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CONTINUUM MECHANICS for ENGINEERS

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Stress Tensor<br />

The quantities σ ji ti are the components of a second-order tensor known<br />

as the stress tensor. This is shown by considering the trans<strong>for</strong>mation of the<br />

components of the stress vector between coordinate systems Px1 x2 x3 and<br />

as given by the trans<strong>for</strong>mation matrix having elements (see Section 2.5)<br />

j<br />

≡ ( ê )<br />

t<br />

( ˆn )<br />

i<br />

Px′ x′ x′<br />

1 2 3<br />

(3.3-9)<br />

Since t can be expressed in terms of its components in either coordinate<br />

system,<br />

(3.3-10a)<br />

nˆ ( )<br />

ˆ ˆ ˆ<br />

t<br />

( n) n n<br />

=<br />

( ) ′<br />

t eˆ = t<br />

( )<br />

eˆ′<br />

or, from Eq 3.3-8,<br />

aij = e′ i ⋅ej<br />

(3.3-10b)<br />

But from Eq 2.5-2, eˆ′ ˆ i = aijej<br />

and from Eq 2.5-9, n′ j = ajsns, so that now<br />

Eq 3.3-10b becomes, after some manipulations of the summed indices,<br />

(3.3-11)<br />

Because the vectors are linearly independent and since Eq 3.3-11 must be<br />

valid <strong>for</strong> all vectors ns, we see that<br />

êr (3.3-12)<br />

But this is the trans<strong>for</strong>mation equation <strong>for</strong> a second-order tensor, and thus by<br />

Eq 2.5-12 the tensor character of the stress components is clearly established.<br />

The Cauchy stress <strong>for</strong>mula given by Eq 3.3-8 expresses the stress vector<br />

associated with the element of area having an outward normal n i at point P<br />

in terms of the stress tensor components σ ji at that point. And although the<br />

state of stress at P has been described as the totality of pairs of the associated<br />

normal and traction vectors at that point, we see from the analysis of the<br />

tetrahedron element that if we know the stress vectors on the three coordinate<br />

planes of any Cartesian system at P, or equivalently, the nine stress<br />

tensor components σ ji at that point, we can determine the stress vector <strong>for</strong><br />

any plane at that point. For computational purposes it is often convenient<br />

to express Eq 3.3-8 in the matrix <strong>for</strong>m<br />

ˆ ˆ<br />

i i i i<br />

t<br />

( nˆ )<br />

= σ neˆ = σ′<br />

n′<br />

eˆ<br />

ji j i ji j i<br />

( σsr − ajsairσ′ ji) nsêr=<br />

0<br />

σsr =ajsa irσ′ ji

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