首页> 外文期刊>Composite Structures >Localized buckling in sandwich struts with inhomogeneous deformations in both face plates
【24h】

Localized buckling in sandwich struts with inhomogeneous deformations in both face plates

机译:夹心支柱中的局部屈曲,两个面板的变形均不均匀

获取原文
获取原文并翻译 | 示例
           

摘要

A nonlinear analytical model for investigating localized interactive buckling in simply supported thin-face plate sandwich struts with weak cores is extended to account for local deformations in both face plates, which have been observed in experiments and finite element simulations. The original model is based on potential energy principles with large displacement assumptions. It assumes Timoshenko shear deformable theory for the core and approximates the overall mode as a half-sine wave along the length of the strut while the local face plate displacements are initially unknown and are found as solutions of the governing equations. The extended model is able to capture measurable local face plate displacements in the less compressed face plate, beyond the secondary bifurcation which leads to localized interactive buckling, for the case where overall buckling is critical. Moreover, the allowance of local displacements in both face plates allows the extended model to predict the post-buckling behavior better in cases where local buckling is critical. The results from this model compare very well with nonlinear finite element simulations with respect to both the equilibrium paths and panel deformations. (C) 2015 Elsevier Ltd. All rights reserved.
机译:非线性分析模型用于研究具有弱芯的简单支撑薄面板夹层支撑中的局部相互作用屈曲,扩展了该模型以解决两个面板中的局部变形,这已在实验和有限元模拟中观察到。原始模型基于具有大位移假设的势能原理。它假定铁木辛柯剪切变形理论是针对岩心的,并且将整个模式近似为沿支杆长度的半正弦波,而局部面板的位移最初是未知的,并且可以作为控制方程的解。对于整体屈曲至关重要的情况,扩展模型能够捕获压缩程度较小的面板中可测量的局部面板位移,该位移超出了二次分叉,从而导致局部交互式屈曲。此外,在两个面板中都存在局部位移的情况下,在局部屈曲至关重要的情况下,扩展模型可以更好地预测屈曲后的行为。该模型的结果与非线性有限元模拟在平衡路径和面板变形方面都非常吻合。 (C)2015 Elsevier Ltd.保留所有权利。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号