2017
DOI: 10.1016/j.ijfatigue.2016.08.010
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Multiaxial fatigue assessment of friction stir welded tubular joints of Al 6082-T6

Abstract: ReuseThis article is distributed under the terms of the Creative Commons Attribution-NonCommercial-NoDerivs (CC BY-NC-ND) licence. This licence only allows you to download this work and share it with others as long as you credit the authors, but you can't change the article in any way or use it commercially. More information and the full terms of the licence here: https://creativecommons.org/licenses/ AbstractThe present paper addresses the problem of designing aluminium friction stir (FS) welded joints again… Show more

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Cited by 33 publications
(16 citation statements)
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References 61 publications
(105 reference statements)
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“…The data from tests at R = −1 (categories C1 and C1H) show that the reference stress range Δ σ A,97.7% is almost halved for tubes compared with flat plate specimens, from 123 MPa (C1) to 56 MPa (C1H). This marked decrease in strength is primarily attributed to the notch effect caused by the slight undercut at the edge of the weld zone arising from the tool shoulder . An average notch root radius of about 0.5 mm was measured by Susmel et al, on both the advancing and the retreating side of the weld, which led to a local stress concentration factor of 2.4 in axial loading and 1.7 in torsion.…”
Section: Introductionmentioning
confidence: 95%
“…The data from tests at R = −1 (categories C1 and C1H) show that the reference stress range Δ σ A,97.7% is almost halved for tubes compared with flat plate specimens, from 123 MPa (C1) to 56 MPa (C1H). This marked decrease in strength is primarily attributed to the notch effect caused by the slight undercut at the edge of the weld zone arising from the tool shoulder . An average notch root radius of about 0.5 mm was measured by Susmel et al, on both the advancing and the retreating side of the weld, which led to a local stress concentration factor of 2.4 in axial loading and 1.7 in torsion.…”
Section: Introductionmentioning
confidence: 95%
“…Aluminum alloy is widely used in aerospace, automotive and marine industries. [6] According to relevant data [7,8] fatigue failure of parts accounts for 50 to 90% of all failures in manufactured parts in general. The FSW method improved the fatigue performance by~2.4 times in comparison with the single riveting method commonly used in aerospace, and reduced the overlap area in the double riveting method, while ensuring the fatigue strength and mechanical properties.…”
Section: Introductionmentioning
confidence: 99%
“…About 50-90 % of structural and mechanical assembly's in-service failures have been attributed to fatigue failures [12]. Welds or joints are often predominantly sensitive to fatigue loads due to their inherent residual stress level [13], microstructural variations, and the presence of inclusions and blowholes (micro or coarse pores).…”
Section: Introductionmentioning
confidence: 99%