A coupled thermal-hydro-mechanical simulation for carbon dioxide sequestration
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Transcript of A coupled thermal-hydro-mechanical simulation for carbon dioxide sequestration
Environmental Geotechnics
A coupled thermal-hydro-mechanical simulation for carbon dioxide sequestrationBao, Xu and Fang
Environmental Geotechnicshttp://dx.doi.org/10.1680/envgeo.14.00002Paper 14.00002Received 20/01/2014; accepted 31/07/2014Keywords: numerical methods/waste containment and disposal system
ICE Publishing: All rights reserved
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Herein, the authors present a coupled thermal-hydro-mechanical model, as an improvement of the isotherm hydro-
mechanical model in their previous work, for geological sequestration of carbon dioxide followed by stress, deformation,
and shear-slip failure analyses. This fully coupled model considers the geomechanical response, fluid flow and thermal
transport relevant to geological sequestration. Both analytical solutions and numerical approach by way of finite
element model are introduced for solving the thermal-hydro-mechanical model. Analytical solutions for pressure,
temperature, deformation and stress field were obtained for a simplified typical geological sequestration scenario by
assuming a simplified temperature profile in an aquifer. The finite element model is more general and can be used for
arbitrary geometry. It was built on an open-source finite element solver, Elmer, and was designed to simulate the entire
period of carbon dioxide injection both stably and accurately – even for large time steps. The shear-slip failure analysis
was implemented based on the numerical results from the finite element model. The analysis reveals the potential
failure zone caused by the fluid injection and thermal effect. From the simulation results, the thermal effect is shown
to reduce the potential failure zone, especially at the early time of the injection.
3 Yilin Fang PhD Scientist, Hydrology Technical Group, Energy and Environment
Directorate, Pacific Northwest National Laboratory, Richland, WA, USA
1 Jie Bao PhD Engineer, Experimental and Computational Engineering Group,
Energy and Environment Directorate, Pacific Northwest National Laboratory, Richland, WA, USA
2 Zhijie Xu PhD Scientist, Computational Mathematics Group, Fundamental and
Computational Sciences Directorate, Pacific Northwest National Laboratory, Richland, WA, USA
A coupled thermal-hydro-mechanical simulation for carbon dioxide sequestration
NotationCl fluid specific heat ((J/kg)/°C)Cs rock specific heat ((J/kg)/°C)
D dimensionless number, µθβ λ
=+ +
/1/( 2 )k
DG
Es rock volumetric thermal expansion (°C–1)F(l) integration of an exponential functionG shear modulus (Pa)g gravity acceleration (m/s2)Kl fluid thermal conductivity ((W/m)/°C))Ks rock thermal conductivity ((W/m)/°C))k permeability (m2)Ms rock bulk modulus (GPa)p pressure (Pa)pp pore pressure (Pa)�p scaling factor,
ψ µπ ρ
′=� 1
4p
k�( , )R r z position of point A
¢ ¢�
0( , )R r z position of centre of dilation′′ ′−�
0( , )R r z position of image of centre of dilationr horizontal distance from injection well (m)T temperature (°C)t injection time (s)�u mechanical displacement vector (m)uz vertical displacement (m)ur horizontal/radial displacement (m)z depth (m)b fluid compressibility (Pa−1)dij the Kronecker deltaeij strain componentg azimuthal anglel Lame’s constant (Pa)l dimensionless number, l = r2/(4Dt)m viscosity (Pa·s)q porosity
1 2 3
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Environmental Geotechnics A coupled thermal-hydro-mechanical simulation for carbon dioxide sequestrationBao, Xu and Fang
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r1 density of liquid (kg/m3)rs rock of liquid (kg/m3)rs density of the soil/rock (kg/m3)
r¢(r,z) distance between point A [ ( , )]R r z�
and centre of dilation 0[ ( , )]R r z¢ ¢
� as shown in Figure 4 (m)
r¢¢(r,z) distance between point A and the image of centre of dilation 0[ ( , )]R r z-¢¢ ¢
� as shown in Figure 4 (m)
σ� total stress tensor (Pa)
sh horizontal remote stress (Pa)ijσ ¢ effective stress component (Pa)
sv vertical remote stress (Pa)σ ′1 maximum principal effective stress (Pa)σ ′3 minimum principal effective stress (Pa)y external source term stands for the carbon dioxide
injection rate ((kg/m3)/s)y ¢ line injection rate (kg/m/s)
IntroductionIt is well known that carbon dioxide sequestration in deep saline
aquifers could be a promising mitigation method for reducing the
amount of carbon dioxide emitted into the atmosphere (Vilarrasa
et al., 2011). It is widely accepted that geothermal energy offers
clean, renewable, reliable electric power with no need for grid-
scale energy storage (Atrens et al., 2009, 2010). Recent research
has presented a novel approach of combining geothermal energy
capture with geologic carbon dioxide sequestration (Randolph and
Saar, 2011a, 2011b). Still, even without combining a geothermal
energy capture system, the temperature of injected carbon dioxide
is lower than the environment temperature in deep ground,
especially in areas with great amounts of geothermal resources.
Injection of carbon dioxide into a site often lasts a few decades,
and carbon dioxide is expected to be retained underground until
well past the end of the fossil fuel era; it could easily last several
hundreds of years or even longer than 1000 years (Holloway, 2005;
Wilson, 1992). Hence, geological injection and sequestration of
supercritical carbon dioxide intrinsically involve a number of
complicated physical and chemical processes that occur within
large spatial domains and extremely long periods of time.
Mathematical models and numerical simulation tools will play
an important role in evaluating and predicting the feasibility of
carbon dioxide storage in subsurface reservoirs, designing and
analysing field tests and designing and operating geologic carbon
dioxide disposal and geothermal extraction systems (Pruess et
al., 2004). In recent years, various thermal-hydro-mechanical
models and simulation tools (Gor et al., 2013; Preisig and Prévost,
2011; Simone et al., 2013; Vilarrasa et al., 2013) have been
applied to the study of geological carbon dioxide sequestration.
However, although a fully coupled 3D multiphase, multiphysics,
multicomponent computational model provides a relatively more
complete description of the problem, it is sometimes fragile because
of various computational challenges, such as the difficulties
in model parameter identification, process coupling, severe
heterogeneity and non-linearity (Xu et al., 2012). An analytical
solution to a simplified model of carbon dioxide sequestration
based on reasonable assumptions is much more efficient and can
uncover the critical relationship between injection conditions
and geomechanical response, which can help us understand
the mechanism and physical effects and provide guidance to
applications on the actual sites where the detailed parameters are
not yet well identified. The purpose of this paper is to present an
efficient model for understanding geomechanical response when a
deep geological formation is subjected to injection of substantial
supercritical carbon dioxide with thermal effects.
In this article, the authors first introduce a thermal-hydro-mechanical
model in ‘Thermal-hydro-mechanical model for carbon dioxide
geological sequestration’. The corresponding analytical solutions
of fluid pressure, temperature, deformation and stress fields for a
typical injection scenario are introduced in ‘Analytical solution for
the thermal-hydro-mechanical model’. A finite element solution,
based on an open-source solver, Elmer, is introduced in ‘Finite
element model for the thermal-hydro-mechanical model’, and
comparisons between analytical and numerical methods are shown
in ‘Comparison of finite element results with analytical solutions’.
‘Failure analysis and thermal effects’ describes the application of
geomechanical shear-slip failure analysis based on the coupled
thermal-hydro-mechanical model to estimate the potential damage
zone during carbon dioxide injection.
Thermal-hydro-mechanical model for carbon dioxide geological sequestrationThe authors’ previous works (Bao et al., 2013a; Xu et al., 2012)
introduced the isothermal hydro-mechanical model companion
with both analytical and numerical solutions for carbon dioxide
geological sequestration. To make the model analytically solvable
and more computationally efficient in numerical simulation,
the flow was assumed as single phase, although carbon dioxide
injection is a multiphase system. Therefore, a carbon dioxide–brine
multiphase subsurface flow simulation, subsurface transport over
multiple phases (STOMP) (White and Oostrom, 2006), was used to
validate the proposed single-phase model in the authors’ previous
works (Bao et al., 2013a, 2013b, 2014), and it was shown that the
single-phase model can capture the characteristics of the pressure
evolution of the carbon dioxide–brine multiphase system in an
aquifer layer, because the pressure evolves more rapidly than flow
transport. In addition, the capillary pressure for supercritical carbon
dioxide and brine is on the order of 103–10
4 Pa (Tokunaga et al.,
2013), while the injection pressure is often higher than 106 Pa; so
the capillary pressure is negligible for the carbon dioxide injection
system, and therefore, the single-phase model is an appropriate
approximation of the carbon dioxide–brine flow system for
estimating the pressure evolution in the aquifer layer. Based on
the single-phase isothermal model in the authors’ previous work
(Bao et al., 2013a; Xu et al., 2012), the thermal effect is involved,
which makes the thermal-hydro-mechanical model include fluid
flow, heat transfer and linear elasticity equations that describe the
geomechanical reaction to fluid injection flow. The coupled hydro-
mechanical model (Biot, 1935, 1941, 1955, 1956, 1962; Terzaghi,
1923; Yin et al., 2010, 2011) reads
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Environmental Geotechnics A coupled thermal-hydro-mechanical simulation for carbon dioxide sequestrationBao, Xu and Fang
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1.
2
1
1 ( ) ψθβ θµβ θρ β
∂ ∂ ∇ ⋅+ = ∇ +∂ ∂
�p u k
p
t t
2.
1 1 1
2
1
[(1 ) ]
[(1 ) ]
θ ρ θρ ρ
θ θ
1¶- + + Ѷ
= - + Ñ
�s s
s
TC C C v T
t
K K T
3. 2
( ) ( )λ + ∇ ∇⋅ + ∇ = ∇ + ∇� �
s sG u G u p M E T
Equation 1 is a fluid flow continuity equation in terms of the pore
pressure p in Pascals, and the units for all parameters are listed in
Table 1 and in Notation. In Equation 1, t is the injection time, u
�
is the mechanical displacement vector in metres, q is the porosity,
b is the compressibility, m is the viscosity, k is the permeability,
r1 is the density of liquid and y is the external source term that
stands for the carbon dioxide bulk injection rate in kilograms per
cubic metre per second. Equation 2 is a heat transfer equation
for temperature field T in degree Celsius. In Equation 2, C1 and
Cs are the heat capacity for liquid and solid parts, respectively.
K1 and Ks are the thermal conductivity for liquid and solid parts,
respectively. rs is the density of solid soil/rock.
�v is the Darcy flux
and is calculated by
4. .
µ= − ∇� kv p
Because the single-phase model is assumed, there is no vertical
gradient of injection-induced pressure in an aquifer, and therefore,
the effects of gravity are neglected. Equation 3 is a Navier-type
elasticity equation in terms of the displacement vector
�u. In
Equation 3, for solid rock or soil, G is the shear modulus, l is
Lamé’s constant, Es is the volumetric thermal expansion coefficient
and Ms is the bulk modulus. Equations 1–3 are valid for arbitrary
geometry and boundary conditions. In the following sections, an
analytical and a numerical solution using finite element method are
introduced.
Methodology
Analytical solution for the thermal-hydro-mechanical modelFor arbitrary geometry and boundary conditions, it is difficult to
get a general analytical solution for Equations 1–3. However, based
on the analytical solution for pressure introduced in the authors’
previous work (Bao et al., 2013a; Xu et al., 2012), Equation 1 can
be solved analytically by ignoring the effects of the thermal stress
term (MsEsÑT) on the pressure-equivalent diffusion coefficient. The
numerical simulation results show that the effects of the thermal
stress term on pressure evolution are very limited; ignoring it in
order to make the system analytically solvable is reasonable, and
the details are shown in ‘Comparison of finite element results
with analytical solutions’. In a simplified practical carbon dioxide
geological sequestration in an axisymmetric coordinate system, as
shown in Figure 1, r is the radial axis, and z is the vertical axis. The
carbon dioxide injection well is located at r = 0 m, and the ground
surface is at z = 0 m. Carbon dioxide is injected into a confined
aquifer formation to a depth between z1 and z2. The permeability
of the caprock and the base rock is assumed to be small enough to
confine the fluid flow. The analytical solution of pressure field is
5. ( )λ= �p pF ,
Lamé’s constant, l: GPa 14Shear modulus, G: GPa 14Permeability of aquifer layer, k: m2 10−13
Permeability of caprock and base rock, k: m2 0Line injection rate, y : (kg/m)/s 0·7, 2·0 and 3·5Porosity, q: dimensionless 0·1CO2 thermal conductivity, Kl: (W/m)/°C 0·087Rock thermal conductivity, Ks: (W/m)/°C 2·1CO2 specific heat, Cl: (J/kg)/°C 2200Rock specific heat, Cs: (J/kg)/°C 1000Fluid density, rl: kg/m3 1000Rock density, rs: kg/m3 2600Fluid viscosity, μ: Pa·s 10−3
Fluid compressibility, b: Pa−1 10−9
Rock volumetric thermal expansion, Es: °C−1 3·6 × 10−5
Rock bulk modulus, Ms: GPa 23
Table 1. Material properties
Z
γ
r
CO2
Z1
Z2 Injection zone Base
Caprock
Injection well
Figure 1. Sketch of the geometry configuration for carbon dioxide injection
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Environmental Geotechnics A coupled thermal-hydro-mechanical simulation for carbon dioxide sequestrationBao, Xu and Fang
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where the dimensionless number λ = r2/(4Dt), and the equivalent
diffusion coefficient /
1/( 2 )
µθβ λ
=+ +
kD
G
. This equivalent diffusion
coefficient ignores the effects of thermal stress as mentioned above.
F(λ) is the integration of an exponential function, defined as
6. ( ) / .
λλ
¥ - ¢= ¢ ¢ò t
F e t dt
The scaling factor �p is defined as
7.
1,
4
p
k
ψ µπ ρ
¢=�
where ψʹ is a line injection rate in kilograms per metre per second.
Details of the analytical solution were introduced in the authors’
previous works (Bao et al., 2013a; Xu et al., 2012).
With the solution for the pressure field, the Darcy flux can be calculated
from Equation 4, which is facilitated by solving Equation 2 for the
temperature-change field T. It is difficult to achieve an analytical
solution for Equation 2 with a time- and space-dependent Darcy
flux distribution, even in the axisymmetric system. The temperature
variation along the vertical axis z is quite small, so the temperature
profile is assumed to be a function of radial r and time t. Figure 2
shows the finite element method simulation results for the proposed
coupled system (Equations 1–3) in an axisymmetric geometry after
10 years of injection with the injection rate of 3×5 (kg/m)/s. Because
the single-phase model slightly overestimates the pressure near the
injection well (Bao et al., 2013b), the Darcy flux is overestimated
as well near the injection well. Therefore, the contribution of the
convection term (1 1C vρ�ÑT ) is also slightly overestimated compared
with the results in Randolph and Saar’s work (Randolph and Saar,
2011a). The geothermal gradient is 25–30°C per kilometre depth
(Fridleifsson et al., 2008), so the temperature of the brine and the
rock in an aquifer (around 2500 m deep) is around 90°C, and the
injected supercritical carbon dioxide is around 15°C. The proposed
model neglects the phase change of supercritical carbon dioxide in an
aquifer with temperature variation. It is assumed that the temperature
of injected carbon dioxide is 75°C lower than the environment
temperature in an aquifer at the injection point, so T = −75°C at the
injection well and T = 0°C in the rest of the investigated domain at the
beginning of injection. Compared with the length scale of the carbon
dioxide geological sequestration problem, the gradual temperature
transition, from T = − 75°C to T = 0°C is negligible as shown in
the simplified solution in Figure 2. Hence, the analytical solution for
Equation 2 in the aquifer layer (z2 ≤ z ≤ z1) is assumed to be
8. 75 C 0 , and 0 C for ,T for r L T r L= - ° £ £ = ° >
where L represents the area that temperature is cooled by the
injected cold carbon dioxide. The authors call this ‘progression
distance’ of the temperature difference (shown in Figure 2), and it
can be expressed as
9. 0
( , ) .
t
L v L t dt= ò�
Figure 3 shows the numerical integration of Equation 9 compared
with the finite element method simulation results for the fully
coupled system (Equations 1–3) at different injection rates (0·7
and 3·5 (kg/m)/s). The distance, L, calculated from Equation 9, can
match the finite element simulation result fairly well, which means
that the simplified solution can represent the temperature evolution
in the aquifer layer accurately. With the solution for the pressure
and temperature field, the displacement field can be solved from
Equation 3 with displacement boundary conditions
10. r r 0 r r z r r z z z| 0, | 0, | 0, | 0, | 0u u u u u= =¥ =¥ =-¥ =-¥= = = = =
Solving Equation 3 requires finding the elastic field of a centre
of dilation 0( , )′ ′�R r z (due to the pressure and thermal stress at the
centre) (Davies, 2003; Mindlin and Cheng, 1950a, 1950b; Sen,
1951) in a semi-infinite solid (Figure 4). The vertical displacement
solution uz is
11.
2
1
0 s s 0
0 0
2
0 03 3 5
1[ ( , ) ( , )]
2 ( 2 )
(1 4 ) (3 4 ) 6 ( ),
z
z
z
u p r t M E T r t
G
z z v z v z z z zr dz d dr
π
π λ
γρ ρ ρ
¥= +
+
é ù- - + - +¢ ¢ ¢- - ¢ê ú¢ ¢¢ ¢¢ë û
ò ò ò
and the radial displacement ur is
12.
2
1
r 0 s s 0 0
0 0
0 03 3 5
1[ ( , ) ( , )]( cos )
2 ( 2 )
1 (3 4 ) 6 ( ),
z
z
u p r t M E T r t r r
G
v z z zr dz d dr
πγ
π λ
γρ ρ ρ
¥= + -
+
é ù- + ¢- - ¢ê ú¢ ¢¢ ¢¢ë û
ò ò ò
Temperature distribution in aquifer layer
FEM simulation result
Simplified solution
0–80
–70
–60
–50
–40
Tem
pera
ture
: °C
–30
–20
–10
0
200
L
400 600r: m
800 1000 1200 1400
Figure 2. Temperature distribution in an aquifer layer for finite element simulation results and simplified solution
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Environmental Geotechnics A coupled thermal-hydro-mechanical simulation for carbon dioxide sequestrationBao, Xu and Fang
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where, as shown in Figure 4,
13. 2 2 2
0 0( , ) ( ) 2 cosρ γ′ ′ ′= − = − + + −
� �r z R R z z r r rr
is the distance between point A [ ( , )
�R r z ] and centre of dilation
[ 0( , )R r z¢ ¢�
]. g is the difference of the azimuthal angle between point
A and the dilation centre.
14. 2 2 2
0 0( , ) ( ) 2 cosρ γ′′ ′′ ′= − = − + + −
� �r z R R z z r r rr
is the distance between point A and the image of centre of dilation
image [ 0( , )′′ ′−�R r z ]. With known displacement, the strain component
eij is related to the displacement vector u
� through the geometry
relationship for small deformation elasticity, where
15. ij i j j i( )/2u uε = ¶ + ¶ .
For a homogeneous, isotropic, linear elastic solid, effective stress
component σ ′ij is related to the strain component eij through
16. ij kk ij ij2 ,Gσ λε δ ε= +¢
where dij is Kronecker’s delta and ekk follows the standard Einstein
summation. In geomechanics, the stress is positive in compression,
so the effective stress tensor is defined as
17. σ σ′ = −�� �
pI ,
where σ� is the total stress tensor.
Finite element model for the thermal-hydro-mechanical modelThe analytical solution for displacements and stresses near the
aquifer layer is not available because of singularity problem for
′−� �R R close to 0 (as shown in Equations 12 and 13). In addition,
the analytical solution is only available for simplified cases with
axisymmetric geometry, completely impermeable caprock and
base rock and homogeneous aquifer and rock properties. To solve
the coupled thermal-hydro-mechanical model (Equations 1–3) for
more general and practical cases, the authors used the open-source
multiphysics finite element solver, Elmer, to compute the pressure,
temperature, deformation and stress field for the proposed coupled
0 2 4
Time: year
6 8 10
0
100
Dis
tanc
e, L
: m
200
300
400
500
600
Progression distance of temperature
3·5 (kg/m)/s analytical
3·5 (kg/m)/s FEM
0·7 (kg/m)/s analytical
0·7 (kg/m)/s FEM
Figure 3. Comparison of progression distance of temperature between finite element solution and analytical solution
Z
r
A
Centre of dilation
Image of centre of dilation
R¢ (r0,z ¢)
R¢¢ (r0,–z¢)
R (r,z)
ρ¢
ρ¢¢
γ
Figure 4. Sketch of the centre of dilation and its image in the cylindrical coordinate system
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Environmental Geotechnics A coupled thermal-hydro-mechanical simulation for carbon dioxide sequestrationBao, Xu and Fang
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system. Elmer applies standard Galerkin finite element method
and residual square method for stabilisation (CSC – IT Centre for
Science, 2011; Franca and Frey, 1992; Franca et al., 1992). For this
study, the advection–diffusion equation solver, flux/gradient solver
and linear-elastic solver are used; a few user-defined codes are
developed to couple the different solvers together (CSC – IT Centre
for Science, 2011), and the detailed simulation steps are as follows.
(a) Use an advection–diffusion equation solver to solve the
pressure-change field p from Equation 1.
(b) Use a flux/gradient solver to solve the pressure gradient Ñp
and calculate the Darcy flux from Equation 4.
(c) Use a user-modified advection–diffusion equation solver to
solve the temperature-change field T from Equation 2 with
Darcy flux as advection effect.
(d) Apply the pressure gradient and thermal stress into Equation 3
as a source term.
(e) Use a linear-elastic solver to get the displacement field,
�u.
(f ) Use a divergence solver to get the transient of displacement’s
divergence term ( )∂ ∇ ⋅∂
�u
t
.
(g) Apply the term ( )∂ ∇ ⋅∂
�u
t
into Equation 1 as an additional
negative source term.
For an explicit coupled transient problem, Elmer can iterate (a)–(g)
substeps within each time step for convergence. Because of this
feature, a relatively large-size time step can be applied in this case,
such as over 1 year. For comparison against analytical solutions,
the geometry of a typical injection (Figure 1) was used in the
finite element study with horizontal bottom boundary and vertical
boundary, which is far away from the asymmetric axis, set at
−164 816 and 80 000 m, respectively, to mimic the semi-infinite
domain boundary conditions (Equation 10). Figure 5 shows a
typical 2D planar mesh with mesh refinement close to the injection
well and aquifer layer for solving the axisymmetric problem. The
actual model contains approximately 150 000 quadratic elements
after the mesh convergence study to achieve balance between
efficiency and accuracy. The aquifer layer is from z1 = −2242 m
to z2 = −2742 m, which is simplified from the sample structure in
Illinois Basin – Decatur (Gollakota and McDonald, 2012).
Results
Comparison of finite element results with analytical solutionsAs introduced in ‘Analytical solution for the thermal-hydro-
mechanical model’, the equivalent diffusion coefficient does not
include the effects of thermal stress, so the pressure distribution
is examined in both analytical and finite element results. The
line injection rate is 0·7 (kg/m)/s, and the material properties and
parameters are listed in Table 1, which is summarised from the
samples in Illinois Basin – Decatur (Gollakota and McDonald,
2012). The fluid density in the aquifer layer varies from about
600 kg/m3 (supercritical carbon dioxide) to approximately 1000 kg/
m3 (water) in the multiphase system. The 1000-kg/m
3 water density
was used in the proposed single-phase model because the water
still occupies the major part of the aquifer layer after 10 years of
injection. Similarly, the viscosity (10−3
Pa×s) and compressibility
(10−9
Pa–1
) of water are used for the fluid in the aquifer. The
analytical solutions of displacements (Equations 11 and 12)
require homogeneous mechanical properties, and the effects of the
variation in mechanical properties on geomechanical response are
very limited (Bao et al., 2013b, 2013c), so the same values are used
for the whole calculation domain. For comparison, the permeability
of caprock and base rock is set to 0. Figure 6 shows the comparison
of the pressure distribution after 10 years of injections along the
centreline of the aquifer layer (z = −2492 m). The size of the time
step is set to 1 year, and the coupled system is iterated 5 to 10 times
in each time step to converge. The pressure distribution can match
the numerical simulation result very well, which solves the fully
coupled system. It means that the impact of the thermal stress on
hydraulic pressure evolution can be neglected. Ground surface
displacements are critical parameters that can be used to monitor the
potential hazard caused by carbon dioxide sequestration activities.
Colesanti and Wasowski’s (2004) work shows that a ground surface
movement velocity of about 10 mm/year has a high probability of
80 km
Z
rCO2 injection
Base: –2742 to –164 816 m
Aquifer: –2242 to –2742 mCaprock: –2044 to –2242 m
Upper: 0 to –2044 m
Figure 5. Sketch of the mesh for Elmer finite element simulation
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Environmental Geotechnics A coupled thermal-hydro-mechanical simulation for carbon dioxide sequestrationBao, Xu and Fang
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inducing severe damage in buildings. For investigating thermal
effects, the authors examine displacement at the top surface (z = 0 m)
with and without thermal stress. Figure 7 shows the comparison of
the displacement at the top surface after 10 years of injections. The
thermal effects reduce about 9% of the vertical displacement near
the injection well because lower temperature near the injection well
causes shrinkage. Here, agreement between analytical and finite
element results is very good, although only a simplified temperature
field solution was used for the analytical solution (Equations 8 and
9). For the area with less geothermal resources or injection point
located less deep, the thermal effects on the ground surface vertical
displacement may not be as large as the example shown here. The
detailed thermal effects on stress distribution and shear-slip failure
are discussed in the following sections.
r : km0
0
2
468
10
12
Pres
sure
: MPa 14
1618
20
5 10 15 20 25
FEM
Analytical
Pressure in aquifer layer after 10 years
30 35 40
Figure 6. Comparison of the pressure at the centre of the aquifer layer between finite element simulation and analytical results
00
0·002
0·004
0·006
0·008
0·010
0·012
0·014
0·016
Radi
al d
ispl
acem
ent:
m
0·018
0·020
0·01
0·02
0·03
0·04
Vert
ical
dis
plac
emen
t: m
0·05
0·06
0·07
(a)
5
Analytical no thermal stress
Analytical with thermal stress
FEM no thermal stress
FEM with thermal stress
Analytical no thermal stress
Analytical with thermal stress
FEM no thermal stress
FEM with thermal stress
Displacement at the top surface after 10 years
Displacement at the top surface after 10 years
10 15
(b)
r: km
20 25 30 35 40
0
0
5 10 15
r : km
20 25 30 35 40
Figure 7. Comparison of the displacement between Elmer and analytical results; (a) vertical displacement at the top surface (z = 0 m); (b) radial displacement at the top surface (z = 0 m)
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Failure analysis and thermal effectsSome shear-slip analysis is conducted using principal stress
magnitudes and orientations with respect to pre-existing fault
planes and fluid pressure within the fault plane (Morris et al., 1996;
Streit and Hillis, 2004; Wiprut and Zodack, 2000). Because the
location and orientation of pre-existing faults underground may
not be well known, the shear-slip failure analysis discussed in this
article assumed that a fault could exist at any point with an arbitrary
orientation, which might be useful as a precaution (Rutqvist et
al., 2007). In this analysis, the authors assume that cohesion is 0
and friction angle is 30° (Rutqvist et al., 2007). The null cohesion
assumption of the pre-existing faults may cause overestimation of
the risk of failure, which is usually favourable when the cohesion
situation is not clear. Thus, the criterion for shear slip is BC BC³¢
in the Mohr circle (shown in Figure 8), and the criterion for the
stress is
18. 1 3 1 3
3 1 3sin 30 3
2 2
σ σ σ σσ σ σ′ ′ ′ ′+ +′ ′ ′− ≥ ° ⋅ → ≥ ,
where σ1́ is the maximum principal effective stress and σ3́ is the
minimum principal effective stress. As shown in Figure 9, remote
stresses are applied to the entire simulation area. The vertical
remote stress is the lithostatic stress sv = rsg|z|, where g is gravity
and |z| is depth. Horizontal remote stress (sh) varies with different
subsurface formations and locations. Generally, a small sh is more
likely to cause tensile failure than shear-slip failure. Thus, in all
the simulations described here, a relatively large horizontal remote
stress sh = 1·5sv (Rutqvist et al., 2007) was used to lead more
easily to shear-slip failure. Because the proposed model (Equation
3) and the failure criterion (Equation 18) are based on elastic theory,
no fracture is actually initiated, and there was no redistribution of
stresses due to failure. It means that once a considerable failure
zone appears in the simulation domain, fractures are highly possibly
initiated, and the continuum material model may not be accurate
enough, so the simulations in this study are all limited to 3 years.
The applied shear-slip failure criterion offers an easy and efficient
way to estimate the potential risk of the injection well under desired
operation conditions. Figures 10, 11 and 12 show the contour of
σ1́–3σ3 MPa after 1 and 3 years of carbon dioxide injection with
a line injection rate ψʹ = 0·7, 2·0, 3·5 (kg/m)/s. The area marked
by a black line is the zone where σ1́ > 3σ3́, namely, where shear-
slip failure can possibility occur if a pre-existing fault is located
in that zone. The injected cold carbon dioxide causes shrinkage
and reduces pressure in the aquifer layer near the injection well
(Yin et al., 2011), so the thermal effects significantly change the
distribution of the failure zone as well as reduce the failure zone
in the aquifer layer for the high injection rate cases (2·0 and 3·5
(kg/m)/s shown in Figures 11 and 12. It was believed that failure in
the aquifer can enhance the injectivity because the fault increases
the porosity and permeability of the aquifer formation (Flekkøy et
al., 2002). However, frequent or continuous failure possibly causes
considerable seismic activity, which may lead to ground building
or facility damage. Therefore, necessary attention should be paid
to the failure zone in the aquifer to avoid considerable ground
surface damage, although it probability enhances the injectivity.
From this point, the thermal stress can possibly reduce the risk of
injection. However, thermal stress also causes small failure zones
in the caprock and the base rock near the aquifer layer, because the
shrinkage in the aquifer layer may reduce the compression stress
in the caprock and the base rock. In addition, for the low injection
rate case (0·7 (kg/m)/s), the hydraulic pressure does not cause any
failure zone, while the thermal effect causes small failure zones in
the caprock and the base rock (Figure 10). Generally, the possible
failure zone in the caprock means the fracture may be activated in
the caprock, which may lead to carbon dioxide leakage, and this
definitely impacts the injectivity. It is unavoidable that the thermal
effects influence stress distribution during carbon dioxide injection
in both the geological sequestration geothermal capture combined
system and the solo carbon dioxide storage system. Coupling the
thermal effect into the hydro-mechanical model can more closely
predict the displacement, stress distribution and possible failure
Effective normal stress
Shea
r st
ress
A
30˚
B
C
C¢
σ ¢3 σ ¢1
Shear-slip failure
Figure 8. Stress state represented by Mohr circles for failure analysis
Remote stress
Local stress
σhσh
σv
σz
σr
σz
σr
Figure 9. Sketch of remote stress
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Environmental Geotechnics A coupled thermal-hydro-mechanical simulation for carbon dioxide sequestrationBao, Xu and Fang
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0
–2742
–2242
–120·0σ ¢1–3σ ¢3: MPa
–87·50
–55·00
–22·50
10·00
1 year
with thermal stress
Line injection rate: 0·7 kg/m.s
Dep
th, z
: m
500 1000
(a)
1500r: m
2000 2500 0
–2742
–2242
1 year
10·00
–22·50
–55·00
–87·50
–120·0
no thermal stress
Line injection rate: 0·7 kg/m.s
Dep
th, z
: m
500 1000
(b)r: m
1500 2000 2500
σ ¢1–3σ ¢3: MPa
–2742
0 500 1000
(c)
r: m1500 2000 2500
–2242
3 years
with thermal stress
Line injection rate: 0·7 kg/m.s
Dep
th, z
: m
10·00
–22·50
–55·00
–87·50
–120·0
σ ¢1–3σ ¢3: MPa
0
–2742
–2242
Dep
th, z
: m
500 1000
(d)
r: m1500 2000 2500
10·00
–22·50
–55·00
–87·50
–120·0
σ ¢1–3σ ¢3: MPa
3 years
no thermal stress
Line injection rate: 0·7 kg/m.s
Figure 10. Contour of σ ¢1–3σ ¢3 MPa for injection rate y ¢ = 0·7 (kg/m)/s. The area marked by the black line is the zone σ ¢1 > 3σ ¢3, which means the shear-slip failure would occur in high potential.
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Environmental Geotechnics A coupled thermal-hydro-mechanical simulation for carbon dioxide sequestrationBao, Xu and Fang
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−2242
−2742
0 500 1000
(a)
1500 2000 2500r: m
Dep
th, z
: m
Line injection rate: 2·0 kg/m.s
with thermal stress
1 year
10·00
−22·50
−55·00
−87·50
−120·0σ ¢1–3σ ¢3: MPa
−2242
−2742
0 500 1000
(b)
1500 2000 2500r: m
Dep
th, z
: m
Line injection rate: 2·0 kg/m.s
no thermal stress
1 year
10·00
−22·50
−55·00
−87·50
−120·0σ ¢1–3σ ¢3: MPa
−2242
−2742
0 500 1000
(c)
1500 2000 2500r: m
Dep
th, z
: m
Line injection rate: 2·0 kg/m.s
with thermal stress
3 years
10·00
−22·50
−55·00
−87·50
−120·0σ ¢1–3σ ¢3: MPa
−2242
−2742
0 500 1000
(d)
1500 2000 2500r: m
Dep
th, z
: m
Line injection rate: 2·0 kg/m.s
no thermal stress
3 years
10·00
−22·50
−55·00
−87·50
−120·0σ ¢1–3σ ¢3: MPa
Figure 11. Contour of σ ¢1–3σ ¢3 MPa for injection rate y ¢ = 2·0 (kg/m)/s
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Environmental Geotechnics A coupled thermal-hydro-mechanical simulation for carbon dioxide sequestrationBao, Xu and Fang
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−2242
−2742
0 500 1000
(a)
1500 2000 2500r: m
Dep
th, z
: m
Line injection rate: 3·5 kg/m.s
with thermal stress
1 year
10·00
−22·50
−55·00
−87·50
−120·0σ ¢1–3σ ¢3: MPa
−2242
−2742
0 500 1000
(b)
1500 2000 2500r: m
Dep
th, z
: m
Line injection rate: 3·5 kg/m.s
no thermal stress
1 year
10·00
−22·50
−55·00
−87·50
−120·0σ ¢1–3σ ¢3: MPa
−2242
−2742
0 500 1000
(c)
1500 2000 2500r: m
Dep
th, z
: m
Line injection rate: 3·5 kg/m.s
with thermal stress
3 years
10·00
−22·50
−55·00
−87·50
−120·0σ ¢1–3σ ¢3: MPa
−2242
−2742
0 500 1000
(d)
1500 2000 2500r: m
Dep
th, z
: m
Line injection rate: 3·5 kg/m.s
no thermal stress
3 years
10·00
−22·50
−55·00
−87·50
−120·0σ ¢1–3σ ¢3: MPa
Figure 12. Contour of σ ¢1–3σ ¢3 MPa for injection rate y ¢ = 3·5 (kg/m)/s
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Environmental Geotechnics A coupled thermal-hydro-mechanical simulation for carbon dioxide sequestrationBao, Xu and Fang
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zone to the practical cases than models that neglect non-isothermal
effects, especially in areas that contain high geothermal resources.
The proposed model can efficiently predict the sustainability of
the injection site and can uncover the critical relationship between
injection conditions and geomechanical response when the detailed
properties and parameters are not yet well identified.
Discussions and conclusionsBased on an isothermal hydro-mechanical model in the authors’
previous works (Bao et al., 2013a; Xu et al., 2012), a thermal-
hydro-mechanical model was developed. The companion analytical
solution and a finite element approach were introduced for solving
the proposed model and were compared against each other. By
neglecting the thermal stress impacts on pressure evolution and
assuming a simplified temperature profile in an aquifer, the model
was analytically solved for a simplified carbon dioxide injection
case, and the assumptions were shown to be reasonable by
comparing with finite element numerical simulation results. The
analytical solution can be used to quantitatively evaluate the typical
sequestration problem instantly, while the finite element model
can be applied in more practical cases and can offer more detailed
results. A shear-slip failure analysis was conducted based on
numerical results. The analysis provides the potential failure zone
and can be used to estimate the maximum sustainable injection
rate and temperature. Thermal effects on deformation and potential
shear-slip failure were quantitatively investigated. Generally,
shrinkage caused by the cooling effects near the injection well
helps on delaying reactivation of pre-existing fault in an aquifer
layer, especially during early well life. However, it will cause small
fractures in the caprock and the base rock near the aquifer layer.
Using the authors’ thermal-hydro-mechanical model instead of
neglecting thermal effects can predict the deformation and fracture
more closely when compared with real applications.
AcknowledgementThis research was funded and conducted through the Pacific
Northwest National Laboratory (PNNL) Carbon Sequestration
Initiative, which is part of the Laboratory Directed Research and
Development Program. PNNL is operated by Battelle for the U.S.
Department of Energy under Contract DE-AC05-76RL01830.
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WHAT DO YOU THINK?
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