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Crack Growth Behavior In Overloaded Specimens with Sharp Notch in Low Carbon Steel

机译:低碳钢尖锐缺口超载试样的裂纹扩展行为

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The purpose of the present study is to evaluate fatigue crack propagation after tensile overloading. A 6-mm long u-shaped notch was cut in the center section of the specimen. Notch root radii of 0.1, 1, and 2 mm were chosen for p. These were regarded as center-notched specimens. The crack propagation behavior of these specimens was compared with a center-cracked specimen. Push-pull fatigue tests were carried out under stress ratios R=0, - 1, and -1.5. A special investigation was made into the results for ρ=1 mm. After overload, retardation of crack growth was observed under R=0 and - 1 for the notched specimens and center-cracked specimens. However, where R= -1.5, crack growth acceleration was observed after overload in both types of specimens. Even though crack growth was accelerated or decelerated, the rate was able to be evaluated by the effective stress intensity factor range after 0.2 mm of crack growth from the notch root.
机译:本研究的目的是评估拉伸过载后的疲劳裂纹扩展。在样品的中心部分切出一个6毫米长的U形缺口。 p的切口根半径为0.1、1、2 mm。这些被认为是中心切口的标本。将这些试样的裂纹扩展行为与中心裂纹的试样进行了比较。推拉疲劳试验是在应力比R = 0,-1和-1.5下进行的。对ρ= 1 mm的结果进行了专门调查。过载后,对于缺口试样和中心裂纹试样,在R = 0和-1下观察到裂纹扩展的延迟。但是,在R = -1.5的情况下,两种类型的试样在过载后都观察到裂纹扩展加速。即使裂纹扩展加速或减速,也可以通过从缺口根部开始0.2 mm裂纹扩展后的有效应力强度因子范围来评估该速率。

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