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Stress Ratio Effects on the fatigue Properties of Biaxially Loaded Tubular FRP-Specimens – Experimental Study

机译:应力比对双轴管状FRP试样疲劳性能的影响-实验研究

摘要

In this work tubular fiber reinforced specimens are tested for fatigue life. The specimens are biaxially loaded with tension and shear stresses, with a load angle β of 30° and 60° and a load ratio of R=0,1. There are many factors that affect fatigue life of a fiber reinforced material and the main goal of this work is to study the effects of load ratio R by obtaining S-N curves and compare them to the previous works (1). All the other parameters, such as specimen production, fatigue loading frequency and temperature, will be the same as for the previous tests. For every specimen, stiffness, temperature of the specimen during testing, crack counting and final fracture mode are obtained.Prior to testing, a study if the literature regarding the load ratio effects on composites fatigue life and with that review estimate the initial stresses to be applied in testing. In previous works (1) similar specimens have only been tested for a load ratio of R=-1 and therefore the behaviour of this tubular specimens for a different load ratio is unknown. All the data acquired will be analysed and compared to the previous works, emphasizing the differences found and discussing the possible explanations for those differences.The crack counting software, developed at the institute, has shown useful before, however different adjustments to the software parameters lead to different cracks numbers for the same picture, and therefore a better methodology will be discussed to improve the crack counting results.After the specimen’s failure, all the data will be collected and stored and fibre volume content for every specimen is also determinate. The number of tests required to make the S-N curves are obtained according to the existent standards.Additionally are also identified some improvements to the testing machine setup and to the procedures for future testing.
机译:在这项工作中,对管状纤维增强的样品进行了疲劳寿命测试。试样被双轴加载拉伸和剪切应力,加载角β为30°和60°,加载比为R = 0,1。影响纤维增强材料疲劳寿命的因素很多,这项工作的主要目的是通过获得S-N曲线来研究载荷比R的影响并将其与以前的工作进行比较(1)。所有其他参数,例如样品生产,疲劳加载频率和温度,将与之前的测试相同。对于每个试样,都获得了试样在试验过程中的刚度,温度,裂纹​​计数和最终断裂模式。在试验之前,应进行一项研究,以研究有关载荷比对复合材料疲劳寿命的影响,并进行综述以评估初始应力为在测试中应用。在以前的工作中(1),仅对相似的样本进行了R = -1的载荷比测试,因此,对于不同载荷比的管状样品,其行为尚不清楚。所获得的所有数据都将进行分析,并与以前的工作进行比较,强调发现的差异并讨论这些差异的可能解释。该研究所开发的裂缝计数软件之前已证明是有用的,但是对软件参数的不同调整导致在同一张图片上使用不同的裂纹数量,因此将讨论一种更好的方法来改善裂纹计数结果。在试样失效后,将收集并存储所有数据,并确定每个试样的纤维体积含量。根据现有标准获得绘制S-N曲线所需的测试次数。此外,还确定了测试机设置和未来测试程序的一些改进。

著录项

  • 作者单位
  • 年度 2013
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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 入库时间 2022-08-20 20:56:06

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