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基于Ｓｃｈａｐｅｒｙ积分型粘弹性本构关系，推导了考虑横向剪切效应的复合材料层合板线性热粘弹性有限元分析列式，对层合板的粘弹性响应和加工成型过程中的残余应力进行了分析，给出一些有意义的结果
Based on the Schapery integral viscoelastic constitutive equation, the linear thermal viscoelastic finite element analysis of composite laminates with transverse shear effect is deduced, and the viscoelastic response of laminates and the residual stress in the process of forming are analyzed , Gives some meaningful results