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

Materials

Longbiao Li¹ 

[1] College of Civil Aviation, Nanjing University of Aeronautics and Astronautics No.29, Yudao St., Nanjing 210016, China; E-Mail

关键词: ceramic-matrix composites (CMCs);    C/SiC;    fatigue;    S-N curve;    hysteresis loops;    matrix multicracking;    interface debonding;   

DOI  :  10.3390/ma8063316

来源: mdpi

【 摘 要 】

The tension-tension fatigue behavior of unidirectional C/SiC ceramic-matrix composite at room temperature and 800 °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 °C under air have been predicted.

【 授权许可】

CC BY   
© 2015 by the author; licensee MDPI, Basel, Switzerland.