2019
DOI: 10.1016/j.ijadhadh.2019.102426
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Tensile behavior of hybrid multi-bolted/bonded joints in composite laminates

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Cited by 39 publications
(13 citation statements)
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“…The failure displacement was 0.21–0.25 mm and the corresponding load was 2670–2919 N. The average maximum load of the four test pieces was 3796.35 N. In this experiment, there were two or more load peaks. Similarly, the characteristics of two load peaks also were reported in the bolted/bonded hybrid joint of the epoxy composite [ 12 , 13 , 14 ].…”
Section: Methodsmentioning
confidence: 67%
“…The failure displacement was 0.21–0.25 mm and the corresponding load was 2670–2919 N. The average maximum load of the four test pieces was 3796.35 N. In this experiment, there were two or more load peaks. Similarly, the characteristics of two load peaks also were reported in the bolted/bonded hybrid joint of the epoxy composite [ 12 , 13 , 14 ].…”
Section: Methodsmentioning
confidence: 67%
“…When stiffeners are bonded to web panels subjected to high shear stresses, peeling forces tend to appear in adhesives and this might lead to a brittle failure [4,10] This undesirable behavior could be avoided by adding fasteners to created hybrid fail-safe joints. For these circumstances, the presence of bolts can delay the peeling stresses and the adhesives reduce the stress concentration around the bolts [15]. According to Lopez-Cruz et al [16], the hybrid joint strength is related to the adhesive thickness, mechanical properties of the adhesive and bolt-hole clearance.…”
Section: Introductionmentioning
confidence: 99%
“…Therefore, mechanical fastening is often coupled to bonding method for increasing the overall safety response of structures. [3][4][5] The bolted/bonded hybrid (HBB) joining technology is of interest in aerospace, automotive, naval and civil applications, but the analysis of HBB system fracture DOI: 10.1002/masy.202100010 behavior, depending on many design parameters, is still an open issue. In [6] the mechanical behavior of HBB single lap configuration was investigated, resulting that the load transferred by bolt is function of adhesive and adherend thickness, adhesive modulus and overlap length.…”
Section: Introductionmentioning
confidence: 99%