Supporting power and optimal design of rigid plastic cylindrical shells

1984 ◽  
Vol 20 (5) ◽  
pp. 433-438
Author(s):  
A. S. Dekhtyar' ◽  
A. O. Rasskazov ◽  
V. S. Rublev
AIAA Journal ◽  
1980 ◽  
Vol 18 (8) ◽  
pp. 1020-1022 ◽  
Author(s):  
Michael Pappas ◽  
Jacob Moradi

1973 ◽  
Vol 95 (1) ◽  
pp. 215-218 ◽  
Author(s):  
H. M. Haydl ◽  
A. N. Sherbourne

This paper suggests a simple numerical approach to the limit analysis of cantilever cylindrical shells. The loads considered are external pressure and external pressure combined with a moment at the free shell end. It is shown that the collapse loads are within 4.5 percent on the safe side of the exact von Mises limit loads. The extension of the method of analysis to more complex problems is suggested.


1999 ◽  
Vol 18 (2-3) ◽  
pp. 116-125
Author(s):  
T. Lepikult ◽  
W. H. Schmidt ◽  
H. Werner

1999 ◽  
Vol 18 (2) ◽  
pp. 116
Author(s):  
T. Lepikult ◽  
W.H. Schmidt ◽  
H. Werner

1970 ◽  
Vol 37 (2) ◽  
pp. 416-425 ◽  
Author(s):  
Norman Jones

A theoretical investigation is herein undertaken in order to examine the response of circular cylindrical shells subjected to dynamic loads of an intensity sufficient to cause large permanent deformations. The shell material is assumed to be rigid, perfectly plastic and the influence of finite deflections is retained in the governing equations. It emerges clearly from the study that geometry changes influence markedly the shell behavior even for quite small deflections and, therefore, they should be retained in any dynamic analyses of cylindrical shells with axial restraints.


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