Tension-Tension Fatigue Behavior of Unidirectional C/Sic Ceramic-Matrix Composite at Room Temperature and 800 °C in Air Atmosphere

被引:19
作者
Li, Longbiao [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Civil Aviat, Nanjing 210016, Peoples R China
关键词
ceramic-matrix composites (CMCs); C/SiC; fatigue; S-N curve; hysteresis loops; matrix multicracking; interface debonding; MACHINING PROCESSES; INTERFACIAL SHEAR; FREQUENCY;
D O I
10.3390/ma8063316
中图分类号
O64 [物理化学(理论化学)、化学物理学];
学科分类号
070304 ; 081704 ;
摘要
The tension-tension fatigue behavior of unidirectional C/SiC ceramic-matrix composite at room temperature and 800 degrees C under air has been investigated. The fatigue hysteresis modulus and fatigue hysteresis loss energy corresponding to different number of applied cycles have been analyzed. The fatigue hysteresis loops models for different interface slip cases have been derived based on the fatigue damage mechanism of fiber slipping relative to matrix in the interface debonded region upon unloading and subsequent reloading. The fiber/matrix interface shear stress has been estimated for different numbers of applied cycles. By combining the interface shear stress degradation model and fibers strength degradation model with fibers failure model, the tension-tension fatigue life S-N curves of unidirectional C/SiC composite at room temperature and 800 degrees C under air have been predicted.
引用
收藏
页码:3316 / 3333
页数:18
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