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      Low-Computational-Cost Technique for Modeling Macro Fiber Composite Piezoelectric Actuators Using Finite Element Method

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          Abstract

          The large number of interdigitated electrodes (IDEs) in a macro fiber composite (MFC) piezoelectric actuator dictates using a very fine finite element (FE) mesh that requires extremely large computational costs, especially with a large number of actuators. The situation becomes infeasible if repeated finite element simulations are required, as in control tasks. In this paper, an efficient technique is proposed for modeling MFC using a finite element method. The proposed technique replaces the MFC actuator with an equivalent simple monolithic piezoceramic actuator using two electrodes only, which dramatically reduces the computational costs. The proposed technique was proven theoretically since it generates the same electric field, strain, and displacement as the physical MFC. Then, it was validated with the detailed FE model using the actual number of IDEs, as well as with experimental tests using triaxial rosette strain gauges. The computational costs for the simplified model compared with the detailed model were dramatically reduced by about 74% for memory usage, 99% for result file size, and 98.6% for computational time. Furthermore, the experimental results successfully verified the proposed technique with good consistency. To show the effectiveness of the proposed technique, it was used to simulate a morphing wing covered almost entirely by MFCs with low computational cost.

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          Most cited references50

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          An investigation into the performance of macro-fiber composites for sensing and structural vibration applications

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            Anisotropic Actuation with Piezoelectric Fiber Composites

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              Mechanics of Composite Materials

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                Author and article information

                Contributors
                Role: Academic Editor
                Journal
                Materials (Basel)
                Materials (Basel)
                materials
                Materials
                MDPI
                1996-1944
                02 August 2021
                August 2021
                : 14
                : 15
                : 4316
                Affiliations
                [1 ]Mechatronics and Robotics Engineering Department, Egypt-Japan University of Science and Technology (E-JUST), New Borg El-Arab, 21934 Alexandria, Egypt; mohamed.fanni@ 123456ejust.edu.eg (M.A.F.); abdelfatah.mohamed@ 123456ejust.edu.eg (A.M.M.)
                [2 ]Mechatronics Department, Faculty of Engineering, Ain Shams University, 11517 Cairo, Egypt
                [3 ]Production Engineering and Mechanical Design Department, Faculty of Engineering, Mansoura University, 35516 Mansoura, Egypt
                [4 ]Electrical Engineering Department, Faculty of Engineering, Assiut University, 71518 Assiut, Egypt
                [5 ]Research Institute for Applied Mechanics, Kyushu University, Fukuoka 816-8580, Japan; yoshidas@ 123456riam.kyushu-u.ac.jp
                [6 ]Institute of Ocean Energy, Saga University, Saga 840-8502, Japan
                Author notes
                Author information
                https://orcid.org/0000-0001-5578-4293
                https://orcid.org/0000-0003-0595-8691
                Article
                materials-14-04316
                10.3390/ma14154316
                8347699
                34361514
                0a28bc60-0a63-43b2-aaba-7de97e6e89b3
                © 2021 by the authors.

                Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license ( https://creativecommons.org/licenses/by/4.0/).

                History
                : 23 June 2021
                : 29 July 2021
                Categories
                Article

                piezoelectric actuator,macro fiber composite,morphing wing,finite element analysis,smart structure

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