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首页> 外文期刊>Thin-Walled Structures >Multiple wrinkling mode transitions in axially compressed cylindrical shell-substrate in dynamics
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Multiple wrinkling mode transitions in axially compressed cylindrical shell-substrate in dynamics

机译:多种皱纹模式在动力学中轴向压缩圆柱形壳体衬底的转变

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We propose an efficient computational model for predicting the surface wrinkling in axially compressed bi-layer cylindrical shell-substrate composites. To capture the transitions between the wrinkling modes in the far post-buckling regime, we use implicit dynamics. In this context we apply a generalized-alpha and an energy-decaying time stepping schemes that numerically dissipate in the high frequency range. The other components of the model are a geometrically exact, rotation-less, nonlinear shell finite element for the cylinder and an elastic foundation that represents the substrate. We show that the proposed computational model predicts the wrinkling pattern transition from axisymmetric to diamond-like mode, which is consistent with the numerical and laboratory experiments reported earlier. Furthermore, the results of our computational model show the existence of several diamond-like mode jumps in the post-buckling regime, a result that has not yet been reported for the axially compressed shell-substrate cylinders.
机译:我们提出了一种有效的计算模型,用于预测轴向压缩的双层圆柱形壳基复合材料中的表面皱纹。为了捕获远屈曲的制度的皱纹模式之间的过渡,我们使用隐式动态。在这种情况下,我们应用了在高频范围内数值散射的通用α和能量衰减时间踩踏方案。该模型的其他组件是用于圆柱的几何精确,旋转的非线性壳有限元,其具有代表基板的弹性基础。我们表明所提出的计算模型预测从轴对称到菱形模式的皱纹模式转变,这与前面报道的数值和实验室实验一致。此外,我们的计算模型的结果表明,在后屈曲的状态下跳跃的几种菱形模式的存在,这是尚未报道轴向压缩的壳体基板缸的结果。

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