium. The induced residual stress field was measured using incremental hole drilling and synchrotron X-ray diffraction techniques. Fatigue samples were subjected to identical laser peening treatments followed by scribing at the peen location to introduce stress concentrations, after which they were fatigue tested. The residual stresses were found to be non-biaxial: orthogonal to the peen line they were tensile at the surface, moving into the desired compression with increased depth. Regions of peen spot overlap were associated with large compression strains; the centre of the peen spot remaining tensile. Fatigue lives showed moderate improvement over the life of unpeened samples for 50 μm deep scribes, and slight improvement for samples with 150 μm scribes. Use of the residual stress intensity Kresid approach to calculate fatigue life improvement arising from peening was unsuccessful at predicting the relative effects of the different peening treatments. Possible reasons for this are explored.
|Item Type:||Journal Article|
|Copyright Holders:||2012 Elsevier B.V.|
|Keywords:||laser peening; aluminium sheet; fatigue; residual stresses; crack growth|
|Academic Unit/Department:||Faculty of Science, Technology, Engineering and Mathematics (STEM)
Faculty of Science, Technology, Engineering and Mathematics (STEM) > Engineering and Innovation
|Depositing User:||Michael E. Fitzpatrick|
|Date Deposited:||18 Apr 2012 13:26|
|Last Modified:||04 Aug 2016 14:07|
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