用于立方体卫星的织物增强复合材料粘塑性弯曲响应的分析模拟和实验验证

IF 4.3 3区 材料科学 Q1 ENGINEERING, ELECTRICAL & ELECTRONIC ACS Applied Electronic Materials Pub Date : 2024-01-16 DOI:10.1016/j.ejrs.2023.12.005
Ehsan Shafiei , Gasser Abdelal
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引用次数: 0

摘要

本研究介绍了一种分析纺织品增强层压复合材料弯曲变形和强度的创新方法,这对立方体卫星结构至关重要。我们的研究开发了一个双尺度建模框架:一个微尺度模型,捕捉纤维和基体的详细粘弹性-粘塑性行为;一个中尺度模型,将其与纺织品几何形状、先进的剪切变形理论和分布式损伤效应整合在一起。广泛的实验室实验验证了我们的模型,证实了它在各种条件下预测复合材料行为的准确性。这项工作显著增强了对纺织品增强复合材料的理解和预测,对立方体卫星的结构设计和性能具有重要意义。
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Analytical simulation and experimental validation of viscoplastic bending response of textile-reinforced composites for CubeSats

This study introduces an innovative approach for analyzing bending deformation and strength in textile-reinforced laminated composites, which is crucial for CubeSat structures. Our research develops a dual-scale modelling framework: a microscale model capturing the detailed viscoelastic-viscoplastic behaviour of fibres and matrices and a mesoscale model that integrates this with textile geometry, advanced shear deformation theories, and distributed damage effects. Extensive laboratory experiments validate our model, confirming its accuracy in predicting the composite behaviour under varied conditions. This work notably enhances the understanding and prediction of textile-reinforced composites, offering significant implications for CubeSat structural design and performance.

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来源期刊
CiteScore
7.20
自引率
4.30%
发文量
567
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