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PRACTICAL FORMULA OF THE SHAPE EVOLUTION OF A SURFACE CRACK UNDER FATIGUE LOADING

机译:疲劳载荷下表面裂纹形状演变的实用公式

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Fatigue life estimation for planar cracks, e.g. part-through surface cracks or embedded cracks is very important because most of fatigue cracks found in welded built-up structures show planar crack morphologies. Although authors had proposed the estimation procedure of crack shape evolution for a planar crack based on the fracture mechanics approach, this method cannot apply if the values of stress intensity factor at the vertices of the surface crack approximated as an ellipse cannot calculated. Then, development of the shape evolution procedure of a planer crack under the stress field with arbitrary gradient, because fatigue cracks in welded built-up structures exist near the stress concentrated region. A Practical estimation formula the shape evolution of a surface crack under stress field with the gradient is proposed in this study. This formula is established by considering the stress field under no crack condition and some former proposed formulae under uniform and pure bending stress fields. The validity of the proposed formula are confirmed by comparing some measured surface crack shape evolutions under some stress gradient conditions.
机译:平面裂纹的疲劳寿命估算,例如部分贯通的表面裂纹或嵌入式裂纹非常重要,因为在焊接的组合结构中发现的大多数疲劳裂纹都显示出平面裂纹形态。尽管作者基于断裂力学方法提出了平面裂纹的裂纹形状演变的估计程序,但如果无法计算近似于椭圆的表面裂纹顶点处的应力强度因子,则该方法将不适用。然后,由于应力集中区域附近存在焊接组合结构中的疲劳裂纹,因此,在任意梯度应力场下,平面裂纹的形状演化过程都得到了发展。提出了一个实用的估算公式,该公式估算了应力场在梯度作用下的表面裂纹的形状演化。该公式是通过考虑无裂纹条件下的应力场以及一些在均匀和纯弯曲应力场下提出的公式而建立的。通过比较在某些应力梯度条件下测得的一些表面裂纹形状的演变,可以证明所提公式的有效性。

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