Size-dependent deflection of cross-ply composite laminated plate induced by piezoelectric actuators based on a re-modified couple stress theory

Wang, H.; Zheng, S.; Li, Z.

doi:10.24423/aom.3047

Artykuł - szczegóły

Tytuł artykułu

Size-dependent deflection of cross-ply composite laminated plate induced by piezoelectric actuators based on a re-modified couple stress theory

Autorzy

Wang H. , Zheng S. , Li Z.

Wybrane pełne teksty z tego czasopisma

https://am.ippt.pan.pl/index.php/am

Identyfikatory

DOI

10.24423/aom.3047

Warianty tytułu

Języki publikacji

Abstrakty

A size-dependent model for cross-ply composite laminated plate bonded with PZT actuators is developed by using re-modified couple stress theory (RMCST), which only uses two material length scale parameters to describe the size-dependent effect. An equivalent bending moment model and a refined model are developed by using two different ways. The analytical solution of equivalent bending moment model for simply supported composite laminated plate is obtained. The equilibrium equation of motion and corresponding boundary constraints of the refined model are established from the potential energy principle. The Ritz approximate solution of transverse deflection of the refined model indicates that the size-effect cannot be ignored in micro-scale. Numerical examples are given to account for the effect of material length scale parameters and dimensions of piezoelectric actuators on the defection of composite laminated plate.

Słowa kluczowe

deflection composite laminated plate piezoelectric actuator re-modified couple stress theory

Wydawca

Instytut Podstawowych Problemów Techniki PAN

Czasopismo

Archives of Mechanics

Rocznik

2019

Tom

Vol. 71, nr 3

Strony

177--205

Opis fizyczny

Bibliogr. 59 poz., rys.

Twórcy

autor

Wang H.

State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, PR China
College of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, PR China

autor

Zheng S.

sjzheng@nuaa.edu.cn

State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, PR China

autor

Li Z.

Pan Asia Technical Automotive Center Co. Ltd., Shanghai 2121, PR China

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Uwagi

Opracowanie rekordu w ramach umowy 509/P-DUN/2018 ze środków MNiSW przeznaczonych na działalność upowszechniającą naukę (2019).

Typ dokumentu

Bibliografia

Identyfikator YADDA

bwmeta1.element.baztech-5f1be2ba-d0e9-4043-b2a4-6d986f5e4dd2