An experimental and theoretical investigation of the effect of general imperfections on the buckling load of a circular cylindrical shell under axial compression was carried out. A noncontact probe has been used to make complete imperfection surveys on electro-formed copper shells before and during the loading process up to the buckling load. The data recording process has been fully automated and the data reduction was done on an IBM 7094. Three-dimensional plots were obtained of the measured initial imperfection surfaces and of the growth of these imperfections under increasing axial load. The modal components of the measured imperfection surfaces were also obtained. The theoretical solution located the limit points of the postbuckled states. A simplified imperfection model was used consisting of one axisymmetric and two asymmetric components. For global buckling the correlation between the theoretical buckling loads and the experimental values was found to be good.
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March 1969
Research Papers
The Effect of General Imperfections on the Buckling of Cylindrical Shells
Johann A´rbocz,
Johann A´rbocz
California Institute of Technology, Firestone Flight Sciences Laboratory, Pasadena, Calif.
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Charles D. Babcock, Jr.
Charles D. Babcock, Jr.
California Institute of Technology, Firestone Flight Sciences Laboratory, Pasadena, Calif.
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Johann A´rbocz
California Institute of Technology, Firestone Flight Sciences Laboratory, Pasadena, Calif.
Charles D. Babcock, Jr.
California Institute of Technology, Firestone Flight Sciences Laboratory, Pasadena, Calif.
J. Appl. Mech. Mar 1969, 36(1): 28-38 (11 pages)
Published Online: March 1, 1969
Article history
Received:
July 1, 1968
Online:
September 14, 2011
Citation
A´rbocz, J., and Babcock, C. D., Jr. (March 1, 1969). "The Effect of General Imperfections on the Buckling of Cylindrical Shells." ASME. J. Appl. Mech. March 1969; 36(1): 28–38. https://doi.org/10.1115/1.3564582
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