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首页> 外文期刊>Fatigue & Fracture of Engineering Materials & Structures >Fatigue crack propagation from a precrack under combined torsional and axial loading
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Fatigue crack propagation from a precrack under combined torsional and axial loading

机译:轴向和轴向载荷共同作用下预裂纹的疲劳裂纹扩展

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摘要

Fatigue tests of crack propagation from a precrack in thin-walled tubular specimens made of a medium-carbon steel were performed under cyclic torsion with and without superposed static or cyclic axial loading. The stress ratio of cyclic loading was -1. The fatigue crack-propagation path from a precrack was compared with the predictions based on the maximum tangential stress criterion. The direction of fatigue crack propagation follows the direction of the maximum of the range of the tangential stress, DELTA sigma_(theta max), near the crack tip determined from the stress intensity factor (SIF) which was calculated by considering the contacts of crack faces at the minimum load. The SIF calculated from the actual crack path by using the body force method (BFM) showed that the mode II SIF range quickly approached zero after a small amount of crack extension. The crack-propagation rate decreased first and then increased with crack extension. The initial dip of the crack-propagation rate was caused by the development of crack closure with crack extension. As cracks extended a long distance, the propagation rate was faster than the uniaxial data. This acceleration of crack propagation was caused by excessive plasticity near the crack tip.
机译:在有和没有叠加的静态或循环轴向载荷的情况下,在循环扭力下,对由中碳钢制成的薄壁管状试件中的裂纹从裂纹扩展处的裂纹扩展进行了疲劳试验。循环载荷的应力比为-1。将来自预裂纹的疲劳裂纹扩展路径与基于最大切向应力准则的预测进行了比较。疲劳裂纹扩展的方向遵循在裂纹尖端附近切向应力范围DELTA sigma_(theta max)的最大值的方向,该应力由应力强度因子(SIF)确定,应力强度因子是通过考虑裂纹面的接触来计算的在最小负载下。通过使用体力法(BFM)从实际裂纹路径计算出的SIF显示,模式II SIF范围在少量裂纹扩展后迅速接近零。裂纹扩展率先下降,然后随着裂纹扩展而增加。裂纹扩展速率的初始下降是由裂纹扩展和裂纹扩展引起的。由于裂纹扩展了很长的距离,因此传播速率要比单轴数据快。裂纹扩展的加速是由于裂纹尖端附近的过度塑性引起的。

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