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遺傳算法( adaptivegeneticalgorithm )和有限元方法( finiteelementmethod , fem )結合即aga - fem方法進行纖維增強型復合材料層合殼結構的優(yōu)化設計,并對某航空發(fā)動機復合材料機匣進行優(yōu)化設計分析,取得了很好的效果。