Numerical Relaxation Analysis of Carbon Fiber Reinforced Polymers

Q3 Materials Science
Flavia Palmeri, Lucia Lambertini, Susanna Laurenzi
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引用次数: 0

Abstract

Carbon fiber reinforced polymers are widely used to manufacture aerospace deployable structures. These structures are folded in launch configuration and then deployed in space for operational activities. Since the stowage of deployable structures in folded configuration occurs for long time, the understanding of the viscoelastic properties of the material is essential to predict the structural behavior during both the deployment phase and the operational life. In this work, numerical relaxation analysis is performed on the representative volume element (RVE) of a carbon fiber reinforced polymer using a homogenization approach at the microscale. This aims to predict the effects of matrix viscoelasticity on the structural performance of a deployable structure.

碳纤维增强聚合物的数值松弛分析
碳纤维增强聚合物被广泛用于制造航空航天可展开结构。这些结构在发射构型中折叠,然后部署到太空中进行操作活动。由于可展开结构在折叠状态下的存放时间较长,因此了解材料的粘弹性能对于预测其在展开阶段和运行寿命期间的结构行为至关重要。在这项工作中,采用微尺度均质化方法对碳纤维增强聚合物的代表性体积元素(RVE)进行了数值松弛分析。其目的是预测基体粘弹性对可部署结构的结构性能的影响。
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来源期刊
Macromolecular Symposia
Macromolecular Symposia Materials Science-Polymers and Plastics
CiteScore
1.50
自引率
0.00%
发文量
226
期刊介绍: Macromolecular Symposia presents state-of-the-art research articles in the field of macromolecular chemistry and physics. All submitted contributions are peer-reviewed to ensure a high quality of published manuscripts. Accepted articles will be typeset and published as a hardcover edition together with online publication at Wiley InterScience, thereby guaranteeing an immediate international dissemination.
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