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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 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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