Affiliation of Author(s):民航学院

Journal:ENGINEERING FRACTURE MECHANICS

Key Words:Ceramic-matrix composites (CMCs) Hysteresis loops Matrix cracking Interface debonding

Abstract:The effects of loading type, i.e., cyclic loading/unloading tensile, cumulative tensile fatigue loading, and tension-tension fatigue loading, temperature and oxidation on the mechanical hysteresis behavior of carbon fiber-reinforced ceramic-matrix composites (CMCs) have been investigated. Based on the damage mechanism of fiber sliding relative to the matrix in the interface debonded region, the stress-strain relationships upon unloading/reloading when the interface partially and completely debonded have been determined considering fibers fracture. The effects of material properties, damage mode and cycle number on the interface slip and hysteresis loops have been analyzed. The mechanical hysteresis behavior of different loading types of C/SiC at room temperature and 800 degrees C in air have been predicted. (C) 2016 Elsevier Ltd. All rights reserved.

ISSN No.:0013-7944

Translation or Not:no

Date of Publication:2017-01-01

Correspondence Author:llb