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首页> 外文期刊>International Journal of Polymer Analysis and Characterization >Digital image processing and thermo-mechanical response of neat epoxy and different laminate orientations of fiber reinforced polymer composites for vibration isolation applications
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Digital image processing and thermo-mechanical response of neat epoxy and different laminate orientations of fiber reinforced polymer composites for vibration isolation applications

机译:用于隔振应用的纤维增强聚合物复合材料的纯环氧和不同层压方向的数字图像处理和热机械响应

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摘要

In this study, tensile tests are performed under quasi-static loading on neat epoxy and for different laminate configurations [(0/90), (0/90/30/-60), (0/90/45/-45) and (30/-60/60/-30)] of glass/epoxy, carbon/epoxy and cross ply interply hybrid (glass/carbon/epoxy) composites. A camera-based advanced image processing technique called as digital image correlation is employed to obtain the full-field strain fields and identify the direction of failure of the matrix and composites as a function of fiber orientation angle. Further, the viscoelastic properties (storage modulus, loss modulus and loss factor) are measured over the temperature range from 20 degrees C-140 degrees C for five different frequencies (1, 10, 20, 33 and 50 Hz) using the dynamic mechanical analyzer. The glass transition temperature (T-g) is found out from temperatures corresponding to the loss modulus and loss factor peak values. The results revealed that as the temperature increases, the storage and loss moduli decrease attributed to the softening of the material because of free molecular movements. The cross ply laminates of GFRP and CFRP exhibit higher storage and loss moduli at all frequencies due to strong fiber network as compared to the other laminate configurations. The hybrid composites possess higher storage and loss moduli than GFRP and neat epoxy. The neat epoxy has higher loss factor values than composites. As the frequency increases, the T-g shifts to higher values. Loss modulus T-g values are found to be lower than that of loss factor T-g values.
机译:在该研究中,拉伸试验在整个环氧树脂上的准静态负载下进行,并且对于不同的层压化构型[(0/90),(0/90/30 / -60),(0/90/45 / -45)和(30 / -60 / 60 / -30)]玻璃/环氧树脂,碳/环氧树脂和交叉层面杂交(玻璃/碳/环氧树脂)复合材料。采用作为数字图像相关的基于相机的高级图像处理技术来获得全场应变场,并作为光纤取向角的函数识别矩阵和复合材料的故障方向。此外,使用动态机械分析仪在20摄氏度范围内测量五种不同频率(1,10,20,33和50Hz)的温度范围内测量粘弹性(储存模量,损耗模量和损耗因子) 。从对应于损耗模量和损耗因子峰值的温度中发现玻璃化转变温度(T-G)。结果表明,随着温度的增加,由于自由分子运动,储存和损失模量减少了材料的软化。与其他层压化配置相比,GFRP和CFRP的十字合层和CFRP的储存和损耗模量具有强大的纤维网络。杂交复合材料具有比GFRP和整齐的环氧树脂更高的储存和损失模育。整齐的环氧树脂具有比复合材料更高的损耗因子值。随着频率的增加,T-G转换为更高的值。发现损耗模量T-G值低于损耗因子T-G值的值。

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