摘要:
爆炸应力波穿过异质界面时,其传播特性会发生显著变化。工程岩体常存在不连续结构面,特别是深部岩体中的节理和裂隙较为发育。为了深入研究围压与爆破耦合作用下节理岩体的动力响应及损伤机制,本文采用显式动力学数值模拟方法,结合ALE算法和流固耦合技术,对节理岩体的破裂过程进行模拟。基于时域递归理论,分别计算了爆炸应力波穿过节理面时的透射与反射系数。通过爆炸光弹性试验,分析了爆炸应力波在节理岩体中的传播过程与特征。此外,利用Riedel-Hiermaier-Thoma (RHT) 损伤模型,讨论了不同节理角度及不同围压对爆破裂纹扩展行为的影响,并结合FracPaQ程序定量描述了爆破裂纹的分布规律。最后,通过分析节理尖端的主应力分布及动态应力强度因子(DSIFs)变化规律,揭示了节理岩体的爆破损伤机制。结果表明:节理面与主围压对爆破裂纹扩展均有导向作用,且各向异性围压的导向效应会因节理面的存在而减弱。当主围压与节理面垂直时,应力波透射和反射系数随着压力的增加分别呈增大和减小的趋势。由节理面两侧法向与切向位移变化规律,发现剪切应力是尖端翼裂纹扩展的主要原因。根据动态应力强度因子判断,拉伸裂纹在爆破初期主导节理尖端的损伤,而剪切裂纹在后期占主导地位。
Abstract:
Propagation features of explosion-induced stress waves undergo substantial alterations as they traverse heterogeneous interfaces. In rock engineering, the prevalence of discontinuous structural planes, such as joints and fissures, becomes increasingly pronounced with increasing burial depth. To gain a comprehensive insight into the dynamic response and damage mechanism, this paper adopted an explicit dynamics numerical method that integrates the ALE algorithm and fluid-solid coupling technology, which enables precise simulation of the fracture process within jointed rock mass under the combined effects of confining pressure and blast. Based on the time-domain recurrence theory, the transmission and reflection coefficients of stress wave were calculated respectively, and then propagation process and features of stress wave were analyzed by the explosion photoelasticity test. Additionally, Riedel-Hiermaier-Thoma (RHT) damage model was employed to investigate the influence of varying joint angles and confining pressures on cracking behavior. Furthermore, the cracks were quantitatively assessed using the FracPaQ program. Finally, the damage mechanism of the jointed rock mass was revealed by analyzing the principal stress distribution and displacement change of the joint tip. The results showed that both the joint and the maximum pressure have a guiding effect on crack extension, and this effect will be weakened by the presence of the joint. When the maximum pressure is perpendicular to the joint surface, the coefficients of transmission and reflection tend to increase and decrease with the pressure increasing, respectively. From the change rule of normal and tangential displacement on both sides of the joint surface, it is found that shear stress is the main cause of tip-wing crack expansion. And judging from the dynamic stress intensity factors (DSIFs), tensile cracks dominate the damage of the tip at the early stage of the blasting, while shear cracks dominate at the later stage.