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Woven thermoplastic composite forming simulation with solid-shell element method

机译:编织热塑性复合材料成形的固体-壳单元法

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Textile composites become more and more popular in aeronautic industries, due to their high performances. In this work, based on the model shown in the paper [9], a solid-shell element is used to simulate the woven composite forming. Comparing with other shell elements, a distinctive advantage of solid-shell elements is that the complication on handing finite rotations does not exist. Accounting the specific mechanical behaviors of woven composite material, the tensile, in-plane shear, bending and compressive energies are taken into account depending on the fiber direction, and then the total strain energy is computed to be the sum of those energies. The necessary material data for the simulation come from standard tensile, compressive and bias test experiments. Some forming simulations are performed with this method, and we can observe the wrinkles that exhibit the influence of bending stiffness. The results show the efficiency of the approach.
机译:纺织复合材料由于其高性能而在航空工业中越来越受欢迎。在这项工作中,基于论文[9]所示的模型,使用了一个固体单元来模拟机织复合材料的成型。与其他壳体元素相比,固体壳体元素的显着优势是不存在处理有限旋转的复杂性。考虑到编织复合材料的特定机械性能,根据纤维方向将拉伸,面内剪切,弯曲和压缩能考虑在内,然后将总应变能计算为这些能量的总和。模拟所需的材料数据来自标准的拉伸,压缩和偏置测试实验。用这种方法进行了一些成形模拟,我们可以观察到表现出弯曲刚度影响的皱纹。结果表明了该方法的有效性。

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