The elasto-plastic buckling and postbuckling of imperfect, thin, circular cylindrical shells in axial compression is studied with the use of a mechanism model specifically designed to achieve an accurate representation of the developable polyhedral surface of Yoshimura. The formulation makes it possible to study the influence of asymmetric imperfection patterns of significantly larger amplitudes than previously treated. Elasto-plastic effects are included using a deformation theory of plasticity and Reissner’s variational principle. Material-sensitive load-shortening curves are obtained exhibiting initial-maximum values for the average axial stresses of imperfect shells that tend toward vanishingly small magnitudes with increasing radius-to-thickness ratio and attendant imperfections.
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June 1979
Research Papers
Limit Point Buckling Loads of Axially Compressed, Circular Cylindrical Shells—The Effect of Nonlinear Material Behavior
R. P. Nimmer,
R. P. Nimmer
General Electric Corporate Research and Development, Solid Mechanics Unit, Schenectady, N. Y. 12301
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J. Mayers
J. Mayers
Department of Aeronautics and Astronautics, Stanford University, Stanford, Calif. 94305
Search for other works by this author on:
R. P. Nimmer
General Electric Corporate Research and Development, Solid Mechanics Unit, Schenectady, N. Y. 12301
J. Mayers
Department of Aeronautics and Astronautics, Stanford University, Stanford, Calif. 94305
J. Appl. Mech. Jun 1979, 46(2): 386-392 (7 pages)
Published Online: June 1, 1979
Article history
Received:
March 1, 1978
Revised:
September 1, 1978
Online:
July 12, 2010
Citation
Nimmer, R. P., and Mayers, J. (June 1, 1979). "Limit Point Buckling Loads of Axially Compressed, Circular Cylindrical Shells—The Effect of Nonlinear Material Behavior." ASME. J. Appl. Mech. June 1979; 46(2): 386–392. https://doi.org/10.1115/1.3424560
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