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Three-dimensional stress analysis for laminated composite and sandwich structures

机译:层状复合材料和夹层结构的三维应力分析

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Accurate stress prediction in composite laminates is crucial for safe design under different loading conditions. Classical laminated theory, i.e. those based on the Euler-Bernoulli and Kirchhoff hypotheses, respectively for beams and plates/shells are inaccurate for relatively thick laminates as three-dimensional (3D) effects such as transverse shear and normal deformations are neglected. Therefore, 3D finite element models are often employed for accurate stress analysis. However, these models are computationally expensive when used for laminates with a large number of layers, in optimisation studies, or for non-linear analyses. To address this issue, a Unified Formulation approach is presented for the analysis of laminated, slender beam-like structures. To define the kinematic field over the beam's cross-section, a recently developed hierarchical set of expansion functions, based on Serendipity Lagrange expansions, are employed and adapted to the layer-wise approach. The present formulation, which has displacements as degrees of freedom, does not ensure continuous transverse stresses across layer interfaces. Thus, an extra post-processing step is required to capture these stresses accurately. The proposed model is benchmarked against a 3D closed-form solution, 3D finite elements, and results available in the literature by means of static analyses of highly heterogeneous, laminated composite and sandwich beams. A key advantage of the present model is its ability to predict accurate 3D stress fields efficiently, including boundary layer regions, i.e. towards clamped ends. As a result, global analyses (e.g. overall displacements, buckling, etc.) and local analyses (e.g. stress concentrations) are combined within a single, computationally efficient model. The performance of the proposed approach, in terms of computational cost and precision, is assessed. Significant computational efficiency gains over 3D finite elements are observed for similar levels of accuracy.
机译:复合材料层压板中的准确应力预测对于不同负载条件下的安全设计至关重要。经典的叠层理论,即分别基于梁和板/壳的Euler-Bernoulli和Kirchhoff假设的理论对于相对较厚的叠层是不准确的,因为忽略了三维(3D)效应,例如横向剪切和法向变形。因此,经常使用3D有限元模型进行精确的应力分析。但是,这些模型在具有大量层的层压板,优化研究或非线性分析中使用时,计算量很大。为了解决这个问题,提出了一种统一配方方法,用于分析层压的细长梁状结构。为了定义梁横截面上的运动场,采用了基于Serendipity Lagrange展开的最近开发的分级展开函数集,并将其应用于分层方法。具有作为自由度的位移的本发明不能确保跨层界面的连续横向应力。因此,需要额外的后处理步骤以准确地捕获这些应力。所提出的模型以3D封闭形式的解决方案,3D有限元为基准,并且通过对高度异质,层合复合材料和夹层梁的静态分析,可以在文献中获得结果。本模型的主要优点是其能够有效地预测准确的3D应力场的能力,包括边界层区域,即朝向被夹紧的端部。结果,将整体分析(例如,整体位移,屈曲等)和局部分析(例如,应力集中)组合在一个有效的计算模型中。在计算成本和精度方面,评估了所提出方法的性能。对于相似的精度水平,可以观察到3D有限元的计算效率显着提高。

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