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Finite-element formulation for analysis of laminated composites

机译:用于层压复合材料分析的有限元公式

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This paper presents a multilayered/multidirector and shear-deformable finite-element formulation of shells for the analysis of composite laminates. The displacement field is assumed continuous across the finite-element layers through the composite thickness. The rotation field is, however, layerwise continuous and is assumed discontinuous across these layers. This kinematic hypothesis results in independent shear deformation of the director associated with each individual layer and thus allows the warping of the composite cross section. The resulting through-thickness strain field is therefore discontinuous across the different material sets. Numerical results are presented to show the performance of the method.
机译:本文提出了一种用于复合材料层压板分析的多层/多向和可剪切变形壳的有限元公式。假定位移场在整个复合材料厚度的有限元层上是连续的。但是,旋转场是逐层连续的,并且假定在这些层之间是不连续的。该运动学假说导致与每个单独层相关的指向矢的独立剪切变形,从而允许复合截面的翘曲。因此,所产生的贯穿厚度应变场在不同材料组之间是不连续的。数值结果表明了该方法的有效性。

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