vertical flow

7
VERTICAL TWO-PHASE FLOW Part III: Pressure Drop P. L. SPEDDING (FELLOW), G. S. WOODS (GRADUATE), R. S. RAGHUNATHAN and J. K. WATTERSON Department of Aeronautical Engineering, The Queen’s University of Belfast, Belfast, UK D ata are presented on the total two-phase pressure drop for air-water vertical ¯ ow in a 0.026m i.d. pipe. The data exhibit a maximum value, at the end of the churn ¯ow regime, set between two minima at the end of the slug and annular ripple regimes respectively. There was a noticeable diameter effect. It was possible to explain the form of the pressure loss data qualitatively. In the slug and allied regimes the rising gas bubble carried a pocket of liquid in its wake resulting in a reduction in the ¯ uid head. None of the current theories of pressure loss prediction proved to be useful. However, it was possible to predict bubble ¯ ow at low gas rates and annular droplet ¯ ow at high gas rates. Keywords: vertical; two-phase; pressure drop; prediction; up lift pressure INTRODUCTION Many studies have been carried out on the pressure drop in vertical 1 90° two-phase gas-liquid ¯ ow. Table 1 details the major literature on the subject. Not all the data has proven to be reliable mainly because of the inclusion of entrance and exit effects into the measurements. Calvert and Williams 5 showed the expected effect on the measurement of pressure drop if either the design of, or the operation of, the apparatus did not eliminate such end effects. In addition, Hewitt et al. 23,52± 54 and Woods and Spedding 55 showed that the method used to premix the phases can exacerbate the problem. Thus there exists a need to evaluate the data (e.g. in Table 1) to ensure that the measured pressure drop truly conformed to the straight pipe geometry. Spedding and Ferguson 56 have shown that prediction of pressure drop for horizontal ¯ ow was ¯ ow regime dependent with either the Olujic 57 model or the Spedding and Hand 58 model achieving reliable prediction across the entire ¯ ow regime range. In general, gravity, can be expected to have a more pronounced effect on pressure drop in vertical ¯ ow. It is therefore highly unlikely that one model will be able to predict pressure drop over the whole range of vertical ¯ ows despite the fact that many workers have attempted to do so 1,7±11,13,14,17,18,25,28±31,34,36,42±44,46,48±51,59,60 . Other workers have, by contrast, developed pressure prediction models dependent on ¯ ow regimes 2,5,7,12,16,19±24,27,32,33,35,37,39,47,58±61 . The three most widely recommended methods of vertical pressure loss prediction are: (a) The general method of Hagedorn and Brown 29±31 , recommended by Gould 44 , Abdul-Majeed et al. 46 and Aggour et al. 51 . (b) The models of Beggs and Brill 62 recommended by Aggour et al. 51 . (c) The four regime dependent model or Orkiszewski 35 recommended by De Gance and Atherton 63 and Mata Iturbe 64 . More recently Holt et al. 65 have developed a ¯ ow pattern speci® c model for pressure drop estimation in vertical two- phase ¯ow using a number of theories to estimate the component of acceleration, gravitational and frictional pressure drop for the bubble, churn and annular ¯ow regimes. RESULTS Figure 1 gives the air-water vertical total two phase pressure drop for the 0.026m i.d. pipe. Also shown are data for 0.0454m i.d. pipe by Nguyen 41 , and for 0.03818m i.d. pipe by the Harwell group 19±24 in annular ¯ ow. Other data [e.g. Govier et al. 7±9 , Beggs 37 , etc] gave general average agreement with Figure 1, but showed a degree of scatter which was no doubt accentuated by an unsystematic approach to measurement of the data. In general, the total pressure drop data presented as a maximum value set between two minima situated at medium and low gas ¯ ow rates. The larger diameter pipe possessed a higher and lower value of pressure drop than the corresponding data for the smaller diameter set at lower and medium gas rates respectively. The cross over point (arrowed on Figure 1) moved to lower gas ¯ows as the liquid rate was increased and approximately coincided with the neutral frictional pressure drop point. Thus a signi® cant diameter effect was in evidence which was particularly noticeable at lower gas rates. Figures 2 to 5 present the 0.26m i.d. data for four liquid rates and also show the average values for the measured total pressure loss and the calculated head and frictional losses. In addition, Figure 2 gives the range of the total pressure drop. The data were obtained by initially setting a liquid rate and systematically increasing the gas rate, and then reversing the process. At ® rst, the total pressure loss was composed of a pure liquid head with a small frictional component. The liquid or gas only data gave agreement with single phase calculations. At very low gas ¯ ows, 628 0263±8762/98/$10.00+0.00 Institution of Chemical Engineers Trans IChemE, Vol. 76, Part A, July 1998

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Page 1: Vertical Flow

VERTICAL TWO-PHASE FLOW

Part III: Pressure Drop

P. L. SPEDDING (FELLOW), G. S. WOODS (GRADUATE), R. S. RAGHUNATHAN and J. K. WATTERSON

Department of Aeronautical Engineering, The Queen’ s University of Belfast, Belfast, UK

Data are presented on the total two-phase pressure drop for air-water vertical ¯ ow in a0.026 m i.d. pipe. The data exhibit a maximum value, at the end of the churn ¯ owregime, set between two minima at the end of the slug and annular ripple regimes

respectively. There was a noticeable diameter effect. It was possible to explain the form of thepressure loss data qualitatively. In the slug and allied regimes the rising gas bubble carried apocket of liquid in its wake resulting in a reduction in the ¯ uid head.

None of the current theories of pressure loss prediction proved to be useful. However, it waspossible to predict bubble ¯ ow at low gas rates and annular droplet ¯ ow at high gas rates.

Keywords: vertical; two-phase; pressure drop; prediction; up lift pressure

INTRODUCTION

Many studies have been carried out on the pressure drop invertical 1 90° two-phase gas-liquid ¯ ow. Table 1 details themajor literature on the subject. Not all the data has proven tobe reliable mainly because of the inclusion of entrance andexit effects into the measurements. Calvert and Williams5

showed the expected effect on the measurement of pressuredrop if either the design of, or the operation of, the apparatusdid not eliminate such end effects. In addition, Hewitt etal.23,52 ± 54 and Woods and Spedding55 showed that the methodused to premix the phases can exacerbate the problem. Thusthere exists a need to evaluate the data (e.g. in Table 1) toensure that the measured pressure drop truly conformed tothe straight pipe geometry.

Spedding and Ferguson56 have shown that prediction ofpressure drop for horizontal ¯ ow was ¯ ow regimedependent with either the Olujic57 model or the Speddingand Hand58 model achieving reliable prediction across theentire ¯ ow regime range. In general, gravity, can be expectedto have a more pronouncedeffect on pressure drop in vertical¯ ow. It is therefore highly unlikely that one model will beable to predict pressure drop over the whole range of vertical¯ ows despite the fact that many workers have attempted to doso1,7±11,13,14,17,18,25,28±31,34,36,42±44,46,48±51,59,60. Other workers have,by contrast, developed pressure prediction models dependenton ¯ ow regimes2,5,7,12,16,19±24,27,32,33,35,37,39,47,58±61. The three mostwidely recommended methods of vertical pressure lossprediction are:

(a) The general method of Hagedorn and Brown29±31,recommended by Gould44, Abdul-Majeed et al.46 andAggour et al.51.(b) The models of Beggs and Brill62 recommended byAggour et al.51.(c) The four regime dependent model or Orkiszewski35

recommended by De Gance and Atherton63 and MataIturbe64.

More recently Holt et al.65 have developed a ¯ ow pattern

speci® c model for pressure drop estimation in vertical two-phase ¯ ow using a number of theories to estimate thecomponent of acceleration, gravitational and frictionalpressure drop for the bubble, churn and annular ¯ owregimes.

RESULTS

Figure 1 gives the air-water vertical total two phasepressure drop for the 0.026m i.d. pipe. Also shown are datafor 0.0454m i.d. pipe by Nguyen41, and for 0.03818m i.d.pipe by the Harwell group19±24 in annular ¯ ow. Other data[e.g. Govier et al.7±9, Beggs37, etc] gave general averageagreement with Figure 1, but showed a degree of scatterwhich was no doubt accentuated by an unsystematicapproach to measurement of the data. In general, the totalpressure drop data presented as a maximum value setbetween two minima situated at medium and low gas ¯ owrates. The larger diameter pipe possessed a higher and lowervalue of pressure drop than the corresponding data for thesmaller diameter set at lower and medium gas ratesrespectively. The cross over point (arrowed on Figure 1)moved to lower gas ¯ ows as the liquid rate was increasedand approximately coincided with the neutral frictionalpressure drop point. Thus a signi® cant diameter effect wasin evidence which was particularly noticeable at lower gasrates.

Figures 2 to 5 present the 0.26 m i.d. data for four liquidrates and also show the average values for the measuredtotal pressure loss and the calculated head and frictionallosses. In addition, Figure 2 gives the range of the totalpressure drop.

The data were obtained by initially setting a liquid rateand systematically increasing the gas rate, and thenreversing the process. At ® rst, the total pressure loss wascomposed of a pure liquid head with a small frictionalcomponent. The liquid or gas only data gave agreementwith single phase calculations. At very low gas ¯ ows,

628

0263±8762/98/$10.00+0.00� Institution of Chemical Engineers

Trans IChemE, Vol. 76, Part A, July 1998

Page 2: Vertical Flow

629VERTICAL TWO-PHASE FLOW: PART III

Trans IChemE, Vol 76, Part A, July 1998

Table 1. Data and Models for Vertical Two Phase Flow.

Diameter VSL VSG

System cm ms2 1 ms 2 1 Comment Reference

diesel-air 0.21, 0.15 0±0.64 0.06±38.5 data correlation [1]kero-air 0.21, 0.15 0±0.19 0.07±35.7

oil-gas 5.07, 5.18, 6.20, 6.27, 0.05±0.73 0.10±2.75 data correlation [2]7.42, 7.60, 7.67, 7.79

water-air 1.32, 5.08 0±0.54 0.74±16.0 data [3]

water-steam 5.94 0.79±0.98 x = 0.315±0.0448 data [4]20±80 atm (a)

water-air 2.54, 2.82, 5.03 0±0.13 2±68.9 data, theory [5]

water-steam 2.21 0.42±0.93 x = 0.004±0.043 data [6]

water-air 1.6, 2.6, 3.81, 6.35 0.02±2.24 0±27.82 data correlation [7±9]

water-air 0.09, 1.95 0.09±0.66 0.16±20.3 data correlation [10±11]aq. soln-air 2.77

water-N2 0.53±0.70 0.05±1.20 4.3±215 data [12]aq soln-N2

water-steam 0.50 0.23±1.45 370±815

water-air 2.70 0.2±3.0 0.3±64 data correlation [13±14]

water-steam 2.21 0.30±0.90 2.75±30.2 data [15]

water-air 1.08 0.65±13.7 2±64 data, theory [16]

water-air 2.66 0.02±0.75 0.6±31 data correlation [17]

water-air 1.27, 1.91, 2.54 0.08±1.0 0.07±1.1 data, theory [18]

water-air 3.18, 3.45 0.±0.2 20±90 data correlation [19±20]

water-air 3.18 0.01±0.96 25.6±64.0 data correlation [21±24]

water-steam 2.54, 3.81 VT = 0.91±2.13 data correlation [25]

water-Argon 2.50 0±2.4 7.4±1324 data [26]aq. soln-Argon 2.50 0±1.2 23.5±565

oil-gas 5.96 0.05±0.62 0.01±4.52 data correlation [27]

water-air 2.66 0.02±0.73 0±32.7 data correlation [28]oil-air 2.66 0.03±0.85 0±32.7aq. soln-air 2.66 0.02±0.70 0±31.8

water-gas 2.66, 3.51 0.01±3.20 5.8±67.8 data correlation [29±31]oil-gas 4.09, 5.25

water-air 1.59, 3.18 0±0.6 16.3±136.1 data correlation [32]

water-air 1.28, 2.23 0.02±0.01 0±28.6 data correlation [33]

water-air 1.3±3.8 0.02±3.64 0.01±105 data [34]

oil-gas 1.27, 1.91, 2.54, 7.62, 0±1.0 0±2.75 data correlation [35]20.32

water-steam 0.5, 0.8, 0.92 0.2±2.58 0.52±26 data correlation [36]water-Argon 2.5 0.25±2.40 0.01±22water-N2 2.5 0.22±1.38 0.01±22EtOH-Argon 1.5 0.28±2.58 0.01±23

water-air 2.66, 4.09 0.02±2.53 1.21±95.9 data correlation [37]

water-air 3.81 0.03±0.32 0.01±0.03 data [38]

water-air 3.18 0.01±0.64 13.39±72.21 data [39]HCl-air 3.18 0.02±0.17 14.91±58.28

water-air 2.54 0.01±2.06 0±45.8 data [40]aq. soln-air

water-air 4.54 0.01±1.05 0.08±60.2 data [41]

water-steam 0.5±1.0 1±13.75 74±4833 data correlation [42]1.5, 2.5 3.5±4.9 40±84440.5±1.5 0.6±12.0 37±133701.2, 1.7 0.76±1.60 46±1852

water-N2 2.5, 5.08 0.1±3.0 2.4±2195

water-N2 7.79±10.5 0±0.96 0.65±175 data correlation [43]

water-steam 19.88 0.08±2 1.8±8 data correlation [44]

water-air 1.17 0.31±10.6 0.07±96.0 data [45]water-He 0.31±10.6 0.13±148

Page 3: Vertical Flow

homogeneous conditions prevailed in the bubble regime. Inthis region the total pressure loss fell rapidly and could becalculated from the two phase density. These conditionswere shown to prevail until QG/QL = 0.1. Again in thisregion, the frictional component was a minor element in thetotal pressure drop. As the gas rate was increased, the totalpressure drop continued to fall rapidly along with the two-phase density, but the bubbles grew in size and formed a capor slug of gas over the whole cross section of the pipe. In thisregion, the Nicklin et al.66 model gave an accurateprediction of holdup right up until the onset of annular¯ ow. The limit of the bubble region was shown to follow theTaitel et al.67 criterion.

V SL = 3.0 V SG 2 1.15g(rL 2 rG)j

r2L

1/4

(1)

In both the large bubble and slug regimes the calculatedfrictional pressure drop became negative in magnitude. Thenormal explanation for the effect has been that the liquid¯ ows downward in an annular ring between the inside of thepipe wall and the rising gas Taylor bubble resulting in anegative frictional region. However, while the downwardliquid annulus ¯ ow can explain the wide ¯ uctuationsobserved in the total pressure drop, it cannot explain thenegative value of the overall average value of frictionalpressure drop.

Guedes de Carvalho et al.68 have shown that a risingTaylor bubble of gas carried a pocket of liquid in its wake

such as to effectively reduce the apparent head loss of thetwo-phase liquid to below that expected from the actualtwo-phase density. Thus the calculated negative friction wasdue to the upward lifting of the liquid in the wake of therising gas Taylor bubble. Indeed, it has been shown69 thatthe annular ring of liquid ¯ owing downward around therising bubble was supercritical and therefore would enwrapa pocket of liquid below the Taylor bubble to a depthprescribed by the onset of the hydraulic jump whichoccurred when the Fr in the annular liquid ® lm passedbelow unity. The calculation of the frictional pressure dropby subtracting the two-phase head from the total pressuredrop would be incorrect, as the rise effect in the Taylorbubble wake liquid has been ignored. Two things were ofimportance. Initially, frictional pressure loss was insignif-icant and the ® rst minimum in the calculated frictionpressure loss in Figures 2 to 5 corresponded to the transitionfrom slug to churn ¯ ow. With the onset of churn ¯ ow, the

630 SPEDDING et al.

Trans IChemE, Vol 76, Part A, July 1998

Table 1. Continued

Diameter VSL VSG

System cm ms2 1 ms 2 1 Comment Reference

water-Freon 12 0.31±4.2 0.16±36.0 data [45]

oil-gas 2.54±16.5 0±2.50 0.02±77.7 data correlation [46]

water-air 1, 1.6, 2.6 0.006±0.1 20±60 data correlation [47]

water-steam [26], [36], [42], [43] [26], [36], [42], [43] [26], [36], [42], [43] correlation [48]

water-air 7.6 0.01±227 0.01±6.00 correlation [49]

aq. cmc-air 1.9 0.3±1.0 0.17±1.62 data correlation [50]

oil-gas 5.07, 16.17 0.03±144 0.05±2.71 data [51]

Figure 1. Total two phase pressure drop for air-water vertical ¯ ow in twopipes of different diameters.

Figure 2. Total two phase pressure drop for air-water vertical ¯ ow in a0.026m i.d. pipe for GSL = 10.97 kg m 2 2 s 2 1 . The bars indicate the¯ uctuations in the measured two phase pressure. Also shown is the head,frictional and up lift pressure.

Page 4: Vertical Flow

frictional component started to become signi® cant while theuplifting component steadily reduced until at the onset ofannular ¯ ow, the destruction took place of the liquid wakefollowing the gas slug. The onset of churn ¯ ow reduced theuplift component and increased the frictional component,thus giving a minimum in the total pressure drop curvewhere the churn ¯ ow regime passed into the semi-annular

pattern. In this and the subsequent regimes the chaoticnature of the ¯ ow experienced in the churn regime wassteadily reduced along with the liquid holdup. The totalpressure drop was reduced as the gravitational, theinterfacial and the ® lm activity were also reduced as the® lm passed successively from annular roll wave to theannular ripple regime. However, the pressure drop com-menced to rise again with increased gas ¯ ow at the onset ofthe annular droplet regime. The momentum exchangebetween the gas and liquid phases increased and, as dropletswere increasingly being formed, the energy necessary wasextracted from the gas phase giving a substantial increase inthe frictional component of pressure drop. These competingeffects resulted in a second minimum being formed in thepressure drop characteristic with increasing gas rate.

Thus the formation of different ¯ ow patterns provided acoherent explanation of the two-phase pressure dropcharacteristics for vertical upward ¯ ow. The differentgeneral behaviour observed for the two sets of pressuredrop curves given in Figures 2 and 3 and Figures 4 and 5resulted from the super® cial liquid velocity being respec-tively below and above the rise velocity of the gas Taylorbubble for this system. For the latter case, the trailing liquidslug was not held securely behind the rising gas bubble dueto disturbance of the enclosing liquid down ¯ ow.

It is clear from the discussion that it is not possible toreliably predict pressure drop using one model alone.

Various prediction models were tested, using data forvarious diameters, Nguyen41, Hewitt et al.52,53, Woods55.The prediction methods tested by Spedding and Ferguson56

631VERTICAL TWO-PHASE FLOW: PART III

Trans IChemE, Vol 76, Part A, July 1998

Figure 3. Total two phase pressure drop for air-water vertical ¯ ow in0.026m i.d. pipe for GSL = 62.67 kg m 2 2 s 2 1 . Also shown is the head,frictional and up lift pressures.

Figure 4. Total two phase pressure drop for air-water vertical ¯ ow in a0.026m i.d. pipe for GSL = 261.00kg m 2 2 s 2 1 . Also shown is the head,frictional and up lift pressures.

Figure 5. Total two phase pressure drop for air-water vertical ¯ ow in0.026m i.d. pipe for GSL = 376.00 kg m 2 2 s 2 1 . Also shown is the head,frictional and up lift pressures.

Page 5: Vertical Flow

for the horizontal condition did not prove to be useful. Thisincluded the Olujic57 and Spedding and Hand58 modelswhich were successful for the horizontal case. The generalmethod of Hagedorn and Brown29±31 gave predictions wellin excess of data. The reason was that the system studied byHagedorn and Brown29±31 was a gas lift operation where ahead of liquid was imposed at the base of the ¯ ow rig. Inaddition, no consideration was given to possible changes of¯ ow regime up the column and there was no assurance thatthe column was indeed vertical. By contrast, the models ofBeggs and Brill62 and Orkisewski35 made provision fordifferent types of ¯ ow regimes. However, neither modelproved useful, with the Beggs and Brill method62 tending tounderpredict the data, while the Orkisewski35 methodshowed a wide scatter around the data. The method ofHolt et al. 65 while allowing for prediction over the wholerange of ¯ ow regimes, tended to overpredict the data.

Prediction has been achieved for low gas ¯ ow rate underQG/QL = 0.1 in the homogeneous regime. For the slug ¯ owregime the amount of liquid holdup which was uplifted bythe gas slug RLU was:

RLU

RL

= 2.34 ´ 10 2 4 d

dc

2 2.34 ´ 10 2 4 ReSG

2 1.638d

dc

1 1.638 (2)

The critical diameter dc = 0.05 m above which RLU = 0,and was a region where the hydraulic jump of the annularliquid ® lm could not enclose and uplift liquid in the gas slugtail. Equation (2) only applies for the condition that V SL wasless than the Taylor bubble rise velocity. When V SL was inexcess of the bubble rise velocity, RLU was small. Equation(2) predicted the slug data for 0.026 and 0.0454m i.d. pipeto within an average of 1% (2 10.2% to 1 4.3% range).

The annular regimes at high gas ¯ ow rates ReSG > 8 ´ 104

followed the relation

DP

D z TP

= 1.5457 ´ 10 2 14Re3.5683SL Re( 2 0.6315 log ReSL 1 3.1909)

SG

´ f0.0317

d

3

(3)

within 6 14%. Values of f are presented in Figure 6. Therationale underlying the model was that total two-phasepressure drop was mainly caused by friction in the annular¯ ow regime and that it varied approximately as 1/d3, thesame as with single phase ¯ ow.

Predictions in the intermediate gas ¯ ow region arepossible but will be the subject of future work.

CONCLUSIONS

The total pressure drop for vertical ¯ ow against gas ratepresented as a maximum value at the end of the churn ¯ owregime, set between two minima situated at low andmedium gas ¯ ow rates. There was a noticeable effect ofdiameter on the pressure drop. It was not possible to predictthe whole range of pressure drop values. However, thegeneral form of the total pressure drop curve was explainedqualitatively.

Calculation of the frictional pressure drop using onlyhold-up data resulted in negative values in the slug, churn

and semi-annular regimes. This was physically unrealisticand resulted from ignoring the pocket of liquid rising in thewake of the Taylor gas bubble.

None of the theories for predicting pressure loss provedeffective. This was particularly true of those models basedon air-lift operation. It was possible to predict the totalpressure drop at very low gas rates (QG/QL # 0.1) in thebubble regime and a high gas rates (GG > 30 kg m 2 2 s 2 1) inthe annular droplet regime.

NOMENCLATURE

D diameter, mg gravitational constant, m s2 2

p pressure, kg m 2 1 s 2 2

Q ¯ ow rate, m3 s 2 1

Re Reynolds NumberV velocity, ms 2 1

Greek lettersr density, kg m2 3

f factor equation (3)

Subscriptsc criticalG gasL liquidS super® cialT totalU uplift

REFERENCES

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632 SPEDDING et al.

Trans IChemE, Vol 76, Part A, July 1998

Figure 6. Frictional factor f values used in equation (2) for prediction oftotal two phase pressure drop for vertical air-water annular droplet ¯ ow.

Page 6: Vertical Flow

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ADDRESS

Correspondence concerning this paper should be addressed to ProfessorP. L. Spedding, Department of Aeronautical Engineering, The Queen’ sUniversity of Belfast, David Keir Buildings, Stranmillis Road, BelfastBT9 5AG, UK.

The manuscript was received 4 August 1997 and accepted for publicationafter revision 3 February 1998.

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