基于多轴损坏模型的纹板的多层压缩故障分析
Jian Shi1, Guang Yang2,3, Nan Sun4
1College of Aviation Engineering, Civil Aviation Flight University of China, Chengdu 641419, China.
Materials (Basel, Switzerland)
|October 16, 2025
概括
碳纤维增强复合材料 (CFRC) 的纹降低了承载能力,并导致曲. 这项研究使用了实验和一种新的多尺度模型来分析纹对CFRC故障模式和性能的影响.
科学领域:
- 材料科学 材料科学 材料科学
- 机械工程 机械工程
- 复合材料 复合材料 复合材料
背景情况:
- 波纹缺陷 (纹) 在复合材料制造中很常见.
- 这些缺陷可以显著降低复合结构的机械性能.
研究的目的:
- 研究纹对碳纤维增强复合材料 (CFRC) 层材的最终负载和故障模式的影响.
- 分析不同波浪度比对压缩下层层材的行为的影响.
主要方法:
- 实验性压缩测试是在CFRC层材上进行的,其堆叠顺序和波浪率不同.
- 为了模拟,开发了一种使用用户材料 (UMAT) 子程序的新型多尺度渐进性损伤模型.
- 该模型整合了细胞的通用化方法与宏观微观损伤分析的哈辛失败标准.
主要成果:
- 多尺度模型准确地预测了负载位移曲线和故障模式,与实验数据有很好的一致性.
- 发现纹缺陷降低了CFRC层材的最终承载能力.
- 纹促进了局部曲,改变了损坏分布和故障机制.
结论:
- 纹严重损害了CFRC层材的结构完整性和性能.
- 开发的多尺度模型对于预测纹复合结构的行为是有效的.
- 了解纹效应对于设计可靠的复合材料组件至关重要.
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