Experimentally-Parameterized Multiscale Fatigue Modeling of a 3D Woven SiC/SiC Composite at High Temperatures

IF 3.9 4区 材料科学 Q3 MATERIALS SCIENCE, COMPOSITES
Fang Guangwu, Zhao Xiangyu, Zheng Mingwei, Gao Xiguang, Song Yingdong
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Abstract

This study presents an experimentally-parameterized multiscale fatigue life prediction framework for a specific three-dimensional (3D) woven silicon carbide fiber-reinforced silicon carbide (SiC/SiC) ceramic matrix composite operating in high-temperature oxygen-free environments. The principal novelty of this work lies in the systematic application of such a framework to this particular material system, wherein most of critical geometric and material parameters at both the fiber yarn (microscale) and woven architecture (mesoscale) levels were quantitatively determined through direct experimental measurement. Key parameters were characterized using high-resolution X-ray computed tomography (X-ray CT) for precise geometric reconstruction of the crimped warp, weft, and stitching yarns. At the yarn level, a periodic micromechanical unit cell incorporating anisotropic continuum damage mechanics and Miner’s cumulative fatigue criterion was formulated to capture progressive stiffness degradation, matrix microcracking, and interfacial debonding under cyclic thermomechanical loading. The evolving yarn-level constitutive properties were then mapped as spatially-dependent inputs into a 3D representative volume element (RVE) that explicitly resolves the experimentally-characterized woven preform architecture. This coupled approach enables direct simulation of damage initiation, trans-yarn propagation, and ultimate fatigue failure. The framework was validated against tension-tension fatigue tests conducted at 1100 °C in a vacuum-nitrogen environment, demonstrating excellent predictive accuracy for fatigue life and damage progression mechanisms.

高温下三维编织SiC/SiC复合材料的实验参数化多尺度疲劳建模
本研究提出了一个实验参数化的三维(3D)编织碳化硅纤维增强碳化硅(SiC/SiC)陶瓷基复合材料在高温无氧环境下的多尺度疲劳寿命预测框架。这项工作的主要新颖之处在于系统地将这种框架应用于这种特殊的材料系统,其中纤维纱线(微尺度)和编织结构(中尺度)水平上的大多数关键几何和材料参数都是通过直接实验测量定量确定的。利用高分辨率x射线计算机断层扫描(x射线CT)对关键参数进行表征,对卷曲的经纱、纬纱和缝合纱进行精确的几何重建。在纱线层面,建立了一个包含各向异性连续损伤力学和Miner累积疲劳准则的周期性微力学单元,以捕捉循环热机械载荷下的渐进式刚度退化、基体微开裂和界面脱粘。然后将纱线级本构性能作为空间相关输入映射到3D代表性体积元素(RVE)中,该元素明确地解析了实验表征的编织预制体结构。这种耦合方法可以直接模拟损伤起始、跨纱传播和最终疲劳失效。该框架在1100°C真空氮环境下进行了拉伸-拉伸疲劳试验,证明了对疲劳寿命和损伤进展机制的出色预测准确性。
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来源期刊
Applied Composite Materials
Applied Composite Materials 工程技术-材料科学:复合
CiteScore
4.20
自引率
4.30%
发文量
81
审稿时长
1.6 months
期刊介绍: Applied Composite Materials is an international journal dedicated to the publication of original full-length papers, review articles and short communications of the highest quality that advance the development and application of engineering composite materials. Its articles identify problems that limit the performance and reliability of the composite material and composite part; and propose solutions that lead to innovation in design and the successful exploitation and commercialization of composite materials across the widest spectrum of engineering uses. The main focus is on the quantitative descriptions of material systems and processing routes. Coverage includes management of time-dependent changes in microscopic and macroscopic structure and its exploitation from the material''s conception through to its eventual obsolescence.
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