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

被引:361
作者
LERICHE, R
HAFTKA, RT
机构
[1] Department of Aerospace and Ocean Engineering, Virginia Polytechnic Institute and State University, Blacksburg, VA
基金
美国国家航空航天局;
关键词
D O I
10.2514/3.11710
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
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 mutation, and the probability of crossover are optimized by numerical experiments. A new genetic operator-permutation-is proposed and shown to be effective in reducing the cost of the genetic search. Results are obtained for a graphite-epoxy plate, first when only the buckling load is considered, and then when constraints on ply contiguity and strain failure are added. The influence on the genetic search of the penalty parameter enforcing the contiguity constraint is studied. The advantage of the genetic algorithm in producing several near-optimal designs is discussed.
引用
收藏
页码:951 / 956
页数:6
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