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Notch fatigue life prediction considering nonproportionality of local loading path under multiaxial cyclic loading

机译:考虑局部载荷路径不成比例的缺口疲劳寿命预测

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摘要

An innovative numerical methodology is presented for fatigue lifetime estimation of notched bodies experiencing multiaxial cyclic loadings. In the presented methodology, an evaluation approach of the local nonproportionality factor F for notched specimens, which defines F as the ratio of the pseudoshear strain range at 45 degrees to the maximum shear plane and the maximum shear strain range, is proposed and discussed deeply. The proposed evaluation method is incorporated into the material cyclic stress-strain equation for purpose of describing the nonproportional hardening behavior for some material. The comparison between multiaxial elastic-plastic finite element analysis (FEA) and experimentally measured strains for S460N steel notched specimens shows that the proposed nonproportionality factor estimation method is effective. Subsequently, the notch stresses and strains calculated utilizing multiaxial elastic-plastic FEA are used as input data to the critical plane-based fatigue life prediction methodology. The prediction results are satisfactory for the 7050-T7451 aluminum alloy and GH4169 superalloy notched specimens under multiaxial cyclic loading.
机译:提出了一种创新的数值方法,用于评估承受多轴循环载荷的缺口体的疲劳寿命。在提出的方法中,提出并深入讨论了一种用于缺口试样的局部非比例因子F的评估方法,该方法将F定义为45度拟剪切应变范围与最大剪切平面和最大剪切应变范围之比。所提出的评估方法被纳入材料循环应力-应变方程,目的是描述某些材料的非比例硬化行为。通过对S460N钢带缺口试样的多轴弹塑性有限元分析(FEA)和实验测得的应变进行比较,表明所提出的非比例因子估计方法是有效的。随后,利用多轴弹塑性有限元分析法计算的缺口应力和应变被用作基于临界平面的疲劳寿命预测方法的输入数据。对于7050-T7451铝合金和GH4169合金缺口试样在多轴循环载荷下的预测结果是令人满意的。

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