OPTIMIZATION OF LAMINATE STACKING-SEQUENCE FOR BUCKLING LOAD MAXIMIZATION BY GENETIC ALGORITHM

Citation
R. Leriche et Rt. Haftka, OPTIMIZATION OF LAMINATE STACKING-SEQUENCE FOR BUCKLING LOAD MAXIMIZATION BY GENETIC ALGORITHM, AIAA journal, 31(5), 1993, pp. 951-956
Citations number
11
Categorie Soggetti
Aerospace Engineering & Tecnology
Journal title
ISSN journal
00011452
Volume
31
Issue
5
Year of publication
1993
Pages
951 - 956
Database
ISI
SICI code
0001-1452(1993)31:5<951:OOLSFB>2.0.ZU;2-#
Abstract
The use of a genetic algorithm to optimize the stacking sequence of a composite laminate for buckling load maximization is studied. Various genetic parameters including the population size, the probability of m utation, and the probability of crossover are optimized by numerical e xperiments. A new genetic operator-permutation-is proposed and shown t o be effective in reducing the cost of the genetic search. Results are obtained for a graphite-epoxy plate, first when only the buckling loa d is considered, and then when constraints on ply contiguity and strai n failure are added. The influence on the genetic search of the penalt y parameter enforcing the contiguity constraint is studied. The advant age of the genetic algorithm in producing several near-optimal designs is discussed.