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  • Volumetric fracturing behav...
    Zhou, T.; Zhu, J.B.; Ju, Y.; Xie, H.P.

    Engineering fracture mechanics, January 2019, 2019-01-00, 20190101, Letnik: 205
    Journal Article

    •We successfully produced resin-based artificial rock specimens with 3D internal flaws with the SLA 3DP technique.•The flaw geometry greatly affects volumetric and mechanical properties of samples with 3D internal flaws.•Wing and anti-wing cracks could only propagate for approximately 1–1.5times the length of the initial flaw.•The ratio of initial cracking stress to uniaxial compressive strength is independent on the number of pre-existing flaws. In nature, rock discontinuities, e.g., cracks, voids and joints, are usually three-dimensional, which to a large extent control the volumetric fracturing behaviors of rock masses. Understanding their growth behaviors and effects on rock volumetric fracturing properties is crucial for the stability assessment of rock engineering. In this study, three-dimensional printing (3DP) method was adopted to fabricate resin-based artificial rocks containing single flaw and double pre-existing penny-shaped 3D internal flaws. Static uniaxial compression tests were, subsequently, conducted on these samples to investigate the influence of flaw number, flaw angle (α) and ligament angle (β) on the volumetric fracturing behaviors of the 3DP artificial rocks. The results indicate that flaw geometry has remarkable influence on the mechanical and fracture behaviors of the flawed samples. The single flawed sample with α equal to 60° has the lowest compressive strength (σc) and axial strain at the peak stress (εa). σc and εa of the double flawed sample generally increase when β changes from 45° to 105°. When the flaw number increases from one to two, the initiation stress of the first wing crack, σc and εa decrease. With the aid of high-speed cameras, we studied 3D crack growth inside the transparent 3DP resin samples in real-time for the first time. Wing and anti-wing cracks wrapped around the flaw edge could only propagate for approximately 1–1.5 times the length of the initial flaw. Wing cracks generated at the inner tips of the flaws cannot coalesce, except for the sample with β of 105°. The maximum crack propagation velocity in single flawed specimens is higher than that in double flawed samples. The continuous propagation of the secondary cracks developed after the peak stress lead to the burst-like failure of the flawed samples. This study could enhance our understanding of volumetric fracturing behaviors of rocks.