A study has been made to determine the dynamic stability of an imperfect circular cylindrical shell subject to a step loading in the axial direction. In the analysis, the radial displacement of the shell is approximated by a finite degree-of-freedom system. The dynamic analysis includes not only the effect of the radial inertia, but also, in an approximate manner, that due to the axial inertia. The critical loads are determined by numerical integration of the equation of motion. Compared with the static case, there is a significant reduction of the dynamic buckling load for the high wave number range of the radial modes. It is concluded that due to frequency coupling between axial and radial motions, the axial inertia plays an essential role in characterizing the dynamic instability of a finite length shell.
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March 1975
Research Papers
Dynamic Stability of Cylindrical Shells Under Step Loading
Y. S. Tamura,
Y. S. Tamura
California Institute of Technology, Pasadena, Calif.
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C. D. Babcock
C. D. Babcock
California Institute of Technology, Pasadena, Calif.
Search for other works by this author on:
Y. S. Tamura
California Institute of Technology, Pasadena, Calif.
C. D. Babcock
California Institute of Technology, Pasadena, Calif.
J. Appl. Mech. Mar 1975, 42(1): 190-194 (5 pages)
Published Online: March 1, 1975
Article history
Received:
January 2, 1974
Revised:
January 21, 1974
Online:
July 12, 2010
Citation
Tamura, Y. S., and Babcock, C. D. (March 1, 1975). "Dynamic Stability of Cylindrical Shells Under Step Loading." ASME. J. Appl. Mech. March 1975; 42(1): 190–194. https://doi.org/10.1115/1.3423514
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