材料科学
极限抗拉强度
复合材料
复合数
结构工程
对偶(语法数字)
材料失效理论
计算机科学
断裂力学
结构破坏
疲劳试验
灾难性故障
抗撕裂性
断裂(地质)
材料性能
机械工程
机械强度
机械故障
复合材料层合板
材料强度
比强度
作者
Zhipeng Qu,Kang Li,Sen Lin,Xinyi Zhang,Lei Wu,Mu Tian,Yongliang Yuan,Fuquan Nie
出处
期刊:AIP Advances
[American Institute of Physics]
日期:2025-11-01
卷期号:15 (11)
摘要
Fiber-reinforced flexible composites are critical materials for stratospheric airship envelopes owing to their excellent mechanical properties and weather resistance. To address the challenge of coupled off-axis and crack-induced failures throughout the entire manufacturing-service cycle, this study overcomes the traditional research limitation of treating “damage-free off-axis strength prediction” and “single-angle tear strength analysis” as separate issues. Based on the Tsai–Hill failure criterion, we propose a synergistic theoretical framework that incorporates dual parameters: off-axis angle and crack length. By introducing an off-axis angle factor and integrating a single-angle failure model, a new failure model that couples multiple damage mechanisms was developed. Uniaxial tensile tests were conducted systematically under varying off-axis angles and crack lengths, and the results demonstrate that the proposed model provides high prediction accuracy and reliability.
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