SiCw—ZTA陶瓷基复合材料增韧、增强机理的分析

采用国产SiC晶须(SiCw)制备SiCw-ZTA陶瓷基复合材料,研究了SiC晶须含量对复合材料的抗弯强度及断裂韧性的影响;并分析了晶须增韧和ZrO2相变增韧两种机制协同作用的条件。     

单纤维段试验中载荷传递机理的微观力学分析

提出了一种新的、单纤维段埋入法(SFFM)试验中载荷传递机理的微观力学模型。当纤维/树脂界面所受到的剪切应力超过了界面的粘结剪切强度后,界面将发生脱粘,并且脱粘裂纹将沿着界面扩展。以Weibull模型来模拟纤维轴向拉伸强度的统计分布。讨论了纤维轴向拉伸强度以及界面粘结剪切强度对复合材料各组分内部应力分布的影响。认为在给定复合材料各相的弹性常数和几何参数后,根据不同的纤维轴向拉伸强度以及界面性能(包括界面粘结剪切强度、界面的摩擦系数和基体的径向压力),可以将单纤维段试验中纤维/树脂界面的状态清楚地分为三类:1)完全粘结界面;2)部分粘结界面;3)完全摩擦界面。给出了单纤维段试验过程中界面处于上述三种状态下时,所必须满足的一些条件。最后,还给出了极限纤维段长度的一个合理的定义,并说明该长度是由粘结纤维长度和脱粘纤维段长度所构成。     

Response surface characterization of the mechanical behavior of impact-damaged sandwich composites

In this research, Response Surface Methodology (RSM) is employed to characterize the influence of material configuration on the damage tolerance and residual strength characteristics of sandwich composites. Test specimens used were comprised of carbon-epoxy woven fabric facesheets, and Nomex honeycomb cores. The ranges of the material configuration used are typical of those employed in aircraft applications. A series of carefully selected tests were used to isolate the coupled influence of various combinations of the number of facesheet plies, core density, and core thickness on the damage formation and residual strength degradation due to normal impact. Response surface estimates suggest that impact damage development and residual strength degradation are highly material and lay-up configuration dependent. Increasing the core thickness for a specific number of facesheet plies resulted in decreasing the impact damage, whereas increasing the number of facesheet plies for a given core thickness resulted in enhancing the residual strength. The derived damage tolerance and residual strength models can lead to a better understanding of the mechanical behavior of the impact-damaged sandwich composites, and hence improve their design and expand their applications.     

EP/TGS铁电复合材料的热电驰豫研究

研究了以环氧树脂EP为基的TGS复合材料的热电驰豫效应,发现效应为同极性电荷产生,并且遵守自由驰豫规律。