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PROBABILISTIC METHOD FOR PREDICTING THE VARIABILITY IN FATIGUE BEHAVIOR OF 7075-T6 ALUMINUM

机译:预测7075-T6铝疲劳行为变异性的概率方法

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摘要

The applicability of a probabilistic model for estimating fatigue life variability for 7075-T6 aluminum is assessed. The test specimens for the experimental program were 7075-T6 aluminum single-edge notch-tension specimens tested under constant-amplitude loading(σ_max = 120 MPa,R = 0.01). A plastic replication procedure was used to identify crack nucleation sites and monitor crack growth. The initiation sites were identified by examination of the plastic replicas and the fracture surfaces of the failed specimens. In agreement with previous studies, the fatigue cracks formed in the center of the notch from material inclusions. For the prediction model, the distribution of inclusion sizes(0.2-45 mu m~2)within the material were used as the distribution of initial flaw sizes. It was assumed that the crack formation life was a small percentage of the total life, and thus life predictions were based entirely on crack propagation. The cumulative distributions for the fatigue lives from the experimental work and the numerical model were compared to assess the effectiveness of the model. Whereas experimental crack formation lives as long as 50-70 of the total life were observed in some of the tests, the model predicted failures well in the shorter life regime. The predicted lives were conservative, and in the shortest life region the predictions were within 15 of the observed lives.
机译:评估了用于估算7075-T6铝疲劳寿命变异性的概率模型的适用性。实验程序的试样是在恒定振幅载荷下(σ_max= 120 MPa,R = 0.01)进行测试的7075-T6铝单边缺口张力试样。使用塑料复制程序来识别裂纹成核位置并监测裂纹的生长。通过检查塑料复制品和失效样本的断裂表面来确定起始位置。与先前的研究一致,疲劳裂纹是由材料夹杂物在缺口中心形成的。对于预测模型,材料中夹杂物的尺寸分布(0.2-45μm〜2)被用作初始缺陷尺寸的分布。假定裂纹形成寿命仅占总寿命的一小部分,因此寿命预测完全基于裂纹扩展。比较了实验工作和数值模型的疲劳寿命累积分布,以评估该模型的有效性。在某些测试中,观察到的裂纹形成寿命可长达总寿命的50-70,而该模型在较短的寿命范围内可以很好地预测失效。预测寿命是保守的,并且在最短寿命区域中,预测值在观察到的寿命的15内。

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