Dissertation
Dissertation > Industrial Technology > General industrial technology > Materials science and engineering > Composite materials > Non-metallic composite materials

Modeling of Hysteresis Loops and Life Prediction in Cross-ply Ceramic Matrix Composites

Author XuRenHong
Tutor SongYingDong
School Nanjing University of Aeronautics and Astronautics
Course Power Machinery and Engineering
Keywords Ceramic Laminated Composites Shear-lag theory Mechanism of injury Hysteresis loop Life Prediction
CLC TB332
Type Master's thesis
Year 2008
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Ceramic Laminated composite materials with high temperature , resistance to wear , high specific strength and advantages to overcome the shortcomings of unidirectional ceramic matrix composite low intensity of the off-axis direction . Ceramic grassroots co hysteresis loop , the SN curve is to be applied to the structural components on the premise of important significance . Developed ceramic Laminated composite under quasi - static loading stress - strain curve simulation method . Under uniaxial loading ceramic Laminated composite damage mechanisms 900 layer transverse cracks , the 00 - layer matrix cracking 00 layer interface debonding and 00 - layer fiber failure . The theoretical analysis using laminated shear lag ceramic Laminated stress distribution in the composite material injury , to discuss the impact of various factors on the stress distribution . Laminated shear-lag theory and micromechanical damage model combined to determine the parameters of the various stages of injury and stress - strain curve simulation , discussion of various factors on the composite damage , and thus the impact of the stress - strain curve . The theoretical prediction of the uniaxial tensile stress - strain curve foreign and C / SiC test results show that : predictive value is consistent with the experimental results . The the laminate shear lag theory and hysteresis theory combining together the hysteresis loop of the composite ceramic grassroots analog , analysis of the impact of various factors on the hysteresis loop , the failure of the fiber the statistical model Evans interface wear model combination of ceramic matrix SN curve of the composite forecast. The theoretical prediction of the hysteresis loop , SN curve with foreign and C / SiC tension - tension fatigue tests were compared : predictive value is consistent with the experimental results .

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