# Countercurrent Flow Limitation at the Junction between the Surge Line and the Pressurizer of a PWR

Authors: Taiga Doi; Takashi Futatsugi; Michio Murase; Kosuke Hayashi; Shigeo Hosokawa; Akio Tomiyama
Journal: Science and Technology of Nuclear Installations
 (2012)

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## Abstract

An experimental study on countercurrent flow limitation (CCFL) in vertical pipes is carried out. Effects of upper tank geometry and water levels in the upper and lower tanks on CCFL characteristics are investigated for air-water two-phase flows at room temperature and atmospheric pressure. The following conclusions are obtained: (1) CCFL characteristics for different pipe diameters are well correlated using the Kutateladze number if the tank geometry and the water levels are the same; (2) CCFL occurs at the junction between the pipe and the upper tank both for the rectangular and cylindrical tanks, and CCFL with the cylindrical tank occurs not only at the junction but also inside the pipe at high gas flow rates and small pipe diameters; (3) the flow rate of water entering into the vertical pipe at the junction to the rectangular upper tank is lower than that to the cylindrical tank because of the presence of low frequency first-mode sloshing in the rectangular tank; (4) increases in the water level in the upper tank and in the air volume in the lower tank increase water penetration into the pipe, and therefore, they mitigate the flow limitation.


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## Body

## 1. Introduction

During a PWR plant outage for maintenance and refueling, the reactor coolant is cooled by a residual heat removal (RHR) system. For a certain period, the reactor coolant level is kept around the primary loop center in order to carry out operations like aeration, attachment, or detachment of the steam generator (SG) nozzle dam. This operation mode is called mid-loop operation. If a failure of the RHR system occurs during the mid-loop operation, there is a possibility of boiling of the reactor coolant. One of the effective methods to cool the reactor core in this event is reflux cooling by the SG. During the reflux condensation, steam generated in the reactor core and water condensed in a pressurizer due to heat transfer to its vessel wall may form a countercurrent flow in a surge line connecting the hot leg and the pressurizer. The ROSA-IV/LSTF (Rig-of-Safety-Assessment No. 4/Large Scale Test Facility) experiment [1] for the loss of RHR systems during mid-loop operation showed that water accumulates in the pressurizer due to the limitation of liquid flow in the countercurrent flow in the surge line. Thus, understanding the characteristics of countercurrent flow limitation (CCFL) in the surge line is of great importance for safety evaluation of the mid-loop operation.In our previous study [2], countercurrent flow limitation (CCFL) in a scale-down model of a PWR surge line, which consists of a vertical pipe and an inclined pipe with several elbows, was investigated by measuring the relationship between the water and gas flow rates in the surge line. The relationship is referred to as CCFL characteristics. The CCFL takes place at three locations in the experiments, that is, at the junction between the vertical pipe and the bottom of the pressurizer, in the inclined pipe and at the junction between the inclined pipe and the hot leg. The CCFL characteristics strongly depend on the location of CCFL. The experiments imply that the CCFL at the junction between the vertical pipe and the bottom of the pressurizer plays an important role in the actual surge line under the reflux cooling.Many studies on CCFL in vertical pipes have been carried out [3–11] using the experimental apparatus consisting of a vertical pipe, an upper tank, and a lower tank. Although a number of experimental data of CCFL for various diameters, lengths, and end geometries of vertical pipes have been obtained [9–11], modeling of CCFL in vertical pipes is insufficient because of a large scatter in the data obtained for the different experiments. This scatter implies that the upper and lower tank geometries may have nonnegligible influence on CCFL. Little has, however, been studied on the effect of tank geometry.In the present study, the effects of upper tank geometry on CCFL characteristics were investigated by using a rectangular tank and a cylindrical tank. The flow rate of water entering into a lower tank was measured to obtain the CCFL characteristics. Flow patterns in the upper tanks were observed by using a high-speed video camera and the pressure difference between the upper and lower tanks was measured to understand relations between CCFL characteristics and flow patterns in the tanks. Furthermore effects of water levels in the cylindrical upper tank and the lower tank on CCFL characteristics were investigated.


## 2. Experimental

### 2.1. Experimental Setup

Figure1 shows the experimental setup. It consists of the upper tank, which corresponds to the bottom part of the pressurizer, the vertical pipe corresponding to a part of the surge line, the lower tank, the air supply system, and the water supply system. The pipe and tanks are made of transparent acrylic resin for observation. The diameters, D, of vertical pipes are 30, 45, and 60 mm. Air was supplied from the oil-free compressor (SRL-11P6AI, Hitachi Ltd.) and flowed into the lower tank from four inlets through the regulator (R600-20, CKD) and the flowmeter (FLT, Flowcell, Ltd.). Tap water was supplied using the magnet pump (MX-F400, Iwaki, Ltd.) and flowed into the upper tank through the flowmeter (FLT-N, Flowcell, Ltd.). Experiments were carried out at room temperature and atmospheric pressure. It is well known that CCFL occurrence is strongly influenced by junction geometry, for example, the liquid flow rate with a sharp-edged junction is lower than that with a round-edged junction [12, 13]. The right-angle junction is used for the junction between the upper tank and the vertical pipe to obtain flow limitation at that junction, whereas the bell-mouth junction is used for the junction between the lower tank and the pipe to prevent liquid flow limitation at that junction.Figure 1
Experimental setup.Three types of upper tanks, which we refer to as the rectangular tank, cylindrical tank (a), and cylindrical tank (b), are shown in Figures2(a), 2(b), and 2(c), respectively. The cylindrical tank (a) and the rectangular tank were used to investigate the effects of upper tank geometry on CCFL characteristics. Water levels in the upper tanks were kept constant by overflowing the supplied water. The effects of water level were investigated by using the cylindrical tank (b). The ratio of its diameter to the pipe diameter was determined so as to be analogous to the actual pressurizer. It has drain holes on its wall at various elevations. The drain holes used in each experiment were changed to test various water levels in the upper tank.Upper tanks.
(a)
Rectangular tank(b)
Cylindrical tank (a)(c)
Cylindrical tank (b)


### 2.2. Experimental Method

#### 2.2.1. CCFL Characteristics

CCFL characteristics were investigated by measuring the time-averaged flow rate,QL, of water entering into the lower tank at constant gas flow rates, QG. The QL was calculated from the rise speed of water level in the lower tank. The ranges of the liquid and gas volume fluxes, JL and JG, tested were 0≤JL≤0.118 m/s and 2.40≤JG≤16.4 m/s, respectively, where JL and JG are defined by(1)Jk=QkA(k=L,G).
Here A is the cross-sectional area of the vertical pipe and the subscripts L and G denote the liquid and gas phases, respectively. The uncertainties in measured JL and JG estimated at 95% confidence were ± 3.0% and ± 2.5%, respectively.


#### 2.2.2. Pressure Difference

The pressure differenceΔP (=PLower-PUpper, where PLower and PUpper are the pressures in the lower and upper tanks, resp.) was measured using a differential pressure transducer (DP45, Valydine, Ltd. natural frequency > 600 Hz). It was connected between the top of the upper tank and the side wall of the lower tank as shown in Figure 1. The sampling rate was 1.0 kHz, and the measurement time was 30 seconds. The uncertainty in measured ΔP was less than 0.5% of the full scale (6 kPa). Flows in the upper tank were observed by using a high-speed video camera (Dantec Dynamics, Nano sence Mk3) to understand the relation between ΔP and the flow behavior in the upper tank. The frame rate was 100 fps and the recording time was 30 s.


## 2.1. Experimental Setup

Figure1 shows the experimental setup. It consists of the upper tank, which corresponds to the bottom part of the pressurizer, the vertical pipe corresponding to a part of the surge line, the lower tank, the air supply system, and the water supply system. The pipe and tanks are made of transparent acrylic resin for observation. The diameters, D, of vertical pipes are 30, 45, and 60 mm. Air was supplied from the oil-free compressor (SRL-11P6AI, Hitachi Ltd.) and flowed into the lower tank from four inlets through the regulator (R600-20, CKD) and the flowmeter (FLT, Flowcell, Ltd.). Tap water was supplied using the magnet pump (MX-F400, Iwaki, Ltd.) and flowed into the upper tank through the flowmeter (FLT-N, Flowcell, Ltd.). Experiments were carried out at room temperature and atmospheric pressure. It is well known that CCFL occurrence is strongly influenced by junction geometry, for example, the liquid flow rate with a sharp-edged junction is lower than that with a round-edged junction [12, 13]. The right-angle junction is used for the junction between the upper tank and the vertical pipe to obtain flow limitation at that junction, whereas the bell-mouth junction is used for the junction between the lower tank and the pipe to prevent liquid flow limitation at that junction.Figure 1
Experimental setup.Three types of upper tanks, which we refer to as the rectangular tank, cylindrical tank (a), and cylindrical tank (b), are shown in Figures2(a), 2(b), and 2(c), respectively. The cylindrical tank (a) and the rectangular tank were used to investigate the effects of upper tank geometry on CCFL characteristics. Water levels in the upper tanks were kept constant by overflowing the supplied water. The effects of water level were investigated by using the cylindrical tank (b). The ratio of its diameter to the pipe diameter was determined so as to be analogous to the actual pressurizer. It has drain holes on its wall at various elevations. The drain holes used in each experiment were changed to test various water levels in the upper tank.Upper tanks.
(a)
Rectangular tank(b)
Cylindrical tank (a)(c)
Cylindrical tank (b)


## 2.2. Experimental Method

### 2.2.1. CCFL Characteristics

CCFL characteristics were investigated by measuring the time-averaged flow rate,QL, of water entering into the lower tank at constant gas flow rates, QG. The QL was calculated from the rise speed of water level in the lower tank. The ranges of the liquid and gas volume fluxes, JL and JG, tested were 0≤JL≤0.118 m/s and 2.40≤JG≤16.4 m/s, respectively, where JL and JG are defined by(1)Jk=QkA(k=L,G).
Here A is the cross-sectional area of the vertical pipe and the subscripts L and G denote the liquid and gas phases, respectively. The uncertainties in measured JL and JG estimated at 95% confidence were ± 3.0% and ± 2.5%, respectively.


### 2.2.2. Pressure Difference

The pressure differenceΔP (=PLower-PUpper, where PLower and PUpper are the pressures in the lower and upper tanks, resp.) was measured using a differential pressure transducer (DP45, Valydine, Ltd. natural frequency > 600 Hz). It was connected between the top of the upper tank and the side wall of the lower tank as shown in Figure 1. The sampling rate was 1.0 kHz, and the measurement time was 30 seconds. The uncertainty in measured ΔP was less than 0.5% of the full scale (6 kPa). Flows in the upper tank were observed by using a high-speed video camera (Dantec Dynamics, Nano sence Mk3) to understand the relation between ΔP and the flow behavior in the upper tank. The frame rate was 100 fps and the recording time was 30 s.


## 2.2.1. CCFL Characteristics

CCFL characteristics were investigated by measuring the time-averaged flow rate,QL, of water entering into the lower tank at constant gas flow rates, QG. The QL was calculated from the rise speed of water level in the lower tank. The ranges of the liquid and gas volume fluxes, JL and JG, tested were 0≤JL≤0.118 m/s and 2.40≤JG≤16.4 m/s, respectively, where JL and JG are defined by(1)Jk=QkA(k=L,G).
Here A is the cross-sectional area of the vertical pipe and the subscripts L and G denote the liquid and gas phases, respectively. The uncertainties in measured JL and JG estimated at 95% confidence were ± 3.0% and ± 2.5%, respectively.


## 2.2.2. Pressure Difference

The pressure differenceΔP (=PLower-PUpper, where PLower and PUpper are the pressures in the lower and upper tanks, resp.) was measured using a differential pressure transducer (DP45, Valydine, Ltd. natural frequency > 600 Hz). It was connected between the top of the upper tank and the side wall of the lower tank as shown in Figure 1. The sampling rate was 1.0 kHz, and the measurement time was 30 seconds. The uncertainty in measured ΔP was less than 0.5% of the full scale (6 kPa). Flows in the upper tank were observed by using a high-speed video camera (Dantec Dynamics, Nano sence Mk3) to understand the relation between ΔP and the flow behavior in the upper tank. The frame rate was 100 fps and the recording time was 30 s.


## 3. Results and Discussion

### 3.1. Effects of Upper Tank Geometry

Flow visualization with the high-speed video camera showed that, under all the test conditions, the CCFL with the rectangular tank occurred only at the junction between the vertical pipe and the upper tank, that is, some water flows into the pipe from the upper tank, but the remaining water does not and returns to the reservoir, and then the water entering the pipe forms liquid film and flows down to the lower tank without flooding in the pipe. This CCFL taking place at the upper junction is referred to as CCFL-U. The CCFL characteristics measured using the rectangular tank are plotted in Figure3(a), where JL* and JG* are the Wallis parameters [14] defined by(2)Jk*=Jk[ρkgD(ρL-ρG)]1/2(k=L,G),
where ρ is the density, g the acceleration of gravity and D the pipe diameter. At constant JG*, JL* becomes smaller with increasing D, that is, the flow limitation becomes stronger. Figure 3(b) shows the CCFL characteristics for the cylindrical tank (a). The CCFL occurs only at the junction at low JG*, whereas at high JG* and D≤45 mm, some water penetrating into the vertical pipe intermittently flowed back into the upper tank due to flooding, that is, the CCFL occurs not only at the junction but also inside the pipe. This CCFL is referred to as CCFL-P. Thus, the CCFL characteristics clearly depend on the pipe diameter and the location where CCFL takes place.CCFL characteristics for rectangular and cylindrical tanks onJG*1/2-JL*1/2 plane.
(a)
Rectangular tank(b)
Cylindrical tank (a)Richter [7] and Jayanti et al. [15] suggested that, for prediction of flooding, the Wallis parameter, J*, is appropriate for small diameter pipes, whereas the Kutateladze number, Ku, [16] is better for large diameter pipes. Vijayan et al. [17] carried out flooding experiments using vertical pipes of D = 25, 67, and 99 mm and confirmed that J* is better for small D (25 mm), whereas Ku is better for large D (67 and 99 mm). The Kutateladze number is defined by(3)Kuk=Jk[ρk2gσ(ρL-ρG)]1/4(k=L,G),
where σ is the surface tension. The Wallis parameter includes D but the Kutateladze number does not. Therefore, the pipe diameter plays an important role in flooding for small D, whereas the mechanism of flooding is less dependent on D in large pipes. The CCFL characteristics are replotted on the KuL1/2-KuG1/2 plane as shown in Figure 4. The CCFL characteristics for different pipe diameters are well correlated with the Kutateladze numbers both for the rectangular and cylindrical tanks when the CCFL occurs only at the junction (CCFL-U). Therefore, the diameter effect on the CCFL characteristics is not so significant in these cases. The CCFL characteristics for the two tanks are compared in Figure 5. The flow limitation with the cylindrical tank (a) is stronger than that with the rectangular tank at high KuG because of the CCFL occurrence inside the pipe. On the other hand, at low KuG, the CCFL with the rectangular tank is stronger. This will be discussed later based on the observation of bubble motions in the upper tanks.CCFL characteristics for rectangular and cylindrical tanks onKuG*1/2-KuL*1/2 plane.
(a)
Rectangular tank(b)
Cylindrical tank (a)Figure 5
Effects of upper tank geometry on CCFL characteristics.Figure6 shows the pressure differences, ΔP, for the cylindrical and rectangular tanks and their power spectrums obtained by the fast Fourier transform analysis. The pressure fluctuations for the cylindrical tank (a) mainly consist of waves in the range of 5–7 Hz. On the other hand, those for the rectangular tank consist of single peaks at 3 Hz and broad peaks in the range of 5–10 Hz. Figure 7 shows a typical bubble generation process in the cylindrical tank (a) and ΔP at JG=4.9 m/s and D=45 mm. There is no bubble at the junction at t = 0.13 s. The ΔP increases as a bubble starts to be generated at the junction until t = 0.18 s. The ΔP then decreases as the bubble grows for t = 0.18–0.23 s. The bubble is released from the junction at t=0.28 s, and then, the next bubble starts to be generated at 0.33 s. The period and the frequency of this process are about 0.20 s and 5 Hz, which corresponds to the peak frequency.Pressure differenceΔP between upper and lower tanks (D=45 mm).
(a)
JG=4.8 m/s (KuG1/2=1.00)(b)
JG=7.3 m/s (KuG1/2=1.23)Figure 7
Bubble generation process in the cylindrical tank (a) (JG=4.9 m/s, JG*1/2=0.50, KuG1/2=1.0, and D=45 mm).A bubble generation process in the rectangular tank atJG=4.9 m/s and D=45 mm is shown in Figure 8. The ΔP increases as the bubble grows at the junction for t = 0.10–0.15 s. For t>0.15 s, a trailing bubble is formed behind the leading bubble. The fluctuation of ΔP for 0.15<t<0.42 s must be due to these trailing bubbles. The next leading bubble starts to grow at t=0.45 s. The period of the generation of leading bubbles is 0.35 s. The single peak at 3 Hz and the broad peak in the range of 5–10 Hz in Figure 5, therefore, correspond to the leading-bubble generation cycle and the fluctuation due to the trailing bubbles, respectively. The first mode sloshing shown in Figure 9 was observed only for the rectangular tank. The free surface in the tank took the maximum inclination at t=0 s as shown in Figure 9(a). Then the water moved to the left side, and the bubble was detached from the junction due to water movement in the horizontal direction (Figure 9(b)). Two leading bubbles were released during one period of the sloshing (Figures 9(a)–9(e)). The natural frequency of the first mode sloshing in a two-dimensional rectangular tank is given by [18](4)f=gktanhkH2π(k=πL),
where H is the height of the free surface and L the width of the tank. According to (4), the frequency for the rectangular tank used is 1.53 Hz, which is about half of the bubble release frequency. The bubble release frequency is, therefore, strongly governed by the sloshing in the tank.Figure 8
Bubble generation process in the rectangular tank (JG=4.9 m/s, JG*1/2=0.50, KuG1/2=1.0, and D=45 mm).First-mode sloshing in the rectangular tank (JG=7.7 m/s, JG*1/2=0.70, KuG1/2=1.3, and D=30 mm).
(a)
0 s(b)
0.18 s(c)
0.35 s(d)
0.53 s(e)
0.73 sFigure10 shows images of flows in the rectangular tank and the pipe. Water lump penetrated into the pipe when a bubble detached. The CCFL is, therefore, mitigated when the bubble release frequency is high. This might be the main reason why the CCFL with the rectangular tank is stronger than that with the cylindrical tank (a) at low KuG as shown in Figure 5.Figure 10
Relation between bubble release and water penetration (JG=5.8 m/s, JG*1/2=0.60, KuG1/2=1.1, and D=30 mm).


### 3.2. Effects of Water Level in Tank

The CCFL characteristics measured using the cylindrical tank (b) shown in Figure2(c) are discussed in this section. Various water levels in the upper and the lower tanks were tested. The water level in the lower tank was kept constant throughout each experiment by manually controlling the drain cock opening. In this case, QL was calculated from the amount of drain water. Figure 11 shows the CCFL characteristics for various water levels in the upper tank at constant water levels in the lower tank, where VLower is the air volume in the lower tank and h the elevation of the drain holes in the upper tank. The CCFL becomes stronger as h decreases at VLower = 0.039 m3. The difference in the CCFL characteristics is, however, not so significant. On the other hand, the CCFL characteristics strongly depend on h at VLower = 0.092 m3. Effects of VLower are shown in Figure 12. The CCFL characteristics do not depend on VLower at h=200 mm, whereas the influence of VLower is significant at h=600 mm, that is, the increase in VLower mitigates the CCFL.Effects of water level,h, in upper tank on CCFL characteristics (D=30 mm).
(a)(b)Effects of air volume,VLower, in lower tank on CCFL characteristics (D=30 mm).
(a)(b)Figure13 shows the pressure differences for the cylindrical tank (b) and their power spectrums. The time-averaged ΔP increases with the water level in the upper tank, which corresponds to the water head in the upper tank. The amplitude of the pressure fluctuation at h=450 mm is larger than that at h=200 mm, and the fluctuation frequency at h=450 mm is lower than that at h=200 mm. Images of flow patterns in the middle part of the vertical pipe for h=450 mm and VLower=0.039 m3 are shown in Figure 14. The amount of falling liquid film is small at t=0.30 s. The large water lump falls for 0.32<t<0.34 s. The ΔP increases during the water lump falling. Then the liquid film flows back to the upper tank and the ΔP decreases. The liquid film restarts to fall at t=0.98 s. The amount of the falling water lump is small at low h and low VLower, and it becomes larger as h and VLower increase. This is the main cause of the difference in the CCFL characteristics for different values of h and VLower.Figure 13
Pressure differenceΔP between upper and lower tanks (Cylindrical tank (b), D=30 mm, VLower = 0.092 m3 and JG=9.1 m/s).Figure 14
Flow patterns at the middle of the vertical pipe (Cylindrical tank (b),D=30 mm, h=450 mm, VLower=0.092 m3, and JG=9.1 m/s).


## 3.1. Effects of Upper Tank Geometry

Flow visualization with the high-speed video camera showed that, under all the test conditions, the CCFL with the rectangular tank occurred only at the junction between the vertical pipe and the upper tank, that is, some water flows into the pipe from the upper tank, but the remaining water does not and returns to the reservoir, and then the water entering the pipe forms liquid film and flows down to the lower tank without flooding in the pipe. This CCFL taking place at the upper junction is referred to as CCFL-U. The CCFL characteristics measured using the rectangular tank are plotted in Figure3(a), where JL* and JG* are the Wallis parameters [14] defined by(2)Jk*=Jk[ρkgD(ρL-ρG)]1/2(k=L,G),
where ρ is the density, g the acceleration of gravity and D the pipe diameter. At constant JG*, JL* becomes smaller with increasing D, that is, the flow limitation becomes stronger. Figure 3(b) shows the CCFL characteristics for the cylindrical tank (a). The CCFL occurs only at the junction at low JG*, whereas at high JG* and D≤45 mm, some water penetrating into the vertical pipe intermittently flowed back into the upper tank due to flooding, that is, the CCFL occurs not only at the junction but also inside the pipe. This CCFL is referred to as CCFL-P. Thus, the CCFL characteristics clearly depend on the pipe diameter and the location where CCFL takes place.CCFL characteristics for rectangular and cylindrical tanks onJG*1/2-JL*1/2 plane.
(a)
Rectangular tank(b)
Cylindrical tank (a)Richter [7] and Jayanti et al. [15] suggested that, for prediction of flooding, the Wallis parameter, J*, is appropriate for small diameter pipes, whereas the Kutateladze number, Ku, [16] is better for large diameter pipes. Vijayan et al. [17] carried out flooding experiments using vertical pipes of D = 25, 67, and 99 mm and confirmed that J* is better for small D (25 mm), whereas Ku is better for large D (67 and 99 mm). The Kutateladze number is defined by(3)Kuk=Jk[ρk2gσ(ρL-ρG)]1/4(k=L,G),
where σ is the surface tension. The Wallis parameter includes D but the Kutateladze number does not. Therefore, the pipe diameter plays an important role in flooding for small D, whereas the mechanism of flooding is less dependent on D in large pipes. The CCFL characteristics are replotted on the KuL1/2-KuG1/2 plane as shown in Figure 4. The CCFL characteristics for different pipe diameters are well correlated with the Kutateladze numbers both for the rectangular and cylindrical tanks when the CCFL occurs only at the junction (CCFL-U). Therefore, the diameter effect on the CCFL characteristics is not so significant in these cases. The CCFL characteristics for the two tanks are compared in Figure 5. The flow limitation with the cylindrical tank (a) is stronger than that with the rectangular tank at high KuG because of the CCFL occurrence inside the pipe. On the other hand, at low KuG, the CCFL with the rectangular tank is stronger. This will be discussed later based on the observation of bubble motions in the upper tanks.CCFL characteristics for rectangular and cylindrical tanks onKuG*1/2-KuL*1/2 plane.
(a)
Rectangular tank(b)
Cylindrical tank (a)Figure 5
Effects of upper tank geometry on CCFL characteristics.Figure6 shows the pressure differences, ΔP, for the cylindrical and rectangular tanks and their power spectrums obtained by the fast Fourier transform analysis. The pressure fluctuations for the cylindrical tank (a) mainly consist of waves in the range of 5–7 Hz. On the other hand, those for the rectangular tank consist of single peaks at 3 Hz and broad peaks in the range of 5–10 Hz. Figure 7 shows a typical bubble generation process in the cylindrical tank (a) and ΔP at JG=4.9 m/s and D=45 mm. There is no bubble at the junction at t = 0.13 s. The ΔP increases as a bubble starts to be generated at the junction until t = 0.18 s. The ΔP then decreases as the bubble grows for t = 0.18–0.23 s. The bubble is released from the junction at t=0.28 s, and then, the next bubble starts to be generated at 0.33 s. The period and the frequency of this process are about 0.20 s and 5 Hz, which corresponds to the peak frequency.Pressure differenceΔP between upper and lower tanks (D=45 mm).
(a)
JG=4.8 m/s (KuG1/2=1.00)(b)
JG=7.3 m/s (KuG1/2=1.23)Figure 7
Bubble generation process in the cylindrical tank (a) (JG=4.9 m/s, JG*1/2=0.50, KuG1/2=1.0, and D=45 mm).A bubble generation process in the rectangular tank atJG=4.9 m/s and D=45 mm is shown in Figure 8. The ΔP increases as the bubble grows at the junction for t = 0.10–0.15 s. For t>0.15 s, a trailing bubble is formed behind the leading bubble. The fluctuation of ΔP for 0.15<t<0.42 s must be due to these trailing bubbles. The next leading bubble starts to grow at t=0.45 s. The period of the generation of leading bubbles is 0.35 s. The single peak at 3 Hz and the broad peak in the range of 5–10 Hz in Figure 5, therefore, correspond to the leading-bubble generation cycle and the fluctuation due to the trailing bubbles, respectively. The first mode sloshing shown in Figure 9 was observed only for the rectangular tank. The free surface in the tank took the maximum inclination at t=0 s as shown in Figure 9(a). Then the water moved to the left side, and the bubble was detached from the junction due to water movement in the horizontal direction (Figure 9(b)). Two leading bubbles were released during one period of the sloshing (Figures 9(a)–9(e)). The natural frequency of the first mode sloshing in a two-dimensional rectangular tank is given by [18](4)f=gktanhkH2π(k=πL),
where H is the height of the free surface and L the width of the tank. According to (4), the frequency for the rectangular tank used is 1.53 Hz, which is about half of the bubble release frequency. The bubble release frequency is, therefore, strongly governed by the sloshing in the tank.Figure 8
Bubble generation process in the rectangular tank (JG=4.9 m/s, JG*1/2=0.50, KuG1/2=1.0, and D=45 mm).First-mode sloshing in the rectangular tank (JG=7.7 m/s, JG*1/2=0.70, KuG1/2=1.3, and D=30 mm).
(a)
0 s(b)
0.18 s(c)
0.35 s(d)
0.53 s(e)
0.73 sFigure10 shows images of flows in the rectangular tank and the pipe. Water lump penetrated into the pipe when a bubble detached. The CCFL is, therefore, mitigated when the bubble release frequency is high. This might be the main reason why the CCFL with the rectangular tank is stronger than that with the cylindrical tank (a) at low KuG as shown in Figure 5.Figure 10
Relation between bubble release and water penetration (JG=5.8 m/s, JG*1/2=0.60, KuG1/2=1.1, and D=30 mm).


## 3.2. Effects of Water Level in Tank

The CCFL characteristics measured using the cylindrical tank (b) shown in Figure2(c) are discussed in this section. Various water levels in the upper and the lower tanks were tested. The water level in the lower tank was kept constant throughout each experiment by manually controlling the drain cock opening. In this case, QL was calculated from the amount of drain water. Figure 11 shows the CCFL characteristics for various water levels in the upper tank at constant water levels in the lower tank, where VLower is the air volume in the lower tank and h the elevation of the drain holes in the upper tank. The CCFL becomes stronger as h decreases at VLower = 0.039 m3. The difference in the CCFL characteristics is, however, not so significant. On the other hand, the CCFL characteristics strongly depend on h at VLower = 0.092 m3. Effects of VLower are shown in Figure 12. The CCFL characteristics do not depend on VLower at h=200 mm, whereas the influence of VLower is significant at h=600 mm, that is, the increase in VLower mitigates the CCFL.Effects of water level,h, in upper tank on CCFL characteristics (D=30 mm).
(a)(b)Effects of air volume,VLower, in lower tank on CCFL characteristics (D=30 mm).
(a)(b)Figure13 shows the pressure differences for the cylindrical tank (b) and their power spectrums. The time-averaged ΔP increases with the water level in the upper tank, which corresponds to the water head in the upper tank. The amplitude of the pressure fluctuation at h=450 mm is larger than that at h=200 mm, and the fluctuation frequency at h=450 mm is lower than that at h=200 mm. Images of flow patterns in the middle part of the vertical pipe for h=450 mm and VLower=0.039 m3 are shown in Figure 14. The amount of falling liquid film is small at t=0.30 s. The large water lump falls for 0.32<t<0.34 s. The ΔP increases during the water lump falling. Then the liquid film flows back to the upper tank and the ΔP decreases. The liquid film restarts to fall at t=0.98 s. The amount of the falling water lump is small at low h and low VLower, and it becomes larger as h and VLower increase. This is the main cause of the difference in the CCFL characteristics for different values of h and VLower.Figure 13
Pressure differenceΔP between upper and lower tanks (Cylindrical tank (b), D=30 mm, VLower = 0.092 m3 and JG=9.1 m/s).Figure 14
Flow patterns at the middle of the vertical pipe (Cylindrical tank (b),D=30 mm, h=450 mm, VLower=0.092 m3, and JG=9.1 m/s).


## 4. Conclusions

Countercurrent flow limitation (CCFL) in vertical pipes are measured using an apparatus consisting of the vertical pipe, the upper tank, and the lower tank to understand effects of tank geometry and water level in the tanks. The tank shapes used were rectangular and cylindrical. The pipe diameters tested were 30, 45, and 60 mm. Air and water at room temperature and atmospheric pressure were supplied from the upper tank and from the lower tank, respectively. The flow rate of water entering into the lower tank was measured to obtain CCFL characteristics. Flow patterns in the upper tanks were observed by using a high-speed video camera and pressure differences between the upper and lower tanks were measured to understand relations between CCFL characteristics and the flow patterns in the tanks. The main conclusions obtained under the present experimental conditions are as follows.(1)
The CCFL characteristics for different pipe diameters are well correlated using the Kutateladze number if the tank geometry and the water levels in the tanks are the same.(2)
CCFL takes place at the junction between the pipe and the upper tank both for the rectangular and cylindrical tanks. In addition, CCFL with the cylindrical tank (a) takes place not only at the junction but also inside the pipe when the gas flow rate is high and the pipe diameter is small.(3)
The flow rate of water entering into the vertical pipe at the junction for the rectangular upper tank is lower than that for the cylindrical tank (a) because of the presence of low frequency first-mode sloshing in the rectangular tank.(4)
Water penetration into the pipe increases with the water level,h, in the cylindrical upper tank and the air volume, VLower, in the lower tank, and, therefore, the flow limitation is to be mitigated with increasing h and VLower.These experimental results clearly show that not only the pipe geometry but also tank geometry and water levels in the tanks must be taken into account when modelling characteristics of CCFL in vertical pipes.



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*Source: 754724-2012-04-05.xml*