Strength and axisymmetric deformation of laminate cylindrical shells under axial impact

1983 ◽  
Vol 18 (4) ◽  
pp. 449-456 ◽  
Author(s):  
A. E. Bogdanovich ◽  
E. G. Fel'dmane
1987 ◽  
Vol 23 (6) ◽  
pp. 669-692 ◽  
Author(s):  
H.E. Lindberg ◽  
M.B. Rubin ◽  
L.E. Schwer

1987 ◽  
Vol 54 (2) ◽  
pp. 287-291 ◽  
Author(s):  
G. W. Brodland ◽  
H. Cohen

Nonlinear equations are derived for the axisymmetric deformation of thin, cylindrical shells made of Mooney-Rivlin materials and subject to arbitrarily large strains and rotations. These equations are then implemented numerically using an energy minimization technique. Finally, an extensive parametric analysis is done of cylindrical shells which are clamped at one end and loaded with either a radial force or an edge moment uniformly distributed along the circumference of the other end.


2011 ◽  
Vol 243-249 ◽  
pp. 1326-1330
Author(s):  
Chao Zhang ◽  
Jian Long Ji ◽  
Jian Ping Lei

Thin-walled cylindrical shells are widely used in many industrial sectors as light structural elements. Determination of their buckling strength under various types of loading conditions is a crucial work for engineering design. Due to the needs of research of crashworthiness, dynamic buckling of cylindrical shells subjected to the strong axial impact becomes a frontier issue in recent years. The axial impact is a very complex dynamic process because of the coupling of multiple effects. In this paper, the buckling mechanism of cylindrical shells subjected to axial impact and the influences of boundary conditions, and energy absorption properties have been investigated by experiments.


2009 ◽  
Vol 31 (5) ◽  
pp. 1132-1140 ◽  
Author(s):  
Xinsheng Xu ◽  
Jianqing Ma ◽  
C.W. Lim ◽  
Hongjie Chu

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