Optimal Design of Composite Lateral Wing Upper Covers Based on Non-Linear Buckling Analysis

Author(s):  
E. Barkanov ◽  
S. Gluhih ◽  
O. Ozolinš ◽  
E. Eglitis ◽  
F. Almeida ◽  
...  
2014 ◽  
Vol 38 ◽  
pp. 1-8 ◽  
Author(s):  
E. Barkanov ◽  
O. Ozoliņš ◽  
E. Eglītis ◽  
F. Almeida ◽  
M.C. Bowering ◽  
...  

2009 ◽  
Vol 31 (1) ◽  
pp. 17-30 ◽  
Author(s):  
Dao Huy Bich

In the present paper the non-linear buckling analysis of functionally graded spherical shells subjected to external pressure is investigated. The material properties are graded in the thickness direction according to the power-law distribution in terms of volume fractions of the constituents of the material. In the formulation of governing equations geometric non-linearity in all strain-displacement relations of the shell is considered. Using Bubnov-Galerkin's method to solve the problem an approximated analytical expression of non-linear buckling loads of functionally graded spherical shells is obtained, that allows easily to investigate stability behaviors of the shell.


2017 ◽  
Vol 2 (4) ◽  
pp. 293-300 ◽  
Author(s):  
SB. Pranesh ◽  
Deepak Kumar ◽  
V. Anantha Subramanian ◽  
D. Sathianarayanan ◽  
GA. Ramadass

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