Free vibration analysis of arbitrarily shaped Functionally Graded Carbon Nanotube-reinforced plates

被引:218
作者
Fantuzzi, Nicholas [1 ]
Tornabene, Francesco [1 ]
Bacciocchi, Michele [1 ]
Dimitri, Rossana [2 ]
机构
[1] Univ Bologna, Sch Engn & Architecture, DICAM Dept, Bologna, Italy
[2] Univ Salento, Dept Innovat Engn, Lecce, Italy
关键词
Layered structures; Mechanical properties; Numerical analysis; Computational modelling; Functionally Graded Carbon Nanotubes; THERMO-ELASTIC COMPOSITE; PLANE STATE STRUCTURES; FINITE-ELEMENT-METHOD; HIGHER-ORDER THEORIES; LAMINATED COMPOSITE; ISOGEOMETRIC ANALYSIS; BUCKLING ANALYSIS; NATURAL FREQUENCIES; DYNAMIC-ANALYSIS; CONICAL SHELLS;
D O I
10.1016/j.compositesb.2016.09.021
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
By means of Non-Uniform Rational B-Splines (NURBS) curves, it is possible to describe arbitrary shapes with holes and discontinuities. These peculiar shapes can be taken into account to describe the reference domain of several nanoplates, where a nanoplate refers to a flat structure reinforced with Carbon Nanotubes (CNTs). In the present paper, a micromechanical model based on the agglomeration of these nanoparticles is considered. Indeed, when this kind of reinforcing phase is inserted into a polymeric matrix, CNTs tend to increase their density in some regions. Nevertheless, some nanoparticles can be still scattered within the matrix. The proposed model allows to control the agglomeration by means of two parameters. In this way, several parametric studies are presented to show the influence of this agglomeration on the free vibrations. The considered structures are characterized also by a gradual variation of CNTs along the plate thickness. Thus, the term Functionally Graded Carbon Nanotubes (FGCNTs) is introduced to specify these plates. Some additional parametric studies are also performed to analyze the effect of a mesh distortion, by considering several geometric and mechanical configurations. The validity of the current methodology is proven through a comparative assessment of our results with those available from the literature or obtained with different numerical approaches, such as the Finite Element Method (FEM). The strong form of the equations governing a plate is solved by means of the Generalized Differential Quadrature (GDQ) method. (C) 2016 Elsevier Ltd. All rights reserved.
引用
收藏
页码:384 / 408
页数:25
相关论文
共 125 条
[21]   An accurate one-dimensional theory for the dynamics of laminated composite curved beams [J].
Carpentieri, Gerardo ;
Tornabene, Francesco ;
Ascione, Luigi ;
Fraternali, Fernando .
JOURNAL OF SOUND AND VIBRATION, 2015, 336 :96-105
[22]   Theories and finite elements for multilayered, anisotropic, composite plates and shells [J].
Carrera, E .
ARCHIVES OF COMPUTATIONAL METHODS IN ENGINEERING, 2002, 9 (02) :87-140
[23]  
Cottrell J.A., 2009, Isogeometric Analysis: Towards Unification of Computer Aided Design and Finite Element Analysis
[24]   Nanocomposites: a state-of-the-art review [J].
Crainic, N ;
Marques, AT .
ADVANCED MATERIALS FORUM I, 2002, 230-2 :656-659
[25]  
Cristescu ND., 2004, Mechanics of Elastic Composite
[26]   A Sublaminate Generalized Unified Formulation for the analysis of composite structures [J].
D'Ottavio, Michele .
COMPOSITE STRUCTURES, 2016, 142 :187-199
[27]   ∞3 Hierarchy plate theories for thick and thin composite plates:: The generalized unified formulation [J].
Demasi, Luciano .
COMPOSITE STRUCTURES, 2008, 84 (03) :256-270
[28]   Determination of critical buckling loads of isotropic, FGM and laminated truncated conical panel [J].
Demir, Cigdem ;
Mercan, Kadir ;
Civalek, Omer .
COMPOSITES PART B-ENGINEERING, 2016, 94 :1-10
[29]   NURBS- and T-spline-based isogeometric cohesive zone modeling of interface debonding [J].
Dimitri, R. ;
De Lorenzis, L. ;
Wriggers, P. ;
Zavarise, G. .
COMPUTATIONAL MECHANICS, 2014, 54 (02) :369-388
[30]  
Dimitri R., COMPUT METHODS APPL, V269, P394