Research Article
Study on the Interaction of Collinear Cracks and Wing Cracks and Cracking Behavior of Rock under Uniaxial Compression
Figure 11
Simulation results of two unequal collinear cracks with varied bridge ligament (). (a) d = 5 mm, shear crack coalescence. (b) d = 10 mm, wing crack coalescence. (c) d = 20 mm, shear-wing crack coalescence. (d) c = 30 mm, wing crack failure. (e) d = 40 mm, wing crack failure.
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