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A MODEL OF FATIGUE CRACK GROWTH BASED ON DAMAGE ACCUMULATION

机译:基于损伤累积的疲劳裂纹扩展模型

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摘要

A fatigue crack growth model based on cumulative damage is presented, when a material element ahead of the crack tip, is approached by the tip of the crack. The cyclic plastic zone and process zone ahead of the crack tip are taken as the area where damage accumulation takes place when the material element, first, enters into the cyclic plastic zone and then into the process zone. During this period, the Coffin-Manson damage law in conjunction with Miner's linear damage accumulation is used to determine the damage in the material element. A constant strain gradient was assumed along the process zone ahead of the crack tip and the size of process zone was taken to be variable and dependent on the range of stress intensity factor. For a cyclic loading, the effective crack driving force takes into consideration the crack tip blunting process. The model results are in good agreement with experimental data available in literature for a number of materials.
机译:当裂纹尖端附近的材料元素接近裂纹尖端时,提出了基于累积损伤的疲劳裂纹扩展模型。裂纹尖端之前的循环塑料区和加工区被视为当材料元素首先进入循环塑料区然后进入加工区时发生损伤累积的区域。在此期间,结合Coffin-Manson损伤定律和Miner的线性损伤累积来确定材料元素中的损伤。假定沿着裂纹尖端之前的加工区具有恒定的应变梯度,并且加工区的大小被认为是可变的,并且取决于应力强度因子的范围。对于循环载荷,有效的裂纹驱动力考虑了裂纹尖端钝化过程。模型结果与许多材料的文献中的实验数据非常吻合。

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