2005
DOI: 10.1016/j.compositesa.2005.01.014
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Pin and bolt bearing strength of fibreglass/aluminium laminates

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Cited by 36 publications
(43 citation statements)
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“…For instance, apart from failure of the concrete pin in either shear or compression, it can be considered that the potential failure modes might be expected to be similar. Specific literature on strength of perforated plates for mechanically fastened joints [11,12] generally considers that the failure of the connection occurs in one of the four potential modes illustrated in Figure 2Figure 2: net-tension, shear-out (or tear-out), bearing, and cleavage. Net-tension is a lateral failure at the minimum cross-section perpendicular to the loading direction (Figure 2Figure 2a).…”
Section: Expected Failure Modesmentioning
confidence: 99%
“…For instance, apart from failure of the concrete pin in either shear or compression, it can be considered that the potential failure modes might be expected to be similar. Specific literature on strength of perforated plates for mechanically fastened joints [11,12] generally considers that the failure of the connection occurs in one of the four potential modes illustrated in Figure 2Figure 2: net-tension, shear-out (or tear-out), bearing, and cleavage. Net-tension is a lateral failure at the minimum cross-section perpendicular to the loading direction (Figure 2Figure 2a).…”
Section: Expected Failure Modesmentioning
confidence: 99%
“…Since it has been previously reported in the literature [10][11][12]16,17] that a pin bearing load configuration is the most conservative means for simulating a mechanically fastened joint by virtue of its encouragement of delamination and buckling, it is merely prudent to examine the local stress-strain behavior of an orthotropic variant of GLARE in this light as well [18]. The hardened side plates employ a 4.8 mm diameter loading pin for easier application to practical joint design and the assurance of geometric congruency to previous FE studies [16], to which the present research is related to.…”
Section: Developed Test Fixturesmentioning
confidence: 95%
“…Simply stated, the YDB mechanism can be described in the following manner: upon loading, delamination develops between the adjacent glass and aluminum layers; once this delamination reaches a critical length, the aluminum layers yield and then buckle, effectively transferring the load to the adjacent glass layers; however, since the glass layers themselves remain laterally unsupported, it is proposed that they too will buckle -along with the aluminum layers -thus precipitating joint collapse. The YDB mechanism builds upon previous observations [10][11][12][13]16,17] and rests upon reducing the heterogeneous nature of GLARE to the behavior of one of its constituents and one parameter within that constituent: that of the yield strength of the aluminum layers.…”
Section: Introductionmentioning
confidence: 97%
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“…The outer aluminium layer was etched away, revealing an area of delamination in the prepreg layer. Caprino et al [14] also provided some experimental evidence by presenting an optical micrograph showing extensive delamination between the glass and metal layers of a fully failed pin-loaded FML. Krimbalis et al [15] showed analytically that the stress needed to buckle the glass prepreg layers in GLARE Ò is small compared to that of the aluminium and concluded that the contribution of the glass layers to the overall bearing strength of the laminate is negligible.…”
Section: Introductionmentioning
confidence: 93%