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Research on the process of micro-crack damage evolution and coalescence in brittle materials

机译:脆性材料中微裂纹损伤演化与聚结过程的研究

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摘要

Damage and failure of quasi-brittle materials are caused by evolution and coalescence of micro-cracks. To solve the problem of elliptical micro-crack growth at the elastic deformation stage, a method of complex potential functions is proposed and the effect of the initial orientation on micro-crack growth and deflection is discussed. The critical stress condition for the initial damage is derived according to the criterion of micro-crack growth. Based on energy conservation during wing-crack propagation, a damage constitutive model is developed with the strain criterion created in the condition of micro-crack coalescence. The stress-strain curves of quasi-brittle materials in uniaxial compression obtained based on this model are examined with the experimental results. In conclusion, (1) wing crack growth, propagation, and coalescence at the tips of micro-cracks eventually lead to the formation of an anisotropic effective compliance tensor in the damaged material; (2) a large number of micro-crack coalescence is a highly nonlinear phenomenon resulting in failure of materials; and (3) the effective elastic modulus of damaged material decreases with the wing crack propagation length increasing.
机译:准脆性材料的损坏和破坏是由微裂纹的演化和结合引起的。为了解决椭圆形微裂纹在弹性变形阶段的生长问题,提出了一种复杂的势函数方法,并讨论了初始取向对微裂纹生长和挠度的影响。初始损伤的临界应力条件是根据微裂纹增长的准则得出的。基于机翼裂纹扩展过程中的能量守恒,建立了基于微裂纹合并条件下的应变准则的损伤本构模型。实验结果验证了基于该模型获得的准脆性材料在单轴压缩下的应力-应变曲线。总之,(1)机翼裂纹在微裂纹尖端的增长,扩展和聚结最终导致在受损材料中形成各向异性的有效顺应张量; (2)大量的微裂纹合并是一种高度非线性的现象,导致材料的破坏; (3)损伤材料的有效弹性模量随机翼裂纹扩展长度的增加而减小。

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