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Simulation of Endovascular Repair of
Abdominal Aortic Aneurysms
David Roy, PhD student
“Les entretiens vasculaires XXXI” (ACVQ)
(May 3rd 2013)
1
Directed by: Dr Gilles Soulez,
Interventional Radiologist (Notre-Dame Hospital),
Full Professor of Radiology (University of Montréal)
Co-directed by: Dr Claude Kauffmann,
Physicist in Medical Imaging (Notre-Dame Hospital)
1/15
1 Finite element analysis: applications
Lumen
Thrombus
(blood clot)
Calcifications
2/15
2 Stent-Graft
2.1 Mechanical properties and modeling strategy
Graft:
polyethylene
terephthalate.
Stent:
316L steel.
Graft tensile tests:
• Young Moduli
E1 = 2E2 = 400MPa
• Poisson’s ratios
12 = 2 21 = 0.42
• Shear modulus
G12 = 12MPa
1 (Axial Dir.)
2 (Circ. Dir.)
Graft: bending stiffness
How to “relax” graft bending stiffness to allow a realistic folding behavior ???
Kirchhoff-Love thin plate theory provides the bending stiffness:
It’s enough to reduce the thickness, while increasing the moduli (E1, E2 and G12)
by the same factor (~ 10), to maintain the same tensile membrane stiffness.
)1(12 2
3
Et
D
E: Young’s modulus
t: thickness (influent parameter)
: Poisson’s ratio
3/15
2 Stent-Graft
Stent: beam elements
Graft: shell elements.
Displacement = 80mm
Clamped
proximal
section
Graft elements size = 0.25mm
max displacement = 78mm.
Graft Element size = 0.12mm
max displacement = 79mm.
2.2 Simple bending of an iliac extension
=> “Mesh size” independent solution !
Force = 0.3N
Displacements (mm) Displacements (mm)
4/15
2 Stent-Graft
2.3 Three-points bending of a main body
Force = 1.1N
Displacement = 27mm
Force = 1.1N
Displacement = 28.6mmSupports made of a "slightly rough"
polymeric material.
Estimated coefficient of friction = 0.6
(Vad, Eskinazi & Corbett, 2010).
5/15
2.4 Transversal compression of a (main body) “sealing” stent
0.00
0.10
0.20
0.30
0.40
0.50
0.60
0.70
0.0 5.0 10.0 15.0
Reactionforce(N)
Displacement (mm)
Imposed displacement = 12mm
Reaction force = 0.62N
Reaction force = 0.60N
Linear behavior !
Undeformed stent. Imposed displacement = 12mm
2 Stent-Graft
6/15
2.5 Radial compression of a (main body) “sealing” stent
1) Radial load (arbitrary
value) distributed on the
undeformed stent.
Initial diameter = 28mm.
3) Final diameter of the
compressed stent including the
graft: 19.07mm.
Negligible compressive
stiffness from the Graft, as it
should be !
2) Final diameter of the
compressed stent: 18.55mm.
2 Stent-Graft
7/15
2 Stent-Graft
Independent
variable
Tests dependent
variable
FEM dependent
variable
Variation (%)
Leg: simple bending force = 0.30 disp. = 79 disp. = 78 1.27
Boby: simple bending force = 0.65 disp. = 96 disp. = 101.40 5.62
Boby: three points bending force = 1.10 disp. = 27 disp. = 28.60 5.93
Boby: axial compression disp. = 12 force = 0.74 force = 0.75 1.35
Boby: transversal compression disp. = 12 force = 0.62 force = 0.60 3.23
Forces and displacements are in N and mm respectively.
2.6 Level of accuracy between mechanical tests and simulation
8/15
3 AAA
3.1 Algorithms for 3D geometry and centerlines reconstruction
Centerlines allow: collagen fibers orientation (material definition), and definition of a path for stent-graft deployment.
9/15
3 AAA
3.2 Element-wise local coordinate system for collagen fibers orientation
Element x axis
(obtained by
centerline projection)
Element y axis
Collagen fibers
Looking normally to
a single element.
Centerline (iliac) branch.
Z axis
“Selection cone”:
to pick the right
centerline point.
10/15
3 AAA
3.3 Anisotropic hyperelastic material
2
2
00
eqxx kx
kxdxFdxU
eqeq
eq
x
kx
x
U
F
eq
Strain energy =
area under the
curve
F
xeqx
dx
F
x
eqF
k
Biaxial stretch tests of
AAA specimen samples:
circ.-load:axial-load = 0.5:1
Axial
dir.
Circum.
dir.
Missing parameters to be fitted with test data: C10, k1, k2, and collagen fiber angle .
Isotropic isochoric
(<=> elastin contribution).
Undeformed
(Reference)
Uniaxial stretch
(@ equilibrium)
eqx
t
rP
ntialcircumfere
Could be the axial force
exerted by catheters.
222
1 tacI
1222
tac
el
J
0/ LLf
cc
c
U
S
1
aa
a
U
S
1
22
1
22
1)11(4 1 ac ccI
)11(4)22(4 II
)cos(1c
2/EEE
Working in tension only.
Isotropic volumetric
(<=> compressibility).
Anisotropy
(<=> collagen fibers).
2nd Piola-Kirchhoff stress components:
11/15
3 AAA
3.4 Parameters based on 2nd Piola-Kirchhoff stresses vs. Green strains best fit
circ.-load:axial-load ratio
Experiments
(26 cadaveric
samples)
.
2
.. 1
2
1
circcirccircE
C10 = 1.10x10e-6 kPa (low value  elastin loss)
k1 = 2853.63 kPa
k2 = 9321.99 dimensionless
= 0.32 dimensionless
= 5o degrees
n
SSSSerror
1ppoint
2model
axial,p
erienceexp
axial,p
2model
circ.,p
experience
circ.,p
Error function to be minimized:
axialaxialaxialE 1
2
1 2
Model
Average Coefficient of determination (R2) = 0.86
12/15
3 AAA
3.5 Pressure case & comparison with literature (in terms of Max. Princ. stresses)
Our model:
• Shell elements
• Thickness: 1.5mm
• Pressure: 120mmHg
• Anisotropic hyperelastic material
• Patient-specific geometry
• Only free radial expansion allowed at extremities.
Rodriguez, Ruiz & Doblaré, 2008:
• Solid elements
• Thickness: 1.5mm
• Pressure: 120mmHg
• Anisotropic hyperelastic material
• Virtual geometry
• Fully fixed extremities (not influencing stresses far from
the prescribed boundary conditions).
Princ. stresses (kPa) Princ. stresses (kPa)
Force “F” (mN)
Fixed face Section area “A” (mm2)
Stress = F/A (kPa)
13/15
3 AAA
3.6 Loads and Boundary conditions (BCs)
Equivalent
pressure for
surrounding
tissues.
Mean blood
pressure on
the lumen.
Tied contact
between
AAA and
thrombus.
Thrombus: hyperelastic isotropic material.
(Wang, Makaroun & Webster, 2001)
2
2221 33 IcIcW
Free renal
artery.
Only radial
expansion
allowed at
extremities.
Only radial
expansion
allowed at
extremities.
Contact
with spine. Nonlinear
equivalent
springs.
F
D
No calcifications yet,
but a promising strategy
under development.
14/15
3 AAA
1) Geometry from imaging 2) Loaded geometry from imaging (120mmHg) 2-bis) Loaded geometry from imaging - cut
Displacements
(mm)
3) Zero-pressure geometry 4) Loaded zero-pressure geometry 4-bis) Stresses in loaded zero-pressure geometry
Zero-pressure geometry =
Geometry from imaging –
displacements due to
Blood pressure.
Displacements
(mm)
Stresses
(kPa)
Should be the similar
geometries
3.7 Identification of the “true zero-pressure” geometry
15/15
4 Contact between the AAA lumen and Guidewire/catheters
1) Guidewire forced to fit the centerline
(contact with the vessel deactivated).
2) Guidewire in contact with the vessel
(forcing load released & contact activated).
The Guidewire actuates as a released spring
and enters in contact with the rigid boundary.
Objective in 2013: put everything together (stent-graft implanted in AAA)
Objective in 2014: workflow automatization
Merci !
Vos questions sont bienvenues
Thank you !
Your questions are welcome
REFERENCES
Vad, S., Eskinazi, A., Corbett, T., McGloughlin, T., & Vande Geest, J.-P. (2010). Determination of coefficient of friction for
self-expanding stent-grafts. Journal of Biomechanical Engineering, 132 (12), 121007-1 to 121007-10.
Rodriguez, J.-F., Ruiz, C., Doblaré, M., & Holzapfel, G.-A. (2008). Mechanical stresses in abdominal aortic aneurysms:
influence of diameter, asymmetry, and material anisotropy. Journal of Biomechanical Engineering, 130, 021023-1 to
021023-10.
Wang, D.-H., Makaroun, M.-S., Webster, M.-W., & Vorp, D.-A. (2001). Mechanical properties and microstructure of
intraluminal thrombus from abdominal aortic aneurysm. Journal of Biomechanical Engineering, 123, 536-539.

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2013session4 3

  • 1. Simulation of Endovascular Repair of Abdominal Aortic Aneurysms David Roy, PhD student “Les entretiens vasculaires XXXI” (ACVQ) (May 3rd 2013) 1 Directed by: Dr Gilles Soulez, Interventional Radiologist (Notre-Dame Hospital), Full Professor of Radiology (University of Montréal) Co-directed by: Dr Claude Kauffmann, Physicist in Medical Imaging (Notre-Dame Hospital)
  • 2. 1/15 1 Finite element analysis: applications Lumen Thrombus (blood clot) Calcifications
  • 3. 2/15 2 Stent-Graft 2.1 Mechanical properties and modeling strategy Graft: polyethylene terephthalate. Stent: 316L steel. Graft tensile tests: • Young Moduli E1 = 2E2 = 400MPa • Poisson’s ratios 12 = 2 21 = 0.42 • Shear modulus G12 = 12MPa 1 (Axial Dir.) 2 (Circ. Dir.) Graft: bending stiffness How to “relax” graft bending stiffness to allow a realistic folding behavior ??? Kirchhoff-Love thin plate theory provides the bending stiffness: It’s enough to reduce the thickness, while increasing the moduli (E1, E2 and G12) by the same factor (~ 10), to maintain the same tensile membrane stiffness. )1(12 2 3 Et D E: Young’s modulus t: thickness (influent parameter) : Poisson’s ratio
  • 4. 3/15 2 Stent-Graft Stent: beam elements Graft: shell elements. Displacement = 80mm Clamped proximal section Graft elements size = 0.25mm max displacement = 78mm. Graft Element size = 0.12mm max displacement = 79mm. 2.2 Simple bending of an iliac extension => “Mesh size” independent solution ! Force = 0.3N Displacements (mm) Displacements (mm)
  • 5. 4/15 2 Stent-Graft 2.3 Three-points bending of a main body Force = 1.1N Displacement = 27mm Force = 1.1N Displacement = 28.6mmSupports made of a "slightly rough" polymeric material. Estimated coefficient of friction = 0.6 (Vad, Eskinazi & Corbett, 2010).
  • 6. 5/15 2.4 Transversal compression of a (main body) “sealing” stent 0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.0 5.0 10.0 15.0 Reactionforce(N) Displacement (mm) Imposed displacement = 12mm Reaction force = 0.62N Reaction force = 0.60N Linear behavior ! Undeformed stent. Imposed displacement = 12mm 2 Stent-Graft
  • 7. 6/15 2.5 Radial compression of a (main body) “sealing” stent 1) Radial load (arbitrary value) distributed on the undeformed stent. Initial diameter = 28mm. 3) Final diameter of the compressed stent including the graft: 19.07mm. Negligible compressive stiffness from the Graft, as it should be ! 2) Final diameter of the compressed stent: 18.55mm. 2 Stent-Graft
  • 8. 7/15 2 Stent-Graft Independent variable Tests dependent variable FEM dependent variable Variation (%) Leg: simple bending force = 0.30 disp. = 79 disp. = 78 1.27 Boby: simple bending force = 0.65 disp. = 96 disp. = 101.40 5.62 Boby: three points bending force = 1.10 disp. = 27 disp. = 28.60 5.93 Boby: axial compression disp. = 12 force = 0.74 force = 0.75 1.35 Boby: transversal compression disp. = 12 force = 0.62 force = 0.60 3.23 Forces and displacements are in N and mm respectively. 2.6 Level of accuracy between mechanical tests and simulation
  • 9. 8/15 3 AAA 3.1 Algorithms for 3D geometry and centerlines reconstruction Centerlines allow: collagen fibers orientation (material definition), and definition of a path for stent-graft deployment.
  • 10. 9/15 3 AAA 3.2 Element-wise local coordinate system for collagen fibers orientation Element x axis (obtained by centerline projection) Element y axis Collagen fibers Looking normally to a single element. Centerline (iliac) branch. Z axis “Selection cone”: to pick the right centerline point.
  • 11. 10/15 3 AAA 3.3 Anisotropic hyperelastic material 2 2 00 eqxx kx kxdxFdxU eqeq eq x kx x U F eq Strain energy = area under the curve F xeqx dx F x eqF k Biaxial stretch tests of AAA specimen samples: circ.-load:axial-load = 0.5:1 Axial dir. Circum. dir. Missing parameters to be fitted with test data: C10, k1, k2, and collagen fiber angle . Isotropic isochoric (<=> elastin contribution). Undeformed (Reference) Uniaxial stretch (@ equilibrium) eqx t rP ntialcircumfere Could be the axial force exerted by catheters. 222 1 tacI 1222 tac el J 0/ LLf cc c U S 1 aa a U S 1 22 1 22 1)11(4 1 ac ccI )11(4)22(4 II )cos(1c 2/EEE Working in tension only. Isotropic volumetric (<=> compressibility). Anisotropy (<=> collagen fibers). 2nd Piola-Kirchhoff stress components:
  • 12. 11/15 3 AAA 3.4 Parameters based on 2nd Piola-Kirchhoff stresses vs. Green strains best fit circ.-load:axial-load ratio Experiments (26 cadaveric samples) . 2 .. 1 2 1 circcirccircE C10 = 1.10x10e-6 kPa (low value  elastin loss) k1 = 2853.63 kPa k2 = 9321.99 dimensionless = 0.32 dimensionless = 5o degrees n SSSSerror 1ppoint 2model axial,p erienceexp axial,p 2model circ.,p experience circ.,p Error function to be minimized: axialaxialaxialE 1 2 1 2 Model Average Coefficient of determination (R2) = 0.86
  • 13. 12/15 3 AAA 3.5 Pressure case & comparison with literature (in terms of Max. Princ. stresses) Our model: • Shell elements • Thickness: 1.5mm • Pressure: 120mmHg • Anisotropic hyperelastic material • Patient-specific geometry • Only free radial expansion allowed at extremities. Rodriguez, Ruiz & Doblaré, 2008: • Solid elements • Thickness: 1.5mm • Pressure: 120mmHg • Anisotropic hyperelastic material • Virtual geometry • Fully fixed extremities (not influencing stresses far from the prescribed boundary conditions). Princ. stresses (kPa) Princ. stresses (kPa) Force “F” (mN) Fixed face Section area “A” (mm2) Stress = F/A (kPa)
  • 14. 13/15 3 AAA 3.6 Loads and Boundary conditions (BCs) Equivalent pressure for surrounding tissues. Mean blood pressure on the lumen. Tied contact between AAA and thrombus. Thrombus: hyperelastic isotropic material. (Wang, Makaroun & Webster, 2001) 2 2221 33 IcIcW Free renal artery. Only radial expansion allowed at extremities. Only radial expansion allowed at extremities. Contact with spine. Nonlinear equivalent springs. F D No calcifications yet, but a promising strategy under development.
  • 15. 14/15 3 AAA 1) Geometry from imaging 2) Loaded geometry from imaging (120mmHg) 2-bis) Loaded geometry from imaging - cut Displacements (mm) 3) Zero-pressure geometry 4) Loaded zero-pressure geometry 4-bis) Stresses in loaded zero-pressure geometry Zero-pressure geometry = Geometry from imaging – displacements due to Blood pressure. Displacements (mm) Stresses (kPa) Should be the similar geometries 3.7 Identification of the “true zero-pressure” geometry
  • 16. 15/15 4 Contact between the AAA lumen and Guidewire/catheters 1) Guidewire forced to fit the centerline (contact with the vessel deactivated). 2) Guidewire in contact with the vessel (forcing load released & contact activated). The Guidewire actuates as a released spring and enters in contact with the rigid boundary. Objective in 2013: put everything together (stent-graft implanted in AAA) Objective in 2014: workflow automatization
  • 17. Merci ! Vos questions sont bienvenues Thank you ! Your questions are welcome
  • 18. REFERENCES Vad, S., Eskinazi, A., Corbett, T., McGloughlin, T., & Vande Geest, J.-P. (2010). Determination of coefficient of friction for self-expanding stent-grafts. Journal of Biomechanical Engineering, 132 (12), 121007-1 to 121007-10. Rodriguez, J.-F., Ruiz, C., Doblaré, M., & Holzapfel, G.-A. (2008). Mechanical stresses in abdominal aortic aneurysms: influence of diameter, asymmetry, and material anisotropy. Journal of Biomechanical Engineering, 130, 021023-1 to 021023-10. Wang, D.-H., Makaroun, M.-S., Webster, M.-W., & Vorp, D.-A. (2001). Mechanical properties and microstructure of intraluminal thrombus from abdominal aortic aneurysm. Journal of Biomechanical Engineering, 123, 536-539.