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Micro-macro Analysis of the Notch Tip Radius and Loading Rate Dependences of the Dynamic Crack Initiation Toughness during a High Transient Dynamic crack Growth Experiment

机译:高瞬态动态裂纹增长实验期间动态裂纹启动韧性凹口尖端半径的微观宏观分析

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The risks due to crack propagation under dynamic loading are still difficult to estimate. Unlike quasi-static cases, where the loading and crack position can be easily established, in dynamic impact cases, loading conditions, propagation parameter variations and exact crack positions are difficult to control. The determination of relevant constitutive crack propagation laws from dynamic crack propagation experiments is thus a challenging operation. Consequently, the first step for assessing dynamic crack propagation laws is the development of numerical simulation tools. Some numerical tools are now able to represent dynamic crack growth but these numerical results have to be compared with experimental results to ensure that the numerical laws introduced are physically consistent. In a previous work [1], crack tip position histories have been determined by standard optical tools. The test rig was a split Hopkinson pressure bar (SHPB) and the specimen geometry was chosen in order to provide direct conversion between impacting compressive waves and tensile waves in the vicinity of a machined notch. Since the material used (PMMA) was transparent, the crack tip position history was obtained by using standard optical tools (four cameras providing one picture per camera) and by carrying out the same tests, repetitively and reproducibly. Three different phases were observed: two propagation phases were separated by a crack arrest phase. Using an eXtended Finite Element Method (X-FEM), numerical simulations were performed and both the crack path and the crack position histories fitted the experimental results. Failure in glassy polymers has been extensively investigated for PMMA, which is well documented [2, 3, 4]. The toughness under mode I loading increases with loading rate and its value is also notch sensitive. Therefore, the criterion adopted in the foregoing X-FEM analysis with a set of parameters for the onset of crack advance, its dynamic propagation, arrest and conditions for re-propagation appears to approximate the rate-dependent process underlying failure. However this kind of comparison allowed the validation of a dynamic crack growth criterion but only in a unique case of loading. The previous process leads to a large experiments number for obtaining different crack tip position histories corresponding to different loading rate and the loading rate influence on the transient propagation phases as arrest and restart cannot be represented accurately if several experiments are needed to obtain a crack tip position history.
机译:由于动态载荷下裂纹传播导致的风险仍然难以估计。与准静态案例不同,在可以轻易建立装载和裂缝位置,在动态冲击案例中,难以控制装载条件,传播参数变化和精确的裂缝位置。因此,确定来自动态裂纹传播实验的相关组成裂纹传播法是一个具有挑战性的操作。因此,评估动态裂纹传播法的第一步是开发数值模拟工具。现在,一些数值工具现在能够表示动态裂纹增长,但必须与实验结果进行比较这些数值结果,以确保引入的数值法在物理上是一致的。在先前的工作[1]中,裂缝尖端位置历史已经通过标准光学工具确定。试验机是分开的霍普金森压力棒(SHPB),选择样品几何形状,以便在机加工凹口附近的冲击压缩波和拉伸波之间提供直接转换。由于所用材料(PMMA)是透明的,因此通过使用标准光学工具(每台相机提供一张图片的四个摄像机)获得裂缝尖端位置历史,并且通过执行相同的测试,重复和可重复地进行。观察到三个不同的阶段:通过裂缝止血阶段分离出两种繁殖相。使用扩展有限元方法(X-FEM),进行数值模拟,裂纹路径和裂缝位置历史都拟合实验结果。对于PMMA进行了广泛研究了玻璃状聚合物的失效,该PMMA有很好的记录[2,3,4]。模式I加载下的韧性随装载速率而增加,其值也是截止值敏感的。因此,在前述X-FEM分析中采用的标准用一组参数进行裂缝前进的开始,其动态传播,逮捕和重新传播的条件似乎近似于速率失败的过程。然而,这种比较允许验证动态裂缝生长标准,而只是在独特的装载情况下。先前的过程导致用于获得不同负载率对应的不同裂纹尖端位置历史的大实验号,并且如果需要几个实验以获得裂缝尖端位置,则不能准确地表示对瞬态传播阶段的加载速率影响历史。

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