A method for identifying the interface shear stress of unidirectional ceramic matrix composites

被引:2
|
作者
Han, Xiao [1 ,2 ]
Gao, Xiguang [1 ,2 ]
Jia, Yunfa [1 ,2 ]
Meng, Weikang [1 ,2 ]
Song, Yingdong [1 ,2 ,3 ]
Feng, Yuchun [1 ,2 ]
机构
[1] Minist Ind & Informat Technol, Key Lab Aeroengine Thermal Environm & Struct, Nanjing 210016, Peoples R China
[2] Nanjing Univ Aeronaut & Astronaut, Coll Energy & Power Engn, Jiangsu Prov Key Lab Aerosp Power Syst, Nanjing 210016, Peoples R China
[3] Nanjing Univ Aeronaut & Astronaut, State Key Lab Mech & Control Mech Struct, Nanjing 210016, Peoples R China
基金
中国国家自然科学基金;
关键词
Unidirectional ceramic matrix composite; Interface shear stress; Identification method; Shear lag model; Hysteresis loop; PULL-OUT; FATIGUE; HYSTERESIS; FAILURE; MODEL; STRENGTH; FRICTION; BEHAVIOR;
D O I
10.1016/j.ceramint.2020.08.046
中图分类号
TQ174 [陶瓷工业]; TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
A method for identifying the interface shear stress of unidirectional ceramic matrix composites (CMCs) under fatigue loading was proposed. A functional relationship between the interface shear stress and the area of the hysteresis loop, the slip strain of the hysteresis loop was established based on the shear lag model by the method of symbolic-graphic combination. A fatigue test of SiC/SiC mini-composites was performed and the hysteresis curves were obtained. Then the interface shear stress under a different number of cycles was identified by inserting the experimental data of the area and slip strain of the hysteresis curves into the functional relation-ship. The identification results using previously introduced methods based on the area or the secant modulus of the hysteresis loop were also examined. To verify these methods, the interface shear stress identified by the three different methods was entered into the shear lag model to simulate the hysteresis curves for the different number of cycles. A comparison between the simulated results and experimental data shows that the proposed method is more appropriate for the composites used in this paper.
引用
收藏
页码:64 / 72
页数:9
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