2016
DOI: 10.1016/j.ijfatigue.2015.10.004
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Fatigue performance of a self-piercing rivet joint between aluminum and glass fiber reinforced thermoplastic composite

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Cited by 43 publications
(27 citation statements)
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“…The fatigue test results of the CFRP to aluminium 6111 T82 SPR lap-shear specimens also displayed a large scatter in fatigue life as the maximum fatigue load approached the maximum quasi-static load (3857 N). A similar scatter in fatigue life was also reported elsewhere in studies performed on SPR in composite to aluminum alloys [1,21,23]. This scatter in fatigue life close to maximum static load may be due to the scatter in the quasi-static behavior of the joints, which is suggested in Figure 3.…”
Section: Fatigue Testsupporting
confidence: 83%
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“…The fatigue test results of the CFRP to aluminium 6111 T82 SPR lap-shear specimens also displayed a large scatter in fatigue life as the maximum fatigue load approached the maximum quasi-static load (3857 N). A similar scatter in fatigue life was also reported elsewhere in studies performed on SPR in composite to aluminum alloys [1,21,23]. This scatter in fatigue life close to maximum static load may be due to the scatter in the quasi-static behavior of the joints, which is suggested in Figure 3.…”
Section: Fatigue Testsupporting
confidence: 83%
“…In several studies of metal-to-metal SPR lap-shear joints, fretting has been observed to be one of the dominant causes for crack initiation and significantly accelerated the crack growth in these SPR lap-shear joints [8,10,[28][29][30]. Even though fretting was also observed in SPR lap-shear joints of aluminum to glass-fiber reinforced thermoplastic composite [23], no traces of fretting were observed in any of the SPR lap-shear test specimens tested in this study. Absence of fretting in this study may be attributed to the presence of a thin layer of CFRP sandwiched between the interfaces of the rivet and the aluminum sheet, as seen in Figure 2(b) and 2(c).…”
Section: Fatigue Testmentioning
confidence: 46%
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