#### Abstract

Abrasive gas jet technologies are efficient and beneficial and are widely used to drill metal and glass substrates. When the inlet pressure is increased, gas jets could be powerful enough to break rock. They have potential uses in coal-bed methane exploration and drilling because of their one-of-a-kind nonliquid jet drilling, which avoids water invasion and borehole collapse. Improving the efficiency of rock breakage using abrasive gas jets is an essential precondition for future coal-bed methane exploration. The nozzle structure is vital to the flow field and erosion rate. Furthermore, optimizing the nozzle structure for improving the efficiency of rock breakage is essential. By combining aerodynamics and by fixing the condition of the nozzle in the drill bit, we design four types of preliminary nozzles. The erosion rates of the four nozzles are calculated by numerical simulation, enabling us to conclude that a nozzle at Mach 3 can induce maximum erosion when the pressure is 25 MPa. Higher pressures cannot improve erosion rates because the shield effect decreases the impact energy. Smaller pressures cannot accelerate erosion rates because of short expansion waves and low velocities of the gas jets. An optimal nozzle structure is promoted with extended expansion waves and less obvious shield effects. To further optimize the nozzle structure, erosion rates at various conditions are calculated using the single-variable method. The optimal nozzle structure is achieved by comparing the erosion rates of different nozzle structures. The experimental results on rock erosion are in good agreement with the numerical simulations. The optimal nozzle thus creates maximum erosion volume and depth.

#### 1. Introduction

A high-pressure gas jet is efficient for drilling and cutting metal or glass. It has been widely used to drill hard and brittle materials for several decades [1–3]. To date, researchers have used the technology for rock or coal breakage in coal-bed methane exploration [4–6]. As a nonliquid invasive jet, the abrasive gas jet avoids borehole collapse, which is mainly induced by water invasion during assisted drilling with high-pressure water jets [7–9]. Like supercritical CO_{2}, the abrasive gas jet has great potential for assisted drilling and perforation in coal-bed methane exploration [10]. The assumption is that high-pressure abrasive gas jet is powerful and effective enough to break rock and coal. There are many methods that improve the impact force of abrasive gas jets. The most significant method is optimization of the nozzle structure.

For compressible fluid jets, the nozzle structure decides the outlet velocity and flow-field structure [11]. There are many nozzle types (e.g., straight nozzle, Laval nozzle, and convergent nozzle) available for rock breakage. Fortunately, many studies have provided essential guidance. Tan et al. proposed that the inclusion of a Laval nozzle would magnify the velocity and eliminate the instability of the airflow field. They also conjectured that the Laval nozzle was best equipped for high velocity and stable flow fields [12]. Li et al. found that the flow generated by the Laval nozzle had a higher exit velocity in the vicinity of the nozzle, compared to a straight nozzle. Thus, a Laval nozzle is more efficient than a straight one. The flow generated by a Laval nozzle is also less convergent, and the velocity gradient along the radial direction is more moderate than a straight nozzle [13], according to flow characteristics. The Laval nozzle is considered a better choice for rock and coal breakage. Alkhimov et al. studied the relationship between nozzle structure and final exit velocity of particles, finding an optimizing structure and substream length [14]. Huang et al. investigated nozzle configurations on rock erosion by comparing convergent and Laval nozzles. He concluded that the Laval nozzle enhanced rock erosion, depending on pressure and temperature conditions. Additionally, the jet from a nozzle with a smooth inner profile always had a greater erosion ability than a Laval with a broken line inner profile [15].

The reason why nozzle structure affects the outlet pressure is that it decides the expansion status of the gas jet. The expansion status depends on the ratio of static pressures between the outlet and the atmosphere, which is equal to the rate of the section between the nozzle outlet and inlet [16]. The expansion status is significant to the flow field, which is substantial to abrasive acceleration and abrasive velocity impacting the material [17]. Gregorio investigated the compressibility effect on a supersonic turbulent jet with a nozzle Mach exit of Ma = 1.5. The results showed that the overexpanded jet presented a larger spreading rate than other conditions. The overexpanded jet was characterized by a strong shock immediately downstream of the nozzle exit, inducing a speed deceleration to Ma = 1.1. The fully expanded state was described by a slight overpressure value with respect to the ambient conditions, presenting a train of weak expansion and oblique shock waves. The underexpanded jet showed extreme Mach fluctuations owing to the stronger train of expansions and shock waves [18]. The underexpanded jet presented the best status for converting high gas velocities. Moreover, the Mach disc was an obvious barrier to obtaining a flow-field and high gas velocity, necessary for rock and coal breakage. Because the expansion status relates to the ratio of inlet and outlet pressures, the inlet pressure should be seriously investigated. Tan et al.’s research showed that the maximum value of gas jets increases with increasing inlet pressure. Thus, it oscillates, accompanied by the formation of compression waves in the supersonic region when the inlet pressure is larger than 15 psi. The simulation demonstrates that a Laval nozzle influences the airflow field by increasing the maximum value of the gas jet velocity and by eliminating the compression waves at specific expected values of the pressure inlet [12].

Whereas earlier investigations clarified the relation between nozzle structure and gas jets, the types of nozzle structures that best apply to accelerate abrasives have been rarely studied. The motion of abrasives in gas jets is so complicated that there is no consensual theory on an abrasive acceleration or abrasive erosion mechanisms. Such mechanisms would be significantly affected by gas pressure, abrasive concentration, abrasive size, abrasive density, etc. [19–25]. Ultimately, the only thing that matters is that this property increases the erosion rate of the abrasive gas jet. Thus, we are inspired to estimate the nozzle structure based on erosion rate.

To optimize the nozzle structure of an abrasive gas jet for rock and coal breakage, we designed a preliminary structure by combining aerodynamics and installing a drilling engineered nozzle. Moreover, the effects of various convergent angles, draw ratio of the throat, divergent angles, etc. on the erosion rate were obtained via numerical simulation, thus providing estimates for the optimal nozzle structures. Moreover, the results of numerical simulation are verified by erosion experiments. Finally, the optimal nozzle structure for rock and coal breakage induced with abrasive gas jets is proposed.

#### 2. Preliminary Nozzle Structure Design

A Laval nozzle is a convergent-divergent nozzle, invented by Gustav Patrik de Laval in 1888 for steam engine applications to produce a supersonic flow in the divergent section, directly following the choked and sonic flow conditions at the narrowest point of the nozzle. Because his paper focused on the erosion rate of the abrasive gas jet, the abrasive velocity was the most relevant to rock breakage. The abrasive velocity largely depended on gas velocity and its gain. The gas velocity reached sonic proportions at the narrowest point, where it transitioned from the convergent section to the divergent section. Lengthening the narrowest section (i.e., throat section) prolonged the sonic and abrasive acceleration times, promoting the higher initial abrasive velocities at the entrance of divergent section and the higher impact velocities on the rock and coal. Thus, the Laval nozzle with a throat section was used to erode the rock, as shown in Figure 1. Because the abrasive velocity gained mainly from gas, the gas state and velocity of the nozzle should be cleared first.

Assuming the flow state is adiabatic and frictionless, the differential equations of a 1-dimensional steady flow in the nozzle are as follows.

The continuity equation is where is volume, is a sectional area, and is density.

Momentum is

Energy is where is temperature and is constant-pressure specific heat.

State equation is

Momentum equation can be rewritten as where is the local speed of sound.

By putting (1) and (5) together, we get where is the Mach number.

Momentum can also be rewritten as

By putting (6) and (7) together, we get

The second terms of the energy equation can be rewritten as and be plugged into (6), such that

It is clear that the thermodynamic parameters (e.g., , , and ) of the gas jet depend on the changes of nozzle section. Thus, these parameters can be calculated by nozzle section area based on (8), (9), and (10). To optimize the nozzle structure, the way the ratio of the nozzle section area affects the thermodynamics parameter should be figured out first. The continuity equation can be rewritten as where is the critical density, is the critical volume, and is the critical sectional area.

Owing to being equal to and the critical velocity of sound, (11) can be rewritten as

The first four items of the right side of (12) can be replaced with a constant entropy equation related to . The fifth item is equal to . Thus, (12) can be rewritten as

According to (13), the relationship between the Mach number of the nozzle exit and the ratio of the sectional area can be obtained. The sectional area of the nozzle exit can be confirmed by setting the Mach number and the sectional area of the nozzle entrance in advance. For rock and coal erosion, the larger the Mach number at the nozzle exit, the better the abrasive gas jet erodes rock and coal, and the larger the sectional area at the nozzle exit. However, it is impossible to enlarge the sectional area infinitely, because the fixing position is limited by the coal-bed methane well. The permitted maximum length of the nozzle is 40 mm, and the maximum sectional area of nozzle entrance and outlet is 4 mm and 10 mm, respectively, based on the size of the drill bit. By combining the thermodynamic equations and the size of the fixed position of the drill bit, four initial nozzle structures can be designed. Their outlet velocities are Mach numbers 2, 3, 4, and 5, as shown in Figure 2.

**(a) Mach 2**

**(b) Mach 3**

**(c) Mach 4**

**(d) Mach 5**

#### 3. Further Optimizing the Laval Nozzle

The four Laval nozzles, discussed in Section 2, differ with outlet velocity. Moreover, the nozzle having a Mach 5 outlet velocity is efficient for energy transformation. However, it cannot tell when it is the best to accelerate to abrasive mode to erode the rock and coal, because abrasive acceleration relates not only to gas velocity but also to gas density, viscosity, temperature, pressure gradient, etc. [26–29]. Furthermore, the inlet pressure is critical to abrasive acceleration and velocity, because it determines the expansion state of the gas jet. Moreover, the convergent angle, divergent angle, and draw ratio of the nozzle throat section dramatically affect the expansion state. Thus, the Laval nozzle should be specially designed. We use ANSYS–FLUENT as an efficient analysis of the flow-field of the gas jet. Its discrete phase model (DPM) can precisely resolve the abrasive motion. It provides an erosion model to calculate the erosion rate of the target material. Thus, this section focuses on the effects of various initial FLUENT conditions and structures of the erosion rate of rock.

##### 3.1. Numerical Simulation Model

According to erosion parameters (e.g., nozzle parameter), when the stand-off distance is 100 mm, the numerical simulation geometry model is designed as shown in Figure 3. A structured grid is used for mesh division, and the mesh number is 17,240, based on the mesh sensitivity analysis. The inlet boundary is the pressure inlet; the outlet boundary is the pressure outlet; and the wall surface is a nonslip wall. Whereas the inlet temperatures are all 300 K and the outlet pressures are all 0.1 MPa, the garnet abrasive is 3500 kg/m^{3}, and the diameter is 180 *μ*m. The gas and solid phases are calculated based on the continuous and discrete phase models. Following the convergence and stability of the gas phase, the DPM model calculates abrasives’ parameters (e.g., velocity and spatial locations).

For the gas phase, the RNG *k*-*ε* turbulence model can simulate a high Reynolds number flow of jets. The gas is assumed to be an ideal gas. The governing equations for the RNG *k*-*ε* turbulence model are described in [30].
where

is density; is turbulent kinetic energy; is dissipation rate of ; is time; are the Cartesian coordinates; and are velocity components along and ; is gas viscosity; is eddy viscosity; is the generation term of the turbulent kinetic energy, , resulting from the mean velocity gradient; is the generation term of the turbulent kinetic energy from buoyancy; is the effect of compressible turbulent pulsatile expansion on the total dissipation rate; and and are the reciprocals of the effective Prandtl numbers for turbulent kinetic energy and dissipation rates. is the turbulence Prandtl number; , , and are empirical constants; is the component of gravitational acceleration in the direction, is the thermal expansion coefficient, and is the acoustic velocity.

The gas phase continuity equation is

The gas phase Navier–Stokes equation is
where is the gas volume fraction; is the gas density, kg/m^{3}; is the time, s; is gas velocity vector, m/s; is pressure, kPa; is fluid particle interaction force, N; is gas phase stress tensor; and is gravity acceleration vector, m/s^{2}.

The DPM of the particle phase is given as in [26, 31]: where is the drag force per unit particle mass. where is an additional acceleration caused by the Saffman lift force. Pressure gradient is the particle velocity, is the velocity of the fluid, is gravity acceleration, is the density of the particle, is the diameter of the particle, is the drag coefficient, and is the relative Reynolds number.

FLUENT provides erosion models for analyzing the erosion rate of the target material. Among those, the McLaury erosion model is optimal for investigating rock erosion of abrasive gas jets, because the particle velocity, shape, diameter, etc. are considered [32, 33].
where is the target erosion; is the Brinell hardness of the material; *F*_{s} is a particle shape coefficient; is constant; and *F*_{s} = 1.0 for sharp (angular), 0.53 for semi-rounded, or 0.2 for sully rounded sand particles. Morsi and Alexander used two functional forms of angle dependence, with matching conditions applied at some intermediate angle, . The dependence on impingement angle, , is given in (21) [34].
where , and are empirical constants.

##### 3.2. Verifying of Outlet Velocity of the Laval Nozzle

Equation (13) shows that the Mach number of the nozzle exit only relates to the ratio of the sectional area between the inlet and outlet. The inlet pressure cannot affect the Mach number but can affect the ratio of static pressure between the outlet pressure and atmosphere. To verify the preliminary nozzle structure and numerical simulation model, the data of the Mach number of the jet axial is extracted and shown in Figure 4. The Mach number of the nozzle exit reflects the theoretical analysis. Thus, the preliminary nozzle structure and the numerical simulation model are available in this study.

**(a) Mach 2**

**(b) Mach 3**

**(c) Mach 4**

**(d) Mach 5**

##### 3.3. Effect of Pressure on Erosion Rate

Inlet pressure can dramatically affect expansion state, deciding the flow-field structure and abrasive acceleration. When the nozzle structure does not change, every nozzle has its own best pressure to erode rock at the greatest extent possible. It is necessary, then, to find the best pressure of abrasive gas jets for rock breakage. If the inlet pressure is too small, the velocity of the abrasive cannot be accelerated high enough, leading to a lesser erosion rate. However, if the inlet pressure is too large, the velocity of abrasive can be accelerated extremely high, but it aggravates the wear of the nozzle and shortens its service time. To find the best inlet pressures of the four nozzles and nozzle structure, the erosion rate will be calculated when the inlet pressure is 10 MPa, 15 MPa, 20 MPa, 25 MPa, 30 MPa, and 50 MPa. The most used abrasive of oil and natural gas well drilling is garnet with a diameter of 80 mesh, reflecting the initial parameters of the solid phase of the numerical simulation. The stand-off distance of good drilling is typically 0–100 mm. Moreover, the larger the stand-off distance, the smaller the impact force and velocity of abrasive when the stand-off distance is beyond optimal value. The optimal stand-off distance depends on the potential core of the abrasive gas jet. To rid the effect of optimal stand-off distances and potential cores, confusing the comparison of erosion rate at the different initial condition, the initial stand-off distance is 100 mm of the numerical simulation.

We extract the maximum erosion rate of every numerical simulation case, as shown in Table 1. Similar to the conclusion of Section 2, every nozzle has its own best pressure for creating the largest erosion rate. Therefore, the maximum erosion of the nozzle at Mach 2 is 7.92 × 10^{−6} kg/m^{2}·s when the pressure is 25 MPa. The biggest erosion rate of the numerical simulation case is 1.26 × 10^{−5} kg/m^{2}·s when the pressure is 25 MPa, and the nozzle type is Mach 3. Figure 5 shows the result of the nozzle at Mach 3 with various pressures, causing different erosion rates, owing to pressure changes.

**(a) 10 MPa**

**(b) 15 MPa**

**(c) 25 MPa**

**(d) 30 MPa**

**(e) 50 MPa**

Because the abrasive gas jet velocity depends on the gas jet flow field, we should clearly define how the pressure affects the gas jet flow field. When the gas exits the nozzle, the jet flow field depends on the ratio of static pressure between the gas jet and atmosphere. When the inlet pressure is 10 MPa, the outlet static pressure is 0.28 MPa. Thus, the gas does not completely expand. The gas expands continuously after flowing out of the nozzle, squeezing the boundary air. This leads to the formation of an expansion wave, causing the gas jet to expand in the radial direction and increase the potential jet core. Moreover, the gas velocity in the axial direction further accelerates. Meanwhile, the static pressure of the gas jet gradually decreases with the expansion of the gas jet. The gas jet ceases to expand when static pressure is less than the atmosphere, and the gas jet velocity reaches the maximum. The expansion wave continually reflects the boundary of jet and overlays, leading to the formation of compression waves. The gas ceases to expand in a radial direction and begins to compress in the axial direction, shrinking the boundary of the potential core and decreasing the gas velocity. However, the density and static pressure of the gas jet increase with the formation and propagation of the compression wave. When the static pressure increases to 0.19 MPa, the gas jet has enough internal energy to expand. Then, the compression wave reflects the boundary and begins to expand again. By comparing the first expansion wave, the static pressure of the second expansion wave is smaller. The reflected angle of the expansion wave will be small, and the wavelength will be short. The expansion and compression waves propagate forward, alternatively in this fashion.

The larger the inlet pressure, the larger the outlet static pressure, leading to an increase of expansion waves and a decrease of compression waves. An extended expansion wave creates a higher gas velocity, favorable and essential to abrasive acceleration. However, when the pressure is 30 MPa, the shield effect is evident and obstructive to abrasive erosion. The shield effect is much more apparent when pressure increases. Additionally, when the pressure reaches 50 MPa, there is a Mach disk next to the nozzle exit. It is well-known that, when the ratio between static pressure and the atmosphere is large enough, the gas jet will overexpand, leading to a Mach disc. Whereas the gas velocity prior to the Mach disk is the largest, the gas velocity decreases significantly after the Mach disk is created. Then, the shield effect is the most obvious, causing the erosion rate to reduce dramatically. Compared to other flow fields, when inlet pressure is 25 MPa, the flow field has the most extended expansion wave and the most subtle shield effect. The most extended expansion wave causes the abrasive to accelerate to the highest velocity. The most subtle shield effect causes the impact energy of abrasive to transfer most efficiently into the breakage energy of rock. These are the two primary causes giving sufficient explanation to the best erosion rate of 25 MPa.

#### 4. Refining Nozzle Structure

Abrasive acceleration depends not only on the gas flow field of a free jet but also on the flow field of the nozzle. The best flow field of a free jet should feature high velocity and an unobvious shield effect, entirely depending on the ratio of expansion ratio and inlet pressure. Refining internal nozzle structures (e.g., convergent angle, divergent angle, contraction ratio, and draw ratio) is merely related to the flow field of the nozzle. Like Section 3, we do not focus on how detailed the nozzle structure affects the flow field. We instead judge it from the erosion rate.

##### 4.1. Effect of Convergent Angle on Erosion Rate

The convergent angle decides the range of convergent section when the diameters of entrance and throat are being constant. While gas flows through the converging section, it will be first compressed and then released reaching a speed of sound. The high-speed gas jet then acts on abrasive hence abrasive acceleration. However, in order to achieve an excellent abrasive acceleration, convergent angle needs to be optimized. Specifically, a too large convergent angle results in a shorter convergent section with a nonuniform and unsteady gas jet, weakening the abrasion. Yet a too small convergent angle not only negatively affects abrasive acceleration but also brings difficulties in nozzle manufacturing. According to aerodynamics experience, the convergent angle is suggested to range between 14° and 60°. To further identify how the convergent angle affects the erosion rate, the erosion processes on rock are simulated with eight divergent angles in the following ranges: 14°, 28°, 36°, 45°, 51°, 53°, 55°, and 60°. The other influential parameters are fixed in the simulation. The results are presented in Figure 6 and Table 2. It is shown that divergent angle has a dramatical influence over the erosion rate. With an increasingly divergent angle, the erosion rate increases and then decreases. The maximum erosion rate is 1.27 × 10^{−5} kg/m^{2}·s when the divergent angle is 53°. When the convergent angle is less than 45°, the erosion rate of the target center is extremely small. The smaller the convergent angle is, the lower the erosion rate will be. By leveraging Figure 5, the smaller convergent angle leads to a more obvious shield effect, which is disadvantaged by the erosion rate. Higher convergent angles cause the gas jets to be difficult to accelerate and to become unstable in the flow field, leading to a decreased erosion rate.

##### 4.2. Effect of Contraction Ratio on Erosion Rate

Contraction ratio refers to the ratio of the nozzle inlet radius to the throat radius. When the contraction ratio is less than 3, the flow field of a gas jet of will be continuous and unseparated. The contraction ratio is designed to be within 1.5, 2, 2.5, 3, 3.5, and 4, whereas other structure parameters remain unchanged, except where at convergent of 53°. The erosion rate of rock at different contraction rates of Laval nozzle was calculated using the same numerical simulation method. The results are shown in Table 3 and Figure 7. Similar to Figure 6, when the contraction ratio equals 2, the shield effect is the most unobvious and is the primary cause of the maximum erosion rate. When the contraction ratio is less than 2.0 or too large, the shield effect decreases the impact energy of incident gas jets, making the wall jet too distant from the target center and inducing a decrease of erosion rate. A high erosion rate will cause a deeper erosion pit of rock, and a low erosion rate will cause the erosion pit of rock to be broader.

##### 4.3. Effects of Divergent Angles on Erosion Rate

The divergent angle is a primary factor influencing expansion state and speed of a gas jet. Thus, it is critical to abrasive acceleration and rock erosion. When the divergent angle is between 5° and 30°, the flow field of the gas jet improves. Based on the effect of convergent angle and contraction ratio on erosion rate, the structure of the Laval nozzle is refined further by adjusting the divergent angle among 5°, 7°, 10°, 12°, 15°, and 30°. The parameters of the Laval nozzle are listed in Table 4. The results of the numerical simulation are shown in Table 5 and Figure 8. The best erosion rate is 1.53 × 10^{−7} kg/m^{2}·s. When the divergent angle is 10°, the erosion rate reaches maximum. The shield effect is subtle when the divergent angle resets between 5° and 15°. If the divergent angle is too large (e.g., 30°), the shield effect is apparent and disadvantageous to rock erosion.

##### 4.4. Effect of the Aspect Ratio of the Throat on Erosion Rate

The aspect ratio of the Laval nozzle refers to the ratio between throat length and diameter. For the gas phase, the velocity reaches the speed of sound and remains unchanged at the throat section. The length of the throat is not related to gas velocity. For solid phase, the length of the throat is significant to abrasive acceleration, because it determines the acceleration time of the abrasive. Thus, the erosion rate can improve when the aspect ratio of the throat is adjusted. To investigate the effect of the aspect ratio on erosion rate, we calculate the rate of rock erosion when the aspect ratio is 0, 2, 3, 4, 5, and 7. Meanwhile, the convergent angle is 53°, the contraction ratio is 2, and the divergent angle is 10°. Results are shown in Table 6 and Figure 9. With the increasing aspect ratio of the nozzle throat, the erosion rate increases and then decreases. When the aspect ratio is 0, the length of the throat is 0, and the erosion rate is minimized. The existence of a throat is vital to abrasive acceleration and erosion rate. The erosion rate reaches its maximum, 153 × 10^{−7} kg/m^{2}·s, when the aspect ratio is 3 and the length is 6 mm.

##### 4.5. Optimal Nozzle Structure

From Section 3, we see that nozzle Mach 3 creates a comparatively maximum erosion rate. Nozzle structure is further refined by analyzing the effects of different convergent angles, contraction ratios, divergent angles, and aspect ratios on erosion rate. The single variable method is used to optimize the structural parameters and to get the optimal nozzle for rock breakage. The optimal nozzle structure parameters are at a convergent angle of 53°, a contraction ratio of 2, a divergent angle of 10°, and an aspect ratio of 3.

#### 5. The Rock Erosion Experiment

To verify whether the nozzle structure is optimal, a rock erosion experiment was induced by comparing the erosion rate of relatively good nozzles, designed based on the optimal nozzle, as shown in Figure 10. Figure 10(a) shows the optimal nozzle. Based on the effect of the convergent angle on the erosion rate, the second best convergent angle is 60°. We change the convergent angle to 60° and keep the other nozzle parameters unchanged, marked as nozzle b in Figure 10(b). Using the same method, we can associate nozzle c with the transition of a divergent angle (10°) to divergent angle (7°), as shown in Figure 10(c). We can also obtain nozzle d associated with the transition of aspect ratio 3 to aspect ratio 5, as shown in Figure 10(d). Like the numerical simulation, the abrasive is garnet with mesh 80, the inlet pressure is 25 MPa, the stand-off distance is 100 mm, and the erosion time is 10 s.

**(a)**

**(b)**

**(c)**

**(d)**

##### 5.1. Experimental System

The high-pressure abrasive gas jet erosion experimental system is used for the experiment, which consists of high-pressure air compressor, high-pressure gas cylinder, digital pressure gauge, pressure control valve, abrasive tank, gate valve, and operation box. The high-pressure air compressor has a maximum pressure of 40 MPa and a maximum air intake of 2 m^{3}/min, while the high-pressure gas cylinder exhibits a maximum allowable pressure of 40 MPa. The system devices are connected as shown in Figures 11 and 12. The nozzle used is a Laval nozzle, whose structural parameters are the same as the nozzle used in the numerical simulation. Before the experiment, high-pressure gas is stored in the high-pressure gas cylinder, and the outlet pressure is adjusted with the pressure-regulating valve. The inlet pressure ranges between 0 and 40 MPa, whereas the outlet pressure ranges between 0 and 25 MPa. With an adjustable outlet pressure accuracy of 0.1 MPa, the pressure regulating valve can accurately control the jet pressure, thereby ensuring a constant jet pressure during the experiment to meet the experimental requirements. To precisely control the mass flow rate of abrasives, a high-pressure gate valve is installed below the abrasive tank. The gate is suitable for controlling the flow of solid particles under high-pressure conditions. Before the experiment, the gate valve scales corresponding to the mass flow of different abrasives are determined by calibration.

Limestone is used for erosion. To ensure that the mechanical and physical properties of the eroded limestone are identical, 50 × 100 rock samples are prepared by coring on the same rock mass. Two rock samples are selected and tested for mechanical properties using MTS, and the results are presented in Table 7. Before performing the erosion experiment, the gas pressure in the gas tank is increased to over 35 MPa, the abrasive tank is filled with the corresponding abrasive, and the gate valve position is adjusted to ensure that the mass flow meets the requirements of experimental conditions. To improve the accuracy of the experimental result, we did a parallel experiment for every nozzle. We used every nozzle to erode three rock samples at the same experimental condition. The detailed experiment procedure is shown in Table 8.

##### 5.2. Experiment Result

Erosion volume and erosion depth were the two primary parameters that reflected the erosion effect of the abrasive gas jet equal to the erosion rate. The results of erosion volume are shown in Table 9. Nozzle a creates the maximum erosion rate of 14.89 mL, which is in good agreement with the numerical simulation. Nozzle c creates minimum erosion rate of 9.38 mL, where the divergent angle most dramatically affects the erosion rate. We obtain the same conclusion with the experimental results of erosion depth. Nozzle a makes a maximum erosion depth of 47.29 mm, as shown in Table 10. Nozzle c makes a minimum depth of 40.13 mm. The erosion pit of nozzle c is also featured with a minimum mouth diameter, as shown in Figure 13. The diameter of the mouth of the pit eroded by nozzle a is the second minimum and is slightly bigger than nozzle c. The conclusion of Section 3.3 tells that the diameter of the mouth is small if the shield effect is subtle. The difference of erosion volume and the depth between nozzles a and c is mainly caused by abrasive acceleration. Thus, the change of divergent angle causes the velocity of gas jet to decrease. This agrees well with the conclusion of Section 4.3. The main reason for the decrease of erosion volume and depth with nozzles b and d is the shield effect. The changes of convergent angle and aspect ratio cause the velocity of the gas jet to increase and the shield effect to enhance, which is unfavorable to abrasive acceleration and rock erosion. These conclusions agree well with Sections 4.1 and 4.4. Thus, nozzle a is optimal, because it can induce a better flow field and less unobvious shield effects.

**(a) Nozzle a**

**(b) Nozzle b**

**(c) Nozzle c**

**(d) Nozzle d**

##### 5.3. Further Experiment Validation

Is the nozzle still the optimal nozzle after changing the experimental conditions? That is, whether nozzle a can still reach the maximum erosion rate when the type of abrasive and gas pressure is changed. To clarify the problem, different abrasives and gas pressure were used for erosion experiments. (1)Abrasive Type. At present, the commonly used abrasives include quartz sand, garnet, brown corundum, and silicon carbide. Each nozzle uses four abrasives for rock erosion. By comparing the erosion parameters, this paper analyzes whether the variety of abrasives can influence the conclusion. The experimental pressure was 25 MPa, the target distance was 100 mm, the erosion time was 10s, and the number of abrasives was 80 mesh. The experimental results are shown in Table 11. It can be seen that no matter which abrasive is used, nozzle a has the maximum erosion depth. Therefore, the optimal structure of nozzle a can be further determined.(2)Gas Pressure. Gas pressure is one of the key factors to determine the erosion effect. Because the pressure of the air compressor applied in engineering is not very high, the gas pressure of the experiment is 10 MPa, 15 MPa, 20 MPa, and 25 MPa. Four kinds of pressure were used to test the erosion of each nozzle. By comparing the erosion parameters, it is analyzed whether the change of gas pressure can affect the conclusion. The experimental abrasive was 80 mesh garnet, the target distance was 100 mm, and the erosion time was 10 s. The experimental results are shown in Table 12. It can be seen that gas pressure can affect the erosion depth, and the influence gradually decreases with the increase of gas pressure. However, under each experimental condition, nozzle a has the maximum erosion depth. Combined with the experimental results of different abrasive erosion, it can be concluded that nozzle a is the optimal structure.

#### 6. Conclusion

Because nozzle structures are essential to erosion rates, it is necessary and vital to design an optimal nozzle to support a highly abrasive gas jet for rock breakage in coal-bed methane exploration. By combining aerodynamics and fixing the nozzle conditions, four types of nozzles were designed. The erosion rates of the nozzles were calculated using numerical simulation, showing that the Mach 3 nozzle was better with an inlet pressure of 25 MPa, and the best abrasive was garnet at 80 mesh. The optimal nozzle structure was featured with more extended expansion waves and more subtle shield effects.

To further optimize the nozzle structure, the erosion rates at various conditions were calculated using the single variable method. Thus, convergent angle, contraction ratio, divergent angle, and aspect ratio were changed at every turn to obtain the erosion rate. The optimal nozzle structure was obtained by comparing the erosion rate of different nozzle structures. Thus, the entrance diameter was 4 mm, the convergent angle was 53°, the contraction ratio was 2, the divergent angle was 10°, the aspect ratio was 3, and the exit diameter was 4.1 mm. The results of the rock erosion experiment show that it is in good agreement with the numerical simulation. The optimal nozzle can erode the maximum volume and depth.

#### Data Availability

The data of the paper refers to numerical simulation and experiment. Their calculation method and results are listed in the paper. That is, the data used to support the findings of this study are included within the article.

#### Conflicts of Interest

The authors declare that they have no conflicts of interest.

#### Acknowledgments

The authors disclosed receipt of the following financial support for the research, authorship, and/or publication of this article: this paper was jointly funded by the National Key Research and Development Program of China (2017YFC0804207), the National Science Foundation of China, (51704096, 51574112, and 51604092), Program for Innovative Research Team in University (IRT_16R22), the Science Research Funds for the Universities of Henan Province (J2018-4), and Scientific Research Foundation of State Key Laboratory Cultivation Base for Gas Geology and Gas Control (WS2017A02).