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CONTINUUM MECHANICS for ENGINEERS

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Note that if principal axes of B ij are chosen the invariants of Eq 8.2-2 are<br />

written in terms of the stretch ratios λ 1, λ 2, and λ 3 as follows:<br />

(8.2-3)<br />

Many rubber or elastomeric materials have a mechanical response that is<br />

often nearly incompressible. Even though a perfectly incompressible material<br />

is not possible, a variety of problems can be solved by assuming incompressibility.<br />

The incompressible response of the material can be thought of as<br />

a constraint on the de<strong>for</strong>mation gradient. That is, the incompressible nature<br />

of the material is modeled by an addition functional dependence between<br />

the de<strong>for</strong>mation gradient components. For an incompressible material the<br />

density remains constant. This was expressed in Section 5.3 by v i,i = 0<br />

(Eq 5.3-8) or ρJ = ρ o (Eq 5.3-10a). With the density remaining constant and<br />

Eq 5.3-10a as the expression of the continuity equation it is clear that<br />

(8.2-4)<br />

For the time, regress from specific incompressibility conditions to a more<br />

general case of a continuum with an internal constraint. Assume a general<br />

constraint of the <strong>for</strong>m<br />

or, since C AB = F iAF iB,<br />

I<br />

2<br />

1 1<br />

I<br />

2 2<br />

2 1 2<br />

I<br />

= λ + λ + λ<br />

2<br />

2<br />

2 2 2<br />

3 1 2 3<br />

(8.2-5)<br />

(8.2-6)<br />

This second <strong>for</strong>m of the internal constraint has the advantage that it is invariant<br />

under superposed rigid body motions. Differentiation of φ results in<br />

(8.2-7)<br />

where it is understood partial differentiation with respect to a symmetric<br />

tensor results in a symmetric tensor. That is,<br />

2<br />

3<br />

= λλ + λλ + λλ<br />

= λλλ<br />

2 2<br />

2 3<br />

J = det{ FiA}= 1<br />

φ F ( iA)=<br />

0<br />

˜ φ( CAB)= 0<br />

2 2<br />

1 3<br />

( iA iB iA iB)<br />

∂<br />

=<br />

∂<br />

∂ φ φ<br />

+<br />

C ∂<br />

C˙<br />

F˙ AB F F F˙<br />

C<br />

AB<br />

AB<br />

∂ ∂<br />

≡ +<br />

∂ ∂<br />

∂<br />

φ 1 ⎛ φ φ ⎞<br />

C 2<br />

⎜<br />

⎝ C ∂C<br />

⎟<br />

⎠<br />

AB AB BA<br />

(8.2-8)

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