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ANALYTICAL SOLUTION FOR RECTANGULAR THICK LAMINATED PLATES SUBJECTED TO ARBITRARY BOUNDARY CONDITIONS

机译:矩形边界条件下矩形矩形厚板的解析解

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摘要

Three-dimensional deformations of a multilayered, linear elastic, anisotropic rectangular plate subjected to arbitrary boundary conditions at its edges are analyzed by the generalized Eshelby-Stroh formalism. The rectangular laminate consists of anisotropic and homogeneous laminae of arbitrary thicknesses. Perfect bonding is assumed between the adjoining laminae in the sense that both surface tractions and displacements are assumed to be continuous across their interfaces. The analytical solution is in terms of infinite series, and the effect of truncating the series on the accuracy of the solution is scrutinized. The method is also applicable to rectangular laminated plates, with edges of each lamina subjected to different boundary conditions. Results are presented for thick plates with different sets of edge boundary conditions ,e.g., two opposite edges simply supported and the other two subjected to eight different conditions or all four edges clamped.
机译:通过广义的Eshelby-Stroh形式主义分析了多层线性弹性各向异性矩形板在其边缘受到任意边界条件的三维变形。矩形层压板由任意厚度的各向异性和均质薄片组成。假定在表面的牵引力和位移在其界面上都是连续的,就可以认为相邻的层板之间具有完美的粘结。分析解是根据无穷级数来进行的,并且研​​究了将级数截断对解精度的影响。该方法也适用于矩形层压板,每个层压板的边缘要经受不同的边界条件。给出了具有不同边缘边界条件集的厚板的结果,例如,两个相对的边缘被简单支撑,而另外两个则经受八个不同条件或所有四个边缘被夹紧。

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