ISSN 1000-3665 CN 11-2202/P
    张科,潘哲,刘享华. 含折线型裂隙砂岩试件翼型裂纹起裂与扩展机制研究[J]. 水文地质工程地质,2022,49(3): 103-111. DOI: 10.16030/j.cnki.issn.1000-3665.202107058
    引用本文: 张科,潘哲,刘享华. 含折线型裂隙砂岩试件翼型裂纹起裂与扩展机制研究[J]. 水文地质工程地质,2022,49(3): 103-111. DOI: 10.16030/j.cnki.issn.1000-3665.202107058
    ZHANG Ke, PAN Zhe, LIU Xianghua. Investigation of the wing crack initiation and propagation mechanism of the sandstone specimen containing a folded fissure[J]. Hydrogeology & Engineering Geology, 2022, 49(3): 103-111. DOI: 10.16030/j.cnki.issn.1000-3665.202107058
    Citation: ZHANG Ke, PAN Zhe, LIU Xianghua. Investigation of the wing crack initiation and propagation mechanism of the sandstone specimen containing a folded fissure[J]. Hydrogeology & Engineering Geology, 2022, 49(3): 103-111. DOI: 10.16030/j.cnki.issn.1000-3665.202107058

    含折线型裂隙砂岩试件翼型裂纹起裂与扩展机制研究

    Investigation of the wing crack initiation and propagation mechanism of the sandstone specimen containing a folded fissure

    • 摘要: 岩体内部赋存的裂隙很多表现为折线型,为探究这类岩体的断裂机制,制备含折线型裂隙砂岩试件并对其进行单轴压缩试验。采用数字图像相关(DIC)方法计算加载过程中的变形场演化,根据新生裂纹两侧的位移差异识别裂纹类型;运用扩展有限元法(XFEM)模拟断裂过程,根据应力分布特征解释翼型裂纹起裂与扩展机制。DIC计算结果表明,新生裂纹处出现应变局部化带,裂纹两侧发生相对分离;含直线型和折线型裂隙砂岩试件的翼型裂纹分别萌生于预制裂隙端部以及折角处,这是因为裂隙几何形态会改变拉应力集中位置;含折线型裂隙砂岩试件的起裂应力小于含直线型裂隙砂岩试件,这是因为相同加载条件下前者的最大拉应力值更大;这2类试件的裂纹扩展均是由于裂纹尖端集中的拉应力引起的,裂纹依然呈张开状态;裂隙几何形态未改变试件的最终破坏模式,均表现为对角剪切破坏。

       

      Abstract: There are many folded fissures in the rock masses. In order to explore the fracture mechanism of these rock masses, the sandstone specimens containing a folded fissure are prepared and the uniaxial compression tests are performed. The digital image correlation (DIC) method is used to calculate the evolution of deformation field during the loading process. The crack type is identified by the displacement difference between the initiated crack sides. The extended finite element method (XFEM) is used to simulate the fracture process. According to the stress distribution characteristics, the wing crack initiation and propagation mechanism are explained. The DIC calculation results show that the strain localization bands appear at the locations of the initiated cracks and the relative separation occurs at the two sides of the cracks. For sandstone specimens containing a straight fissure and a folded fissure, the wing cracks initiate at the tips of the pre-existing fissure and at the angle of fissure, respectively. The reason for this is that the location of tensile stress concentration is dominated by the geometric shape of the fissure. The crack initiation stress of the sandstone specimen containing a folded fissure is smaller than that of the specimen containing a straight fissure, because the maximum tensile stress of the former is larger under the same loading condition. The crack propagation of these specimens is caused by the concentrated tensile stress at the crack tip and the propagated cracks remain open. The geometric shape of the fissure does not change the final failure mode of the specimens, which is shown as the diagonal shear failure.

       

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