Numerical buckling analysis of graded CNT-reinforced composite sandwich shell structure under thermal loading

被引:132
作者
Mehar, Kulmani [1 ]
Panda, Subrata Kumar [2 ]
Devarajan, Yuvarajan [1 ]
Choubey, Gautam [1 ]
机构
[1] MITS, Mech Engn Dept, Madanapalle 517325, Andhra Pradesh, India
[2] NIT Rourkela, Mech Engn Dept, Rourkela 769008, Odisha, India
关键词
Buckling; FEM; FG-CNT; HSDT kinematics; Shell panel; Sandwich; SHEAR DEFORMATION-THEORY; FREE-VIBRATION ANALYSIS; FINITE-ELEMENT-ANALYSIS; REFINED PLATE-THEORY; BENDING ANALYSIS; ELASTIC FOUNDATIONS; BEHAVIOR; QUASI-3D; ZIGZAG;
D O I
10.1016/j.compstruct.2019.03.002
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The buckling load parameters of the graded nanotube sandwich structure reported in this article under the influence of uniform thermal loading. The corresponding properties of the graded nanotube sandwich evaluated via the extended rule of mixture including temperature dependent properties of each constituent. The nanotube structural model derived mathematically using a higher-order polynomial displacement to maintain the required shear stress continuity and thermal distortion via Green-Lagrange strain. Further, the variational technique is adopted to obtain the governing equilibrium equation of the sandwich structural panel and the subsequent algebraic form achieved using the isoparametric displacement finite element steps. The computational buckling load parameter predicted using the own MATLAB code with the help of the current mathematical model. The model accuracy and the consistency are established through simultaneous convergence and validity study with available published results. Finally, the detail applicability of the current higher-order model is highlighted through a series of numerical examples and corresponding inferences.
引用
收藏
页码:406 / 414
页数:9
相关论文
共 69 条
[1]  
[Anonymous], 2004, INTRO NONLINEAR FINI, DOI DOI 10.1093/ACPROF:OSO/978019-8525295.003.0002
[2]   Influence of nature of core on vibro acoustic behavior of sandwich aerospace structures [J].
Arunkumar, M. P. ;
Pitchaimani, Jeyaraj ;
Gangadharan, K. V. ;
Babu, M. C. Lenin .
AEROSPACE SCIENCE AND TECHNOLOGY, 2016, 56 :155-167
[3]   Dynamic and bending analysis of carbon nanotube-reinforced composite plates with elastic foundation [J].
Bakhadda, Boumediene ;
Bouiadjra, Mohamed Bachir ;
Bourada, Fouad ;
Bousahla, Abdelmoumen Anis ;
Tounsi, Abdelouahed ;
Mahmoud, S. R. .
WIND AND STRUCTURES, 2018, 27 (05) :311-324
[4]   An efficient and simple four variable refined plate theory for buckling analysis of functionally graded plates [J].
Bellifa, Hichem ;
Bakora, Ahmed ;
Tounsi, Abdelouahed ;
Bousahla, Abdelmoumen Anis ;
Mahmoud, S. R. .
STEEL AND COMPOSITE STRUCTURES, 2017, 25 (03) :257-270
[5]  
Bouderba B, 2013, STEEL COMPOS STRUCT, V14, P85
[6]   Improved HSDT accounting for effect of thickness stretching in advanced composite plates [J].
Bouhadra, Abdelhakim ;
Tounsi, Abdelouahed ;
Bousahla, Abdelmoumen Anis ;
Benyoucef, Samir ;
Mahmoud, S. R. .
STRUCTURAL ENGINEERING AND MECHANICS, 2018, 66 (01) :61-73
[7]   Nonlinear vibration analysis of composite laminated and sandwich plates with random material properties [J].
Chandrashekhar, M. ;
Ganguli, Ranjan .
INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES, 2010, 52 (07) :874-891
[8]  
Cook RD, 2009, CONCEPTS APPL FINITE, V4th
[9]   Role of material combination and new results of mechanical behavior for FG sandwich plates in thermal environment [J].
Do, T. V. ;
Bui, T. Q. ;
Yu, T. T. ;
Pham, D. T. ;
Nguyen, C. T. .
JOURNAL OF COMPUTATIONAL SCIENCE, 2017, 21 :164-181
[10]   A refined theory with stretching effect for the flexure analysis of laminated composite plates [J].
Draiche, Kada ;
Tounsi, Abdelouahed ;
Mahmoud, S. R. .
GEOMECHANICS AND ENGINEERING, 2016, 11 (05) :671-690