首页> 外文期刊>International Journal of Computational Methods and Experimental Measurements >FUNDAMENTAL SOLUTIONS FOR THE GENERAL LAMINATE PROBLEM WITH THE STRESS FUNCTION FORMALISM
【24h】

FUNDAMENTAL SOLUTIONS FOR THE GENERAL LAMINATE PROBLEM WITH THE STRESS FUNCTION FORMALISM

机译:对压力函数形式主义的一般层压件问题的基本解决方案

获取原文
获取原文并翻译 | 示例
           

摘要

The linear coupled stretching-bending problem for general laminates is here formulated with the mid-plane stress function and the lateral deflection as independent field variables. A mathematical similarity between the two problems is achieved by introducing a re-arranged mid-plane strain tensor as one of the dependent variables. As a step towards a genuine boundary element solution for this problem, its fundamental solutions are derived using a Fourier transform approach. First, the transforms of the solutions are obtained in terms of the transform space variables and their inverses are deduced using complex integral calculus. Through the use of these fundamental solutions, boundary integral equations of the linear coupled stretching-bending problem are formulated without the presence of any irreducible domain integrals. Issues regarding the numerical implementation of this formulation are raised and discussed.
机译:作为一般层压板的线性耦合拉伸弯曲问题在此配制在内平面应力函数和作为独立场变量的横向偏转。 通过将重新排列的中平面应变张量引入作为所属变量之一来实现这两个问题之间的数学相似性。 作为对该问题的真正边界元件解决方案的一步,它的基本解决方案是使用傅里叶变换方法导出的。 首先,在变换空间变量方面获得解决方案的变换,并且使用复杂的积分微积分推导出它们的逆。 通过使用这些基本解决方案,在没有任何不可缩小的结构域积分的情况下配制线性耦合拉伸弯曲问题的边界积分方程。 提出并讨论了关于该制剂的数值执行的问题。

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