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An Experimental Study of Fatigue Crack Propagation of 16MnR Pressure Vessel Steel in Mode-I Constant Amplitude Loading

机译:第1型恒定幅度负荷16MNR压力容器钢疲劳裂纹谱的实验研究

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An experimental investigation was performed on fatigue crack growth behavior of a 16MnR pressure vessel steel. Standard compact tension (CT) specimens with three specimen thicknesses and notch sizes were subjected to Mode I constant amplitude loading with several stress ratios and loading amplitudes. The results revealed that the stress ratio had an insignificant influence on the fatigue crack growth of the material. The stable fatigue crack growth rate (FCGR) was accelerated as specimen thickness increased. The fatigue crack was extended in terms of the curve crack shape. The crack front at the surface was retarded compared to that at the interior along thickness direction, and the crack front at the mid-thickness plane reached the maximum value of the crack length. The similar curve crack shape was obtained in the stable crack growth stage. The maximum difference of the crack front along thickness direction was increased with the increasing of the specimen thickness. The early crack growth from the notch was effected by the size of the notch, the stress ratio and loading amplitude.
机译:对16Mnr压力容器钢的疲劳裂纹生长行为进行了实验研究。具有三个样品厚度和凹口尺寸的标准紧凑张力(CT)样本进行了恒定幅度载荷,具有几种应力比和装载幅度。结果表明,应力比对材料的疲劳裂纹生长有微不足道的影响。随着样品厚度的增加,稳定的疲劳裂纹生长速率(FCGR)加速。就曲线裂缝形状而延长了疲劳裂缝。与沿厚度方向的内部的内部的表面相比,表面的裂缝前部延迟,并且在中厚平面处的裂纹前沿达到裂缝长度的最大值。在稳定的裂纹生长阶段获得了类似的曲线裂纹形状。随着样品厚度的增加,沿厚度方向沿厚度方向的最大差异增加。从凹口,应力比和装载幅度的尺寸实现了来自凹口的早期裂纹生长。

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