Minimization of maximum failure criterion of laminated composite shell structure by optimizing distributed-material orientation
Minimization of maximum failure criterion of laminated composite shell structure by optimizing distributed-material orientation
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DOI:
10.1007/s00158-019-02435-z
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发表时间:
2020-04
影响因子:
3.9
通讯作者:
M. Shimoda;Yoshiaki Muramatsu;Ryosuke Tsukihara
中科院分区:
文献类型:
--
作者:
M. Shimoda;Yoshiaki Muramatsu;Ryosuke Tsukihara
In this study, we propose a distributed-parameter optimization method for the material-orientation design aiming at maximizing the strength of a laminated composite shell structure with anisotropic material, which is homogenized based on a laminate theory. The modified Tsai–Hill criterion is employed as a failure criterion in this study, and its maximum value is minimized with the state equation constraint. The issue of non-differentiability inherent in this min–max problem is avoided by transforming the singular local measure to a smooth differentiable integral functional using the Kreisselmeier–Steinhauser function. The optimum design problem is formulated as a distributed-parameter optimization problem, and the sensitivity function with respect to the material-orientation variation is theoretically derived based on a variational method. The optimal material-orientation variation is determined using the H1gradient method with Poisson’s equation proposed by the authors, where the sensitivity function are applied as Robin condition to vary and optimize the material-orientation distribution. We transfer the sensitivity function to the internal heat generation and determine the material-orientation variation using Poisson’s equation to ensure continuous distribution of material orientation. The optimum design examples show that the proposed optimization method can effectively and efficiently obtain the optimum material orientation with the smooth curvilinear distribution and minimize the maximum strength measured by a failure criterion.