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Fatigue Crack Propagation of Al Alloy 2017-T4 under Mixed Mode of Modes I and III and Modes I, II and III

机译:I和III以及I,II和III混合模式下铝合金2017-T4的疲劳裂纹扩展

摘要

Fatigue crack propagation behavior under the mixed-mode condition which combined modes I and III and modes I, II and III was investigated in a push-pull fatigue test of notched specimen. The notch inclined in the thickness direction was cut at the center of the specimen. Four values were selected for the notch length 2b, that is, 2b=9,15, 25, 35 mm. In the present study, the crack propagation behavior under the mixed modes is assumed to be dominated by the maximum principal stress criterion. The stress intensity factor K_p of mode I was calculated with the projected crack length along the load direction and the crack propagation rate da/dN under the mixed modes was evaluated using it. This stress intensity factor K_p can approximate relatively well the stress intensity factor determined on the basis of the maximum principal stress criterion in the case of the specimen used in the present experiment. The crack propagation rate da/dN can reasonably be evaluated with the effective stress intensity factor range of K_p independent of the applied mean stress.
机译:在缺口试样的推拉疲劳试验中研究了混合模式条件下疲劳裂纹扩展行为,该模式组合了模式I和III以及模式I,II和III。沿厚度方向倾斜的切口在试样的中央切开。切口长度2b选择了四个值,即2b = 9,15,25,35 mm。在本研究中,假定混合模式下的裂纹扩展行为受最大主应力准则支配。利用沿载荷方向的预测裂纹长度计算出模式I的应力强度因子K_p,并使用其评估混合模式下的裂纹扩展速率da / dN。在本实验中使用的样品的情况下,该应力强度因子K_p可以相对较好地近似基于最大主应力标准确定的应力强度因子。裂纹扩展速率da / dN可以通过有效应力强度因子范围K_p独立于所施加的平均应力来合理评估。

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