The numerical model and direct shear test of joint specimens were simulated by the Particle Flow Code software (PFC2D). In this software, the mechanical behavior of materials could be simulated by displacement and force interaction in particles. The basic relationship between forces and motion of particles is Newton’s second law of motion37.
3.1 Establishment of numerical model
In earlier numerical studies, many scholars used bond removal method (BRM) to generate joint22-23. Since joint can only occur at the contact of particles, the roughness of joint generated by the BRM is greatly affected by particle distribution. Later, the smooth joint model (SJM) was introduced into PFC and allows particles to pass through or overlap each other rather than to spin around each other. So, the SJM solved the shortcomings of the BRM very well and had been widely used in numerical studies of jointed rock masses24-26. However, Bahaaddini et al. 26 found that the smooth joint model might lead to an unreliable increase in the shear strength and normal displacement of joint sample. Finally, the modified smooth joint model (MSJM) had been proposed to achieve better simulation results. In this paper, the same idea was used to establish the numerical model of joint specimens.
Firstly, two contact boxes were established and each box had four frictionless walls. The overall dimensions of the model were 100 mm in width and 60 mm in height. The upper wall of the box below and the bottom wall of the upper box were overlapping. They were generated from the geometric coordinates of the 10 standard roughness joint profiles obtained in Section 2.1. The input of the joint node must follow the right-hand rule as only one face of the wall is active by default.
Second, randomly placed particles were separately generated in the upper and lower parts of the joint sample. The particle size is between 0.15 mm and 0.24mm, which satisfied uniform size distribution. Each numerical joint specimens contained 41 883 particles at a porosity of 0.15. At the beginning of particle formation, there was many overlaps between the particles. After giving an initial stiffness, the overlapping particles generated previously were allowed to rearrange and reached the static equilibrium under friction free conditions. Next, particles with less than one contact were eliminated to reduce internal locking phenomenon24-26.
Then, the BPM was installed on the upper and lower parts of the specimen respectively and the two rough walls in the middle of the specimen were deleted. Next, an appropriately low normal pressure was applied to the specimen. New contacts were generated between the particles of the upper and lower part of the specimen. Finally, the discrete fractures network (DFN) was applied to determine the location of 10 rough joint profiles, and the SJM was applied at the DFN37. According to the above ideas, joint samples with 10 standard roughness were established respectively. Figure 5 shows the 7th joint specimen for illustration.
3.2 Setting and calibration of microscopic parameters
In DEM such as PFC2D, the macroscopic mechanical behavior of the material that we are expecting to simulate is derived by the interaction of constituents such as particle and bond. So far, researchers had not found that the micro parameters of these components have a specific corresponding relationship with the macroscopic mechanical behavior of the model. Therefore, these microscopic parameters must be calibrated through repeated trial and error of conventional physical tests.
3.2.1 Calibration process of microscopic parameters of the BPM
In order to calibrate microscopic parameters of the BPM applied in intact rock, numerical specimen with length of 50 mm and height of 100 mm were generated22-28. The setting of particle distribution and microscopic parameters is completely consistent with Section 3.2. The specimen contained 34901 particles. The uniaxial compression tests were carried out without confining pressure, and the result showed that the uniaxial compressive strength (UCS) was 59.09 MPa and the deformation modulus (E0)was 8.83 GPa for the intact rock. The macroscopic mechanical properties and failure mode of the numerical specimen were consistent with the physical test results of real rock (Fig. 6). The calibrated microscopic parameters of BPM are summarized in Table 1.
Table 1. Microscopic parameters of balls and bonds in intact rock.
Particle parameters
|
|
Parallel bond parameters
|
|
Particle density [kg/m3]
|
2000
|
Modulus`E* [GPa]
|
5.5
|
Modulus E* [GPa]
|
5.5
|
Stiffness ratio`kn/`ks
|
1.5
|
Stiffness ratio kn/ks
|
1.5
|
Tensile strength [MPa]
|
34.5
|
Friction coefficient μ
|
0.7
|
Cohesion [MPa]
|
34.5
|
3.2.2 Calibration process of microscopic parameters of the SJM
In order to calibrate microscopic parameters of the SJM, the direct shear tests on planar joints were conducted. The establishment of joint specimen is consistent with Section 3.1, while the position of rough joints is replaced with a flat joint established by the SJM. In the direct shear tests, a constant normal stress was applied to the top wall by using a servo mechanism (see section 3.4 for details). The shear stress shear displacement curves of numerical direct shear test of flat joints under normal stresses of 2, 4, 6 and 8MPa are shown in Fig. 7. It can be seen that the shear stress curve shows the characteristics of slip failure, which is consistent with the indoor physical test.
As shown in Fig. 7(b), the difference of shear strength results between numerical test and indoor physical test of flat joints under the same scheme was very small and the friction angle of joint surface was near 40.22°. Therefore, it can be considered that the simulation and parameter setting of joint surfaces in the numerical calculation of this paper are very reasonable. The calibrated microscopic parameters of the SJM were presented in Table 2.
Table 2. Microscopic parameters of joint surface.
Normal stiffness
sj_kn
[GPa/m]
|
Shear stiffness
sj_ks
[GPa/m]
|
Friction coefficient
sj_fric
|
Large deformation
sj_large
|
400
|
100
|
0.83
|
1
|
3.3 Shearing process control
Figure 8 shows the scheme of the direct shear test of rough joint specimen. 3#, 4# and 5# walls belong to the upper shear box and 1#, 2# and 6# walls belong to the lower shear box. During the direct shear test, the lower shear box was fixed and a constant horizontal velocity of 4 mm/s was applied to the upper shear box. Shear stress and shear strain could be calculated by recording the force and displacement of the corresponding wall including 2#, 5# and 6# walls.
The calculations in PFC software were carried out by a time-stepping algorithm. The real time between each calculation step had a small value about 2.904× 10−7 s. That is, the upper and lower wall moved at the rate of 11.616 × 10−7 mm per time step. This movement rate was so slow enough to ensure that the test process of joint specimen was in quasi-static equilibrium. The direct shear tests of joint specimens with 10 standard roughness were carried out and the shearing direction was from left to right by default.
3.4 Servo mechanism
During the direct shear test under constant stress conditions, the normal stress applied to the upper and lower surfaces of sample must be kept constant. However, the direct application of load cannot be realized in the PFC software. The constant load state could only be maintained by a servo function that can automatically changing the normal moving speed of the upper and lower walls at each calculation step.
The normal velocity v(wall) of the upper surface of joint specimen could be set as follows:
v(wall) = G(σmeasure - σrequire) = GΔσ (4)
Where G represent the servo parameter, σmeasure represented the normal stress actually applied to the upper surface of the joint specimen, σrequire represented the expected normal stress set by us and Δσ represent the stress difference between σmeasure and σrequire. The maximum value of Δσ was defined as:
Δσ(wall) = (kn(wall)Ncv(wall)Δt)/A (5)
In Eq. (5), kn(wall) represented the average stiffness of the particles in contact with 1# and 4# walls, Nc represent the number of particles and A represent the area of the wall. In order to minimize the difference between σmeasure and σrequire, a release factor α was introduced as shown in Eq. (6).
|Δσ(wall)|< α|Δσ| (6)
When substituting Eq. (4) and Eq. (5) into Eq. (6), the Eq. (7) could be obtained.
(kn(wall)NcG|Δσ|Δt)/A < α|Δσ| (7)
Thus, the servo coefficient G could be defined as follows:
G = αΑ/(kn(wall)NcΔt) (8)
When the software runs a calculation step, the servo parameter G of the next calculation step is calculated by the servo function in advance. The normal velocity v(wall) of the upper walls well be updated by Eq. (4). Next, the servo parameter G required for the next calculation step is also calculated simultaneously.
In order to verify the reliability of the above method, the direct shear tests of planar joint under normal stress conditions of 1MPa, 2MPa and 3MPa were carried out. After data monitoring, Figure 9 shows the normal stresses applied to the upper and lower walls. It could be seen that σmeasure and σrequire was very close and the normal stress application process was very stable and reliable. In the follow-up study, the normal stresses applied to the joint specimens were 2 MPa, 4 MPa, 6MPa and 8 MPa respectively.