Composite laminate shells have been applied more and more widely in aerospace structures . in order to increase thrust to weight ratio and improve the comprehensive performance of airplane , optimization design must be carried out . this thesis brings forward utilizing the method of aga - fem , which combines adaptive genetic algorithm ( aga ) and finite element method ( fem ) , to optimize fibre - reinforced composite shells 本文提出采用自適應(yīng)遺傳算法( adaptivegeneticalgorithm )和有限元方法( finiteelementmethod , fem )結(jié)合即aga - fem方法進(jìn)行纖維增強(qiáng)型復(fù)合材料層合殼結(jié)構(gòu)的優(yōu)化設(shè)計(jì),并對(duì)某航空發(fā)動(dòng)機(jī)復(fù)合材料機(jī)匣進(jìn)行優(yōu)化設(shè)計(jì)分析,取得了很好的效果。