Hamiltonian system for dynamic buckling of transversely isotropic cylindrical shells subjected to an axial impact

被引:10
|
作者
Xu, Xinsheng [1 ,2 ]
Chu, Hongjie [1 ,2 ]
Lim, C. W. [3 ]
机构
[1] Dalian Univ Technol, State Key Lab Struct Anal Ind Equipment, Dalian 116024, Peoples R China
[2] Dalian Univ Technol, Dept Engn Mech, Dalian 116024, Peoples R China
[3] City Univ Hong Kong, Dept Bldg & Construct, Hong Kong, Hong Kong, Peoples R China
基金
高等学校博士学科点专项科研基金; 中国国家自然科学基金;
关键词
dynamic buckling; eigenvalue; Hamiltonian system; thin cylindrical shell; stress wave; transversely isotropic;
D O I
10.1142/S0219455408002764
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
This paper investigates the prebuckling dynamics of transversely isotropic thin cylinder shells in the context of propagation and reflection of axial stress waves. By constructing the Hamiltonian system of the governing equation, the symplectic eigenvalues and eigenfunctions are obtained directly and rationally without the need for any trial shape functions, such as the classical semi-inverse method. The critical loads and buckling models are reduced to the problem of eigenvalues and eigensolutions, in which zero-eigenvalue solutions and nonzero-eigenvalue solutions correspond to axisymmetric buckling and nonaxisymmetric buckling, respectively. Numerical results reveal that energy is concentrated at the unconstrained free ends of the shell and the buckling modes have bigger bell-mouthed shapes at these positions.
引用
收藏
页码:487 / 504
页数:18
相关论文
共 50 条
  • [41] BUCKLING OF INELASTIC CYLINDRICAL-SHELLS UNDER AXIAL IMPACT
    GORDIENKO, BA
    ARCHIVES OF MECHANICS, 1972, 24 (03): : 383 - +
  • [42] BUCKLING OF THICK ORTHOTROPIC CYLINDRICAL-SHELLS UNDER EXTERNAL-PRESSURE AND STABILITY LOSS IN THICK TRANSVERSELY ISOTROPIC CYLINDRICAL-SHELLS UNDER AXIAL-COMPRESSION
    DONG, SB
    JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 1994, 61 (01): : 225 - 225
  • [43] NONLINEAR RESPONSE OF CYLINDRICAL SHELLS SUBJECTED TO DYNAMIC AXIAL LOADS
    ROTH, RS
    KLOSNER, JM
    AIAA JOURNAL, 1964, 2 (10) : 1788 - 1794
  • [44] Inelastic Buckling of FGM Cylindrical Shells Subjected to Combined Axial and Torsional Loads
    Huang, Huaiwei
    Zhang, Yongqiang
    Han, Qiang
    INTERNATIONAL JOURNAL OF STRUCTURAL STABILITY AND DYNAMICS, 2017, 17 (09)
  • [45] On the influence of laminate stacking on buckling of composite cylindrical shells subjected to axial compression
    Geier, B
    Meyer-Piening, HR
    Zimmermann, R
    COMPOSITE STRUCTURES, 2002, 55 (04) : 467 - 474
  • [46] Experimental investigation of buckling behavior of cracked cylindrical shells subjected to axial compression
    Ifayefunmi, O.
    Kasiman, Norehan
    Khan, Hazrin Ibrahim
    PROCEEDINGS OF MECHANICAL ENGINEERING RESEARCH DAY 2016, 2016, : 153 - 154
  • [47] DYNAMICS AND FAILURE OF CYLINDRICAL-SHELLS SUBJECTED TO AXIAL IMPACT
    MAYMON, G
    LIBAI, A
    AIAA JOURNAL, 1977, 15 (11) : 1624 - 1630
  • [48] Dynamic pulse buckling of cylindrical shells subjected to external impulsive loading
    Gu, W
    Tang, W
    Liu, T
    JOURNAL OF PRESSURE VESSEL TECHNOLOGY-TRANSACTIONS OF THE ASME, 1996, 118 (01): : 33 - 37
  • [49] DYNAMIC AXIAL PLASTIC BUCKLING OF STRINGER STIFFENED CYLINDRICAL-SHELLS
    JONES, N
    PAPAGEORGIOU, EA
    INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES, 1982, 24 (01) : 1 - 20
  • [50] Asymmetric buckling analysis of cylindrical shells under axial dynamic loads
    Liu, Li
    Liu, Tuguang
    Li, Tianyun
    Jiang, Songqing
    Huazhong Ligong Daxue Xuebao/Journal Huazhong (Central China) University of Science and Technology, 27 (06): : 95 - 97