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3D layerwise impact investigation of sandwich plates with multi-directional phase transformation SMA face sheets and nearly incompressible compliant hyperelastic cores

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Abstract

In the present article, the finite element (FE) simulation of the low-velocity impact of a sandwich plate with a nearly incompressible compliant hyperelastic core and SMA face sheets is accomplished for the first time, using a 3D pseudoelasticity phase transformation model and a semi-3D layerwise sandwich plate theory. The changes in the thickness and the time/load-dependence of the stiffness of the contact region are taken into account and various (neo-Hookean, Mooney-Rivlin, and Yeoh) hyperelasticity models and clamped and simply supported boundary conditions are examined. The resulting nonlinear coupled governing finite element equations of the damped impact response of the hyperelastic and pseudoelastic plate are solved by an iterative updating algorithm that is capable of tracing the impact and complete/incomplete direct and converse 3D phase transformation events. The modeling procedure, formulation, and solution algorithm feature apparent superiorities, even on the well-known commercial finite element analysis codes, due to employing higher scientific and mathematical accuracies. It is found that while the Mooney-Rivlin model induces larger compliance in comparison with the neo-Hookean and Yeoh hyperelasticity models, the SMA face sheets significantly reduce the resulting lateral deflections but increase the global stiffness of the contact region and the contact force, and that simply supported plates feature larger recovery strains and hysteresis loops that lead to higher damping and smoother time histories.

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Shariyat, M., Hosseini, S.H. 3D layerwise impact investigation of sandwich plates with multi-directional phase transformation SMA face sheets and nearly incompressible compliant hyperelastic cores. Acta Mech 233, 4385–4406 (2022). https://doi.org/10.1007/s00707-022-03337-w

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