Study on the Actuating Performance of an Embedded Macro Fiber Composite Considering the Shear Lag Effect

Author:

Wei Jianhui,Gao Shuang,Zhang JiaruiORCID,Tu Jianwei

Abstract

Macro fiber composite (MFC), which are new ultrathin piezoelectric smart materials, are mostly applied in the fields of shell structure deformation and vibration control. Among others, the application of embedded MFCs in sandwich structures has received wide attention. Currently, its actuating force formula is primarily acquired based on the Bernoulli–Euler Model, which does not consider the shear lag effect and actuating force of MFC ends. To study the actuating performance of an MFC in a sandwich structure, according to its action characteristics, the MFC is divided into upper and lower actuating units without any interaction between to two under the condition of plane strain, and the shear lag effect is considered between the units and the top and bottom of the sandwich structure. The actuating force of the MFC ends is obtained by considering its influence on the bending deformation of the sandwich structure, which deduces the actuating force formula of the embedded MFC. In contrast to ANSYS piezoelectric simulation, the distribution of the MFC interior normal stress is similar to the result from ANSYS piezoelectric simulation, and there is a very small deviation between the MFC end and central normal stress and the result from ANSYS piezoelectric simulation. Taking the end deflection of the sandwich structure with an embedded MFC as an example, the actuating force simulation of the MFC considering the shear lag effect is compared with the ANSYS piezoelectric simulation and actuating force simulation based on the Bernoulli–Euler model. The result indicates that the actuating force simulation of the MFC considering the shear lag effect is closer to the ANSYS piezoelectric simulation, which proves the rationality and necessity of considering the shear lag effect and end actuating force of the MFC.

Funder

National Natural Science Foundation of China

Fundamental Research Funds for the Central Universities

Natural Science Foundation of Hubei Province

Key Research Plan of Ministry of Science and Technology

Publisher

MDPI AG

Subject

General Materials Science

Reference38 articles.

1. Finite element analysis of bird strike on composite wing leading edge based on the coupling eulerian-lagrangian method;Du;J. Vib. Shock.,2012

2. Experimental research on fatigue life of bolt hole in marine composite laminates;Yao;Shipbuild. China,2010

3. Numerical simulation of strain rate effect of fiber reinforced composites;Ye;J. Jilin Univ. Eng. Technol. Ed.,2019

4. Induced strain actuation of composite beams and rotor blades with embedded piezoceramic elements

5. Wind Tunnel Test of a Smart Rotor Model with Individual Blade Twist Control

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