A novel surrogate modeling strategy of the mechanical properties of 3D braided composites

被引:15
作者
Liu, Zeyi [1 ]
Hou, Yuliang [1 ]
Zhao, Qiaoli [1 ]
Li, Cheng [1 ]
机构
[1] Zhengzhou Univ, Sch Mech & Power Engn, Zhengzhou 450001, Peoples R China
基金
中国国家自然科学基金; 中国博士后科学基金;
关键词
Braided composites; Diffuse approximation; Elastic properties; Multiscale model; Surrogate model; DAMAGE SIMULATION; CELL MODEL; BEHAVIOR;
D O I
10.1016/j.cja.2020.05.017
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In this paper, a surrogate-based modeling methodology is developed and presented to predict the elastic properties of three dimensional (3D) four-directional braided composites. Using this approach, the prediction process becomes feasible with only a limited number of training points. The surrogate models constructed using Finite Element (FE) method and Diffuse Approximation, reduce the computational time and cost for preparing experimental samples. In the FE model, multiscale method is applied to couple the computations of elastic properties at microscale and mesoscale. Subsequently, a parametric study is performed to analyze the effects of the three design parameters on the elastic properties. Satisfactory results are obtained via the surrogate-based modeling predictions, which are compared with the experimental measurements. Moreover, the predictions obtained from surrogate models concur well with the FE predictions. This study orients a new direction for predicting the mechanical properties based on surrogate models which can effectively reduce the sample preparation cost and computational efforts. (C) 2020 Chinese Society of Aeronautics and Astronautics. Production and hosting by Elsevier Ltd.
引用
收藏
页码:2589 / 2601
页数:13
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