Pratihar, S.; Ganguly, S.; James, J. A.; Fitzpatrick, M. E. and Edwards, L.
|DOI (Digital Object Identifier) Link:||http://doi.org/10.1080/10238160701374139|
|Google Scholar:||Look up in Google Scholar|
Neutron diffraction has been used to determine the full three dimensional residual stress in a demonstrator variable polarity plasma arc (VPPA) welded Al-7150 skin-stringer fatigue sample. Uniquely, the design of this demonstrator panel took into account the residual stress distribution likely to present due to the presence of the weld by using residual stress data measured on smaller laboratory-sized butt welded plates. The stress-free lattice parameter was obtained by measuring a comb sample and point-to-point strain corrections for the three principal directions were performed to determine strains and hence calculate stresses. A significant amount of stress redistribution was observed in the demonstrator sample when compared to the laboratory size plate specimen.
|Item Type:||Journal Article|
|Keywords:||Neutron diffraction; VPPA; Residual stress; Wing skin panel|
|Academic Unit/Department:||Faculty of Science, Technology, Engineering and Mathematics (STEM) > Engineering and Innovation
Faculty of Science, Technology, Engineering and Mathematics (STEM)
|Depositing User:||Michael E. Fitzpatrick|
|Date Deposited:||16 Dec 2008 08:17|
|Last Modified:||02 Aug 2016 13:13|
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