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Effect of thickness of face sheet on the bending fatigue strength of aluminum honeycomb sandwich beams

机译:面板厚度对铝蜂窝夹芯梁弯曲疲劳强度的影响

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摘要

Three types of aluminum honeycomb sandwich beam specimens with different face sheet thicknesses were employed in the four-point bending fatigue tests to study the effect of face sheet thickness on the fatigue strength. The experimental results show that under the same applied bending loads, no evident relationships exist between the face sheet thickness and the fatigue life of the studied specimens. The main failure mode of the studied specimens is the debonding at the interface between the adhesive and the face sheet based on the observations during the tests. To correlate with the scattering fatigue life data of the studied specimens with different face sheet thicknesses by using the local approaches, three parameters based on the finite element simulated interfacial stresses were proposed herein. The sub-modeling technique was applied in the finite element simulations to determine the local interfacial stresses. The employed local parameters in the study were the interfacial peeling stress, the in-plane interfacial shear stress, and the linear combination of interfacial peeling and shear stress. The comparison of the correlation performance between these employed parameters was made in the study. Furthermore, the nodes with the maximum value of prediction parameters were considered as the potential locations where the debonding failure initiated. The predicted locations of debonding initiation obtained using the three parameters were also compared with the observed ones. The analytical results show that the linearly combined peeling and shear stress parameter yields better fatigue-life correlation and failure-location prediction results than the other two parameters.
机译:在四点弯曲疲劳试验中,采用了三种不同面板厚度的铝蜂窝夹芯梁试件,研究了面板厚度对疲劳强度的影响。实验结果表明,在相同的弯曲载荷下,面板厚度与所研究试样的疲劳寿命之间没有明显的关系。根据测试过程中的观察结果,研究样品的主要破坏模式是粘合剂与面板之间界面处的剥离。为了通过局部方法与不同面板厚度的被测样品的散射疲劳寿命数据进行关联,本文提出了基于有限元模拟界面应力的三个参数。在有限元模拟中应用了子建模技术,以确定局部界面应力。研究中采用的局部参数是界面剥离应力,面内界面剪切应力以及界面剥离和剪切应力的线性组合。在研究中对这些使用的参数之间的相关性能进行了比较。此外,将具有最大预测参数值的节点视为脱胶失败开始的潜在位置。还将使用这三个参数获得的脱粘引发的预测位置与观察到的位置进行了比较。分析结果表明,线性组合的剥离应力和剪应力参数比其他两个参数产生更好的疲劳寿命相关性和失效位置预测结果。

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