首页> 外文期刊>Archive of Applied Mechanics >Steady-state thermomechanical analysis of composite laminated plate with damage based on extended layerwise method
【24h】

Steady-state thermomechanical analysis of composite laminated plate with damage based on extended layerwise method

机译:基于扩展层法的损伤复合材料层合板稳态热力学分析

获取原文
获取原文并翻译 | 示例
           

摘要

A steady-state thermomechanical analysis model is established for the composite laminated plate with transverse cracks and delaminations based on the extended layerwise method. The one-dimensional weak and strong discontinuous functions are employed to simulate the interlaminar interfaces and the delaminations, respectively, while the transverse crack is simulated in the in-plane displacement fields by using the standard extended finite element method. The temperature field in the thickness direction is obtained by using a one-dimensional steady-state heat conduction equation and constructed with the linear Lagrange interpolation functions in the thickness direction. In several numerical examples, the proposed model is verified for the laminated plates with/without transverse crack and/or delaminations against the classic laminated plate theory, first-order shear deformation theory, Reddy's layerwise theory or three-dimensional elastic model.
机译:基于扩展的分层方法,建立了具有横向裂纹和分层的复合层合板的稳态热力学分析模型。利用一维的弱和强不连续函数分别模拟层间界面和分层,同时使用标准扩展有限元方法模拟平面内位移场中的横向裂纹。通过使用一维稳态热传导方程获得厚度方向上的温度场,并利用线性Lagrange插值函数构造厚度方向上的温度场。在几个数值示例中,根据经典的层压板理论,一阶剪切变形理论,Reddy的分层理论或三维弹性模型,对带有/不具有横向裂纹和/或分层的层压板的提出的模型进行了验证。

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