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Appendix 6: 3D Linearization of Fungs Exponential Strain... 245
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Table 4.18 Material constants of the constitutive equation obtained from experimental data of LAD (left anterior descending) artery
(a) Generalized Hookes law. Units of linear material parameters, i.e., c
are kPa. Nonlinear
11–c23
parameter n is a nondimensional number
2
2
R
nc
11c22
c
33c12c13c23
R
(FT)
( pi)
RMS% (FT)
RMS% ( pi)
Heart71.41 9.54 37.68 50.53 4.56 5.77 15.92 0.96 0.97 15.7 23.7
Heart81.45 18.33 59.11 18.00 18.16 13.71 29.40 0.99 0.99 7.6 9.1
Heart91.88 31.86 48.00 47.00 29.70 30.25 36.26 0.92 0.98 29.6 17.4
Heart101.44 37.45 55.86 61.34 15.00 24.01 26.64 0.98 0.99 13.0 13.4
Heart111.11 43.74 70.35 30.00 35.56 32.38 37.61 0.98 0.98 13.9 16.7
Heart121.49 37.43 139.92 50.00 56.25 39.42 80.89 0.95 0.98 22.0 11.1
Mean 1.46 29.73 68.49 42.81 26.54 24.26 37.79 0.96 0.98 17.0 15.2
SD 0.25 13.09 36.67 15.82 18.22 12.53 22.51 0.03 0.01 7.7 5.2
(b) Fungs exponential model. Material parameter C has the units of stress (kPa), b
are dimensionless constants
and b
6
Cb
b2b3b
1
b5b
4
2
2
R
R
(FT)
6
( pi)
1
RMS% (FT)
, b2, b3, b4, b5,
RMS% ( pi)
Heart711.64 1.03 2.09 0.38 0.37 0.02 0.06 0.98 0.97 26.3 21.1
Heart85.94 1.27 2.78 0.62 0.45 0.13 0.13 0.97 0.99 25.1 21.4
Heart94.16 1.58 2.66 0.73 0.30 0.03 0.08 0.96 0.98 34.5 18.4
Heart1011.39 1.39 2.62 0.51 0.32 0.06 0.06 0.99 0.99 28.0 18.5
Heart115.48 1.54 4.29 1.31 0.05 0.22 0.21 0.98 0.99 12.6 13.0
Heart124.43 1.48 5.15 0.24 0.25 0.46 0.01 0.88 0.97 33.2 22.1
Mean 7.17 1.38 3.27 0.63 0.29 0.15 0.09 0.96 0.98 26.6 19.1
SD 3.43 0.21 1.18 0.37 0.13 0.17 0.07 0.04 0.01 7.8 3.3
(c) Bi-phasic model. Material parameter μ > 0 and k
> 0 have the units of stress, k2> 0 and
1
ρ 2 [0, 1] are dimensionless parameters, and the unit of φ is degree
μ k
k2φρR2(FT) R2( pi) RMS% (FT) RMS% ( pi)
1
Heart 7 10.87 0.47 0.65 37.89 0.26 0.99 0.98 10.6 19.5 Heart 8 11.62 0.83 0.79 89.71 0.47 0.97 0.98 15.7 19.8 Heart 9 10.14 0.01 1.39 6.97 0.51 0.98 0.99 9.3 19.3
Heart 10 13.80 0.27 1.18 39.13 0.56 0.99 0.99 10.4 14.0
(continued)
246 4 Constitutive Models of Coronary Vasculature
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(c) Bi-phasic model. Material parameter μ > 0 and k1> 0 have the units of stress, k2> 0 and ρ 2 [0, 1] are dimensionless parameters, and the unit of φ is degree
μ k
k2φρR2(FT) R2( pi) RMS% (FT) RMS% ( pi)
1
Heart 11 9.72 0.51 0.96 1.15 0.41 0.98 0.98 12.7 18.5 Heart 12 17.97 0.60 2.17 90.00 0.91 0.98 0.91 24.3 35.6
Mean 12.35 0.45 1.19 44.14 0.52 0.98 0.97 13.8 21.1
SD 3.10 0.28 0.55 38.66 0.22 0.01 0.03 5.6 7.4
2
R
is correlation coefcient; RMS% is the percentage of the root mean square error of the t compared to the mean value. Both were computed for the total axial force (F
). Reproduced from Zhang, Wang, et al. (2007) with permission
( p
i
) and inner pressure
T
Table 4.19 Results of the sensitivity analysis for generalized Hookes law (a), Fungs exponential model (b), and bi-phasic model (c)
(a) Generalized Hookes law. Units of linear material parameters, i.e., c
are kPa. Nonlinear
11–c23
parameter n is a nondimensional number
Ratio nc
11
R
( pi)
RMS
2
% (FT)
2
c
c
c
22
33
c
12
13
R
c
(FT)
23
RMS % ( pi)
0.8 0.65 21.32 60.86 30.00 23.75 18.93 28.41 0.97 0.97 15.9 21.8
0.9 0.83 25.63 62.47 30.00 23.92 19.95 28.53 0.97 0.98 15.7 20.4
1.0 1.11 43.74 70.35 30.00 35.56 32.38 37.61 0.98 0.98 13.9 16.7
1.1 1.54 54.59 59.02 30.01 31.85 34.30 31.67 0.98 0.99 12.5 14.2
1.2 2.00 74.38 37.30 30.09 24.59 36.18 18.09 0.98 0.99 11.3 13.9 Mean 1.23 43.93 58.00 30.02 27.93 28.35 28.86 0.98 0.98 13.9 17.4 SD 0.55 21.72 12.35 0.04 5.44 8.25 7.09 0.01 0.007 2.0 3.6 Note: Ratio of inner and outer circumference C
constants, coefcient of determination (R
and Cois indicated in the rst column. Material
i
2
), and percent root mean square error (percentage of the root mean square error of the t compared to the mean value, RMS%) of the different data sets are shown. The values of mean and standard derivation for all of the parameters are given as well. F and P represent the axial force and pressure, respectively
(b) Fungs exponential model
Ratio Cb
0.8 6.91 0.43 3.32 0.34 0.07 0.15 0.01 0.98 0.98 13.8 47.0
0.9 3.76 0.94 4.43 1.70 0.02 0.15 0.08 0.99 0.99 12.8 27.7
1.0 5.48 1.54 4.29 1.31 0.05 0.22 0.21 0.98 0.99 12.6 13.0
1.1 6.91 0.43 3.32 0.34 0.07 0.15 0.01 0.98 0.98 13.8 47.0
1.2 4.74 4.69 5.08 0.32 0.21 0.07 0.02 0.99 0.99 12.3 46.0 Mean 5.56 1.61 4.09 0.80 0.09 0.15 0.06 0.98 0.99 13.1 36.1 SD 1.38 1.79 0.76 0.65 0.07 0.06 0.09 0.002 0.003 0.7 15.3 Note: Ratio of inner and outer circumference C
units of stress (kPa), b
determination (R of the t compared to the mean value, RMS%) of the different data sets are shown. The values of mean and standard derivation for all of the parameters are given as well. F and P represent the axial force and pressure, respectively
2
2
R
( pi)
RMS% (FT)
b2b3b4b5b
1
and Cois indicated in the rst column. C has the
, b2, b3, b4, b5, and b6are dimensionless constants. Coefcient of
1
2
), and percent root mean square error (percentage of the root mean square error
i
(FT)
6
R
RMS% ( pi)
(continued)
Appendix 7: Shear Modulus in Reference to New Strain Measure Zhang... 247
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Table 4.19 (continued)
(c) Bi-phasic model Ratio μ k
0.8 3.57 5.51 0.38 90.00 0.83 0.98 0.98 15.1 18.6
0.9 6.46 2.31 0.57 90.00 0.68 0.99 0.98 12.5 19.5
1.0 9.72 0.51 0.96 65.72 0.41 0.98 0.98 12.7 18.5
1.1 10.07 2.54 0.68 0.07 0.10 0.97 0.98 17.8 16.8
1.2 9.54 10.94 0.79 0.11 0.29 0.92 0.96 36.9 31.1 Mean 7.87 4.36 0.68 49.18 0.46 0.97 0.98 19.0 20.9 SD 2.81 4.09 0.22 45.90 0.29 0.03 0.009 10.2 5.8 Note: Ratio of inner and outer circumference C
parameters μ > 0 and k parameters, and the unit of φ is degree. Coefcient of determination (R
square error (percentage of the root mean square error of the t compared to the mean value, RMS %) of the different data sets are shown. The values of mean and standard derivation for all of the parameters are given as well. F and P represent the axial force and pressure, respectively
Reproduced from Zhang, Wang, et al. (2007) with permission
k
1
1
φρR2(FT) R2( pi) RMS% (FT) RMS% ( pi)
2
and Cois indicated in the rst column. Material
> 0 have the units of stress, k2> 0 and ρ 2 [0, 1] are dimensionless
i
2
) and percent root mean
Appendix 7: Shear Modulus in Reference to New Strain Measure Zhang, Wang, et al. (2007)
The coronary arteries are assumed to be homogeneously elastic, cylindrically orthotropic, and volumetrically incompressible solids. The arterial wall is also assumed to remain as an axisymmetric tube with a uniform cross section at various combinations of ination pressure P Fig. 4.20. Therefore, the cylindrical coordinates of a vessel segment in the deformed state (r, θ, z) are related to those in the zero-stress state (R, Θ, Z ) by:
, axial stretch λz, and torque T, as illustrated in
i
where χ ¼ π/(π Φ) with Φ being the opening angle that characterizes the residual strain, α is the twist angle, L ratio with L being the length at deformed state. The origins of the coordinate systems are assumed to be at one end of the vessel segment. The change of axial stretch from zero-stress to no-load state is neglected.
The deformation gradient matrix F with respect to the zero-stress state is given
by:
where j, k ¼ r, θ, z and
αZ
r ¼ rRðÞ, θ ¼ χΘ þ
the length at zero-stress state, λL/L0the axial stretch
0
2
λ

F
jk
r
4
¼
0 λ 00λ
, z ¼ λzZ, ð4:74Þ
L
0
3
00
5
, ð4:75Þ
ξ
θ
θ
z
248 4 Constitutive Models of Coronary Vasculature
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dr
dR
, λ
λr¼
The incompressibility condition, det[F
R
λ
¼
r
χλ
θ
, r ¼
r
z
χr
, ξ
¼
R
] ¼ 1 in Eq. (4.75), yields
jk
s
αr
¼
¼
θ
L
0
ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi
R2 R
2
r
þ
i
χλ
z
λzαr
L
2 i
ð4:76Þ
ð4:77Þ
Therefore, the right Cauchy-Green deformation tensor C (Ogden, 1984) is given by:
C ¼ F
T
F ¼
2
2
λ
r
4
0 λ 0 λθξθλ
00
2
θ
λθξ
2
z
þ ξ
3
5
θ
2
θ
ð4:78Þ
Lagrangian strains can be dened by the symmetric tensor C.
Generalized Hookes Law
To simplify the constitutive relation of blood vessels, a logarithmic-exponential (log-exp) strain tensor is dened as (Appendix 6):
1
ln Cexp nJ
D ¼
2
where n is called the nonlinearity parameter and J
3ðÞ½ ð4:79Þ
1
denotes the rst invariant of the
1
right Cauchy-Green deformation tensor C. The D reduces to the Hencky (logarith­mic) strain (ln C)/2 when n ¼ 0. In the specic case of Eq. (4.78), one nds:
2
2
2
J
¼ tr CðÞ¼λ
1
θ
þ λ
z
þ λ
2
þ ξ
r
θ
ð4:80Þ
It is postulated that the second Piola–Kirchhoff stress and the log-exp strain are
connected by a generalized Hookes law (Appendix 6), namely,
0
B B B B B B @
1
2
S
θθ
C
S
zz
C C
S
rr
C C
S
zr
C A
S
θr
S
θz
c
11c12c13
6
c
12c22c23
6 6
c
13c23c33
6
¼
6
000c
6 4
0000c 00000c
000 000 000
00
44
55
3
0
7
B
7
B
7
B
7
B
7
B
7
B
5
@
0
66
D D D
2D 2D 2D
1
θθ
C
zz
C C
rr
C C
zr
C A
θr
θz
ð4:81Þ
Φ
Θ
R
R
o
R
i
θ
r
o
r
i
r
α
r
T
T
αro/L r
o
r
i
L
λ
z
z
P
i
Appendix 7: Shear Modulus in Reference to New Strain Measure Zhang... 249
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Fig. 4.20 (a) The zero­stress state, (b) the deformed cross section, and (c) the deformed coronary artery under transmural pressure
, axial stretch λz, and twist
P
i
torque T. R
and Ro, riand ro,
i
are the inner and outer radii in the (R, Θ, Z ) and (r, θ, z)
(a) (b)
coordinate systems,
angle, L is vessel segment length, α is twist angle. Reproduced from Zhang, Wang, et al. (2007) with permission
λ
(c)
where cs (with unit of stress) can be interpreted as the elastic moduli with respect to the log-exp strains. In particular, c Fig. 4.20.
To compute the log-exp strains, the logarithm of tensor C (Eqs. 4.78 and 4.79) must be calculated. In terms of spectral decomposition (Ogden, 1984), if u 2, 3) are the unit vectors (eigenvectors) along the Lagrangian principal axes of C, then:
is the shear modulus for the torsion test in
66
(i)
(i ¼ 1,
z
The eigenvalues and eigenvectors of tensor C (the rst equation) must be determined, and subsequently the logarithm of those eigenvalues must be calculated to project the result back to the original coordinates.
Shear Modulus
In the experiments of Lu et al. (2003), a typical angle of twist is α ¼ 0.4 radian (23). The representat ive radius and length of porcine left anterior descending artery are
r ¼ 2.5 mm and L ¼ 20 mm, respectively, and the typical value of ξ L ¼ 0.05λ
rst-order terms of ξ
which is much smaller than λθand λz(on the order of unity). If only the
z
C ¼
3
X
2
iðÞ
u
iðÞ
,lnC ¼
λ
u
i
i¼1
is retained, the logarithm of tensor C in Eq. (4.78) can be
θ
3
X
i¼1

ln λ
2
iðÞ
u
iðÞ
is ξθ¼ λr/
θ
u
i
ð4:82Þ
250 4 Constitutive Models of Coronary Vasculature
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approximated by the following Taylor expansion (which is obtained from Eq. (4.82) and then expanded with respect to ξ
ln C
):
θ
2
2
ln λ
r
4
0lnλ 02eθzln λ
2e
3
5
θz
2
z
00
2
θ
ð4:83Þ
where
λθξθln λθ=λ
ðÞ
e
¼
θz
2
λ
θ
λ
z
2
z
ð4:84Þ
Note that e
ξθ/(2λz) ¼ ar/(2L ) when λθ λz, which is the small shear strain
θz
used in Lu et al. (2003).
Since it is found that the measured torque (T) and the angle of twist per unit length (α/L) are linearly proportional in the range of interest, Cauchy shear stress has been used to compute shear modulus with respect to shear strain (αr/(2L )) (Lu et al.,
2003). According to the theory of continuum mechanics (Humphrey & Na, 2002),
the Cauchy stress of incompressible materials can be derived from the second Piola– Kirchhoff stress as:
σ
¼ FjlFkmSlmþ Hδjkj; k; l; m ¼ r; θ; zðÞð4:85Þ
jk
where δ
is the Kronecker delta and H is an arbitrary scalar that needs to be
jk
determined from boundary conditions. Einstein summation has been assumed in Eq. (4.85). Equations (4.75) and (4.85) yield the Cauchy shear stress in the ination– stretch–torsion test as:
σ
¼ λθSθzþ ξθS
ðÞλ
θz
zz
z
ð4:86Þ
Equation (4.86) shows that Cauchy shear stress depends on both shear and axial second Piola–Kirchhoff stresses. Substituting the incompressibility condition
D
+ Dzz+ Drr¼ 0 (i.e., λθλzλr¼ 1, also see Eqs. (4.79) and (4.83)) into
θθ
Eq. (4.81), the following holds:
S
¼ 2c66Dθz, Szz¼ d21Dθθþ d22D
θz
zz
ð4:87Þ
where d
¼ c12 c23and d22¼ c22 c23. Equation (4.83) can be substituted into
21
Eq. (4.79) to obtain the following log-exp strains needed in Eq. (4.87):
D
¼ eθzexp nJ1 3ðÞ½ ð4:88Þ
θz
D
¼ ln λθexp nJ1 3ðÞ½ ð4:89Þ
θθ
Appendix 8: Incompressibility in the Generalized Hookes Law (Li ... 251
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Dzz¼ ln λzexp nJ1 3ðÞ½ ð4:90Þ
If Eqs. (4.87)–(4.90) are substituted into Eq. (4.86), the result is:

2c66λθe
σ
¼
θz
θz
þ d21ln λθþ d22ln λ
ξ
θ
λzexp nJ1 3ðÞ½: ð4:91Þ
ξ
z
θ
The shear modulus of Cauchy stress with respec t to Cauchy small strain can be evaluated as (Lu et al., 2003):
G ¼
σ
αr=LðÞ
λzσ
θz
θz
¼
ξ
θ
ð4:92Þ
The substitution of Eqs. (4 .84) and (4.91) into Eq. (4.92) yields
"#
2
2c66λ
ln λθ=λ
ðÞ
Since λ
J
λ
1
G ¼
2
þ λ
θ
θ
2
λ
θ
¼ 1/(λθλz) and ξθis a small value in Eq. (4.80), i.e.,
r

2
þ 1= λ
z
z
þ d21ln λθþ d22ln λ
2
λ
z
2
2
, one can readily conclude from Eq. (4.93) that the incre-
λ
θ
z
2
exp nJ1 3ðÞ½ð4:93Þ
λ
z
z
mental shear modulus G depends on the circumferential and axial stretches nonlinearly. Providing that c for given λ
and λz, independent of Cauchy small shear strain ξθ/(2λz) ¼ αr/(2L ),
θ
, d21and d22are material constants, G will be constant
66
consistent with the ndings in (Lu et al., 2003). The small shear strain assumption is still valid in the above analysis although the strains in the circumferential and axial directions are large in the ination–stretch–torsion test.
Appendix 8: Incompressibility in the Generalized Hookes Law (Liu, Zhang, et al., 2011)
A cylindrically orthotropic elastic model that accounts for large deformation of arteries is necessary to capture the mechanical response of the vessel. For simplicity, a linearized stress–strain relation (constitutive model) is used that makes the analysis easier and more amenable to interpretation as outlined Appendix 6.
As per standard notations in continuum mechanics, the deformation gradient F can be decomposed as tensor product of a rigid rotation tensor R (R right stretch tensor U; i.e., F ¼ RU. The right Cauchy-Green deformation tensor C ¼
T
F
F ¼ U2. Following the approach in Appendix 6, a logarithmic-exponential
(log-exp) strain tensor D that absorbs the material nonlinearity is dened as:
T
R ¼ I) and
252 4 Constitutive Models of Coronary Vasculature
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1
Q ln C ¼ exp nJ
D ¼
2
3ðÞ½ln U ð4:94Þ
1
with

Q ¼ exp nJ
3ðÞ½, Jtr CðÞ¼tr U
1
2
, ð4:95Þ
where n is a nonlinearity parameter, i.e., the tensor D is the product of the logarith­mic (natural, Hencky) strain and a scalar Q which is proposed to account for the strong exponential strain– stress relation found in vascular tissues (Fung, 1993). It can be shown, under the principal-axis representation, that D satises all the mathematical requirements for a strain tensor (Ogden, 1997). It can also be proven that tr(D)¼ ln(J )Q, where J ¼ det(F) ¼ det(U), i.e., tr(D) ¼ 0 for incompressible deformation where J 1. In fact, this property arises from the classical Hencky strain. Furthermore, D is a Lagrangian strain similar to the Green strain E.
Deformation of blood vessels is considered incompressible under physiological loading. The Cauchy stress (σ) for incompressible material is decomposed as
e
σ ¼ σ
pressure and σ interpreted as the deviatoric stress, i.e., tr(σ
pI, where p is a Lagrange multiplier that accounts for the hydrostatic
e
is the extra stressdue to deformation of the material. σeis also
e
) ¼ 0. It is noted for incompressible
materials that hydrostatic stress σ ¼pI does not lead to any deformation. In other words, the hydrostatic pressure p must be determined from the boundary condition rather than the stress–strain relation. The second Piola–Kirchhoff stress (S), how­ever, cannot be physically decomposed into hydrostatic stress and “extra stress” since S ¼ F
1σFT
¼ F1σeFTpC1(note J ¼ 1). This presents some
complexity for modeling anisotropic incompressible materials in Lagrangian frame, e.g., the linear relationship between D and S becomes problematic since it is difcult to ensure tr( D) ¼ 0 under arbitrary stress S.
A modied formulation is presented to directly address the hydrostatic pressure and material incompressibility, with the introduction of a co-rotational Cauchy stress T (Ogden, 1984) as:
Although T is in Lagrangian frame (because both U and S are in Lagrangian frame), it preserves the decomposition of σ, i.e., T generated by material deformation:
and the trace tr(T) is exclusively contributed by the hydrostatic stress p I which is independent of deformation.
T ¼ USU ¼ R
e
tr T
ðÞ¼tr RTσeR
T
σR ¼ RTσeR  pI ¼ Te pI ð4:96Þ
e
is a deviatoric extra stress

¼ tr σeðÞ¼0 ð4:97Þ
Appendix 8: Incompressibility in the Generalized Hookes Law (Li ... 253
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Incompressibility Condition
It is proposed that the stress T and the log-exp strain D are conn ected by a constant fourth-order compliance tensor M as:
D ¼ M : T ¼ M : T
e
pIðÞ: ð4:98Þ
The tensor M has major and minor symmetries, and must satisfy certain condi­tions such as M : I ¼ 0 (Mehrabadi & Cowin, 1999), i.e., to ensure zero deformation (D ¼ 0) when the stress is hydrostatic (T ¼pI). If the orthotropic symmetry of vessel tissue is considered, Eq. (4.98) can be expressed in a matrix form (generalized Hookes law):
0
B B B B B B B B @
1
2
6 6 6 6 6 6 6 6 4
0
B B B B B B B B B @
νν
1=E
θz=Eθ
θr=Eθ
T
T
T
ffiffiffi2p
ffiffiffi2p
ffiffiffi2p
νθz=Eθνθr=E
θ
1=E
νzr=E
νzr=E
z
1=E
z
r
0001=2G
000
θ
000
z
000
zr
00001=2G
000001=2G
1
e
θθ
C
e
C
zz
C
e
C
rr
C
,
C
e
T
C
zr
C C
e
T
A
θr e
T
θz
00
θr
D
θθ
C
D
zz
C C C
D
rr
C
ffiffiffi2p ffiffiffi2p ffiffiffi2p
¼
C
D
zr
C C A
D
θr
D
θz
3
7 7 7 7 7 7 7 7 5
0
θz
ð4:99aÞ
or
where θ, z, and r denote circumferential, axial, and radial directions. The parameters
E
, Ez, and Ercan be interpreted as Youngs moduli in reference to the log-exp
θ
strains, G
, Gθr, and Gzrare shear moduli, and vθz, vθr, and vzrare Poisson s ratios.
θz
Except for the denition of strain and stress, this constitutive relation is identical to the classical generalized Hookes law for orthotropic elast ic materials. Note that the use of factor presentation (Mehrabadi & Cowin, 1999).
Unlike the general orthotropic materials where the six parameters Es and νsin Eqs. (4.99a, 4.99b) are independent, the incompressibility condition M : I ¼ 0 imposes restrictions (Itskov & Aksel, 2002; Loredo & Klocker, 1997), namely:
D
fg
¼ M½T
e
fg
ð4:99bÞ
ffiffiffi2p
in Eqs. (4.99a , 4.99b) preserves the tensorial properties in the matrix
254 4 Constitutive Models of Coronary Vasculature
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
E
1
1
vij¼
i
þ
E
2
i
1
E
E
j
ij ¼ θz; θr; zr; k i; jðÞð4:100Þ
k
such that Eqs. (4.99a, 4.99b) is rewritten for vessel tissue as:
ffiffiffi3p
1
z
T
e
θθ
2
1
E
θ
1
e
zz
C C C C C C C C C C C C C A

1
1
E
E
θ
z
1
1
þ
E
2E
z
r
3
000
000
00
zr
θr
7 7 7 7 7 7 7 7 7 7 7 7
0
5
θz
0
2Drr Dθθ D
B B B B
Dzz D
B B B B B B B B @
ffiffiffi2p
ffiffiffi2p
ffiffiffi2p
1
2
zz
ffiffiffi6p
C C C C
θθ
C
ffiffiffi2p
C C
¼
C
D
D
D
C
zr
C C C
θr
A
θz
3
6
2E
6 6 6 6 6 6 6 6 6 6 6 4
0
B B B B B B B B B B B B B @
r
ffiffiffi3p

1
E
2
2T
E
θ
001=2G
0001=2G
00001=2G
e
e
T
rr
θθ
ffiffiffi6p
e
T
T
zz
ffiffiffi2p
ffiffiffi2p
e
T
zr
ffiffiffi2p
e
T
θr
ffiffiffi2p
e
T
θz
ð4:101aÞ
or
¼
^
D
which involves six, instead of nine, material parameters: {E Together with tr(D) ¼ D
+ Dzz+ Drr¼ 0 and tr TeðÞ¼T
θθ
M
^

e
^
T
ð4:101bÞ
, Ez, Er, Gθz, Gθr, Gzr}.
θ
e
e
þ T
θθ
e
þ T
rr
¼ 0,
zz
Eqs. (4.101a, 4.101b) is identical to Eqs. (4.99a, 4.99b) with the advantage that the relation is invertible (note: matrix [M] in Eqs. (4.99a, 4.99b) is singular), i.e.,
¼
e
^
T
M

1
^
^
D
ð4:102Þ
which is convenient for strain-based computations.
Equilibrium equati ons and boundary conditions for nite strain deformations are conventionally formulated in terms of second Piola–Kirchhoff stress S or Cauchy stress σ. Given a deformation gradient F, the log-exp strain D is calculated by Eqs. (4.94) and (4.95), then the deviatoric co-rotational Cauchy stress T lated by Eq. (4.102) and condition tr(T
e
) ¼ 0, and nally S or σ is obtained by
e
is calcu-
Eq. (4.96). For some deformation modes such as the ination–stretch experiment on vessels, the shear stress vanish, an d the stress–strain relation (Eqs. 4.101a, 4.101b and 4.102) can be further simplied as in Eq. (4.104).