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Extended slip band mixed-mode fatigue crack growth in an AA8090 Al-Li alloy

机译:AA8090 Al-Li合金中的延长滑槽混合模式疲劳裂纹生长

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The complexities of crack growth processes have been examined for various combinations of mode I and mode II loading of long cracks in the Al-Li alloy AA8090, for which shear crack growth processes can be dominant. An equivalent co-planar strain energy release rate formulation of crack driving force for mixed mode loading has been utilised, which, for a given R-ratio, provides a consistent interpretation of crack growth with respect to pure mode II loading; and also for the different R-ratios of 0.1 and 0.5, with the latter showing a factor of 10 increase in growth rates. The paper concludes by discussing shielding mechanisms, with contact shielding having only a limited influence when compared to previously reported mixed mode fatigue work. This is consistent with the unusually flat crack paths produced under mixed mode loading conditions in such strongly textured materials. The applicability of established sliding contact modelling approaches is discussed with respect to the present data.
机译:已经检查了抗裂纹的各种组合的裂纹生长过程的复杂性,在Al-Li合金AA8090中的长裂纹的各种组合,剪切裂纹生长过程可以是显性的。已经利用了用于混合模式载荷的裂纹驱动力的等效共平面应变能量释放速率制剂,其对于给定的R比率,这提供了相对于纯模式II负载的裂纹生长的一致解释;而且对于0.1和0.5的不同R比,后者显示出增长率10增加10。本文通过讨论屏蔽机构结束,与先前报道的混合模式疲劳工作相比,接触屏蔽仅具有有限的影响。这与在这种强烈纹理材料的混合模式负载条件下产生的异常平坦的裂纹路径一致。关于本数据讨论了建立的滑动触点建模方法的适用性。

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