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Buckling of imperfect thick cylindrical shells and curved panels with different boundary conditions under external pressure

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Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
In this paper, the effects of initial imperfections on the buckling behavior of thick cylindrical shells and curved panels are investigated. It is assumed that the shell has an axisymmetric and periodic initial imperfection in the axial direction. The shell is assumed to have different boundary conditions and subjected to pure external pressure loading. Governing differential equations are developed on the basis of the second Piola-Kirchhoff stress tensor and are re- duced to a homogenous linear system of equations using the differential quadrature method. The effects of different boundary conditions, geometric ratios, curvature and imperfection parameter on the buckling behavior of isotropic thick cylindrical shells and curved panels are carefully discussed. The results obtained by the present method are verified with finite element solutions and those reported in the literature.
Rocznik
Strony
25--36
Opis fizyczny
Bibliogr. 17 poz., rys., tab.
Twórcy
  • Babol University of Technology, Department of Mechanical Engineering, Babol, Iran
autor
  • Babol University of Technology, Department of Mechanical Engineering, Babol, Iran
Bibliografia
  • 1. Brush D.O., Almroth B.O., 1975, Buckling of Bars, Plates and Shells, Chapter 5, McGraw-Hill, New York
  • 2. Bushnell D., 1985, Computerized Buckling Analysis of Shells, Martinus Nijhoff Publishers, Doedrecht
  • 3. Ciarlet P.G., 1988,Mathematical Elasticity, Vol. I, Three Dimensional Elasticity, North-Holland: Amsterdam
  • 4. Danielson D.A., Simmonds, J.G., 1969, Accurate buckling equations for arbitrary and cylindrical elastic shells, International Journal of Engineering Science, 7, 459
  • 5. Donnell L.H., 1933, Stability of Thin-Walled Tubes Under Torsion, NACA Rep. 479
  • 6. Elishakoff I., Li Y., Starners J.H., 2001, Non-Classical Problem in Theory of Elastic Stability, Cambridge University Press, Cambridge, 43-98
  • 7. Flugge W., 1960, Stresses in Shells, Springer-Verlag, Berlin, Heidelberg
  • 8. Gusic G., Combescure A., Jullien J.F., 2000, The influence of circumferential thickness variations on the buckling of cylindrical shells under lateral pressure, Computer Structures, 74, 461-477
  • 9. Kardomateas G.A., 1993, Stability loss in thick transversely isotropic cylindrical shells under axial compression, Journal of Applied. Mechanics (ASME), 60, 506
  • 10. Kardomateas G.A., 1996, Benchmark three-dimensional elasticity solution for the buckling of thick orthotropic cylindrical shells, Composites, Part B, 27, B(6), 569-580
  • 11. Koiter W.T., 1963, The effect of axisymmetric imperfection on the buckling of cylindrical shells under axial compression, Academia van Wetenschappen-Amsterdam, Series B, 66, 265-279
  • 12. Koiter W.T., 1980, Buckling of cylindrical shells under axial compression and external pressure: Thin shell theory new trends and applications, [In:] CISM Courses and Lectures, 40, W. Olszak (Edit.), Wien and New York, Springer, 77-87
  • 13. Koiter W.T., Elishakoff I., Li Y.W., Starnes J.H., 1994, Buckling of an axially compressed cylindrical shell of variable thickness, International Journal of Solids and Structures, 31, 6, 797-805
  • 14. Lai W.M., Rubin D., Krempl E., 1996, Introduction to Continuum Mechanics, 3rd ed. Butterworth-Heinemann, Massachusetts
  • 15. Nguyen T.H.L., Elishakoff I., Nguyen T.V., 2009, Buckling under external pressure of cylindrical shell with variable thickness, International Journal of Solids and Structures, 46, 4163-68
  • 16. Sanders J.L., 1963, Nonlinear theories of thin shells, Quarterly of Applied Mathematics, 21
  • 17. Shu C., 2000, Differential Quadrature and its Application in Engineering, London, Springer-Verlag
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-d5107971-eef8-4e95-83c0-60c23f2e1005
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