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Detecting Overload from Strain Information during Fatigue Crack Propagation under Negative Stress Ratio

机译:负应力比下疲劳裂纹扩展过程中应变信息的过载检测

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In the present study, a detection method of an overload application during stress cycles under constant amplitude was investigated. Also, the effect of the tensile overload was shown at three Stress ratios: R = 0, -1, and -1.5, to understand the effects of R on crack propagation after an overload. At the baseline of R = 0, after the overload, retardation in the crack propagation was observed, and the crack growth rate decreased. However, in the case of R = -1.5, the fatigue crack growth rate actually accelerated after the tensile overload. The detection of that crack propagation behavior was attempted through the information of the strain waveform h; h = epsilon_y + 1.2 lambda epsilon_x, where epsilon_x and epsilon_y are the local strains at the specimen axis, and lambda is the strain range ratio DELTA epsilon_y/DELTA epsilon_x. The waveform shape of h was changed after the overloading. Also, the application of the overload could be detected by the variation of the strain range ratio lambda. Especially, the present method is useful for cases of the crack propagation stage under negative R conditions.
机译:在本研究中,研究了在恒定振幅下应力循环过程中过载应用的检测方法。同样,以三种应力比显示了拉伸过载的影响:R = 0,-1和-1.5,以了解R对过载后裂纹扩展的影响。在R = 0的基线处,过载后,观察到裂纹扩展的延迟,并且裂纹扩展速率降低。但是,在R = -1.5的情况下,拉伸过载后疲劳裂纹的成长速度实际上加快。试图通过应变波形h的信息来检测裂纹的扩展行为。 h = epsilon_y + 1.2 lambda epsilon_x,其中epsilon_x和epsilon_y是样本轴上的局部应变,而lambda是应变范围比率DELTA epsilon_y / DELTA epsilon_x。 h的波形形状在过载后发生变化。另外,可以通过应变范围比λ的变化来检测过载的施加。特别地,本方法对于负R条件下的裂纹扩展阶段的情况是有用的。

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