2. Post-buckling behaviour of perfect and randomly imperfect grid shell structures

1993 ◽  
pp. 1: 9-15 ◽  
Author(s):  
O. Bacco ◽  
C. Borri
Author(s):  
A I Siyanov ◽  
M Rynkovskaya ◽  
E Tupikova

2001 ◽  
Vol 23 (1) ◽  
pp. 29-36 ◽  
Author(s):  
S.M.L Adriaenssens ◽  
M.R Barnes
Keyword(s):  

2021 ◽  
Vol 157 (A1) ◽  
Author(s):  
X-Y Ni ◽  
B G Prusty ◽  
A K Hellier

Stiffened panels made out of isotropic or anisotropic materials are being extensively used as structural elements for aircraft, maritime, and other structures. In order to maintain stiffness and strength with light weight, new design techniques must be employed when utilising these materials. Their stability, ultimate strength and loading capacity are the key issues pertaining to these engineering structures which have attracted a number of investigators to undertake in- depth research, either in an academic or actual engineering context. This paper provides an extensive review of the research which has been conducted in recent years (2000-2012) on the buckling and post-buckling response of isotropic and composite stiffened plate and shell structures related to analysis and experiment. The key objective of this review article is to collate the research performed in the area of buckling and post-buckling behaviour of stiffened structures, thereby giving a broad perspective of the state-of-the-art in this field.


1989 ◽  
Vol 111 (2) ◽  
pp. 88-96 ◽  
Author(s):  
R. K. Kapania

Laminated shell structures are increasingly being used in chemical, mechanical, marine and aerospace applications. A significant amount of research has been conducted in the past on studying the structural response of these structures. A review of various investigations on the analysis of these shells is given here. Specifically, this review deals with the development of various theories for modeling the thick laminated shells, including shear effects; analytical studies, development of various finite elements to model these shells, including applications to tire modeling; buckling and post-buckling analysis of perfect and imperfect laminated shells; and vibration and dynamic response analysis of various laminated shells.


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