Parameters Identification of Interface Friction Model for Ceramic Matrix Composites Based on Stress-Strain Response

被引:4
作者
Han, Xiao [1 ]
Gao, Xiguang [1 ,2 ]
Song, Yingdong [1 ,2 ,3 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Jiangsu Prov Key Lab Aerosp Power Syst, Coll Energy & Power Engn, Nanjing 210016, Peoples R China
[2] Minist Ind & Informat Technol, Key Lab Aeroengine Thermal Environm & Struct, 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
Ceramic matrix composites; Identification of interface parameters; Symbolic-graphic combination; Stress-strain curve; HYSTERESIS LOOPS; DAMAGE; MINICOMPOSITES;
D O I
10.1007/s10443-017-9651-3
中图分类号
TB33 [复合材料];
学科分类号
摘要
An approach to identify parameters of interface friction model for Ceramic Matrix composites based on stress-strain response was developed. The stress distribution of fibers in the interface slip region and intact region of the damaged composite was determined by adopting the interface friction model. The relation between maximum strain, secant moduli of hysteresis loop and interface shear stress, interface de-bonding stress was established respectively with the method of symbolic-graphic combination. By comparing the experimental strain, secant moduli of hysteresis loop with computation values, the interface shear stress and interface de-bonding stress corresponding to first cycle were identified. Substituting the identification of parameters into interface friction model, the stress-strain curves were predicted and the predicted results fit experiments well. Besides, the influence of number of data points on identifying the value of interface parameters was discussed. And the approach was compared with the method based on the area of hysteresis loop.
引用
收藏
页码:1057 / 1073
页数:17
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