OS0905 Plastic Buckling Behavior of Thin-Walled Cylindrical Shells under Impact Loading

2008 ◽  
Vol 2008 (0) ◽  
pp. _OS0905-1_-_OS0905-2_
Author(s):  
Takayuki KUSAKA ◽  
Hiroki HYODO
2018 ◽  
Vol 877 ◽  
pp. 453-459
Author(s):  
B. Angelina Catherine ◽  
R.S. Priyadarsini

Buckling is a prominent condition of instability caused to a shell structure as a result of axial loadings. The process of buckling becomes more complex while analyzing thin walled structures like shells. Today such thin walled laminated composite shells are gaining more importance in many defense and industrial applications since they have greater structural efficiency and performance in relation to isotropic structures. Comprehensive understanding of the buckling response of shell structures is necessary to assure the integrity of these shells during their service life. The presence of defects, such as cracks, may severely compromise their buckling behavior and jeopardize the structural integrity. This work aims in conducting numerical analysis of cracked GFRP (Glass fibre-reinforced polymer) composite cylindrical shells under combined loading to study the effect of crack size on the buckling behavior of laminated composite cylindrical shells with different lay-up sequences. The numerical analyses were carried out using the finite element software, ABAQUS in order to predict the buckling behaviour of cracked laminated composite cylinders subject to different combinations of axial compression, torsion, internal pressure and external pressure from the interaction buckling curves.


2013 ◽  
Vol 135 (5) ◽  
Author(s):  
Xinsheng Xu ◽  
Jiabin Sun ◽  
C. W. Lim

This study is mainly concerned with the analytical solutions of plastic bifurcation buckling of cylindrical shells under compressive load. The analysis is based on the J2 deformation theory with a linear hardening and proportional loading is adopted in the calculation. A symplectic solution system is established and Hamilton's governing equations are derived from the Hamilton variational principle. The basic problem in plastic buckling is converted into solving for the symplectic eigenvalues and eigensolutions, respectively. The obtained results reveal that boundary conditions have a very limited influence on bucking loads but its influence on buckling modes and plastic borders cannot be neglected. Meanwhile, it is demonstrated that the shell material properties significantly affect the plastic buckling behavior. This proposed symplectic method is shown to be a rigorous approach. It also provides a uniform and systematic way to any other similar problems.


1998 ◽  
Vol 1 ◽  
pp. 65-72
Author(s):  
Kouichi KOHNO ◽  
Kaoru YOKOYAMA ◽  
Masatoshi NAKAZAWA ◽  
Tetsuo IWAKUMA

2007 ◽  
Vol 56 (11) ◽  
pp. 1042-1048 ◽  
Author(s):  
Yoshiaki NAKAZAWA ◽  
Kenji TAMURA ◽  
Takayuki KUSAKA ◽  
Michitaka YOSHIDA ◽  
Masaki HOJO

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