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Modeling the response of laminated composite structures to mechanical and environmental loadings is complicated, even in the elastic phase, by the multilayered material architecture and the presence of unavoidable imperfections and flaws at the layer interfaces; stress and displacement fields exhibit complex zig-zag through-thickness distributions and discontinuities.
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Furthermore, the interface behavior is investigated, including the interface stress analysis and interface slip.
Next, a linear small deformation interface stress model is developed.
The effects of the crucial parameters on the interface stress were further investigated with FEM.
A method for estimating the joint strength under static loadings is proposed using interface stress distributions.
There was also a pronounced difference between the shear interface stress pattern around the PEEK and CoCr implants.
By imposing physical connections between interface surfaces, gap elements distort the interface stress distributions under large slip.
The addition of yttrium has beneficial effect on the decrease of the interface stress because it decreases the Δρmin.
In general, the mechanistic model is used to calculate the interface stress by drying shrinkage and thermal expansion.
Obtained results suggest that the interface stress distributions are related to the slip and the rotation angle.
In addition, the possible physical background of positive or negative interface stress is analyzed.
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CEO of Professional Science Editing for Scientists @ prosciediting.com