微力学模型能否确定纤维增强聚合物复合材料中基质主导破坏的连续损伤模型输入?

IF 14.2 1区 材料科学 Q1 ENGINEERING, MULTIDISCIPLINARY
Wenkai Chang , L.R. Francis Rose , Bingnong Jiang , Anthony J. Kinloch , Chun Hui Wang
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引用次数: 0

摘要

连续损伤力学(CDM)仍然是分析纤维增强聚合物(FRP)层压板层内和层间损伤进展的最广泛采用和计算可行的方法。然而,它的应用需要大量的实验和经验估计的胶合层强度和韧性参数,其中许多缺乏标准化的测试方法,从而大大限制了其实际适用性。为了支持和潜在地补充这些实验成果,本研究引入了一种新的微力学损伤模型(MDM),旨在表征与基质主导破坏模式相关的牵引-分离行为。这是通过采用具有代表性的体积元(RVE)框架,通过内聚区模型模拟多轴应力状态下基体内部和纤维基体界面处的损伤演变来实现的。所得的牵引-分离特性可作为CDM模型的输入,用于大型FRP层压板的层合层有限元分析。本研究中提出的基于mdm的CDM (MDM-CDM)框架在模拟(a)玻璃钢层压板的横向层裂和(b)冲击损伤方面具有与传统CDM模型相当的预测能力。虽然MDM方法引入了一组不同的材料参数(其中一些需要进一步的实验验证),但它提供了一种物理基础和计算效率高的方法,可以通知通过当前测试方法无法访问的CDM输入。因此,这项工作代表了在开发FRP复合材料中基质主导失效的多尺度建模框架方面向前迈出的一步。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Can micromechanical modelling determine the continuum damage model inputs for matrix-dominated failure in fibre-reinforced polymer composites?
Continuum damage mechanics (CDM) remains the most widely adopted and computationally viable approach for analysing intralaminar and interlaminar damage progression in fibre-reinforced polymer (FRP) laminates. However, its application necessitates extensive experimental and empirical estimation of numerous ply-level strength and toughness parameters, many of which lack standardized testing methods, thereby significantly limiting its practical applicability. To support and potentially complement these experimental efforts, this study introduces a new micromechanical damage model (MDM) designed to characterize the traction-separation behaviour associated with matrix-dominated failure modes. This is achieved through employing a representative volume element (RVE) framework to simulate the damage evolution within the matrix and at the fibre-matrix interfaces under multi-axial stress states by using a cohesive zone model. The resultant traction-separation properties serve as inputs to a CDM model for ply-level finite element (FE) analysis of large-scale FRP laminates. The MDM-informed CDM (MDM-CDM) framework presented in this study demonstrates a predictive capability comparable to conventional CDM models in simulating (a) transverse ply cracking and (b) impact damage in FRP laminates. While the MDM approach introduces a distinct set of material parameters—some of which warrant further experimental validation—it offers a physically grounded and computationally efficient means of informing CDM inputs that are otherwise inaccessible through current testing methods. Thus, this work represents a step forward in developing a multiscale modelling framework for matrix-dominated failure in FRP composites.
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来源期刊
Composites Part B: Engineering
Composites Part B: Engineering 工程技术-材料科学:复合
CiteScore
24.40
自引率
11.50%
发文量
784
审稿时长
21 days
期刊介绍: Composites Part B: Engineering is a journal that publishes impactful research of high quality on composite materials. This research is supported by fundamental mechanics and materials science and engineering approaches. The targeted research can cover a wide range of length scales, ranging from nano to micro and meso, and even to the full product and structure level. The journal specifically focuses on engineering applications that involve high performance composites. These applications can range from low volume and high cost to high volume and low cost composite development. The main goal of the journal is to provide a platform for the prompt publication of original and high quality research. The emphasis is on design, development, modeling, validation, and manufacturing of engineering details and concepts. The journal welcomes both basic research papers and proposals for review articles. Authors are encouraged to address challenges across various application areas. These areas include, but are not limited to, aerospace, automotive, and other surface transportation. The journal also covers energy-related applications, with a focus on renewable energy. Other application areas include infrastructure, off-shore and maritime projects, health care technology, and recreational products.
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