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CONTINUUM MECHANICS for ENGINEERS

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( )<br />

ˆn<br />

and because t = σjinj, we can convert the surface integral to a volume<br />

i<br />

integral having the integrand σji,j. By the use of Eq 5.3-11 on the left-hand<br />

side of Eq 5.4-2 we have, after collecting terms,<br />

( ρ ˙vi−σ ji,j −ρbi)<br />

dV = 0<br />

(5.4-3)<br />

where ˙v is the acceleration field of the body. Again, V is arbitrary and so the<br />

i<br />

integrand must vanish, and we obtain<br />

(5.4-4)<br />

which are known as the local equations of motion in Eulerian <strong>for</strong>m.<br />

When the velocity field is zero, or constant so that = 0, the equations<br />

of motion reduce to the equilibrium equations<br />

˙v i<br />

= 0 (5.4-5)<br />

which are important in solid mechanics, especially elastostatics.<br />

5.5 The Piola-Kirchhoff Stress Tensors,<br />

Lagrangian Equations of Motion<br />

∫<br />

V<br />

σ + ρb = ρv˙<br />

ji,j i i<br />

σ ρb<br />

+<br />

ji,j i<br />

As mentioned in the previous section, the equations of motion Eq 5.4-4 are<br />

in Eulerian <strong>for</strong>m. These equations may also be cast in the referential <strong>for</strong>m<br />

based upon the Piola-Kirchhoff tensor, which we now introduce.<br />

Recall that in Section 3.3 we defined the stress components σij of the<br />

t ( eˆ<br />

j )<br />

i<br />

n=e ˆ ˆj<br />

Cauchy stress tensor as the ith component of the stress vector acting<br />

on the material surface having the unit normal . Notice that this unit<br />

normal is defined in the current configuration. It is also possible to define a<br />

stress vector that is referred to a material surface in the reference configuration<br />

and from it construct a stress tensor that is associated with that configuration.<br />

In doing this, we parallel the development in Section 3.3 <strong>for</strong> the<br />

Cauchy stress tensor associated with the current configuration.<br />

Let the vector p be defined as the stress vector referred to the area<br />

element ∆S° in the plane perpendicular to the unit normal . Just<br />

as we defined the Cauchy stress vector in Eq 3.2-1, we write<br />

(N) o ˆ<br />

N= ˆ N Iˆ<br />

A A<br />

∆f<br />

df<br />

lim = =<br />

∆<br />

o o o<br />

∆S<br />

→0<br />

S dS<br />

( )<br />

o ˆ<br />

p N<br />

(5.5-1)

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