DOI | Resolve DOI: https://doi.org/10.4028/www.scientific.net/AMR.996.794 |
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Author | Search for: Bach, Michael; Search for: Merati, Ali1; Search for: Gharghouri, Michael |
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Affiliation | - National Research Council of Canada. Aerospace
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Format | Text, Article |
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Conference | 9th European Conference on Residual Stresses, ECRS 2014, 7 July 2014 through 10 July 2014, Troyes |
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Subject | Fatigue of materials; Fatigue testing; Fracture mechanics; Joints (structural components); Neutron diffraction; Nondestructive examination; Stringers; Welding; Crack nucleation; Fatigue performance; Friction stir; Lap joint; Structural failure; Tri-axial; Residual stresses |
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Abstract | This research uses a non-destructive method of neutron diffraction to measure the tri-axial residual stresses in a friction stir welded aerospace fuselage component: a stringer-to-skin lap joint. Two different specimens were examined. Fatigue testing was performed on both specimens to determine their fatigue lives. Effects of the different components of residual stresses were examines and related to fatigue performance. A combination of fractography, hardness testing, and residual stress measurement was used to predict areas of high probability of structural failure in the friction stir welded lap joints. |
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Publication date | 2014-08 |
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In | |
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Language | English |
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Peer reviewed | Yes |
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NPARC number | 21272618 |
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Export citation | Export as RIS |
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Report a correction | Report a correction (opens in a new tab) |
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Record identifier | 06eb4716-4c95-4046-97f6-7e05e2b9ba5e |
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Record created | 2014-12-03 |
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Record modified | 2020-04-22 |
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