期刊文献+

EFFECT OF FIBER FAILURE ON QUASI-STATIC UNLOADING/RELOADING HYSTERESIS LOOPS OF CERAMIC MATRIX COMPOSITES 被引量:1

纤维失效对陶瓷基复合材料准静态加卸载迟滞回线的影响(英文)
下载PDF
导出
摘要 The two-parameter Weibull model is used to describe the fiber strength distribution.The stress carried by the intact and fracture fibers on the matrix crack plane during unloading/reloading is determined based on the global load sharing criterion.The axial stress distribution of intact fibers upon unloading and reloading is determined based on the mechanisms of fiber sliding relative to matrix in the interface debonded region.The interface debonded length,unloading interface counter slip length,and reloading interface new slip length are obtained by the fracture mechanics approach.The hysteresis loops corresponding to different stresses considering fiber failure are compared with the cases without considering fiber failure.The effects of fiber characteristic strength and fiber Weibull modulus on the fiber failure,the shape,and the area of the hysteresis loops are analyzed.The predicted quasi-static unloading/reloading hysteresis loops agree well with experimental data. 采用双参数威布尔模型描述纤维强度分布,结合总体载荷承担准则确定基体裂纹平面处断裂纤维和完好纤维承担载荷。基于卸载/重新加载时纤维相对基体滑移损伤机理,确定了纤维轴向应力分布。采用断裂力学方法确定了界面脱粘长度、卸载界面反向滑移长度和重新加载新界面滑移长度,对比了不同峰值应力下考虑和未考虑纤维失效影响的迟滞回线,分析了纤维特征强度和纤维威布尔模量对纤维失效、迟滞回线形状和面积的影响,预测的迟滞回线与试验数据相吻合。
出处 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 2011年第1期94-102,共9页 南京航空航天大学学报(英文版)
基金 Supported by the National Natural Science Foundation of China(51075204) the Graduate Innovation Foundation of Jiangsu Province(CX08B-133Z) the Doctoral Innovation Foundation of Nanjing University of Aeronautics and Astronautics(BCXJ08-05)~~
关键词 ceramic matrix composites hysteresis loops matrix cracking interface debonding fiber failure 陶瓷基复合材料 迟滞回线 基体开裂 界面脱粘 纤维失效
  • 相关文献

参考文献2

二级参考文献15

  • 1孙志刚,宋迎东,高德平.改进的二维高精度通用单胞模型[J].固体力学学报,2005,26(2):235-240. 被引量:11
  • 2俞学中,刘鹏飞,郭乙木,陶伟明.纤维拔出时Coulomb摩擦界面应力传递[J].浙江大学学报(工学版),2006,40(8):1413-1417. 被引量:4
  • 3张立同,成来飞.连续纤维增韧陶瓷基复合材料可持续发展战略探讨[J].复合材料学报,2007,24(2):1-6. 被引量:209
  • 4Mall Shankar, Engesser J M. Effects of frequency of fatigue behavior of CVI C/SiC at elevated temperature [J]. Composites Science and Technology, 2006, 66: 863-874.
  • 5Pryce A W,Smith P A. Matrix Cracking in Unidirectional Ceramic Matrix Composites under Quasi-Static and Cyclic Loading[J]. Acta Metallurgica Meterialia. ,1993,41:1269-1281.
  • 6Krith W P,Kedward K T. The stress-strain behavior of a porous unidirectional ceramic matrix composites[J]. Composites, 1995,26 : 163-174.
  • 7Gao Y, Mai Y, et al. Fracture of fiber-reinforced materials [J]. Journal Applied Mathematics and Physics (ZAMP),1988,39(7) :550-72.
  • 8Yih-Cherng Chiang. On fiber debonding and matrix cracking in fiber-reinforced ceramics [J], Composites Science and Technology,2001,61 : 1743-1756.
  • 9Kotil T, Holems J W, Comninou M. Origin of hysteresis observed during fatigue of ceramic matrix composites[J]. Journal of the American Ceramic Society, 1990,73(7) : 1879-1883.
  • 10Pryce A W, Smith P A. Matrix cracking in unidirectional ceramic matrix composites under quasi-static and cyclic loading[J]. Acta Metall Mater, 1993, 41 (4):1269-1281.

共引文献4

同被引文献18

  • 1梅辉,成来飞,张立同,徐永东,孟志新,刘持栋.2维C/SiC复合材料的拉伸损伤演变过程和微观结构特征[J].硅酸盐学报,2007,35(2):137-143. 被引量:25
  • 2R. Naslain.Design, preparation and properties of non-oxide CMCs for application in engines and nuclear reactors: an overview[J].Composites Science and Technology.2003(2)
  • 3G. Fantozzi,P. Reynaud.Mechanical hysteresis in ceramic matrix composites[J].Materials Science & Engineering A.2009
  • 4Yiqiang Wang,Litong Zhang,Laifei Cheng,Junqiang Ma,Weihua Zhang.Tensile Performance and Damage Evolution of a 2.5-D C/SiC Composite Characterized by Acoustic Emission[J].Applied Composite Materials (-).2008(4-6)
  • 5Yiqiang Wang,Litong Zhang,Laifei Cheng,Hui Mei,Junqiang Ma.Characterization of tensile behavior of a two-dimensional woven carbon/silicon carbide composite fabricated by chemical vapor infiltration[J].Materials Science & Engineering A.2008(1)
  • 6Hui Mei.Measurement and calculation of thermal residual stress in fiber reinforced ceramic matrix composites[J].Composites Science and Technology.2008(15)
  • 7Gregory N. Morscher,Mrityunjay Singh,J. Douglas Kiser,Marc Freedman,Ram Bhatt.Modeling stress-dependent matrix cracking and stress–strain behavior in 2D woven SiC fiber reinforced CVI SiC composites[J].Composites Science and Technology.2006(6)
  • 8Zhang Li Tong,Cheng Lai Fei,Luan Xin Gang,Mei Hui,Xu Yong Dong.Environmental Performance Testing System for Thermostructure Materials Applied in Aeroengines[J].Key Engineering Materials.2006(313)
  • 9Shankar Mall,John Mark Engesser.Effects of frequency on fatigue behavior of CVI C/SiC at elevated temperature[J].Composites Science and Technology.2005(7)
  • 10S. Schmidt,S. Beyer,H. Knabe,H. Immich,R. Meistring,A. Gessler.Advanced ceramic matrix composite materials for current and future propulsion technology applications[J].Acta Astronautica.2004(3)

引证文献1

二级引证文献5

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部