Loading…
Nature inspired optimization techniques for the design optimization of laminated composite structures using failure criteria
► Comparison of the nature inspired optimization techniques such as VEPSO and GA are considered along with the comparison of different failure criteria are considered for the study. ► Optimum weight predictions obtained for three different failure criteria by VEPSO and GA are evaluated for different...
Saved in:
Published in: | Expert systems with applications 2011-03, Vol.38 (3), p.2489-2499 |
---|---|
Main Authors: | , , , |
Format: | Article |
Language: | English |
Subjects: | |
Citations: | Items that this one cites Items that cite this one |
Online Access: | Get full text |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Summary: | ► Comparison of the nature inspired optimization techniques such as
VEPSO and
GA are considered along with the comparison of different failure criteria are considered for the study. ► Optimum weight predictions obtained for three different failure criteria by
VEPSO and
GA are evaluated for different loading conditions. ► Optimization using
VEPSO and
GA shows that, the optimum weight of the laminate predicted by Tsai–Wu criterion differ considerably than the predictions made by MS and FMB failure criteria. ► It is found that, there is an enormous difference in the prediction of weight of the laminate in the third-quadrant of the failure envelope, in this quadrant the laminate is subjected to biaxial compressive loading. ► The effect of stacking sequence is also studied and it is noted that as the stacking sequence of the laminate varies the optimum weight of the laminate varies. ► Both
VEPSO and
GA agree reasonably well, except there are very marginal difference, for certain types of loading combinations and stacking sequence.
The design optimization of laminated composites using naturally inspired optimization techniques such as vector evaluated particle swarm optimization (
VEPSO) and genetic algorithms (
GA) are used in this paper. The design optimization of minimum weight of the laminated composite is evaluated using different failure criteria. The failure criteria considered are maximum stress (
MS), Tsai–Wu (
TW) and failure mechanism based (
FMB) failure criteria. Minimum weight of the laminates are obtained for different failure criteria using
VEPSO and
GA for different combinations of loading. From the study it is evident that
VEPSO and
GA predict almost the same minimum weight of the laminate for the given loading. Comparison of minimum weight of the laminates by different failure criteria differ for some loading combinations. The comparison shows that
FMBFC provide better results for all combinations of loading. |
---|---|
ISSN: | 0957-4174 1873-6793 |
DOI: | 10.1016/j.eswa.2010.08.038 |