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Effect of compressive load and crack closure on fatigue crack growth of commercial pure titanium at negative load ratios

机译:压缩载荷和裂纹闭合对负载荷比疲劳纯钛疲劳裂纹生长的影响

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摘要

In this paper, the effect of compressive load and crack closure on mode-I fatigue crack growth (FCG) behavior at negative load ratios is studied with compact-tensile-shear (CTS) specimens made from commercial pure titanium (CP-Ti). The FCG behavior at negative load ratios under constant maximum load controlled has been explained by the interaction of compressive load effect and crack closure. The variation of crack closure level at negative load ratios within stable crack growth stage is obtained by the experiment. The crack closure level keeps constant which makes the crack closure effect dominate the FCG behavior in pre-stage. While in post-stage, the crack closure level drops gradually. The crack closure effect can be neglected currently and the compressive load effect plays a dominate role in post-stage. Meanwhile, the influence of crack closure effect on mechanical behavior at crack tip is described by finite element method (FEM) to explain the anomaly in pre-stage. It is confirmed that there exists a maximum reversed plastic zone induced by the crack closure effect during unloading process in pre-stage at negative load ratios.
机译:在本文中,研究了由商业纯钛(CP-Ti)制成的紧凑型拉伸剪切(CTS)试样对负载量裂解裂纹裂纹(FCG)行为的压缩载荷和裂纹闭合的影响。通过压缩载荷效应和裂纹闭合的相互作用,已经解释了在恒定最大负荷控制下的负载荷比下的FCG行为。通过实验获得在稳定的裂缝生长阶段内的负载荷比的裂纹闭合水平的变化。裂缝闭合水平保持恒定,使裂缝闭合效果在前阶段中的FCG行为主导。虽然在后阶段,裂缝关闭水平逐渐下降。目前可以忽略裂纹闭合效果,并且压缩载荷效应在后阶段起到主导作用。同时,通过有限元方法(FEM)描述了裂纹尖端裂纹对裂纹尖端机械行为的影响,以解释前阶段的异常。确认,在负载比率的预级卸载过程中,存在由裂纹闭合效应引起的最大反转塑料区。

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