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Fatigue cracks emanating from sharp notches in high-strength aluminium alloys: The effect of loading direction, kinking, notch geometry and microstructure

机译:高强度铝合金尖锐缺口产生的疲劳裂纹:加载方向,扭结,缺口几何形状和微观结构的影响

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摘要

The effect of notch geometry on the propagation of fatigue cracks emanating from sharp V-shaped notches was investigated. To this purpose, an experimental campaign has been conducted on Al-7075-T651 specimens carrying notches with aperture angles of 45°, 90°, and 135°. In order to investigate the role of microstructure texture, specimens were extracted from the plates with the main axis either in the longitudinal rolling direction (L-samples) or in the transversal direction (T-samples), or 45° inclined with respect to both directions (LT-samples). The effect of stress amplitude was investigated by performing tests at two load levels. Three loading directions 0 = 0°, 45° and 90° were considered. Some specimens experienced pure Mode I loading condition, whereas the remaining ones were subjected to combined Mode I and Mode II loading condition. The crack deflection induced by the variation in loading direction was determined by measuring the kinking angle. A linear elastic fracture mechanics approach was adopted for the analysis of experimental results. Stress intensity factors (SIF) of straight cracks were calculated using an appropriate weight function set up for studying inclined edge cracks emanating from sharp V-notches. On the contrary, a finite element model has been built up to derive the SIFs at the tip of the kinked cracks. The influence of K_II on the crack propagation was discussed on the basis of theoretical and semi-empirical models. It has been found that (ⅰ) the crack initiation at the notch root occurred in mixed mode conditions, (ⅱ) a decreasing Mode II component with growing crack length was observed under initial loading direction 0_o = 45° and 0_o = 90°, (ⅲ) a crack deflection was observed after 45° rotation of the initial loading direction; a good prediction of the kinking angle was obtained using the maximum tangential stress criterion, and (iv) a fairly good rationalization of all the collected crack growth rate data is obtained if the driving force for crack propagation is expressed in terms of K_I.
机译:研究了缺口几何形状对由尖锐的V形缺口产生的疲劳裂纹扩展的影响。为此,已经对带有缺口角为45°,90°和135°的缺口的Al-7075-T651标本进行了实验。为了研究微结构织构的作用,从板中取出标本,主轴在纵向滚动方向(L样本)或在横向方向(T样本)或相对于两者倾斜45°方向(LT样本)。通过在两个负载水平下进行测试,研究了应力振幅的影响。考虑了三个加载方向0 = 0°,45°和90°。一些标本经历了纯模式I加载条件,而其余样本则经受了模式I和模式II的组合加载条件。通过测量扭结角确定由载荷方向变化引起的裂纹挠度。采用线性弹性断裂力学方法对实验结果进行分析。直裂纹的应力强度因子(SIF)是使用适当的权重函数计算得出的,该权重函数用于研究由尖锐的V形缺口产生的倾斜边缘裂纹。相反,已经建立了一个有限元模型来推导扭结裂纹尖端的SIF。在理论模型和半经验模型的基础上,讨论了K_II对裂纹扩展的影响。已经发现(ⅰ)切口根部的裂纹萌生在混合模式条件下发生,(ⅱ)在初始载荷方向0_o = 45°和0_o = 90°时观察到II型分量随裂纹长度的增加而降低,( ⅲ)在初始加载方向旋转45°后观察到裂纹挠度;使用最大切向应力准则可以很好地预测弯折角,并且(iv)如果用K_I表示裂纹扩展的驱动力,则可以很好地合理化所有收集的裂纹扩展速率数据。

著录项

  • 来源
    《International Journal of Fatigue》 |2009年第12期|1996-2005|共10页
  • 作者单位

    Department of Materials Engineering and Industrial Technologies, University of Trento, via Mesiano 77, 38100 Trento, Italy;

    Department of Mechanical, Nuclear and Production Engineering, University of Pisa, via Diotisalvi 2, 56126 Pisa, Italy;

    Department of Materials Engineering and Industrial Technologies, University of Trento, via Mesiano 77, 38100 Trento, Italy;

    Department of Materials Engineering and Industrial Technologies, University of Trento, via Mesiano 77, 38100 Trento, Italy;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    crack kinking; Sharp V-notches; loading direction; mixed mode; Al-7075-T651;

    机译:裂缝扭结锋利的V型缺口;加载方向;混合模式;Al-7075-T651;

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