Biomedical Engineering Reference
In-Depth Information
Anisotropic H OOKE 's Law. In identifying material parameters of anisotropic
(aircraft seat) fabric materials in Sect. 4.2.2.2 , the H OOKE model for orthotropic
materials is shown to be applicable and is thus treated as a special case. Equations
( 3.98 ) and ( 3.276 ) provide a relation between the C AUCHY stress tensor and the
second P IOLA -K IRCHHOFF stress tensor in the following form
F T :
ð 4 Þ
S ¼ J 1 F P II F T ¼ J 1 F C
G
ð 3 : 284 Þ
= 2 according to ( 3.284 ) leads
Considering ( 3.57 ) 1 and G ¼ H þ H T þ H T H
to
I þ H
S ¼ 1
2
1
det I þ H
ð 4 Þ
Þ T : ð 3 : 285 Þ
H þ H T þ H T H
Þ I þ H
ð
Þ C
ð
ð
Factoring out the terms in ( 3.285 ) yields
þ O H T H
ð 4 Þ
S ¼ 1
2
1
det I þ H
H þ H T þ H T H
Þ C
ð 3 : 286 Þ
ð
where terms of higher order in the displacement gradient H are summed up by the
term O H T H .
A consequent geometrical linearization (also shown at the end of Sect. 3.2.3.6 )
includes the elimination of the quadratic term H T H in square brackets in ( 3.286 )
as well as reducing the denominator to det I ¼ 1 (this can be realized by writing
det I þ ð Þ in coordinate notation). Considering ( 3.77 ), the most general strictly-
linear relation between the C AUCHY stress tensor S and the deformator E for
arbitrary anisotropic material behaviour results in:
ð 4 Þ
S ¼ C
E :
ð 3 : 287 Þ
Based on the approach outlined following Eq. ( 3.276 ), this constitutive equation
structure for orthotropy between S and E results from ( 3.287 ) (analogue to ( 3.281 ))
S ¼ u 1 trM 1 E þ u 2 trM 2 E þ u 3 trM 3 ð Þ M 1
þ u 2 trM 1 E þ u 4 trM 2 E þ u 5 trM 3 E
ð
Þ M 2
þ u 3 trM 1 E þ u 5 trM 2 E þ u 6 trM 3 E
ð
Þ M 3
þ u 7 M 1 E M 2 þ M 2 E M 1
ð
Þþ u 8 M 1 E M 3 þ M 3 E M 1
ð
Þ
þ u 9 M 2 E M 3 þ M 3 E M 2
ð
Þ:
ð 3 : 288 Þ
Considering ( 3.78 ), ( 3.219 ) and ( 3.220 ) as well as trM a E ¼ e aa ; M a E
M b ¼ e ab e a e b (a and b not summed!), r ij ¼ r ji and e ij ¼ e ji ,Eq.( 3.288 ) leads to
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