The hydraulic characteristics of the lock chamber section in a bottom outlet are complex. Particularly, cavitation is a prominent problem when the flow in the tunnel transitions from pressurized to unpressurized conditions. As a countermeasure, sidewall contractions are often installed at the end of the pressurized section. In this paper, with numerical simulations and vacuum tank experiments, we analyzed the design parameters of several prototype projects and studied the flow properties and cavitation characteristics of the transition section. The four main factors that influence cavitation risks are the contraction ratio of the transition section, the top press slope, the length of the transition section, and the shape of the orifice. The study of a real-world project demonstrates that by implementing a severe constriction degree, the top press slope can be slowed down, and the pressurized transition section can be extended, thereby reducing cavitation risks and improving flow patterns. These research results provide a reference for the optimal design of hydraulic structures.

  • This paper analyses four factors that affect the cavitation of the bottom discharge tunnel.

  • This paper collects the design parameters of 23 lock chambers and summarizes the value range and design law of these design parameters.

  • The cavitation and flow pattern of the LW hydropower station are verified through the vacuum tank experiment and numerical simulation.

Bottom discharge tunnels are often used in reservoir flood discharge, and the operating water level of such flood discharge tunnels varies greatly. In the lock chamber of the discharge tunnel, the flow state converted pressurized flow to unpressurized flow. There are some complex hydraulic problems such as strong water wings and cavitation erosion caused by this change of flow. Figure 1 shows the layout of the discharge tunnel of the Jinping dam, the location of its lock chamber, and the cavitation damage occurring in the Zipingpu dam.
Figure 1

Discharge tunnel of the Jinping hydropower station (China) (a) and cavitation damage zones on the side walls in Zipinpu dam's tunnel (Li et al. 2016) (b).

Figure 1

Discharge tunnel of the Jinping hydropower station (China) (a) and cavitation damage zones on the side walls in Zipinpu dam's tunnel (Li et al. 2016) (b).

Close modal

Some literature studied the cavitation and flow characteristics of outlets using numerical simulations and model experiments. Aminoroayaie Yamini et al. (2021) used Flow-3D to study the hydrodynamic performance and cavitation of the bottom outlet at Sardab Dam. They analyzed flow patterns at the different gate openings and the working status of the branch. Kyriakopoulos et al. (2022) used numerical simulation and model experiments to study the flow pattern and vorticity of different distances between the butterfly valves. Through 3D flow simulation, Sadat Helbar et al. (2021) investigated the effect of the area, number and shape of the bottom outlet gates on the velocity, concentration, and volume of the removed sediments and the dimensions of the flushing cone. Through three-dimensional numerical simulation, Nikseresht et al. (2012) studied pressure, and cavitation index under different conditions of the gate openings and water levels of the reservoir. Dargahi (2010) used numerical simulation and model experiments to study the flow characteristics of Aswan Dam bottom outlet gates under different operating modes. Li et al. (2016) observed that the degree of gate opening has a great effect on the pressure and flow cavitation index of side walls. The lateral expansion and partial gate opening increased the risk of cavitation erosion on side walls downstream. Based on the results of numerical simulations, Jamali Rovesht & Manafpour (2019) observed that cavitation indices are lower than the critical amount (0.2) on the tunnel bottom for 10–80% of service gate openings.

There some literature conducted model tests under normal atmospheric pressure to study the flow pattern of the spillway tunnel and prevent cavitation risk. In order to ensure the safe operation of the gate under high water levels, the arc-shaped working gate was usually used, and the sudden expansion and sudden fall structure type was set at the end of the lock chamber to increase the aeration of the downstream channel (Feng et al. 2001). Abdolahpour & Roshan (2014) carried out model tests at normal atmospheric pressure and studied a bottom outlet for high-velocity discharges past from the control gate. According to the measured pressure and velocity data, they calculated the distribution of cavitation numbers along the bottom and between the two gates. Mohaghegh & Wu (2010) studied various geometry parameters for the discharge tunnel in the atmospheric model and discriminate different flow regimes under different conditions. Mohaghegh & Wu (2009) studied the influence of different angles of top press slope on the downstream cavity length. They observed that steep top press slope results in shorter bottom cavity length downstream in big discharges. In addition, for the flow with high Fr number (Fr > 3.4), the length of the bottom cavity increases monotonously with the increase in the step height. Zhou et al. (2018) proposed an expression for calculating the geometrical morphology and the length of bottom and lateral cavities. Based on experimental results, Li et al. (2021) developed an improved model for calculating airflows in the cavity downstream of a bottom offset. Wang et al. (2019) studied the influence of the relative step height and working gate opening on pressure distribution. Wenhai et al. (2007) combined with the right bank flood relief tunnel of the Jiudian Gorge water conservancy pivot project to carry out experimental research on the sudden expansion and sudden fall section of the flood relief tunnel, the top press slope of the lock chamber is 1:6 and the area contraction ratio is 0.88. Jamali et al. (2023) studied the pressure and cavitation number in the transition zone of the discharge tunnel with different Fr number. The change of expansion angles in the transition zone will bring great changes to the pressure and cavitation number in the transition zone The pressure and cavitation number in the transition zone were obtained by atmospheric pressure experiment and numerical simulation.

Another important way was to conduct a model test in the vacuum tank to reduce environmental pressure and used the hydrophone to monitor the sound generated by cavitation bubble collapse to judge the cavitation risk of the discharge tunnel. Wang et al. (2022) used the vacuum tank to observe the cavity length and entrained air of chute aerators under various atmospheric pressures. Liu et al. (2020) used the vacuum tank to reduce the ambient pressure environment to observe the atomized rain of a high-velocity waterjet.

Some literature works have made prototype observations on actual engineering projects. Zhenlian et al. (2006) carried out the prototype observation of the gas doping facility of the sudden expansion and sudden fall step of the lock chamber in the bottom tunnel.

To assess cavitation occurrence at the dam outlet, three primary methods are commonly employed: evaluating the critical cavitation number based on experience, conducting vacuum tank tests, and prototype observations. But the prototype observations tend to be costly, the vacuum tank experiment offers an efficient approach for studying cavitation risks.

There are many papers that studied bottom outlet structures. Apart from these studies, to the best of our knowledge, there is little research on the cavitation characteristic of the different top press slopes of the tunnel when drastic reduction in the outlet flow area.

How to design the shape of the transition section to achieve better cavitation characteristics under severe flow area contractions? This issue is not clear. Therefore, we studied the impact of different top press slopes on the cavitation characteristics of water flows under severe flow area contraction.

Although many papers have used numerical simulation and model experiments to study the cavitation and flow characteristics at the outlet of dams, relatively little literature combines numerical simulation and vacuum tank to study cavitation characteristics of the outlet of a dam. The vacuum tank experiment can effectively determine whether the structure occurs cavitation, but it is difficult to measure flow field data in the vacuum tank model experiment. Therefore, we used numerical simulation to obtain flow field data and calculate the water flow cavitation number. In this paper, we combine numerical simulation and a vacuum tank to study the cavitation characteristics of the transition section.

In order to understand the effects of different transition sections on the characteristics of cavitation, we first collected the design parameters of multiple projects. Also, then based on the experience of these projects we have provided suggestions for contraction ratio η, orifice shape h/B, the top press slope i, and the transition section length L. (in section 3.1). Then we proposed the following hypothesis: ‘extending the length of the transition section may make the cavitation characteristics better, under severe flow area contraction’. According to this hypothesis, we carried out a numerical simulation to obtain pressure and velocity field (in Section 3.2), and then implemented a vacuum tank experiment of different transition sections to verify (in Section 3.3). With significant contraction in the flow section, extending the length of the transition section appropriately will achieve better cavitation performance.

This paper takes the bottom outlet of the LW dam (LaWa dam in China) chamber as the research object, as the high-speed flow in the bottom outlet is prone to cavitational damages in the chamber section. So, it is necessary to optimize the shape of the transition section of the lock chamber, as shown in Figure 2. We used numerical simulation methods to obtain data on the flow field and used the vacuum tank model experiment to verify whether the optimized body shape will cause cavitation, and calculated the initial cavitation number of the body shape.
Figure 2

Model diagram (a); design parameters of the transition section (b); and schematic diagram for top press slope i of the transition section and water wing at the open channel (c).

Figure 2

Model diagram (a); design parameters of the transition section (b); and schematic diagram for top press slope i of the transition section and water wing at the open channel (c).

Close modal

As shown in Figure 2, there are some key design parameters of the lock chamber. These parameters would affect the flow characteristics and cavitation prevention. They are tunnel diameter D, transition section L, the top press slope of the tunnel, contraction ratio , orifice height h, orifice width B. In this paper, the ratio of orifice height h and width B is used to express the change in the orifice shape. When = 1, the orifice is a square orifice; when h/B < 1, the orifice is wide-flat orifice; when >1, the orifice is narrow-high orifice. The main influencing factors of the hydraulic and cavitation characteristics of the lock chamber include the transition section length L, contraction ratio , and top press slope i. In this paper, , , , , , , , . Where D = 12 m is the diameter of the discharge tunnel. is the inlet area of the section and is the outlet area of the section, then η is the contraction ratio of the lock chamber outlet orifice. is the flow velocity at the orifice, h is the height of the orifice, L is the length of the transition section, Δb is the width of lateral expansion, Llateral is the length of the lateral cavity, and θ is the angle of incidence after lateral diffusion of flow.

We think that the top press slope, the length of the transition section, the contraction ratio, and the orifice shape h/B, will have an obvious impact on the cavitation characteristics of the transition section. The reasons for our selection of these four parameters are as follows.

For the top press slope, a slower slope will bring a longer transition section, which is conducive to water flow adjustment, but the protection ability of the pipeline top will be weakened. For the contraction ratio, a more severe contraction ratio can also cause drastic changes in the flow pattern. When it is used together with the lateral aeration facilities, after the flow out of the orifice, the pressure on the side walls of the open channel may undergo adverse drastic changes due to the rapid diffusion of the flow toward the sides wall. For the orifice shape , when >1, the flow is compressed into a thin and tail shape, and the pressure distribution at the top may be bad at the outlet. When <1, the flow is compressed into a flat shape, and when used in conjunction with the lateral aeration facilities, the flow may have a stronger impact on the side wall after being out from the orifice.

The LW dam is an earth dam with a crest elevation of a bottom outlet is 2,617.5 m (m.a.s.l.), a design water level is 2,702 m (m.a.s.l.) and a dam height of 239 m. The flow rate at the design water level is 2,530 m3/s, and the velocity of the lock chamber outlet is 32.8 m/s. Therefore, the Reynolds number is calculated by orifice width B, , and the Froude number = 3.7. The original design of the transition section parameters is shown in Table 1.

Table 1

Original design of the transition section parameters

Tunnel diameter D (m)Orifice width B (m)Orifice height h (m)Top press slope (i)Transition section length (L/D)Contraction ratio (η)Orifice shape (h/B)
12 10 7.7 1:6 2.87 0.681 0.77 
Tunnel diameter D (m)Orifice width B (m)Orifice height h (m)Top press slope (i)Transition section length (L/D)Contraction ratio (η)Orifice shape (h/B)
12 10 7.7 1:6 2.87 0.681 0.77 

Numerical simulation method

Numerical simulation using Flow-3D to calculate various cases with a grid size of and the total mesh cell counts was 7.8 million, as shown in Figure 2(a) and 2(b). The numerical simulation size adopts the LW dam prototype size, with a tunnel diameter of . The inlet used the pressure inlet and set up the fluid elevation as 5.8D. The outlet was set to free outflow, the vent was set to pressure outlet, 0 Pa, and the other region was set to the wall. The following equations are used to control the fluid motion. The continuity equation. ; The momentum equation:, where = 1,000 m3/s, the water density. Turbulent model is used standard k-ε model. k Equation: ; the turbulent dissipation rate ε is given by the equation:, turbulent viscosity coefficient, , and are constants. We used Volume-Of-Fluid (VOF) method to deal with a free surface. Fractional area-volume obstacle representation (FAVOR): to simulate the rigid surfaces and some components, such as geometric boundaries. The VOF method was utilized to deal with water air interface. The flow mode is an incompressible fluid.

The 3D geometry of the bottom outlet was drawn in actual size by Creo software. The post processing using Tecplot and FlowSight. The format of the geometry file is ‘.stl’. The boundary conditions of the numerical model are provided in Table 2. The fluid was considered an incompressible and single phase. The inlet head was equal to the reservoir water head. The inlet boundary conditions were set to a specified pressure (P). The outflow (O) and walls (W) were introduced to the model, respectively (see Figure 3). For a solid wall, the surface roughness is 0.25 mm. The simulations only have a mesh block. We save the calculation results every 0.1 s.
Table 2

Boundary conditions and parameter settings in the numerical model

ItemDefinition
Model input Specified pressure, fluid elevation H = 70.06 m (P, color red) 
Lateral air vent Specified pressure, 0 Pa (P, color green) 
Model output Outflow (O, color red) 
Walls Wall, no-slip (W, color blue) 
Total number of computational mesh 7,884,066 
ItemDefinition
Model input Specified pressure, fluid elevation H = 70.06 m (P, color red) 
Lateral air vent Specified pressure, 0 Pa (P, color green) 
Model output Outflow (O, color red) 
Walls Wall, no-slip (W, color blue) 
Total number of computational mesh 7,884,066 

The mesh block size is: Xmin = −60 m, Xmax = 105 m, Ymin = −7 m, Ymax = 7 m, Zmin = −18 m, Zmax = 7 m.

Figure 3

Domain and boundary conditions in the Flow-3D numerical model (a); Flow-3D-generated orthogonal mesh associated with STL (b); and fluid domain mesh profile of lock chamber S (c).

Figure 3

Domain and boundary conditions in the Flow-3D numerical model (a); Flow-3D-generated orthogonal mesh associated with STL (b); and fluid domain mesh profile of lock chamber S (c).

Close modal

The velocity and pressure fluctuations of high-speed water flow are significant. In order to obtain statistically significant results, we used the time average method to extract pressure and velocity data, which time average within 5 s. We pay more attention to the cavitation number in the near wall region, so we extract data at a distance of 0.2 m from the wall.

Numerical model validation

The accuracy of the numerical model is verified below. As shown in Figure 4, so the flow patterns of the experimental and numerical simulations are similar. Also, some hydraulic characteristics are compared. After model scale conversion, the height of the water surface line of the measuring point in the experiment is 10.15 m, and the side cavity length is 6.35 m; the values obtained from the numerical simulation are 10.53 and 6.54 m, respectively, corresponding to an error of 3.7 and 3.0%, respectively. The errors of the three values of side cavity length, water surface line height and pick distance are not more than 5%, so the accuracy of numerical simulation can meet the engineering requirements. After the comparison, verification of the previous mathematical model and test results are calculated. The model and boundary condition settings used in this simulation are feasible.
Figure 4

Comparison of flow patterns between vacuum tank experiment and numerical simulation (a, b) and water wing profile of numerical simulation and experiment results (c).

Figure 4

Comparison of flow patterns between vacuum tank experiment and numerical simulation (a, b) and water wing profile of numerical simulation and experiment results (c).

Close modal

Experiment method

In high-altitude areas, the decrease in air density can reduce the ambient pressure. To assess the low ambient pressure effect, it is helpful to conduct a relevant experiment in an artificial low-pressure environment. The vacuum tank has been applied to mechanism research and practical applications in many fields. The experiment was conducted on a lock chamber model test and low ambient pressure at the State Key Laboratory of Hydraulics and Mountain River Engineering of Sichuan University.

As shown in Figure 5(a) and 5(b), the experiment is guaranteed to satisfy the gravity similarity criterion and the cavitation similarity criterion.
Figure 5

Test model diagram (a); experiment site (b); hydrophone arrangement and model coordinate axis (c); and vacuum tank experiment (d).

Figure 5

Test model diagram (a); experiment site (b); hydrophone arrangement and model coordinate axis (c); and vacuum tank experiment (d).

Close modal

The modeled using a model scale 35, the velocity scale is , and the volume of flow scale is . Therefore, the pipeline diameter of the experiment model is . The flow rate of the engineering prototype is 2,530 m/s, so the maximum discharge of model is = 349 L/s:

The cavitation number in the vacuum tank is
(1)
is the relative pressure, is the local atmospheric pressure; is the local vaporization pressure, g = 9.81 m/s2 is gravitational acceleration, u is velocity. The smaller the cavitation number is, the easier it is to occur cavitation. For the vacuum tank experiment, it used an air extraction pump to reduce the ambient air pressure in the tank.

The cavitation number of the actual engineering project is , the cavitation number of vacuum tank model is .

In order to achieve the cavitation number similarity criterion, we reduced the ambient air pressure in the tank, the cavitation number of the actual engineering project is equal to the cavitation number of model, i.e., .

When , according to (1), we can get
(2)
that is
(3)
According to the gravity similarity criterion,
(4)
Simultaneous formulas (3) and (4), now we can get the ambient pressure in the vacuum tank:
(5)
where is the ambient pressure in the prototype, is the altitude for the actual project. is the vapor pressure of prototype water flow with 6°C water temperature. (1.71 kPa) is the vapor pressure of model water flow with 15°C water temperature. Finally, we can calculate the 0.38 m (3.73 kPa).

All experiment data are obtained under the 0.38 m ambient pressure inside the vacuum tank. In addition, we would gradually adjust the ambient pressure inside the vacuum tank to obtain the incipient cavitation number of the body type.

In this paper, if cavitation occurred under ambient pressure in the vacuum tank, we call that cavitation number of flow the incipient cavitation number . The relative pressure P and velocity u obtained by numerical simulation were used to calculate the cavitation number :
(6)
(7)
We used hydrophones (produced by Brüel & Kjær) to monitor whether the flow near the lock chamber produces cavitation bubble collapse during the experiment, as shown in Figure 5(c). If the cavitation bubble collapses, the hydrophone would hear a high frequency sound of large decibels. Two methods are used to determine whether cavitation occurs during the test. One method is based on whether the difference between the cavitation sound and the background sound maximum value is greater than the critical value. Another method is to monitor whether the ratio of sound energy to background sound energy is greater than the critical value. The sound is calculated by the average value of 10 times, and the analyzed frequency is 30–100 kHz, which is the frequency range of cavitation bubble collapse. The sound difference maximum is , the relative sound energy ratio
(8)
As shown in Figure 6, under normal atmospheric pressure, the sound is the background sound . Reduce the ambient air pressure in the vacuum tank to the cavitation similarity criterion atmospheric pressure 0.38 m for the prototype project. If cavitation occurs at this pressure, the cavitation sound is . Also, E is the cavitation sound energy, is the background sound energy. According to the sound difference and relative sound energy ratio , four types of cavitation intensities are shown in Table 3.
Table 3

Criteria for discriminating cavitation

Cavitation typeNo cavitationWeak cavitationSignificant cavitationIntense airing
Sound difference 0–5 dB 5–7 dB 7–10 dB 10 to +∞dB 
E/E0 relative energy ratio 0–2 2–4 4–6 >6 
Cavitation typeNo cavitationWeak cavitationSignificant cavitationIntense airing
Sound difference 0–5 dB 5–7 dB 7–10 dB 10 to +∞dB 
E/E0 relative energy ratio 0–2 2–4 4–6 >6 
Figure 6

Cavitation noise monitoring diagram.

Figure 6

Cavitation noise monitoring diagram.

Close modal

Lock chamber transition section and orifice shape

We used numerical simulation to calculate the operating conditions of free outlet flow in the pipeline and observed the pressure distribution at the top of the pipeline. As shown in Figure 7(a) and 7(b), the interior of the tunnel (0–100 m), the pressure P to x derivative, then . In the outlet section of the tunnel (100–120 m), the mainstream downward deviation, the upper part of the pipe flow velocity decreases, so the pressure increases gradually, so . Because the pressure at the top of this section of the pipe gradually increases to zero, the pressure at the top of this section of the pipe (60–120 m) must be negative. In order to eliminate or mitigate the negative pressure at the top of the outlet section of the pressurized tunnel, the top press slope is used at the outlet of the tunnel to increase the pressure at the top of the tunnel. As shown in Figure 7(c) , the transition section of the discharge tunnel often adopts the contraction on three sides, i.e., contraction on both sides and top press slope on the top plate, which makes the overflow area decrease along the pipe and achieves the purpose of eliminating negative pressure. In Figure 7(c), after adopting the form of three-sided contraction, the pressure inside the pipe is greater than 0 Pa.
Figure 7

Pressure of the top of the free outflow of the pressurized pipe (a, b) and relative pressure distribution of the transition section (c).

Figure 7

Pressure of the top of the free outflow of the pressurized pipe (a, b) and relative pressure distribution of the transition section (c).

Close modal

In addition, the shape of the orifice also has an effect on the pressure distribution at the top of the tunnel. The study shows that when , the pressure distribution and cavitation number of a wide-flat orifice (h/B< 1) is better than other orifice shapes; when , with low water level working conditions, narrow- tall orifice shape (h/B> 1) performance is better, and the square orifice (h/B= 1) is suitable for use in applications with large variations in water level (Zeyu 1982, 1988).

According to the above description, the lock chamber should be designed with appropriate contracting ratio η, top press slope i, transition section length and orifice shape h/B to prevent negative pressure at the top of the transition section, negative pressure zone and water wing near the downstream side wall. As shown in Figure 8, the relationship between the four factors is to be considered comprehensively to select a reasonable design.
Figure 8

Influence of four design parameters on hydraulic characteristics.

Figure 8

Influence of four design parameters on hydraulic characteristics.

Close modal
In order to compare the selection of the design parameters of the lock chamber of previous projects, this paper analyzed the parameters of the transition section and orifice shape of the completed discharge tunnel and summarizes the design laws. Various engineering data are provided in Supplementary material, Appendix, Table A1. Supplementary material, Table A1 listed the design parameters of 23 projects for the transition section, the hydraulic properties of the lock chamber are influenced by four geometric parameters: contraction ratio η, the top press slope, the length of the transition section L/D, and orifice shape h/B. The geometric parameters of each project are plotted in Figure 9. In Figure 9(a) and 9(d), for the orifice shapes, more projects use wide-flat orifices and square orifices with h/B ranging from 0.8 to 1.0, and few projects with h/B > 1.2, because these projects use narrow, tall orifices in combination with their layout considerations. The top press slope for most of the projects was between 1:6 and 1:10, the contraction ratio was mostly concentrated between 0.7 and 0.9, and the length of the transition section is mostly between 1.5 and 2.5. For the contraction ratio , they are more likely to adopt a steep top press slope i of about 1:6, because the contraction degree is small. This indicates that when the degree of contraction is small, the projects tend to use steeper top press slopes to prevent low pressure at the top of the tunnel.
Figure 9

Distribution of geometric design parameters (a, b, c) and histogram of the distribution for the four geometric parameters (d).

Figure 9

Distribution of geometric design parameters (a, b, c) and histogram of the distribution for the four geometric parameters (d).

Close modal

As shown in Figure 9(b), when the Froude number is greater than 2, the wide-flat orifice and square orifice is used in many projects, and the narrow-high orifice is used in a few projects. Figure 9(c) reflects the relationship between the top press slope and the length of the transition section. When the top press slope i is steep, the corresponding transition section is short; when the top press slope i is slow, the corresponding transition section length is large.

In Figure 9, some projects had been damaged before. Longyang Gorge (Baoqin & Taishan 2000) The orifice shape h/B = 1.4, and a top press slope is 1:6. It is a narrow-height type orifice shape, and high number of the orifice. The pressure distribution at the top section of the narrow-height orifice is undesirable at high numbers (Zhongyi & Xia 1986; Meilan 2009). Although no damage to the top of the tunnel of Longyang Gorge dam was seen, damage to the sidewall occurs, and the cavitation prevention performance at this location is weak. Liujiaxia hydropower station (Linsheng 1999) has h/B = 1.3 and an number of 7 and damage due to sediment had occurred.

According to Figure 9, the analysis can be summarized as follows: high water level discharge tunnel mostly uses wide-flat and square orifices, and the orifice ranges from 0.8 to 1.0. The contraction ratio η of the orifice can range from 0.7 to 0.9, the top press slope i can range from 1:6 to 1:10, and the length of transition section L/D in the range of 1.5–2.5D. These experiences can be referred to in the actual engineering design.

Numerical simulation of practical engineering

We would optimize the body design of the LW hydropower station according to the rules summarized above. This contraction ratio is relatively small compared with other projects η(0.7,0.9). Compared with other projects in Section 3.1, the contraction ratio of the LW hydropower station is small. The top press slope i is also steeper, resulting in a short length of the transition section and a drastic change of flow section in the transition section, which had a negative impact on the hydraulics characteristics. Referring to the design law obtained above, the press slope i of the LW hydropower station was changed from 1:6 to 1:8, thus being able to extend the length of the transition section with 2.87D and making the water flow more smoothly. Because of the arrangement of the LW hydropower station lock chamber, this optimization is only for the top press slope and the length of the transition section. The numerical simulation working condition parameters are shown in Table 4.

Table 4

Numerical simulation of different top press slope conditions

Top press slope ()Transition section length ()Orifice shape ()Contraction ratio ()
1:4 1.43 0.77 0.681 
1:6 2.15 
1:8 2.87 
1:10 3.58 
1:12 4.30 
Top press slope ()Transition section length ()Orifice shape ()Contraction ratio ()
1:4 1.43 0.77 0.681 
1:6 2.15 
1:8 2.87 
1:10 3.58 
1:12 4.30 
Table 5

Table of key parameters of two body types

Projectsi = 1:6 top press slopei = 1:8 top press slope
Transition section length, L/D 2.15 2.87 
Contraction ratio,  0.68 
Orifice height to width ratio,  0.77 
Projectsi = 1:6 top press slopei = 1:8 top press slope
Transition section length, L/D 2.15 2.87 
Contraction ratio,  0.68 
Orifice height to width ratio,  0.77 

To study the changes in hydraulic characteristics brought about by the optimization of body shape, this paper sets up five kinds of top press slope i for numerical simulation. The numerical simulation is used to make a comparison, as shown in Figure 10. The top press slope i change is 1:4 to 1:12, and the water level difference is set to with a corresponding discharge is 2,603 m3/s. In Figure 11, the top press and water cavitation number of the five slopes are shown, and the pressure and velocity data are time-averaged over 5 s and dimensionless processed as . For the transition section of the lock chamber, the concern is that the top press slope i is too slow leading to the appearance of negative pressure. In Figure 11, no negative pressure appears at the top of the tunnel whether it is a steep slope or a gentle slope, so it is safe to change the slope within a reasonable range. Therefore, the top of the tunnels is safe.
Figure 10

Numerical simulation pressure contour of five top press slope types in the LW hydropower station.

Figure 10

Numerical simulation pressure contour of five top press slope types in the LW hydropower station.

Close modal
Figure 11

LW hydropower station pressure variation corresponding to top press slope (a) and water cavitation number of transition section (b).

Figure 11

LW hydropower station pressure variation corresponding to top press slope (a) and water cavitation number of transition section (b).

Close modal
As shown in Figure 12(a), we extracted the average pressure and average velocity data from point A to point B at the central axis of the orifice height and 0.2 m away from the side wall, where point A is the point of the flow diffused and hit the side wall, and point B is the point of the pressure changes little. We studied the pressure change near the side wall. Figure 12(b) shows the pressure distribution of the sidewall. For the top press slope 1:4 and top press slope 1:6 generate the maximum pressure near the impact point of the sidewall and the pressure decreases along the way, with a secondary pressure rise in the middle. When the top press slope continues to slow down, no secondary pressure lift occurs, and the gradient of pressure reduction is gentler under the condition of a gentle top press slope. When the pressure changes slowly, the intensity of cavitation bubble formation and collapse will decrease. The secondary pressure rise will increase the risk of cavitation damage, and during the secondary pressure rise, cavitation bubbles have experienced two periods of generation and collapse.
Figure 12

Pressure extraction line of side wall at an open-channel section (a); pressure distribution of side wall with top press slope change for LW hydropower station (b); the cavitation number of the open-channel section, and incipient cavitation number of two body types (c).

Figure 12

Pressure extraction line of side wall at an open-channel section (a); pressure distribution of side wall with top press slope change for LW hydropower station (b); the cavitation number of the open-channel section, and incipient cavitation number of two body types (c).

Close modal

Figure 12(c) shows the flow cavitation number of open-channel sections under different top press slopes. Through the experiment in the vacuum tank, we detected cavitation in the open-channel section on the NO.4 hydrophone (Figure 5), so we calculated the incipient cavitation number of the two types. For a top press slope of 1:8, . The incipient cavitation number of the body shape of the top press slope 1:6, . As shown in Figure 12(c), the cavitation number of flows for each case is basically greater than 0.05. The cavitation number in the downstream part of the top press slope of 1:6 is smaller than the incipient cavitation number = 0.122. Therefore, there is a risk of weak cavitation. In contrast, for the top press slope = 1:8 body type, cavitation number K are greater than the incipient cavitation number Ki = 0.024. There is no risk of cavitation for the top press slope .

Figure 13(a) demonstrates that as the slope slows down, the transition section has a more pronounced effect in guiding the water flow to go downstream, so the length of the lateral cavity gradually increases. As mentioned above, the calculation of impact angle is . When was fixed, the longer , the smaller the angle . The impact pressure produced is not so dramatic, as shown in Figures 12(b) and 13(a). In Figure 13(b), the comparison of the mainstream water surface line and the surface line of the water wing, where the solid line is the mainstream water surface line and the dashed line is the surface line of the water wing. After the slope is slower than 1:8, the flow pattern is good and the water wing is small. When the slope is 1:6 and 1:4, there is more obvious water wing, among which the water wing height of slope 1:4 is the largest, about 1.5 m, which is an unfavorable flow pattern and may impact the hinge support of the lock gate.
Figure 13

Variation of lateral cavity length of LW hydropower station with the change of top press slope (a) and water wing height and water surface line (b).

Figure 13

Variation of lateral cavity length of LW hydropower station with the change of top press slope (a) and water wing height and water surface line (b).

Close modal

We finally optimize the original design top press slope 1:6 to top press slope 1:8, the length of the transition section is changed from 2.15D to 2.87D, other parameters keep the original design orifice height to width ratio h/B = 0.77, contraction ratio η = 0.68.

Vacuum tank experiment of practical engineering

Based on the analysis above, the two body types are now compared in a vacuum tank experiment. The vacuum experiment results are obtained for similar vacuum conditions. The specific design parameters are shown in Table 5.

Considering the actual operation demand of the discharge tunnel, there may be the operation mode of partial opening of the gate, so this vacuum tank experiment considers three modes of gate operation and three reservoir water levels that were high water level, medium water level, and low water level. In Figure 14, the vacuum tank experiment results are shown, we could see that the experiment results of the top press slope 1:8 body type are better than those of 1:6. Both top press slope 1:8 and top press slope 1:6 do not have cavitation at low water level at 100% gate opening, and weak cavitation may occur at high water level for top press slope 1:6. At 50% gate opening, the experiment result of top press slope 1:6 was obvious cavitation, and top press slope 1:8 was likely to have weak cavitation at high water level. At 25% gate opening, the test result of the top press slope 1:6 was strong cavitation, and the top press slope 1:8 was likely to have weak cavitation under high water levels.
Figure 14

Sound difference (a) and energy ratio (b) for the vacuum tank experiment.

Figure 14

Sound difference (a) and energy ratio (b) for the vacuum tank experiment.

Close modal
In Figure 15, the top press slope 1:8 body type did not appear bad flow pattern, we can see the various gate opening degree, and the water wing generated was small. It can ensure the safety of the curved gate strut support. The water wing of the top press slope 1:6 body type was obvious when the gate opening was 100%. From the results of this vacuum tank experiment can also see that the flow pattern was complex and cavitation risk was high when the gate was partially opened.
Figure 15

Water flow pattern of 1:8 top press slope (a) and 1:6 top press slope (b), the water wing is obvious for 1:6 top press slope, at H = 5.8D water level with three gate openings.

Figure 15

Water flow pattern of 1:8 top press slope (a) and 1:6 top press slope (b), the water wing is obvious for 1:6 top press slope, at H = 5.8D water level with three gate openings.

Close modal

Under the condition that the gate was fully open, according to the vacuum tank test results, it can be calculated that at the gate opening of 100%, the incipient cavitation number of the body shape of the top press slope 1:8 was = 0.024, the incipient cavitation number of body shape for top press slope 1:6 was = 0.122. In Figure 14, weak cavitation occurs downstream during high water level conditions when the top press slope was 1:6. Combined with the Figure 9 numerical simulation results, we can see that the cavitation number K of the open channel is smaller than the incipient cavitation number = 0.122. Therefore, the weak cavitation phenomenon occurs. Considering that the discharge tunnel has the need of gate partially opening in actual application because the top press slope 1:8 has better performance under different gate openings. Finally, top press slope 1:8 was selected as the optimized body type.

For the bottom discharge tunnel, the top press slope i, transition section L, orifice shape h/B, and contraction ratio η are important design parameters. The design should ensure that the low pressure at the top of the transition section is within a reasonable range, but also consider reducing the height of the water wing and the risk of cavitation of the side wall. This paper analyzes the flow and cavitation characteristics of the pressurized to unpressurized lock chamber through data statistics, numerical simulations, and vacuum tank experiment results to obtain the following conclusions.

  • (1)

    It is recommended that the contraction ratio of the lock chamber section is between 0.7 and 0.9; the top press slope i is 1:6–1:10, among which the top press slope of 1:8 is better for the downstream the water wing control. The orifice shape mostly uses the square orifice and the wide-flat orifice, and the orifice height to width ratio h/B is better around 0.8–1.0. The range of the transition section length L is between 1.5D–2.5D, and the body shape with a longer transition section L has better hydrodynamic characteristics.

  • (2)

    For practical engineering with the high number and the small contraction ratio η, we can use a longer transition section L/D, a slower top press slope i, and a wide-flat orifice shape. This design can effectively solve the water wing and cavitation problems for the bottom tunnel with a high Froude number.

  • (3)

    The water flow in the pressurized to unpressurized lock chamber is unusually complex, especially when the lateral sudden expansion facility is used in the lock chamber of the high-velocity flow discharge tunnel. In order to effectively control the hydraulics and cavitation problems in the chamber section. we need to comprehensively consider the relationship between the contraction ratio , orifice shape , the top press slope, and the transition section length L.

  • (4)

    For cavitation characteristics, the four factors top press slope i, transition section length L, contraction ratio , and orifice height to width ratio h/B are interdependent, and in specific engineering, selecting appropriate design parameters should comprehensively consider the mutual influence of these four factors.

This research was funded by the National Natural Science Foundation of China (No. 52130904).

All relevant data are included in the paper or its Supplementary Information.

The authors declare there is no conflict.

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Supplementary data