Analytical investigation on mechanical buckling of FGM truncated conical shells reinforced by orthogonal stiffeners based on FSDT

被引:65
作者
Dao Van Dung [1 ]
Do Quang Chan [2 ]
机构
[1] Vietnam Natl Univ, Hanoi, Vietnam
[2] Univ Transport Technol, Hanoi, Vietnam
关键词
Functionally graded material (FGM); Stiffened truncated conical shell; Buckling; Critical buckling load; First order shear deformation theory; CIRCULAR CYLINDRICAL-SHELLS; FREE-VIBRATION ANALYSIS; LAMINATED COMPOSITE CYLINDERS; NONLINEAR DYNAMIC-ANALYSIS; ELASTIC MEDIUM; SEMIANALYTICAL APPROACH; BOUNDARY-CONDITIONS; EXTERNAL-PRESSURE; PANELS; LOADS;
D O I
10.1016/j.compstruct.2016.10.006
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
This work presents an analytical investigation for analyzing the mechanical buckling of truncated conical shells made of functionally graded materials, subjected to axial compressive load and external uniform pressure. Shells are reinforced by closely spaced stringers and rings. The change of spacing between stringers in the meridional direction also is taken into account. Using the adjacent equilibrium criterion, the first order shear deformation theory (FSDT) and Lekhnitskii smeared stiffener technique, the linearization stability equations have been established. The resulting equations which they are the system of five variable coefficient partial differential equations in terms of displacement components are investigated by Galerkin method. The closed-form expression for determining the critical buckling load is obtained. The effects of material properties, dimensional parameters, stiffeners and semi-vertex angle on buckling behaviors of shell are considered. Shown that for thick conical shells, the use of FSDT for determining their critical buckling load is necessary and more suitable. (C) 2016 Elsevier Ltd. All rights reserved.
引用
收藏
页码:827 / 841
页数:15
相关论文
共 54 条
[1]   Thermal buckling of temperature-dependent FGM conical shells with arbitrary edge supports [J].
Akbari, M. ;
Kiani, Y. ;
Eslami, M. R. .
ACTA MECHANICA, 2015, 226 (03) :897-915
[2]   Free vibration of FGM Levy conical panels [J].
Akbari, M. ;
Kiani, Y. ;
Aghdam, M. M. ;
Eslami, M. R. .
COMPOSITE STRUCTURES, 2014, 116 :732-746
[3]  
[Anonymous], 1993, FUNCT GRADIENT MAT
[4]   Enhanced thermal buckling of laminated composite cylindrical shells with shape memory alloy [J].
Asadi, H. ;
Kiani, Y. ;
Aghdam, M. M. ;
Shakeri, M. .
JOURNAL OF COMPOSITE MATERIALS, 2016, 50 (02) :243-256
[5]  
Bagherizadeh E, 2012, AIAA J, V50, P500, DOI [10.2514/1.J051278, 10.2514/1.J051120]
[6]   Mechanical buckling of functionally graded material cylindrical shells surrounded by Pasternak elastic foundation [J].
Bagherizadeh, E. ;
Kiani, Y. ;
Eslami, M. R. .
COMPOSITE STRUCTURES, 2011, 93 (11) :3063-3071
[7]  
Boroujerdy MS, 2014, J THEOR APP MECH-POL, V52, P869
[8]  
BRUSH DO, 1975, BUCKLING BARS PLATES
[9]   A semi-analytical approach for linear and non-linear analysis of unstiffened laminated composite cylinders and cones under axial, torsion and pressure loads [J].
Castro, Saullo G. P. ;
Mittelstedt, Christian ;
Monteiro, Francisco A. C. ;
Arbelo, Mariano A. ;
Degenhardt, Richard ;
Ziegrnann, Gerhard .
THIN-WALLED STRUCTURES, 2015, 90 :61-73
[10]   Evaluation of non-linear buckling loads of geometrically imperfect composite cylinders and cones with the Ritz method [J].
Castro, Saullo G. P. ;
Mittelstedt, Christian ;
Monteiro, Francisco A. C. ;
Degenhardt, Richard ;
Ziegmann, Gerhard .
COMPOSITE STRUCTURES, 2015, 122 :284-299