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Experimental study on evolution process of short fatigue crack in 2A12 alloy under complex stress state

机译:复合应力状态下2A12合金短疲劳裂纹演化过程的实验研究

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The fatigue behavior of 2A12 Aluminum alloy was experimentally studied through different annular notched specimens under symmetrical triangle with the frequency of 0.5 Hz. The experimental result showed that the microstructure played an important role during the entire fatigue life of 2A12 Aluminum alloy. The short fatigue crack only initiated due largely to the second-phase particle such as the S phase (Al_2CuMg), the 9 phase (CuAl_2) and especially the black impurity phases debonding from the basal body when the fatigue cycle was sufficient. The cracks propagated separately along the circumferential direction of the notch, crack coalescence and interaction of cracks were not common at early and middle stage of short crack's fatigue life. Cracks tended to propagate along direction different from the original one after crack coalescence. Surface crack length at early and middle stage of short crack's fatigue life were presented. These curves showed crack growth rate increased relatively as the reducing of notched radius or the increasing of nominal strain amplitude which implied that geometry and loading conditions were the factors of the crack propagation.
机译:通过不同的环形缺口试样在对称三角形下通过不同的环形缺口试样进行实验研究了2A12铝合金的疲劳行为,频率为0.5Hz。实验结果表明,在2A12铝合金的整个疲劳寿命期间,微观结构起到了重要作用。仅当疲劳循环充足时,仅由于诸如S期(Al_2cumg),9相(Cual_2),特别是黑色杂质相位剥离的黑色杂质相位,而仅引起的短疲劳裂缝。沿着凹口的圆周方向分开传播的裂缝,裂缝结合和裂缝的相互作用在短裂缝疲劳寿命的早期和中间阶段并不常见。裂缝沿着在裂缝结束后沿着与原始的方向传播。提出了短裂缝疲劳寿命的早期和中期地表裂缝长度。这些曲线显示出裂纹的生长速率相比,由于缺口半径或增加了暗示几何形状和装载条件是裂纹传播的因素的增加而增加。

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