1995
DOI: 10.1016/0142-1123(95)98238-x
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Fatigue failure mechanisms in fibre-reinforced plastic laminated tee joints

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Cited by 33 publications
(15 citation statements)
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“…The load~teflection characteristics of the tee joint under this form of loading have been reported previously in Refs. [8,23]. The joints failed initially by delamination in the boundary angle on the side in tension.…”
Section: Tee Joint Loading Configurationmentioning
confidence: 99%
See 1 more Smart Citation
“…The load~teflection characteristics of the tee joint under this form of loading have been reported previously in Refs. [8,23]. The joints failed initially by delamination in the boundary angle on the side in tension.…”
Section: Tee Joint Loading Configurationmentioning
confidence: 99%
“…This has differentiated between single skin [5] and sandwich [6] configurations. Characterisation under static [7] and fatigue [8] load regimes has been done; this has involved experimentation coupled with numerical analysis. The thrust of the experimental work has been to obtain overall load-deflection features.…”
Section: Introductionmentioning
confidence: 99%
“…Shenoi et al [1] have worked on adhesive bonded joints on ship structures, and particularly on T-joints. Those joints transmit tensile, flexwal and shear stresses between the different parts of the ship.…”
Section: Introductionmentioning
confidence: 99%
“…Failure of composite T-joints has also been studied experimentally from different point of view by many investigators [3,4,[20][21][22][23][24][25][26][27][28][29]. The initiation of delamination in the composite T-joint is almost always initiated on the joint's corner due to the maximum stresses developed in this region.…”
Section: Introductionmentioning
confidence: 99%