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CONTINUUM MECHANICS for ENGINEERS

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where dependence on I 3 has been included <strong>for</strong> subsequent algebra. Using<br />

the Cayley-Hamilton theorem in the <strong>for</strong>m<br />

results in<br />

(8.2-23)<br />

(8.2-24)<br />

∂<br />

Incompressibility requires I3 = 1 and<br />

∂<br />

. Furthermore, since the<br />

pressure term of the internal constraint stress is arbitrary, the first term of<br />

Eq 8.2-24 may be combined with the pressure term. The result is the following<br />

expression <strong>for</strong> the Cauchy stress<br />

=<br />

W<br />

I<br />

0<br />

3<br />

or<br />

ˆσ = γ δ + γ B + γ B B<br />

ij o ij 1 ij 2 ik jk<br />

( ) + ( − )<br />

−1<br />

= γ IB + γ −γ<br />

I δ γ γ I B<br />

2 3 ij o 2 2 ij 1 2 1 ij<br />

ˆσ<br />

W<br />

I I δ<br />

I<br />

W W W<br />

B I<br />

I I I B<br />

⎛ ∂ ∂ ⎞<br />

= ⎜ −<br />

⎝ ∂ ∂<br />

⎟ +<br />

⎠<br />

∂ ∂<br />

3 2<br />

+ 3<br />

∂ ∂<br />

ij ij ij<br />

−1<br />

ij<br />

3<br />

2 1<br />

2<br />

W<br />

σ pδ<br />

I B<br />

W<br />

I B<br />

=− +∂ +<br />

∂<br />

∂<br />

ij ij<br />

1<br />

ij<br />

∂ 2<br />

−1<br />

ij<br />

W<br />

σ pδ<br />

I B<br />

W<br />

I c<br />

=− +∂ +<br />

∂<br />

∂<br />

∂<br />

ij ij ij ij<br />

1 2<br />

(8.2-25)<br />

(8.2.26)<br />

where c ij is defined in Eq 4.6-16.<br />

At this point, the strain energy has been assumed a function of I 1 and I 2,<br />

but the exact functional <strong>for</strong>m has not been specified. Rivlin (1948) postulated<br />

the strain energy should be represented as a general polynomial in I 1 and I 2<br />

∑ αβ<br />

( ) ( − )<br />

W = C I −3<br />

I 3<br />

1 2<br />

α β<br />

(8.2-27)<br />

It is noted that the strain energy is written in terms of I 1 –3 and I 2 – 3 rather<br />

than I 1 and I 2 to ensure zero strain corresponds to zero strain energy.<br />

Depending on the type of material and de<strong>for</strong>mation, that is, experimental<br />

test data, the number of terms used in Eq 8.2-27 is chosen. For instance,<br />

choosing C 10 = G and all other coefficients zero results in a neo-Hookean<br />

response where G is the shear modulus. Stresses are evaluated with Eq 8.2-26<br />

and used in the equations of motion, Eq 5.4-4. This results in a set of differential<br />

equations solved with the use of the problem’s appropriate boundary

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