Numerical study on the buckling and vibration of functionally graded carbon nanotube-reinforced composite conical shells under axial loading

被引:164
作者
Ansari, Reza [1 ]
Torabi, Jalal [1 ]
机构
[1] Univ Guilan, Dept Mech Engn, POB 3756, Rasht, Iran
关键词
FG-CNTRC conical shell; Vibration; Buckling; Numerical analysis; SHEAR DEFORMATION-THEORY; DIFFERENTIAL QUADRATURE METHOD; MIXED BOUNDARY-CONDITIONS; MESH-FREE METHOD; THERMAL ENVIRONMENTS; NONLINEAR VIBRATION; CYLINDRICAL-SHELLS; ELASTIC FOUNDATIONS; MECHANICAL-PROPERTIES; PIEZOELECTRIC LAYERS;
D O I
10.1016/j.compositesb.2016.03.080
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
An efficient numerical method within the framework of variational formulation is employed to study the buckling and vibration of axially-compressed functionally graded carbon nanotube-reinforced composite (FG-CNTRC) conical shells. The effective material properties of functionally graded composite conical shell are estimated based on the extended rule of mixture. To derive the governing equations, the matrix form of Hamilton's principle is first presented on the basis of the first order shear deformation theory. Then, employing the generalized differential quadrature (GDQ) method in axial direction and periodic differential operators in circumferential direction, the numerical differential and integral operators are introduced to perform the discretization process. The comparison study is carried out to verify the accuracy and efficiency of the proposed method. Numerical results indicate that the volume fraction and types of distribution of CNTs have considerable effects on the buckling and vibration characteristics of FG-CNTRC conical shells subjected to axial loadings. (C) 2016 Elsevier Ltd. All rights reserved.
引用
收藏
页码:196 / 208
页数:13
相关论文
共 51 条
[1]   Elasticity Solution of Free Vibration and Bending Behavior of Functionally Graded Carbon Nanotube-Reinforced Composite Beam with Thin Piezoelectric Layers Using Differential Quadrature Method [J].
Alibeigloo, A. ;
Liew, K. M. .
INTERNATIONAL JOURNAL OF APPLIED MECHANICS, 2015, 7 (01)
[3]  
[Anonymous], 2000, DIFFERENTIAL QUADRAT
[4]   Analytical solution for nonlinear postbuckling of functionally graded carbon nanotube-reinforced composite shells with piezoelectric layers [J].
Ansari, R. ;
Pourashraf, T. ;
Gholami, R. ;
Shahabodini, A. .
COMPOSITES PART B-ENGINEERING, 2016, 90 :267-277
[5]   Size-dependent nonlinear mechanical behavior of third-order shear deformable functionally graded microbeams using the variational differential quadrature method [J].
Ansari, R. ;
Shojaei, M. Faghih ;
Gholami, R. .
COMPOSITE STRUCTURES, 2016, 136 :669-683
[6]   A novel variational numerical method for analyzing the free vibration of composite conical shells [J].
Ansari, R. ;
Shojaei, M. Faghih ;
Rouhi, H. ;
Hosseinzadeh, M. .
APPLIED MATHEMATICAL MODELLING, 2015, 39 (10-11) :2849-2860
[7]   Forced vibration analysis of functionally graded carbon nanotube-reinforced composite plates using a numerical strategy [J].
Ansari, R. ;
Hasrati, E. ;
Shojaei, M. Faghih ;
Gholami, R. ;
Shahabodini, A. .
PHYSICA E-LOW-DIMENSIONAL SYSTEMS & NANOSTRUCTURES, 2015, 69 :294-305
[8]   Nonlinear forced vibration analysis of functionally graded carbon nanotube-reinforced composite Timoshenko beams [J].
Ansari, R. ;
Shojaei, M. Faghih ;
Mohammadi, V. ;
Gholami, R. ;
Sadeghi, F. .
COMPOSITE STRUCTURES, 2014, 113 :316-327
[9]   Nonlinear vibration analysis of Timoshenko nanobeams based on surface stress elasticity theory [J].
Ansari, R. ;
Mohammadi, V. ;
Shojaei, M. Faghih ;
Gholami, R. ;
Rouhi, H. .
EUROPEAN JOURNAL OF MECHANICS A-SOLIDS, 2014, 45 :143-152
[10]  
BRUSH DO, 1975, BUCKLING BARS PLATES