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Some remarks on the engineering application of the fatigue crack growth approach under nonzero mean loads

机译:非零平均载荷下疲劳裂纹扩展方法在工程上的一些应用

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The well-known fatigue crack growth (FCG) curves are two-parameter dependents. The range of the stress intensity factor ΔX and the load ratio R are the parameters normally used for describing these curves. For engineering purposes, the mathematical representation of these curves should be integrated between the initial and final crack sizes in order to obtain the safety factors for stresses and life. First of all, it is necessary to reduce the dependence of the FCG curves to only one parameter. ΔK is almost always selected and, in these conditions, considered as the crack driving force. Using experimental data from literature, the present paper shows how to perform multiple regression analyses using the traditional Walker approach and the more recent unified approach. The correlations so obtained are graphically analyzed in three dimensions. Numerical examples of crack growth analysis for cracks growing under nominal stresses of constant amplitude in smooth and notched geometries are performed, assuming an identical material component as that of the available experimental data. The resulting curves of crack size versus number of cycles (a vs. N) are then compared. The two models give approximately the same (a vs. N) curves in both geometries. Differences between the behaviors of the (a vs. N) curves in smooth and notched geometries are highlighted, and the reasons for these particular behaviors are discussed.
机译:众所周知的疲劳裂纹扩展(FCG)曲线取决于两个参数。应力强度因子ΔX的范围和负载率R是通常用于描述这些曲线的参数。出于工程目的,应将这些曲线的数学表示形式合并到初始和最终裂纹尺寸之间,以获得应力和寿命的安全系数。首先,有必要将FCG曲线的依赖性降低到仅一个参数。几乎总是选择ΔK,并且在这些条件下,将其视为裂纹驱动力。本文利用文献中的实验数据,展示了如何使用传统的Walker方法和最新的统一方法执行多元回归分析。这样获得的相关性在三个维度上以图形方式进行了分析。假设在与恒定的实验数据相同的材料成分的情况下,进行了在恒定振幅的名义应力下以平滑和缺口几何形状生长的裂纹的裂纹扩展分析的数值示例。然后比较所得的裂纹尺寸与循环次数(a与N)的曲线。两种模型在两种几何结构中给出的曲线大致相同(a对N)。突出显示了在平滑几何形状和缺口几何形状中(a与N)曲线的行为之间的差异,并讨论了这些特殊行为的原因。

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