2017
DOI: 10.1016/j.ijfatigue.2017.05.025
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Analysis of the fatigue behaviour of laminated composite holes subjected to pin-bearing loads

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Cited by 25 publications
(16 citation statements)
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“…Polymer composites must be drilled with the optimized parameters to avoid drilling-induced damage. 3133…”
Section: Introductionmentioning
confidence: 99%
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“…Polymer composites must be drilled with the optimized parameters to avoid drilling-induced damage. 3133…”
Section: Introductionmentioning
confidence: 99%
“…The existing damages gradually increase due to contact of the bolts/ rivets and maybe results in catastrophic errors. 31 Besides matrix degradation due to overheating during drilling causes different mechanical failures as fibre pull-out, fiber breakage, matrix cracking, peel-up delamination, push-out delamination. Polymer composites must be drilled with the optimized parameters to avoid drilling-induced damage.…”
Section: Introductionmentioning
confidence: 99%
“…This technique has been applied to fatigue damage assessment of composite structures, 5,6 but the disadvantage is that it is not capable of continuous monitoring of real operating structures. The digital image correlation (DIC) technique allows real‐time and non‐contact interrogation of the surface displacement as well as strain distributions of composite structures under fatigue loadings 7,8 . However, DIC requires a speckle pattern on the surface of the structure and extensive calibration; thus, it has poor applicability for continuous monitoring of real structures.…”
Section: Introductionmentioning
confidence: 99%
“…DIC is applied to different problems in composites, such as 3D woven carbon/epoxy composite to characterize the strain field distribution during quasi-static tests [ 37 ] or to locate the fracture initiation in the GFRP tensile tests [ 62 ]. It has been also applied to fatigue studies, for example, to determine the interlaminar shear stress distributions and their variations with the number of cycles for carbon/epoxy composites [ 51 ] or to measure deformations on the pin surface for low cycle fatigue loads [ 63 ].…”
Section: Introductionmentioning
confidence: 99%