Dynamic analysis of functionally graded carbon nanotubes-reinforced plate and shell structures using a double directors finite shell element

被引:113
|
作者
Frikha, A. [1 ]
Zghal, S. [1 ]
Dammak, F. [1 ]
机构
[1] Univ Sfax, Natl Engn Sch Sfax, Engn Prod Mech & Mat Unit UGPM2, BP W3038, Sfax, Tunisia
关键词
Carbon nanotubes; Functionally graded material; Double directors shell element; Dynamic behavior; FREE-VIBRATION ANALYSIS; SHEAR DEFORMATION-THEORY; COUPLE-STRESS THEORY; ELASTIC FOUNDATIONS; ISOGEOMETRIC ANALYSIS; NONLINEAR VIBRATION; CYLINDRICAL PANELS; BUCKLING ANALYSIS; MOVING LOAD; ELASTODYNAMIC ANALYSIS;
D O I
10.1016/j.ast.2018.04.048
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The present paper aims at the study of the dynamic behavior of functionally graded carbon nanotubes-reinforced composite shell structures (FG-CNTRC) via forced vibration analysis. The governing equations of motion are developed using a linear discrete double directors finite element model. The elaborated model is based on high-order-distribution of displacement field and uses a cubic variation of the vector position along the thickness direction. A zero transverse shear stress at top and bottom surfaces is also imposed. Four types of distributions of carbon nanotubes (CNTs) such that uniformly and three functionally graded distributions are considered. The extended rule of mixture is used to estimate the effective material properties of carbon nanotube-reinforced composite (CNTRC) shell. The applicability and the performance of the present model are illustrated by three numerical examples of FG-CNTRC square plates, spherical caps and annular ring plates. The transient center deflections of the studied shell structures are computed and depicted for different volume fractions and profiles of CNTs, various boundary conditions and other geometrical parameters in order to show the effect of these parameters on dynamic behavior of FG-CNTRC shells. (C) 2018 Elsevier Masson SAS. All rights reserved.
引用
收藏
页码:438 / 451
页数:14
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