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In-phase thermomechanical fatigue damage evolution of long fiber-reinforced ceramic-matrix composites using fatigue hysteresis-based damage parameters

机译:使用疲劳滞后基损伤参数的长纤维增强陶瓷 - 基质复合材料的相位热机械疲劳损伤演化

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摘要

Under in-phase (IP) thermomechanical fatigue (TMF) loading, the thermal cyclic temperature changes with decreasing or increasing applied stress upon unloading or loading, and the fiber/matrix interface shear stress in the long fiber-reinforced ceramic-matrix composites (CMCs) changes with applied cycles. In this paper, the in-phase TMF damage evolution of CMCs has been investigated, considering the coupling effects of TMF loading stress level, thermal cyclic temperature and applied cycles. The interface debonding and sliding lengths are determined based the thermomechanical micromechanical stress field and the fracture mechanics approach. The relationships between the TMF hysteresis parameters, interface damage, thermal cyclic temperature and applied cycles have been developed. The damage accumulation processes subjected to in-phase TMF for different fibers volume fraction, peak stress, matrix crack spacing, interface properties and thermal cyclic temperature range have been analyzed. The distinction of the damage evolution between the in-phase TMF and isothermal fatigue (IF) loading at the same applied stress has been analyzed. The damage evolution of cross-ply CMCs subjected to the in-phase TMF and IF loading have been predicted. (C) 2018 Elsevier Ltd. All rights reserved.
机译:在同相(IP)热机械疲劳(TMF)负载下,热循环温度随着在卸载或加载时的施加或增加施加的应力而变化,以及长纤维增强陶瓷 - 基质复合材料中的纤维/基质界面剪切应力(CMC )使用应用周期的变化。本文研究了CMCS的同相TMF损伤演化,考虑了TMF负荷应力水平,热环度温度和施用循环的偶联效应。基于热机械微机械应力场和断裂力学方法确定界面剥离和滑动长度。已经开发了TMF滞后参数,接口损伤,热循环温度和应用循环之间的关系。已经分析了对不同纤维体积分数,峰值应力,基质裂缝间距,界面性能和热循环温度范围进行的损伤累积过程。分析了在相同施加应力下的相位TMF和等温疲劳(IF)加载之间的损伤进化的区别。预测了对In-相TMF的交叉层CMC的损伤演变,并且已经预测了装载。 (c)2018年elestvier有限公司保留所有权利。

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