北京航空航天大学学报 ›› 2021, Vol. 47 ›› Issue (7): 1311-1322.doi: 10.13700/j.bh.1001-5965.2020.0229
程小全, 杜晓渊
收稿日期:
2020-06-01
发布日期:
2021-08-06
通讯作者:
程小全
E-mail:xiaoquan_cheng@buaa.edu.cn
CHENG Xiaoquan, DU Xiaoyuan
Received:
2020-06-01
Published:
2021-08-06
摘要: 随着纤维增强复合材料主承力结构在多领域内的广泛应用,疲劳成为复合材料结构设计必须面对的问题,出现了大量用于复合材料结构疲劳寿命预测及损伤演化的分析模型与方法。目前的复合材料疲劳性能分析模型可以分为疲劳寿命模型、唯象模型和渐进损伤模型。对这3类模型的发展情况进行了综述和对比分析。其中,疲劳寿命模型原理相对简单,适用于工程结构的寿命估算;唯象模型建立了材料剩余强度/刚度与循环数的数学关系,可以预测结构的寿命与材料剩余力学性能;渐进损伤模型不仅可以预测结构寿命和材料剩余力学性能,还能分析结构疲劳损伤机理。对各类疲劳性能分析模型的发展趋势进行了讨论。指出了降低实施成本和提高通用型是各类疲劳性能分析模型有待解决的问题。
中图分类号:
程小全, 杜晓渊. 纤维增强复合材料疲劳寿命预测及损伤分析模型研究进展[J]. 北京航空航天大学学报, 2021, 47(7): 1311-1322.
CHENG Xiaoquan, DU Xiaoyuan. Research development of fatigue life prediction and damage analysis model of fiber-reinforced composite[J]. Journal of Beijing University of Aeronautics and Astronautics, 2021, 47(7): 1311-1322.
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