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Modelling crack-tip behaviour in a directionally solidified nickel alloy under fatigue-oxidation conditions

机译:模拟定向氧化镍合金在疲劳氧化条件下的裂纹尖端行为

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A finite-element approach, to study crack-tip behaviour for a directionally solidified nickel-based superalloy subjected to high-temperature fatigue loading in vacuum and air, is presented. In vacuum, crack-tip behaviour was entirely controlled by mechanical deformation, hence, a criterion based on accumulated plastic strain was sufficient to describe damage. In air, effects of oxidation on crack-tip deformation were studied using a diffusion-based approach; further developed to investigate a synergetic interaction between fatigue loading and oxygen penetration. Stress-assisted diffusion and dilatation from oxygen penetration into a crack tip, were considered. A local compressive stress induced by oxygen penetration compensated part of the tensile stresses from mechanical loading. To predict crack growth rate under fatigue-oxidation conditions, a two-parameter crack-growth criterion, based on accumulated plastic strain and oxygen concentration at the crack tip, was developed. Obtained numerical results compared well with experimental data in the literature.
机译:提出了一种有限元方法,以研究定向凝固的镍基高温合金在真空和空气中承受高温疲劳载荷时的裂纹尖端行为。在真空中,裂纹尖端的行为完全由机械变形控制,因此,基于累积塑性应变的准则足以描述损伤。在空气中,使用基于扩散的方法研究了氧化对裂纹尖端变形的影响。进一步研究疲劳负荷和氧气渗透之间的协同作用。考虑了应力辅助的扩散和从氧气渗透到裂纹尖端的扩散。由氧气渗透引起的局部压应力补偿了部分机械负荷引起的拉应力。为了预测疲劳氧化条件下的裂纹扩展速率,基于累积的塑性应变和裂纹尖端处的氧气浓度,建立了一个两参数的裂纹增长准则。获得的数值结果与文献中的实验数据进行了比较。

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