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Effect of Air on the Mode II Fatigue Crack Growth Mechanism and Threshold

机译:空气对模式II疲劳裂纹增长机制和阈值的影响

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In order to make clear the effect of air on the Mode n fatigue crack growth mechanism and threshold, the Mode II fatigue crack growth test was carried out in a vacuum. The Mode n fatigue fracture surface of the specimen tested in a vacuum was clearer than that tested in air. The Mode II fatigue crack of the specimen tested in a vacuum was more indistinct than that tested in air. This is because that the influence of oxidation in a vacuum was smaller than that in air. The layer with the microstructural change was observed in the vicinity of the Mode II fatigue crack. The Vickers hardness of the layer of the specimen tested in a vacuum was 770. The value was much higher than that of the original matrix (HV=190). The layer consisted of very line grains (approx 130nm). The Mode II threshold stress intensity factor range. DELTA K_(11th), in a vacuum was tentatively estimated to be larger than that in air based on the assumption of the same frictional coefficient.
机译:为了清除空气对模式N疲劳裂纹生长机制和阈值的影响,在真空中进行模式II疲劳裂纹生长试验。在真空中测试的样本的模式N疲劳断裂表面比空气中测试的样品更清晰。在真空中测试的样本的模式II疲劳裂纹比空气中的测试更模糊。这是因为氧化在真空中的影响小于空气中的影响。在模式II疲劳裂缝附近观察到具有微观结构变化的层。在真空中测试的样本层的维氏硬度为770.该值远高于原始基质(HV = 190)的值。该层由非常线颗粒(约130nm)组成。模式II阈值应力强度因子范围。 ΔK_(11th),在真空中暂时估计基于相同摩擦系数的假设大于空气中的。

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