Buckling analysis of embedded laminated plates with agglomerated CNT-reinforced composite layers using FSDT and DQM

被引:33
作者
Shokravi, Maryam [1 ]
机构
[1] Buein Zahra Tech Univ, Buein Zahra, Qazvin, Iran
关键词
buckling of laminated plates; SWCNT; agglomeration effects; DQM; elastic medium; SHEAR DEFORMATION-THEORY; FREE-VIBRATION ANALYSES; SANDWICH PLATES; DYNAMIC-RESPONSE; STABILITY;
D O I
10.12989/gae.2017.12.2.327
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
Laminated plates have many applications in different industrials. Buckling analysis of these structures with the nano-scale reinforcement has not investigated yet. However, buckling analysis of embedded laminated plates with nanocomposite layers is studied in this paper. Considering the single-walled carbon nanotubes (SWCNTs) as reinforcement of layers, SWCNTs agglomeration effects and nonlinear analysis using numerical method are the main contributions of this paper. Mori-Tanaka model is applied for obtaining the equivalent material properties of structure and considering agglomeration effects. The elastic medium is simulated by spring and shear constants. Based on first order shear deformation theory (FSDT), the governing equations are derived based on energy method and Hamilton's principle. Differential quadrature method (DQM) is used for calculating the buckling load of system. The effects of different parameters such as the volume percent of SWCNTs, SWCNTs agglomeration, number of layers, orientation angle of layers, elastic medium, boundary conditions and axial mode number of plate on the buckling of the structure are shown. Results indicate that increasing volume percent of SWCNTs increases the buckling load of the plate. Furthermore, considering agglomeration effects decreases the buckling load of system. In addition, it is found that the present results have good agreement with other works.
引用
收藏
页码:327 / 346
页数:20
相关论文
共 32 条
[1]  
A K N., 1975, Fibre Sci Technol, V8, P81, DOI [https://doi.org/10.1016/0015-0568(75)90005-6, DOI 10.1016/0015-0568(75)90005-6]
[2]   Axial buckling of multi-walled carbon nanotubes and nanopeapods [J].
Chan, Yue ;
Thamwattana, Ngamta ;
Hill, James M. .
EUROPEAN JOURNAL OF MECHANICS A-SOLIDS, 2011, 30 (06) :794-806
[3]   Thermal stability analysis of solar functionally graded plates on elastic foundation using an efficient hyperbolic shear deformation theory [J].
El-Hassar, Sidi Mohamed ;
Benyoucef, Samir ;
Heireche, Houari ;
Tounsi, Abdelouahed .
GEOMECHANICS AND ENGINEERING, 2016, 10 (03) :357-386
[4]   Blood vessel buckling within soft surrounding tissue generates tortuosity [J].
Han, Hai-Chao .
JOURNAL OF BIOMECHANICS, 2009, 42 (16) :2797-2801
[5]   Exact solution for transverse bending analysis of embedded laminated Mindlin plate [J].
Heydari, Mohammad Mehdi ;
Kolahchi, Reza ;
Heydari, Morteza ;
Abbasi, Ali .
STRUCTURAL ENGINEERING AND MECHANICS, 2014, 49 (05) :661-672
[6]   Free vibration and buckling analysis of composite cylindrical shells conveying hot fluid [J].
Kadoli, R ;
Ganesan, N .
COMPOSITE STRUCTURES, 2003, 60 (01) :19-32
[7]   Dynamic stability analysis of temperature-dependent functionally graded CNT-reinforced visco-plates resting on orthotropic elastomeric medium [J].
Kolahchi, Reza ;
Safari, Morteza ;
Esmailpour, Masoud .
COMPOSITE STRUCTURES, 2016, 150 :255-265
[8]   Differential cubature and quadrature-Bolotin methods for dynamic stability of embedded piezoelectric nanoplates based on visco-nonlocal-piezoelasticity theories [J].
Kolahchi, Reza ;
Hosseini, Hadi ;
Esmailpour, Masoud .
COMPOSITE STRUCTURES, 2016, 157 :174-186
[9]   A cell-based smoothed finite element method using three-node shear-locking free Mindlin plate element (CS-FEM-MIN3) for dynamic response of laminated composite plates on viscoelastic foundation [J].
Luong-Van, H. ;
Nguyen-Thoi, T. ;
Liu, G. R. ;
Phung-Van, P. .
ENGINEERING ANALYSIS WITH BOUNDARY ELEMENTS, 2014, 42 :8-19
[10]   Vibration and stability of cross-ply laminated composite plates according to a global higher-order plate theory [J].
Matsunaga, H .
COMPOSITE STRUCTURES, 2000, 48 (04) :231-244