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Full Length Article | Open Access

Layerwise third-order shear deformation theory with transverse shear stress continuity for piezolaminated plates

Yingshan GAOa, Shunqi ZHANGa,b( ), Wei HUa, Songyun MAc, Bernd MARKERTc
School of Mechatronic Engineering and Automation, Shanghai University, Shanghai 200444, China
Key Laboratory of Silicate Cultural Relics Conservation (Shanghai University), Ministry of Education, Shanghai 200444, China
Institute of General Mechanics, RWTH Aachen University, Aachen 52062, Germany

Peer review under responsibility of Editorial Committee of CJA

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Abstract

Regarding laminated structures, an electromechanically coupled Finite Element (FE) model based on Layerwise Third-Order Shear Deformation (LW-TOSD) theory is proposed for static and dynamic analysis. LW-TOSD ensures the continuity of in-plane displacements and transverse shear stresses. The current LW-TOSD can be applied to arbitrary multi-layer laminated structures with only seven Degrees of Freedom (DOFs) for each element node and eliminates the use of the shear correction factors. Moreover, a shear penalty stiffness matrix is constructed to satisfy artificial constraints to optimize the structural shear strain. A dynamic finite element model is obtained based on LW-TOSD using the Hamilton’s principle. First, the accuracy of the current model is validated by comparing with literature and ABAQUS results. Then, this study carries out numerical investigations of piezolaminated structures for different width-to-thickness ratios, length-to-width ratios, penalty stiffness matrix, boundary conditions, electric fields and dynamics.

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Chinese Journal of Aeronautics
Pages 490-505

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Cite this article:
GAO Y, ZHANG S, HU W, et al. Layerwise third-order shear deformation theory with transverse shear stress continuity for piezolaminated plates. Chinese Journal of Aeronautics, 2024, 37(9): 490-505. https://doi.org/10.1016/j.cja.2024.07.013

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Received: 07 October 2023
Revised: 23 November 2023
Accepted: 14 December 2023
Published: 10 July 2024
© 2024 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).