2015
DOI: 10.1016/j.ijfatigue.2015.05.003
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Fatigue strength evaluation of self-piercing riveted Al-5052 joints under different specimen configurations

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Cited by 37 publications
(30 citation statements)
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“…Figure shows the load amplitude, P amp (= (P max − P min ) / 2), against the number of cycles to failure, N f . Fatigue test results for U.A–L.A with the same Al‐5052 alloy sheet are included for comparison . The results show a relationship between the applied load amplitude and number of cycles, Pamp=20589Nfprefix−0.215 and Pamp=5131Nfprefix−0.087 for the U.S–L.A and U.A–L.S specimens, respectively.…”
Section: Resultsmentioning
confidence: 99%
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“…Figure shows the load amplitude, P amp (= (P max − P min ) / 2), against the number of cycles to failure, N f . Fatigue test results for U.A–L.A with the same Al‐5052 alloy sheet are included for comparison . The results show a relationship between the applied load amplitude and number of cycles, Pamp=20589Nfprefix−0.215 and Pamp=5131Nfprefix−0.087 for the U.S–L.A and U.A–L.S specimens, respectively.…”
Section: Resultsmentioning
confidence: 99%
“…SPR joints generally experience multiaxial stresses during fatigue loading. Recently, Kang and Kim tried to predict the fatigue lifetimes of SPR joints with different specimen configurations by adopting several fatigue parameters, such as the von Mises stress, maximum principal stress, and SWT (Smith–Watson–Topper) fatigue parameter . However, none of the parameters were sufficient to correlate the fatigue lifetimes of SPR joints for various types of specimen geometries.…”
Section: Resultsmentioning
confidence: 99%
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“…It was found that these two events were able to be related to the path of the tip of the flaring rivet and hence the internal characteristics of the SPR samples via a simplified geometric approach. Static and fatigue tests were conducted using coach-peel, cross-tension and tensile-shear specimens with Al-5052 plates for evaluation of the fatigue strength of the SPR joints [10]. The results showed that the equivalent stress intensity factor range can properly predict the current experimental fatigue lifetime.…”
Section: Introductionmentioning
confidence: 99%