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Experimental study on crack coalescence mechanisms of pre-existing flaws under blast loading

机译:爆炸载荷作用下预先存在缺陷的裂纹聚并机理的实验研究

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The PMMA model transmission-type experiment of dynamic caustics was carried out to simulate the fracture blasting process of material containing pre-existing flaws using the dynamic caustic-test system. The mechanism of the fracture coalescence among four prefabricated flaws with echelon geometry distribution was studied under blast loading. The experiment results show that two wing cracks respectively coalescing with the flaw F2 and flaw F3 appear at both tips of the flaw F1 closest to the blasthole. Whereas the flaw F4 doesn't produce wing cracks, the flaw F2 and flaw F3 also respectively generate two wing cracks which don't link up the flaw F4. Crack propagation is greatly affected by preexisting flaws. During the whole fracture process, the wing crack velocity oscillates with the increase of crack propagating time. The value of dynamic stress intensity factor reaches the maximum in a moment and then gradually decreases. The changes of dynamic stress intensity factor also oscillate in the whole time. Furthermore, the value of dynamic stress intensity factor K_Ⅱ~d is smaller than that of dynamic stress intensity factor K_Ⅰ~d. The results of the present research can provide the theoretical basis for the study on blasting of rock containing flaws.
机译:进行了动态苛性碱的PMMA模型传递型实验,以使用动态苛性碱试验系统来模拟包含预先存在的缺陷的材料的破裂喷砂过程。研究了爆炸载荷作用下四个具有梯形几何分布的预制缺陷之间的断裂聚结机理。实验结果表明,在最靠近爆破孔的缺陷F1的两个尖端出现两个分别与缺陷F2和缺陷F3合并的机翼裂纹。裂纹F4不会产生机翼裂纹,而裂纹F2和F3也会分别产生两个不会将裂纹F4连接起来的机翼裂纹。预先存在的缺陷会极大地影响裂纹的扩展。在整个断裂过程中,机翼裂纹速度随裂纹扩展时间的增加而振荡。动应力强度因子的值在瞬间达到最大值,然后逐渐减小。动应力强度因子的变化也在整个时间里振荡。此外,动应力强度因子K_Ⅱ〜d的值小于动应力强度因子K_Ⅰ〜d的值。研究结果可为含缺陷岩石的爆破研究提供理论依据。

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