经典层合板理论（Classical laminate Theory, CLT）构成了层合板复合材料结构的剖析基础，并且是ESAComp软件中大大都剖析的基础。
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A design oriented structural analysis capability for filament wound composite pressure vessels that utilize membrane theory and classical laminate plate theory is described. The paper focuses on the filament wound composite pressure vessel model definition and associated analytical formulation.
基于薄膜理论和经典层合板理论 ,导出了纤维缠绕轴对称壳的薄膜内力、应力、应变和位移等计算公式 ,旨在探讨一种面向纤维缠绕复合材料压力容器设计的结构分析方法。
参考来源 - 面向设计的纤维缠绕复合材料压力容器结构分析方法·2,447,543篇论文数据，部分数据来源于NoteExpress
介绍用于复合材料层合板理论计算的经典层合板理论、一阶剪切变形理论以及高阶剪切变形理论及其各种简化形式，重点介绍了前两者理论。
This chapter shows some laminate theories such as the Classical Plate Theory and the first Order Shear Deformation Theory and the High Order Shear Deformation Theory and it's simple forms firstly.
基于经典的层合板理论及板的大挠度基本假设，得到四边简支层合板的非线性运动方程及变形协调方程；
On the basis of classical lamination theory and large deflection hypotheses of plate, the equilibrium and compatibility equations of simply supported composite laminated plates were obtained.
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