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d
x
E
2
sin
2
x
)
3
/
2
=
(1
−
=
x
1+
3
64
E
4
4
cos
x
sin
x
1+
15
16
E
2
E
2
4
E
2
+
45
3
15
32
E
4
cos
x
sin
3
x
+O(
E
6
)
−
−
(I.16)
⇒
c
1
(see first equation of (
I.10
))
,
Λ
E
d
Λ
Φ
E
Φ
S
E
2
sin
2
Φ
)
=
Φ
N
d
Φ
(
Λ
E
−
Λ
W
)d
Φ
E
2
sin
2
Φ
)
,
(I.17)
cos
Φ
(1
−
cos
Φ
(1
−
Λ
W
Φ
S
d
x
E
2
sin
2
x
)
=
cos
x
(1
−
=(1+
E
2
+
E
4
)lntan
π
2
4
+
x
1
E
2
(1 +
E
2
)sin
x
3
E
4
sin
3
x
+O(
E
6
)
−
−
(I.18)
⇒
c
2
(see second equation of (
I.10
))
.
Note that for the proof of Lemma
I.4
, we have collected all constitutional items in (
I.10
)-(
I.18
).
Indeed, as soon as we represent the left principal stretches
Λ
1
=
Λ
2
=
Λ
S
accordingto(
I.3
) within
the left Airy distortion energy
J
l
A
, in particular (
I.9
), we are left with the quadratic polynomial
of (
I.11
) which constitutes the integrals of (
I.12
)and(
I.13
). First, the left principal stretch
Λ
S
has to be integrated over the area of interest. Second, the squared left principal stretch
Λ
S
has
to be integrated over the area of interest. In this way, we are led to the coecients
c
0
,c
1
,abd
c
2
of type (
I.14
). (
I.15
)-(
I.18
) describe the involved integrals which are computed by term-wise
integration of the uniformly convergent kernel series, namely by interchanging integration and
summation. The integral series expansions are of the order O(
E
6
)for(
I.16
)and(
I.18
).
Lemma I.5 (Minimal Airy distortion energy).
The Airy distortion energy (
I.9
) is minimal if the dilatation factor amounts to
ρ
=
c
1
/c
2
and
ρ
(
Φ
S
,Φ
N
)=
=
(
Φ
N
− Φ
S
)
1+
3
64
E
4
1+
15
16
E
2
E
2
(cos
Φ
N
sin
Φ
N
−
cos
Φ
S
sin
Φ
S
)
4
E
2
+
45
3
4
−
cos
Φ
S
sin
3
Φ
S
)
/
ln
tan
π
/
tan
π
15
4
+
Φ
N
4
+
Φ
S
32
E
4
(cos
Φ
N
sin
3
Φ
N
−
−
×
2
2
sin
3
Φ
S
)
+O(
E
6
)
,
1
(1 +
E
2
+
E
4
)
E
2
(1 +
E
2
)(sin
Φ
N
3
E
4
(sin
3
Φ
N
×
−
−
sin
Φ
S
)
−
−
(I.19)
ρ
(
Φ
S
=
−
Φ
N
)=
=
Φ
N
1+
3
64
E
4
1+
15
16
E
2
E
2
cos
Φ
N
sin
Φ
N
−
32
E
4
cos
Φ
N
sin
3
Φ
N
/
4
E
2
+
45
3
4
15
−
(1 +
E
2
+
E
4
)lntan
π
3
E
4
sin
3
Φ
N
+O(
E
6
)
.
4
+
Φ
N
1
E
2
(1 +
E
2
)sin
Φ
N
−
−
2
End of Lemma.
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