A nonlinear finite element analysis of laminated shells with a damage model

IF 5.3 Q2 MATERIALS SCIENCE, COMPOSITES Composites Part C Open Access Pub Date : 2024-08-21 DOI:10.1016/j.jcomc.2024.100505
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引用次数: 0

Abstract

This paper presents a study on the development and validation of a nonlinear finite element model for laminated composite shells, that considers a first-order shear deformation theory (FSDT) and an explicit through-thickness integration. The model integrates a meso-scale damage analysis that considers progressive matrix and fiber failures. The model is compared with envelopes of experimental curves extracted from 3-point bending test coupons and shows accurate predictions.

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采用损伤模型对层叠壳体进行非线性有限元分析
本文研究了层状复合材料壳体非线性有限元模型的开发和验证,该模型考虑了一阶剪切变形理论(FSDT)和明确的厚度积分。该模型集成了中尺度损伤分析,考虑了基体和纤维的渐进失效。该模型与从三点弯曲试验片中提取的实验曲线包络线进行了比较,结果显示预测准确。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Composites Part C Open Access
Composites Part C Open Access Engineering-Mechanical Engineering
CiteScore
8.60
自引率
2.40%
发文量
96
审稿时长
55 days
期刊最新文献
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