Fatigue-creep damage model for carbon fibre reinforced composites under high temperature cyclic loading

被引:0
|
作者
Guo, Yi-Er [1 ,3 ]
Shang, De-Guang [1 ]
Zuo, Lin-Xuan [2 ]
Qu, Lin-Feng [2 ]
Chen, Chao-Lin [1 ]
机构
[1] Beijing Univ Technol, Fac Mat & Mfg, Beijing 100124, Peoples R China
[2] Aviat Ind Corp China Ltd, Shenyang Aircraft Design & Res Inst, Shenyang, Peoples R China
[3] Chinese Acad Sci, CAS Ctr Excellence Nanosci, Natl Ctr Nanosci & Technol, Lab Theoret & Computat Nanosci, Beijing 100190, Peoples R China
基金
中国国家自然科学基金; 中国博士后科学基金;
关键词
Composite laminates; Fatigue damage; Creep damage; Fatigue life prediction; Elevated temperature; S-N CURVES; LIFE PREDICTION; BEHAVIOR; RUPTURE; MECHANISMS; FRACTURE; FAILURE; TENSION;
D O I
10.1016/j.compscitech.2024.110909
中图分类号
TB33 [复合材料];
学科分类号
摘要
In this paper, a fatigue-creep damage model that can take into account the interaction of fatigue and creep damage is proposed under high temperature cyclic loading. In the proposed model, the effect of temperature on creep damage, the variation of creep damage under different high temperature cyclic loading conditions, and fatigue-creep interaction damage are considered. In addition, in order to accurately describe the creep behavior of unidirectional laminates with different orientations, the damage mechanism of unidirectional laminates was also analyzed. The creep and fatigue test results at different temperatures showed that the proposed creep rupture time model and the fatigue-creep damage model considering the damage mechanisms can successfully predict the creep and fatigue lives of unidirectional laminates at high temperature, and the prediction results are in good agreement with the experimental data.
引用
收藏
页数:13
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