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Transcript of TWO-PHASE WELLBORE SIMULATOR AND … · TWO-PHASE WELLBORE SIMULATOR AND ANALYSIS OF REINJECTION...
TWO-PHASE WELLBORE SIMULATOR AND ANALYSIS OF REINJECTION
DATA FROM SVARTSENGI, ICELAND
Mahmut Parlaktuna*,
UNU Geothermal Training Programme,
National Energy Authority,
Grensasvegur 9. 108 Reykjavik.
ICELAND .
• Permanent Address:
Middle East Technical University, Petroleum Engineering Department.
Ankara. TURKEY.
2
3
ABSTRACT
A computer program Is developed for the simulation of flowing geothermal wells. Th e necessary correc t ions of the
salt and C02 concentrations on the thermophysical proper ties of the geothermal fluid are included 1n the program.
The program is tested wi th the data from the Svartsengi
geothermal field in Iceland and the Kizl1dere geotherma!
field in Turkey.
The response of the Svartsengl geothermal field to the
injection is also investigated. A lumped model, called "the
steam model" is used to analyze the effect of injection.
and the actual data from th e injection test at the Svarts
eng! field in 1984 Is used for that purpose.
4
5
TABLE OF CONTENTS
Page
ABSTRAC T ..... ... . . •.. . .. .. •..•..•.. . . .. .. . . ... . ... . . .. . . . . 3
INTRODUCTION
1.1 Purpose of the study
1.2 Statement of the prob l em
2 FLOW PERFORMANCE CALCU LATIONS IN GEOTHE RMAL WELLS
9
9
2 . 1 Introduction........... . . ... . ......... . . . ... . . .. .... , t
2 . 2 De r ivation of the equatio n s for f luid flow In a
vertical pipe . . ....... . .. . ..... .. ........ . .. .. . . ... 1 2
2.2.1 Single - phas e r egion ... ..... .... . . . .... .. . . .. . 14
2 . 2.2 Two-phase region
2 . 3 Wellbore heat transfer
2 . 4
2 . 5 2 . 6
Thermodynamic pro perties of geo t he r mal fluids ..... .
Ef f ect of C02 ...... . . . ... . ...... .. .. . .. ... . ....... . .
Applications of the prog r am
2 . 6 • 1 Svartsengl well No . 4
2.6.2 Svartsengl well No. 1 1
2.6 . 3 Kizl1dere well No . 6
3 RESPONSE OF SV ARTSENG I FIELD TO REINJ ECTION 3 . 1 Ana l ysis of injec t io n data .... .. . . ... .. . .. .... . ... .
3 . 2 Model description ....... . .... .. . .. . ... .... . ...... . .
4 SUMMARY ... . .. .... . . .. .. . . . ... .. .. ........ .. .. . . . .. . ....
ACKNOWLEDGEMENTS
NOMENCLATURE . . . . ... .. .. . ... ..... . ..... . .. . . .. . .. ........ .
REFERENCES .... ...... ... .. .... .. .. ... .......... .. ...... ...
APPENDIX A, Program listing ... .. . ... .. . ..... . . . ... . . . .
APPENDIX B . 1 : Computer outputs fo r Sva r tsengi well No. 4
15
1 9 20
22 24
25 26
27
29 30
33
7
35
48
without calc i te deposi ti o n . . .. .. .......... 53
APPEND I X B.2 : Compu t er o ut puts for Svartse ngi well No. 4
with calcite de position 55
6
LIST OF FIGURES
Fig. Svartsengi well No . 4 output characteristiCS 38
Fig. 2 Svartsengl well No . 4 calcit e deposition accordi ng
to callper log measured 78.12.13 ... . .. . .. .. . .. . . . 39
Fig. 3 Pressure profiles in Svartsengi well No. 4 40
Fig. 4 Change In flashing depth with mass flow rate 41
Fi g . 5 Deliverabl1ity curves for SG - l1 fo r different reservoir pressures 41
Fig. 6 Effect of casing size on the outp ut cu r ves of geothermal wells 42
Fig . 7 Scaling thick ness e s measured by go-devil In
Klzildere well No. 6 43
Fig. 8 Net production and injection rates with time 44
Fig. 9 Drawdown with time 45
Fig . 10 Conceptual model of the Sva r tsengi reservoir •.. . . . 46
Fig . 11 Schematic representation of the steam model for
the Svartsengl reservoir 46
Fig . 12 Measured and fitted drawdown from the steam model.. 47
LIST OF TABLES
1 • Svartsengi well No . 4 output measurements 25
2. Data and comp uter output for Kizildere well No. 6 .. ..• 28
NOMENCLATURE
C
C
Cm o ( d P ) t
(dp)acc
(dp)fri
(dp)pot
dz
E
f
G
g
H
h1
m
P
Ps Pwf P
Q
Q
r
R
Re
Cross - sectional area to flow , (m2)
~low area in water zone. (m 2 )
Flow area in feed zo n e, (m 2 ) Pressure drop factor fo r skin effect and long
term drawdown, (Pa/(kg/s»
Leakage co nstan t for steam model (kg/sec/m)
Turbulence factor, (Pa/(kg/s)2)
Specific heat of the rock matrix, (J/kgK) Diameter of pipe , (m)
Total pressure drop , (Pa)
Pressure drop due to acceleration,
Pressure drop due to friction, ( P a )
Pressure drop due to gravitational I ncremental pipe length. (m)
Energy of fluid. (J/.)
Friction factor
Mass flux, (kg/m 2 s)
Accelerat i on due to gravity. (m/5 2 )
Enthalpy, (kJ/kg)
( P a )
gradient ,
Drawdown between two-phase and liquid phase inter f ace, (m)
Drawdown i n feed zone. (m)
Permeability of the aquifer , (m 2 ) Thermal conductivity of rock, (W/mK)
(Pa)
Molality of the solution, (moles/kg)
Concentration of carbondioxide in liquid phase , ($ by weight)
Pressure. (Pa)
Steam saturation pressure , (Pa)
Bottom hole flowing pressure, (Pa) Wellhead pressure, (Pa)
Heat loss to surroundings, (J/s/m)
Amount of wa t er flowing out of storage in the
water zone, (kg/s)
Radial distanc e, (rn)
Universal gas consta n t, (kJ/krnoleK)
Rey nol ds nurn ber
Well bore radius , (m)
Storage in the liquid zone
Storage in the feed zone
7
8
T
t
V
W
x
Temperature. (OC)
Time, (sec)
Fluid velocity. (m/s)
Mass flow rate . (kg/ s)
Steam quality, (%)
Aquifer depth, (m)
Flashing point in the well, (m)
Greek symbols:
p
P 1
P2 ,
"
K
SUbscripts
L
m
s
Fluid density. (kg/m3)
Density of fluid in water zone, (kg/m 3 )
Density of fluid 1n feed zone, (kg/m 3 ) Absolute roughness factor of the pipe, (m)
Dynamic viscosity of fluld. (Pa 5) Void fraction
Slip factor
Two-phase multiplier
Specific volume of fluid. (m3/kg)
Thermal diffusivity of the rock, (m2/sec)
Liquid phase
Rock matrix
Vapour phase
9
1 INTRODUCTION
1.1 Purpose of the study
This report is the final part of a 6 month training at the UNU Geothermal Training Programme I at the National Energy
Authority 1n Reykjavik, Iceland 1n the summer of 1985.
The author's training programme can be divided into four
main sections, namely introductory lectures in various
disciplines of geothermal technology, lectures on reservoir engineering for the specialized training in this subject.
two weeks field excursion and seminars on the various
geothermal fields of Iceland and the final project on the
subjects of simulation of flowing wells and response of the Svartsengl field to injection.
The experience and knowledge gained will be helpful to
solve not only problems dealt with in this report but a
wide range of problems associated with evaluation and
utilization of geothermal energy in Turkey.
1.2 Statement of the problem
Among the several factors affecting the flow performance of
the wells, diameter of the we ll as well as the reduction in
the diameter due to calcite scaling and the drawdown in the reservoir can be mentioned. It is a common practi ce to develop simulators to study the effects of those factors. Because of the chemical composition of the geothermal
fluid, the thermodynamic properties of pure water should be
corrected for salt concentration . Another factor which
should be taken into account in the two-phase pressure drop
calculations is the effect of non-condensable gases.
Reinjection is increasingly becoming an integral part of
the deSign of geothermal projects. The necessity of
reinjection mainly arises from three factors I disposal of chemically hazardous geothermal waste water, possibility of
pressure recovery of the declining aquifer and more heat extraction from the reservoir rock.
1 0
The main pr o blems encoun t ered
Turkey are the reduction 1n the
1n geoth e rma l fields in
yields of the wells due to
both scaling and drawdown 1n the reservo i r , and the disposal of waste water. These two problems were selected
to provide the writer with a useful experience and knowl
edge on the methods of solution.
11
2 FLOW PERFORMANCE CALCULATIONS IN GEOTHERMAL WELLS
2.1 Introduction
Good production wells 1n high temperature fields are characterized by high flowrates which make the downhole
measurement of the flowing wells impractical. This diffi
culty makes simulation of the flowing wells important .
Therefore, it is necessary to develop and test the flow
models for geothermal wells by using limite d data which
exists for low flowrates.
Wells 1n high temperature, liquid dominated geothermal
reservoirs generally produce two-phase mixtures . In the
case of liquid water inflow to the wellbore, the drop 1n
pressure during upflow results in flashing of the fluid in the wellbore. Since the thermodynam i c properties of a brine
change with the salt concentration, it is necessary to
correlate the properties of fluid with respect to salt concentration. One of the constituents in geothermal fluid
is non - condensable gas, especially C02, which causes an increase in the flashing pressure. To analyze the behaviour
of flowing wells, a wellbore simulator was developed which
takes the effects of salt and C02 concentration into
account. This simulator was used to estimate the
deliverability curves for two wells in the Svartsengi
geothermal field 1n Iceland. The effect of C02 was studied by using data from the Kizilde r e geothermal field in Turkey . As a final applica t ion, the changes 1n the output
of a wel l as a result of calcite deposition was also
stUdied.
In the following sections, the derivation of flow equations
and corrections for
presented .
salt concentration and C02 are
1 2
2.2 Derivation of the equations for fluid flow in a
vertical pipe
To describe the fluid flow in a vertical pipe, one can use the equations of conservation of mass, momentum and energy.
During the following derivation of equations it is assumed that the flow 1s homogeneous, steady and one - d i mensional.
- Equation for conservation of mass:
w pVA (1)
- Equation for conservation of momentum:
This
pOint
equation of view.
1s generally wr i tten
Total pressure drop
from a pressure
is made up of
individual gradients,
- {dP)t = (dP)fric + (dP)acc + (dP)pot ( 2 )
Let us define each gradient separately.
i) Frictional pressure drop
drop
three
This pressure drop is def ioed by the Darcy-Weisbach
equation as;
(dP)fric pfV2 --dz
2D ( 3 )
The friction factor "f" is a function of the Reynolds
Number, Re, and the relative roughness of pipe and is given
by the modified Colebrook's equation as;
where
< f = [ [ -2 log (--J +
3.7D
pVD Re
7 0.9 2 -1 (-J 1 1
Re ( 4 )
( 5 )
1 3
11) Acceleration pressure drop
(dP)acc = pVdV ( 6 )
If the mass flux ls defined as G - W/A, and from Eg o 1.
V Gip. then the acce l eration pressure drop can be
expressed as;
(dP)acc • G dV
ill) Potential pressure drop
This pressure drop is defined as;
(dP)pot • pgdZ ( 8 )
By using equations 3.7 and 8 the total pressure drop can be
written as;
pfV2 - (dP)t - dZ + GdV + pgdZ
2D ( 9 )
- Energy equation:
The total energy equation can be expressed as;
dE WdH + Wd (':'.:.) 2
- WgdZ - QdZ ( 1 0 )
since there is no energy input for a self-flowing well,
E- O. equation 10 becomes;
o V2 Q
dH + d ( - ) + gdZ - dZ 2 W
( 1 1 )
The total enthalpy ls a function of the enthalpies of each
phase, HI and Ha. and the flowing steam quality. x.
H - xHs + (l - x) HI ( 1 2 )
1 ~
Integration of equation 11 between any two points in the
well 1n an upward direction gives;
Q ( 1 3 )
By introducing equation 12, the steam quality at point 2
can be found as;
H8 .2 - Hl,2 ( 1 ~ )
The heat 10S8 to the surrounding, Q. will be discussed 1n a
later section.
It 1s known that a liquid-dominated geothermal reservoir
will initially produce undersaturated water at the well bore
sand - face. During the upflow of the fluid along the
wellbore. the drop 1n pressure results 1n saturated water
and the flow becomes a two - phase flow. In order to examine
these two different sections, namely single-phase and two - phase, it is necessary to study the above equations at
each section separately.
2 • 2 • 1 Singe - phase region
In this section, the fluid density is almost constant which
corresponds to the density of the inflow temperature . This
constant density results in a constant velocity, V,R V2,
then according to equation 7 (dP)acc - o.
Now, total pressure drop for Single-phase region is reduced
to;
-(dP) -pfV2 --dZ
20 + pgd Z ( 1 5 )
1 5
2.2 . 2 Two-phase region
When the fluid starts flashing 1n the wellbore, it under
goes different two - phase flow regimes. namely bubble . slug
and annular. These flow regimes have been studied by several authors (Ros, 1961; Hagedorn , 1964; Orkiszewski.
1967). In these flow regimes , the vapour and liquid phases
travel separately at different velocities. Since the vapour
always "slips " past the liquid 1n vertical flow, equation
9 has to be corrected.
In general the mixture density Is presented 1n terms of
actual void fraction defined f r om the volume occupied by
the vapour phase,
where
o • or Al
(1 - 0) • A
( 1 6 )
( 1 7l
On the other hand the slip factor , '\, Is defined as the
velocity ra t io,
, . ( 1 8 )
Another important definition for the two - phase region is the steam quality. x.
x • Ws
W or (l-x) • ( 1 9 )
Now , let us define individual pressure drops in the two - phase region .
1 6
i) Potential pressure drop
By substituting equation 17 into equation 8
(dP)pot : ( 20 )
11) Acceleration pressure drop
From the equation for conservation of mass, equation 1. the
velocities of each phase can be written as;
xW V . (21 )
PsAs
and
V . (l - x)W ( 22)
P1Al
On the other hand. the acceleration pressure drop in
two- phase region is defined as;
(23)
By substituting the definitions of velocities from equa
tions 21 and 22
_W_W,,-l..:.( ..:.1 _- ,,-x .c) d(
A P1Al ( 24 )
By making further substitutions for rates of mass flow and
cross - sectional areas for each phase from equations 17 and
19 the final equation is obtained as;
(dP)acc • (l-x)2 --J (I-.)Pl
( 25 )
1 7
111) Frictional pressure drop
If we introduce the definition of mixture dens i ty , equation 16, into eq uation 3 the frictional pressure drop for the two-phase region can be obtained.
( 2 6 )
But the difficulty a r ises here In the evaluation of the
two - phase friction factor and velocity of the fluid,
because oC the definition of the two - phase viscosity and
the difference between the velocities of phases due to
slip. In order to overcome this difficulty several empiri
cal correlations have been studied.
Martinelli-Nelson (1948) defined an empirical relation to
calculate the friction pressure gradient by assuming a
ratl-o, called two-phase multIplier.
(dP/dZ)rtp - ~21 ors (27 )
where (dP/dz)rtp Is the two - phase frictional pressure gra dient, (dP/dz)l and (dP/dz)s are the frictional pr essure gradients for the li quid or gas respectively if they a re flowing alone in the same tube .
Other correlating parameters have been defined if the total mass is flowing with the physical properties of one of the
phases .
(28)
where (dP/dz)lo and (dP/dz)so are the pressure gradients for the total flow of fluid having the liquid or gas physical properties respect i vely .
In this correlation , frictional pressure drop for the single phase is obtai ned by assuming that all the flo wing
fluid is in this phase , then this single phase pressure
drop is multiplied by the two-phase multiplier to obtain
the frictional pressure drop in the two-phase flow.
1 8
In the literature, there are several correlations fo r a
two- phase multip l ier. In this report, the correlation given
by Chisholm (1972) is used.
4> 2= C 1 1 + + 7 X
( 29 )
where
X2 . 1-x 2 vl (-).- (30 )
x Vs
and
C 1 + xVs - a ( 3 1 )
xvs + (1 - xlvl
As can be seen in equation 31 the void fraction, hould
be known to calculate t he two - phase multiplier . In order to
calculate the vo i d fraction the correlation by Ar ma nd and
Teacher (1959) is used .
a = 0 . 833 + 0 . 05 log(P)
(1-x) Vl +
This concludes the equations for
two- phase section . The location of
be calculated as follows.
- (dP)t . (Pwf - Ps) . (d P)fr! +
From equation 1 5 • by substituting dZ
- (dP)t .
z* - Za -
pfV2 pg)( Za - Z*) (""2D +
Pwf - Ps
pfV2 pg +
2D
Pin bar
pressure drop in the
the flashing point can
(dP)pot (33 )
. Za - Z*
(34 )
(35 )
, 9
But. the high flowrates and temperatures in geothermal wells, make it difficult t o run downhole measurements
under normal operati ng conditions. Therefore, in order to get the value o f the bottom hole flowing pressure, Pwf. we
should find a relationship between the conditions of static well and flowing well.
Durlng the flow of fluid 1n the reservoir. the pressure
drops from undisturbed reservoir pressure, Pal to the
bottom hole flowing pressure. Pwf. at the sand-face. This
pressure drop in the reservoir Is due to the skin effect,
the longterm drawdown factor. and the turbulence pressure
drop. (Kjaran , 1983) Therefore, Pwf can be written as;
Pwf • Pa - (SW + Cw2) (36)
where Band C are some factors.
In the high flowrate geothermal wells, initially the pressure drop due to turbulence is the dominant factor and
equation 36 can be rewritten as;
Pwf - Pa - CW2 (37)
Since we have some measurements of Pwf for the low flowrates, equation 39 can be solved analytically by taking
the slope of (Pa-Pwf)/W vs. W graph as turbulence factor C.
Another way of obtaining the C value is the use of
simulators to match the deliverability measurements of the wells since the wellhead pressure is given by,
Po • Pwf - (dP)t • Pa - CW 2 - (dP)t (38 )
In this procedure, Pa is an i nput and C is the variableto match the measured wellhead pressure for a given flowrate.
2.3 Well bore heat transfer
During the flow of fluid in the wellbore, some heat is transferred by conduction through the rock surrounding the
well bore. This heat transfer to the surrounding has been
20
studied by Ramey (1962). By assuming that the conductive
heat flow Is normal to the axis of the well. the equation
for heat conduction can be written as;
1 3 3T K -.-(r. - )
3T PmCm-
3T r ar ar
The boundary conditions are as follows,
where Tr •
T
(r + "').
(r - r w)
undisturbed reservoir temperature, (OK) temperature at the well face, (OK)
<39 )
The conductive heat transfer per unit length of the
well bore Is given by:
(T r - Tw)
f(t)
where let) Is defined as;
2;'](t f(t)-ln( ) - 0.29
rw
( ~ 0 )
( ~ 1 )
In fact. the boundary condition given for undisturbed
reservoir temperature occurrs at a certain distance from
the wellbore instead of infinity. By introducing this new
boundary condition, the solution of the problem becomes
more complicated and is given by Carslaw and Jaeger (1959).
2 . ~ Thermodynamic properties of geothermal fluids
Geothermal fluids are solutions of various types of salts.
These are primarily NaCl, KC1, and CaC12, but it is a
common practice to use the "equivalent NaCl content" to
define the salinity of a geothermal fluid. The "equivalent
NaCl content" is the amount of NaCl in solution that will
bring the same effect on the properties as the amount of
all the salts combined.
21
For the model ling of the geotherma! well, it is necessary
to know some thermophysical properties accurately. such as
the density, the enthalpy, the entropy. the viscosity and the saturation pressure at a given temperature. To make the
corrections on the pure water properties, Michaelides
(19Bl) presented some formulas which are based on "equivalent NaCl content".
One of the effective changes in the properties of pure
water wi th salt content is the depression of saturation
pressure at a given temperature,
1 .8R(T + 273.15) m OF -
Vs - VI 55.56 ( 4 2 )
where R - (8.314/18) - 0.4619 kJ/kgK. 55.56 15 the moles of
water in 1 kg of the substance
Salinity of water in pprn and m -
Molecular weight of NaCl
The saturation pressure of pure water Is given by the
following simplified correlation;
P(T) • exp(0.21913E - 6T3- 0.17816E-3T 2
+ 0.0653665T - 4.96087) (43)
In his paper Michaelides gives the gas constant as 8 . 314
kJ/kgK for equation 42, but if the unit analysis is done
carefully, it is found that the actual gas constant is the
ratio of universal gas constant (8.314 kJ/kmoleK) to the
molecular weight of water ('8 kg/kmole). The reader should
give attention to this change in the formula.
Let us take an example to show the effect of salt on the
depression of saturation pressure. If we take the common
values from the Svartsengi geothermal field in Iceland,
T • 240DC and salinity - 20.000 ppm
by using equation 43, P(T) - 32 .93 bar
22
20.000 mg/kg m = = 0.342 mol/kg
58.500 mg/mol
and Vs 0.0595 m3/kg . vI 0.0012 m3/kg from the steam
tables for pure water.
By substituting the above values into equatIon 42
6P - 45.05 kPa = 0.45 bar
The true saturation pressure therefore reduces to.
P P(T) - 6P - 32.93 - 0.45 - 32.48 bar
For the correlations of densIty. enthalpy. viscosity,
entropy and elevation of saturation temperature, the reader is referred to Michaelldes (198 1 ).
2.5 Effect of C02
C02 provides an Important component to the total pressure
of geothermal fluid. Presence of C02 causes the transition between single-phase and two-phase flow to happen deep er in
the well bore than one would expect by ignoring C02.
The pressure of the vapour phase Is the sum of steam and
gas partIal pressures,
p - Ps + Pg ( 4 4 )
The partial pressure of gas can be expressed in terms of
the concentration o f gas in liquid phase and solubility.
The solubility data for C02 was fitted to an equation by
Sutton (1976).
a(T) - {5.4-3.5(T/IOO)+1.2(T/IOO)2IE - 9. (I/Pa) (45)
The partial pressure of C02 i s given by the following
formula,
( 45)
23
In order to show the effect of C02 on the flashing pressure
of the fluid I let us take an example from the Kizildere geothermal field in Turkey.
The well number KD-6 is producing 15% C02 by weight in the
steam phase and the wellhead steam quality is measured as
9.47%. The inflow temperature of fluid is 201°C.
In order to get the flashing pressure, the steam saturation
pressure and C02 partial pressure should be calculated separately.
By using equation 45 the steam pressure can be found.
Ps(T) • 15.79 bar
Now,first of all we should convert the wellhead C02 meas
urement to downhole concentration. By assuming all the C02
was in the vapour phase at the wellhead,
n1 • 0.15·9.47 • 1.42 % by weight
By using equation 45. a(T) - 3.21E-9
0.0142
3.21E-9 4.42E6, Pa
l/Pa
1i4.2 bar
Therefore, the flashing pressure of this system 1s;
P • 15.8 + 44.2 • 60 bar
which is far beyond the steam saturation pressure.
After flashing, the C02 pressure in the vapour diminishes
from its inl tial value as flashing progresses. Most of the
mass of C02 is exsolved in the first few weight percent of flashing. Mlchels (1981) developed a relationship for the
C02 pressure in a developing vapour phase.
The partial pressure of C02 is given accurately enough by
the real gas equation, PV = znRT, and the final form can be
expressed as a function of three factors, namely initial
24
CO 2 partial system. and
developed.
pressure, the present temperature of the the weight percent of flashing that has
Pc(O) {l 44 \lsx -1
+ .(T)R(T+273.15)1 (47)
where pc{o) Initial C02 partial pressure and 42 is molecular weight of C02.
2.6 Applications of the program
The developed computer program can find the main applica
tions in the follow i ng subjects:
i. Prediction of flowing well pressure and temperature
profiles.
11. Development of deliverability curves for a certain
well for different aquifer pressures.
iil. Determination of the effect of salt and C02 concentra
tion on the flashing point of the fluid.
iv. Determination of the e ff ect of calcite deposition and plugging on production .
These four items were analyzed for two wells in the
Svartsengi the effect
During the
field in Iceland
of CO 2 from the applicatio n of
a nd one exampl e is gi ven for
Kizildere field in Turkey. the computer program , the
relative roughness coefficients of the slotted liner,
casing and calcite deposition were taken as 1.37 E- 4, 4.57
E- 5 and 3.041 E- 4 m respectively.
The listing of the program is presented in Appendix A.
25
2.6.1 Svartsengl Well No. q
This well was initially drilled to 1113 m depth, and it was used as a production well until a casing damage occurred 1n
the well in 1980. Presently it Is used as an observation
well.
The depth of the aquifer Is found from the temperature
profiles as 1024 m, initial temperature and pressure values
were 240 0 C and 88 bars respectively.
During the application
deliverability curves of
of the computer program. the
the well, with or without calcite
deposition, and the pressure profile of the well were
obtained. These results are compared with the actual
measurements. The output measurements for well 4 In
Svartsengi are given in Table t. As can be seen from
Fig. 1, the deliverability curves for the cases with or
without calcite are in good agreement with the measured
ones. This fit was obtained by using the turbulence
coefficient as 0.0035 bar/(kg/s)2.
TABLE 1 Svartsengi well no 4 output measurements
WHP(bara) Flow(kg/s) WHP(bara) Flow(kg/s) Without calcite With calcite
19.0 33.0 18.9 28.0 17.1 59.0 1 6.8 39.0 1 4 . 0 75.0 1 3. 5 49.0 1 3.2 80.0 1 1 .2 50.0 1 1 . 7 85.0 9.2 51 .0
8.9 52.0
Data derived from Fig. 2 was used to see the ef fect of
calcite deposition. The length of deposition was taken as
60 m between the interval 350-410 m and the best fit was
obtained by using 11.5 cm as the average diameter of the
calcite section. The calcite deposition causes a very high
in high flowrates and the chang e in pressure drop
deliverability curve
flowrate. In Svartsengi
Is very abrupt at a parti cular
kg/S and with a flowrate
choked.
51 4, this flowrate is found as
higher than this value the flow is
26
The measured and calculated pressure profiles were also
compared at Fig. 3. The calculated pressure profUe at 30
kg/s flowrates gives a good fit with the measured one.
As a final application, mass flowrate vs. flashing depth
from wellhead was plotted. and the caliper log of the well,
Fig. 2, was compared with this plot (Fig . 4) . By taking the
flashing depth as 410 m from Fig. 2, the corresponding
f!owrate Is found as 31 kg/a from Fig. 4 which was the
actual average flowrate of the well before callper log.
The computer outputs for Svartsengl Appendix B.
are given in
2.6.2 Svartsengi Well No. 11
This well was used as an example for the effect of reser
voir pressure and casing size on the dellverabl11ty curves.
The family curves for different reservoir pressures are
shown on Fig. 5. The pressure drawdown causes a reduction
in the wellhead pressure but this reduction is not of the
magnitude as the reduction of reservoir
the other hand, the shape of the
same order of
pressure. On
deliverability curves are almost the same for all reservoir
pressures, therefore it is possible to find a common
formula depending on the reservoir pressure, wellhead
pressure and mass flowrate by knowing
deliverability curve for a reservoir pressure.
only o n e
As a part of this study, three production tests were
carried out and the data is used in the program. The lip
pressure method developed by James (1970) was use to test
the well. A V-notch was used to measure the low mass
flowrates and
James's formula
area, en thal py
the enthalpy of fluid is calculated from
which relates mass flow, discharge pipe
of fluid, and lip pressure. For a higher
mass flowrate, the well was discharged vertically, direct
to the atmosphere. The enthalpy value obtained from low
flowrates is used to get the flowrate from James ' s formula.
The results of the test are given in Fig. 5. Since there is
about 12 bar pressure reduction in the field from the
initial reservoir pressure, due to the production, the
27
reservoir pressure is taken as 76 bar. The best fit is
obtained by using zero turbulence factor.
The effect of casing size on the output curves was also
studied and the results obtained for two different wells
are plotted in Fig. 6 . The main effect of the casing size
on the output characteristics of the wells is the decrease
1n the turbulence pressure drop in the wider wells. The
dellverabl11ty curve for Svartsengi 11 was obtained by
using zero turbulence factor and as can be seen from Fig.
6. the change in flowrate does not affect the wellhead
pressure in the wider well as in the narrower wel l .
2.6.3 Kizildere Well No. 6
To see the effect of C02 on the output curves, data from
Kizildere geothermal field in Turkey was used. The
Kizildere field is a hot-water type geothermal field which
is producing through six wells. One of the important problems in this field is CaCO scaling in wells which is
related not only to the calcium but also to the C02 content of the geothermal fluid. High percentage of C02 in the geothermal fluid of Kizildere causes early flashing of
the fluid because of higher C02 partial press ure . The data from Kizildere Well no 6 (KD-6) was used in the program and
the flashing depth and the wellhead pressure were examined. The actual data (Tan, 1982) and computer output for this
well are given in Table 2. Fig. 7 shows the configuration
of casing string and flashing point.
By using zero turbulence pressure drop, the wellhead pressure was obtained as 3.14 bar and the flashing point is at 576 m which shows a good agreement with the measure
ments.
28
TABLE 2: Data and computer output for Kiz1!dere well No. 6
NME or FII:r.n ~
W~tL fl\'l~
DAtE OF CALe ,
KIll LOr.nE KP· 6
17·0'-8~
~!N~t£ · I'H."'':;r.(W!1'Efl) !iECTI9N·
r~ (aAAS) (llp)tu!b (W,S) . I'wr (RA.1S) CC02 (p~~)
C!l.a..CL (p~)
D~rIH! !I ) rf ba! )
1100 . 000 7'1 .H4 7 !10.l!O ~ 70 .1!2 fj 6~ . ~OO ~1.750 61j; . fj~O 67 .7U Gao .OOG 62 .o"
84.0 00 !I.eo!!
QUOD 14204.0 1200.0
VeW )
J,034 3.oJ4 3. 034 2. 366 2.36'
1.'\ (K'J /~ ) .. '!G .O!!O I'w t (MlI.:; J 84.000 B (tJ/~'.I) , Oj6.617 rna!lh (S,,,'S) 5' , '85
O!'!'Ti! , re ore
~7) . 1 j, .!, 1~ . 21 !I .aao ~ O!! . O n.'-9 2.79 · 41.421 ~ O ~ . !! 11.26 1.21 ·U~9
~ ~~ . ~ o .~~ U, · 0.~4 2
200 . 0 6. 12 0. 40 - 0. 288 leO . D 3.'0 0. 22 - 0. 178
' . 0 l . 12 US · 0.0 39
WII r (AAJl. ) .. l.12
Ka~:; nOM taLe
Oepth
»,
Sall >:ontcnl
Haclor
0.018 O.O!! O. OIB O. !lt4 0.014
0 %01
24.~5 D.' 2U~ 2.1 '- U5 U 14.45 '-' 2U~ I . ' 1.4. 4512.1 24.45 \3 . 5
96 k1J/ ~
851 •
3. 0 bi[
1200 p~lII
O{ru~AT . DrM! QPFIlIC W(ku/51 f(CJ
21.5'0 -4.406 - 4.242 · 0.164 ' !i.!!!! 201. !I 2\.5'0 . B.B\2 - g. 4S~ -o. m '6 .00 201.0 2U'O -l.m -2.,n -0. lt3 '5.00 20U 14.448 0 .1102 0. 000 O . O~!I 96 . 0(1 201.!! 14 . 448 -5.Ii56 -5.5" -0 .0'0 ",00 201 .0
0" OrIl?! OrACe DPrRIC I!fJt~!l Hq F!
o.lloa C . ~~~ ~ . OoO 0 .000 B~6 . 6 2et . O ~ . OlH . H .700 · J. OIJ4 ·o.m; ~!I . I 12 e~~ . 9 I" . B O . ~t41
~4.m ·2.l72 ·U170 - O.!!!! 8~4. 9 179 .9 O. OW . 2. ~13 . L7~J · 0.057 - 0.3 \7 a~1 .0 m.9 o.om -2.l31 · 1.508 · 0. !!7!! · 0.466 952 . 7 m.B 0.0141 ·2 .m · 1.267 · 0.204 -0 .776 m .2 140 . 1 0. 0141 - !l .771 -o.m -a . 105 -11 .334 B~a . 5 132 . 5 0. 0141
Boll~ hole P(C~5U(£ B4 b~[ , T\!:IIpl! [atull: 201 C
CO2 content of I lea. 15 t by lidyhl
SICiU. qUllity 'U7 ~
Tabl\! 2. D~la and to~puLc( out pul fer I:i:iltkrl! Wdl no 6
f'F!.AS1I
5' .'85 ~ ~ . '95 H . ~m S, .,R5 5' . 985
Stf t-1QIJl.!Y
1. !!O ~ . a, S!! 1.56 0. 70 ;":1 Ut ~.7!' M 3.17 !I.8) /Ill 4.S! 0.84 11:1 6. I! ~.89 AI{ 6.71 !! . 90 A!l
29
3 RESPONSE OF THE SVARTSENGI GEOTHERMAL FIELD TO INJECTION
The Svartsengl geothermal field is a high temperature
liquid dominated field with a temperature range 235-2400C
and the fluid produced is in composition of two-thirds sea water and one - third fresh water. The geology of the
Svartsengl field has been deseri bed by Franzson ('983).
Res e rvoir engineering studies in Svartseng l are discussed
by Kj aran et al . (1979) and Gudmundsson et al. (, 985a.
1985b). The fluid production in Svartsengl has resulted 1n
a draw down of 135 m, after a fluid production of about 41
E9 kg. The rap i d drawdown in the field may affect the
following items of the future performance of the field, i) cold water
cooling of
production
encroachment from surrounding
the formation, i1) decline in
wells with falling reservoir
aqu ifers, and
the output of pressure, iii)
migration of the flashing zone down the wells and into the formation, iv) sealing of the producing fractures by
calcite deposition if the fluid flashes in the formation.
Injection would be a solution to the pressure recovery of
the field as well as the efficient disposal of waste brine and condensate.
To study the effects of injection in the field two injection and tracer tests were carried out in 1982 and 1984.
These tests are discussed by Gudmundsson (1983) and Hauksson (1985). The purpose of this study is to investi
gate the pressure response of the field to injection and match one year production history of the field by using a
lumped-parameter model.
3.1 Analysis of injection data
In the Svartsengi injection test, a brine - condensate
mixture was injected for 72 days between 25th July to 4th October, 1984. The mixture was 80 percent flashed brine and 20 percent steam condensate and the injection flowrate
was kept at 50 kg/so The mixture had a pH close to 6.7 and the temperature 80°C. During the injection test, the
drawdown was measured as water level in a monitoring well . The critical problem encountered during the injection was
the silica scaling in the i njection well. It was tried to
30
avoid this by controlling the pH of the injected fluid and by dilution of the
plant. During the
brine with the condensate of the
test the condensate concentration
power
could
not be kept constant because of the unavailability of
adequate amount of condensate from the power plant. As a
resul t the concentration of the condensate decreased down
to 10 percent which caused an increase in the rate of
silica deposition. One of the proposed solutions to
decrease the rate of silica deposition Is the injection of
CO 2 with the condensate, which produces a weak acid to lower the pH down to 5.5 (Hauksson, T. personal communi cat 1 on) •
To see the effect of injection on the drawdown of the
field. the rate of production and drawdown data are used
for the time period of October 1983 to January 1985. The
total rate of production and injection data are shown in
Fig. 8 with time, and the net production is the difference
between production and injection rates. The water level
drawdown is shown in Fig. 9 with time.
The drawdown data shows a linear trend for the first seven
months in which the net production rate is almost constant.
But after a decrease in production. the rate of drawdown
also decreases and during the time of injection the water
level starts to increase. The effect of reinjection can
also be seen from the late portion of the data when the
production rate reaches the initial value. During this
period, the change in drawdown shows the similar trend as
of the early data. By using these two graphs it can be
concluded that the injection can be helpful to recover
pressure .
3.2 Model description
Fluid extraction and reservoir drawdown in the Svartsengi
field developed an increased steam zone after a few years
of fluid production. This is evident from Well 10 which
changed from being liquid-fed to producing steam only which
is the shallowest well among the six main producing wells
(424 m deep). Other wells in the field are still liquid
fed. A conceptual model of the Svartsengi reservoir is
31
shown in Fig. 1 0 • The liquid dominated reservoir Is
overlaln with a steam zone, which increases in size with
drawdown (Hauksson, 1985).
Based on the above conceptual model Vatnaskil (1983)
developed a lumped parameter model of the field. The schematic representation of the model Is given In Fig. 11.
The boundaries of the reservoir are impermeable and there
Is a slightly impermeable barrier between the feed zone and the liquid dominated zone. The drawdown In the feed zone
leads to a leakage from the water zone. This leakage
results in an increase In the size of the two-phase zone.
The balance equations for this model can be written as;
W "" q +
where c is a constant .
If we solve these equations for h, and h2 we get;
t
h1 (t) • Cdm(t-tle-t/kdt o
t
h2(t) - Cl(t) - C2 fm(t-t)e-t/kdt o
where;
C
( 4 8 )
( 49)
( 5 0 )
(51 )
(52)
( 5 3 )
( 5 4 )
32
c C3 •
A, " S, A2'2S2 ( 5 5 )
A, " S, A2'2S2 K • ( 5 6 )
C A, P, S, +A2P2S2
and
k
M (t ) • fW(T)dT (57)
0
The same set of production and drawdown data given In Figs . 8 and 9 were used to test the proposed model. The produc
tion rate of Well 10 was subtracted from the total field
product i on. because it i s producing from the two" phase
region. For the best fit of dr a w-down, the variables in Eq.
54 are found as;
K '" 125 days, C = 5.1 E- 9 m/kg, C = 2.5 E- l1 m/kg/day
A good fit is obtained for the long term behavio r of t he
drawdown (Fig. ' .2). but the model was not able to produce
the sharp changes In the draw-down . This is due to the
nature of the model, which assumes the storage is given by
the free surface effect at the boiling surface. which is
the long term effect thus neglecting the short term elastic
storage. The model also assumes that all the introduced
change in the flowrate should reach to the boundaries to be
effecti ve on the drawdown, The time required to see the
boundary effects in the Svartsengi field was found to be
10 " 30 days by Kjaran e t .al. (1979) , Therefore, it is not
possible to simulate any changes
time less than 30 days.
in the flowrate for a
33
4 SUMMARY
Simulation of flowing wells can be a useful tool for geothermal well analysis. Using the flow model, It Is still possible to get information for the conditions where the
actual measurements failed. The following parameters can be deduced by the application of a well bore simulator.
1. The temperature and pressure profiles of flowing wells
can be obtained.
2. The change In the performance of the well after scaling
development In the well can be simulated.
3. The magnitude of decline In wellhead pressure with aquifer pressure can be found
4. The wellbores with wider production casings give higher
flowrates than those with smaller sized wells .
The practical use of the model presented here can be listed as follows:
a. The flash level of the geothermal fluid can be found
within a good accuracy. therefore it gives a valuable data
for the cleaning operations of the wells.
b. The wellhead pressure and mass flowrate history of the
wells can be forecasted by using the predicted drawdown of
the reservoir itself. This Information is used for the
planning of the operational life of a geothermal power
plant, since it requires some minimum values for both mass
flowrate and pressure values in the turbine.
It is found that the decline in the drawdown can be reduced
by injection. Reinjection also has merits for the waste
disposal problems of geofluid which causes pollution
problems. To fit the immediate response of the Svartsengi
field to injection, a new model should be developed which
can respond to changes in the
less than a month. In order to
steam model the flowrate of
constant for a longer time.
flowrate over a period of
see the validity of the
injection should be kept
34
ACKNOWLEDGEMENTS
It is a great pleasure for me to express my appreaciatlons
to Dr. Snorri Pall Kjaran for his helpful and patient
guidance during this study.
I would like to extend my thanks to Mr. Sigurdur Larus Holm
who provided the field data and helped in the computer work of this study.
Thanks are due to Mr. Trausti Hauksson who conducted the
well test and supplied his experience about the practical
aspects of the injection test.
Special acknowledgements are also due to Dr. Ingvar 8irgir
Fridleifsson for critical reading of this report.
I also wish to extend my gratitude to the United Nations
University for the Fellowship. the National Energy Author
ity of Iceland in the use of the computer and other facilities and the Middle East Technical University for the
leave of absence which made this work possible.
35
REFERENCES
Armand, A.A., Teacher, C.G. (1959): Investigation of the
Resistance During the Movement of Steam-Water Mixtures In
a Heated Boiler Pipe at High Pressures. Atomic Energy
Research Establishments. Hartwell. Berkshire.
Bjarnason, J.O •• Stelngrlmsson. B., and Gudmundsson,
G. ,(1983), I. Drawdown In the Geothermal Reservoir. 11. The
Chemistry of the brine and Steam 1980-1983. Ill. Tempera-
ture and Pressure in the Reservoir: National Energy
Authority of Iceland, Report OS 83086-JHD-17.
Carslaw, H.S. and Jaeger, J.S. (1959): Conduction of Heat
In Solids. Oxford Press. London, 386 pp.
Chlsholm. D. (1972): Pressure Gradients Due to Friction
During the Flow of Evaporating Two-Phase Mixtures in Smooth
Tubes and Cha nnels. Int. Jo u. Heat and Mass Trans., 16,
347-358.
Franzson, H. (1983):The Svartsengi High-Temperature Field,
Iceland, Subsurface Geology and Alteration. Geothermal
Resources Counsil, Trans., Vol. 7, 75-78.
Gudmundsson, J.S. (1983): Injection Testing in 1982 at the
Svartsengi High-Temperature Field in Iceland. Geothermal
Resources Counsil, Trans., Vol 7 ,423-428.
Gudmundsson, J.S ., Olsen, G.
Sva rtsengi Field Production
and Thorhallsson, S. (1985a) :
Data and Depletion Analysis .
Proc., Tenth Workshop Geoth. Reservoir Engineering, Report
SGP -TR-84 ,45-51, Stanford, California .
Gudmundsson, J.S. and Olsen , G. (1985b) : Water Influx
Modeling of Svartsengi Geothermal Field, Iceland. paper SPE
13615 presented at the California Regional Meeting,
Bakersfield, March 27 - 29.
Hagedorn, A.R. and Brown. K.E. (1964): The Effect of Liquid
Viscosity in Vertical Two-Phase Flow. Jour. of Pet. Tech.,
203-210.
36
Hauksson, T. and Gudmundsson, J.S. (1985) : Tracer Survey 1n
Svartsengl Field 1984 . Geothermal Resources Couns!l.
Trans . , Val 9, part 11, 307-315 .
Jarnes, R . (1970): Factors Cont r olling Well bore Performance .
Proe. of UN Symposium on the Development and Utilization of Geotherrnal Resources, Val 2, Part 2, 22 Sept-l Oct., Pisa,
1502-1515.
Kjaran,
Eliasson,
s . P • •
J.
Halldorsson, G . K ••
(1979), Reservoir
Thorhallsson, S.
Engineering Aspects
and
of
Svartsengi Geothermal Area . Geothermal Recources Couns!l,
Trans . , Val 3. 337-339.
Kjaran, S.P . and Eliasson, S . (1983): Geothermal Reservoir
Engineering Lecture Notes. UNU Geothermal Training
Programme, Iceland, Report 1983-2, 250 pages.
Martinell! , R.e . and Nelson, D.B . (19118): Prediction of
Pressure Drop Duri n g Forced Circulation Boiling of Water.
ASME Trans •• 70. 695-702.
Michaelides, E. E. (1981) , Thermodynamic Properties of
Geothermal Fluids.
Vol 5. 361 - 36~.
Geothermal Resources Counsil, Trans.,
Michels, D.E. (1981), C02 and
to Geothermal Engineering .
Lawrence Berkeley Laboratory,
Carbonate Chem i stry Applied
Rep. LBL - 11509(GREMP - 15).
Berkeley, California .
Orkiszewski, J. (1967): Predicting Two-Phase Pressure Drop
in Vertical pipe. Jour. of Pet. Tech., 829 - 838.
Ramey, H.J.Jr. (1962): Well bore Heat Transmission . Jour. of
Pet. Tech . , 1127-1135 .
ROS, N.C.J. (1961): Simultaneous Flow of Gas - Liquid as
Encountered in Well Tubing. Jour. of Pet . Tech., 1037 - 10119.
Sutton, F.M . (1976) : Pressure-Temperature Curves for a
Two-Phase Mixture of Water and Carbon Dioxide. N.Z . J.Sci.,
19. 297-301.
37
Tan, E. (1982): Reservoir Characteristics of the Kizildere Geothermal Field. First Turkish-Italian Geothermal Energy
Seminar, Vcl 11, Comparative
and Cesano Geotherrnal Fields, Examination of the Kizildere (6-28 Sept.), Ankara.
38
•
2 • • • %
~ .
O~-------;,--------;,--------;o,-------~c-------co~ · o g ~ or g
~~ · , -. , -· , · . ·0 'u •
• • · !: .!! •
~'--------"o<' --------"O'"'-------;~------~'-------Co~= 8 \0 <D ~ ~
5. "S o
39
Diome!er
__ -,0_" __ -,-' '_' _ _ 2~" __ -,3~" __ -,4_' _ _ 5-,-" _ __ 6~" __ -,7_" __ ~8'_' __ ,-~"-=-(inche3]
<OE- C.::Ising (0.0 . 9~le")
Fig.2
, , , , 0" " 2" 3"
Svartsengi Well nO.4 Calcite deposi tion according to caliper log measured· 78.12 ,13
, , 4" ," 6" 7"
19.01 .2"-
3~O-
4~O
, , [inches] 8" 9"
B.SI1S J·S~Q,ts ... o;; "'18019
40
~JHD·HSb - 2300 - MP L.J::J 85.09.1180-00
o
100
200
300
E
-= 400 <> m
'" 500
600
700
800
10
Pressure (kg/cmZ)
o 30 40 50 60
o Measured
~ Calculated
. Figure 3. Pressure Profile in Svartsengi 'Well no. 4
70
.. • • ;; • ! ii:
• 0 •
r;T"=tJHD-HSI:J -230Q-MP ~85.09 . IIBI-'OD
'00
.0
60
"Or 31 kg/s
20
01 1
300 ' 40U 000 600
FlashlnQ Oepih rroll'! Wellhtad(lfI)
"-:: • 0 • • ~ · · 0 •
700
Figure 4. Change in Flashing Depth with Mass Flow Rale
200 •
060
020
.0
· \" • 0 • ~ • • •
o
\~ \;
..
o Calculated
.. Measured
Meo , ,,,red Value '
W(h / . )
32 . 6
53. " 2 01.0
WtlP{ba r)
16 . 8
14 .2 12. 8
0~1--r--r--r-~~'-~~--.---------6 • '0 .. '4 ,. " 20 22
WHP (bar)
Figure 5. Deliverabilily curves for SG- Il for different reservoir pressures
=
42
~JHD'HS~'2300'MP ~85.09.1182·OD
!! o 0:
~ ...
200~
160~
: 80 o ,.
40
.... SG-II 9 5/S"cosi rq
O~~--~--~--~~---r--~---------6 8 10 12 14 16 18 20
. WHP (ber)
Figure 6. Effect of Casing Size an the Output Curves af geathermal Wells
KO-6
Om 8"
40m 7" 47m 6"
112 m 5"
575 m 4"
~Flashing depth
655.63m ...
50m I--
Fig.7 Scaling thicknesses measured by go-devil in kizildere well no 6
~3
280 Net
260
240
220
200
180
160
140
120
100
80
60
40
20
o -o
. . production role (kg/s)
Production rate of We ll no. 10
1 -
-
- - . - - - - -N 0 J F M A M
1983
.
In jection --l
, -- , -J J
1984
. .
, -A s
. . . I NJECTION RATE
II -
. JUt I - , o N
Figure 8. Net Production and In jeclion ra tes with time
I
(kg/ s)
-- -
-o J
1985
~
~
45
-, ~
'" en ~
-,
) • •
" '" E -~ -~ • c: ~ 0
g • "0 ~ 0
z >-
'" 0 D D • oi '" " "' a:
~ " " '" ::J
"' Z <D
'" a: en ~ ;:) ~
'" • "' "' " "
<D '" ~ N 0 <D '" " N 0 <D '" ~ N 0 N N N N N ~ ~ ~ ~
~ JHO-HStl-2 30Q-MP ~ 95. 09. 1I05-'OD
Well, 4- 9, 11,12:
Two-phou
(OC) o ISO soo
or '00 ,. n
'. , '. r
r~
1000
1000
Figure 10. Conceptual Model of the Svorlsengl Reservoir
"
i~~~~~~I@ TWO-PHASE
~~~It ~~~ur\ 111 1111111 1 111 111111111 r I 11 I I I I lWO-PHASE WATER
INTERFACE
WATER
.,.-BOREHOLE
f-::.----=--=------~ :: :::-= !.E.!~~I.!.E_:" __ :
Figure 11. Schematic Representollon of Steam Model of the Svorlsenol Reservoir
c
'"
28 DRAWDOWN IHI
26
2.
22
20
18
16
,. 12
10
8
6
• 2
0 0 N
1983 0 J F H
+ MEASURED 6 CALCULATED
"I,,!,"" +
~ *'-"""'~> ....;:;;:; : ~ K' 125 da,. ~ + C - 51 E-9 m/ko # .~ c~; 2:5E- 1I m/kg/day
A H J J A s o N o 1984
J 1985
Figure. 12. Measured and Fitted Oro wdown from steam Model
~ ....,
48
"
:c= " -0 -
•
, , , , " . " " , 0
f , . ,g , ~
" < '~ ," ~ . g
E f
~
, , , , UUu
00 _ N
::: , " , . '. :f :.
g '" ' il " I f
," ,~ ,. '. • , " , " • '.
W N ~~~ ~. ~_N ~
~~~ ~ ~~~<~o~g!89~ ~~~ ~N~<~~ NQ_<N~%~~~2~_o _~ -~~H~ ~ ZHC~~CUUU~_CQ~UC~
o o
a-. g~ o· % •
~ ; f : ->--: =:= wo-
g : ..> -" w _
"w _ --ii: .-
..............
"
.. .. .. .. .. uuuuuuuuuuuuuuuuuvuuuuuuuuuuvuuuuuuuuuuuuu
: ,
, , , , , , , , i· , , , , ,
, UuU
, , , ,
, , , ,
" '-, ~ , . ," .. ,.
w , 0
'. • .. E
' " ,. .. :2 ,~ '. :~ , , , , uuu
. :; " . ~ " U
" -N
;t . , ;..: ~ ' <, w w,
t
w ..
, uu
, , , , , , , , , , , , , , , , , , , , , , , , , , ,
1 ~: I, : e '" ,
• •
0 :8' : ~ : .... ... ::;;:g i:ti~
! ~ : ~ ~:!& : :. (j . ... , '" , ,
: ( , , , , uuu uu
, , , , , , , , , , , , , , ' u ,
'~ : e " ' 8' : -' I :;; 1 ~ i ~ g : 1if ~ I ...
",tif ~ > c:. ' ~ • , >
, , , , uuu
:~ " '. ' f ,~ " ,. " I ~
:~ u ' M ,. ,
' U ~ •
, , uuu
, , , , , '. :~ e
, " '" ': ,g lE ,~
o I f ~ w . •
· " · • ~ w u e
" e ~ Q
~ ~ " ~ , . . ,. '~: ... ". .., .. ; !:>
uz ,~ , '" a~ I .... : ::l ~~ '~ : f ... ... : .. :"'" ;:;~ . e ! ~ <o:~ I ~ : ;
:;8 Cl ' ''' , ' ,
~uu.:. ,!, ... .:,
· •
· · · ;:; •
• . 0 ,,~
;:.=-· , ,. "-0, '. _u wU ;;' 6 :i~
, , , ,
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