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An experimental investigation on fatigue crack growth of AL6XN stainless steel

机译:AL6XN不锈钢疲劳裂纹扩展的实验研究

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The crack growth behavior of AL6XN stainless steel was experimentally investigated using round compact tension (CT) specimens. The influences of the R-ratio (the ratio of the minimum load over the maximum applied load in a cycle), the tensile and compressive overloads, and the loading sequence on crack growth were studied in detail. The results from the constant-amplitude experiments show a sensitivity of the crack growth rate to the R-ratio. The application of a tensile overload has a profound effect on crack growth, resulting in a significant retardation in the crack propagation rate. A com-pressive overload (underload) leads to a short-lived acceleration in crack growth. Results from the two-step high-low loading reveal a period of crack growth retardation at the beginning of the lower amplitude step, an effect similar to that of a single overload. A crack driving force parameter together with a modified Wheeler model is found to correlate the crack growth experiments well.
机译:使用圆形致密拉伸(CT)标本对AL6XN不锈钢的裂纹扩展行为进行了实验研究。详细研究了R比(循环中最小载荷与最大施加载荷之比),拉伸和压缩过载以及载荷顺序对裂纹扩展的影响。恒定振幅实验的结果表明,裂纹扩展速率对R比具有敏感性。施加拉伸过载对裂纹扩展具有深远的影响,从而导致裂纹扩展速率的显着降低。压缩性过载(欠载)会导致裂纹扩展的短暂加速。两步高-低载荷的结果表明,在较低幅度步长的开始,裂纹扩展被延迟了一段时间,其效果类似于单次过载。发现裂纹驱动力参数和改进的Wheeler模型可以很好地关联裂纹扩展实验。

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