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Analytical solutions for the deformation of anisotropic elastic and piezothermoelastic laminated plates.

机译:各向异性弹性和压电热弹性层压板变形的解析解。

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摘要

The Eshelby-Stroh formalism is used to analyze the generalized plane strain quasistatic deformations of an anisotropic, linear elastic laminated plate. The formulation admits any set of boundary conditions on the edges and long faces of the laminate. Each lamina may be generally anisotropic with as many as 21 independent elastic constants. The three dimensional governing differential equations are satisfied at every point of the body. The boundary conditions and interface continuity conditions are satisfied in the sense of a Fourier series. Results are presented for three sample problems to illustrate the versatility of the method.The solution methodology is generalized to study the deformation of finite rectangular plates subjected to arbitrary boundary conditions. The effect of truncation of the series on the accuracy of the solution is carefully examined. Results are presented for thick plates with two opposite edges simply supported and the other two subjected to eight different boundary conditions. The results are compared with three different plate theories. The solution exhibits boundary layers at the edges except when they are simply supported. Results are presented in tabular form for different sets of edge boundary conditions to facilitate comparisons with predictions from various plate theories and finite element formulations.The Eshelby-Stroh formalism is also extended to study the generalized plane deformations of piezothermoelastic laminated plates. The method is capable of analyzing laminated plates with embedded piezothermoelastic patches. Results are presented for a thermoelastic problem and laminated elastic plates with piezothermoelastic lamina attached to its top surface. When a PZT actuator patch is attached to an elastic cantilever substrate, it is observed that the transverse shear stress and transverse normal stress are very large at the corners of the PZT-substrate interface.This dissertation is organized in the form of three self-contained chapters each of which will be submitted for possible publication in a journal.This work was parially supported by the NSF grant CMS9713453 and the ARO grant DAAG55-98-1-0030 to Virginia Polytechnic Institute and State University.
机译:Eshelby-Stroh形式主义用于分析各向异性线性弹性层压板的广义平面应变准静态变形。该配方允许在层压板的边缘和长表面上使用任何边界条件集。每个层通常可以是各向异性的,具有多达21个独立的弹性常数。在人体的每个点都满足三维控制微分方程。在傅立叶级数的意义上满足边界条件和界面连续性条件。给出了三个样本问题的结果,以说明该方法的通用性。推广了求解方法,以研究有限矩形板在任意边界条件下的变形。仔细检查了序列的截断对求解精度的影响。给出了厚板的结果,该厚板的两个相对边缘被简单支撑,另外两个则受到八个不同边界条件的影响。将结果与三种不同的板理论进行比较。该解决方案在边缘处显示边界层,除非简单支撑它们。结果以表格形式显示了不同边缘边界条件的集合,以利于与各种板理论和有限元公式的预测进行比较.Eshelby-Stroh形式主义还扩展到研究压电热弹性层压板的广义平面变形。该方法能够分析具有嵌入式热弹性补丁的叠层板。给出了一个热弹性问题的结果,以及在其顶面上附着了压电热弹性薄片的层压弹性板。当将PZT执行器贴片附着到弹性悬臂基板上时,在PZT-基板界面的各个角落处的横向剪切应力和横向法向应力非常大。本论文以三个独立的形式组织NSF赠款CMS9713453和ARO赠款DAAG55-98-1-0030分别由弗吉尼亚理工学院和州立大学提供支持,这项工作得到了部分支持。

著录项

  • 作者

    Vel, Senthil Subramanian.;

  • 作者单位

    Virginia Polytechnic Institute and State University.;

  • 授予单位 Virginia Polytechnic Institute and State University.;
  • 学科 Engineering Aerospace.Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 1998
  • 页码 135 p.
  • 总页数 135
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-17 11:48:25

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