Buckling analysis of thick cylindrical shells using micropolar theory

被引:0
|
作者
Behzadi, Parham [1 ]
Salehi, Manouchehr [1 ]
机构
[1] Amirkabir Univ Technol, Mech Engn Dept, Valiasr Sq,Hafez Ave, Tehran 159163431, Iran
关键词
Micropolar theory; Buckling; Cylindrical shell; Characteristic length; Finite element; Nonlinear; FINITE-ELEMENT; STABILITY; MEDIA; BONE;
D O I
10.1177/23977914231157908
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
Modeling complex materials with internal structure such as porous solids is challenging as in some cases the classical theory cannot provide precise responses. By considering the scale effects through additional kinematic descriptors and six constants for isotropic materials, the micropolar theory can accurately model complex materials like bone. This paper studies the buckling of a thick cylindrical shell using classical and non-classical theories. The cylinder's material is considered bone and isotropic, and the critical load value for different geometries and boundary conditions has been obtained. Finally, the size-effect and importance of micropolar theory in micro dimensions are investigated. The micropolar equations are solved by a numerical solution using the 3D finite element method. The results show that decreasing the macroscopic length increases the stiffness of the cylinder more than that predicted by classical theory; In addition, by increasing the thickness of the cylinder and the importance of shear stresses, the micropolar theory predicts a more critical load than the classical one, and the result differences become more significant between micropolar and classical theories. Also, the characteristic length of the micropolar is investigated. The results show that the change of the critical load increased by moving toward the micro dimensions.
引用
收藏
页数:13
相关论文
共 50 条
  • [1] Generic buckling of thick orthotropic cylindrical shells
    Yang, I.H.
    Kuo, W.S.
    Aeronautical Journal, 1992, 96 (958):
  • [2] Buckling Analysis of Functionally Graded Thick Cylindrical Shells with Variable Thickness Using DQM
    Alashti, R. Akbari
    Ahmadi, S. A.
    ARABIAN JOURNAL FOR SCIENCE AND ENGINEERING, 2014, 39 (11) : 8121 - 8133
  • [3] Buckling Analysis of Functionally Graded Thick Cylindrical Shells with Variable Thickness Using DQM
    R. Akbari Alashti
    S. A. Ahmadi
    Arabian Journal for Science and Engineering, 2014, 39 : 8121 - 8133
  • [4] Buckling of thick orthotropic cylindrical shells under torsion
    Kim, YS
    Kardomateas, GA
    Zureick, A
    JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 1999, 66 (01): : 41 - 50
  • [5] GENERIC BUCKLING OF THICK ORTHOTROPIC CYLINDRICAL-SHELLS
    YANG, IH
    KUO, WS
    AERONAUTICAL JOURNAL, 1992, 96 (958): : 313 - 318
  • [6] Buckling of thick orthotropic cylindrical shells under torsion
    Kim, Y.S.
    Kardomateas, G.A.
    Zureick, A.
    Journal of Applied Mechanics, Transactions ASME, 1999, 66 (01): : 41 - 50
  • [7] Buckling of moderately thick laminated cylindrical shells: A review
    Simitses, GJ
    COMPOSITES PART B-ENGINEERING, 1996, 27 (06) : 581 - 587
  • [8] A study of the plastic buckling of axially compressed cylindrical shells with a thick-shell theory
    Lu, G
    Mao, RJ
    INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES, 2001, 43 (10) : 2319 - 2330
  • [9] A rigorous method for the analysis of localization of axisymmetric buckling patterns in thick cylindrical shells
    Goto, Y
    Zhang, CH
    Wang, QY
    Obata, M
    THIN-WALLED STRUCTURES, 1998, 31 (1-3) : 73 - 88
  • [10] Buckling analysis of cylindrical thin-shells using strain gradient elasticity theory
    Krishnan, N. M. Anoop
    Ghosh, Debraj
    MECCANICA, 2017, 52 (06) : 1369 - 1379