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    王兴路, 贺利乐. 金属材料表面裂纹疲劳扩展形状演变规律[J]. 机械工程材料, 2019, 43(11): 57-61. DOI: 10.11973/jxgccl201911013
    引用本文: 王兴路, 贺利乐. 金属材料表面裂纹疲劳扩展形状演变规律[J]. 机械工程材料, 2019, 43(11): 57-61. DOI: 10.11973/jxgccl201911013
    WANG Xinglu, HE Lile. Shape Evolution Rule of Surface Crack Fatigue Propagation of Metallic Materials[J]. Materials and Mechanical Engineering, 2019, 43(11): 57-61. DOI: 10.11973/jxgccl201911013
    Citation: WANG Xinglu, HE Lile. Shape Evolution Rule of Surface Crack Fatigue Propagation of Metallic Materials[J]. Materials and Mechanical Engineering, 2019, 43(11): 57-61. DOI: 10.11973/jxgccl201911013

    金属材料表面裂纹疲劳扩展形状演变规律

    Shape Evolution Rule of Surface Crack Fatigue Propagation of Metallic Materials

    • 摘要: 基于裂纹扩展过程中的能量释放率理论提出一种表面裂纹疲劳扩展形状的计算方法,研究了在拉伸和弯曲疲劳载荷作用下金属板材中表面裂纹扩展形状演变规律,并进行了试验验证。结果表明:计算得到在拉伸载荷作用下的裂纹扩展初始阶段,表面裂纹呈半圆形,随着裂纹深度的增加,表面裂纹形状逐渐变为扁长型半椭圆形;在弯曲载荷作用下的裂纹扩展初始阶段,表面裂纹呈半圆形,随着裂纹深度的增加,表面裂纹形状逐渐变为细长型半椭圆形;试验得到表面裂纹在疲劳扩展过程中的形状逐渐靠近计算得到的形状;在表面裂纹长度相等的条件下,试验与计算得到的裂纹深度的相对误差小于4.5%,说明采用基于能量释放率理论的表面裂纹扩展形状计算方法来预测表面裂纹疲劳扩展的形状演变是可行的。

       

      Abstract: A calculation method for surface crack fatigue propagation shape was proposed based on the theory of energy release rate during crack propagation, and the shape evolution of surface crack propagation in metal sheet under tensile and bend fatigue loads was studied and verified by experiments. The results show that the surface crack shape obtained by calculation was semi-circular in the initial stage of surface crack propagation under the tensile load, and gradually changed to flat long semi-elliptical shape with the increase of crack depth; the surface crack shape was semi-circular in the initial stage of crack propagation under the bending load, and gradually became slender semi-elliptical shape with the increase of crack depth. The shape of surface crack during fatigue propagation obtainbed by tests was getting closer to that obtained by calculation. The relative error of crack depth between the tested value and calculated value was less than 4.5% under the condition of equal surface crack length, indicating that the calculation method of surface crack propagation shape based on the theory of energy release rate was feasible to predict shape evolution of surface crack fatigue propagation.

       

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