Int J Adv Eng Sci Appl Math
https://doi.org/10.1007/s12572-020-00257-7
IIT, Madras
Comparison of fractional flow reserve value of patient-specific left
anterior descending artery using 1D and 3D CFD analysis
Supratim Saha1 • T. Purushotham1 • K. Arul Prakash1
Ó Indian Institute of Technology Madras 2020
Abstract Coronary heart disease is a primary source of
mortality in India and around the globe. There are different
types of disease state, but the primary focus of this study is
on the disease where there is a narrowing down of the
lumen area in the blood vessel. The left anterior descending
artery is under investigation, which is a part of the left
coronary artery, and it delivers the heart muscles with
blood. The stenosed coronary artery impedes the blood
flow and triggers heart failure. In a mild situation, medicine
can be prescribed, but in severe cases, surgery is required.
The cases which fall between mild and severe are a
dilemma to the doctor for taking clinical decisions. The
fractional flow reserve (FFR) tells us about the functional
acuteness of stenosed coronary artery in this situation. The
patient-specific left anterior descending artery of a human
arterial tree is numerically investigated based on computational fluid dynamics approach for quantifying the functional acuteness of stenosis in terms of FFR. The CAD
models of patient-specific geometries are generated from
multislice computed tomographic scan data obtained from
various Indian patients. The simulation of the 3D model is
done using finite volume-based solver in OpenFOAM.
Similarly, the 1D stenosed artery is generated using an
analytical equation, and the solution is obtained using
locally conservative Galerkin method. A comparative study
of FFR between 3D and 1D models is carried out in this
study, and a correlation is proposed among 3D FFR, 1D
FFR and different geometric attributes.
& K. Arul Prakash
arulk@iitm.ac.in
1
Department of Applied Mechanics, Indian Institute of
Technology Madras, Chennai, India
Keywords Coronary heart disease Coronary lesion
Computational fluid dynamics Fractional flow reserve
1 Introduction
Atherosclerotic heart disease is a condition that causes
about 20 million loss of life worldwide. The number of
deaths associated with CHD in India went up from 17% in
2001–2003 (26 per cent in adults) to 23% in 2010–2013
(32% in adults) [1]. Any quick and precise approach of
diagnosing defects in the coronary artery will, therefore,
boost its succession planning, including clinical therapy
anywhere in the world. For very critical coronary occlusions, it is often straightforward to make angioplasty or
more effective surgical repair processes. Medication is a
pervasive way to treat the mild situation of coronary artery
disease. Nevertheless, most of the CHD cases fall between
very mild and serious cases. It creates a quandary situation
for clinicians to determine the safest option in this scenario.
Fractional flow reserve (FFR) is the coronary stenosis
pressure ratio used as a diagnostic measure to assess the
severity. Pd is the distal pressure of the stenotic lesion, and
Pp is the proximal pressure of the stenotic lesion [2]
FFR ¼
Pd
:
Pp
ð1Þ
Patient’s diagnostic technique for determining stenosis
seriousness is intrusive. The process requires insertion of a
wire probe in a patient’s blood vessel and sending it for
examination to the stenosis site. Ultimately, pressure
values are assessed across the stenosis to quantify the
seriousness of the blockage. However, because of its an
intrusive process, FFR measurement can be involved with
clinical complications, such as blood vessel rupturing, and
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Int J Adv Eng Sci Appl Math
is not only unsuitable for monitoring medically treated
stenoses, but also for cost implications [3]. A computed
tomography angiogram (CTA) acquires 3D images of the
beating heart and larger blood vessel of patients. This 3D
picture is replicated, and computational calculations are
carried out to predict the FFR value on the created 3D
artery model. There is no risk associated with this
treatment as it is non-intrusive. Although 3D modeling
predicts FFR performance close to that achieved
employing the intrusive wire insertion method, the time
needed for computations is massive because it incorporates
for the realistic stenosed configuration and also considers
the integration of terminal vessels as a lumped model into
the 3D computational domain, which is responsible for the
overall computing expense. The numerical simulation is
done to conduct complete arterial network with the
stenosed condition in one of the blood vessels, and with
reasonably good precision 1D simulation can model such
accuracy at a low computational cost. The guiding
equations which govern flow of blood through the artery
were provided by Sherwin et al. [4]. A complete 1D
numerical model of arterial flow was considered by taking
into account of the connections between the systemic
circulatory system and coronary flow developed by Mynard
and Nithiarasu [5] and also incorporated a model of the
heart in the arterial circulation for numerical simulation.
Almost all the earlier research includes a 3D computational
model to calculate FFR.
However, 3D numerical study require a great deal of
computational cost, while 1D simulations not only comparatively require less time and but also less cost. Iguchi
et al. [6] clinically investigated the effect of lesion size on
functional severeness for intermediate coronary stenosis
and found that lesion size has clinical importance in
intermediate-grade coronary stenosis. Different authors
have clinically investigated the importance of lesion size
on the severeness of the stenosed artery, but there has been
no significant computational study reported. Due to the
effect of the size of the lesion, there is a dearth of comprehension about intermediate level stenosis. A comprehensive study of the hemodynamics parameter is needed
due to the concurrent effect of blockage percentage and the
length of lesion. Several studies were conducted using
either 1D simulations or 3D simulations for FFR computing, but there are very few comparative studies that take
together 1D and 3D models. Etienne et al. [7] perform a
comparative work of 1D model and 3D model for arterial
blood flow for hemodynamic parameters. Due to the
enormous simulation time for full-scale 3D model, a
comparison between 1D model and 3D model for patientspecific cases is necessary to determine the functional
seriousness of stenosis using the FFR values. For different
geometric attributes of coronary stenosis, hemodynamic
123
parameters are evaluated in this study. The comparative
study of 1D FFR and 3D FFR values in the left anterior
descending arteries is also performed. Error investigation is
being studied between the two models. A correlation
between 1D and 3D result will be proposed in this study
that may be used instead of carrying out 3D simulations.
2 Numerical methodology
2.1 1D computational details
The artery is perceived to be a cylindrical-shaped vessel
with an elastic boundary condition at the wall. The 1D
equations for continuity and momentum conservation are
given in Sherwin et al. [4] and are
oA oðAuÞ
þ
¼0
ot
ox
ou
ou 1 op
þu þ
ot
ox q ox
ð2Þ
f
¼0
qA
ð3Þ
where A considered to be the cross-sectional area, u is the
average velocity across flow area, p is considered as the
pressure within the artery, q & 1060 kg/m3 is the blood
density and f is considered as the friction force per unit
length.
For the modeling of the friction term, a steady, laminar
and Poiseuille flow is assumed.
The closing of the system of equations is achieved by
providing additional constraint to relate the pressure with
cross-sectional area based on vessel elasticity, Poisson’s
ratio, and thickness of the wall. The relationship is defined
in Formaggia et al. [8] and Olufsen et al. [9]. The pressure
in the artery and area dependence is used as:
pffiffiffi pffiffiffiffiffi
p ¼ pext þ b A
A0
ð4Þ
where pext is the transmural pressure, A0 is the cross section
where the transmural pressure is considered zero (i.e.,
p ¼ pext ) and material properties of the vessel are b.
The unknown parameters (A) and (u) are gleaned from
the expression of forward (w1 ) characteristics and the
backward (w2 ) characteristics as:
ðw1 w2 Þ2 q 2
A¼
ð5Þ
b
1024
1
u ¼ ðw1 þ w2 Þ
2
ð6Þ
The numerical simulation is done using the process
(Mynard et al. [5]) developed by the locally conservative
Galerkin (LCG). Each element is treated with its own
boundaries as a sub-domain in this method.
Int J Adv Eng Sci Appl Math
2.2 Modeling of the arterial tree
The entire arterial network is modeled with both systemic
and coronary circulation and is shown in Fig. 1. The arteries
and their simulation properties were taken from Mynard
et al. [5] and implemented in the current study. The left
endocardial artery is modeled as stenotic one and all the
other parts of the arterial tree are modeled to be normal.
2.3 Geometry of the stenosed segment
The equation for a straight duct representing the stenosed
region is given by Sonu et al. [10]. Some improvement in the
equation is made by incorporating the tapering nature of the
duct which is shown in Fig. 2 and the modified expression is
e Lseg x
y¼
Lseg
x Lm L2s
R
S0 1 cos 2p
ð7Þ
2
Ls
to the maximum cross-sectional blockage location, Ls is the
length of the stenosis region of the artery, Di is the diameter at inlet, Do is the exit diameter and the severity is
percent blockage of the lumen area through which blood
flows in the artery.
2.4 1D validation study
The simulated (present) results obtained are compared with the
numerical results of Low et al. [11] as shown in Figs. 3 and 4.
The artery selected for validation study is the right carotid
artery. For normal conditions and heart function, the pressure
and flow waveform pattern are found to be almost similar.
2.5 Boundary conditions
Using a sigmoid function, the pressure profile is generated
as an inlet to the arterial tree as shown in Fig. 5. The
arterial tree outlet is given a zero coefficient of reflection.
where
Lm
S0 ¼
Ls
x Lm
2
severity
;
100
e¼
Ls
;
2
ðD i
2
ð8Þ
Do Þ
ð9Þ
Lseg is the arterial segment length, Rs is the radius of the
stenosed zone, Lm is the distance from the start of the artery
2.6 Grid independent study
The numerical investigation using three mesh sizes of 50
nodes, 100 nodes and 150 nodes is performed. For the three
mesh sizes, the axial velocity magnitude along the arterial
length (Left Endocardial artery) is compared as shown in
Fig. 6. It is observed that the mesh sizes of both 100 and
150 yield similar results. Therefore, for the simulation, 100
nodes per artery are considered.
2.7 3D computational details
Blood is perceived as a Newtonian fluid in this study, and it
is assumed that its movement through the arterial vessel is
laminar and incompressible. The mass and momentum
conservation is given by,
oui
¼0
oxi
oui o ui uj
þ
¼
oxj
ot
ð10Þ
1 oq
o2 ui
þ#
q oxi
oxi oxj
ð11Þ
The above equations are in conservative form.
A OpenFOAM solver based on finite volume method is
used to solve the CFD problem being studied. The
pimpleFoam solver of OpenFOAM is used with secondorder accurate scheme for time, gradient and divergence.
Fig. 1 1D branched network of arteries having important blood
vessels taken from Mynard et al. [5]
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Int J Adv Eng Sci Appl Math
Fig. 2 Geometry of the stenosed segment with label
Fig. 5 The pressure profile which is provided as a inlet to arterial tree
Fig. 3 Comparison of right carotid artery pressure waveforms with
the results of Low et al. [11]
Fig. 6 Variation of axial velocity along the arterial length for grid
independence test of a 70% severity
2.8 3D computational domain
Fig. 4 Comparison of right carotid artery flow waveforms with the
results of Low et al. [11]
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The flowchart for the generation of computational domain
is shown in Fig. 7. The multislice computed tomographic
Int J Adv Eng Sci Appl Math
scan data collected of Indian patients are segmented using
the snake algorithm and transformed into a CAD model. It
is further meshed in an ICEM-CFD, which is a commercial
software package where the aspect ratio of the cells is kept
close to one.
2.9 3D validation study
The flow through a stenosed artery was validated with Sonu
et al. [10] under steady-state condition. Reynolds number
(Re) based on characteristics length (D) and reference
velocity (Uavg ) at inlet is defined as Re = qUavgD/l. The
hydrodynamic properties considered in the simulation are
density (q = 1000 kg/m3), viscosity (l = 1 Pa s), velocity
(Uavg = .5 m/s) and diameter (D = 1 m). Based on the
following relationships, velocity and diameter are nondimensionalized
u
y
U¼
ð12Þ
; U¼ :
Uavg
D
The dimensionless velocity here is U, the dimensional
speed is u, the average inlet velocity is Uavg . The inlet
diameter is D, the cross-stream and the dimensionless length
is y and Y. At the inlet of the computational domain, a
parabolic velocity profile is imposed. The wall is given noslip boundary condition along with pressure (p = 0) at the
outlet for simulation. Velocity at different locations along
the computational domain is computed, as shown in Fig. 8. It
has been observed to be in good accordance with the findings
of the literature. The numerical results of FFR are compared
with the experimental results by Saha et al. [12] using the 3D
numerical model used in the present study and showed a
similar trend with experimental results.
2.10 Boundary condition
The Womersley velocity variation is achieved from the
patient-specific left anterior descending artery’s volume
Fig. 8 Comparison of velocity results at different downstream
distance to stenosis
flow rate waveform using the 1D numerical simulation.
Figure 9 indicates the patient-specific flow waveform
obtained from 1D simulation. The profiles of velocity are
determined from the volume flow rate waveform based
on the FFT operation. The velocity profile of Womersley
is applied at the inlet of the left anterior descending
artery which is the computational domain and constant
pressure (p = 0) condition for outlet of the computational
domain.
2.11 Grid independence test
The analysis of grid independence is carried out for all
cases, but for only one case it is shown here. The error is
measured to the finest mesh that the simulation considers.
The simulation is conducted in the computational domain
using 300,232 elements.
Fig. 7 Flowchart for generation of the computational domain
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Int J Adv Eng Sci Appl Math
Fig. 10 Location where primitive variables are computed in the
computational domain
and distal location of the stenosis, respectively. For the
computation of FFR, the pressure values at probe a and
probe c will be required.
3 Results and discussion
Fig. 9 Flow waveform for 1D patient-specific case
3.1 1D numerical results
No. of elements
FFR
Error (%)
105,433
.949
1.05
200,543
.954
.89
300,232
.956
.74
450,232
.963
–
2.12 Modeling viscosity
The different viscosity models are incorporated in 3D simulation for computation of FFR and comparison are done among
them. Non-Newtonian Models like Carreau Yasuda and Power
law are compared with the Newtonian model for computation
of FFR. The model constants of Carreau Yesuda and Power law
are taken from Shibeshi et al. [13]. As the shear rate in our
patient-specific models are more than 100 s-1, so it is a fair
good approximation of Newtonian fluid [14]. It also seen that
with different non-Newtonian model, the FFR value marginally
changes with different viscosity models as shown in Table 1.
The flow waveform indicates the amount of blood flow
supplied to one of the coronary arteries. The reduction of
flow due to any disease state means that the supply of all
essential components such as oxygen and vital nutrients to
the artery’s neighbouring cells are impeded. This may lead
to the failure of cardiac function. Thus, flow waveform
gives us more understanding of the disease state condition
of the cardiovascular system. The flow waveform for different geometric attributes like severity and lesion length of
stenosis is investigated.
Figure 11 shows that with higher severity or blockage
percent, the flow through the artery is hampered and
indicative of more severe disease state. Another geometric
2.13 Probe locations
The location where the computation of primitive variables
like pressure and velocity is done is shown in Fig. 10. The
probe location at a, b and c indicates the proximal, throat
Table 1 FFR comparison for different Non-Newtonian model with
the Newtonian model
Model
Newtonian
Carreau Yasuda
Power law
FFR
.68
.72
.71
123
Fig. 11 Flow waveform at different severity for corresponding lesion
length
Int J Adv Eng Sci Appl Math
Fig. 12 Pressure waveform at different lesion length for corresponding severity
parameter which plays a vital role in the functional severity
of stenosis is lesion length. The flow investigation through
various stenosis models having different lesion length for
the same percent blockage is done. Figures 12 and 13
clearly show that the values of pressure and flow are significantly different for various lesion lengths. It is observed
that with the increment in the length of lesion, the pressure
and flow are reducing for given severity.
The possible explanation of these above results can be
given with the help of the two characteristics which dominate in 1D pulse propagation study. The two characteristics are forward traveling characteristics (w1 ) and backward
Fig. 13 Flow waveform at different lesion length for 70% severity
traveling characteristics (w2 ). Whenever there is a blockage
or obstruction in the flow path, the backward traveling
component dominates due to wave reflection. The wave
reflection increases with the increase in blockage percent of
stenosis. Because of this, w2 will increase the backward
traveling characteristics. As a result, the velocity value
ðu / ðw1 þ w2 ÞÞ that depends on the wave characteristics
will decrease with the increment of percent blockage.
Thus, the blood flow in the left anterior descending
artery reduces with the increment in severity. For the same
blockage percent, the same trend is found with the
increasing lesion length as shown in Fig. 13. These
observations suggest that not only blockage percent is a
significant hemodynamic parameter but also the length of
the lesion plays an vital role in the intermediate-grade
coronary artery.
The pressure waveforms for 70 severity of stenosis are
plotted in Fig. 14 for one heart cycle, and the magnitude of
pressure at the probes is observed in order as pa [ pc [ pb .
The velocity waveform for 70 severity of stenosis is plotted
in Fig. 15 for one heart cycle, and the magnitude of
velocity at the probes is observed in order as vb [ vc [ va .
3.2 3D computational results
The comparison is made between a diseased state artery
and an artery without occlusion at a particular instant of the
cardiac cycle. The typical pressure contours obtained from
the patient-specific CFD simulation are shown in Fig. 16.
The diseased artery is reconstructed into normal one by
recovering the reduced lumen area due to build-up of
Fig. 14 Variation of pressure waveform at different probe location
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Int J Adv Eng Sci Appl Math
Fig. 17 Streamlines along with velocity magnitude of the patientspecific case, a normal artery, b stenosed artery
Fig. 15 Variation of velocity at different probe location
models, which are consistent with different literature
findings as shown in Fig. 18. This finding is obvious as the
pressure head loss occurs due to the separation of the flow
after the lowest cross-sectional region where the flow of
blood has to take place against the gradient of the adverse
pressure.
The error between the models is shown in Table 2.
Various geometric parameters may contribute to error.
Severity, lesion length and coronary tortuosity may play a
significant role in error. The wall distensibility can also be
responsible for the error but while comparing with the
silicon model, it qualitatively followed the same trend [12].
It is also seen that artery having almost the same severity,
the error differs due to the tortuous nature of the artery.
Regression testing suggests a correlation exists based on
Fig. 16 Pressure contour of the patient-specific case, a normal artery,
b stenosed artery
plaque. The change in pressure is significant in the stenosed
artery near the throat location than in normal artery.
The streamlines in diseased and normal artery are shown
in Fig. 17 for the same patient-specific case. The corresponding velocity magnitude is used to color each
streamline. The velocity is maximum at the throat location
in the diseased artery.
3.3 Comparison between FFR3D and FFR1D results
In this study, the comparison of three patient-specific cases
is performed for 1D and 3D FFR value. It is observed that
with increasing severity, the FFR value decreases for all
123
Fig. 18 Comparison of FFR1D and FFR3D for patient-specific cases
Int J Adv Eng Sci Appl Math
Table 2 Error between the two models for three patient-specific
cases
4 Conclusion
Data
FFR3D
FFR1D
Error (%)
Case 1
.956
.939
1.8
Case 2
.889
.84
5.5
Case 3
.67
.626
6.5
The blood flow within the coronary artery is influenced by
the forward and backward traveling wave characteristics.
The flow and pressure waveform depends not only on the
severity of coronary lesion, but also on the span of the
lesion. The size of the lesion seems to have a clinical
significance on the functional seriousness of stenosed
coronary artery. FFR comparison between 1D and 3D
model is done for different patients, and error is quantified
between the models. The comparison of FFR is also performed based on statistical analysis, and a correlation is
proposed that can be used instead of the real 3D numerical
computation. A good estimation of the FFR values can be
achieved by Windkessel component which can be implemented at the terminal of vessels instead of the model
which has resistance and it may boost the 1D model. The
effort is made to a clinical relevant problem to hasten the
decision taken by practitioners using fractional flow
reserve (FFR) parameter using a 1D model employing
locally conservative Galerkin method, and the study predicts FFR errors with full-scale 3D numerical simulation
done in an open-source software using CT scan data from
patients. This may be stepping stone for generating a more
feasible and accurate correlation which will predict the
value of FFR instead of carrying out the full-scale 3D
simulation.
Fig. 19 Confrontation between numerical simulation and correlation
for calculating FFR
computational results. The results obtained by means of
numerical methods and correlation are in good concurrence. The correlation for FFR calculation can be used
instead of 3D full-scale simulation
FFR3D ¼ aFFR1D þ bB þ cL þ d
where B is severity, L is size of lesion in mm, a = .81626,
b = 1.2677 9 106, c = 4.5419 9 106, d = .2599.
It is found that at 99 confidence, the value of R2 , for
FFR is .9939 for the correlation model is sufficiently
significant. Figure 19 shows the effectiveness of the FFR
regression model, where the contrast between the expected values of the correlation model and the numerical
results is shown. The errors have been determined
between the computational results for simulation and
those provided by correlation. The variation from the
simulated values is within ± 2%. The correlation may not
be very feasible, but it may be a stepping stone for
developing a more reliable and accurate correlation which
will incorporate more intricate details of the 3D model for
using it clinically.
Acknowledgements The authors appreciate exploratory research
support (APM1718844RFERKARU) provided by IIT Madras and
Global
Challenges
Research
Fund
(GCRF)
Grant
(RB1819APM003SWA-NKARU) partial funding from Swansea
University, UK. The authors also appreciate the arrangement for
Computed Tomographic scan results by Sri Ramachandra Medical
Center Institute, Chennai. The authors want to thank Prof.
P. Nithiarasu from Swansea University for his scientific deliberation.
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