Content area

Abstract

The applications of piezoelectric materials in the field of smart structures have received significant attention from both the communities of science and engineering. Numerous experimental studies have been carried out to endow smart structures with good flexibility. The flexible/stretchable piezoelectric materials are developed to fit this emerging trend. Generally, these materials undergo significant deformation before reaching fracture failure, and they often exhibit a stress-softening phenomenon during the deformation process. However, the traditional linear constitutive model, typically used for rigid piezoelectric ceramics, continues to dominate theoretical and modeling processes in many scenarios. Existing nonlinear constitutive models usually introduce additional coefficients besides elastic, piezoelectric, and dielectric coefficients. Determining these coefficients requires a substantial number of experiments. In this work, based on a Neo-Hookean material model and electromechanical theory, a novel model for flexible piezoelectric material considering large deformation has been established. In contrast with existing models, the present model describes the nonlinear behavior of flexible piezoelectric material without the need for introducing additional parameters. Furthermore, this model exhibits a quadratic dependence of stress on the electric field. To facilitate practical applications, the constitutive model has been implemented using the commercial simulation software ABAQUS through a user subroutine. The accuracy of the subroutine is validated by comparing simulations with analytical solutions for uniaxial stretching of a flexible piezoelectric ribbon. Several numerical examples are followed to demonstrate the robustness of the elements. The proposed model offers a valuable tool for the analysis and design of flexible piezoelectric material.

Details

Title
Large deformation modeling of flexible piezoelectric materials
Author
Lv, Shihao 1 ; Shi, Yan 1 ; Li, Bingyang 2 ; Gao, Cunfa 1 

 Nanjing University of Aeronautics and Astronautics, State Key Laboratory of Mechanics and Control for Aerospace Structures, Nanjing, China (GRID:grid.64938.30) (ISNI:0000 0000 9558 9911) 
 China Academy of Aerospace Science and Innovation, Beijing, China (GRID:grid.64938.30); Peking University, College of Engineering, Beijing, China (GRID:grid.11135.37) (ISNI:0000 0001 2256 9319) 
Pages
3667-3685
Publication year
2024
Publication date
Dec 2024
Publisher
Springer Nature B.V.
ISSN
09391533
e-ISSN
14320681
Source type
Scholarly Journal
Language of publication
English
ProQuest document ID
3259013633
Copyright
© The Author(s), under exclusive licence to Springer-Verlag GmbH Germany, part of Springer Nature 2024.