The chessboard buckle pattern in the solution of the linearized Donnell equations for buckling of a thin, cylindrical shell under axial compression is so sensitive to uncertainties in shell dimensions that the number of circumferential waves and the aspect ratio of the buckles is indeterminate. This problem is treated statistically. Shell dimensions are treated as random variables with probability distributions dependent on nominal values and manufacturing tolerances. Distributions for aspect ratio and number of circumferential waves are found by a Monte-Carlo technique. It is found that the linear theory does contain a mechanism for distinguishing among buckle modes. There is always a preferred buckle mode. For thin shells and attainable manufacturing tolerances, the aspect ratio of the preferred mode is closer to one than that of any other possible mode, and the corresponding number of buckles is large.
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December 1965
Research Papers
The Preferred Mode Shape in the Linear Buckling of Circular Cylindrical Shells Under Axial Compression
P. Mann-Nachbar,
P. Mann-Nachbar
Lockheed Missiles and Space Company, Palo Alto, Calif.
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W. Nachbar
W. Nachbar
Aeronautics and Astronautics, Stanford University, Stanford, Calif.
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P. Mann-Nachbar
Lockheed Missiles and Space Company, Palo Alto, Calif.
W. Nachbar
Aeronautics and Astronautics, Stanford University, Stanford, Calif.
J. Appl. Mech. Dec 1965, 32(4): 793-802 (10 pages)
Published Online: December 1, 1965
Article history
Received:
July 2, 1964
Revised:
April 21, 1965
Online:
September 15, 2011
Citation
Mann-Nachbar, P., and Nachbar, W. (December 1, 1965). "The Preferred Mode Shape in the Linear Buckling of Circular Cylindrical Shells Under Axial Compression." ASME. J. Appl. Mech. December 1965; 32(4): 793–802. https://doi.org/10.1115/1.3627318
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