Abstract
In this paper, a layerwise theory and associated finite element model are presented to study the bending deformations of delaminated composite shell panels. The layerwise theory is based on the assumption of first-order shear deformation theory in each layer, and it satisfies the displacement continuity at layer interfaces. The presence of multiple discrete delaminations is modeled through the use of Heaviside step functions. Delamination movements (relative slip and opening) are included in the theory as additional degrees of freedom. The finite element model developed is validated by comparing the present results with those available in the literature. This model based on the layerwise theory is subsequently used for the first time in the literature to study the static response and delamination movements such as interfacial slipping and opening of delaminated composite shell panels.
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Nanda, N. Static analysis of delaminated composite shell panels using layerwise theory. Acta Mech 225, 2893–2901 (2014). https://doi.org/10.1007/s00707-014-1200-7
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DOI: https://doi.org/10.1007/s00707-014-1200-7