考虑有效应力和临界刚度增长的复合材料疲劳可靠性分析

IF 0.1 4区 工程技术 Q4 ENGINEERING, AEROSPACE Aerospace America Pub Date : 2023-09-06 DOI:10.3390/aerospace10090785
Jianxiong Gao, Fei Heng, Yi-Ping Yuan, Yuanyuan Liu
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引用次数: 2

摘要

疲劳损伤的累积不仅会导致材料性能的退化,而且会导致有效应力和临界刚度的增长。然而,现有的疲劳可靠性模型往往忽略了有效应力增长及其对复合材料临界刚度的影响。考虑了复合材料的性能退化和有效应力增长的综合影响,提出了复合材料的疲劳可靠性模型。首先,利用复合材料的性能退化对其疲劳损伤进行量化,并比较几种典型疲劳损伤模型的拟合精度。在此基础上,考虑了初始强度和初始刚度的不确定性,提出了一对残余强度和残余刚度的概率模型。利用Gr/PEEK[0/45/90/−45]2S层压板的性能退化数据验证了所提出的概率模型。最后,阐述了复合材料的有效应力增长机理及其对失效阈值的影响,建立了复合材料的疲劳可靠性模型。此外,还对基于强度和刚度的复合材料可靠度分析结果的差异进行了比较和讨论。
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Fatigue Reliability Analysis of Composite Material Considering the Growth of Effective Stress and Critical Stiffness
Fatigue damage accumulation will not only cause the degradation of material performance but also lead to the growth of effective stress and critical stiffness. However, the existing fatigue reliability models usually ignore the effective stress growth and its influence on the critical stiffness of a composite material. This study considers the combined effects of performance degradation and effective stress growth, and a pair of fatigue reliability models for a composite material are presented. Firstly, the fatigue damage in a composite material is quantified by its performance degradation, and the fitting accuracy of several typical fatigue damage models is compared. Subsequently, the uncertainties of initial strength and initial stiffness are considered, and a pair of probabilistic models of residual strength and residual stiffness are proposed. The performance degradation data of Gr/PEEK [0/45/90/−45]2S laminates are utilized to verify the proposed probabilistic models. Finally, the effective stress growth mechanism and its influence on the failure threshold are elaborated, and a pair of fatigue reliability models for composite materials are developed. Moreover, the differences between the strength-based and stiffness-based reliability analysis results of composite materials are compared and discussed.
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来源期刊
Aerospace America
Aerospace America 工程技术-工程:宇航
自引率
0.00%
发文量
9
审稿时长
4-8 weeks
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