Optimization of Laminated Composite Plates for Maximum Biaxial Buckling Load
Keyword(s):
This paper proposes an optimization procedure for maximization of the biaxial buckling load of laminated composite plates using the gradient-based interior-point optimization algorithm. The fiber orientation angle and the thickness of each lamina are considered as continuous design variables of the problem. The effect of the number of layers, fiber orientation angles, thickness and length to thickness ratios on the buckling load of the laminated composite plates under biaxial compression is investigated. The effectiveness of the optimization procedure in this study is compared with previous works.
2014 ◽
Vol 709
◽
pp. 144-147
2014 ◽
Vol 709
◽
pp. 135-138
2007 ◽
Vol 334-335
◽
pp. 89-92
◽
2012 ◽
Vol 19
(3)
◽
pp. 323-330
◽
2014 ◽
Vol 709
◽
pp. 130-134
2014 ◽
Vol 21
(4)
◽
pp. 551-558
◽
1985 ◽
Vol 9
(1)
◽
pp. 45-50
◽
Experimental and Numerical Buckling Analyses of Laminated Composite Plates under Temperature Effects
2010 ◽
Vol 19
(4)
◽
pp. 096369351001900
◽
2004 ◽
Vol 64
(7-8)
◽
pp. 1049-1056
◽
2007 ◽
Vol 348-349
◽
pp. 725-728
◽