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Load History Effects Resulting from Compression Precracking

机译:压缩预焊接引起的负载历史效果

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Compression precracking (CPC) has seen renewed interest as a possible alternative procedure for generating fatigue crack growth threshold data with minimal load history effects, but recent testing confirms results from the literature that compression precracking does induce load history effects through residual stresses that influence subsequent fatigue crack growth test data. Using the CPC method, specimens are precracked with both maximum and minimum compressive loads. Compressive yielding occurs at the crack-starter notch, resulting in a local tensile residual stress field through which the fatigue crack must propagate. Although the tensile residual stress field contributes to the driving force for precracking, it also introduces the possibility of history effects that may affect subsequent fatigue crack growth. The tensile residual stress field elevates the local driving force at the crack tip, promoting higher crack growth rates than would be expected from the applied loading. This paper presents three-dimensional finite element results and experimental data for compact tension specimens that characterize the load history effects induced by compression precracking. The analysis results indicate that for low tensile loading levels near the threshold region, the residual stresses cause the calculated crack tip driving force to increase from the applied driving force by 25 % or more. In addition, significant crack growth of about two times the estimated plastic zone size is needed to grow away from the residual stress field and reduce the calculated crack tip driving force to within 5 % of the applied driving force. Experimental results show that growth of about two to three times the estimated plastic zone size is necessary to establish steady growth rates under constant ΔK loading for the materials and loading levels evaluated. Constant ΔKtesting following compression precracking will demonstrate when residual stress effects are no longer significant and will ensure consistent growth rates.
机译:已经看到压缩预裂(CPC)作为一种可能的替代过程,以产生具有最小负载历史效应的疲劳裂纹生长阈值数据的可能替代过程,但最近的测试证实了通过影响随后疲劳的残余应力诱导负荷历史效应的文献的结果。裂缝增长试验数据。使用CPC方法,用最大和最小压缩负载预处理样品。在裂缝启动器凹口处发生压缩产量,导致局部拉伸残余应力场,疲劳裂缝必须繁殖。尽管拉伸残余应力场有助于预粘的驱动力,但它还介绍了可能影响随后疲劳裂纹生长的历史效应的可能性。拉伸残余应力场在裂纹尖端升高局部驱动力,促进比施加的载荷所期望的更高的裂纹生长速率。本文介绍了紧凑型张力标本的三维有限元结果和实验数据,其表征了通过压缩预粘引起的负载历史效应。分析结果表明,对于阈值区域附近的低拉伸负载水平,残余应力导致计算出的裂缝尖端驱动力从施加的驱动力增加25%或更多。另外,需要大约两倍的显着裂纹生长估计的塑料区尺寸来远离残余应力场生长,并将计算出的裂缝尖端驱动力降低到施加驱动力的5%内。实验结果表明,估计的塑料区大小约两到三倍的生长是在恒定ΔK载荷下建立稳定的生长速率,用于评价的材料和装载水平。在压缩预裂后恒定ΔKTESTing将显示剩余应力效应不再重要并且确保一致的增长率。

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