A Three-Layer Quasi-3D Finite Element Analysis for Smart Actuation on Sandwich Plates
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ORIGINAL PAPER
A Three‑Layer Quasi‑3D Finite Element Analysis for Smart Actuation on Sandwich Plates Airton Nabarrete1 Received: 14 June 2020 / Revised: 4 October 2020 / Accepted: 12 October 2020 © Krishtel eMaging Solutions Private Limited 2020
Abstract Background The quasi-3D finite element model includes the smart actuation on a three-layer sandwich plate with laminated composite face-sheets. In the model, the face-sheets are represented as Reissner-Mindlin plates and the core is modeled as a three-dimensional continuum. Purpose This representation allows accurate modeling for a wide range of core types. In this model, the electrical constitutive relations of piezoelectric layers are included in the formulation of the face-sheets. In previous publications, this quasi-3D finite element formulation has demonstrated some advantages in comparison with solid finite element models. The aspect ratio of three-dimensional elements can make it rather inconvenient to use on very thin faces-sheets, which makes the number of degrees of freedom very high. Methods Analytical through-thickness integration of the energy expressions is used to reduce the three-dimensional problem to two dimensions for the evaluation of mass and stiffness matrices. In the same way, the analytical integration of the electrical voltages work applied to the piezoelectric layers produces the piezoelectric actuation force vector. Result This research assesses the accuracy of the proposed model for dynamic responses of sandwich plates using a broad range of core-to-face-sheet stiffness ratio. Conclusions The numerical results show that deflections promoted by the voltage applied to piezoelectric layers of the sandwich plate are very small, even if the core is very flexible. The results also indicate that the core flexibility strongly affects the natural frequencies of the higher bending modes. Keywords Sandwich plate · Piezoelectric · Finite element model · Smart structure · Structural dynamics
Introduction The composite sandwich concept has been accepted for representing beam, plate and shell structures with several layers of different materials. Composite sandwiches have many advantages in the construction of structures subject to transverse forces or bending moments, being stiffer, lighter and more durable. However, severe restrictions exist for the numerical analysis using three-dimensional finite elements in a sandwich structure with thin face-sheets and thick cores due to the element aspect ratios that may lead to numerical errors. Another consideration is the very different physical characteristics between face-sheets * Airton Nabarrete [email protected] 1
Aerospace and Aeronautics Division, Aeronautics Institute of Technology - ITA, Praça Marechal Eduardo Gomes, 50, São José dos Campos, SP 12228‑900, Brazil
and core which require a degree of sophistication much greater than that of classical plate theories. The three-layer quasi-3D finite element formulation was first presented by Oskooei and Hansen [1] to solve the static problem
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