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Effects of T-stresses on fracture initiation for a closed crack in compression with frictional crack faces

机译:T应力对具有摩擦裂纹面的压缩闭合裂纹裂缝萌生的影响

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摘要

This paper studies crack extension resulting from a closed crack in compression. The crack-tip field of such a crack contains a singular field relative to K_(II) and non-singular T-stresses T_x and T_y parallel and perpendicular to the crack plane, respectively. Using a modified maximum tensile stress criterion with the singular and non-singular terms, the kinking angle at the onset of crack growth is determined by a two parameter field involving the mode-II stress intensity factors and T-stresses, and at fracture initiation a wing crack may be created at an arbitrary angle from 0 deg to 90 deg. A compressive T_y increases the kinking angle and reinforces apparent mode-II fracture toughness, while a compressive T_x decreases the kinking angle and enhances apparent mode-II fracture toughness. The direction and resistance of fracture onset is strongly affected by T-stresses as well as frictional stress. The von Mises effective stress is determined for small-scale yielding near the crack tip. The effective stress contour shape exhibits a marked asymmetrical behavior unless 2T_x = T_y <= 0 for plane stress state. Coulomb friction between two crack faces generally increases the kinking angle, shrinks the size enclosed by the effective stress contour and enhances apparent fracture toughness. Field evidence and experimental observations of many phenomena involving the growth of closed cracks in compression agree well with theoretical predictions of the present model.
机译:本文研究了由压缩闭合裂纹导致的裂纹扩展。此类裂纹的裂纹尖端场包含相对于K_(II)的奇异场和分别平行于并垂直于裂纹平面的非奇异T应力T_x和T_y。使用带有奇异项和非奇异项的修改后的最大拉伸应力准则,裂纹扩展开始时的扭结角由涉及模式II应力强度因子和T应力的两个参数字段确定,并且在断裂开始时由机翼裂纹可能会以0度到90度之间的任意角度产生。压缩T_y增加扭结角并增强表观II型断裂韧性,而压缩T_x减小扭结角并增强表观II型断裂韧性。 T应力和摩擦应力强烈影响断裂的方向和阻力。 von Mises有效应力是针对裂纹尖端附近的小规模屈服确定的。有效应力轮廓形状表现出明显的不对称行为,除非平面应力状态的2T_x = T_y <= 0。两个裂纹面之间的库仑摩擦通常会增加扭结角,缩小有效应力轮廓所包围的尺寸,并增强表观断裂韧性。涉及压缩中闭合裂纹增长的许多现象的现场证据和实验观察与本模型的理论预测非常吻合。

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