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Point estimate method is used to estimate the first four statistical moments of bearing strength of composite pinned joint.
Consequently, in this case of pinned joint, only the hole surface among the composite boundary and interfaces needs to be discretized.
The deterministic progressive failure analysis of composite pinned joint is based on a two-dimensional ABAQUS model, which takes into account large deformation theory and the non-linear shear behavior of composite material.
A mechanical pinned joint in the CFRP laminates such as [0/±45/90]3S, [90/±45/0]3S, [0/±45/90]2S and [90/±45/0]2s is loaded statically and cyclically to finally obtain the critical condition for fatigue.
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CFRP/Ti pinned joints are widely applied on main load-bearing structures of aircrafts.
Tests have been carried out on single pinned joints in [0/90/0]s and [90/0/90]s laminated composites.
Mechanical joints such as bolted, riveted or pinned joints are widely used to join the constituent parts of structural components.
Current Australian practice supports composite beams with web-side-plate connections, which are assumed to behave as nominally pinned joints.
Bearing strength of pinned joints in woven fabric composites with small weaving angles is examined experimentally in this study.
In the design of single-layer structures, the hypothesis of pinned joints leads to structures with low capacity in terms of stability and resistance.
Therefore, a dynamic test platform based on electromagnetic loading method was developed to investigate the dynamic behavior of CFRP/Ti single-lap pinned joints under tensile dynamic loading.
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